TCDS A16WE

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 82 61 57 56 54 57 54 56 60 54 56 67 65 63 61 56 57 67 77 77 Page No. 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 Rev No. 67 54 54 81 57 80 71 65 71 63 65 66 66 65 77 74 81 77 77 75 Page No. 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Rev No. 75 71 75 65 75 77 62 67 74 72 81 63 77 77 81 62 81 72 65 62 Page No. 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 Rev No. 64 67 77 81 77 77 82 82 82 82 82 82 82 82 82 82 82 82 82 82 Page No. 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 Rev No. 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 82 Page No. 101 102 103 104 105 106 107 108 109 110 111 112 113 Rev No. 82 82 82 82 82 82 82 82 82 82 82 82 82 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A16WE Revision 82 BOEING 737-100 Series 737-200 Series 737-200C Series 737-300 Series 737-400 Series 737-500 Series 737-700 Series 737-800 Series 737-600 Series 737-700C Series 737-900 Series 737-900ER Series 737-8 737-9 737-8200 737-7 737-10 Date: October 20, 2026 TYPE CERTIFICATE DATA SHEET A16WE This data sheet, which is part of Type Certificate No. A16WE, 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 737-100 (Approved December 15, 1967) Transport Aircraft Engines: 2 Pratt and Whitney Turbofan Engines JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, and JT8D-15; refer to the FAA Approved Airplane Flight Manual for aircraft engine and engine intermix eligibility. (Engine Type Certificate No. E2EA) Fuel: See NOTE 4 for authorized types of fuel. Engine Ratings: Takeoff static thrust Maximum continuous static standard day, sea level thrust, standard day, conditions (5 min.) lb. sea level conditions lb. JT8D-7, -7A, -7B 14,000 12,600 JT8D-9, -9A 14,500 12,600 JT8D-15 15,500 13,700 Engine and Weight Limits: For engine operating limits see engine Type Certificate Data Sheet No. E2EA or the FAA Approved Airplane Flight Manual. Thrust Setting: The appropriate EPR thrust setting curve (EPR or PT 7), in the FAA Approved Airplane Flight Manual of AFM Appendices must be used for control of engine thrust. Airspeed Limits: See the appropriate FAA Approved Airplane Flight Manual listed in NOTE 2. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual listed in NOTE 2. A16WE 2 I - Model 737-100 (Cont’d) Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual listed in NOTE 2. Eligible Serial Numbers: Model: 737-112 19768-19772 737-130 19013-19017, 19018 -19033, 19794, 19437 737-159 19679, 19680 NOTES FOR SECTION I (737-100): NOTE 1. A current weight and balance report, including a list of equipment included in the certificated empty weight and loading instructions when necessary, must be provided for each aircraft at the time of original certification. For each Model the Weight and Balance Control and Loading Manual (Boeing Document D6-15066-1) consists of the Basic Manual and a Supplement Aircraft Report. This is in accordance with 14 CFR 25.29 and 25.1519 which establishes operating limitations determined under 25.23 through 25.27. NOTE 2. Airplane operation must be in accordance with the FAA Approved AFM, Boeing Document No. D6-8737. All placards required in either the FAA Approved AFM, the applicable operating rules or the Certification Basis must be installed in the airplane. NOTE 3. The FAA approved Airworthiness Limitations Section of the Instructions for Continued Airworthiness are referenced in Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), Document D6-38278-CMR. The Airworthiness Limitations section is FAA-approved and specifies maintenance required under 14 CFR 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has been FAA approved. Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6-38278-CMR, is the FAA approved requirement to comply with 14 CFR 25.1529, 43.16 and 91.403. Each operator must incorporate into their airline’s FAA-Approved maintenance program the applicable requirements of this document. NOTE 4. (a) JP-1, JP-4 and JP-5 fuels conforming to P & WA specification No. 522 and later revisions may be used separately or mixed in any proportions without adversely affecting the engine operation or power output. No fuel control adjustment is required when switching fuel types. See AFM specified in Note 2 for limitations on fuel use. (b) Anti-icing fuel additive PFA-55MB may be used if concentration delivered to airplane does not exceed 0.15% by volume. No fuel system anti-icing credit is allowed. See AFM specified in Note 2 for limitations on fuel additive use. NOTE 5. Model designation of the airplanes are identified by the "Dash No." suffix to "737". Consider, for example, the designation “737-105”. The "1" represents the "-100 Series," and the "05" represents the customer's configuration for which initial approval was obtained. NOTE 6. Not used. NOTE 7. The Boeing Supplemental Structural Inspection Document (SSID), D6-37089 and D6-37089-1, are applicable to the 737-100, 737-200 and 737-200C (Sec ADs 98-11-04, Amendment 39-10531, 98-11-04 R1, Amendment 39-10984, and 2008-11-03, Amendment 39-15525). NOTE 8. Except for trunnion pins described below, the life limit for 737-100 main and nose landing gear is 81,000 flight cycles when operated within the ranges of 95 – 111.2 KIPS for taxi weight and 89.7 – 103 KIPS for landing weight. The trunnion pins 65-46113-3 and -5 are to be replaced at 76,000 flight cycles. For detail components lives, see Boeing Service Letter 737-SL-32-21. NOTE 9. Not used. NOTE 10. Individual airplanes may be limited to weights different than those specified herein. Refer to the FAA Approved Airplane Flight Manual or the FAA Approved Weight and Balance Manual to determine maximum permissible operating weights and balance limitations. NOTE 11. JT8D-15 engines equipped with MOD 10 exhaust mixer (Pratt & Whitney Aircraft Part No. 5004027) have same engine limits as JT8D-15 engines with splitter type exhaust system. NOTE 12. Not used. NOTE 13. 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 D6-19567 titled "Service Bulletin 737". The records of airplanes imported into the USA should be reviewed to be sure that further modifications are accomplished to ensure compliance, if the non FAA-approved service bulletins modifications have been installed. NOTE 14. Not used. NOTE 15. Not used. 3 A16WE I - Model 737-100 (Cont’d) NOTE 16. The FAA has determined that the occurrence of any uncontrollable high thrust failure condition “may endanger the safe operation of an airplane” and hence is reportable under §121.703, 125.409, and 135.415. NOTE 17. 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 document, Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations and Certification Maintenance Requirements, Document D6-38278-CMR, Revision May 2006 or later FAA-approved revision (see AD 2008-10-09R1, Amendment 39-16148). II - Model 737-200 (Approved December 21, 1967) Transport Aircraft Engines: 2 Pratt and Whitney Turbofan Engines JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, JT8D-15, JT8D- 15A, JT8D-17, and JT8D-17A; Refer to the FAA Approved Airplane Flight Manual for aircraft engine and engine intermix eligibility. (Engine Type Certificate No. E2EA) Fuel: See NOTE 4 for authorized types of fuel. Engine Ratings: Takeoff static thrust, Maximum continuous static standard day, sea level thrust, standard day, conditions (5 min) lb. sea level conditions lbs. JT8D-7, -7A, -7B 14,000 12,600 JT8D-9, -9A 14,500 12,600 JT8D-15, -15A 15,500 13,750 JT8D-17, -17A 16,000 15,200 Engine and Weight Limits Thrust Settings: The appropriate thrust setting curve (EPR or Pt7), in the FAA Approved Airplane Flight Manual or AFM Appendices must be used for control of engine thrust. Airspeed Limits: See the appropriate FAA Approved Airplane Flight Manual listed in Note 2. C.G. 