# TCDS T00001SE: The Boeing Company - Type: Type certificate data sheet - Status: Current - Holder: The Boeing Company - Revision: 48 - Revised: September 5, 2025 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Registered aircraft: 280, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/f0/4e/f04e68d92e20ae54a821e30398f06dd5525bb351d631b003dcf6be20d24c1812 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174046058620250908140952.0001 - Page: https://openairdocs.org/tcds/T00001SE ## Models (5) As the data sheet lists them. - 777-300ER Series - 777-200 Series - 777-200LR Series - 777F Series - 777-300 Series ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. T00001SE This data sheet, which is part of Type Certificate No. T00001SE, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: The Boeing Company 737 Logan Ave N Renton, WA 98057-0000 I - Model 777-200 Series (Transport Category) Approved April 19, 1995 Engines: 2 Pratt and Whitney Turbofan Model: PW4074, PW4074D, PW4077, PW4077D, PW4090, PW4084D, and PW4090-3 (Engine Type Certificate No. E46NE) 2 General Electric Turbofan Model: GE90-76B, GE90-85B, GE90-90B, GE90-94B (Engine Type Certificate No. E00049EN) 2 Rolls-Royce Turbofan Model: RB211-Trent 875-17, RB211-Trent, 877-17, RB211-Trent 884-17, RB211-Trent 892-17, or RB211 Trent 892B-17, RB211 Trent 895-17 (Engine Type Certificate E00050EN) Authorization for engine intermix is contained in the appropriate FAA approved Airplane Flight Manual. Fuel: Pratt and Whitney Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8 are acceptable. Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of P&W Service Bulletin 2016. General Electric Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of GE Aviation Turbine Fuels Specification D50TF2. Rolls-Royce Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 48 44 42 48 48 38 48 48 48 47 47 48 48 47 48 48 48 39 48 48 Page No. 21 22 23 Rev. No. 48 41 43 T00001SE Revision 48 BOEING 777-200 Series 777-300 Series 777-300ER Series 777-200LR Series 777F Series September 5, 2025 T00001SE 2 I. Model 777-200 (cont’d): Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the relevant Engine Operating Instructions. Engine Ratings & Operating Limits: Pratt & Whitney Engines: See the FAA approved Flight Manual for engine ratings and operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. General Electric Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Rolls-Royce Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Airspeed Limits: VMO/MMO = 330KIAS/.87M. For other airspeed limits, see the appropriate FAA approved Airplane Flight Manual. CG Range: See the appropriate FAA approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA approved Airplane Flight Manual. Model Eligible Serial Numbers 777-206 28691, 29397-29399, 32704, 32705, 32720, 32721, 33711-33714, 34711, 34712, 35295 777-212 28507-28514, 28518-28527, 28529-28533, 28998, 28999, 30866-30875, 32316, 32318, 32320, 32321, 32334-32336, 33368-33373 777-219 29401, 29403, 29404, 32712, 34376-34379 777-222 26916-26919, 26921, 26924-26948, 26950, 26951, 26953, 26954, 28713, 28714, 30212-30226, 30549-30557 777-223 29578-29588, 29955, 29956, 30003-30005, 30010-30012, 30250-30264, 30796, 30797-30798, 31477- 31479, 32636-32638, 32879, 32880, 33539, 33540 777-224 27577-27581, 28678, 28679, 29476-29480, 29859-29862, 31679, 31680, 31687, 35547, 39776, 39777 777-228 27609, 28675, 28682-28684, 29002-29011, 30456-30457, 30614-30615, 32305, 32306, 32308- 32311, 32698 777-232 29734-29738, 29743, 29951, 29952 777-236 27105-27109, 27483-27493, 28840, 28841, 29319-29323, 29962-29967, 30302-30317, 36516- 36519 777-240 33775-33777, 35296 777-243 32781-32784, 32855-32860 777-246 27364-27366, 27651-27653, 27656, 27657, 32889-32896, 33394-33396 777-258 30831-30833, 33169, 36083, 36084 777-266 28423-28425, 32629, 32630 777-267 27263-27266, 27116 777-268 28344-28366 777-269 28743, 28744 777-281 27027-27037, 27938, 28276-28279, 29029, 32646, 32647, 33406, 33407, 33414, 33415, 40900- 40904 777-289 27636-27642 777-21B 27357-27360, 27524, 27525, 27604-27606, 32703 777-21H 27247-27253, 29324, 29325 777-24Q 29271 777-26K 33502-33505 777-28E 28681, 28685, 28686, 29171, 29174, 29175, 30859-30862, 35525, 40198, 40199 777-2AN 29953, 29956 777-2B5 27945-27947, 27949, 27951, 28372, 28444, 28445, 33727, 34206-34214 777-2D7 27726-27733, 34586-34591 777-2H6 28408-28422, 29065, 29066 777-2J6 29153-29157, 29744-29748 777-2M2 34565-34567 3 T00001SE I. Model 777-200 (cont’d): 777-2Q8 27607, 27608, 28676, 28688, 28689, 28692, 29402, 29908, 32701, 32716-32719 777-2U8 33681-33683, 36124 777-2Z9 28698, 28699, 29313, 35960 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot Maximum Passengers: 440 Maximum Baggage/Cargo: See appropriate FAA approved Weight and Balance Manual. Fuel and Oil Capacities: See appropriate FAA approved Weight and Balance Manual. Certification Basis: A. 14 CFR part 25 of the Federal Aviation Regulations: Amendment 25-1 through 25-82, except for: §25.571(e)(1) which remains at amendment 25-71 level. §25.1457 at amendment 25-124 applicable to Line Number 858 and on. §25.1459 at amendment 25-124 applicable to Line Number 858 and on. Optional Design Regulations: Ditching: §25.801, 25.1411(d), (e), (f), (g) and 25.1415 Ice Protection: §25.1419 14 CFR part 26: Based on 14 CFR §21.101(g) for changes made to TCs applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections Compliance has been found for the following regulations at Amendment 26-0: §26.11 Compliance has been found for the following regulations at Amendment 26-1: §26.43, 26.45, 26.47, and 26.49 Compliance has been found for the following regulations at Amendment 26-3: §26.33 and §26.39 Compliance has been found for the following regulations at Amendment 26-6: §26.21 In addition to 14 CFR part 25 of FARs, the type certification basis for the Model 777-200 airplane includes compliance with the emissions standards of 14 CFR part 34, Amendment 34-1 through 34- 3, and with the noise standards of 14 CFR part 36, Amendment 36-1 through 36-28. Exemptions from 14 CFR part 25: 1. Floor Warpage for Flight Deck Seats Exemption from 14 CFR 25.562(b)(2). (Exemption No. 5436, April 1, 1992). 2. Partial Exemption from 14 CFR 25.1435(b)(1), Hydraulic Proof Pressure Test. (Exemptions No. 5758, Oct. 1, 1993 and No. 5758A, Oct. 29, 1993). 3. Partial Exemption from 14 CFR 25.901(c), No single powerplant or auxiliary power unit failure will jeopardize the safe operation of the airplane. (Exemption No. 7955, January 17, 2003) See Note 8 4. Partial Time-Limited Exemption from 14 CFR §25.853(a), appendix F, paragraph (a)(1)(i), Testing on Large Interior Panels, granted through November 28, 2011. (Exemption No. 9791, November 28, 2008, Exemption No. 9791B, March 1, 2010 , Exemption No. 9791C, February 4, 2011) 5. Partial Time Limited Exemption from 14 CFR 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.613, 25.901(b)(2), 25.901(c), 25.1103(d), 25.1191, and 25.1301(d), Thrust reverser inner wall damage and pneumatic duct failures on all Rolls Royce engine powered 777 series aircraft production line numbers 1 through 796, granted through October 27, 2015. (Exemption No. 9949, October 27, 2009) 6. Time-Limited Exemption from 14 CFR 25.1535 as specified in Appendix K, §K25.1.4(a)(3) as the regulation applies to low-fuel alerting for approval extended operations (ETOPS) beyond 180 minutes, granted through January 11, 2015 (Exemption No. 10193, January 11, 2011) (Exemption No. 10193A, December 17, 2013) 7. Time-Limited Exemption from 14 CFR 25.901(c), Amendment 25-126 and 25.981(a)(3), Amendment 25-125, as they pertain to fuel-tank-ignition prevention associated with the FQIS, limited to design changes within the FQPU in support of parts obsolescence, for in-service Model 777-200 and -300 series airplanes prior to line number 562. (Exemption No. 10922, January 31, 2014) T00001SE 4 I. Model 777-200 (cont’d): 8. Time-Limited Exemption from 14 CFR §§25.901(c) and 25.903(c), Appendix K, §K25.1.1 to part 25, and item 6 of Special Conditions 25-ANM-78 pertaining to an engine fan blade for airplanes equipped with PW4000-112 engines through March 4, 2027 for production, and March 4, 2028 for the fleet. (Exemption No. 19032, March 4, 2022) Equivalent Safety Findings exist with respect to the following regulations: 14 CFR §25.125(a)(2) and §25.149 - Landing Minimum Control Speed. 14 CFR 25.331(d), 25.333, 25.335(d), 25.341, 25.345, 25.349(b), 25.351(b), 25.371, 25.373, 25.391, and 25.427 - Design Gust Criteria. 14 CFR 25.365(g)- Pressurized Compartment Loads (documented in ELOS Memo PS14-0508-A-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS09-0445-CS-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS13-0075-C-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - for Single Occupant Side-Facing Seats.(documented in ELOS Memo PS13-0216-C-1) 14 CFR 25.562(b)(2) - Emergency Landing Dynamic Conditions 14 CFR 25.785(f)(3) - for Flexible Interior Items Track Mounted 1.33 Fitting Factor. 14 CFR 25.791(a) and FAR 25.853(d) – “No Smoking” Limitation in the passenger compartment 14 CFR 25.803(c) - for Inoperative Floor Proximity Light System during the Full Scale Evacuation Demonstration. 14 CFR 25.811 - Exterior Exit Markings 14 CFR 25.811(f) - Door sill reflectance 14 CFR 25.813(e) – Doors between passenger compartments (documented in Transport Airplane Directorate ELOS Memo PS05-0272-C-1) 14 CFR 25.819 - Lower Lobe Attendant Rest (LLAR) 14 CFR 25.853(a) – Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08-0670-C-1) 14 CFR 25.853(a) and (d) Compartment Interiors (Documented in TAD ELOS Memorandum PS13- 1000-C-5) 14 CFR 25.869(a)(4) - for Fiber Optic Cables used in the Model 777. 14 CFR 25.933(a)(1)(ii) - Inflight Thrust Reverser Deployment Demonstration. 14 CFR 25.981, Amdt 25-125 - Fuel tank ignition prevention (see Note 12) 14 CFR part 25.981, Amdt 25-125 - for the Fuel Tank Flammability Rule (FTFR). (documented in ELOS Memo PS05-0177-P-2) 14 CFR 25.1182(a) and 25.1183(a) - for Fire Resistant Requirement for Hydraulic Components Located in the Strut Aft Fairing. 14 CFR 25.1183(a) - Fire Resistance of Power Door Opening System on Engine Compartments (GE Engines) 14 CFR 25.1303(c)(1) - Overspeed Aural Warning. 14 CFR 25.1305(c)(7) - Warning Means for Engine Oil Filter Indication Contamination. (PW engines only) 14 CFR 25.1351(b)(5) - Flight Controls DC Power 14 CFR 25.1387(b) & (c) - for Forward Position Lights. 14 CFR 25.1389(b)(3) – Red and Green Position Lights - Aft Lamps Only 14 CFR 25.1441(c) Crew Determination of the Quantity of Oxygen Available in the Lavatory Passenger Service Units Bottles (documented in ELOS Memo PS13-0901-ES-1) 14 CFR 25.1443(c) Determination of Minimum Oxygen Flow for the Lavatory Oxygen System (documented in TAD ELOS Memo TS13-0005-S-1) 14 CFR 25.1459(a)(2) - for Flight Data Recorder Accelerometers. 