# TCDS A2NM: The Boeing Company - Type: Type certificate data sheet - Status: Current - Holder: The Boeing Company - Revision: 32 - Revised: February 16, 2016 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Registered aircraft: 283, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/63/35/633543413e7cbd4d1246f1328adaee0d119cda77fb02f8752ce1af0c0d9f0291 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E114C6BAFEC130A086257F5B007AEB12.0001 - Page: https://openairdocs.org/tcds/A2NM ## Models (4) As the data sheet lists them. - 757-200CB Series - 757-200PF Series - 757-300 Series - 757-200 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 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 Rev. No. 32 30 23 23 32 32 32 32 31 32 32 31 31 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A2NM Revision 32 BOEING 757-200 Series 757-200PF Series 757-200CB Series 757-300 Series February 16, 2016 TYPE CERTIFICATE DATA SHEET A2NM This data sheet, which is part of Type Certificate No. A2NM, 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 1901 Oakesdale Avenue SW Renton, WA 98057-2623 I - Model 757-200 (approved December 21, 1982) Engines: 2 Rolls-Royce RB211-535-C-37, 2 Rolls-Royce RB211-535-E4-37, 2 Rolls-Royce RB211-535-E4-B-37, 2 Pratt & Whitney PW2037, 2 Pratt & Whitney PW2037(M) or 2 Pratt & Whitney PW2040; refer to the FAA-Approved Airplane Flight Manual for aircraft engine intermix eligibility. Fuel: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Engine Ratings Takeoff static thrust Maximum continuous static standard day, sea level thrust, standard day, conditions (5 min) lb. sea level conditions lb. RR RB211-535-C-37 36,720 33,500 RR RB211-535-E4-37 39,610 35,205 RR RB211-535-E4-B-37 42,540 35,205 P&W PW2037 37,530 34,640 P&W 2037(M) 37,530 34,640C P&W PW2040 40,900 34,640 For engine operating limits see engine TC Data Sheet No. E12EU for the RR RB211-535-C- 37, RB211-535-E4-37, or RB211-535E4-B-37 engine; TC Data Sheet No. E17NE for the P&W PW2037, P&W2037 (M) or PW2040, or the FAA-Approved Airplane Flight Manual. Except for RR RB211-535-C-37 engine, 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 = 350 KCAS/.86 M VLE = 270 KCAS/.82 M VLO = 270 KCAS/.82 M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. CG Range: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. A2NM 2 I. Model 757-200 (cont’d): Maximum Weights: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Model Eligible Serial Numbers 757-204 25623, 25626, 26266, 26267, 26962-26967, 27208, 27219, 27220, 27234-27238, 28834, 28836 757-208 24739, 24760, 25085, 28989, 29436, 30423, 30424 757-212 23125-23128 757-222 24622-24627, 24743, 24744, 24763, 24780, 24799, 24809, 24810, 24839, 24840, 24860, 24861, 24871, 24872, 24890, 24891, 24931, 24932, 24977, 24978, 24994, 24995, 25018, 25019, 25042, 25043, 25072, 25073, 25129, 25130, 25156, 25157, 25222, 25223, 25252, 25253, 25276, 25277, 25322, 25323, 25367, 25368, 25396-25399, 25698, 26641, 26644, 26647, 26650, 26653, 26654, 26657, 26660, 26661, 26664, 26665, 26666, 26669, 26670, 26673, 26674, 26677, 26678, 26681, 26682, 26685, 26686, 26689, 26690, 26693, 26694, 26697, 26698, 26701, 26702, 26705, 26706, 26709, 26710, 26713, 26717, 28142-28145, 28707, 28708, 28748-28751 757-223 24486-24491, 24524-24526, 24577-24617, 25294-25301, 25333-25343, 25695-25697, 25730, 25731, 26972-26977, 26980, 27051-27058, 27446, 27447, 29423-29428, 29589-29594, 31308, 32379-32400 757-224 27291-27302, 27555-27567, 28966-28971, 29281-29285, 30229, 30351-30354 757-225 22191-22211, 22611, 22612, 22688-22691 757-230 24737, 24738, 24747-24749, 25140, 25436-25441, 25901, 26433-26436 757-231 28479-28488, 29378, 29385, 29954, 30319, 30338-30340 757-232 22808-22823, 22907-22920, 23612-23615, 23760-23763, 23993-23998, 24216-24218, 24372, 24389-24396, 24419-24422, 24972, 24991, 24992, 25012, 25013, 25034, 25035, 25141, 25142, 25331, 25332, 25977-25983, 26955-26958, 27103, 27104, 27585-27589, 29724- 29728, 29911, 29970, 30187, 30188, 30234, 30318, 30337, 30395-30397, 30422, 30480- 30486, 30777, 30838, 30839 757-236 22172-22190, 23227, 23398-23400, 23492, 23493, 23532, 23533, 23710, 23975, 24072- 24074, 24101, 24102, 24118-24122, 24266-24268, 24370, 24371, 24397, 24398, 24771, 24772, 24792-24794, 24882, 25053, 25054, 25059, 25060, 25133, 25592, 25593, 25597, 25598, 25620, 25806-25808, 28665-28667, 29113-29115, 29941-29946 757-251 23190-23209, 23616-23620, 23842-23846, 24263-24265, 26482-26501, 33391-33393 757-256 26239-26254, 29306-29312, 30052 757-258 23917, 23918, 24254, 24884, 25036, 26053, 26054, 27622 757-260 25014, 25353, 26057, 26058 757-21B 24014-24016, 24330, 24331, 24401, 24402, 24714, 24758, 24774, 25083, 25258, 25259, 25884, 25888-25890 757-21K 28674 757-22K 28336, 28337, 30863 757-22L 29304, 29305, 30834 757-23A 24289-24293, 24527, 24528, 24566, 24567, 24636, 24923, 24924, 25345, 25487-25495 757-23N 27598, 27971- 27976, 29330, 30232, 30233, 30548, 30735, 30886, 30887 757-23P 28338, 30060, 30061 757-24Q 28463 757-25C 25898-25900, 27513, 27517, 32941, 32942, 34008, 34009 757-25F 28718, 30757, 30758 757-26D 24471-24473, 27152, 27183, 27342, 27681, 28446, 33959-33961, 33966, 33967 757-27A 29607-29611 757-27B 24135-24137, 24838 757-28A 23767, 23822, 24017, 24235, 24260, 24367-24369, 24543, 24544, 25621, 25622, 26269, 26274-26277, 27621, 28161, 28164, 28166, 28171, 28174, 28203, 28833, 28835, 29381, 30043, 32446- 32449, 33098-33101 757-28S 29215-29217, 32341-32343 757-29J 27203, 27204 3 A2NM I. Model 757-200 (cont’d): 757-2B6 23686,23687 757-2B7 27122-27124, 27144-27148, 27198-27201, 27244-27246, 27303, 27805-27811 757-2F8 23850 757-2G4 29025-29028 757-2G5 23118, 23119, 23651, 23928, 23929, 23983, 24176, 24451, 24497, 26278, 28112, 29379, 29488, 29489, 30394 757-2G7 24233, 24522, 24523 757-2J4 25155, 25220 757-2K2 26330, 26633-26635 757-2M6 23452-23454 757-2Q8 24964, 24965, 25044, 25131, 25624, 26268, 26270-26273, 26332, 27351, 27599, 27620, 27623-27625, 28160, 28162, 28163, 