# TCDS A3WE: The Boeing Company - Type: Type certificate data sheet - Status: Current - Holder: The Boeing Company - Revision: 19 - Revised: February 20, 1991 - Product: Aircraft, Large Airplane - Certification basis: CAR 4b - Registered aircraft: 25, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/3e/91/3e9155b0beebf6749a27e1c6bbe7bfa84bf401e236fb7f257cdbb4878dc585e8 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5D48FC77A31B7F6985256722006B0C1C.0001 - Page: https://openairdocs.org/tcds/A3WE ## Models (6) As the data sheet lists them. - 727-100 Series - 727 Series - 727-200 Series - 727-100C Series - 727-200F Series - 727C Series ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 7 8 9 Rev. No. 19 19 19 19 19 19 19 19 19 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A3WE Revision 19 BOEING 727 Series 727-100 Series 727C Series 727-100C Series 727-200 Series 727-200F Series February 20, 1991 TYPE CERTIFICATE DATA SHEET A3WE This data sheet, which is part of Type Certificate No. A3WE, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder: The Boeing Company P.O. Box 3707 Seattle, Washington 98124 I. Model 727, 727-100 (approved December 24, 1963) and 727C and 727-100C (approved January 13, 1966) Transport Aircraft Engines 3 Pratt and Whitney JT8D-1, JT8D-1A, JT8D-1B, JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, JT8D-11, JT8D-15, or JT8D-17 Turbofans (see -11, -15, and -17 ratings under 727-200). (For engine intermix, see Note 9). Fuel See Note 5. Engine Ratings: JT8D-1, -1A, -1B, -7, -7A, -7B JT8D-9, -9A Takeoff static thrust, standard day, sea level conditions (5 min) lb. 14,000 14,500 Maximum continuous static thrust, standard day, sea level conditions lb. 12,600 12,600 For engine operating limits see TC 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 or AFM Appendices must be used for control of engine thrust. Airspeed limits: VMO/MMO - 390/0.9 (KEAS), Dual Mode 390/350/0.88 (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. Model Eligible Serial Numbers: 727-11 19242 727-14 18908-18912, 18990, 19398 727-17 20327, 20328, 20512, 20513 727-21 18992-18999, 19005-19007, 19035-19038, 19257-19262 727-21C 19134-19137 A3WE 2 I. Model 727, 727-100 and 727C and 727-100C (cont’d) Maximum Weights: (cont’d) Model Eligible Serial Numbers: 727-22 18293-18332, 18791, 18848, 18849, 18851-18857, 18859-18872, 19079-19088, 19140-19154 727-22C 19089-19103, 19191-19205, 19805, 19806, 19890-19895 727-23 18426-18450, 18900-18901, 19128, 19132, 19180-19184, 19385-19 390, 19428-19432, 20044-20046 727-24C 19524-19528 727-25 18252-18291, 18965-18974 727-25C 19298-19302, 19356-19360, 19717-19722, 19850-19858 727-27 19499-19501, 19534, 19535 727-27C 19109-19120, 19246, 19497, 19532, 19533 727-29 19400, 19401 727-29C 19402, 19403, 19987 727-30 18360-18371, 18933-18936 727-30C 19008-19012, 19310-19314, 19793 727-31 18569-18578, 18750-18755, 18902-18907, 19228, 20112-20115 727-31C 19229-19234 727-35 18811-18817, 18845-18847, 19165-19167, 19833-19835 727-41 20422-20425 727-44 18892-18896, 19318 727-44C 19319, 20475, 20476 727-46 18874-18879, 19279-19283, 20078 727-51 18797-18807, 18942-18944, 19121-19126 727-51C 18897-18899, 18945-18947, 19206, 19287-19290 727-59 19127, 19303, 19662, 19663 