14 CFR 25.1529, 25.1729 - Inclusion of Airworthiness Limitations within the Boeing ICA manuals (Documented in TAD ELOS Memo TC6918SE-T-G-8) 14 CFR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments (Documented in TAD ELOS Memorandum AT00010BA-T-S-1) Equivalent Safety Findings exist with respect to the following regulations (cont’d): 14 CFR 25.1555(d)(1) Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (documented in ELOS Memo PS06-0496-F-18) 14 CFR 25. (several sections) Use of 1g Speed Instead of Minimum Speed in the Stall as a Basis for Compliance. (All 14 CFR 25 Sections, except structural, dealing with stall speeds/related factors for turbojet airplanes) Special Conditions with respect to the following subjects apply to the Model 777-200: Special Conditions No. 25-ANM-78, effective on December 10 1993, addressed the following issues: 1. Operation without Normal Electrical Power 2. Integrated Command Signal Integrity 3. Protection from Lightning and High-Intensity Radiated Fields Protection 5 T00001SE I. Model 777-200 (cont’d): 4. Effect of Flight Control Systems on Structure 5. Design Maneuver Requirements 6. Limit Engine Torque Loads for Sudden Engine Stoppage 7. Flight Characteristics Compliance via Handling Qualities Rating Method 8. Electronic Flight Control System - Control Surface Awareness Note: (Special Conditions on lightning are no longer part of the Type Certificate as a result of Boeing's voluntary compliance with Amendment 25 -80 which resulted in issuance of 14 CFR 25.1316, "System Lightning Protection"). Special Conditions No. 25-ANM-84A, effective on October 8 2003, addressed airplane type design approval for Extended Range Operation With Two-Engine Airplanes (ETOPS). Special Conditions No. 25-07-12-SC, effective on June 1, 2007, Lithium Ion Battery installation Special Conditions No. 25-141-SC, effective on December 7, 1998, Seats With Articulating Seat Backs Special Conditions No. 25-187A-SC, effective on October 29, 2004, addressed seats with inflatable lapbelts. Special Conditions No. 25-192-SC, effective on November 6, 2001, addressed Overhead Crew Rest Compartments. Special Conditions No. 25-230-SC, effective on April 9, 2003, addressed Overhead Crew Rest Compartments Special Conditions No. 25-260-SC, effective on April 14, 2004, addressed the Overhead Crew Rest Compartment Occupiable During Taxi, Take-off, and Landing Special Conditions No. 25-295-SC, effective on August 9, 2005, Side-Facing Single-Occupant Seats equipped with inflatable lapbelts Special conditions No. 25-336-SC, effective on November 15, 2006. addressed overhead cross aisle stowage compartments Special Conditions No. 25-367-SC, effective on February 7, 2008, addressed Seats With Non- Traditional, Large, Non-Metallic Panels Special Conditions No. 25-503-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized Internal Access Special Conditions No. 25-504-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized External Access Special Conditions No. 25-621B-SC, effective on October 22, 2018, addressed Single Occupant Oblique (Side-Facing) Seats Special Conditions No. 25-687-SC, effective to design changes applied for after May 31, 2017, addressed Non-Rechargeable Lithium Batteries. See the applicability section of these special conditions for more information on which design changes must meet them. Special Conditions No. 25-758-SC, effective on December 2, 2019, addressed Seats with Inertia Locking Devices Special Conditions No. 25-769-SC, effective on August 10, 2020, addressed Dynamic Test Requirements for Single- Occupant Oblique Seats With Pretensioner Restraint Systems Special Conditions No. 25-841-SC, effective on November 24, 2023, addressed Seats with Pretensioner Restraint Systems II - Model 777-300 Series (Transport Category) Approved May 4, 1998 Engines: 2 Rolls-Royce Turbofan Model: RB211-Trent 884-17, RB211-Trent 884B-17, or RB211-Trent 892- 17 (Engine Type Certificate E00050EN) 2 Pratt & Whitney Turbofan Model: PW4090, PW4098 (Engine Type Certificate E46NE) Fuel: Rolls-Royce Engines: Fuel conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the relevant Engine Operating Instructions. Fuel (cont’d): Pratt & Whitney Engines: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8 are acceptable. Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of P&W Service Bulletin 2016. T00001SE 6 II. 777-300 (cont’d): Engine Ratings & Operating Limits: Rolls-Royce Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Pratt & Whitney Engines: See the FAA approved Flight Manual for engine ratings and operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Airspeed Limits: VMO/MMO = 330KIAS/.89M. For other airspeed limits, see the appropriate FAA approved Airplane Flight Manual. CG Range: See the appropriate FAA approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA approved Airplane Flight Manual. Model Eligible Serial Numbers 777-312 28515-29517, 28528, 28531, 28534, 30868, 32317, 32327, 33374-33376 777-346 27654, 27655, 28393-28397 777-367 27504-27510, 33702-33704, 34243, 34244 777-381 27039, 27040, 27939, 28272-28275 777-3B5 27948, 27950, 27952, 28371 777-3D7 29150, 29151, 29211-29214 777-31H 28680, 28687, 29062-29064, 29067, 29395-29397, 32697, 32699, 32700, 32702 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot. One flight attendant is required at each door no. 3 overwing exit. Maximum Passengers: 550 For passenger capacity above 500, an 11th flight attendant is required at door 3 exit. Maximum Baggage/Cargo: See appropriate Weight and Balance Manual. Fuel and Oil Capacities: See appropriate Weight and Balance Manual. Minimum Required Fuel: See appropriate FAA approved Airplane Flight Manual. Maximum Operating Altitude: 43,100 feet Certification Basis: A. Part 25 of the Federal Aviation Regulations: Amendment 25-1 through 25-86, except for 14 CFR 25.201 which remains at Amendment 25-83, 14 CFR 25.203 which remains at Amendment 25-83, 14 CFR 25.571(e)(1), which remains at Amendment 25-71 (remains from 777-200 certification basis), 14 CFR 25.335(d) which remains at Amendment 25-85, 14 CFR 25.853(d)(3), which remains at Amendment 25-82, 14 CFR 25.1457, which is at Amendment 25-124 applicable to Line Number 858 and on, 14 CFR 25.1459, which is at Amendment 25-124 applicable to Line Number 858 and on. 14 CFR part 26: Based on 14 CFR §21.101(g) for changes made to TCs applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections Compliance has been found for the following regulations at Amendment 26-0§26.11 Compliance has been found for the following regulations at Amendment 26-1: §26.43, 26.45, 26.47, and 26.49 Compliance has been found for the following regulations at Amendment 26-3: §26.33 and §26.39 Compliance has been found for the following regulations at Amendment 26-6: §26.21 14 CFR part 34 of the Federal Aviation Regulations: Amendment 34-1. 7 T00001SE II. 777-300 (cont’d): 14 CFR part 36 of the Federal Aviation Regulations: Amendment 36-1 through 36-20 Optional Design Regulations: Ditching: 14 CFR 25.801, 25.1411(d), (e), (f), (g) and 25.1415 Ice Protection: 14 CFR 25.1419 Exemptions from 14 CFR part 25: 1. Floor Warpage for Flight Deck Seats Exemption from 14 CFR 25.562(b)(2) (Exemption No. 5436, April 1, 1992 and No. 5436A, January 3, 1997). 2. Partial Exemption from 14 CFR 25.1435(b)(1), Hydraulic Proof Pressure Test. (Exemptions No. 6504, September 3, 1996). 3. Partial Exemption from 14 CFR 25.901(c), No single powerplant or auxiliary power unit failure will jeopardize the safe operation of the airplane. (Exemption No. 7955, January 17, 2003) See Note 8. 4. Partial Time-Limited Exemption from 14 CFR §25.853(a), appendix F, paragraph (a)(1)(i), Testing on Large Interior Panels, granted through November 28, 2011. (Exemption No. 9791, November 28, 2008, Exemption No. 9791B, March 1, 2010 , Exemption No. 9791C, February 4, 2011) 5. Partial Time Limited Exemption from 14 CFR 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.613, 25.901(b)(2), 25.901(c), 25.1103(d), 25.1191, and 25.1301(d), Thrust reverser inner wall damage and pneumatic duct failures on all Rolls Royce powered 777 series aircraft production line numbers 1 through 796, granted through October 27, 2015. (Exemption No. 9949, Oct 27, 2009) 6. Time-Limited Exemption from 14 CFR 25.901(c), Amendment 25-126, and 25.981(a)(3), Amendment 25-125, as they pertain to fuel-tank-ignition prevention associated with the FQIS, limited to design changes within the FQPU in support of parts obsolescence, for in-service Model 777-200 and -300 series airplanes prior to line number 562. (Exemption No. 10922, January 31, 2014) 7. Time-Limited Exemption from 14 CFR §§25.901(c) and 25.903(c), Appendix K, §K25.1.1 to part 25, and item 6 of Special Conditions 25-ANM-78 pertaining to an engine fan blade for airplanes equipped with PW4000-112 engines through March 4, 2027 for production, and March 4, 2028 for the fleet. (Exemption No. 19032, March 4, 2022) Equivalent Safety Findings exist with respect to the following regulations: 14 CFR 25.201 – Stall Demonstration (documented in TAD ELOS Memo AT3908SE-T-F-8) 14 CFR 25.201(d) – Stall identification/characteristics (documented in TAD ELOS Memo AT3907SE-T-F-8) 14 CFR 25.203 – Stall Characteristics (documented in TAD ELOS Memo AT3908SE-T-F-8) 14 CFR 25.203(a) – Stall identification/characteristics (documented in TAD ELOS Memo AT3907SE-T-F-8) 14 CFR 25.331(d), 25.333, 25.341, 25.345, 25.349(b), 25.351(b), 25.371, 25.373, 25.391, and 25.427 - Design Gust Criteria. 14 CFR 25.365(g)- Pressurized Compartment Loads (documented in ELOS Memo PS14-0508-A-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS09-0445-CS-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS13-0075-C-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - for Single Occupant Side-Facing Seats.(documented in ELOS Memo PS13-0216-C-1) 14 CFR 25.785(f)(3) - for Flexible Interior Items Track Mounted 1.33 Fitting Factor. 14 CFR 25.791(a) and 14 CFR 25.853(d) – “No Smoking” Limitation in the passenger compartment 14 CFR 25.803(c) – Inoperative Floor Proximity Light System during Full Scale Evacuation Demonstration 14 CFR 25.807(g) – Emergency Exits, Type and Number Required 14 CFR 25.810 - Off-wing Escape System/Bottle Loss During Landing Gear Collapse 14 CFR 25.811(f) - Door Sill Reflectance 14 CFR 25.811(f) - Exterior Exit Marking 14 CFR 25.813(e) – Doors between passenger compartments (documented in Transport Airplane Directorate ELOS Memo PS05-0272-C-1) 14 CFR 25.853(a) – Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08-0670-C-1) 14 CFR 25.853(a) and (d) Compartment Interiors (Documented in TAD ELOS Memorandum PS13- 1000-C-5) 14 CFR 25.869(a)(4) - for Fiber Optic Cables used in the Model 777. 14 CFR 25.933(a)(1)(ii) - Inflight Thrust Reverser Deployment Demonstration. 14 CFR 25.981, Amdt 25-125 - Fuel tank ignition prevention (see Note 12) T00001SE 8 II. 777-300 (cont’d): 14 CFR part 25.981, Amdt 25-125 - for the Fuel Tank Flammability Rule (FTFR). (documented in ELOS Memo PS05-0177-P-2) 14 CFR 25.1182(a) and 25.1183(a) - for Fire Resistant Requirement for Hydraulic Components Located in the Strut Aft Fairing. 14 CFR 25.1303(c)(1) - Overspeed Aural Warning. 14 CFR 25.1305 and 25.1501(b) - APU Instrumentation and Monitoring Requirements. 14 CFR 25.1305(c) (7) - Warning Means for Engine Oil Filter Indication Contamination. 14 CFR 25.1351(b)(5) - for Flight Controls DC Power. 14 CFR 25.1387(b) & (c) - for Forward Position Lights. 14 CFR 25.1389(b)(3) - for Red and Green Position Lights, Aft Lamps Only. 14 CFR 25.1441(c) Crew Determination of the Quantity of Oxygen Available in the Lavatory Passenger Service Units Bottles (documented in ELOS Memo PS13-0901-ES-1) 14 CFR 25.1443(c) Determination of Minimum Oxygen Flow for the Lavatory Oxygen System (documented in TAD ELOS Memo TS13-0005-S-1) 14 CFR 25.1459(a)(2) - for Flight Data Recorder Accelerometers. 