28165, 28167-28170, 28172, 28173, 29377, 29380, 29382, 29442, 29443, 30044-30046 757-2S7 23321-23323, 23566-23568 757-2T7 22780, 22781, 22960, 23293, 23770, 23895, 24104, 24105 757-2Y0 25240, 25268, 26151-26156, 26158, 26160, 26161 757-2Z0 25885-25887, 27258-27260, 27269, 27270, 27367, 27511, 27512, 29792, 29793 II - Model 757-200PF (approved September 3, 1987) The Model 757-200PF (Package Freighter) is a derivative of the Model 757-200 and is designed for commercial transportation of palletized and bulk cargo. Major configuration changes from the Model 757-200 are as follows: One main cargo compartment door, with an opening 134 inches wide and 86.5 inches high, is installed in the left side of the forward fuselage. All passenger doors are deleted and a new crew entry door is added to the forward left side. All passenger windows are deleted. Passenger floor is modified for cargo pallets or containers. A 9G cargo barrier is installed behind the flight deck. The Maximum Zero Fuel Weight and Maximum Landing Weight are increased. Engines: 2 Pratt & Whitney PW2037, 2 Pratt & Whitney PW2037(M), 2 Pratt & Whitney PW2040, or 2 Rolls-Royce RB211-535-E4-37, 2 Rolls Royce RB211-535-E4-B-37; refer to FAA- Approved Airplane Flight Manual for aircraft engine intermix eligibility. Fuel: See the appropriate FAA-Approved Flight Manual listed in Note 2. Engine Takeoff static thrust Maximum continuous static Ratings: standard day, sea level thrust, standard day, conditions (5 min) lb. sea level conditions lbs. P&W PW2037 37,530 34,640 P&W PW2037 (M) 37,530 34,640 P&W PW2040 40,900 34,640 RR RB211-535-E4-37 39,610 35,205 RR RB211-535-E4-B-37 42,540 35,205 For engine operating limits, see engine TC Data Sheet No. E17NE for the P&W PW2037, PW2037(M) or PW2040; engine TC Data Sheet No. E12EU for RR RB211-535-E4-37, RB211-535-E4-B-37; or the FAA-Approved Airplane Flight Manual. 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. A2NM 4 Model 757-200PF (cont’d): Airspeed Limits: VMO = 350 KCAS/.86 M VLE = 270 KCAS/.82 M VLO = 270 KCAS/.82 M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. CG Range: See the appropriate FAA-Approved Flight Manual listed in Note 2. Maximum Weights: See the appropriate FAA-Approved Flight Manual listed in Note 2. Model Eligible Serial Numbers 757-23APF 24456, 24635, 24868, 24971 757-24APF 23723-23732, 23851-23855, 23903-23907, 25281, 25324, 25325, 25369, 25370, 25457- 25486, 27386-27390, 27735-27739, 28265-28269, 28842-28846 757-260PF 24845 III - Model 757-200CB (approved September 7, 1988) The Model 757-200CB (Combi) is a derivative of the Model 757-200 and is designed for commercial transportation of passengers and a maximum of two cargo pallets. A partition is installed between the passenger and main deck cargo. Engines: 2 Rolls-Royce RB211-535-E4-37 engines. Fuel: See the appropriate FAA-Approved Flight Manual listed in Note 2. Engine Ratings: Takeoff static thrust Maximum continuous standard day, sea level static thrust, standard day conditions (5 min) lb. sea level conditions lb. RR RB211-535-E4-37 39,610 35,205 For engine operating limits see engine TC Data Sheet No. E12EU for the RR RB211-535-E4- 37 or the FAA-Approved Airplane Flight Manual. 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 = 350 KCAS/.86 M VLE = 270 KCAS/.82 M VLO = 270 KCAS/.82 M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. CG Range: See the appropriate FAA-Approved Flight Manual listed in Note 2. Maximum Weights: See the appropriate FAA-Approved Flight Manual listed in Note 2. Model Eligible Serial Number 757-2F8CB 23863 5 A2NM IV - Model 757-300 (approved January 22, 1999) Engines: 2 Rolls-Royce RB211-535E4-37 or 2 Rolls-Royce RB211-535E4-B-37 or 2 Rolls-Royce RB211-535E4-C-37. Refer to FAA-Approved Airplane Flight Manual for aircraft engine intermix eligibility. 2 Pratt & Whitney PW2037, 2 Pratt & Whitney PW2040, or 2 Pratt & Whitney PW2043. Refer to FAA-Approved Airplane Flight Manual for aircraft engine intermix eligibility. Fuel: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Engine Ratings: Takeoff static thrust, Maximum continuous static standard day, sea level thrust, standard day, sea conditions, (5 min), lbs. level conditions, lb. RR RB211-535E4-37 39,610 35,205 RR RB211-535E4-B-37 42,540 35,205 RR RB211-535E4-C-37 42,540 35,205 P & W PW2037 37,530 34,640 P & W PW2040 40,900 34,640 P & W PW2043 43,000 36,420 For engine operating limits, see engine TC Data Sheet No. E12EU for the RB211-535E4-37, RB211-535E4-B-37 or RB211-535E4-C-37 engine or FAA-approved Airplane Flight Manual. 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. For PW2037, PW2040 and PW2043 engine operating limits see engine TC Data Sheet E17NE or the FAA-Approved Airplane Flight Manual. 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 = 350 KCAS/.86 M VLE = 270 KCAS/.82 M VLO = 270 KCAS/.82 M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. CG Range: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Maximum Weights: See the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Model Eligible Serial Numbers 757-308 29434 757-324 32810-32818 757-330 29012-29023, 30030 757-351 32981-32996 757-3CQ 32241, 32242 757-3E7 30178, 30179 757-33N 32584-32593, 33525, 33526 Data Pertinent to all Models: Production Basis: Production Certificate No. 700 A2NM 6 Data Pertinent to All Models (cont'd): Minimum Crew: Two (2): pilot and co-pilot. For 757-200CB: The airplane minimum crew must include an individual who is dedicated, trained cargo fire fighter when cargo is carried in the main deck Class "B" cargo compartment. This required crew member is in addition to those required by FAR 121.385 and 121.391. Maximum Passengers: For 757-200 and 757-200CB airplanes the total passenger capacity is limited to: 219 (Four pair of Type I exits) 239 (Three pair of Type I exits plus one pair of improved Type I exits at Door No. 2). See Note 5. 