727-61 19176 727-62C 19244, 19245 727-63 19846 727-64 19255, 19256, 19427 727-76 18741, 18742, 18843, 19254, 20228, 20371 727-77 18743, 18744, 18844, 19253 727-77C 20278, 20370 727-78 18794-18796 727-81 18821-18823, 18919, 18920, 18951, 18952, 19557 727-82 19404-19406, 20489 727-82C 19597, 19968 727-86 19171, 19172, 19816, 19817 727-89 19138, 19139 727-90C 19169, 19170, 19728 727-92C 19173, 19174 727-95 18850, 18858, 19249-19252, 19595, 19596, 19836, 19837 727-108C 19503 727-109 19399, 19520 727-109C 20111 727-113C 19690, 20343 727-114 19815 727-116 19811, 19812, 20217 727-116C 19813, 19814 727-121C 19818, 19819 727-123 19838, 19839 727-134 19691, 19692 727-134C 20042 727-151C 19867, 19868 727-155C 19618, 19619 727-162 19243 727-171C 19859, 19860 727-172C 19665, 19666, 19807, 19808 727-173C 19504-19509 3 A3WE I. Model 727, 727-100 and 727C and 727-100C (cont’d) Maximum Weights: (cont’d) Model Eligible Serial Numbers: 727-180C 19873, 19874 727-185C 19826, 19827 727-191 19391-19395 727-193 19304, 19305, 19620 727-1A0 20279 727-1A7C 20143 727-1F8 20421 727-1H2 20533 727-1J1 20426 727-C3 20418-20420 Minimum crew When in the mixed passenger/cargo configuration, one flight attendant is required in the passenger compartment (review Case No. 5 dated July 17, 1963). Maximum passengers 119 129 under provisions of Exemption No. 255. 131 under provisions of Exemption No. 255 and if compliance with FAR 25.2 is shown. Maximum Baggage/Cargo: See appropriate Weight and Balance Control and Loading Manual. Fuel and Oil Capacities: See appropriate Weight and Balance Control and Loading Manual. Minimum Required Fuel: See appropriate FAA Approved Airplane Flight Manual. Maximum Operating Altitude 42,000 feet Datum All production stations coincide numerically with arms. Horizontal distance of datum to nose gear jack point is 303.2 inches. MAC 180.7 inches (L.E. of MAC is at 860.2 inches) Certification basis CAR 4b, dated December 31, 1953, Amendments 4b-1 through 4b-11 thereto: Special CAR SR-422B: Special Conditions listed in Attachment “A” of FAA letter to Boeing dated October 27, 1961, and FAA letter to Boeing dated June 12, 1963. Exemptions from CAR 4b: 727, 727-100, 727C and 727-100C : Exemption No. 255 - Exemption from CAR 4b.362(c)(1) - allows 131 passengers. 727 and 727-100: Exemption No. 1834 - Exemption from CAR 4b.356(b) - allow removal of aisle strap from 727 and 727-100 incorporating a Type I emergency exit on each side of the fuselage near the aft end of the passenger cabin and an inflatable evacuation slide at each side exit. 727C and 727-100C: Exemption No. 348 - Exemption from CAR 4b.362(c)(1) - allow 79 passengers with main deck cargo (one or two cargo pallets). Exemption No. 348 - Exemption from CAR 4b.362(c)(1) - allow 56 passengers with main deck (three or four cargo pallets). Other Information: See “Data Pertinent to All Models.” A3WE 4 II. Model 727-200 (approved November 29, 1967) Transport Aircraft Engines 3 Pratt and Whitney JT8D-1, JT8D-1A, JT8D-1B, JT8D-7, JT8D-7A, JT8D-7B, JT8D-9, JT8D-9A, JT8D-11, JT8D-15, JT8D-15A, JT8D-17, JT8D-17A, or JT8D-17R, JT8D-17AR turbofans. (For engine intermix, see Note 9) Fuel See Note 5. JATO: 6 Aerojet 15KS-1000-A1 thrust augmentation units, approved for use