TCDS T00021SE

T00021SE 1 of 27 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 Rev. No. 40 37 40 38 37 37 36 36 37 40 40 36 37 36 36 37 40 37 37 Page No. 20 21 22 23 24 25 26 27 Rev. No. 36 36 20 37 33 32 39 37 T00021SE Revision 40 BOEING 787-8 787-9 787-10 September 22, 2025 TYPE CERTIFICATE DATA SHEET T00021SE This data sheet, which is part of Type Certificate No. T00021SE, 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 - 787-8, Transport Category, Approved August 26, 2011 Engines: 2 Rolls-Royce plc Turbofan Engines; Models: Trent 1000-A, Trent 1000-A2, Trent 1000-AE3, Trent 1000-C, Trent 1000-C2, Trent 1000-CE3, Trent 1000-D, Trent 1000-D2, Trent 1000-D3, Trent 1000-E, Trent 1000-G, Trent 1000-G2, Trent 1000-G3, Trent 1000-H, Trent 1000-H2, Trent 1000-H3, Trent 1000-L2 (Engine Type Certificate No. E00076EN) 2 General Electric Turbofan Engines; Models: GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2, GEnx-1B67, GEnx-1B67/P1, GEnx-1B67/P2, GEnx-1B70, GEnx-1B70/P1, GEnx-1B70/P2, GEnx-1B70C/P1, GEnx-1B70C/P2, GEnx-1B70/75/P1or GEnx-1B70/75/P2 (Engine Type Certificate No. E00078NE) Authorization for engine intermix is contained in the appropriate FAA approved Airplane Flight Manual Fuel: Rolls-Royce plc Turbofan Engines: Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1 MIL-DTL-5624 grade JP-5 MIL-DTL-83133 grade JP-8 GOST 10227-86 grade TS-1 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 relevant Engine Operating Instructions. General Electric Turbofan Engines (also, see Note 9): Fuels conforming to: ASTM D-1655 grades Jet-A and Jet A-1 MIL-DTL-5624 grade JP-5 MIL-DTL-83133 grade JP-8 GOST 10227-86 grade TS-1 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 relevant Engine Operating Instructions. Operation of the General Electric GEnx-1B series engine with fuel containing Kathon™ FP 1.5 biocide is prohibited. T00021SE 2 of 27 I - 787-8 (cont’d) Engine Limits: Static thrust lb, standard day, sea level Takeoff (see Note 10 for operating limits) Maximum continuous RR Trent 1000-A (See Note 7 for ICAO env comp) (see Note 11 for Applicability) 69,194 64,722 RR Trent 1000-C (See Note 7 for ICAO env comp) (see Note 12 for Applicability) 74,511 69,523 RR Trent 1000-D (See Note 7 for ICAO env comp) (see Note 12 for Applicability) 74,511 69,523 RR Trent 1000-E (See Note 7 for ICAO env comp) (see Note 12 for Applicability) 59,631 58,866 RR Trent 1000-G (See Note 7 for ICAO env comp) (see Note 12 for Applicability) 72,066 64,722 RR Trent 1000-H (See Note 7 for ICAO env comp) (see Note 12 for Applicability) 63,897 58,866 RR Trent 1000 - A2 (See Note 20 for ICAO env comp) 69,194 64,722 RR Trent 1000 - C2 (See Note 20 for ICAO env comp) 74,511 69,523 RR Trent 1000 – D2 (See Note 20 for ICAO env comp) 74,511 69,523 RR Trent 1000 - G2 (See Note 20 for ICAO env comp) 72,066 64,722 RR Trent 1000 - H2 (See Note 20 for ICAO env comp) 63,897 58,866 RR Trent 1000 – L2 (See Note 20 for ICAO env comp) 74,511 69,523 RR Trent 1000-AE3 (See Note 24 for ICAO env comp) 69,194 64,722 RR Trent 1000-CE3 (See Note 24 for ICAO env comp) 74,511 69,523 RR Trent 1000-D3 (See Note 24 for ICAO env comp) 74,511 69,523 RR Trent 1000-G3 (See Note 24 for ICAO env comp) 72,066 64,722 RR Trent 1000-H3 (See Note 24 for ICAO env comp) 63,897 58,866 GEnx-1B64 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 13 for applicable BOM) 67,000 61,500 GEnx-1B64/P1 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 16 for applicable BOM) 67,000 61,500 GEnx-1B64/P2 (See Note 21 for SDR Reporting) (See Note 24 for ICAO env comp) (See Note 18 for applicable BOM) 67,000 61,500 GEnx-1B67 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 14 for applicable BOM) 69,400 61,500 GEnx-1B67/P1 