224 (Three pair of Type I exits plus two pair of Type III exits) 164 (757-200CB in two pallet main deck cargo configuration), limited by 25.807(c) 0 (757-200PF) 2 crew, 5 persons per Exemption No. 4808 For 757-300 airplanes, the total passenger capacity is limited to: 275 (Three pair of Type C exits, one pair of Type I exits and two pair of Type III exits). 295 (Two pair of Type C exits, one pair of Type B exits, one pair of Type I exits, and two pair of Type III exits). Maximum Baggage/Cargo: See Weight and Balance Manual Boeing Document No. D043N302. Fuel and Oil Capacities: See Weight and Balance Manual Boeing Document No. D043N302. Maximum Operating Altitude: 42,000 ft. Leveling Means: Two inclinometers, plumb bob support and target (scale), right main gear well. Datum: Sta. 0.0, located 159 inches forward of airplane nose (B.S.159) MAC: 199.7 inches Control Surface Movements: 757-200 Series: Control surfaces must be rigged in accordance with Boeing Drawings 251N1001, 251N2001, 251N3001, 251N4001, 251N5001, 254N1001, and 275N2001. 757-300 Series: Control surfaces must be rigged in accordance with Boeing Drawings: Lateral and Speedbrake Control 251N1018; Elevator Control System 251N2007; Rudder Control System 251N3038; Stabilizer Trim Control 251N2001 Compliance with the following optional requirements has been established for all Models: Ditching Provision 25.801 (Overwater operation can be approved when the aircraft has been equipped and has been approved according to FAR 25.801) Ice Protection Provisions 25.1419 7 A2NM Data Pertinent to All Models (cont'd): Required Equipment: The basic required equipment as prescribed in the applicable Federal Aviation Regulations must be installed in the aircraft. Service Information: The following Boeing "Structural Repair Manual" Documents are FAA-approved: 757-200 D634N201 757-200CB D634N211 757-200PF D634N210 757-300 D634N230 Compliance with 14 CFR §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 demostrate 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 Exemptions from 14 CFR part 25: 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) Service Bulletins and other service information when FAA-approved will carry a statement to that effect. Certification Basis for 757-200/200CB/-200PF: Federal Aviation Regulations (FAR) Part 25 with Amendments 25-1 through 25-45 effective December 1, 1978, except Section 25.109 Amendment 25-42, 25.345 Amendment 25-46, 25.351(a) Amendment 25-46, 25.365(e)(1) and (2) Amendment 25-54 (aft cargo compartment); 25.365(e)(1) and (2) Amendment 25-0 (forward cargo compartment) (See Note 11); 25.571 Amendment 25-45, 25.629 Amendment 25-46,25.697 Amendment 25-46, 25.733 Amendment 25-49, 25.803(c) and (d) Amendment 25-46, 25.901(d), 25.1103(a),(b)(2),(d), (e), and (f) Amendment 25-46, 25.1142 and 25.1522 Amendment 25-46. Federal Aviation Regulations (FAR) Part 36 with Amendments 36-1 through 36-12 effective August 1, 1981. Stage 3 or Stage 4 Noise Compliance: Stage 4 Amendment 28 noise compliance with the appropriate Service Bulletin, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Special Federal Aviation Regulation 27. Equivalent safety findings exist with respect to the following regulations: 25.251 Vibration and buffeting (documented in TAD ELOS Memo 10336-1-F-1) 25.791 Passenger Information Signs and Placards 25.803(c)(8) Emergency Evacuation Demonstration 25.807(c) Passenger Emergency Exits 25.809(f)(1)(ii) Escape Slide Automatic Erection 25.811(e)(3) Amdt 25-46, Type III Exit Handle Illumination 25.811(f) (2) Exit Band Contrast A2NM 8 Certification Basis for 757-200/200CB/200PF (cont'd): 25.811(f) Emergency Exit Marking (documented in ELOS Memo TD6444SE-T-C-1) 25.812(b)(1)(i) Emergency Exit Locator and Marking Signs 25.813(c) Type III Emergency Exit Access (documented in TAD ELOS Memo CT1192NW-D-C-1) 25.853(a) Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08-0670-C-1) 25.853(c) Compartment Interiors 25.901(d) Auxiliary Power Unit Installation 25.981(a)(3) Amdt 25-102, Installation of Ground Fault Interrupter (GFI) Relays (documented in ELOS Memos PS05-0123-P-1 and PS-05-0123-P-1, Revision 1) 25.981(b)(2) Amdt 25-125, Fuel Tank Flammability Rule (FTFR) (Documented in ELOS Memo PS05- 0177-P-2) 25.1301 Model 757 Instrument Switching 25.1305(a)(4), (a)(6), (c)(1), and (c)(3) - Auxiliary Power Unit Instruments 25.1309(a) Model 757 Instrument Switching 25.1415(c) Survival Equipment 25.1415(d) Emergency Locator Transmitter (ELT) 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) 25.1443(c) Minimum mass flow of supplemental oxygen (documented in TAD ELOS Memo TS13-0005-S- 1) 25.1522 Auxiliary Power Unit Limitations 25.1549(b) Powerplant and Auxiliary Power Unit Instruments 25.1555(d)(1) Control markings (documented in TAD ELOS Memorandum PS06-0496-F-18) Exemption from FAR Part 25: Exemption No. 5613 was granted on March 5, 1993 Exemption from FAR 25.1415(c) for survival kit attachment requirements. (Subject to Operational Procedures) Partial Exemption No. 9405 granted on July 18, 2007 – Partial Exemption from 25.901(c), Thrust Control Malfunction Accommodation and Single Failures of Thrust Levers. See note 14 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) Exemption No. 13180 granted on October 9, 2015- Exemption from SFAR 88, and §§ 25.901(c) and 25.981(a)(3), as they pertain to fuel-tank-ignition prevention associated with the FQIS, limited to in-service 757-200 (freighter only) and 757-200PF center wing tank (CWT) Fuel Quantity Indication System (FQIS) fuselage-wiring installation. For 757-200PF: Same as 757-200 airplane plus FAR 25.783, as amended by Amendment 25-54, applicable only to the main deck cargo door, the crew entry door, and the flight deck first officer's No. 2 window; and FAR 25.723(a), Amendment 25-46. Equivalent Safety Findings exist with respect to the following Regulations (for 757-200PF): FAR 25.855(e) Cargo and Baggage Compartments FAR 25.1447(c)(1) and (3) Equipment Standards for Oxygen Dispensing Units. Exemption from FAR Part 25 (for 757-200PF): Exemption No. 4808 was granted on June 9, 1987 - Exemption from FAR’s 25.783(g), 25.807(c)(1), 25.809(f), and 25.813(b) - to allow the carriage in the flight deck of not more than five persons other than flight crew members. Exemption No. 4808A granted on April 17, 1997 in addition allowed the removal of the escape slides and permitted the installation of inertia reels and harness for each occupant in lieu of a rope as the escape means as specified in Exemption 4808. 