TCDS A20WE

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 63 56 44 56 56 56 56 56 55 56 56 63 58 59 59 63 59 59 59 63 Page No. 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 Rev. No. 59 61 59 63 59 59 59 59 59 59 59 59 59 59 59 61 62 59 59 59 Page No. 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Rev. No. 59 59 59 59 59 59 59 59 59 59 59 60 59 59 59 59 59 64 59 59 Page No. 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 Rev. No. 59 59 59 59 59 59 59 59 59 59 60 59 60 59 59 60 59 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A20WE BOEING Revision 64 747-100 Series 747-200B Series 747-200F Series 747-200C Series 747SR Series 747SP Series 747-100B Series 747-300 Series 747-100B SUD Series 747-400 Series 747-400D Series 747-400F Series 747-8F Series 747-8 Series August 8, 2025 TYPE CERTIFICATE DATA SHEET NO. A20WE This data sheet, which is a part of Type Certificate No. A20WE, 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 - 747-100 (Approved December 30, 1969) Transport Aircraft Engines: 4 Pratt and Whitney JT 9D-3, JT9D-3A, or JT9D-7, JT9D-7A, JT9D-7F, JT9D-7J. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (K EAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manual: D6-13703 A20WE 2 I - 747-100 (cont’d): Model Eligible Serial Numbers 747-1D1 20208 747-121 19637-19661, 20235, 20347-20354 747-122 19753-19757, 19875-19883, 19925-19928 747-123 20100-20109, 20323-20326, 20390, 20391 747-124 19733-19735, 20305 747-127 20207 747-128 19749-19752, 20355, 20376-20378, 20541-20543, 20798-20800, 20954, 21141 747-129 20401, 20402 747-130 19746-19748 747-131 19667-19678, 20080-20083, 20320-20322 747-132 19896-19898, 20246, 20247 747-133 20013-20015, 20767, 20881 747-135 19918, 19919 747-136 19761-19766, 20269-20273, 20284, 20708, 20809, 20810, 20952, 20953, 21213 747-143 19729, 19730 747-146 19725-19727, 20332, 20528, 20531, 20532, 21029 747-148 19744, 19745 747-151 19778-19787 747-156 19957, 19958 II - 747-200B (Approved December 23, 1970) Transport Aircraft The 747-200B is an extended-range passenger version of the basic 747-100 series aircraft. The exterior geometry of the 747-200B is identical to the 747-100 and aircraft systems are essentially unchanged except for differences resulting from changes outlined below. The principal differences involve the following: Increased strength wing structure, local body and empennage changes for increased strength, increased center wing tank fuel capacity, increased strength landing gear, modified nacelle and engine acoustic treatment, increased gross weight, and modified balance limits. Engines: 4 Pratt and Whitney JT9D-3 A, JT9D-7, JT9D-7A, JT9D-7F, JT9D-7J, JT9D-70A, JT9D-7Q, JT9D-7Q3, JT9D-7R4G2 4 General Electric CF6-50E, CF6-50E1, CF6-50E2, CF6-80C2B1 4 Rolls Royce RB211-524B2-19, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700, 1E-4A-5, 1E-4B-5 FAA Approved Airplane Flight Manuals: D6-13703, D6-33747, D6-34747, D6-35747 3 A20WE II - 747-200B (cont’d): Model Eligible Serial Numbers 747-206B 19922-19924, 20398-20400, 20427, 21110, 21111, 21549, 21550, 21659, 21660, 21848, 22376, 22379, 22380 747-209B 21454, 21843, 22446, 22447 747-211B 21516, 21517 747-212B 20712, 20713, 20888, 21048, 21162, 21316, 21439, 21683, 21684, 21935-21944 747-217B 20801, 20802, 20927, 20929 747-219B 22722-22725, 22791 747-222B 23736, 23737 747-227B 21682, 21991, 22234 747-228B 21326, 21429, 21537, 21731, 21745, 21982, 22272, 22427, 22428, 22794, 23611, 23676, 24067 747-230B 20372, 20527, 21220, 21221, 21380, 21588-21591, 21643, 21644, 22363, 22669-22671, 23286, 23287, 23393, 23407, 23509, 23622 747-233B 20977, 21627 747-236B 21238-21241, 21350, 21351, 21536, 21635, 21830, 21831, 22303-22305, 22442, 23711, 23735, 23799, 24088 747-237B 19959, 19960, 20459, 20558, 21182, 