14 CFR 25.1529, 25.1729 - Inclusion of Airworthiness Limitations within the Boeing ICA manuals (Documented in TAD ELOS Memo TC6918SE-T-G-8) 14 CFR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments (Documented in TAD ELOS Memorandum AT00010BA-T-S-1) 14 CFR 25.1555(d)(1) Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (documented in ELOS Memo PS06-0496-F-18) 14 CFR 25. (several sections) Use of 1g Speed Instead of Minimum Speed in the Stall as a Basis for Compliance. (All 14 CFR 25 Sections, except structural, dealing with stall speeds/related factors for turbojet airplanes). Special Conditions with respect to the following subjects apply to the Model 777-300: Special Conditions No. 25-ANM-78, effective December 10, 1993, addressed the following issues: 1. Operation without Normal Electrical Power 2. Integrated Command Signal Integrity 3. Protection from Lightning and High-Intensity Radiated Fields Protection 4. Effect of Flight Control Systems on Structure 5. Design Maneuver Requirements 6. Limit Engine Torque Loads for Sudden Engine Stoppage 7. Flight Characteristics Compliance via Handling Qualities Rating Method 8. Electronic Flight Control System - Control Surface Awareness Note: (Special Conditions on lightning are no longer part of the Type Certificate as a result of Boeing’s voluntary compliance with Amendment 25-80 which resulted in issuance of 25.1316, “System Lightning Protection”). Special Conditions No. 25-ANM-84A, effective on October 8, 2003, addressed airplane type design approval for Extended Range Operation With Two-Engine Airplanes (ETOPS). Special Conditions No. 25-07-12-SC, effective on June 1, 2007, Lithium Ion Battery installation Special Conditions No. 25-141-SC, effective on December 7, 1998, Seats With Articulating Seat Backs Special Conditions No. 25-187A-SC, effective on October 29, 2004, addressed seats with inflatable lapbelts. Special Conditions No. 25-230-SC, effective on April 9, 2003, addressed Overhead Crew Rest Compartments Special Conditions No. 25-260-SC, effective on April 14, 2004, addressed the Overhead Crew Rest Compartment Occupiable During Taxi, Take-off, and Landing Special Conditions No. 25-295-SC, effective on August 9, 2005, Side-Facing Single-Occupant Seats equipped with inflatable lapbelts Special conditions No. 25-336-SC, effective on November 15, 2006. addressed overhead cross aisle stowage compartments Special Conditions No. 25-367-SC, effective on February 7, 2008, addressed Seats With Non- Traditional, Large, Non-Metallic Panels Special Conditions No. 25-503-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized Internal External Access Special Conditions No. 25-504-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized External Access Special Conditions No. 25-621B-SC, effective on October 22, 2018, addressed Single Occupant Oblique (Side-Facing) Seats Special Conditions No. 25-687-SC, effective to design changes applied for after May 31, 2017, addressed Non-Rechargeable Lithium Batteries. See the applicability section of these special conditions for more information on which design changes must meet them. 9 T00001SE II. 777-300 (cont’d): Special Conditions No. 25-758-SC, effective on December 2, 2019, addressed Seats with Inertia Locking Devices Special Conditions No. 25-769-SC, effective on August 10, 2020, addressed Dynamic Test Requirements for Single-Occupant Oblique Seats With Pretensioner Restraint Systems Special Conditions No. 25-841-SC, effective on November 24, 2023, addressed Seats with Pretensioner Restraint Systems III - Model 777-300ER Series (Transport Category) Approved March 16, 2004 Engines: 2 General Electric Turbofan Model: GE90-115B (Engine Type Certificate No. E00049EN) Fuel: General Electric Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of GE Aviation Turbine Fuels Specification D50TF2. Engine Ratings & Operating Limits: General Electric Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual Airspeed Limits: VMO/MMO = 330KEAS/.89M. For other airspeed limits, see the appropriate FAA approved Airplane Flight Manual. CG Range: See the appropriate FAA approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA approved Airplane Flight Manual. Model Eligible Serial Numbers 777-306ER 35671, 35946, 35947, 35979, 36145, 37582, 38867, 39972, 42172, 44549, 44555, 61603 777-309ER 43977- 43981, 43982 777-312ER 34568-34585, 42235-42242 777-319ER 38405-38407, 39041, 40689, 44546, 44547 777-323ER 31480, 31543, 31546- 31550, 31553, 31554, 32439, 33125, 33127, 33522- 33524, 33538, 33541, 41665, 41666. 41668 777-328ER 32711, 32723-32727, 32845-32854, 32960-32964, 32968, 35297, 35542-35544, 35676, 35677, 35678, 37432, 37433, 37435, 38665, 38705, 38706, 39970, 39971, 39973, 40063, 40064, 40376, 44553, 61701 777-333ER 35240-35242, 35248-35251, 35254-35256, 35298, 35784, 42218, 42219, 43249-43251, 62400, 62401 777-336ER 38430, 38431, 40542, 40543, 42121, 42124, 42143, 43702, 43703 777-337ER 36308-36319 777-340ER 33778-33780 777-346ER 32430-32437, 36126-36130 777-360ER 44550, 44551 777-367ER 34432, 35299-35301, 36154-36165, 36832, 36833, 37896, 37897-37901, 39232-39237, 41428, 41429- 41433, 41757-41766, 42142- 42145, 60723- 60725 777-368ER 41048-41055, 41056-41059, 42261- 42268 777-381ER 27038, 27041, 27940, 28281, 32649-32651, 33416, 34892-34894, 34895, 37948-37951, 40686, 40687, 60136, 60137, 60381 777-31BER 43219-43228 777-31HER 32706-32710, 32713-32715, 32728 -32730, 33501, 34481-34484, 35574, 35575, 35579-35581, 35583-35585, 35588, 35591-35605, 38980-38991, 41070-41087, 41359-41370, 42122, 42318-42333 777-32WER 37664-37667, 38886-38889, 40588, 40589 777-35EER 32639-32645, 33750-33757, 43289-43291, 44552, 44554 777-35RER 35157-35166, 36563 777-36NER 32785, 32787-32795, 33862-33865, 37703-37707, 37709, 37712, 38284-38291, 38695, 38696, 41740, 41818-41823, 41845, 42101-42103, 42107, 42108 777-39LER 38666- 38680, 41441-41443, 44931, 60374 T00001SE 10 III. 777-300ER (cont’d): 777-39MER 37434 777-39PER 43269-43278, 43282, 43286, 43288 777-3ALER 41520- 41527 777-3DEER 44582-44587 777-3DZER 36009-36011, 36014, 36095, 36096, 36097, 36103, 36104, 37661, 37662, 38244-38248, 41062, 41738-41741, 41778, 41779, 41780, 41781, 43215, 43216, 60330- 60336 777-3FGER 61518, 61595 777-3FXER 34597-34601, 39681, 39683-39690, 39700, 41699, 41700, 41701, 44548 777-3ZGER 35302, 37938-37940, 37943 777-3B5ER 37136, 37643-37652, 40377-41999, 42120, 42123, 43815, 43816, 60375, 60376 777-3D7ER 42110- 42115 777-3E9ER 40120-40123 777-3F2ER 40707-40711, 40791-40797, 44116-44130, 60401, 60405 777-3F6ER 35555, 35556, 38718, 38719 777-3M0ER 41679- 41691 41694 777-3M2ER 40805, 40806, 43252-43254 777-3Q8ER 35782, 35783 777-3U3ER 29143- 29145, 29146-29148, 40072-40074, 40075 777-3U8ER 42097 777-300ER 36320-36322, 40683, 41692, 41693, 41824, 42104-42106, 42334-42355, 42359-42364, 43228, 43279-43281, 43283-43285, 43287, 60377-60380, 60402, 61512-61517, 61590-61594, 61596-61602, 61604, 61702, 61730, 61731, 61733, 61735, 61736, 61769, 61770, 62286, 62287, 62439, 62440, 62561-62570, 62642-62651, 62752-62755, 62761-62765, 63352-63357, 63434, 63435, 63528, 63529, 63721-63724, 64062- 64066, 64085-64089, 64989-64991, 64994, 65300-65305, 65307-65309, 65310, 65311, 65312, 65415, 65416-65419, 65420, 66091, 66092, 66582-66584, 66586, 66587, 66588, 66589, 66590-66592, 66633, 66888, 66889 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot. One flight attendant is required at each door no. 3 overwing exit. Maximum Passengers: 550. For passenger capacity above 500, an 11th flight attendant is required at door 3 exit. Maximum Baggage/Cargo: See appropriate FAA approved Weight and Balance Manual. Fuel and Oil Capacities: See appropriate FAA approved Weight and Balance Manual. Minimum Required Fuel: See appropriate FAA approved Airplane Flight Manual. Maximum Operating Altitude: 43,100 feet Certification Basis: A. 14 CFR part 25 of the Federal Aviation Regulations: Amendment 25-1 through 25-98, except for: §14 CFR 25.3(b)(2) at amendment 25-120 §25.831(a) and (g) which remains at amendment 25-86, §25.841(a), which remains at amendment 25-86, and §25.853(d)(3), which remains at amendment 25-82. §25.1457 at amendment 25-124 applicable to Line Number 858 and on. §25.1459 at amendment 25-124 applicable to Line Number 858 and on. §25.1517 is not part of the TC §25.1535 at amendment 25-120 14 CFR part 26: Based on 14 CFR §21.101(g) for changes made to TCs applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections Compliance has been found for the following regulations at Amendment 26-0: §26.11 Compliance has been found for the following regulations at Amendment 26-1: §26.43, 26.45, 26.47, and 26.49 Compliance has been found for the following regulations at Amendment 26-3: §26.33 and §26.39 Compliance has been found for the following regulations at Amendment 26-6: §26.21 14 CFR part 34 of the Federal Aviation Regulations: Amendment 34-1 through 34-7A. 11 T00001SE III. 777-300ER (cont’d): 14 CFR part 36 of the Federal Aviation Regulations: Amendment 36-1 through 36-24. Optional Design Regulations: Ditching: 14 CFR 25.801, 25.1411(d), (e), (f), (g) and 25.1415 Ice Protection: 14 CFR 25.1419 Exemptions from 14 CFR Part 25: 1. Floor Warpage for Flight Deck Seats Exemption from 14 CFR 25.562(b)(2). (Exemption No. 5436, April 1, 1992 and No. 5436A, January 3, 1997 and No. 5436B, November 15, 2000). 2. Partial Exemption from 14 CFR 25.1435(b)(1), Hydraulic Proof Pressure Test. (Exemption No. 7478, March 28, 2001). 3. Partial Exemption from 14 CFR 25.901(c), Thrust Control Malfunction Accommodation and Single Failures of Thrust Levers (Exemption No. 7955, January 17, 2003). 4. Partial Time-Limited Exemption from 14 CFR §25.853(a), appendix F, paragraph (a)(1)(i), Testing on Large Interior Panels, granted through November 28, 2011. (Exemption No. 9791, November 28, 2008, Exemption No. 9791B, March 1, 2010 , Exemption No. 9791C, February 4, 2011) 5. Business Class Seat installation on Boeing model 777-300ER aircraft from 14 CFR 853(d) and Special Condition 25-367-SC, condition 1, granted October 25, 2010 (Exemption No. 10156, October 25, 2010) 6. Time-Limited Exemption from 14 CFR 25.1535 as specified in Appendix K, §K25.1.4(a)(3) as the regulation applies to low-fuel alerting for approval for extended operations (ETOPS) beyond 180 minutes, granted through January 11, 2015 (Exemption No. 10193, January 11, 2011) (Exemption No. 10193A, December 17, 2013) 7. Partial Exemption from 14 CFR 25.813(e), Installation of Doors between Passenger Compartments (Exemption No. 17634, November 3, 2017 and No. 17634A, December 6, 2018) 8. Exemption from 14 CFR 25.813(e), Installation of Doors between Passenger Compartments (Exemption No. 17301, April 11, 2017) 9. Exemption from 14 CFR 25.562, Emergency Landing Dynamic Conditions, and 25.785(b), Seats, Berths, Safety Belts, and Harnesses (Exemption No. 17944, August 16, 2018) Equivalent Safety Findings exist with respect to the following regulations: 14 CFR 25.201(d) – Stall Demonstration 14 CFR 25.203(a) – Stall Characteristics 14 CFR 25.251(a) (b), PS15-0568-F-1 - Finding for Vibration / Buffeting Compliance Criteria, Vibration/Buffeting Compliance Criteria, Modifications to Boeing 777 Aircraft 14 CFR 25.335(b) – Dive Speed Definition with Dive Speed Protection 14 CFR 25.365(g)- Pressurized Compartment Loads (documented in ELOS Memo PS14-0508-A-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS09-0181-C-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS09-0445-CS-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS13-0075-C-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - for Single Occupant Side-Facing Seats.(documented in ELOS Memo PS13-0216-C-1) 14 CFR 25.571(b) – Freedom from Wide Spread Structural Fatigue Damage 14 CFR 25.613 – Material strength properties and material design values (documented in Transport Airplane Directorate ELOS Memo AT3907SE-T-A-15) 14 CFR 25.723(a) – Shock Absorption 14 CFR 25.791(a) and 25.853(d) – “No Smoking” Limitation in the passenger compartment 14 CFR 25.809(b)(2) and 25.810(a)(1) – Escape Slide Inflation Times 14 CFR 25.810 - Off-wing Escape System/Bottle Loss During Landing Gear Collapse 14 CFR 25.811 - Exterior Exit Marking 14 CFR 25.811(f) - Door Sill Reflectance 14 CFR 25.813(e) – Doors between passenger compartments (documented in Transport Airplane Directorate ELOS Memo PS05-0272-C-1) 14 CFR 25.853(a) – Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08-0670-C-1) 14 CFR 25.853(a) and (d) Compartment Interiors (Documented in TAD ELOS Memorandum PS13- 1000-C-5) 14 CFR 25.869(a)(4) - for Fiber Optic Cables used in the Model 777. 14 CFR 25.933(a)(1)(ii) - Inflight Thrust Reverser Deployment Demonstration 14 CFR 25.831(a) – Airplane Operation with Air Conditioning Packs Off During Takeoff 14 CFR 25.934 – Thrust Reverser Installation for Engine Endurance Testing 14 CFR 25.981, Amdt 25-125 - Fuel tank ignition prevention (see Note 12) T00001SE 12 III. 777-300ER (cont’d): 14 CFR part 25.981, Amdt 25-125 - for the Fuel Tank Flammability Rule (FTFR). (documented in ELOS Memo PS05-0177-P-2) 14 CFR 25.1181(a)(6), 25.1181(b), and 25.1182(a) – for Fire Safey Requirements for the GE90- 110/-115B Engine Fan Case (Documented in ELOS Memo PS25-0108-P-26) 14 CFR 25.1182(a) and 25.1183(a) - for Fire Resistant Requirement for Hydraulic Components Located in the Strut Aft Fairing. 