with Pratt and Whitney JT8D-11, JT8D-15, JT8D-15A, and JT8D-17, JT8D-17A turbofans with 15° flaps. Engine ratings JT8D-11 JT8D-15, -15A JT8D-17, -17A JT8D-17R*, -17AR Takeoff static thrust, standard day, sea level conditions (5 min.) lb. 15,000 15,500 16,000 17,400 Maximum continuous static thrust standard day, sea level conditions lb. 12,600 13,750 15,200 15,200 *A takeoff thrust setting limited to the alternate takeoff rating of 16,400 lbs. static thrust at sea level, flat rated to 77°F ambient temperature has been established for normal takeoff operation. When the automatic reset mechanism in the fuel control is utilized, operation to the alternate takeoff operating limits will prevent the engine from exceeding the takeoff rating operating limits when the reset mechanism is actuated. NOTE: For engine operating limitations see engine T.C. 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 or AFM Appendices must be used for control of engine thrust. Airspeed limits VMO/MMO Single mode 390/0.9 (KEAS) - Dual Mode for 191,000 lb. GW or less 390/350/.9(KEAS) - Greater than 191,000 lbs. GW 390/350/.88(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. Model Eligible Serial Numbers 727-208 22295 727-212 21347-21349, 21458-21460, 21945-21948 727-214 19683-19689, 20161-20169, 20366, 20367, 20678, 20679, 20875, 21512, 21513, 21691, 21692, 21958 727-217 21055, 21056 727-221 22535-22542 727-222 19537-19542, 19899-19915, 20037-20041, 21398-21425, 21557-21574, 21892-21921 727-223 19475-19495, 19700-19704, 20180-20193, 20984-20997, 21084-21090, 21369-21374, 21382-21391, 21519-21527, 22006-22015, 22459-22470 727-224 19510-19514, 19797-19804, 20243-20245, 20384-20388, 20463-20465, 20654-20668, 22448-22452 727-225 20144-20155, 20379-20383, 20415, 20416, 20441-20448, 20614-20628, 20823, 20824, 21288-21293, 21449-21453, 21578-21581, 21854-21861, 22432-22441, 22548-22557, 22559 727-227 20392-20394, 20608-20613, 20729-20738, 20772-20775, 20837-20840, 21041-21045, 21118, 21119, 21242-21249, 21363-21366, 21394, 21395, 21461-21466, 21488-21493, 21529-21532, 21669, 21670, 21996-22005, 22091, 22092 727-228 19543-19546, 19861-19865, 22075, 20202-20204, 20409-20411, 20470, 20538-20540, 22081-22085, 22287-22290 5 A3WE II. Model 727-200 (cont’d) Maximum weights (cont’d) 727-230 20430, 20431, 20525, 20526, 20560, 20673-20677, 20757, 20788-20792, 20899-20906, 20918, 21113, 21114, 21442, 21618-21623 727-231 19558-19565, 19828-19832, 20047-20055, 20098, 20099, 20232-20234, 2030 6-20310, 20460-20462, 20490-20491, 20843-20859, 21628-21634, 21967-21969, 21983-21989 727-232 20634-20647, 20743-20756, 20860-20867, 21018-21020, 21060-21062, 21074-21077, 21142-21153, 21222, 21223, 21232, 21233, 21256-21259, 21271-21274, 21303-21315, 21430-21433, 21469-21472, 21582-21587, 21702, 21703, 21813, 21814, 22045-22049, 22073, 22076, 22385-22387, 22391, 22392, 22493, 22494, 22677 727-233 20932-20942, 21100-21102, 21624-21626, 21671-21675, 22035-22042, 22345-22350, 22621-22623 727-235 19450-19474 727-243 21264-21270, 21661-21664, 22052, 22053, 22165-22168, 22702 727-247 20263-20268, 20579-20581, 20648, 20649, 20868-20874, 21057-21059, 21327-21331, 21392, 21393, 21481-21485, 21697-21701, 22108-22112, 22532-22534 727-251 19970-19985, 20289-20296, 