21446, 21473, 21829, 21993-21995 747-238B 20009-20012, 20534, 20535, 20841, 20842, 20921, 21054, 21140, 21237, 21352-21354, 21657, 21658, 21977, 22145, 22614-22616 747-240B 21825, 22077 747-243B 19731, 19732, 20520, 22506-22508, 22510-22513, 22969, 23300, 23301, 23476 747-244B 20237-20239, 20556, 20557, 22170, 22171 747-246B 19823-19825, 20333, 20503-20505, 20529, 20530, 20924, 21030, 21031, 21678-21680, 22064, 22065, 22478, 22479, 22745, 22746, 22990, 22991, 23389 747-247B 22378 747-251B 20356-20360, 21704-21709, 22389, 23111, 23112, 23547-23549 747-256B 20137, 22238, 22239, 22454, 22455, 22764, 24071 747-257B 20116, 20117 747-258B 20135, 20274, 20704, 22254 747-259B 21730 747-267B 21746, 21966, 22149, 22429, 22530, 22872, 23048, 23120 747-269B 21541-21543, 22740 747-281B 23501, 23502, 23698, 23813, 24399 747-282B 20501, 20502, 20928, 21035 747-283B 20120, 20121, 21381, 21575, 22381, 22496 747-284B 20742, 20825 747-286B 21217, 21218 747-287B 21189, 21725-21727, 22297, 22592, 22593 747-2B2B 21614 747-2B3B 22514, 22515 747-2B4B 21097-21099 747-2B5B 20770, 20771, 21772, 21773, 22482, 22485 747-2B6B 21615 747-2D3B 21251, 21252, 22579 747-2D7B 21782-21784, 22337, 22471, 22472 747-2F4B 20493, 20559 747-2F6B 21832-21834, 22382 747-2G4B 23824, 23825 747-2J6B 23071, 23461, 23746 747-2L5B 22105-22107 747-2Q2B 21468 747-2U3B 22246-22249, 22768, 22769 747-E4A 20682-20684 747-E4B 20949 A20WE 4 III - 747-200F (Approved March 7, 1972) Transport Aircraft The 747-200F is a freighter version of the basic 747-200B series aircraft. The exterior geometry of the 747-200F is identical to the 747-200B and aircraft systems are essentially unchanged except for differences resulting from the changes outlined below. The principal differences involve the following: Upward opening nose cargo door. Redesigned interior for freight handling. Revised upper deck layout for additional crew members. Increased strength of main deck floor and keel beam. Increased strength of center wing section. Deletion of main deck windows and passenger doors 1 through 5 right side and 2 through 4 left side. T.E. flap two position load relief system. Revised air conditioning system to suit freight requirements. Main deck smoke detection system. Optional main deck smoke detection system. Optional side cargo door. Engines: 4 Pratt and Whitney JT9D-3 A, JT9D-7, JT9D-7A, JT9D-7F, JT9D-7J, JT9D-70A, JT9D-7Q, JT9D-7Q3, JT9D-7R4G2 4 General Electric CF6-50E, CF6-50E1, CF6-50E2 4 Rolls Royce RB211-524B2-19, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manuals: D6-13703, D6-33747, D6-35747, D6-34747 Model Eligible Serial Numbers 747-209F 22299, 24308 747-212F 24177 747-221F 21743, 21744 747-228F 20887, 21255, 21576, 21787, 22678, 22939, 24158, 24735, 24879, 25266 747-230F 20373, 21592, 22668, 23348, 23621, 24138 747-236F 22306 747-243F 22545 747-245F 20826, 20827, 21764, 21841, 22150, 22151 747-246F 21034, 21681, 22063, 22477, 22989, 23391, 23641 747-249F 21827, 21828, 22237, 22245 747-251F 21120-21122, 21321, 22388, 23887, 23888 747-258F 21737 747-267F 23864, 24568 747-268F 24359 747-281F 23138, 23139, 23350, 23919, 24576, 25171 747-2B3F 21515, 21835 747-2B5F 22480, 22481, 22486, 24195, 24196 747-2J6F 24960 747-2J9F 21486, 21487, 21507, 21514, 21668 747-2R7F 21650, 22390 747-2S4F 22169 5 A20WE IV - 747-200C (Approved April 17, 1973) Transport Aircraft The 747-200C is a convertible version of the basic 747-200B series aircraft. The exterior geometry of the 747-200C is identical to the 747-200B and aircraft systems are essentially unchanged except for differences resulting from the changes outlined below. The principal differences involve the following: Upward opening nose cargo door. Redesigned interior permitting all passenger, all cargo, or mixed passenger/cargo configurations. Increased strength of main deck floor and keel beam. Increased strength of center wing section. T.E. flap two position load relief system. Main deck smoke detection system. Optional side cargo door. Engines: 4 Pratt and Whitney JT9D-3 A, JT9D-7, JT9D-7A, JT9D-7F, JT9D-7J, JT9D-70A,JT9D-7Q, JT9D-7Q3, JT9D-7R4G2 4 General Electric CF6-50E, CF6-50E1,CF6-50E2 4 Rolls Royce RB211-524B2-19, RB211-524C2, RB211-524D4. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/ Cargo: See the appropriate Weight an d Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manuals: D6-13703, D6-33747 Model Eligible Serial Numbers 747-21AC 23652, 24134 747-258C 21190, 21594 747-270C 21180, 21181, 22366 747-271C 21964, 21965, 22403 747-273C 20651-20653 V - 747SR (Approved September 26, 1973) Transport Aircraft The 747SR is basically a 747-100 series airplane with certain modifications to improve the fatigue life. Engines: 4 General Electric CF6-45A, CF6-45A2, CF6-50E2 4 Pratt and Whitney JT9D-7, JT9D-7A. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. A20WE 6 V - 747SR (cont’d): MaximumBaggage/Cargo: See the appropriate Wei ght and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manuals: D6-13703, D6-33747 Model Eligible Serial Numbers 747SR-46 20781-20784, 20923, 21032, 21033 747SR-81 21604-21606, 21922-21925, 22291-22294, 22594, 22595, 22709-22712 VI - 747SP (Approved February 4, 1976) Transport Aircraft The 747SP (Special Performance) is basically a long-range derivative of the 747-100. The exterior geometry of the 747SP has been changed from the 747-100. Aircraft systems are essentially unchanged except for differences resulting from changes outlined below. The principal differences involve the following: Overall airplane length is 47'1" shorter. Body is 48'5" shorter. Overall airplane height is approximately 2'11" higher. Vertical tail has been extended 5 feet. Horizontal tail has been extended on each end. Flaps have been modified to a single variable pivot flap. Main deck doors are reduced to 4 on each side. Engines: 4 Pratt and Whitney JT9D-3, JT9D-3 A, JT9D-7, JT9D-7A, JT9D-7F, JT9D-7J 4 Rolls Royce RB211-524B2-19, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-33800 FAA Approved Airplane Flight Manuals: D6-34047, D6-36747 Model Eligible Serial Numbers 747SP-09 21300, 22298, 22547, 22805 747SP-21 21022-21026, 21441, 21547, 21548, 21648, 21649 747SP-27 21785, 21786, 21992, 22302 747SP-31 21961-21963 747SP-38 22495, 22672 747SP-44 21132-21134, 21253, 21254, 21263 747SP-68 21652, 22503, 22750 747SP-70 22858 747SP-86 20998, 20999, 21093, 21758 747SP-94 21174, 21175 747SP-B5 22483, 22484 747SP-J6 21932-21934 747SP-Z5 23610 7 A20WE VII - 747-100B (Approved August 1, 1979) Transport Aircraft The 747-100B is basically a 747SR series airplane with certain modifications to permit increases in maximum permissible operating weights. Engines: 4 Pratt and Whitney JT9D-7A, JT9D-7F 4 Rolls Royce RB2ll-524B2-19, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manuals: D6-13703, D6-35747 Model Eligible Serial Numbers 747-146B 22066, 22067, 23150 747-168B 22498-22502, 22747-22749 747-186B 21759 See NOTE 8. VIII - 747-300 (Approved March 1, 1983) Transport Aircraft The 747-300 is basically a 747-200 series airplane with a stretched upper deck. Engines: 4 Pratt and Whitney JT9D-7R4G2 4 General Electric CF6-50E2, CF6-80C2B1 4 Rolls Royce RB211-524B2-19, RB211-524C2-19, or RB211-524D4-19, RB211-524D4-39. See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manuals: D6-13703, D6-33747, D6-35747 A20WE 8 VIII – 747-300 (cont’d): Model Eligible Serial Numbers 747-306 23056, 23137, 23508 747-312 23026-23033, 23243-23245, 23409, 23410, 23769 747-329 23439, 24837 747-337 24159, 24160 747-338 23222-23224, 23408, 23688, 23823 747-341 23394, 23395, 24106-24108 747-344 