TCDS A1NM

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A1NM This data sheet, which is part of Type Certificate No. A1NM, 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 767-200 (Approved July 30, 1982) Engines: 2 Pratt and Whitney JT9D-7R4D, JT9D-7R4E, JT9D-7R4E4, PW4052, PW4056, PW4060A, or 2 General Electric CF6-80A, CF6-80A2, CF6-80C2-B2, -B4, -B6 or CF6-80C2B4F, -B6F, -B7F, CF6-80C2B2F. WARNING: To prevent unsafe airplane handling characteristics, PW4000 series engines with electronic engine control (EEC) part number 791100-14-102 (Pratt & Whitney part number 54D043) must not be installed on the same airplane as PW4000 series engines that have the ring case compressor configuration. This combination of engine configurations is not approved because of a significant difference in engine acceleration rates and the effect of that difference on airplane handling characteristics. Ring case compressor equipped engines were approved with the same engine model number as previously approved PW4000 configurations, and must be identified by the presence of a “/A5” marked at the end of the “INSTL ARR” block on the engine data plate. The General Electric CF6-80A engines may be intermixed with CF6-8 0A2 engines with appropriate limitations as noted in the FAA-Approved Airplane Flight Manual. Fuel: Pratt and Whitney Engines: Fuels conforming to the latest version of Pratt & Whitney Service Bulletin 2016 General Electric Engines: Fuel conforming to GE Specification D50TF2. (See Note 14) All Engines: ASTM D-1655 grades Jet A or Jet A1. (See Note 14) ASTM D 6615 grades Jet B (see Note 14) MIL-T-5624 grades JP-4 or JP-5. (See Note 14) MIL-T-83133 grades JP-8. Refer to the FAA approved Airplane Flight Manual listed in Note 2 for fuel limitations Engine Ratings & For engine ratings and operating limits see engine TC Data Sheet No. E3NE for the P&W JT9D-7R4D, -7R4E, or - Operating Limits: 7R4E4; TC Data Sheet E13NE for the GE CF6-80A, CF6-80A2, or CF6-80C2; TC Data Sheet E24NE for the PW4000, or the FAA-Approved Airplane Flight Manual. Airspeed Limits: VD = 420 KCAS to 17,854 ft/.91M above 23,000 ft, linear variation between these points. VFC = 390 KCAS to 17,600 ft/382 KCAS at 23,000 ft/.87M above 26,000 ft, linear variation between these points. VMO = 360 KCAS/.86M VLE = 270 KCAS/.82M VLO = 270 KCAS/.82M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual. CG Range: See the appropriate FAA-Approved Flight Manual. Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Rev. No. 41 36 37 39 37 36 39 36 37 39 36 41 41 36 41 36 Page No. 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 Rev. No. 36 36 41 37 36 37 36 41 38 37 39 37 39 38 38 40 A1NM Revision 41 BOEING 767-200 Series 767-300 Series 767-300F Series 767-400ER Series 767-2C Series August 21, 2024 2 A1NM I. Model 767-200 (cont’d): Maximum Weights: See the appropriate FAA-Approved Flight Manual. Maximum 255 with 2 pairs of Type A plus 1 pair of Type III exits. Passengers: 290 with 2 pairs of Type A plus 2 pairs of Type III exits. Model Eligible Serial Numbers 767-201 23897-23902 767-204 22980, 22981, 23072, 23250, 23807, 24013, 24239, 24457, 24736, 24757, 25058, 25139 767-205 23057, 23058 767-209 22681, 22682 767-212 28525 767-216 23623, 23624, 24973 767-219 23326-23328, 24150 767-222 21862-21880 767-223 22307-22336, 30256 767-224 30430-30439 767-231 22564-22573 767-232 22213-22227 767-233 22517-22528, 24142-24145, 