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 16 for applicable BOM) 69,400 61,500 GEnx-1B67/P2 (See Note 21 for SDR Reporting) (See Note 24 for ICAO env comp) (See Note 18 for applicable BOM) 69,400 61,500 GEnx-1B70 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 15 for applicable BOM) 72,300 66,500 GEnx-1B70/P1 (See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 16 for applicable BOM) 72,300 66,500 T00021SE 3 of 27 I - 787-8 (cont’d) Engine Limits (cont’d): Takeoff (see Note 10 for operating limits) Maximum continuous GEnx-1B70/P2 (See Note 21 for SDR Reporting) (See Note 24 for ICAO env comp) (See Note 18 for applicable BOM) 72,300 66,500 GEnx-1B70C/P1(See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 16 for applicable BOM) 72,300 66,500 GEnx-1B70C/P2 (See Note 21 for SDR Reporting) (See Note 24 for ICAO env comp) (See Note 18 for applicable BOM) 72,300 66,500 GEnx-1B70/75/P1(See Note 21 for SDR Reporting) (See Note 7 for ICAO env comp) (See Note 16, 17 for applicable BOM) 72,300 66,500 GEnx-1B70/75/P2 (See Note 21 for SDR Reporting) (See Note 24 for ICAO env comp) (See Note 18,19 for applicable BOM) 72,300 66,500 For engine operating limits see the applicable Engine Type Certificate Data Sheet or the FAA approved Airplane Flight Manual. (See Note 2 for AFM reference) Airspeed Limits: VMO/MMO = 350KEAS / 360KIAS / 0.90M. For other airspeed limits, see the appropriate FAA-approved Airplane Flight Manual. CG Range: See the appropriate FAA-approved Airplane Flight Manual. Empty Weight C.G.: None Maximum Weights: See the appropriate FAA-approved Airplane Flight Manual. Model Eligible Serial Numbers 787-8 34422-34425, 34485-34488, 34490, 34491-34494, 34496-34498, 34501-34503, 34505-34512, 34514-34516, 34518, 34520, 34521, 34525, 34528, 34743-34752, 34785, 34786, 34788, 34789, 34791, 34795, 34796, 34821-34840, 34842, 34844, 34846, 34847, 34849, 34850, 34853-34857, 34859, 34860, 34923-34932, 34938-34945, 35257-35264, 35303-35316, 35319, 35320, 35435- 35440, 35506-35511, 35879, 35938-35944, 36040-36046, 36109-36112, 36227-36233, 36235- 36238, 36273-36299, 36400, 36412-36419, 36424, 36426-36429, 36526, 36843, 36844, 37117, 37118, 37120-37127, 37164-37167, 37227-37230, 37306, 37502-37511, 37894, 37920, 37921, 37982-37985, 38055, 38056, 38135, 38136, 38319-38348, 38363, 38364, 38464, 38466, 38471- 38473, 38475-38477, 38480, 38484, 38609-38615, 38619, 38754, 38757-38759, 39406, 39407, 40053, 40059, 40108, 40109, 40124-40127, 40618-40637, 40695, 40748-40750, 40899, 41538- 41543, 41987, 42224, 42225, 42243-42249, 42378, 42379, 43817, 43818, 44572, 60265, 60267, 60279, 60626, 60629-60631, 63396-63399, 64249, 64435-64438, 65315, 65990-66006, 66133, 67792 PERTINENT DATA Minimum Crew: Two (2): pilot and copilot Maximum Passengers: The maximum number of passengers approved for emergency evacuation is: 381with four pairs of exits in an (A, A, A, A) exit arrangement, 355 with four pairs of exits in a (C, A, A, A) exit arrangement, 330 with four pairs of exits in an (A, A, C, A) exit arrangement, and 300 with four pairs of exits in a (C, A, C, A) exit arrangement. Maximum passenger capacity may be further limited by Environmental Control System ventilation per occupant requirement defined in 25.831(a). Max. Baggage/Cargo: See appropriate FAA-approved Weight and Balance Manual. (See Note 1 for W&B ref) Fuel and Oil Capacities: See appropriate FAA-approved Weight and Balance Manual. (See Note 1 for W&B ref) Maximum Operating Altitude: 43,100 feet T00021SE 4 of 27 I - 787-8 (cont’d) Certification Basis: 14 CFR Part 25, Airworthiness Standards, through Amendment 25-119 and Amendments 25-120, 25-124, 25-125 and 25-128 with exceptions as noted below. Section No. Title At Amdt. 25- 25.1309 For Cargo Fire Protection Systems and Uncommanded High Thrust 119 Amendment 25-118 was not published and therefore has no applicability. 