9 A2NM Certification Basis for 757-200/200CB/200PF (cont'd): Exemption No. 4808B granted on November 5, 1998 clarified condition 3 in Exemption 4808A allowing that “initial and recurrent training may be via an oral briefing”. For 757-200CB: Same as 757-200 airplane plus 25.783 Amendment 25-54, applicable only to the main deck cargo door and FAR 25.783(a), Amendment 25-46. Certification Basis For 757-300: Part 25 as amended by Amendments 25-1 through 25-85 for the complete airplane with the exceptions listed below; SECTION NO. TITLE AT AMDT. 25.- 25.101 General 92 25.105 Takeoff 92 25.109 Accelerate-stop distance 92 25.113 Takeoff distance and takeoff run 92 25.115 Takeoff flight path 92 25.365 Pressurized cabin load 54 25.519 Jacking and Tie-Down Provisions. not part of the TC basis 25.562 Emergency Landing Dynamic Conditions. 85* 25.571 Damage Tolerance and Fatigue Evaluation of Structure. 45 25.735 Brakes 92 25.783 Doors. 23, 85** 25.807 Emergency exits 88 25.810 Emergency egress assist means and escape routes 88 25.813 Emergency exit access 75, 88*** 25.853(d)(3) Improved Flammability Standards for Material Used in Compartment Interiors 72 25.858(a) Cargo Compartment Fire Detection System not part of the TC basis 25.1316 System Lightning Protection 85** 25.1419(c) Ice Protection Flight Deck Indication 23 25.1533 Additional operating limitations 92 * Flight attendant seats are qualified to Technical Standard Order C127. Passenger and flight deck seats comply with 25.562(a), (b), ((c (1), (2), (3), (4), (7), and (8)). Flight deck seats also comply with § 25.562(c)(5). Stretchers are not required to comply with §25.562, for transporting non-ambulatory occupants. ** Applicable to new and significantly modified structure and systems and portions of the airplane affected by these changes. Where two amendment levels are shown for the same paragraph, the number without the asterisk (**) applies to structures, systems and portions of the airplane, which are not new or significantly modified. The structure, systems, and components, which comply with the later amendment, will be identified in a Boeing drawing approved by the FAA and JAA. *** Boeing has complied with §25.813 at Amendment 25-88 except for §25.813(c), which used Amendment 25-75. In addition, Boeing is providing a 13 inch aisle with a 6½ inch offset with 2 inches of cushion compression to clear the exit opening. Or, two 6 inch wide passageways that lead to an unobstructed space adjacent to each exit. Also, Boeing has complied with the placarding requirements of §25.813(c)(3) at Amendment 25-88. (Reference Issue Paper C-5) Part 34, through Amendment 34-1, effective July 31, 1995 Part 36, with Amendments 36-1 through 36-21, effective December 28, 1995 A2NM 10 Certification Basis For 757-300 (cont’d): Stage 3 or Stage 4 Noise Compliance: Stage 4 Amendment 28 noise compliance with the appropriate Service Bulletin, see the appropriate FAA-Approved Airplane Flight Manual listed in Note 2. Special Conditions for the following subjects were issued in Renton, Washington and are applicable to the 757-300. 1. High Intensity Radiated Fields (HIRF) 2. Engine Torque Loads for Sudden Engine Stoppage Equivalent Safety Findings: The equivalent Safety findings were proposed in accordance with §21.21. The following Equivalent Safety Findings have been identified for the 757-300 airplane: 25.21(b) Proof of compliance 25.103 Stalling speed. 25.107(b)(1), (C)(3) & (g) Takeoff speeds 25.111(a) Takeoff path 25.119(b) Landing climb: All-[engines]-operating 25.121(c), (d), & (d)(3) Climb: One-engine-inoperative 25.125(a)(2) Landing 25.143(g) General 25.145(a), (a)(1), (b)(1) - (4), (b)(6), & (c) Longitudinal control 25.147(a), (a)(2), (c), (d) Directional and lateral control 25.149(c) Minimum control speed 25.161(b), (c)(1), (c)(2), (c)(3), (d), & (e)(3) Trim 25.175 Demonstration of static longitudinal stability 25.177(c) Static directional and lateral stability 25.181(a), (b) Dynamic stability 25.201(a)(2), & (b)(4) Stall demonstration 25.207(b), (c), (d), (e), & (f) Stall warning 25.231(a)(2) Longitudinal stability and control 25.233(a) Directional stability and control 25.237(a), (b)(1) and (b)(2) Wind velocities 25.561 General 25.562 Emergency landing dynamic conditions 25.571 Damage Tolerance & Fatigue evaluation of structure 25.613 Material Strength Properties and Design Values 25.735(f)(2), (g) Brakes 25.773(b)(1)(i) Pilot compartment view 25.791 & 25.853 No ashtrays/Passenger Information Signs 25.810(a)(1)(ii) Escape Slides-Manual Inflation at Low Sill Heights 25.811(f) Emergency exit marking (documented in ELOS Memo TD6444SE-T-C-1) 25.812(b)(1)(i) Emergency Lighting-Text Height to Stroke-Width Ratio 25.813(c)(1) Emergency Exits/Emergency Exit Access-Cushion compression 25.853(a) Adhesives used in interior panel bent joint potting applications (documented in TAD ELOS Memo PS08- 0670-C-1) 25.901(d) Installation (Auxiliary Power Unit) 25.933(a)(1)(ii) Reversing Systems 25.981(a)(3) Amdt 102 Installation of Ground Fault Interrupter (GFI) Relays (documented in ELOS Memos PS05-0123-P-1 and PS-05- 0123-P-1, Revision 1) 25.981(b)(2) Amdt 125 Fuel Tank Flammability Rule (FTFR) (documented in TAD ELOS Memo PS05-0177-P-2). Certification Basis For 757-300 (cont’d): 11 A2NM 25.1001(c)(1) & (c)(3) Fuel jettisoning system 25.1103(e) Induction system ducts and air duct systems - (APU) 25.1303(c)(1) Airplane Overspeed Warning-unique aural warning 25.1305 Powerplant instruments 