21154-21161, 21322-21325, 21375-21379, 21503-21506, 21788, 21789, 22152-22155, 22543, 22544 727-254 20250-20252, 20437, 20438 727-256 20592-20607, 20811-20821, 20974, 20975, 21609-21611, 21777-21781 727-259 22474-22476 727-260 21978, 21979, 22759 727-264 20432-20434, 20709, 20710, 20780, 20787, 20894-20896, 21071, 21072, 21577, 21617, 21637, 21638, 21836-21838, 22156-22158, 22409-22414, 22661-22664, 22676, 22982-22984, 23014 727-269 22359-22361, 22763 727-270 21197-21199, 22261, 22262, 23052 727-276 20552-20555, 20950, 20951, 21171, 21479, 21646, 21696, 22017, 22069 727-277 20548-20551, 20978, 20979, 21178, 21480, 21647, 21695, 22016, 22068, 22641-22644 727-281 20285, 20286, 20435, 20436, 20466-20469, 2 0509, 20510, 20568-20573, 20724-20728, 20876-20878, 21455, 21456, 21474 727-282 20972, 20973, 21949, 21950, 22430 727-284 19536, 20003-20006, 20201 727-286 20945-20947, 21078, 21079 727-287 21688-21690, 22603-22606 727-290 21510, 21511, 22146, 22147 727-291 19991-19995 727-294 21203-21205, 22043, 22044 727-295 19444-19449, 20139-20141, 20248, 20249 727-2A1 21341-21346, 21600, 21601 727-2A7 20240, 20241 727-2B6 20304, 20471, 20705, 21068, 21297-21299, 22377 727-2B7 20302, 20303, 21953, 21954, 22162-22164 727-2D3 20885, 20886, 21021, 22268-22271 727-2D4 21849, 21850 727-2D6 20472, 20473, 20955, 21053, 21210, 21284, 22372-22375, 22765 727-2F2 20980-20983, 21260, 21603, 22992, 22993, 22998, 22999 727-2F9 21426, 21427 727-2H3 20545, 20739, 20822, 20948, 21179, 21234, 21235, 21318-21320 727-2H9 20930, 20931, 21037-21039, 22393, 22394, 22665, 22666 727-2J0 21105-21108 727-2J1 21036 727-2J4 20764-20766, 21438, 21676, 22079, 22080, 22574 727-2J7 20706, 20707, 20879, 208 80 727-2K3 21082, 21494, 21495, 22770 727-2K5 21851-21853 727-2L4 21010 727-2L5 21050-21052, 21229, 21230, 21332, 21333, 21539, 21540 727-2L8 21040, 21080 727-2M1 21091 A3WE 6 II. Model 727-200 (cont’d) Maximum weights (cont’d) 727-2M7 21200-21202, 21457, 21502, 21655, 21656, 21741, 21742, 21823, 21824, 21951, 21952 727-2N6 22825 727-2N8 21842, 21844-21847 727-2P1 21595 727-2Q4 22424, 22425 727-2Q6 21971, 21972 727-2Q8 21608, 21826 727-2Q9 21930, 21931 727-2R1 21636 727-2S7 22019-22021, 22344, 22490-22492 727-2T3 22078 727-2U5 22362 727-2X3 22608, 22609 727-2X8 22687 727-2Y4 22968 Maximum passengers: 170 189 if compliance with FAR 25.2(b), (c), and (d) is shown. Maximum baggage/cargo: See appropriate Weight and Balance Control and Loading Manual. Fuel and oil capacities: See appropriate Weight and Balance Control and Loading Manual (for fuel and oil capacities, including undumpable and unusable amounts). Minimum required fuel: See appropriate FAA Approved Airplane Flight Manual. Maximum operating altitude: 42,000 feet Datum: See appropriate Weight and Balance Control and Loading Manual. Horizontal distance of datum to nose gear jack point is 183.2 inches. MAC: 180.7 inches (L.E. of MAC is 860.2 inches). Certification basis CAR 4b, dated December 31, 1953, Amendments 4b-1 through 4b-11 thereto: Special CAR SR-422B; Special Conditions set forth in FAA letter to Boeing dated February 2, 1967, as revised by FAA letters to Boeing dated June 20, 1967, September 1 and 13, 1967; FAR Amendment 25-15; FAR Amendment 36-2. Special Condition 25-64-NW-2 