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. Eligible Serial Numbers: Model: 737-201 19418-19423, 20211-20216, 21665-21667, 21815-21818, 22018, 22273-22275, 22352-22355, 22443- 22445, 22751-22758, 22795-22799, 22806, 22866-22869, 22961, 22962 737-204 19707-19712, 20236, 20417, 20632, 20633, 20806-20808, 21335, 21336, 21693, 21694, 22057-22059, 22364, 22365, 22638-22640, 22966, 22967 737-205 19408, 19409, 20412, 20711, 21184, 21219, 21445, 21729, 21765, 22022, 23464-23469 737-209 23795, 23796, 23913, 24197 737-210 21820 737-212 20492, 20521 737-214 19681, 19682, 19920, 19921, 20155-20160, 20368 737-217 19884-19888, 20196, 20197, 21716-21718, 22255-22260, 22341, 22342, 22658, 22659, 22728, 22729, 22864, 22865 737-219 19929-19931, 20344, 21130, 21131, 21645, 22088, 22657, 23470-23475 737-222 19039-19078, 19547-19556, 19758, 19932-19956 737-228 23000-23011, 23349, 23503, 23504, 23792, 23793 737-229 20907-20912, 21135-21137, 21176, 21177, 21596, 21839, 21840 737-230 22113-22143, 22402, 22634-22637, 23153-23158 737-232 23073-23105 737-236 21790-21808, 22026-22034, 23159-23172, 23225, 23226 737-241 21000-21009 737-242 21186, 22074, 22075 737-244 19707, 19708, 20229, 20329-20331, 22580-22591, 22828 737-247 19598-19617, 20125-20134, 23184-23189, 23516-23521, 23602-23609 737-248 19424, 19425, 20221-20223, 21714, 21715 737-258 22856, 22857 737-260 23914, 23915 737-266 21191-21196, 21227 737-268 20576-20578, 20882, 20883, 21275-21277, 21280-21283, 21360-21362, 21653, 21654, 22050 A16WE 4 II - 737-200 (Cont’d) 737-269 21206 737-275 19742, 20142, 20588, 20670, 20785, 20922, 20958, 20959, 21115, 21639, 21712, 21713, 21819, 22086, 22087, 22159, 22264-22266, 22807, 22873, 22874, 23283-23285 737-277 22645-22656 737-281 20226, 20227, 20276, 20277, 20413, 20414, 20449-20452, 20506-20508, 20561-20563, 21766-21771 737-282 23041-23046 737-284 21224, 21225, 21301, 21302, 21500, 21501, 22300, 22301, 22338, 22339, 22343, 22400, 22401 737-286 20498, 20499, 21317 737-287 20403-20406, 20523, 20537, 20768, 20964-20966 737-291 20361-20365, 21069, 21508, 21509, 21544-21546, 21640-21642, 21747-21751, 21980, 21981, 22089, 22383, 22384, 22399, 22456, 22457, 22741-22744, 23023, 23024 737-293 19306-19309, 19713, 19714, 20334, 20335 737-296 22276, 22277, 22516, 22398 737-297 20209, 20210, 20242, 21739, 21740, 22051, 22426, 22629-22631 737-25A 23789-23791 737-25C 24236 737-27A 23794 737-2A1 20092-20096, 20589, 20777-20779, 20967-20971, 21094, 21095, 21597-21599, 22602 737-2A3 20299, 20300, 22737-22739 737-2A6 20194, 20195, 20412 737-2A8 20480-20486, 20960-20963, 21163, 21164, 21496-21498, 22280-22286, 22860-22863, 23036, 23037 737-2A9 20956 737-2B1 20280, 20281, 20786 737-2B2 20231, 20680 737-2B6 21214-21216, 22767 737-2B7 22878-22892, 23114-23116, 23131-23135 737-2C0 20070-20074 737-2C3 21012-21017 737-2C9 21443, 21444 737-2D6 20544, 20759, 20884, 21063-21065, 21211, 21212, 21285, 21286, 22766 737-2E1 20396, 20397, 20681, 20776, 20976, 21112 737-2E3 22703, 22792 737-2E7 22875, 22876 737-2F9 20671, 20672, 22771-22774, 22985, 22986 737-2H3 21973, 22624, 22625 737-2H4 20336, 20345, 20369, 20925, 21117, 21262, 21337-21340, 21447, 21448, 21533-21535, 21593, 21721, 21722, 21811, 21812, 21970, 22060-22062, 22356-22358, 22673-22675, 22730-22732, 22826, 22827, 22903-22905, 22963-22965, 23053-23055, 23108-23110, 23249 737-2H5 20453, 20454 737-2H6 