25.1323(c)(1), & (c)(2) Airspeed indicating system 25.1325(e) Static pressure systems 25.1337 Powerplant instruments 25.1389(b)(3) Position light distribution and intensities 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) 25.1443(c) Minimum mass flow of supplemental oxygen (documented in TAD ELOS Memo TS13-0005-S-1) 25.1522 Auxiliary power unit limitations 25.1549 Powerplant and auxiliary power unit instruments 25.1555(d)(1) Control markings (documented in TAD ELOS Memorandum PS06-0496-F-18) 25.1587(b)(2) Performance information Exemptions: Exemptions were requested in accordance with Paragraph 11.25. The following exemptions have been granted for the 757-300: Floor Warpage for Flight Deck Seats Exemption from FAR 25.562(b)(2), (Exemption No. 6600, issued April 8, 1997). Partial exemption from FAR 25.1435(b)(1), Hydraulic Proof Pressure Test (Exemption No. 6577, issued February 25, 1997). Ditching Equipment FAR 25.1415(c) Exemption No. 5613A, issued August 5, 1998). Exemption from 14 CFR Paragraph 25.961(a)(5) to allow a temperature limitation of 85°F for JP-4 and Jet B Type fuels (with RB211-535E4 series engines: Exemption No. 6867, issued February 24, 1999; with PW2037, PW2040, and PW2043 engines: Exemption No. 7790, issued June 3, 2002). Exemption from 14 CFR Paragraph 25.901(c) as it relates to single failures resulting in uncontrollable high thrust conditions with Pratt & Whitney PW2037, PW2040 and PW2043 engines. (Exemption No. 7798, issued June 4, 2002). See Note 14. Partial Exemption No. 9405 granted on July 18, 2007 – Partial Exemption from 25.901(c), Thrust Control Malfunction Accommodation and Single Failures of Thrust Levers. In the interest of standardization, as of the date of issuance this Partial grant of Exemption should be used in lieu of Exemption No. 7798. See note 14 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) NOTES APPLY TO ALL MODELS UNLESS OTHERWISE SPECIFIED: Note 1. A current weight and balance report including list of equipment included in certificated empty weight, and loading instructions must be in each aircraft at the time of original certification and at all times thereafter except in the case of operators having an approved weight control system. A2NM 12 NOTES APPLY TO ALL MODELS UNLESS OTHERWISE SPECIFIED (cont’d): The aircraft must be loaded so that the C.G. is within specified limits at all times, considering fuel loading and usage, gear retraction, and movement of crew and passengers from their assigned positions. Note 2. The aircraft must be operated in accordance with the FAA-Approved Airplane Flight Manual. All placards required in either the FAA-Approved Airplane Flight Manual, the applicable operating rules or the Certification Basis must be installed in the airplane. Boeing Document No. D631N001 is the basic FAA-Approved Flight Manual for Model 757-200 airplanes powered by RB211-535-C-37 engines. Boeing Document No. D631N002 is the basic FAA-Approved Flight Manual for Model 757-200 airplanes powered by P&W 2037 and P&W 2040 engines, and for Model 757-200PF airplanes powered by P&W 2037 and 2040 engines. Boeing Document No. D631N005 is the basic FAA-Approved Flight Manual for Model 757-200 airplanes powered by RB211-535-E4-37 and RB211-535-E4-B-37 engines, and for Models 757- 200PF and 757-200CB powered by RB211-535-E4-37 engines. Boeing Document No. D631N007.F00 is the basic FAA-Approved Flight Manual for Model 757- 300 airplanes powered by RB211-535E4-37, RB211-535E4-B-37, or RB211-535E4-C-37 engines. Boeing Document No. D631N007.F01 is the basic FAA-Approved Flight Manual for Model 757- 300 airplanes powered by PW2037, PW2040 or PW2043 engines. Note. 3 The FAA-approved Airworthiness Limitations and Certification Maintenance Requirements (Section 9) of Boeing document D622N001-9 lists the required inspection thresholds for certain structural items, the retirement times for safe-life parts, and the Certification Maintenance Requirements (CMR). All Boeing model 757 airplanes must fully comply with the appropriate revision of this section. However, regarding the damage tolerance structural inspections contained in Subsection (B) of this section, all Boeing Model 757-200 airplanes production line number 765 and on, must comply with Revision May 1997, or a later FAA approved revisions. Applicable to all 757-200 airplanes with production numbers lower than 765, the FAA issued Airworthiness Directive AD 2001-20-12, mandating compliance with Revision May 1997 or Revision November 1998 of Section 9. For all 757-200 airplanes equipped with PW2000 series engines, Airworthiness Directive AD 94-01-10 mandated compliance with certain inspections that are now contained within Section 9 as CMRs. For airplanes affected by these ADs, each subsequent revision to Section 9 must be approved as an alternative method of compliance (AMOC). All 757-300 airplanes equipped with Rolls-Royce RB211-535E4 series engines must comply with Revision November 1998 (or later FAA-approved revisions). All 757-300 airplanes equipped with W2000 series engines must comply with Revision May 2002 (or later FAA approved revisions). Note 4. Crew procedures identified as required by engineering failure analyses in Document D230N405 must not be changed unless approved by FAA engineering. Note 5. Door No. 2 must meet the requirements of FAR 25.807(a)(7)(ii) through (viii). Note 6. Certification Maintenance Requirements (CMR): The CMRs are listed in either the FAA- approved Section 9 of the Maintenance Planning Data document D622N001-9 (Airworthiness Limitations and Certification Maintenance Requirements), or the applicable engine Type Certificate Data Sheet. The more restrictive requirement from these two documents shall be in force. 