22970, 22971 747-346 23067, 23068, 23149, 23151, 23482, 23638-23640, 23967-23969, 24018, 24019, 24156 747-357 22704, 22705, 22995, 22996, 23751 747-366 24161, 24162 747-367 23221, 23392, 23534, 23709, 23920, 24215 747-368 23262-23271 747-3B3 22870, 23413, 23480 747-3B5 22487, 22489, 24194 747-3D7 23721, 23722 747-3G1 23070 747-3H6 23600 IX - 747-100B SUD (Approved March 24, 1986) Transport Aircraft The 747-100B SUD is basically a 747-100B series airplane with a stretched upper deck. Engines: 4 Pratt and Whitney JT9D-7A See NOTE 6 regarding intermixing of engines. Fuel: See NOTE 4. Engine Limits: See data pertinent to all models. Airspeed Limits: VMO/MMO 375/0.92 (KEAS) For other airspeed limits see the appropriate FAA Approved Airplane Flight Manual. C.G. Range: See the appropriate FAA Approved Airplane Flight Manual. Maximum Weights: See the appropriate FAA Approved Airplane Flight Manual. Maximum Baggage/Cargo: See the appropriate We ight and Balance Control and Loading Manual. Fuel and Oil Capacity: See the appropriate Weight and Balance Control and Loading Manual. FAA Approved Weight and Balance Control and Loading Manual: D6-13700 FAA Approved Airplane Flight Manual: D6-13703 Model Eligible Serial Numbers 747-146B SUD 23390, 23637 DATA PERTINENT TO ALL MODELS, EXCEPT MODEL 747-400 AND 747-8 SERIES Engine Limits: (Pratt & Whitney) JT9D-3 JT9D-3A JT9D-7 JT9D-7A JT9D-7F JT9D-7J Takeoff static thrust 43,500 43,500 45,500 46,150 46,750 48,650 standard day, lbs. lbs. lbs. lbs. lbs. lbs. seal level conditions (in pounds); Dry (5 min) (Ideal) With water injection 43,500 45,000 47,000 47,670 48,650 (2 1/2 min.) lbs. lbs. lbs. lbs. lbs. 9 A20WE DATA PERTINENT TO ALL MODELS, EXCEPT MODEL 747-400 AND 747-8 SERIES (cont’d): Maximum continuous JT9D-3 JT9D-3 A JT9D-7 JT9D-7A JT9D-7F JT9D-7J static thrust, standard day, sea 36,400 36, 400 39,650 40,080 39,200 40,200 level condition: lbs. lbs. lbs. lbs. lbs. lbs. (Ideal) Engine Limits: (Pratt & Whitney) JT9D-70A JT9D-7Q JT9D-7Q3 JT9D-7R4G2 Takeoff static thrust standard day, 51,140 51,100 51,100 54,750 sea level conditions lbs. lbs. lbs. lbs. (in pounds) Dry (5 min) (Ideal) Maximum continuous static thrust: 44,290 44,290 44,290 50,200 standard day, sea level lbs. lbs. lbs. lbs. condition: (Ideal) Engine Limits (General Electric) CF6-50E CF6-50E1 CF6-45A CF6-50E2 CF6-45A2 CF6-80C2B1 Engine thrust ratings: (Ideal) Takeoff (5 min) 51,800 lbs. 45,600 lbs. 55,980 lbs. Maximum continuous 46,300 lbs. 43,250 lbs. Engine Limits: (Rolls Royce) RB211-524B2-19 Rated takeoff thrust (5 min.) 49,120 lbs. Sea level static conditions (Ideal) Rated Maximum continuous thrust 44,780 lbs. Engine Limits: RB211-524D4-19 (Rolls Royce) RB211-524C2-19 RB211-524D4-39 Rated takeoff thrust (5 min.) 50,600 lbs. 51,980 lbs. Sea level static conditions (Ideal) Rated Maximum continuous thrust 46,120 lbs. 47,230 lbs. For engine operating limits see the FAA Approved Airplane Flight Manual under the serial numbers section of this data sheet or the appropriate engine type certificate data sheet: Pratt & Whitney E3NE and E20EA General Electric E23EA and E13NE Rolls Royce E12EU Thrust Setting: The appropriate EPR or N1 thrust setting curve in Section 4 of the Airplane Flight Manual must be used for control of engine thrust. Maximum Operating Altitude: The maximum operati ng altitude is 45,100 feet. A20WE 10 DATA PERTINENT TO ALL MODELS, EXCEPT MODEL 747-400 AND 747-8 SERIES (cont’d): Minimum Crew: For all flights, 3 persons (pilot, copilot, flight engineer). When passengers are being carried, one attendant is required at each No. 3 over-wing exit. At least one flight attendant is required on the upper deck during taxi, takeoff and landing when passengers occupy the upper deck. Maximum Passengers: For 747SR and 747-100, -100B, -200B, -200C