14 CFR 25.1183(a) – Fire Resistance of Power Door Opening system on Engine Compartments (GE Engines) 14 CFR 25.1303(c)(1) - Overspeed Aural Warning. 14 CFR 25.1305 and 25.1501(b) - APU Instrumentation and Monitoring Requirements. 14 CFR 25.1351(b)(5) - for Flight Controls DC Power. 14 CFR 25.1389(b)(3) and 25.1395 – Red & Green Position Lights (documented in TAD ELOS Memo AT3908SE-T-SE-25) 14 CFR 25.1441(c) Crew Determination of the Quantity of Oxygen Available in the Lavatory Passenger Service Units Bottles (documented in ELOS Memo PS13-0901-ES-1) 14 CFR 25.1441(c) Crew Determination of the Quantity of Oxygen Available in the Supplemental Oxygen System for the High Wall Passenger Seating Unit (documented in ELOS Memo PS14-0508- ES-1) 14 CFR 25.1443(c) Determination of Minimum Oxygen Flow in the Supplemental Oxygen System for the High Wall Passenger Seating Unit (documented in ELOS Memo PS14-0508-ES-2) 14 CFR 25.1443(c) Determination of Minimum Oxygen Flow for the Lavatory Oxygen System (documented in TAD ELOS Memo TS13-0005-S-1) 14 CFR 25.1443(d) Portable Pulse Oxygen System (documented in ELOS Memo TC6918SE-T-ES- 20) 14 CFR 25.1459(a)(2) - for Flight Data Recorder Accelerometers. 14 CFR 25.1529, 25.1729 - Inclusion of Airworthiness Limitations within the Boeing ICA manuals (Documented in TAD ELOS Memo TC6918SE-T-G-8) 14 CFR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments (Documented in TAD ELOS Memorandum AT00010BA-T-S-1) 14 CFR 25.1555(d)(1) Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (documented in ELOS Memo PS06-0496-F-18) 14 CFR 25. (several sections) Use of 1g Speed Instead of Minimum Speed in the Stall as a basis for Compliance. 14 CFR 25 Appendix K25.2.2(b)(1) and (d), Amdt 25-120 – Early Extended Operations (ETOPS) Approval of GE90-110B1/-115B Modification when Early ETOPS was not the Basis of the Airplane-Engine Combination’s ETOPS Type Design Approval (documented in ELOS Memorandum PS21-0254-EE-1) Special Conditions with respect to the following subjects apply to the Model 777-300ER: Special Conditions No. 25-ANM-78, effective on December 10, 1993, addressed the following issues: 1. Operation without Normal Electrical Power 2. Integrated Command Signal Integrity 3. Protection from Lightning and High-Intensity Radiated Fields Protection 4. Effect of Flight Control Systems on Structure 5. Design Maneuver Requirements 6. Limit Engine Torque Loads for Sudden Engine Stoppage 7. Flight Characteristics Compliance via Handling Qualities Rating Method 8. Electronic Flight Control System - Control Surface Awareness Note: (Special Conditions on lightning are no longer part of the Type Certificate as a result of Boeing’s voluntary compliance with Amendment 25-80 which resulted in issuance of 25.1316, “System Lightning Protection”). Special Conditions No. 25-ANM-84A, effective on October 8, 2003, addressed airplane type design approval for Extended Range Operation With Two-Engine Airplanes (ETOPS). Special Conditions No. 25-07-12-SC, effective on June 1, 2007, Lithium Ion Battery installation Special Conditions No. 25-141-SC, effective on December 7, 1998, Seats With Articulating Seat Backs Special Conditions No. 25-187A-SC, effective on October 29, 2004, addressed seats with inflatable lapbelts. Special Conditions No. 25-230-SC, effective on April 9, 2003, addressed Overhead Crew Rest Compartments Special Condition No. 25-260-SC, effective on April 14, 2004, addressed Overhead Crew Rest Compartment Occupiable During Taxi, Takeoff, and Landing. Special Conditions No. 25-295-SC, effective on August 9, 2005, Side-Facing Single-Occupant Seats equipped with inflatable lapbelts 13 T00001SE III. 777-300ER (cont’d): Special conditions No. 25-336-SC, effective on November 15, 2006. addressed overhead cross aisle stowage compartments Special Conditions No. 25-367-SC, effective on February 7, 2008, addressed Seats With Non- Traditional, Large, Non-Metallic Panels Special Conditions No. 25-503-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized Internal Access Special Conditions No. 25-504-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized External Access Special Conditions No. 25-569-SC, effective on September 25, 2014, addressed Model 777-300ER airplanes with single-occupant, oblique (side-facing) seats equipped with inflatable lapbelts. Special Conditions No. 25-621B-SC, effective on October 22, 2018, addressed Single Occupant Oblique (Side-Facing) Seats Special Conditions No. 25-687-SC, effective to design changes applied for after May 31, 2017, addressed Non-Rechargeable Lithium Batteries. See the applicability section of these special conditions for more information on which design changes must meet them. Special Conditions No. 25-703-SC, effective on October26, 2017, addressed Passenger Cabin High- Wall Suites Special Conditions No. 25-758-SC, effective on December 2, 2019, addressed Seats with Inertia Locking Devices Special Conditions No. 25-769-SC, effective on August 10, 2020, addressed Dynamic Test Requirements for Single-Occupant Oblique Seats With Pretensioner Restraint Systems Special Conditions No. 25-841-SC, effective on November 24, 2023, addressed Seats with Pretensioner Restraint Systems IV - Model 777-200LR Series (Transport Category) Approved February 2, 2006 Engines: 2 General Electric Turbofan Model: GE90-110B1 2 General Electric Turbofan Model: GE90-115B (Engine Type Certificate No. E00049EN) Fuel: General Electric Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of GE Aviation Turbine Fuels Specification D50TF2. Engine Ratings & Operating Limits: General Electric Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Airspeed Limits: VMO/MMO = 330KEAS/.89M. For other airspeed limits, see the appropriate FAA approved Airplane Flight Manual CG Range: See the appropriate FAA approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA approved Airplane Flight Manual. Model Eligible Serial Numbers 777-2FBLR 40668, 60116 777-2DZLR 36012, 36013, 36015-36018, 36101, 36102, 41061, 41062 777-2KQLR 40753 777-21HLR 35572, 35573, 35576-35578, 35582, 35586, 35587, 35589, 35590 777-22KLR 39548, 42296, 42297 777-29MLR 40955, 40993 777-232LR 29739-29742, 30440, 32222, 39091, 39254, 40559, 40560 777-233LR 35239, 35243-35247 777-237LR 36300-36307 777-240LR 33781, 33782 777-260LR 40770-40774, 43814 T00001SE 14 IV - Model 777-200LR (cont’d) 777-200LR 66536, 66893 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot. Maximum Passengers: 440 Maximum Baggage/Cargo: See appropriate FAA approved Weight and Balance Manual. Fuel and Oil Capacities: See appropriate FAA approved Weight and Balance Manual. Minimum Required Fuel: See appropriate FAA approved Airplane Flight Manual. Maximum Operating Altitude: 43,100 feet Certification Basis: A. 14 CFR part 25 of the Federal Aviation Regulations: Amendment 25-1 through 25-100, except for: 14 CFR 25.3(b)(2) at amendment 25-120 14 CFR 25.831(a) and (g) which remains at amendment 25-86, 14 CFR 25.841(a), which remains at Amendment 25-86, and 14 CFR 25.853(d)(3), which remains at Amendment 25-82 level. 14 CFR 25.1457 at amendment 25-124 applicable to Line Number 858 and on. 14 CFR 25.1459 at amendment 25-124 applicable to Line Number 858 and on. 14 CFR 25.1517 is not part of the TC 14 CFR 25.1535 at amendment 25-120 14 CFR part 26: Based on 14 CFR §21.101(g) for changes made to TCs applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections Compliance has been found for the following regulations at Amendment 26-0: §26.11 Compliance has been found for the following regulations at Amendment 26-1: §26.43, 26.45, 26.47, and 26.49 Compliance has been found for the following regulations at Amendment 26-3: §26.33 and §26.39 Compliance has been found for the following regulations at Amendment 26-6: §26.21 In addition to 14 CFR part 25 of FARs, the type certification basis for the Model 777-200LR airplane includes compliance with the emissions standards of 14 CFR part 34, Amendment 34-1 through 34-7A, and with the noise standards of 14 CFR part 36, Amendment 36-1 through 36- 28. B. This Amended Type Certification was obtained under the delegation option authorization provisions of 14 CFR part 21 Optional Design Regulations: Ditching: 14 CFR 25.801, 25.1411(d), (e), (f), (g) and 25.1415 Ice Protection: 14 CFR 25.1419 Exemptions from 14 CFR part 25: 1. Floor Warpage for Flight Deck Seats Exemption from 14 CFR 25.562(b)(2). (Exemption No. 5436, April 1, 1992 and No. 5436A, January 3, 1997 and No. 5436B, November 15, 2000). 2. Partial Exemption from 14 CFR 25.1435(b)(1), Hydraulic Proof Pressure Test the static pressure test requirement (Exemption No 7478, March 28, 2001) 3. Partial Exemption from 14 CFR 25.901(c), Thrust Control Malfunction Accommodation and Single Failures of Thrust Levers (Exemption No. 7955, January 17, 2003). 4. Partial Time-Limited Exemption from 14 CFR §25.853(a), apx F, paragraph (a)(1)(i), Testing on Large Interior Panels, granted through November 28, 2011. (Exemption No. 9791, November 28, 2008, Exemption No. 9791B, March 1, 2010 , Exemption No. 9791C, February 4, 2011) 5. Time-Limited Exemption from 14 CFR 25.1535 as specified in Appendix K, §K25.1.4(a)(3) as the regulation applies to low-fuel alerting for approval for extended operations (ETOPS) beyond 180 minutes, granted through January 11, 2015 (Exemption No. 10193, January 11, 2011) (Exemption No. 10193A, December 17, 2013) 15 T00001SE IV - Model 777-200LR (cont’d) 6. Partial Exemption from 14 CFR 25.813(e), Installation of Doors between Passenger Compartments (Exemption No. 17634, November 3, 2017 and No. 17634A, December 6, 2018) Equivalent Safety Findings exist with respect to the following regulations: 14 CFR 25.201(d) – Stall Demonstration 14 CFR 25.203(a) – Stall Characteristics 14 CFR 25.251(a) (b), PS15-0568-F-1 - Finding for Vibration / Buffeting Compliance Criteria, Vibration/Buffeting Compliance Criteria, Modifications to Boeing 777 Aircraft 14 CFR 25.335(b) – Dive Speed Definition with Dive Speed Protection 14 CFR 25.365(g)- Pressurized Compartment Loads (documented in ELOS Memo PS14-0508-A-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS09-0445-CS-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - Dynamic Test Requirements for Single Occupant Side-Facing Seats on Boeing Model 777 (documented in ELOS Memo PS13-0075-C-1) 14 CFR 25.562, 25.785, Special Condition No. 25-295-SC - for Single Occupant Side-Facing Seats.(documented in ELOS Memo PS13-0216-C-1) 14 CFR 25.571(b) – Freedom from Wide Spread Structural Fatigue Damage 14 CFR 25.613 – Material strength properties and material design values (documented in Transport Airplane Directorate ELOS Memo AT3907SE-T-A-15) 14 CFR 25.723(a) – Shock Absorption 14 CFR 25.791(a) and 25.853(d) – “No Smoking” Limitation in the Passenger Compartment 14 CFR 25.809(b)(2) and 25.810(a)(1) – Escape Slide Inflation Times 14 CFR 25.811 - Exterior Exit Marking 14 CFR 25.811(f) - Door Sill Reflectance 14 CFR 25.813(e) – Doors between passenger compartments (documented in Transport Airplane Directorate ELOS Memo PS05-0272-C-1) 14 CFR 25.831(a) – Airplane Operation with Air Conditioning Packs Off During Takeoff 14 CFR 25.853(a) – Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08-0670-C-1) 14 CFR 25.853(a) and (d) Compartment Interiors (Documented in TAD ELOS Memorandum PS13- 1000-C-5) 14 CFR 25.869(a)(4) - for Fiber Optic Cables used in the Model 777. 14 CFR 25.933(a)(1)(ii) - Inflight Thrust Reverser Deployment Demonstration. 14 CFR 25.934 – Thrust Reverser Installation for Engine Endurance Testing 14 CFR 25.981, Amdt 25-125 - Fuel tank ignition prevention (see Note 12) 14 CFR 25.981, Amdt 25-125 - for the Fuel Tank Flammability Rule (FTFR). (documented in ELOS Memo PS05-0177-P-2) 14 CFR 25.1181(a)(6), 25.1181(b), and 25.1182(a) – for Fire Safey Requirements for the GE90- 110/-115B Engine Fan Case (Documented in ELOS Memo PS25-0108-P-26) 14 CFR 25.1182(a) and 25.1183(a) - for Fire Resistant Requirement for Hydraulic Components Located in the Strut Aft Fairing 14 CFR FAR 25.1183(a) – Fire Resistance of Power Door Opening system on Engine Compartments (GE Engines) 14 CFR 25.1303(c)(1) - Overspeed Aural Warning. 