24323-24325 767-238 23304-23306, 23309, 23402, 23403, 23896 767-241 23801-23806 767-246 23212-23214 767-258 22972-22975 767-259 24618, 24835 767-260 23106, 23107, 23916 767-266 23178-23180 767-269 23280-23282 767-275 22683, 22684 767-277 22692-22696 767-281 22785-22790, 23016-23022, 23140-23147, 23431-23434 767-283 24727, 24728 767-284 24716, 24742, 24762 767-23B 23973, 23974 767-24Q 28270 767-25D 24733, 24734 767-25E 27192-27195 767-27C 27385, 27391, 28016, 28017 767-27E 24832, 24854 767-27G 25537, 27048, 27049 767-2B1 25421, 26471 767-2B7 24764, 24765, 24894, 25225, 25257, 26847 767-2AX 33685 767-2DX 32954 767-2EY 33686-33689 767-2FK 33844, 33958, 34433, 35498 767-2J6 23307, 23308, 23744, 23745, 24007, 24157 767-2N0 24713, 24867 767-2Q4 22921-22923 767-2Q8 24448 767-2S1 23494 Certification Basis: Part 25 of the Federal Aviation Regulations as amended by Amendments 25-1 through 25-37, except where superseded by the following sections of Part 25 as amended by Amendments 25-1 through: Amendment Sections 25-38 25.101, 25.161, 25.397, 25.603, 25.675, 25.685, 25.775, 25.787, 25.815, 25.841, 25.941, 25.951, 25.979(a), (b), (c), 25.999, 25.1027, 25.1041, 25.1093(b), 25.1125, 25.1143(a), (b), (c), (d), 25.1167, 25.1303, 25.1305, 25.1322, 25.1355, 25.1385, 25.1403, 25.1439, 25.1515, 25.1533, 25.1557 25-39 25.807 25-40 25.901(a), (b)(1)(ii), (b)(2), (b)(3), (b)(4), (c), 25.903, 25.933, 25.939, 25.943, 25.945, 25.952, 25.959, 25.963, 25.965, 25.973, 25.995, 25.1091(a), (b), (c), (d), 25.1093(a), (c), 25.1121, 25.1123, 25.1141, 25.1145, 25.1197, 25.1199, 25.1207, 25.1337, 25.1549 25-41 25.831, 25.1309, 25.1321, 25.1325, 25.1331, 25.1333, 25.1335, 25.1351, 25.1401, 25.1421, 25.1435, 25.1447, 25.1450, 25.1457, 25.1459, 25.1461 25-42 25.21, 25.29, 25.107, 25.111, 25.143, 25.147, 25.149, 25.177, 25.181, 25.201, 25.207, 25.233, 25.237, 25.255, 25.703, 25.729, 25.1043, 25.1353, 25.1501, 25.1521, 25.1581, 25.1583, 25.1585, 25.1587 3 A1NM I. Model 767-200 (cont’d): Certification Basis (cont’d): Amendment Sections 25-43 25.1326 25-44 25.1413 25-45 25.571, and 25.573 25-46 25.345, 25.351(a), 25.629, 25.697, 25.803, 25.901(d), 25.1103(a), (b)(2), (d), (e), (f), 25.1142, and 25.1522 25-49 25.733 25-54 25.365 (e)(1), (2) Compliance with the following optional requirements has been established with respect to the following sections of 14 CFR Part 25: §25.801 - Ditching Provisions (Over- water operation can be approved when the aircraft has been equipped and installation has been approved according to 14 CFR 25.801) §25.1419 - Ice Protection Provisions 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 demonstrate compliance with the applicable sections). Compliance has been found for the following regulations at Amendment 26-0: 26.11 and Amendment 26-1: 26.43, 26.45, 26.47, and 26.49 14 CFR part 36 of the Federal Aviation Regulations with Amendments 36-1 through 36-12, effective August 1, 1981. See the appropriate FAA Approved Airplane Flight Manual listed in Note (2) for applicability of Stage 4 Noise Recertification through Amendment 36-28. Special Federal Aviation Regulation 27 Exemption from Part 25: Exemption Title Issued Date Expiration Date 4725 Exemption from 25.785(h) -Allows one seat for a required flight attendant to be located near the overwing Type III exits. 