13 A2NM NOTES APPLY TO ALL MODELS UNLESS OTHERWISE SPECIFIED (cont’d): Note 7. There are service bulletins which call for modifications which do not comply with the Type Certification Basis. These service bulletins are listed in Boeing Document D624N001 titled "Service Bulletin 757". The records of airplanes imported into the United States should be reviewed to ensure compliance, if the non FAA-approved service bulletins modifications have been installed. Note 8. Airplane line numbers 182, 189, and on, were manufactured on or after August 20, 1988, and airplane line numbers 258, 306 and on, were manufactured on or after August 20, 1990. Reference FAR 121.312(a)(1) and (2), Amendment 121-198. Airplanes 306 through 317 are exempt (Exemption No. 5176A). See Service Bulletin Index Part 3 for cross reference of line number to airplane serial number. Note 9. The type design reliability and performance of the Model 757-200, -200PF, -200CB, and -300 series airplanes have been evaluated in accordance with FAA Advisory Circular 120-42A and found suitable for Extended Range Operations with Two-Engine Airplanes (ETOPS) when operated and maintained in accordance with Boeing Document D011N002 "Configuration, Maintenance, and Procedures for Extended Range (ER) Operation Model 757". Note 10. The Model 757-300 series 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 draft 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 11. The aft cargo compartment is certified for a 6.2 square foot opening. The forward cargo compartment is certified for a 5.7 square foot opening. (Reference FAA Letter ANW-120S: 8110- 5, dated December 17, 1980. Note 12. The location of the flight attendant seats demonstrated to comply with the direct view requirements of FAR 25.785(h)(1); for the Boeing 757-300, are shown on the manufacturers “Interior Certification Diagram”. Note 13. For 757-300 with RB211-535E4 series engines only: For non-flight operations, static engine thrust is limited to 1.2 EPR when the ambient air temperature is 110°F or more. Note 14 The FAA has concluded that the occurrence of any uncontrollable high thrust failure condition, or any of the associated causal failures listed in Boeing Document D332N402, "may endanger the safe operation of an airplane" and hence are reportable under §121.703(c), 125.409(c) and 135.415(c). A copy of D332N402 or a listing of reportable failures shall be provided in the Limitations Section, Section 9, of the Maintenance Planning Document. Note 15: Mandatory replacement times, inspection intervals, related inspection procedures and all critical design configuration control limitation 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 757 Maintenance Planning Data Document D622N001-9, Revision January 2006 or later FAA-approved revision. Note 16: Certification Basis for §14 CFR 25.981 at Amendment 25-125, and Equivalent Safety Finding P- 2, dated May 25, 2010, for the Flammability Reduction System (FRS), is applied if fuel tank inerting is installed as a modification on existing in service aircraft per Boeing Service Bulletin 757-47-0001. Airworthiness Limitations for the FRS are contained in Section 9 of the applicable Maintenance Planning Document. ....END..... ``` ## ADs (364, first 50, in force first) - [AD 2026-20-04](https://openairdocs.org/ad/2026-20-04): Fuselage · Boeing 757-300 Series. Effective Nov 5, 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 2026-13-16](https://openairdocs.org/ad/2026-13-16): Navigation · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 6 more. Effective Jul 1, 2026 - [AD 2026-08-09](https://openairdocs.org/ad/2026-08-09): Wings · Boeing 757-200 Series and 757-300 Series with STC ST01518SE. Effective Jun 3, 2026 - [AD 2026-04-06](https://openairdocs.org/ad/2026-04-06): Wings · Boeing 757-200 Series and 757-300 Series. Effective Feb 26, 2026 - [AD 2026-01-05](https://openairdocs.org/ad/2026-01-05): Wings · Boeing 757-200 Series and 757-300 Series. Effective Feb 20, 2026 - [AD 2025-23-03](https://openairdocs.org/ad/2025-23-03): Fire protection · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Jan 13, 2026 - [AD 2025-20-14](https://openairdocs.org/ad/2025-20-14): Equipment/furnishings · Boeing 757-200 Series. Effective Jan 2, 2026 - [AD 2025-19-11](https://openairdocs.org/ad/2025-19-11): Landing Gear · Boeing 757-200 Series, 757-200PF Series and 757-200CB Series. Effective Nov 6, 2025 - [AD 2025-20-04](https://openairdocs.org/ad/2025-20-04): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Nov 6, 2025 - [AD 2025-11-01](https://openairdocs.org/ad/2025-11-01): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jul 8, 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 2025-02-13](https://openairdocs.org/ad/2025-02-13): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Mar 17, 2025 - [AD 2024-25-09](https://openairdocs.org/ad/2024-25-09): Hydraulic power · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Feb 14, 2025 - [AD 2024-24-01](https://openairdocs.org/ad/2024-24-01): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Jan 13, 2025 - [AD 2024-12-09](https://openairdocs.org/ad/2024-12-09): Wings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Aug 22, 2024 - [AD 2024-10-05](https://openairdocs.org/ad/2024-10-05): Equipment/Furnishings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jul 19, 2024 - [AD 2024-10-07](https://openairdocs.org/ad/2024-10-07): Fuselage · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Jul 19, 2024 - [AD 2024-12-07](https://openairdocs.org/ad/2024-12-07): Fuselage · Boeing 757-200 Series with STC ST01529SE or ST02278SE. Effective Jul 11, 2024 - [AD 2024-07-05](https://openairdocs.org/ad/2024-07-05): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jun 5, 2024 - [AD 2024-05-09](https://openairdocs.org/ad/2024-05-09): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective May 8, 2024 - [AD 2023-13-12](https://openairdocs.org/ad/2023-13-12): Oxygen · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 17 more. Effective Sep 5, 2023 - [AD 2023-12-12](https://openairdocs.org/ad/2023-12-12): Navigation · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 6 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 