14 CFR 25.1305 and 25.1501(b) - APU Instrumentation and Monitoring Requirements. 14 CFR 25.1351(b)(5) - for Flight Controls DC Power. 14 CFR 25.1389(b)(3) – Red & Green Position Lights, Aft Lamps Only. 14 CFR 25.1441(c) Crew Determination of the Quantity of Oxygen Available in the Lavatory Passenger Service Units Bottles (documented in ELOS Memo PS13-0901-ES-1) 14 CFR 25.1443(c) Determination of Minimum Oxygen Flow for the Lavatory Oxygen System (documented in TAD ELOS Memo TS13-0005-S-1) 14 CFR 25.1459(a)(2) - for Flight Data Recorder Accelerometers. 14 CFR 25.1529, 25.1729 - Inclusion of Airworthiness Limitations within the Boeing ICA manuals (Documented in TAD ELOS Memo TC6918SE-T-G-8) 14 CFR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments (Documented in TAD ELOS Memorandum AT00010BA-T-S-1) 14 CFR 25.1555(d)(1) Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (documented in ELOS Memo PS06-0496-F-18) 14 CFR 25. (several sections) Use of 1g Speed Instead of Minimum Speed in the Stall as a Basis for Compliance 14 CFR 25 Appendix K25.2.2(b)(1) and (d), Amdt 25-120 – Early Extended Operations (ETOPS) Approval of GE90-110B1/-115B Modification when Early ETOPS was not the Basis of the Airplane-Engine Combination’s ETOPS Type Design Approval (documented in ELOS Memorandum PS21-0254-EE-1) T00001SE 16 IV - Model 777-200LR (cont’d) Special Conditions with respect to the following subjects apply to the Model 777-200LR: Special Conditions No. 25-ANM-78, effective on December 10, 1993, addressed the following subjects: 1. Operation without Normal Electrical Power 2. Integrated Command Signal Integrity 3. Protection from Lightning and High-Intensity Radiated Fields Protection 4. Effect of Flight Control Systems on Structure 5. Design Maneuver Requirements 6. Limit Engine Torque Loads for Sudden Engine Stoppage 7. Flight Characteristics Compliance via Handling Qualities Rating Method 8. Electronic Flight Control System - Control Surface Awareness Note: (Special Conditions on lightning are no longer part of the Type Certificate as a result of Boeing’s voluntary compliance with Amendment 25-80 which resulted in issuance of 25.1316, “System Lightning Protection”) Special Conditions No. 25-ANM-84A, effective on October 8, 2003, addressed airplane type design approval for Extended Range Operation With Two-Engine Airplanes (ETOPS). Special Conditions No. 25-07-12-SC, effective on June 1, 2007, Lithium Ion Battery installation Special Conditions No. 25-141-SC, effective on December 7, 1998, Seats With Articulating Seat Backs Special Conditions No. 25-187A-SC, effective on October 29, 2004, addressed seats with inflatable lapbelts. Special Conditions No. 25-230-SC, effective on April 9, 2003, addressed Overhead Crew Rest Compartments Special Conditions No. 25-260-SC, effective on April 14, 2004, addressed the Overhead Crew Rest Compartment Occupiable During Taxi, Take-off, and Landing Special Conditions No. 25-295-SC, effective on August 9, 2005, Side-Facing Single-Occupant Seats equipped with inflatable lapbelts Special Conditions No. 25-336-SC, effective on November 15, 2006. addressed overhead cross aisle stowage compartments Special Conditions No. 25-367-SC, effective on February 7, 2008, addressed Seats With Non- Traditional, Large, Non-Metallic Panels Special Conditions No. 25-503-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized Internal Access Special Conditions No. 25-504-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized External Access Special Conditions No. 25-621B-SC, effective on October 22, 2018, addressed Single Occupant Oblique (Side-Facing) Seats Special Conditions No. 25-687-SC, effective to design changes applied for after May 31, 2017, addressed Non-Rechargeable Lithium Batteries. See the applicability section of these special conditions for more information on which design changes must meet them. Special Conditions No. 25-758-SC, effective on December 2, 2019, addressed Seats with Inertia Locking Devices Special Conditions No. 25-769-SC, effective on August 10, 2020, addressed Dynamic Test Requirements for Single-Occupant Oblique Seats With Pretensioner Restraint Systems Special Conditions No. 25-841-SC, effective on November 24, 2023, addressed Seats with Pretensioner Restraint Systems V-Model 777F Series (Transport Category) Approved February 3, 2009 Engines: 2 General Electric Turbofan Model: GE90- 110B1 2 General Electric Turbofan Model: GE90-115B (Engine Type Certificate No. E00049EN) Fuel: General Electric Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1, MIL-T-5624 grade JP-5, and MIL-T-83133 grade JP-8, and Fuels produced to other specifications and having properties meeting the requirements of the above specifications are acceptable. The fuel and any fuel additives must conform to the latest approved version of GE Aviation Turbine Fuels Specification D50TF2. 17 T00001SE V-Model 777F Series (cont’d) Engine Ratings & Operating Limits: General Electric Engines: See the FAA approved Airplane Flight Manual for engine ratings. See the FAA approved Airplane Flight Manual and Note 6 for engine operating limits. The normal 5 minute takeoff time limit may be extended to 10 minutes for engine out contingency if permitted by the Limitations Section of the FAA approved Airplane Flight Manual. Airspeed Limits: VMO/MMO = 330KEAS/.89M. For other airspeed limits, see the appropriate FAA approved Airplane Flight Manual. CG Range: See the appropriate FAA approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA approved Airplane Flight Manual. Model Eligible Serial Numbers 777F16 38091, 41518 777F28 32965-32967, 32969 777F60 42031- 42034 777F1B 37309-37314, 41632-41637 777F1H 35606-35613, 42230-42234 777F6N 37708, 37710, 37711, 37713-37717, 41817, 41846 777FBT 41674-41678 777FDZ 36098-36100, 39644, 39645, 41427, 42298, 42299, 62083, 62085 777FEZ 62631 777FFG 60337- 60340 777FFT 44678-44685 777FFX 39682, 39691-39692, 62744, 62745 777FHT 37138, 38969, 39285, 39286 777FZB 37986-37989 777FZN 36001-36004, 36198- 36201 777FB5 37638-37642 777FS2 37137, 37721-37730, 37732-37735, 38707, 40674, 40675, 41064-41067, 41439, 41749 777F 37731, 40671-40673, 40676, 40679, 40682-40685, 41440, 41736, 41737, 41750, 42704, 42705, 60403, 60404, 60509, 62084,62086, 62632, 62693-62697, 62770-62773, 62824-62828, 65397, 65398, 65421, 65422, 65476, 65477, 65742-65744, 65756, 65757, 66079-66090, 66164, 66255, 66256-66258, 66259, 66260, 66262, 66263, 66264, 66265, 66266, 66267, 66335-66341, 66578-66580, 66623-66625, 66632, 66814, 66815, 66862, 66863, 66870, 66871, 66872, 66890-66892, 66900, 66901, 66902, 66911, 66912, 67031-67033, 67138, 67139, 67140, 67141, 67142, 67143, 67144, 67145, 67146, 67453, 67454, 67455, 67460, 67461, 67462, 67463, 67464, 67763, 67764, 67769, 67770, 67771, 67796, 67797, 67798, 67799, 67800, 67820, 67821, 67822, 67823, 67824, 67833, 67834, 67835, 67836, 67837, 67866, 67867, 67992, 67993, 67994, 67995, 68057, 68058, 68059, 68060, 68063, 68064, 68139, 68140, 68141, 68144, 68145, 68146, 68147, 68186, 68187, 68195, 68196, 68197, 68230, 68617, 68618, 68619, 68620, 69033, 69512, 69513, 69514, 69787, 69788 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot. Maximum Passengers: For 777F total persons capacity is limited to: Maximum of eleven (11) persons per Exemption 9779 and limitations outlined in the FAA approved Airplane Flight Manual. Maximum Baggage/Cargo: See appropriate FAA approved Weight and Balance Manual. Fuel and Oil Capacities: See appropriate FAA approved Weight and Balance Manual. Minimum Required Fuel: See appropriate FAA approved Airplane Flight Manual. Maximum Operating Altitude: 43,100 feet Certification Basis: A. 14 CFR part 25 of the Federal Aviation Regulations (FAR) as amended by Amendments 25-1 through 25-117, with the exceptions listed below: SECTION NO. TITLE AT AMDT. 25- 25.3(b)(2) Special provisions for ETOPS type design approvals 120 25.103 Performance – stalling speed 108 T00001SE 18 V. 777F (cont’d) 25.107 Takeoff speeds 108 25.111 Takeoff path 115 25.119 Landing Climb: All engines operating 108 25.121 Climb: One Engine Inoperative 108 25.125 Landing 108 25.143 Controllability and Maneuverability General 108 25.149 Minimum control speed 108 25.201 Stall demonstration 108 25.207 Stall warning 108 25.233 Directional stability and control 108 25.237 Wind velocities 108 25.473 Ground load conditions and assumptions 103 25.613 Material strength properties and design values 112 (1) 25.723 Shock Absorbtion Test 103 25.731 Wheels 72 (2) 25.735 Brakes 92 (3) 25.773 Pilot Compartment View 108 (4) 25.783 Doors 114 (5) 25.807 Passenger Emergency Exits 114 (6) 25.812 Emergency Lighting 116 (7) 25.813 Emergency Exit Access 116 25.820 Lavatory Doors 114 25.841(a) Pressurized Cabins 86 25.853 Compartment Interiors 116 25.855 Cargo or Baggage Compartments 116 25.856 Thermal/Acoustic insulation materials 111 25.869 Fire Protection: Systems 113 25.981(a)(b) Fuel Tank temperature 102 25.1001(f) Fuel jettisoning system 108 25.1141 Powerplant Controls: General 115 25.1305 Powerplant Instruments 115 25.1323 Airspeed Indicating System 109 25.1325 Static Pressure Systems 108 25.1353 Electrical Equipment & Installation 113 (8) 25.1411 Safety Equipment: General 116 25.1431 Electronic Equipment 113 (9) 25.1439 Protective Breathing Equipment 115 25.1447 Oxygen Dispensing Units 116 25.1457 Cockpit Voice Recorder 124 (10) 25.1459 Flight Data Recorder 124 (10) 25.1516 Other Speed Limitations 105 25.1527 Ambient Air Temperatures and Operating Altitude 105 25.1535 ETOPS Approval 120 25.1583 Operating Limitations 105 25.1585 Operating Procedures 105 25.1587 Performance Information 108 (1) Comply with Amendment 25-112 except that Not Significant changes comply with 25.613(c) at Amdt 25-72: existing doors, wing, keel/wheelwell, fairings, empennage, landing gear, propulsion structure, lower lobe cargo structure, flight controls, high lift (2) Main and nose wheels from both suppliers (Messier-Bugatti and Goodrich) are unchanged. (Goodrich nose wheel is unchanged, but the TSO load rating for the wheel has been increased compared to the 777-200LR due to increased loads on the 777F). 14 CFR 25.731(a), (b), (c) amendment 72 for wheels, tires, brakes, and landing gear systems. (3) Complies with Amendment 25-92 due to Not Significant changes to brake control cable (rerouting of cable runs 3” inboard due to installation of the new aluminum floor beams) and unchanged main wheel brakes and reassessed for landing brake kinetic energy for increased landing weights, Landing gear systems and Hydraulic controls – mechanical. (4) Complies with Amendment 25-108 except for the window heat control unit which remains at amendment level 25-72. (5) Complies at Amendment 25-114 for the new Main Deck Cargo Door only. All other pressurized doors remain at amendment 25-88. (6) Complies with Amendment 25-114 for weights only. Escape systems are not affected by this change and comply with 25-94 (7) Complies with amendment 116 except for: 25.812(g) is not applicable to 777F. Physical lighting of the emergency escape means complies with 25.812(h) at amendment 25-88. 19 T00001SE V. 777F (cont’d) (8) Complies with Amendment 25-113 except for Avionics – SATCOM complies with Amendment 25-42 for 25.1353(a) due to Not Significant changes to the system (9) Complies with Amendment 25-113 except for Avionics – SATCOM complies with Amendment 25-0 for 25.1431(a), (c) due to Not Significant changes to the system. Avionics- CVR and FDR comply with Amendment 25-0 for 25.1431(c). Cabin Systems – PAS complies with Amendment 25- 0 for 25.1431 (10) Compliance to amendment 25-124 applicable to Line Number 858 and on. Following Optional Design Regulations have been complied with: Ditching: 14 CFR 25.801, 25.1411(d), (e), (f) and 25.1415 Ice Protection: 14 CFR 25.1419 Exemptions from 14 CFR part 25: 1. Floor Warpage for Flight Deck Seats Exemption from 14 CFR 25.562(b)(2). (Exemption No. 5436, April 1, 1992 and No. 5436A, January 3, 1997 and No. 5436B, November 15, 2000). 