3 November, 1986 Permanent 8119 Partial Exemption from §25.901(c), Single Failures resulting in Uncontrollable High Thrust Conditions 11 June, 2003 Permanent 9749A Exemption from 14 CFR 25.785(j), 25.807(d), 25.807(g)(1), 25.807(i)(1), 25.810(a)(1), 25.812(e), 25.813(b), 25.857(e), and 25.1447(c)(1) for 767- 200 series airplanes converted from passenger to freighter with provisions for the carriage of mixed cargo/live animal operation 24 July, 2009 Permanent 9791C Partial Time-Limited Exemption from 14 CFR §25.853(a), appendix F, paragraph (a)(1)(i), Testing on Large Interior Panels (Expired Exemption No. 9791, November 28, 2010, Exemption No. 9791B, 28 February, 2011) 28 November, 2008 28 November, 2011 10767C Time-limited exemption from 14 CFR 25.901(c) and 25.981(a)(3), fuel tank ignition prevention associated with the FQIS is limited to the replacement of the ARINC 429 chip within the fuel quantity processer unit’s IOC cards and the BITE card (Expired Exemption No. 10767, 17 May, 2016, Exemption No. 10767A, 17 May, 2016) 17 December, 2015 17 May, 2016 14593 Exemption from SFAR 88, and §§ 25.901(c) and 25.981(a)(3), as they pertain to fuel-tank-ignition prevention associated with the fuel-quantity indication system and fuel-overfill-shutoff surge tank wiring installation, limited to in-service 767-200 (freighter only) 25 January, 2016 Permanent Equivalent Safety Findings (ESF’s) exist with respect to the following sections of 14 CFR Part 25: ELOS IP Title 14 CFR ANM-100S-0811-CI-2 Pressurized Cabin Loads (Crew Rest) 25.365(e)(2) ANM-100S-1727-CI-1 Cross Aisle Between Type III Exits 25.807, 25.813 ANM-100S-2332-CI-1 Pressurized Cabin Loads (Crew Rest) 25.365(e)(2) ANW-212:8110-5 Test Subjects for Emergency Evacuation Demonstration 25.803(c)(8) AT0328ST-T-C-5 "No Smoking" limitation in the passenger compartment 25.791,25.853, CAR 4b.3 81 AT1736SE-T-C-14 Door Sill Reflectance 25.811 4 A1NM I. Model 767-200 (cont’d): Certification Basis (cont’d): Equivalent Safety Findings (Cont’d) ELOS IP Title 14 CFR AT2251SE-T-F-1 Use of the 1-g Stall Speed Instead of Minimum Speed in the Stall as a Basis for Determining Compliance (Non-Structural Sections) 1.2, 25.21(b), 25.103(a),(a)(1),(a)(3- 6),(b)(c), 25.107(b)(1),(b)(2),(c)(3),(g), 25.111(a), 25.119(b), 25.121(c),(d),(d)(3), 25.125(a)(2), 25.143(g), 25.145(a),(a)(1),(b)(1- 4),(b)(6),(c), 25.147 (a),(a)(2),(c),(d), 25.149 (c), 25.161(b),(c)(1),(c)(2),(c)(3)(d),(e)(3), 25.175(a)(2),(b)(1),(b)(2),(b)(2)(ii),(b) (3),(c),(c)(4),(d),(d)(5), 25.177(c), 25.181(a),(b), 25.201(a)(2),(b)(4), 25.207(b),(c),(d),(e),(f), 25.231(a)(2), 25.233(a), 25.237(a),(b)(1),(b)(2), 25.735(f)(2),(g), 25.773(b)(1)(i), 25.1001(c)(1),(c)(3), 25.1323(c)(1),(c)(2), 25.1325(e), 25.1587(b)(2) AT6937SE-T-S-1 Hydraulic System Proof Pressure Test 25.1435 (25-45) CT1180NW-D-A-5 Emergency Exit Arrangement 25.807, 25.809, 25.813 CT1180NW-D-A-7 Type A Exit Passageway Dimensions 25.807, 25.811 CT1180NW-D-P-10 Engine Fan Cowl Compartment Fire Zone 25.1181(a)(6), 25.1182 CT1180NW-D-P-9 Induction System Deicing and Anti-icing Protection 25.1093(b)(1) CT1180NW-D-S-20 Forward Position Light Intensity in the Vertical Plane and Overlap 25.1393, 25.1395 PS05-0123-P-1 Ground Fault Interrupter Relays 25.981(a)(3) PS05-0177-P-2 Fuel Tank Flammability Rule (see Note 17) 25.981 (25-125) PS06-0496-F-18 Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design 25.1555(d)(1) PS08-0670-C-1 Adhesives Used in Interior Panel Bent Joint Potting Applications 25.853(a) PS13-0901-ES-1 Oxygen Quantity