airplanes the total passenger capacity is limited to: 550 with 5 pair of Type "A" exits on main deck 440 with 4 pair of Type "A" exits on main deck Upper deck passenger capacity is limited to: 8 with one exit on the upper deck 16 with one exit, improved slide and smoke barrier 24 with one exit, straight stairway, smoke barrier, and escape slide capable of operation in 25 kt. Wind 32 if in compliance with the requirements of Special Condition No. 25-61-NW-1 45 if in compliance with the requirements of Special Condition No. 25-71-NW-3 5 persons on upper deck per Exemption 1870D. (747-100 and 747-200) For 747SP the total passenger capacity is limited to: 400 passengers with the same upper deck limits as listed above. For 747-200F the total passenger capacity is limited to: 19 passengers on upper deck with 2 doors, 25 knot slides, C.G. Limitation, and compliance shown with AD 93-07-15; or 19 persons on upper deck equipped with emergency descent reels and harnesses, 2 doors and 25 knot slides. 5 persons on upper deck per Exemption 1870D. For 747-300 and 747-100B SUD the total passenger capacity is limited to: 660 passengers with 5 pair of Type "A" exits on the main deck plus one pair of Type "A"exits on the upper deck. Main deck limited to 550 and upper deck limited to 110 if in compliance with the requirements of modified Special Condition No. 25-71-NW-3, transmitted to Boeing by FAA letter dated August 3, 1981.) See NOTE 10. 550 passengers with 4 pair of Type "A" exits on the main deck limited to 440 and upper deck limited to 110 if in compliance with the requirements of modified Special Condition No. 25-71-NW-3, transmitted to Boeing by FAA letter dated August 3, 1981. Required Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (See Certification Basis) must be installed in the aircraft for certification. The required equipment is noted in the Type Design Data. Datum: Balance Arm Datum corresponds to Body Station 0 and is 90 inches (290 inches on SP) forward of nose. All productions stations coincide numerically with arms except on 747SP. Horizontal distance of datum to nose gear jack points in 384.7 inches. (584.7 inches on 747SP) Mean Aerodynamic Chord (MAC): MAC length is 327.8 inches. Lead ing edge of MAC is 1258 inches aft of datum. Level Means: A plumb-bob attachment and leveling provision scale are provided in the R.H. body wheel well at BS 1444.0. They are referred to as ARM on the 747SP and are a true measure in inches aft of a forward reference datum which is located 290 inches ahead of the airplane nose. Balance ARMS have the following relationship with Body Stations on the 747SP: BODY STATION ADJUSTMENT ARM INCHES INCHES INCHES 90 to 800 +200 290 to 1,000 (800 to 1,000 Section removed) 1,000 to 1,480 0 1,000 to 1,480 (1,480 to 1,640 Section removed) 1,640 to 2,140 -160 1,480 to 1,980 (2,140 to 2,360 Section removed) 2,360 to 2,792 -380 1,980 to 2,412 11 A20WE DATA PERTINENT TO ALL MODELS, EXCEPT MODEL 747-400 AND 747-8 SERIES (cont’d): Control Surface Movements: To insure proper operation of the airplane, the movement of the various control surfaces must be carefully controlled by proper rigging of the flight control systems. The airplane must, therefore, be rigged according to the following FAA-approved data: Boeing Drawing Numbers 65B04001 Control Installation Aileron and Spoiler 65B04002 Control Installation Elevator 65B04003 Control Installation Rudder 65B04004 Control Installation Stabilizer Trim 65B04006 Control Installation Rudder Trim 65B04007 Control Installation Wing Flap 65B04016 Control Installation Speed Brakes Service Information: Boeing Reports D6-13592, "Structura l Repair Manual", (except for 747SP) is FAA-Approved. Boeing Reports D6-34024, "Structural Repair Manual", is FAA-Approved for the 747SP. Service