20582-20584, 20586, 20587, 20631, 20926, 21732, 22620, 23320, 23849 737-2J8 22859 737-2K2 21397, 22025, 22296, 22906 737-2K3 23912, 24139 737-2K5 22596-22601 737-2K6 20957, 22340 737-2K9 22415, 22416, 22504, 22505, 23386, 23404, 23405 737-2L7 21616 737-2L9 21278, 21279, 21528, 21685, 21686, 22070-22072, 22406-22408, 22733-22735 737-2M2 21172, 21723, 22626, 22775, 22776, 23220, 23351 737-2M6 20913, 21138 737-2M8 21231, 21736, 21955, 22090 737-2M9 21236 737-2N1 21167 737-2N3 21165, 21166 737-2N7 21226 737-2N8 21296 737-2N0 23677-23679 737-2P5 21440, 21810, 22267, 22667, 23113 737-2P6 21355-21359, 21612, 21613, 21677, 21733, 21734 737-2Q3 21476-21478, 22367, 22736, 23117, 23481, 24103 737-2Q8 21518, 21687, 21735, 21960, 22453, 22760, 23148 737-2Q9 21719, 21720, 21975, 21976 737-2S3 21774-21776, 22278, 22279, 22633, 22660 737-2S9 21957 737-2T2 22793 737-2T4 22054, 22055, 22368-22371, 22529, 22697-22701, 22800-22804, 23272-23274, 23443-23447 5 A16WE II - 737-200 (Cont’d) 737-2T5 22023, 22024, 22395-22397, 22632, 22979 737-2T7 22761, 22762 737-2U4 22161, 22576 737-2U9 22575 737-2V2 22607 737-2V5 22531 737-2V6 22431 737-2W8 22628 737-2X2 22679 737-2X9 22777-22779 737-2Y5 23038-23040, 23847, 23848, 24031 737-2Z6 23059 737-T43A 20685-20703 NOTES FOR SECTION II (737-200): NOTE 1. A current weight and balance report, including a list of equipment included in the certificated empty weight and loading instructions when necessary, must be provided for each aircraft at the time of original certification. For each Model the Weight and Balance Control and Loading Manual (Boeing Document D6-15066-2) consists of the Basic Manual and a Supplement Aircraft Report. This is in accordance with 14 CFR 25.29 and 25.1519 which establishes operating limitations determined under 25.23 through 25.27. NOTE 2. Airplane operation must be in accordance with the FAA Approved AFM, Boeing Document No. D6- 8737. All placards required in either the FAA Approved AFM, the applicable operating rules or the Certification Basis must be installed in the airplane. NOTE 3. The FAA approved Airworthiness Limitations Section of the Instructions for Continued Airworthiness are referenced in Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), Document D6-38278-CMR. The Airworthiness Limitations section is FAA-approved and specifies maintenance required under 14 CFR 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has been FAA approved. Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6-38278-CMR, is the FAA approved requirement to comply with 14 CFR 25.1529, 43.16 and 91.403. Each operator must incorporate into their airline’s FAA-Approved maintenance program the applicable requirements of this document. NOTE 4. (a) JP-1, JP-4 and JP-5 fuels conforming to P & WA specification No. 522 and later revisions may be used separately or mixed in any proportions without adversely affecting the engine operation or power output. No fuel control adjustment is required when switching fuel types. See AFM specified in Note 2 for limitations on fuel use. (b) Anti-icing fuel additive PFA-55MB may be used if concentration delivered to airplane does not exceed 0.15% by volume. No fuel system anti-icing credit is allowed. See AFM specified in Note 2 for limitations on fuel additive use. NOTE 5. Model designation of the airplanes are identified by the "Dash No." suffix to "737". Consider, for example, the designation “737-105”. The "1" represents the "-100 Series," and the "05" represents the customer's configuration for which initial approval was obtained. NOTE 6. Not used. NOTE 7. The Boeing Supplemental Structural Inspection Document (SSID), D6-37089 and D6-37089-1, are applicable to the 737-100, 737-200 and 737-200C (Sec ADs 