14 CFR Part 26, Continued Airworthiness and Safety Improvements, through Amendment 26-5, for §§ 26.11, 26.21, 26.37, 26.43, and 26.45 14 CFR Part 34, Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered, through Amendment 34-7A. In addition, the engine meets ICAO environmental standards defined in Annex 16, amendment 10, dated July 20, 2020. (See Note 24 for additional considerations) 14 CFR Part 36, Noise Standards: Aircraft Type Certification and Airworthiness Certification, through Amendment 36-28. Demonstrated compatibility with the ICAO Annex 16, Volume I, Amendment 9 is documented in the AFM. (See Note 25 for additional considerations) The Following Optional Design Regulations have been complied with: Ditching: 14 CFR §§ 25.801, 25.1411(d), (e), (f), (g) and 25.1415 Ice Protection: 14 CFR § 25.1419 ETOPS: The 787-8 has 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 No. D021Z002-01, “Model 787 ETOPS Configuration, Maintenance, and Procedures.” This finding does not constitute approval to conduct ETOPS Exemptions from 14 CFR Part 25: 1. Grant of Exemption, § 25.562(b)(2), Relief from floor warpage testing requirements for flightdeck seats on the Boeing Model 787 series airplanes; Exemption No. 9486, September 11, 2007. 2. Grant of Exemption, § 25.809(a), Relief from the requirement that flightcrew emergency exits have a means to view outside conditions under all lighting situations for the Boeing Model 787 series airplanes; Exemption No. 10114, August 11, 2010. 3. Grant of Exemption, § 25.809(a), Relief for a limited number of the Boeing Model 787 series airplanes from the requirement that passenger emergency exits have a means to view outside conditions under all lighting situations; Exemption No. 10235A, May 01, 2013 (Limited to aircraft below Line Number 127 for the 787-8 series only). 4. Partial Grant of Exemption, § 25.841(a)(2)(i)(ii), Relief for the Boeing Model 787 series airplanes from the requirement that, during a decompression caused by failures of the engines, airplane cabin pressure altitude not exceed 25,000 feet for more than 2 minutes or exceed 40,000 feet for any duration; Exemption No. 8857, March 30, 2007. 5. Time Limited Grant of Exemption, § 25.1309(c), Temporary relief from the requirement to provide indication of anticipated fuel system contamination to the flightcrew of Boeing Model 787-8 airplanes powered by Rolls- Royce Trent 1000 engines; Exemption No. 10199, January 28, 2011, and Exemption No. 10199A, August 18, 2011, Exemption No. 10199B, June 30, 2014 (Expires April 30, 2017). 6. Grant of Exemption, § 25.1447(c)(1), Relief from the requirement for passenger oxygen masks to be automatically presented before the cabin pressure altitude exceeds 15,000 feet for the Boeing Model 787 series airplanes; Exemption No. 9801, December 12, 2008. 7. Time Limited Grant of Exemption, §§ 25.1305(c)(6) and 25.1309(c), Temporary relief from the requirements to provide indication of impending bypass of the engine oil fuel cooled oil coolers and to provide indication of impending bypass on the main fuel filters of multiple engines, for the Boeing Model 787-8 airplanes powered by General Electric GEnx-1B, or subsequent variants of the engine; Exemption No. 10268 (corrected copy), May 24, 2011, and Exemption No. 10268A, August 15, 2011, Exemption No. 10268B, June 30, 2014 (Expires April 30, 2017). T00021SE 5 of 27 I - 787-8 (cont’d) Exemptions (cont’d) 8. Grant of Exemption, Section 25.853(d) which requires that certain interior components of airplanes with passenger capacities of 20 or more meet the flammability test requirements of parts IV and V (heat release and