TCDS A2NM

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