98-11-04, Amendment 39-10531, 98-11-04 R1, Amendment 39-10984, and 2008-11-03, Amendment 39-15525). NOTE 8. All Model 737-200 series airplanes having serial numbers 20492 and on, are of the -200 advanced series airplane. All earlier airplanes can be kit modified to the advanced configuration. NOTE 9. The "Advanced" configuration (for aircraft with serial numbers before 20492) consists of the following performance modification kits to be operator installed in the following order, if desired: (a) A stopping package, MC 3452, (S.B. 32-1051) plus a high lift package (MC-3400). (b) The above (a) plus JT8D-15 engine (MC-3510). NOTE 10. Individual airplanes may be limited to weights different than those specified herein. Refer to the FAA Approved Airplane Flight Manual or the FAA Approved Weight and Balance Manual to determine maximum permissible operating weights and balance limitations. NOTE 11. JT8D-15 engines equipped with MOD 10 exhaust mixer (Pratt & Whitney Aircraft Part No. 5004027) have same engine limits as JT8D-15 engines with splitter type exhaust system. A16WE 6 II - 737-200 (Cont’d) NOTE 12. Reference Boeing Document D6-37349 for approved autoland equipment limitations for Model 737-200 series airplanes. NOTE 13. 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 D6-19567 titled "Service Bulletin 737". The records of airplanes imported into the USA should be reviewed to be sure that further modifications are accomplished to ensure compliance, if the non FAA-approved service bulletins modifications have been installed. NOTE 14. Airplanes line numbers 1591, 1593, 1595, and on, were manufactured on or after August 20, 1988, and airplane line numbers 1718, 1903, 1907, and on, were manufactured on or after August 20, 1990. Reference §121.312(a)(1) and (2) Amendment 121-198. Airplanes 1718, 1907 through 1927 are exempt (Exemption No. 5176A). See Service Bulletin Index Part 3 for cross reference of line number to airplane serial number. NOTE 15. The type design reliability and performance of the Model 737-200, -300, -400, and -500 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 D6-38091 “CONFIGURATION, MAINTENANCE, AND PROCEDURES FOR EXTENDED RANGE (ER) OPERATION” for the Model 737-200, and Boeing Document D6-38123 for the Models 737-300, -400, and -500. NOTE 16. The FAA has determined that the occurrence of any uncontrollable high thrust failure condition “may endanger the safe operation of an airplane” and hence is reportable under §121.703, 125.409, and 135.415. NOTE 17. 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 and Special Conditions 25-308-SC are listed in the FAA-approved Airworthiness Limitations document, Boeing 737- 100/200/200C/300/400/500 Airworthiness Limitations and Certification Maintenance Requirements, Document D6-38278-CMR, Revision May 2006 or later FAA-approved revision (see AD 2008-10-09R1, Amendment 39-16148). NOTE 18. (a) For 737-200 airplanes operated within the ranges of 95 – 111.2 KIPS for taxi weight and 89.7 – 103 KIPS for landing weight: The life limit for main and nose landing gear is 81,000 flight cycles. (b) For 737-200 High Gross Weight (HGW) airplanes, operated within 114 – 128.6 KIPS taxi weight and 103 – 107 KIPS landing weight: The life limit for main and nose gear is 100,000 and 90,000 flight cycles respectively (c) Trunnion pins 65-46113-3 and -5 are to be replaced at 76,000 flight cycles and (d) Forward trunnion fuse bolts 65-42196-4, -5 and 69-58854-2 are to be replaced at 83,000 flight cycles. (e) For detail components lives, see Boeing Service Letter 737-SL-32-21. III - Model 737-200C (Approved October 29, 1968) Transport Aircraft Engines: 2 Pratt and Whitney Turbofan Engines JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, JT8D-15, JT8D- 