Indication of the Lavatory Supplemental Oxygen System 25.1441(c) PS13-1000-C-5 Flammability Testing Hierarchy 25.853(a)(d), part 25 appendix F parts I and IV SA06091WI-T-P-1 Powerplant Instrumentation for RCI LDS-2100 installation on Boeing 767-200 series aircraft equipped with General Electric CF6-80A2 engines 25.1305 & 25.1549 TC6918SE-T- G-8 Formatting of Boeing Instructions for Continued Airworthiness Manuals - Airworthiness Limitations 25.1529 (25-54), 25.1729(25-123), H25(25-132) TD1990SE-T-C-1 Emergency Locator Transmitter (ELT) 25.1415(d) TD2695SE-T-C-1 Exterior Exit Markings 25.811(f) TD7075SE-T-C-1 Type III Exit Accessibility 25.803, 25.807(c), 25.813(c) TS13-0005-S-1 Determination of Minimum Oxygen Flow for the Lavatory Oxygen System 25.1443(c) Special Conditions with respect to the following subjects apply: Special Condition Title Effective Date 25-ANM-18 Lightning Protection, Protection from Unwanted Effects of Radio Frequency (RF) Energy and Propulsion Control System for Pratt and Whitney PW4000 series engines, General Electric CF6-80C2 FADEC engine, and Rolls Royce RB211-524H-36 engine installations 29 April, 1988 25-ANM-20 Installation of a longitudinal partition in the cabins 23 August, 1988 25-369-SC Seats with Non-Traditional, Large, Non-Metallic Panels 17 March, 2008 25-630-SC Non-Rechargeable Lithium Batteries 22 April, 2017 5 A1NM II - 767-200SF Major Design Change A 767-200SF (Special Freighter) is a 767-200 series passenger airplane that has been modified in accordance with FAA-approved Boeing Service Bulletin(s) 767-00-0038 to operate in a freighter configuration. These aircraft remain 767-200 series aircraft for documentation purposes on this TCDS and with regard to the applicability of airworthiness directives. Because of the magnitude of this design change, the certification basis for the changed aspects was required to be established and documented in accordance with section 21.101 (Changed Product Rule) All general information in TCDS A1NM for the 767-200 Series remains applicable to an airplane operating in the 767- 200SF configuration, with the following exceptions: Maximum Passengers: There are no provisions for the carriage of passengers. A maximum of four supernumeraries can occupy the flight deck as given in Exemption 9749A. The 767-200SF certification basis was established according to the requirements given in § 21.101 and AC 21.101-1, and was determined in accordance with FAA Order 8110.48. The 767-200SF consists of the following product level change which is considered significant per AC 21.101-1: Significant Product Level Change: Passenger to Freighter Conversion Certification basis: Part 36: Unchanged under the “No Acoustical Change” Provisions of § 21.93(b) SFAR 27: Unchanged from 767-200 Series Part 26, Amendments 26-0 through 26-1 Part 25 of the FAR, effective February 1, 1965, as amended by Amendments 25-1 through 25-115 with the following exceptions per section 21.101(b): SECTION NO. TITLE AT AMDT. 25- 25.365(e)(2) Pressurized Compartment Loads 25-54 (for compartments outside of the pressurized area) 25.561(c)(2) General 25-64 25.571 Damage-tolerance and fatigue evaluation of structure 25-54 25.831(g) Ventilation 25-41 25.841(a) Pressurized cabins 25-38 Changed Areas: The following is a high level description of the listing of changes incorporated as part of the passenger to SF conversion: • Installed strengthened floor