2. Partial Exemption for the following regulations (Exemption No. 9779, October 31, 2008) a. Partial Exemption from 14 CFR 25.785(j), Seat Back Hand hold b. Partial Exemption from 14 CFR 25.857(e), Class E Cargo Compartments c. Partial Exemption from 14 CFR 25.1447(c)(1), Equipment standards for oxygen dispensing units ( Also Exemption No. 9779A, September 15, 2009) 3. Partial Exemption from 14 CFR 25.901(c), Thrust Control Malfunction Accomodation and Single Failures of Thrust Levers (Exemption No. 7955, January 17, 2003) 4. Partial Time-Limited Exemption from 14 CFR §25.853(a), appendix F, paragraph (a)(1)(i), Testing on Large Interior Panels, granted through November 28, 2011. (Exemption No. 9791, November 28, 2008, Exemption No. 9791B, March 1, 2010 , Exemption No. 9791C, February 4, 2011) 5. Time-Limited Exemption from 14 CFR 25.1535 as specified in Appendix K, §K25.1.4(a)(3) as the regulation applies to low-fuel alerting for approval for extended operations (ETOPS) beyond 180 minutes, granted through January 11, 2015 (Exemption No. 10193, January 11, 2011) (Exemption No. 10193A, December 17, 2013) 6. Exemption from 14 CFR 25.562, Emergency Landing Dynamic Conditions, and 25.785(b), Seats, Berths, Safety Belts, and Harnesses (Exemption No. 17944, August 16, 2018) The following regulations have been complied by Equivalent Level of Safety: 14 CFR 25.201(d), Amdt 25-84 – Stall Demonstration 14 CFR 25.203(a), Amdt 25-84 – Stall Characteristics\ 14 CFR 25.251(a) (b), PS15-0568-F-1 - Finding for Vibration / Buffeting Compliance Criteria, Vibration/Buffeting Compliance Criteria, Modifications to Boeing 777 Aircraft 14 CFR 25.335(b), Amdt 25-91 – Dive Speed Definition with Dive Speed Protection 14 CFR 25.341, Amdt 25-86 – Design Gust Criteria 14 CFR 25.343, Amdt 25-86 – Design Gust Criteria 14 CFR 25.345, Amdt 25-91 – Design Gust Criteria 14 CFR 25.371, Amdt 25-91 – Design Gust Criteria 14 CFR 25.373, Amdt 25-86 – Design Gust Criteria 14 CFR 25.391, Amdt 25-86 – Design Gust Criteria 14 CFR 25.365(g)- Pressurized Compartment Loads (documented in ELOS Memo PS14- 0508-A-1) 14 CFR 25.571(b), Amdt 25-96 – Freedom from Wide Spread Structural Fatigue Damage 14 CFR 25.791(a). Amdt 25-72 – “No Smoking” Limitation in the Passenger Compartment 14 CFR 25.809(b)(2), Amdt 25-72 – Escape Slide Inflation Times 14 CFR 25.810(a)(1), Amdt 25-88 - Escape Slide Inflation Times 14 CFR 25.811, Amdt 25-79 - Exterior Exit Marking 14 CFR 25.811(f), Amdt 25-88 - Door Sill Reflectance 14 CFR 25.831(g), Acceptable High Temperature Physiological Environment During Failure Conditions. (documented in ELOS Memo PS05-0020-ES-3) 14 CFR 25.853(d), Amdt 25-83 - “No Smoking” Limitation in the Passenger Compartment14 CFR 25.853(a) and (d) Compartment Interiors (Documented in TAD ELOS Memorandum PS13- 1000-C- 5) 14 CFR 25.855, Amdt 25-116 - Inadvertent Smoke Detection in Lower Lobe Cargo Compartments 14 CFR 25.857, Amdt 25-93 - Inadvertent Smoke Detection in Lower Lobe Cargo Compartments 14 CFR 25.858(a), Amdt 25-93 – Inadvertent Smoke Detection in Lower Lobe Cargo Compartments14 CFR 25.933(a)(1)(ii), Amdt 25-72 - Inflight Thrust Reverser Deployment Demonstration. 14 CFR 25.934, Amdt 25-23 – Thrust Reverser Installation for Engine Endurance Testing T00001SE 20 V. 777F (cont’d) 14 CFR 25.981, Amdt 25-125 - Fuel tank ignition prevention (see Note 12) 14 CFR part 25.981, Amdt 25-125 - for the Fuel Tank Flammability Rule (FTFR). (documented in ELOS Memo PS05-0177-P-2) 14 CFR 25.1181(a)(6), 25.1181(b), and 25.1182(a) – for Fire Safey Requirements for the GE90- 110/-115B Engine Fan Case (Documented in ELOS Memo PS25-0108-P-26) 14 CFR 25.1182(a), Amdt 25-11 - for Fire Resistant Requirement for Hydraulic Components Located in the Strut Aft Fairing 14 CFR 25.1183(a), Amdt 25-57 – Fire Resistance of Power Door Opening system on Engine Compartments (GE Engines) 14 CFR 25.1303(c)(1), Amdt 25-90 - Overspeed Aural Warning. 14 CFR 25.1305, Amdt 25-72 - APU Instrumentation and Monitoring Requirements. 14 CFR 25.1351(b)(5), Amdt 25-72 - for Flight Controls DC Power. 14 CFR 25.1389(b)(3), Amdt 25-0 – Red & Green Position Lights, Aft Lamps Only. 14 CFR 25.1435(a),(b)(1), Amdt 25-104 - Hydraulic Systems (documented in ELOS Memo PS05- 0020-S-1) 14 CFR 25.1443(c), Amdt 25-0 - Determination of Minimum Oxygen Flow for the Lavatory Oxygen System (documented in TAD ELOS Memo TS13-0005-S-1) 14 CFR 25.1459(a)(2), Amdt 25-65 - for Flight Data Recorder Accelerometers 14 CFR 25.1529, 25.1729 - Inclusion of Airworthiness Limitations within the Boeing ICA manuals (Documented in TAD ELOS Memo TC6918SE-T-G-8) 14 CFR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments (Documented in TAD ELOS Memorandum AT00010BA-T-S-1) 14 CFR 25.1555(d)(1) Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (documented in ELOS Memo PS06-0496-F-18) 14 CFR 25.1501(b), Amdt 25-42 - APU Instrumentation and Monitoring Requirements 14 CFR 25. (several sections), Amdt 25-75 Use of 1g Speed Instead of Minimum Speed in the Stall as a Basis for Compliance. 14 CFR 25 Appendix K25.2.2(b)(1) and (d), Amdt 25-120 – Early Extended Operations (ETOPS) Approval of GE90-110B1/-115B Modification when Early ETOPS was not the Basis of the Airplane-Engine Combination’s ETOPS Type Design Approval (documented in ELOS Memorandum PS21-0254-EE-1) . Special Conditions with respect to the following subjects apply to the Model 777F: Special Condition No. 25-ANM-78, effective on December 10, 1993, addressed the following subjects: 1. Operation without Normal Electrical Power 2. Integrated Command Signal Integrity 3. Protection from Lightning and High-Intensity Radiated Fields (HIRF) Protection 4. Effect of Flight Control Systems on Structure 5. Design Maneuver Requirements 6. Limit Engine Torque Loads for Sudden Engine Stoppage 7. Flight Characteristics Compliance via Handling Qualities Rating Method 8. Electronic Flight Control System - Control Surface Awareness Note: (Special Conditions on lightning are no longer part of the Type Certificate as a result of Boeing’s compliance with 14 CFR part 25 Amendment 25-80 which resulted in issuance of 25.1316, “System Lightning Protection”). Special Condition No. 25-ANM-84A, effective on October 8, 2003, addressed airplane type design approval for Extended Range Operation With Two-Engine Airplanes (ETOPS). Special Condition No. 25-187A-SC, effective on October 29, 2004, addressed seats with inflatable lapbelts. Special Conditions No.25-462-SC, effective on March 22, 2012, 777F; Enhanced Flight Vision System. Special Conditions No. 25-503-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized Internal Access Special Conditions No. 25-504-SC, effective on November 18, 2013, addressed Aircraft Electronic System Security Protection From Unauthorized External Access Special Conditions No. 25-687-SC, effective to design changes applied for after May 31, 2017, addressed Non-Rechargeable Lithium Batteries. See the applicability section of these special conditions for more information on which design changes must meet them. Special Conditions No. 25-758-SC, effective on December 2, 2019, addressed Seats with Inertia Locking Devices Special Conditions No. 25-769-SC, effective on August 10, 2020, addressed Dynamic Test Requirements for Single-Occupant Oblique Seats With Pretensioner Restraint Systems Special Conditions No. 25-841-SC, effective on November 24, 2023, addressed Seats with Pretensioner Restraint Systems 21 T00001SE V. 777F (cont’d) 14 CFR part 26: Based on 14 CFR §21.101(g) for changes made to TCs applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections Compliance has been found for the following regulations at Amendment 26-0: 26.11 Compliance has been found for the following regulations at Amendment 26-1: §26.43, 26.45, 26.47, and 26.49 Compliance has been found for the following regulations at Amendment 26-3: §26.33 and §26.39 Compliance has been found for the following regulations at Amendment 26-6: §26.21 In addition to 14 CFR part 25 of FARs, the type certification basis for the Model 777F airplane includes compliance with the emissions standards of 14 CFR part 34, Amendment 34-1 through 34- 7A, and with the noise standards of 14 CFR part 36, Amendment 36-1 through 36-28. THE FOLLOWING INFORMATION AND NOTES APPLY TO ALL MODELS UNLESS OTHERWISE NOTED: B. This type certificate was obtained under the delegation option authorization provisions of 14 CFR part 21. Certification Maintenance Requirements (CMRs): CMRs are listed in the FAA approved Section 9 of Boeing Maintenance Planning Data Document D622W001-9 and the applicable engine Type Certificate Data Sheet. The more restrictive requirement from these two documents shall be in force Production Basis: Production Certificate 700. See Note 4 and Note 11 Leveling Means: A plumb bob attachment and leveling provision scale are provided in the right hand body wheel well. Datum: Sta 0.0, located 92.5 in forward of airplane nose (B.S. 92.5). Mean Aerodynamic Chord: 278.51 inches Control Surface Movements: To insure proper operation of the airplane, the movement of the various control surfaces must be carefully controlled by proper rigging of the flight control systems. The airplane must, therefore, be rigged according to the following FAA-approved data: Boeing Drawing Numbers: 251W1001 Rigging Instructions Lateral Control 251W2001 Rigging Instructions Elevator Control 251W3001 Rigging Instructions Rudder Control 251W4001 Rigging Instructions Stabilizer Trim Control System 256W2001 Systems Rigging Leading Edge Slat 256W3001 Rigging Instructions Drive System Flap Actuation Required Equipment: The basic required equipment as prescribed in the applicable Federal Aviation Regulations must be installed in the aircraft. Service Information: Boeing Documents D634W201 "777-200 Structural Repair Manual", D634W210 "777-300 Structural Repair Manual", and D634W215 "777F Structural Repair Manual" are FAA-approved. Service Bulletins and other service information when FAA-approved will carry a statement to that effect. Note 1. A current Weight & Balance Report must be in each aircraft at the time of original airworthiness certification and at all times thereafter except in the case of an operator having an FAA approved loading system for weight and balance control. Note 2. Airplane operation must be in accordance with the FAA Approved Airplane Flight Manual. All placards required by either FAA Approved Airplane Flight Manual, the applicable operating rules, or the Certification Basis must be installed in the airplane. Note 3. Required structural inspections and the retirement times for safe-life parts are listed in the FAA Approved Airworthiness Limitations Section (Section 9) of Boeing Document D622W001-9. The inspection intervals for those inspections are based upon the curves contained in Boeing Document D101W801-36. The Boeing Commercial Airplanes Universal Airplane Network Security Operator Guidance, D925W704-04, contains required Instructions for Continued Airworthiness and security guidance that when followed meets compliance requirements of the Network Cybersecurity Special Conditions. T00001SE 22 THE FOLLOWING INFORMATION AND NOTES APPLY TO ALL MODELS UNLESS OTHERWISE NOTED: (cont’d) Note 4. The following Serial Number Airplanes were produced under Type Certificate only: 777-200: 26916-26919, 26921, 26925, 26929, 26930, 26932, 26936, 27105, 27106, 27116, 27265 777-300: 27507, 27506, 28275, 27505, 27950, 28273, 27504, 28272 Note 5. The Models 777-200 and 777-300 have been evaluated in accordance with FAA Special Conditions Number 25-ANM-84, and found suitable for 180-minute Extended Range Operations with Two-Engine Airplanes (ETOPS) operations when operated and maintained in accordance with Boeing Document D044W054 “Model 777 ETOPS Configuration, Maintenance, and Procedures.” This finding does not constitute approval to conduct ETOPS operations. The Models 777-200LR, 777-300ER, and 777F have been evaluated in accordance with FAA Special Conditions Number 25-ANM-84A, and found suitable for 180-minute Extended Range Operations with Two- Engine Airplanes (ETOPS) operations when operated and maintained in accordance with Boeing Document D044W054 “Model 777 ETOPS Configuration, Maintenance, and Procedures.” This finding does not constitute approval to conduct ETOPS operations. The Models 777-200, 777-200LR and 777-300ER have been evaluated in accordance with the type design requirements contained in FAA ETOPS Policy Letter EPL 20-1, dated March 21, 2000, and approved for 207- minute ETOPS when configured in accordance with Boeing Document D044W054. The use of 207-minute maximum diversion time is limited to a flight-by-flight exception basis from normal 180-minute ETOPS operations, as authorized in the FAA policy letter. This finding does not constitute approval to conduct 207- minute ETOPS operations. The airplane/engine combinations 777-200/GE90-85B/-90B, 777-200/GE90-94B, 777- 200/PW4084D/PW4090/PW4090-3, 777-200/RB211-Trent 884-17/Trent 892-17/Trent 892B-17/Trent 895- 17, 777-300ER/GE90-115B, 777-200LR/GE90-110B1/-115B, and 777F/GE90-110B1/-115B have been evaluated in accordance with the type design requirements of 14 CFR 25.3(b)(2) and 25.1535 and found suitable for greater than 180-minute ETOPS operations when operated and maintained in accordance with Boeing Document D044W054 "Model 777 Configuration, Maintenance, and Procedures." This finding does not constitute approval to conduct ETOPS operations. Note 6. For General Electric and Rolls-Royce engines only: The engines must be operated at idle for at least 10 minutes prior to shutdown after static operation at N1 settings greater than 70%. This limitation applies to static operation only; under normal operation conditions, the idle cooling instructions contained in the engine manufacturers operating instructions are acceptable. Note 7. The Model 777 has been approved to operate in “Reduced Vertical Separation Minimum” (RVSM) airspace. Continued airworthiness and operational approval aspects of RVSM must be constructed according to Advisory Circular (AC) 91-RVSM, titled “Approval of Aircraft and Operators for Flight in Airspace Above Flight Level (FL) 290 Where a 1,000 Foot Vertical Separation Minimum is Applied.” Note 8. The FAA has determined that the occurrence of any uncontrollable high thrust failure condition, or any of the associated causal failures listed within the Boeing 777 Maintenance Planning Document, “may endanger the safe operation of an airplane” and hence are reportable under FAR 121.703, 125.409, and 135.415. Note 9. For Model 777-200LR an optional single auxiliary body fuel tank cell may be installed for use with this Mandatory replacement times, inspection intervals, related inspection procedures and all critical design configuration control limitations for the fuel tank system determined during the Special Federal Aviation Regulation No. 88 program and for compliance with 14 CFR 25.981 are listed in the FAA-approved Airworthiness Limitations and Certification Maintenance Requirement, Section 9, of Boeing 777 Maintenance Planning Data Document D622W001-9, Revision February 2006 or later FAA-approved revision. All Model 777-200, -300, -300ER, and -200LR series airplanes, production line number 569 and on, must comply with Revision March 2006, or a later FAA-approved revision. The FAA has issued airworthiness directive 2008- 11-13 mandating compliance with Revision March 2006, or a later FAA- approved revision, applicable to all Model 777-200, -300, -300ER, and - 200LR series airplanes with production numbers lower than 569. The Maintenance Planning Data Document, Section 9 for the 777F meets Special Federal Aviation Regulation No. 88 and compliance to 14 CFR 25.981. Note 10. For Model 777-200LR an optional single auxiliary body fuel tank cell may be installed for use with this airplane. This auxiliary tank adds another 1,875 USG of airplane fuel capacity. The certification basis for this auxiliary body fuel tank includes §25.981 Amendment 25-102. Note 11. A production certificate number 700 was amended to include the 777F and issued. Boeing is authorized to issue airworthiness certificates under the delegation option authorization provisions of 14 CFR part 21. 23 T00001SE THE FOLLOWING INFORMATION AND NOTES APPLY TO ALL MODELS UNLESS OTHERWISE NOTED: (cont’d) Note 12. Certification basis for §25.981 at amendment 25-125, and Equivalent Safety Finding for the Flammability Reduction System (FRS), is applied if fuel tank inerting is installed in new airplane production (starting with Line # 772) or as a modification on existing aircraft per Boeing Service Bulletin 777-47-0002. Airworthiness Limitations for the FRS are contained in Section 9 of the applicable Maintenance Planning Document. Note 13. For aircraft delivered after July 15, 2019, information regarding the effective revision of the 777- 200/200LR/300/300ER/777F MPD Section 9 document (D622W001-9) and the 777- 200/200LR/300/300ER/777F DTR Document (D622W001-DTR) at the time each aircraft line number was issued its Original Standard Airworthiness Certificate can be found in MPD Section 9 and DTR Revision Effectivity Report letter MPE-RER-777-LNXXXX. .....END..... ``` ## ADs (260, first 50, in force first) - [AD 2026-19-04](https://openairdocs.org/ad/2026-19-04): Hydraulic Power · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Nov 2, 2026 - [AD 2026-15-02](https://openairdocs.org/ad/2026-15-02): Fuel · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Sep 1, 2026 - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2026-13-10](https://openairdocs.org/ad/2026-13-10): Navigation · Boeing 747-8 Series, 747-8F Series, 777-200 Series and 4 more. Effective Jul 1, 2026 - [AD 2026-05-15](https://openairdocs.org/ad/2026-05-15): Lights · Boeing 777-200LR Series and 777-300ER Series. Effective Apr 20, 2026 - [AD 2025-21-02](https://openairdocs.org/ad/2025-21-02): Flight controls · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jan 2, 2026 - [AD 2025-15-09](https://openairdocs.org/ad/2025-15-09): Equipment/furnishings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Aug 21, 2025 - [AD 2025-05-10](https://openairdocs.org/ad/2025-05-10): Flight Controls, Fuel, Landing Gear, Doors, Fuselage, Nacelles/Pylons, Stabilizers, Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective May 13, 2025 - [AD 2025-06-12](https://openairdocs.org/ad/2025-06-12): Auto flight · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective May 2, 2025 - [AD 2025-06-02](https://openairdocs.org/ad/2025-06-02): Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Apr 23, 2025 - [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025 - [AD 2024-16-09](https://openairdocs.org/ad/2024-16-09): Fuselage · Boeing 777-200 Series, 777-200LR Series, 777-300ER Series and 2 more. Effective Nov 12, 2024 - [AD 2024-15-07](https://openairdocs.org/ad/2024-15-07): Fuel · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Oct 15, 2024 - [AD 2024-04-09](https://openairdocs.org/ad/2024-04-09): Instruments · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Apr 23, 2024 - [AD 2024-01-07](https://openairdocs.org/ad/2024-01-07): Flight controls · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Mar 7, 2024 - [AD 2023-21-09](https://openairdocs.org/ad/2023-21-09): Flight controls · Boeing 777-200LR Series, 777-200 Series, 777-300 Series and 2 more. Effective Dec 18, 2023 - [AD 2023-17-14](https://openairdocs.org/ad/2023-17-14): Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Sep 15, 2023 - [AD 2023-08-05](https://openairdocs.org/ad/2023-08-05): Fuselage · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jun 30, 2023 - [AD 2023-12-05](https://openairdocs.org/ad/2023-12-05): Navigation · Boeing 747-8F Series, 747-8 Series, 777-200 Series and 4 more. Effective Jun 21, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2023-03-04](https://openairdocs.org/ad/2023-03-04): Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Apr 4, 2023 - [AD 2022-23-10](https://openairdocs.org/ad/2022-23-10): Water/waste · Boeing 777F Series. Effective Jan 4, 2023 - [AD 2022-23-11](https://openairdocs.org/ad/2022-23-11): Fuel · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jan 4, 2023 - [AD 2022-14-05](https://openairdocs.org/ad/2022-14-05): Flight Controls · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Oct 12, 2022 - [AD 2022-13-18](https://openairdocs.org/ad/2022-13-18): Oxygen · Boeing 737-700 Series, 737-800 Series, 747-8 Series and 3 more. Effective Sep 15, 2022 - [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022 - [AD 2022-11-05](https://openairdocs.org/ad/2022-11-05): Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jul 20, 2022 - [AD 2022-06-07](https://openairdocs.org/ad/2022-06-07): Fuselage · Boeing 777-200 Series and 777-300 Series. Effective May 31, 2022 - [AD 2022-06-10](https://openairdocs.org/ad/2022-06-10): Powerplant · Boeing 777-200 Series and 777-300 Series. Effective Apr 15, 2022 - [AD 2022-06-11](https://openairdocs.org/ad/2022-06-11): Nacelles/pylons · Boeing 777-200 Series and 777-300 Series. Effective Apr 15, 2022 - [AD 2021-24-12](https://openairdocs.org/ad/2021-24-12): Fuel, Inert Gas System · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Feb 1, 2022 - [AD 2021-19-15](https://openairdocs.org/ad/2021-19-15): Equipment/furnishings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 1 more. Effective Jan 19, 2022 - [AD 2021-18-09](https://openairdocs.org/ad/2021-18-09): Fuselage · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Oct 22, 2021 - [AD 2021-13-02](https://openairdocs.org/ad/2021-13-02): Equipment/Furnishings · Boeing 777-300ER Series. Effective Aug 19, 2021 - [AD 2021-13-10](https://openairdocs.org/ad/2021-13-10): Wings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Aug 19, 2021 - [AD 2020-22-10](https://openairdocs.org/ad/2020-22-10): Equipment/furnishings · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 1 more. Effective Jan 14, 2021 - [AD 2020-18-12](https://openairdocs.org/ad/2020-18-12): Fuel · Boeing 777-200 Series, 777-200LR Series and 777-300 Series. Effective Oct 26, 2020 - [AD 2020-11-11](https://openairdocs.org/ad/2020-11-11): Fuel · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jun 18, 2020 - [AD 2020-05-24](https://openairdocs.org/ad/2020-05-24): Engine exhaust · Boeing 777-200 Series. Effective Apr 24, 2020 - [AD 2020-04-19](https://openairdocs.org/ad/2020-04-19): Auto flight · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Apr 21, 2020 - [AD 2019-25-14](https://openairdocs.org/ad/2019-25-14): Fuselage · Boeing 777-300ER Series and 777F Series. Effective Feb 10, 2020 - [AD 2019-25-12](https://openairdocs.org/ad/2019-25-12): Oxygen · Boeing 777-200 Series and 777-300ER Series. Effective Jan 21, 2020 - [AD 2019-19-10](https://openairdocs.org/ad/2019-19-10): Fuel · Boeing 737-300 Series, 737-400 Series, 737-500 Series and 21 more. Effective Jan 16, 2020 - [AD 2019-16-13](https://openairdocs.org/ad/2019-16-13): Fuel · Boeing 777-200 Series and 777-300 Series. Effective Nov 14, 2019 - [AD 2019-11-02](https://openairdocs.org/ad/2019-11-02): Fuselage · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 2 more. Effective Jul 5, 2019 - [AD 2018-26-05](https://openairdocs.org/ad/2018-26-05): Fuel · Boeing 777-200 Series, 777-200LR Series, 777-300 Series and 1 more. Effective Feb 1, 2019 - [AD 2018-25-11](https://openairdocs.org/ad/2018-25-11): Engine exhaust · Boeing 777-200 Series and 777-300 Series. Effective Jan 18, 2019 - [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018 - [AD 2018-14-08](https://openairdocs.org/ad/2018-14-08): Fuel · Boeing 777-200LR Series. Effective Jul 27, 2018 - [AD 2018-12-04](https://openairdocs.org/ad/2018-12-04): Equipment/furnishings · Boeing 777-300ER Series. Effective Jun 25, 2018 All 260: https://openairdocs.org/tcds/T00001SE/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Boeing 777-222](https://openairdocs.org/model/boeing-777-222): 52 aircraft (registry code 1385219) - [Boeing 777-223](https://openairdocs.org/model/boeing-777-223): 49 aircraft (registry code 1385213) - [Boeing 777F](https://openairdocs.org/model/boeing-777f): 47 aircraft (registry