15A, JT8D-17, and JT8D-17A; Refer to the FAA Approved Airplane Flight Manual for aircraft engine and engine intermix eligibility. (Engine Type Certificate No. E2EA) Fuel: See NOTE 4 for authorized types of fuel. Engine Ratings: Takeoff static thrust, Maximum continuous standard day, sea level static thrust, standard conditions (5 min) lb. day, sea level conditions lb. JT8D-7, -7A, -7B 14,000 12,600 JT8D9D-9, -9A 14,500 12,600 JT8D-15, -15A 15,500 13,750 JT8D-17, -17A 16,000 15,200 Engine and Weight Limits For engine operating limits see engine TC Data Sheet No. E2EA or the FAA Approved Airplane Flight Manual. Thrust Settings: The appropriate thrust setting curve (EPR or Pt7), in the FAA Approved Airplane Flight Manual or AFM Appendices must be used for control of engine thrust. Airspeed Limits: See the appropriate FAA Approved Airplane Flight Manual listed in NOTE 2. 7 A16WE III - 737-200C (cont’d) C.G. 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. Eligible Serial Numbers: Model: 737-202C 19426 737-204C 20282, 20389 737-205C 20458 737-210C 19594, 20138, 20440, 20917, 21066, 21067, 21821, 21822 737-219C 22994 737-229C 20914-20916, 21139, 21738 737-230C 20253-20258 737-242C 19847, 19848, 20455, 20496, 21728, 22877 737-248C 20218-20220, 21011 737-268C 20574, 20575 737-270C 20892, 20893, 21183 737-275C 19743, 21116, 21294, 22160, 22618 737-282C 23051 737-286C 20500, 20740 737-287C 20407, 20408 737-290C 22577, 22578, 23136 737-298C 20793-20795 737-2A1C 21187, 21188 737-2A8C 22473 737-2A9C 20205, 20206 737-2B1C 20536 737-2B6C 23049, 23050 737-2D6C 20650, 20758, 21287 737-2H3C 21974 737-2H4C 20346 737-2H6C 21109 737-2H7C 20590, 20591, 23386 737-2J8C 21169, 21170 737-2K2C 20836, 20943, 20944 737-2L7C 21073 737-2M2C 21173 737-2M6C 21809 737-2N9C 21499 737-2Q2C 21467 737-2Q5C 21538 737-2Q8C 21959 737-2R4C 21763, 23129, 23130 737-2R6C 22627 737-2R8C 21710, 21711 737-2S2C 21926-21929 737-2S5C 22148 737-2T2C 22056 737-2T4C 23065, 23066 737-2X6C 23121-23124, 23292 NOTES FOR SECTION III (737-200C): NOTE 1. A current weight and balance report, including a list of equipment included in the certificated empty weight and loading instructions when necessary, must be provided for each aircraft at the time of original certification. For each Model the Weight and Balance Control and Loading Manual (Boeing Document D6-15066-3) consists of the Basic Manual and a Supplement Aircraft Report. This is in accordance with 14 CFR 25.29 and 25.1519 which establishes operating limitations determined under 25.23 through 25.27. NOTE 2. Airplane operation must be in accordance with the FAA Approved AFM, Boeing Document No. D6- 8737. All placards required in either the FAA Approved AFM, the applicable operating rules or the Certification Basis must be installed in the airplane. A16WE 8 III - 737-200C (cont’d) NOTE 3. The FAA approved Airworthiness Limitations Section of the Instructions for Continued Airworthiness are referenced in Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), Document D6-38278-CMR. The Airworthiness Limitations section is FAA-approved and specifies maintenance required under 14 CFR 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has been FAA approved. Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6-38278-CMR, is the FAA approved requirement to comply with 14 CFR 25.1529, 43.16 and 91.403. Each operator must incorporate into their airline’s FAA-Approved maintenance program the applicable requirements of this document. NOTE 4. (a) JP-1, JP-4 and JP-5 fuels conforming to P & WA specification No. 522 and later revisions may be used separately or mixed in any proportions without adversely affecting the engine operation or power output.