beams and fuselage frames • Installed main deck cargo door • Installed rigid cargo barrier/smoke barrier • Revised cargo ventilation system • Removal of passenger windows and installation of window plugs • Installed main deck cargo fire protection system and smoke detection system • Installed aural and visual alerts in the main deck Class E cargo compartment • Installation of seats and provisions to the flight deck for four supernumeraries The certification basis for the following changes incorporated as part of the passenger to SF conversion remains at the original certification basis for the Model 767-200 shown on TCDS A1NM: • Rerouting and some minor changes to hardware associated with flight controls, landing gear, and wheel brake cables • Rerouting of air data tubing, hydraulic tubing, certain electrical wiring • Changes to performance characteristics associated with static and dynamic loads • Forward lavatory with recirculating waste system, including flush motor and related timer and circuit breaker • Re-use of passenger airplane interior mounting hardware and attach points to accommodate cargo compartment equipment like sidewall panels and ceilings. • Installation of a floor-mounted first observer seat • Revision to the Ditching and Flotation analysis document as affected by the SF modification • Revision of the EICAS to the 767-200SF configuration • Revision of Door 1L counterbalance associated with the slide removal The certification basis for areas not affected by the change will remain at the original certification basis for the Model 767-200. . Special Conditions: Special conditions that are part of the certification basis for the 767-200 Series apply to the airplane operating in the 767-200SF configuration 6 A1NM II - 767-200SF Major Design Change (cont’d) Exemptions: All exemptions from 14 CFR Part 25 listed in TCDS A1NM for the 767-200 Series apply to the 767-200SF configuration, except those listed below: Exemption No. 4725 - Exemption from 25.785(h) -Allows one seat for a required flight attendant to be located near the overwing Type III exits. Does not apply. Exemption 9749A, dated 07/24/09, provides relief from the requirements of Sections 25.785(j); 25.807(d), (g)(1), (i)(1); 25.810(a)(1); 25.812(e); 25.813(b); 25.857(e); and 25.1447(c)(1) to allow for the carriage of supernumeraries on the 767-200SF. Equivalent Safety Findings: All existing Equivalent Safety Findings listed in TCDS A1NM for the 767-200 Series apply to the 767-200 operated in the 767-200SF configuration, except those listed below: • Test Subjects for Emergency Evacuation Demonstration, Section 25.803(c)(8). Does not apply. • Passenger Emergency Exits, Section 25.807(a)(7)(iv) and (c). Does not apply. • Type III Exit Access, 25.803, 25,807(c) and 25.813(c). Does not apply. • Emergency Exit Access, 25.807, 25.809 and 25.813. Does not apply. • Exterior Exit Markings, 25.811(f)(2). Does not apply. • “No Smoking” limitation in passenger compartment, 25.791 and 25.853(c). Does not apply. • Type A Exit Passageway Dimensions, 25.807 and 25.811. Does not apply. • Cross-Aisle between Type III Exits, 25.807 and 25.813. Does not apply TCDS Notes: All Notes in TCDS A1NM that apply to the 767-200 Series also apply to an airplane operated in the 767- 200SF configuration Optional All optional requirements applicable to 767-200 Series also apply to aircraft operated in the 767-200SF Requirements: configuration. III - Model 767-300 (Approved September 22, 1986) Engines: 2 Pratt and Whitney JT9D-7R4D, JT9D-7R4E, JT9D-7R4E4, PW4056, PW4060, PW4060C, or PW4062; or 2 General Electric CF6-80A2, or CF6-80C2-B2, -B4, or -B6, or CF6-80C2-B2F, B4F, B6F, or -B7F; or 2 Rolls Royce RB211- 524H-36, or RB211-524H-T-36. WARNING: To prevent unsafe airplane handling characteristics, PW4000 series engines with electronic engine control (EEC) part number 791100-14-102 (Pratt & Whitney part number 54D043) must not be installed on the same airplane as PW4000 series engines that have the ring case compressor configuration. This combination of engine configurations is not approved because of a significant difference in engine acceleration rates and the effect of that difference on airplane handling characteristics. Ring case compressor equipped engines were approved with the same engine model number as previously approved PW4000 configurations, and must be identified by the presence of a “/A5 marked at the end of the “INSTL ARR” block on the engine data plate. Fuel: Pratt and Whitney Engines: Fuels conforming to the latest version of P&W Service Bulletin 2016 General Electric Engines: Fuel conforming to GE Specification D50TF2. (See Note 14) Rolls Royce Engines: See Rolls Royce "Operating Instructions RB211-524H on the Boeing 767-300. (See Note 15) All Engines: ASTM D-1655 grades Jet A or Jet A1. (See Note 14, 15) ASTM D 6615 grades Jet B (see Note 14) MIL-T-5624 grades JP-4 or JP-5. (See Note 14, 15) MIL-T-83133 grades JP-8. Refer to the FAA approved Airplane Flight Manual listed in Note 2 for fuel limitations Engine Ratings & Operating Limits: For engine ratings and operating limits see engine TC Data Sheet No. E3NE for the P&W JT9D- 7R4D, - 7R4E, or - 7R4E4; TC Data Sheet E13NE for the GE CF6-80A2, or CF6-80C2; TC Data Sheet E24NE for the PW4000, TC Data Sheet E30NE for the Rolls Royce RB211-524H-36, or RB211-524H-T-36; or the FAA-Approved Airplane Flight Manual. Airspeed Limits: VD = 420 KCAS to 17,854 ft/.91M above 23,000 ft, linear variation between these points. VFC = 390 KCAS to 17,600 ft/382 KCAS at 23,000 ft/.87M above 26,000 ft, linear variation between these points. VMO = 360 KCAS/.86M VLE = 270 KCAS/.82M VLO = 270 KCAS/.82M For other airspeed limits, see the appropriate FAA-Approved Airplane Flight Manual. CG Range: See the appropriate FAA-Approved Flight Manual. Maximum Weights: See the appropriate FAA-Approved Flight Manual. 7 A1NM III - Model 767-300 (Cont’d) Maximum 290 with 2 pairs of Type A plus 2 pairs of Type III exits Passengers: 290 with 3 pairs of Type A plus 1 pair of Type III exits. (See Note 6 for Type III Exit requirements.) 351 with 3 pairs of Type A plus 1 pair of Type I exits. Model Eligible Serial Numbers 767-304 28039-28042, 28208, 28883, 28979, 29137, 29138, 29384 767-306 26263, 27610-27612, 27614, 27957-27960, 28098, 28884, 30393 767-316 26327, 26329, 27597, 27613, 27615, 29227-29229, 34626, 34628, 34629, 35229-35231, 35696-35698, 36710-36712, 37800-37802, 40590-40593,40798, 40799, 41746-41748, 41993-41997, 42213, 42214 767-319 24875, 24876, 26264, 26912, 26913, 26915, 26971, 28745, 29388, 30586 767-322 25091-25094, 25280, 25283-25287, 25389-25394, 27112-27115, 27158-27160, 29236-29243, 30024-30029 767-323 24032-24046, 25193-25202, 25445-25451, 26995, 26996, 27059, 27060, 27184, 27448-27451, 29429-29432, 29603- 29606, 33081-33089 767-324 