code 138527B) - [Boeing 777-300ER](https://openairdocs.org/model/boeing-777-300er): 24 aircraft (registry code 1385256) - [Boeing 777-224](https://openairdocs.org/model/boeing-777-224): 22 aircraft (registry code 1385225) - [Boeing 777-323ER](https://openairdocs.org/model/boeing-777-323er): 20 aircraft (registry code 1385324) - [Boeing 777-212](https://openairdocs.org/model/boeing-777-212): 13 aircraft (registry code 1385229) - [Boeing 777-200](https://openairdocs.org/model/boeing-777-200): 8 aircraft (registry code 1385218) - [Boeing 777-232LR](https://openairdocs.org/model/boeing-777-232lr): 8 aircraft (registry code 1385278) - [Boeing 777-232](https://openairdocs.org/model/boeing-777-232): 7 aircraft (registry code 1385232) - [Boeing 777-246](https://openairdocs.org/model/boeing-777-246): 7 aircraft (registry code 1385279) - [Boeing 777-237LR](https://openairdocs.org/model/boeing-777-237lr): 3 aircraft (registry code 1385272) - [Boeing 777-266](https://openairdocs.org/model/boeing-777-266): 3 aircraft (registry code 1385281) - [Boeing 777-289](https://openairdocs.org/model/boeing-777-289): 3 aircraft (registry code 1385241) - [Boeing 777-346](https://openairdocs.org/model/boeing-777-346): 3 aircraft (registry code 1385228) - [Boeing 777-367ER](https://openairdocs.org/model/boeing-777-367er): 3 aircraft (registry code 1385277) - [Boeing 777-219](https://openairdocs.org/model/boeing-777-219): 2 aircraft (registry code 1385800) - [Boeing 777-312](https://openairdocs.org/model/boeing-777-312): 2 aircraft (registry code 1385226) - [Boeing 777-381ER](https://openairdocs.org/model/boeing-777-381er): 2 aircraft (registry code 1385700) - [Boeing 777-236](https://openairdocs.org/model/boeing-777-236): 1 aircraft (registry code 1385220) - [Boeing 777-268](https://openairdocs.org/model/boeing-777-268): 1 aircraft (registry code 1385227) - [Boeing 777-200LR](https://openairdocs.org/model/boeing-777-200lr): 0 aircraft (registry code 1385275) - [Boeing 777-206](https://openairdocs.org/model/boeing-777-206): 0 aircraft (registry code 1385600) - [Boeing 777-228](https://openairdocs.org/model/boeing-777-228): 0 aircraft (registry code 1385234) - [Boeing 777-233LR](https://openairdocs.org/model/boeing-777-233lr): 0 aircraft (registry code 138004C) - [Boeing 777-240](https://openairdocs.org/model/boeing-777-240): 0 aircraft (registry code 1385501) - [Boeing 777-240LR](https://openairdocs.org/model/boeing-777-240lr): 0 aircraft (registry code 1385502) - [Boeing 777-243](https://openairdocs.org/model/boeing-777-243): 0 aircraft (registry code 1385282) - [Boeing 777-258](https://openairdocs.org/model/boeing-777-258): 0 aircraft (registry code 1385280) - [Boeing 777-260LR](https://openairdocs.org/model/boeing-777-260lr): 0 aircraft (registry code 1385321) - [Boeing 777-267](https://openairdocs.org/model/boeing-777-267): 0 aircraft (registry code 1385222) - [Boeing 777-269](https://openairdocs.org/model/boeing-777-269): 0 aircraft (registry code 1385235) - [Boeing 777-278](https://openairdocs.org/model/boeing-777-278): 0 aircraft (registry code 1385320) - [Boeing 777-281](https://openairdocs.org/model/boeing-777-281): 0 aircraft (registry code 1385239) - [Boeing 777-300](https://openairdocs.org/model/boeing-777-300): 0 aircraft (registry code 138525A) - [Boeing 777-306ER](https://openairdocs.org/model/boeing-777-306er): 0 aircraft (registry code 1385284) - [Boeing 777-309ER](https://openairdocs.org/model/boeing-777-309er): 0 aircraft (registry code 138527W) - [Boeing 777-312ER](https://openairdocs.org/model/boeing-777-312er): 0 aircraft (registry code 1385266) - [Boeing 777-316](https://openairdocs.org/model/boeing-777-316): 0 aircraft (registry code 138527J) - [Boeing 777-319ER](https://openairdocs.org/model/boeing-777-319er): 0 aircraft (registry code 138527N) - [Boeing 777-323](https://openairdocs.org/model/boeing-777-323): 0 aircraft (registry code 1385323) - [Boeing 777-328ER](https://openairdocs.org/model/boeing-777-328er): 0 aircraft (registry code 1385252) - [Boeing 777-333ER](https://openairdocs.org/model/boeing-777-333er): 0 aircraft (registry code 1385273) - [Boeing 777-336ER](https://openairdocs.org/model/boeing-777-336er): 0 aircraft (registry code 1385288) - [Boeing 777-337ER](https://openairdocs.org/model/boeing-777-337er): 0 aircraft (registry code 138004D) - [Boeing 777-340ER](https://openairdocs.org/model/boeing-777-340er): 0 aircraft (registry code 1385268) - [Boeing 777-346ER](https://openairdocs.org/model/boeing-777-346er): 0 aircraft (registry code 1385249) - [Boeing 777-360ER](https://openairdocs.org/model/boeing-777-360er): 0 aircraft (registry code 138527Y) - [Boeing 777-367](https://openairdocs.org/model/boeing-777-367): 0 aircraft (registry code 1385247) - [Boeing 777-368ER](https://openairdocs.org/model/boeing-777-368er): 0 aircraft (registry code 13852ER) All 51: https://openairdocs.org/tcds/T00001SE/aircraft.md ## STCs approved under this data sheet (540, first 50) - [STC ST03438NY](https://openairdocs.org/stc/ST03438NY): Installation of Adams Rite Lavatory Equipment. Delta Engineering Corporation - [STC ST12468SE](https://openairdocs.org/stc/ST12468SE): Removal of In-Flight Entertainment and Communications System. Space Exploration Technologies Corp./Starlink Aviation - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems - [STC ST12456IB](https://openairdocs.org/stc/ST12456IB): Thinkom Satcom Antenna Installation. EAD Aerospace Airworthiness T/A Eclipse Technics - [STC ST11270DS](https://openairdocs.org/stc/ST11270DS): Modification of the passenger cabin of the Boeing 777-323ER aircraft to install new business class seats, new premium economy seats, new economy seats, new class dividers, new and modified closets, new and modified galleys, new and modified lavatories, and new entertainment and connectivity systems. (777-323ER). American Airlines, Inc. Maintenance and Engineering (M&E) Division - [STC ST04738NY](https://openairdocs.org/stc/ST04738NY): Installation of Dual SpaceX Starlink Aero Terminals. Space Exploration Technologies Corp./Starlink Aviation - [STC ST04739NY](https://openairdocs.org/stc/ST04739NY): Installation of Dual SpaceX Starlink Aviation System. Space Exploration Technologies Corp./Starlink Aviation - [STC ST11835AT](https://openairdocs.org/stc/ST11835AT): Removal of floating panel from cabin interior partition and installation of vases and magazine racks. B/E Aerospace, Inc. - Aftermarket Services - [STC ST04474NY](https://openairdocs.org/stc/ST04474NY): Activation of Wireless Local Area Network (WLAN) system. Jet Aviation AG - [STC ST09851DS](https://openairdocs.org/stc/ST09851DS): Panasonic Server and Starlink to IFE & AID Interface Installation. United Airlines - [STC ST02256SE](https://openairdocs.org/stc/ST02256SE): Installation of an interior reconfiguration. B/E Aerospace, Inc. - FSI - [STC ST02308SE](https://openairdocs.org/stc/ST02308SE): First class furniture trim and finish change. B/E Aerospace, Inc. - FSI - [STC ST00750DE](https://openairdocs.org/stc/ST00750DE): Installation of an International Communications Group (ICG) Iridium Communication (SATCOM) system. L2 Aviation - [STC ST01849SE](https://openairdocs.org/stc/ST01849SE): Installation of an interior reconfiguration on Boeing Model 777-200 series airplanes.. B/E Aerospace, Inc. - FSI - [STC ST02162SE-D](https://openairdocs.org/stc/ST02162SE-D): Installation of an interior reconfiguration. B/E Aerospace, Inc. - FSI - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc. - [STC ST02073SE](https://openairdocs.org/stc/ST02073SE): Fabrication of a LiteAir window plug assembly. LiteAir Aviation Products Inc - [STC ST02312AT-D](https://openairdocs.org/stc/ST02312AT-D): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST02487AT-D](https://openairdocs.org/stc/ST02487AT-D): Installation of Flight Attendant Rest Seats and Door 3 Centerline Lavatories. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03380AT-D](https://openairdocs.org/stc/ST03380AT-D): Cabin re-configuration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03553AT-D](https://openairdocs.org/stc/ST03553AT-D): Installation of Aircraft Cabin Systems (ACS) 32 inch LCD Monitors.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03661AT-D](https://openairdocs.org/stc/ST03661AT-D): Installation of a Triple Seat in the Center Row 45 of a Boeing 777-200. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03664AT-D](https://openairdocs.org/stc/ST03664AT-D): Installation of a Cell Modem in a Boeing 777-200, for Operation on the Ground Only.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03928AT-D](https://openairdocs.org/stc/ST03928AT-D): Installation of an Audio Video On-Demand (AVOD) In-Flight Entertainment System and In-Seat Power System (ISPS) installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03961AT](https://openairdocs.org/stc/ST03961AT): Installation of TIMCO Aerosystems lavatories and bi-fold doors in the 2A-LC and 2A-RC lavatories. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04144AT](https://openairdocs.org/stc/ST04144AT): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04188AT](https://openairdocs.org/stc/ST04188AT): Installation of 32 Supplemental Oxygen Bottles. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04223AT](https://openairdocs.org/stc/ST04223AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04236AT](https://openairdocs.org/stc/ST04236AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04237AT](https://openairdocs.org/stc/ST04237AT): Installation of a Panasonic eX3 Audio Video On-Demand (AVOD) In-Flight Entertainment System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04245AT](https://openairdocs.org/stc/ST04245AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04246AT](https://openairdocs.org/stc/ST04246AT): Installation of a Panasonic eX3 Audio Video On-Demand (AVOD) In-Flight Entertainment System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04256AT](https://openairdocs.org/stc/ST04256AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04257AT](https://openairdocs.org/stc/ST04257AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04258AT](https://openairdocs.org/stc/ST04258AT): Panasonic IFE System Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04275AT](https://openairdocs.org/stc/ST04275AT): Installation of a HAECO cabin interior reconfiguration kit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04357AT](https://openairdocs.org/stc/ST04357AT): Cabin Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04385AT](https://openairdocs.org/stc/ST04385AT): Interior reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON LLC d/b/a MASS Systems - [STC ST02814LA](https://openairdocs.org/stc/ST02814LA): Installation of Lower Deck Civil Reserve Air Fleet (CRAF) Cargo System. Telair International - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST12282SE](https://openairdocs.org/stc/ST12282SE): Cargo loading system installation. B/E Aerospace, Inc. - FSI - [STC ST12333LA](https://openairdocs.org/stc/ST12333LA): Conversion of a Boeing 777-200LR all-passenger configuration to an all-cargo configuration airplane. Mammoth Freighters LLC - [STC ST12322AC](https://openairdocs.org/stc/ST12322AC): Installation of a Thales Aviator 200S satellite communication system. L2 Aviation - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc. - [STC ST02905NY](https://openairdocs.org/stc/ST02905NY): Installation of a Panasonic Avionics Corporation Global Communications Suite Antenna. Delta Engineering Corporation - [STC ST03161NY](https://openairdocs.org/stc/ST03161NY): Installation of a Panasonic Avionics Corporation Global Communications Suite (GCS). Delta Engineering Corporation - [STC ST03010CH](https://openairdocs.org/stc/ST03010CH): Installation of an advertisement container on the bottom of a seat back tray table. Atin OOH LLC - [STC ST04266CH](https://openairdocs.org/stc/ST04266CH): Modify the aircraft interior to match standard passanger configurations. Atin OOH LLC All 540: https://openairdocs.org/tcds/T00001SE/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.