2022-20-15](https://openairdocs.org/ad/2022-20-15): Wings · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Dec 7, 2022 - [AD 2022-15-09](https://openairdocs.org/ad/2022-15-09): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Aug 17, 2022 - [AD 2022-13-04](https://openairdocs.org/ad/2022-13-04): Fuselage · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Aug 12, 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 2022-07-07](https://openairdocs.org/ad/2022-07-07): Equipment/furnishings · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective May 26, 2022 - [AD 2021-26-28](https://openairdocs.org/ad/2021-26-28): Fuel · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Mar 3, 2022 - [AD 2021-22-23](https://openairdocs.org/ad/2021-22-23): Wings · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Dec 29, 2021 - [AD 2021-08-04](https://openairdocs.org/ad/2021-08-04): Oxygen · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 23 more. Effective May 26, 2021 - [AD 2021-05-11](https://openairdocs.org/ad/2021-05-11): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Apr 19, 2021 - [AD 2020-20-10](https://openairdocs.org/ad/2020-20-10): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Nov 10, 2020 - [AD 2020-04-15](https://openairdocs.org/ad/2020-04-15): Air conditioning · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 4 more. Effective May 8, 2020 - [AD 2020-05-25](https://openairdocs.org/ad/2020-05-25): Fuselage · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective May 4, 2020 - [AD 2020-01-18](https://openairdocs.org/ad/2020-01-18): Fuel, Fuselage, Wings · Winglets, wing structural reinforcement (Aviation Partners Boeing STC ST01518SE). Effective Mar 5, 2020 - [AD 2019-24-18](https://openairdocs.org/ad/2019-24-18): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 11 more. Effective Feb 3, 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 2019-07-04](https://openairdocs.org/ad/2019-07-04): Editorial Note: Rule document 2019-07587 was originally published on pages 15949 through 15952 in the issue of Wednesday, April 17, 2019. In that publication, on page 15951, in the title of the Airworthiness Directive, ''-04'' was inadvertently left out. The corrected document is republished in its entirety. · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective May 22, 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 2018-20-13](https://openairdocs.org/ad/2018-20-13): Fuel · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 13 more. Effective Nov 15, 2018 - [AD 2018-19-23](https://openairdocs.org/ad/2018-19-23): Doors · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 15 more. Effective Nov 7, 2018 - [AD 2018-18-07](https://openairdocs.org/ad/2018-18-07): Fuselage · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Oct 10, 2018 - [AD 2018-06-08](https://openairdocs.org/ad/2018-06-08): Fuselage · Boeing 757-200 Series. Effective Apr 19, 2018 - [AD 2018-03-10](https://openairdocs.org/ad/2018-03-10): Fuselage · Boeing 757-300 Series. Effective Mar 19, 2018 - [AD 2017-26-07](https://openairdocs.org/ad/2017-26-07): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Feb 7, 2018 - [AD 2017-26-02](https://openairdocs.org/ad/2017-26-02): Doors · Boeing 757-200 Series. Effective Jan 24, 2018 - [AD 2017-22-12](https://openairdocs.org/ad/2017-22-12): Wings · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Dec 26, 2017 - [AD 2017-20-05](https://openairdocs.org/ad/2017-20-05): Fuselage · Boeing 757-200 Series and 757-300 Series. Effective Nov 6, 2017 All 364: https://openairdocs.org/tcds/A2NM/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Boeing 757-232](https://openairdocs.org/model/boeing-757-232): 63 aircraft (registry code 1384965) - [Boeing 757-224](https://openairdocs.org/model/boeing-757-224): 40 aircraft (registry code 1384958) - [Boeing 757-222](https://openairdocs.org/model/boeing-757-222): 38 aircraft (registry code 1384956) - [Boeing 757-223](https://openairdocs.org/model/boeing-757-223): 23 aircraft (registry code 1384957) - [Boeing 757-236](https://openairdocs.org/model/boeing-757-236): 20 aircraft (registry code 1384971) - [Boeing 757-251](https://openairdocs.org/model/boeing-757-251): 18 aircraft (registry code 1384970) - [Boeing 757-351](https://openairdocs.org/model/boeing-757-351): 16 aircraft (registry code 1384991) - [Boeing 757-231](https://openairdocs.org/model/boeing-757-231): 13 aircraft (registry code 1384908) - [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a): 13 aircraft (registry code 1384967) - [Boeing 757-324](https://openairdocs.org/model/boeing-757-324): 9 aircraft (registry code 1384930) - [Boeing 757-200 SERIES](https://openairdocs.org/model/boeing-757-200-series): 7 aircraft (registry code 1384950) - [Boeing 757-204](https://openairdocs.org/model/boeing-757-204): 6 aircraft (registry code 13844CO) - [Boeing 757-225](https://openairdocs.org/model/boeing-757-225): 5 aircraft (registry code 1384959) - [Boeing 757-230](https://openairdocs.org/model/boeing-757-230): 4 aircraft (registry code 1384952) - [Boeing 757-256](https://openairdocs.org/model/boeing-757-256): 3 aircraft (registry code 1384925) - [Boeing 757-258](https://openairdocs.org/model/boeing-757-258): 3 aircraft (registry code 1384918) - [Boeing 757-260PF](https://openairdocs.org/model/boeing-757-260pf): 2 aircraft (registry code 1384919) - [Boeing 757-200CB](https://openairdocs.org/model/boeing-757-200cb): 0 aircraft (registry code 1384915) - [Boeing 757-200PF](https://openairdocs.org/model/boeing-757-200pf): 0 aircraft (registry code 1384916) - [Boeing 757-208](https://openairdocs.org/model/boeing-757-208): 0 aircraft (registry code 1384929) - [Boeing 757-212](https://openairdocs.org/model/boeing-757-212): 0 aircraft (registry code 1384951) - [Boeing 757-285](https://openairdocs.org/model/boeing-757-285): 0 aircraft (registry code 1384985) - [Boeing 757-300](https://openairdocs.org/model/boeing-757-300): 0 aircraft (registry code 