27392-27394, 27568, 27569 767-328 27135, 27136, 27212, 27427, 27428 767-330 25137, 25208, 25209, 26983-26988, 26991, 26992 767-332 23275-23279, 23435-23438, 24075-24080, 24759, 24775, 24800, 24802, 24803, 24852, 24981, 24982, 25061, 25122, 25123, 25143-25146, 25306, 25409, 25984-25991, 27110, 27111, 27582-27584, 27961, 27962, 28447-28458, 29689- 29698, 30180, 30198, 30199, 30388, 30573-30575, 30594-30597, 32776 767-333 25583-25588, 30846, 30850-30852 767-336 24333-24343, 25203, 25204, 25442-25444, 25732, 25733, 25826, 25828, 25829, 25831, 25832, 25834, 27140, 29230- 29232 767-338 24146, 24316, 24317, 24407, 24531, 24853, 24929, 24930, 25246, 25274, 25316, 25363, 25575-25577, 28153, 28154, 28724, 28725, 29117, 29118, 30186 767-341 24752, 24753, 24843, 24844, 30341, 30342 767-343 30008, 30009 767-346 23215-23217, 23645, 23961-23966, 24498, 24782, 24783, 27311-27313, 27658, 27659, 28553, 28837, 28838, 29863, 32886-32888, 33493-33497, 33845-33851, 35813-35815, 36131, 37547-37550, 40363-40569 767-352 26261, 26262 767-360 33767-33769 767-366 24541, 24542 767-375 24082-24087, 24306, 24307, 24574, 24575, 25120, 25121, 25864, 25865, 30108, 30112 767-381 23756-23759, 24002-24006, 24350, 24351, 24400, 24415-24417, 24632, 24755, 24756, 24880, 25055, 25136, 25293, 25616-25619, 25654-25662, 27050, 27339, 27444, 27445, 27942, 27943, 27944, 32972-32980, 33506-33508, 35876, 35877, 37719, 37720, 37872, 40564-40567, 40894-40898 767-383 24318, 24357, 24358, 24475-24477, 24729, 24846-24849, 25088, 25365, 26544 767-31A 24428, 24429, 25273, 25312, 26469, 26470, 27619 767-31B 25170, 26259, 26265 767-31K 27205, 27206, 28865 767-32K 33968 767-32L 40342, 40343, 41063 767-33A 25346, 25403, 25530-25536, 27189, 27310, 27376, 27377, 27468, 27476, 27477, 27908, 27909, 27918, 28043, 28138-28141, 28147, 28159, 28495, 33421-33425 767-34G 41519 767-33P 28370, 28392, 33078, 35796, 40533, 40534-40536 767-34P 33047-33049 767-35D 24865, 27902, 28656 767-35E 26063, 26064 767-35H 26387-26389 767-36D 27309, 27684, 27685, 27941, 35155, 35156 767-36N 29898, 30107, 30109-30111, 30115, 30841, 30843, 30847, 30853, 30854 767-37D 26328 767-37E 25077 767-38A 29617, 29618 767-38E 24797, 24798, 25132, 25347, 25404, 25757-25760, 25762, 25763, 29129, 30840 767-39H 26256, 26257 767-3BG 30564-30566 767-3D6 24766-24768 767-3G5 24257-24259, 28111, 29435 767-3J6 25875-25878 767-3KY 42220, 42221, 42223 767-3P6 23764, 24349, 24484, 24485, 24495, 24496, 24983-24985, 25241, 25269, 25354, 26233-26238, 27254, 27255 767-3Q8 24745, 24746, 27600, 27616-27618, 27686, 27993, 28132, 28206, 28207, 29390, 29383, 29386, 29387, 30048, 30301 767-3S1 25221, 26608 767-3T7 25076, 25117 767-3W0 28148, 28149, 28264 767-3X2 26260 767-3Y0 24947, 24948, 24952, 24953, 24999, 25000, 25411, 26200, 26204-26208 767-3Z9 23765, 24628, 26417, 27095, 29867, 30331, 30383 8 A1NM III - Model 767-300 (Cont’d) 767-3BG 30563 767-3CB 33466-33469 Certification Basis: Part 25 of the Federal Aviation Regulations as amended by Amendments 25-1 through 25-37, except where superseded by the following sections of Part 25 as amended by Amendments 25-1 through: Amendment Sections 25-38 25.101, 25.161, 25.397, 25.603, 25.675, 25.685, 25.775, 25.787, 25.815, 25.841, 25.941, 25.951, 25.979(a), (b), (c), 25.999, 25.1027, 25.1041, 25.1093(b), 25.1125, 25.1143(a), (b), (c), (d), 25.1167, 25.1303, 25.1305, 25.1322, 25.1355, 25.1385, 25.1403, 25.1439, 25.1515, 25.1533, 25.1557 25-39 25.807