smoke emission) of appendix F of 14 CFR part 25; 10868A, November 5, 2013 9. Grant of Exemption, Section 25.813(e) at Amendment 25-116 – No door may be installed between any passenger seats that is occupiable for takeoff and landing and any passenger emergency exit, such that the door crosses any egress path (including aisles, cross aisles and passageways); Exemption 10879, October 18, 2013. Partial Grant of Exemption 10879A, amended in entirety on March 7, 2018, Partial Grant of Exemption 10879B, amended in entirety on December 3, 2018. Grant of Exemption 10879C, amended in entirety on February 1, 2023 10. Time Limited Grant of Exemption §25.1305(c)(5) at Amendment 25-120, providing flight-deck annunciation of operation of the engine VBV ice-protection system; Exemption 11081, issued October 10, 2014, requires production airplanes to be fully compliant after June 30, 2015 and the in-service fleet to be fully compliant after March 31, 2016. Time Limited Grant of Exemption § 25.939(a), at Amendment 25-40, for airplanes that have incorporated engine ice protection system modifications and associated AFM limitations; Exemption 11081A, issued January 20, 2015, requires production airplanes to be fully compliant by June 30, 2015 and prohibits in-service fleet retrofit after June 30, 2015. Exemption 11081B, issued June 10, 2015, extends the dates of 11081A requiring production airplanes to be fully compliant to § 25.939(a), at Amendment 25-40, to December 31, 2015and prohibits in-service fleet retrofit after December 31, 2015. 11. Time Limited Grant of Exemption, § 25.901(c), 25.1301(a)(4), 25.1309(a), and 25.1309(b).Temporary relief from the requirements as they relate to single failures of the thrust control module that could result in uncommanded high thrust conditions and to the extent necessary to allow type certification of new propulsion control system designs for Model 787-8 and 787-9 airplanes equipped with General Electric GEnx-1B engines; Exemption No. 17112 dated September 23, 2016. The conditions of TLE 17112 require production airplanes to be fully compliant after December 31, 2018, and the in-service fleet to be fully compliant by December 31, 2020. 12. Grant of Exemption, § 25.901(c) to allow type certification of new propulsion control system designs for the Model 787 airplanes without an exact showing of compliance with the "no single failure" requirement of § 25.901(c) relating to UHT in combination with high crosswinds in certain takeoff and approach-and-landing scenarios. This exemption applies only to those UHT failure conditions that, when combined with high crosswinds, do not comply with § 25.901(c).; Exemption 17319, issued May 2, 2017 13. Time Limited Grant of Exemption, § 25.903(a)(1) to allow type certification of the Model 787 airplanes equipped with Rolls-Royce Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3 and Trent 1000- H3 engines from the engine requirement that mandates engines comply with the smoke emissions requirements of 14 CFR Part 34. This exemption is based on Time-Limited Grant of Exemption 17550A which was issued to Rolls-Royce plc and is required to meet the conditions and limitations of, that time- limited exemption for their engines. Exemption No. 17613, issued October 25, 2017. The conditions of TLE 17613 requires that all in-service airplanes be fully compliant by December 31, 2022. On February 12, 2018 Rolls-Royce plc met condition 6.b of Exemption 17550A showing full compliance to 14 CFR Part 34 which meets the requirement of § 25.903(a)(1). 