1384924) - [Boeing 757-308](https://openairdocs.org/model/boeing-757-308): 0 aircraft (registry code 1384941) - [Boeing 757-330](https://openairdocs.org/model/boeing-757-330): 0 aircraft (registry code 1384923) ## STCs approved under this data sheet (784, first 50) - [STC ST03438NY](https://openairdocs.org/stc/ST03438NY): Installation of Adams Rite Lavatory Equipment. Delta Engineering Corporation - [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 ST12442IB](https://openairdocs.org/stc/ST12442IB): Installation of Iridium Certus Satellite System. ALAMO ENGINEERING GmbH - [STC ST02158SE-D](https://openairdocs.org/stc/ST02158SE-D): Installation of 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 ST02215AT-D](https://openairdocs.org/stc/ST02215AT-D): Interior reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST02391AT-D](https://openairdocs.org/stc/ST02391AT-D): Installation of Collins VDL Mode 2 System.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST02428AT-D](https://openairdocs.org/stc/ST02428AT-D): Installation of a TCC AERIS System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST02623AT-D](https://openairdocs.org/stc/ST02623AT-D): Interior reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03083AT-D](https://openairdocs.org/stc/ST03083AT-D): Installation of bin doors and system interfaces necessary to adapt galley installations. Relocation of the Video Control Center and reconfiguration of mounted video monitors to align with new seating arrangements and other interior modifications. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03493AT-D](https://openairdocs.org/stc/ST03493AT-D): Interior reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03848AT-D](https://openairdocs.org/stc/ST03848AT-D): Installation of a Legrest and Curtain in a Crew Rest Area.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03937AT](https://openairdocs.org/stc/ST03937AT): Installation of an Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03951AT](https://openairdocs.org/stc/ST03951AT): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03953AT](https://openairdocs.org/stc/ST03953AT): Installation of TIMCO Aerosystems Cabin Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST03989AT](https://openairdocs.org/stc/ST03989AT): 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 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 ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc. - [STC SA7473SW](https://openairdocs.org/stc/SA7473SW): Installation of tail floodlights.. The Boeing Company - [STC ST03186NY](https://openairdocs.org/stc/ST03186NY): Installation of a Panasonic Global Communication Suite (GCS) Antenna. Delta Engineering Corporation - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc. - [STC ST03187NY](https://openairdocs.org/stc/ST03187NY): Installation of a Panasonic Global Communication Suite (GCS). Delta Engineering Corporation - [STC ST04635NY](https://openairdocs.org/stc/ST04635NY): Installation of Data Transmission & Automatic Calling. APTOZ EHF. - [STC ST03562AT](https://openairdocs.org/stc/ST03562AT): Modification of Passenger Aircraft to Freighter Configuration. STE Pensacola Aerospace, Inc. - [STC ST03952AT](https://openairdocs.org/stc/ST03952AT): Modification of Passenger Aircraft to Cargo/Passenger (Combi) Configuration. STE Pensacola Aerospace, Inc. - [STC ST12026AT](https://openairdocs.org/stc/ST12026AT): Installation of Portable Emergency Locator Transmitter. Delta Flight Products LLC - [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net.. Satco Inc. - [STC ST02258LA-D](https://openairdocs.org/stc/ST02258LA-D): Installation of Row 44 Wireless Broadband System Activation. Anuvu IFC Corporation - [STC ST02904CH](https://openairdocs.org/stc/ST02904CH): Installation of Row 44 Wireless Broadband System Provisions.. ANUVU OPERATIONS LLC - [STC ST03450AT](https://openairdocs.org/stc/ST03450AT): Installation of a horse stall system. Gregory Jackson - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC - [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC SA3452NM](https://openairdocs.org/stc/SA3452NM): Installation of waste cart. Safran Cabin Inc. - [STC SA4203NM-D](https://openairdocs.org/stc/SA4203NM-D): Installation of one (1) galley G4A storage unit.. Safran Cabin Inc. - [STC SA4210NM-D](https://openairdocs.org/stc/SA4210NM-D): Installation of one class divider.. Safran Cabin Inc. - [STC SA4561NM](https://openairdocs.org/stc/SA4561NM): Installation of Driessen Galleys. Safran Cabin Inc. - [STC SA5819NM](https://openairdocs.org/stc/SA5819NM): Installation of closet and class divider.. Safran Cabin Inc. - [STC SA6005NM](https://openairdocs.org/stc/SA6005NM): Installation of galleys, stowage unit, doghouses and curtain tracks.. Safran Cabin Inc. - [STC ST00247LA](https://openairdocs.org/stc/ST00247LA): Installation of Closet.. Safran Cabin Inc. - [STC ST00487LA](https://openairdocs.org/stc/ST00487LA): Installation of stowage bin door kit.. Safran Cabin Inc. - [STC ST00657SE](https://openairdocs.org/stc/ST00657SE): Installation of ATIX2 Interior retrofit kit. Safran Cabin Inc. - [STC ST00784SE](https://openairdocs.org/stc/ST00784SE): Installation of ATIX 2 Interior retrofit kit.. Safran Cabin Inc. - [STC ST00869SE](https://openairdocs.org/stc/ST00869SE): Modification to overhead stowage bins located in passenger cabin to extend bins inboard.. Safran Cabin Inc. - [STC ST00955LA](https://openairdocs.org/stc/ST00955LA): Installation of bin extension assembly.. Safran Cabin Inc. - [STC ST01144LA](https://openairdocs.org/stc/ST01144LA): Installation of a L/H closet p/n 501081-1.. Safran Cabin Inc. - [STC ST01145LA](https://openairdocs.org/stc/ST01145LA): Installation of a R/H Divider p/n 501082-1.. Safran Cabin Inc. - [STC ST01146LA](https://openairdocs.org/stc/ST01146LA): Installation of a Curtain Header p/n 501083-1.. Safran Cabin Inc. All 784: https://openairdocs.org/tcds/A2NM/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.