14. Grant of Exemption, §§ 25.863(a), 25.863(b)(3), 25.901(c), 25.981(a)(3), 25.981(b), 25.981(d), 25.1309(b), and Special Conditions 25-414-SC will either improve or maintain the current level of safety on existing in- service Boeing Model 787 airplanes by incorporation of design changes required to address the unsafe condition in AD 2018-11-13 for the upper wing stringer-to-skin joints and address the installation of cap seals in lighting Zone 3 and the separate installation of edge sealant; Exemption 20370, issued June 11, 2023. Equivalent Levels of Safety (ELOS) are identified as: TC6918SE-T-A-9 §§ 25.341, 25.343, 25.345, 25.371, 25.373, and 25.391 ELOS Finding for Gust and Continuous Turbulence Design Loads TC6918SE-T-A-10 § 25.335(b) ELOS Finding for Design Airspeeds TC6918SE-T-A-11 §§ 25.391, 25.393, and 25.415 ELOS Finding for the Ground Gust Requirements TC6918SE-T-A-12 § 25.331(c) ELOS for Symmetric Maneuvering Conditions TC6918SE-T-A-13 § 25.629 ELOS for Aeroelastic Stability T00021SE 6 of 27 I - 787-8 (cont’d) ELOS (cont’d) PS08-0670-C-1 § 25.853(a) ELOS Finding for Adhesives Used in Interior Panel Joint Potting Applications PS13-1000-C-5 § 25.853(a)(d) ELOS Finding for Flammability Testing Hierarchy PS19-0580-C-44 Exemption 10879B ELOS Finding for Moveable Privacy Dividers between Adjacent Mini-suites TC6918SE-T-CS-1 § 25.810(a)(1)(ii) ELOS Finding for Escape Slide Inflation Times TC6918SE-T-CS-2 § 25.811(f) ELOS Finding for Emergency Exit Markings and Door Sill Reflectance PS07-0585-CS-10 §§ 25.811(d), 25.811(g), 25.812(b)(1)(i), and 25.812(b)(1)(ii) ELOS Finding for Graphical Exit Signs TC6918SE-T-CS-12 § 25.791(a) ELOS Finding for Lighted “No Smoking” Signs in Lieu of Placards TC6918SE-T-CS-14 §§ 25.853 and 25.856(b) ELOS Finding for Associated to Post-Crash Fire Survivability PS07-0585-CS-18 § 25.811(e)(4)(i), (ii), and (iii) ELOS Finding for the Passenger Door Operational Arrow Location and Color PS06-0413-CS-25 § 25.783(e)(2) ELOS Finding for Passenger and Large Cargo Door Indication PS09-0987-CS-28 § 25.562 and 25.785 ELOS Finding for Dynamic Test Requirements for Single Occupant Side- Facing Seats PS12-1032-CS-31 RevA §§ 25.562 and 25.785 ELOS Finding for Dynamic Test Requirements for Single Occupant Oblique Seats with Inflatable Restraints PS12-1033-C-32 §§ 25.562 and 25.785 ELOS Finding for Dynamic Test Requirements for Single Occupant Side- Facing Seats PS13-0679-CS-33 §§ 25.561 and 25.621 ELOS Finding for Critical Casting Factor Requirements for Model 787 Series Aircraft PS13-0906-CS-37 §§ 25.562 and 25.785 ELOS Finding for Dynamic Test Requirements for Side-Facing Seats with Shoulder Restraints PS18-0046-EE-10 §§ 25.1535 and K25.2.2 ELOS Finding for 787 Rolls-Royce Trent 1000-TEN Early ETOPS Airplane Demonstration Tests TC6918SE-T-ES-5 § 25.831(g) ELOS Finding for Acceptable High Temperature Physiological Environment During Failure Condition TC6918SE-T-ES-16 § 25.1443(c) ELOS Finding for the Passenger Oxygen System TC6918SE-T-ES-18 § 25.1441(c) ELOS Finding for Pulse Oxygen System for Passenger TC6918SE-T-ES-19 § 25.841(b)(6) ELOS Finding for Cabin Altitude Warning System for Operations into High Altitude Airports TC6918SE-T-ES-20 § 25.1443(d) ELOS Finding for Portable Pulse Oxygen System TS15-0029-F-1 § 25.251 ELOS Finding for Vibration/Buffeting Compliance Criteria, Taxi Aid Camera TC6918SE-T-F-4 § 25.1517 ELOS Finding for Rough Air Speed (VRA) TC6918SE-T-F-6 § 25.107 (e)(1)(iv) ELOS Finding for Minimum Unstick (VMU) Speed Margin T00021SE 7 of 27 I - 787-8 (cont’d) ELOS (cont’d) TC6918SE-T-F-14 § 25.677(b) ELOS Finding for Trim Displays TC6918SE-T-F-17 § 25.255 ELOS Finding for Out-of-Trim Characteristics PS06-0496-F-18 § 25.1555 ELOS Engine and APU Fire Handle Design PS06-0413-F-20 § 25.1325(e) ELOS Finding for the Standby Air Data System PS14-0452-F-23A § 25.251 ELOS Finding for Vibration/Buffeting Compliance Criteria, Panasonic Ku-Band Radome Antenna TC6918SE-T-G-8 §§ 25.1529, Appendix H25.4 ELOS Finding for formatting of Boeing ICA Manuals – Airworthiness PS05-0177-P-2 § 25.981(b)(2) ELOS Finding for the Fuel Tank Flammability Rule (FTFR) TC6918SE-T-P-2 §§ 25.933(a)(1)(i) and 25.933(a)(1)(ii) ELOS Finding for Flight Critical Thrust Reverser TC6918SE-T-P-3 § 25.1182(a) ELOS Finding for Fire Safety Requirements for the Aft Strut Fairing Compartment TC6918SE-T-P-13 §§ E25.1, F25.1 and G25.1 ELOS Finding for the Auxiliary Power Unit (APU) Installation PS14-0470-P-15 K25.2.2(d)(1) ELOS Finding for the 787-8/-9 Rolls-Royce Trent 1000-TEN ETOPS Ground Test TC6918SE-T-P-17 § 25.934 ELOS Finding for the Engine and Thrust Reverser System Testing TC6918SE-T-P-19 §§ 25.1023(b) and 25.1121(c) ELOS Finding for Auxiliary Power System TC6918SE-T-P-20 §§ 25.997 and 25.1305(c)(6) ELOS Finding for Warning Means for Engine Fuel Filter Contamination TC6918SE-T-P-27 § 25.1145(a) ELOS Finding for Engine Igniter Flight-deck Switch Configuration PS06-0414-P-34 §§ 25.1181(a)(6), 25.1181(b), 25.1182, and 25.1183(a) ELOS Finding for Fire Safety Requirements for GEnx-1B PS13-0546-P-36 §§ 25.1549(a) and 25.1549(b) ELOS Finding for the Display of Powerplant Instruments TC6918SE-T-SA-7 §§ 25.1301, 25.1309 and 25.1310 ELOS Finding for use of ARAC Recommended Revision TC6918SE-T-SA-10 § 25.1459(a)(2) ELOS Finding for Flight Recorders TC6918SE-T-SA-11 § 25.1303(c)(1) ELOS Finding for Overspeed Aural Warning TC6918SE-T-SA-29 § 25.1333(a) ELOS Finding for Instrument Systems TC6918SE-T-SE-14 § 25.1351(b)(5) ELOS Finding for the Flight Control Electronics DC Power System PS06-0496-T-SE-15 § 25.1317(b) ELOS Finding for High Intensity Radiated Fields (HIRF) TC6918SE-T-SF-1 § 25.671(c)(2) ELOS Finding for Flight Control System Failure Criteria TC6918SE-T-SF-5 § 25.777(e) ELOS Finding for the Wing Flap Control Lever PS06-0496-SF-7 § 25.675 ELOS Finding for Seal Krueger Flap Stops T00021SE 8 of 27 I - 787-8 (cont’d) Special Conditions with respect to the following subjects apply to the Model 787-8: Special Condition. Subject 25-348-SC Composite Wing and Fuel Tank Structure—Fire Protection Requirements 25-354A-SC Interaction of Systems and Structures, Electronic Flight Control System- Control Surface Awareness, High Intensity Radiated Fields (HIRF) Protection, Limit Engine Torque Loads for Sudden Engine Stoppage, and Design Roll Maneuver Requirement 25-355-SC Reinforced Flightdeck Bulkhead 25-356-SC Systems and Data Networks Security-Isolation or Protection from Unauthorized Passenger Domain Systems Access 25-357-SC Systems and Data Networks Security-Protection of Airplane Systems and Data Networks from Unauthorized External Access 25-359-SC Lithium Ion Battery Installation 25-360-SC Composite Fuselage In-Flight Fire/Flammability Resistance 25-362-SC Crashworthiness Emergency Landing Conditions 25-363-SC Tire Debris Penetration of Fuel Tank Structure 25-365-SC Operation Without Normal Electrical Power 25-370-SC Seats with Non-Traditional, Large, Non-Metallic Panels 25-414-SC Lightning Protection of Fuel Tank Structure to Prevent Fuel Tank Vapor Ignition 25-418-SC Overhead Flight Crew Rest Compartment Occupiable during Taxi, Takeoff, and Landing 25-419-SC Overhead Crew Rest Compartment 25-431-SC Seats with Inflatable Lapbelts 25-458-SC Single-place Side-facing Seats with Inflatable Lapbelts 25-605-SC Structure- Mounted Airbags 25-626A-SC Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With or Without Airbag Devices or 3-Point Restraint Systems 25-682-SC Non-Rechargeable Lithium Battery Installations 25-745-SC Seats with Inertia Locking Devices 25-770-SC Dynamic Test Requirements for Single-Occupant Oblique Seats With Pretensioner Restraint Systems 25-786-SC Seats With Pretensioner Restraint Systems