issued August 6, 1975, and Amendment 1 thereto issued November 16, 1976, applies to Model 727-200 series airplanes equipped with an operative automatic takeoff thrust control system (called by Boeing an “Automatic Performance Reserve” (APR) system) issued an original airworthiness certificate before December 3, 1980. Special Condition 25-64-NW-2, Amendments 2 and 3 thereon, issued 5/18/79, and 12/12/79, respectively, apply to Boeing Model 727-200 series airplanes equipped with an operative automatic takeoff thrust control (ATTCS) system and issued an original airworthiness certificate on and after 12/3/80. Exemptions from CAR 4b: Exemption 1834 - Exemption from CAR 4b.356(b) - allow removal of aisle strap from 727-200 incorporating a Type I emergency exit on each side of the fuselage near the aft end of the passenger cabin and an inflatable evacuation slide at each such exit. Other information: See “Data Pertinent to All Models.” 7 A3WE III. Model 727-200F (approved June 22, 1983) Transport Aircraft Engines 3 Pratt and Whitney JT8D-17A turbofans. Fuel See Note 5. JATO None Engine ratings: JT8D-17A Takeoff static thrust, standard day, sea level 16,000 conditions (5 min.) lb. Maximum continuous static thrust standard day, sea level condition lb. 15,200 NOTE: For engine operating limitations see engine TC 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 or AFM Appendices must be used for control of engine thrust. Airspeed limits VMO/MMO Single mode 350/0.88 (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. Model Eligible Serial Numbers: 727-2S2F 22924-22938 Maximum passengers None Maximum baggage/cargo See appropriate Weight and Balance Control and Loading Manual. Fuel and oil capacities See appropriate Weight and Balance Control and Loading Manual (for fuel and oil capacities, including undumpable and unusable amounts). Minimum required fuel See appropriate FAA Approved Airplane Flight Manual. Maximum operating altitude 42,000 feet Datum See appropriate Weight and Balance Control and Loading Manual. Horizontal distance of datum to nose gear jack point is 183.2 inches. MAC 180.7 inches (L.E. of MAC is 860.2 inches.) Certification basis CAR 4b, dated December 31, 1953, Amendments 4b-1 through 4b-11 thereto: Special CAR SR-422B; Special Conditions set forth in FAA letter to Boeing dated February 2, 1967, as revised by FAA letters to Boeing dated June 20, 1967, September 1 and 13, 1967; FAR Amendment 25-15; FAR 25.723 (Amendment 25-46); FAR 36.2 (Amendment 36-10). Special Condition 25-64-NW-2, Amendments 2 and 3 thereon, issued 5/18/79, and 12/12/79, respectively, apply to Boeing Model 727-200 series airplanes equipped with an operative automatic takeoff thrust control (ATTCS) system and issued an original airworthiness certificate on and after 12/3/80. Equivalent Safety Findings exist with respect to CAR 4b.651(d)(3)(i) and CAR 4b.651(d)(3)(iii). Other information See “Data Pertinent to All Models.” A3WE 8 Data Pertinent to All Models Minimum crew for all flights Three (3) pilot, copilot, and flight engineer Leveling means A plumb bob attachment and leveling provision scale are provided in the left wheel well on 727/727-100 and 727C/727-100C airplanes, and in the right wheel well on 727-200 airplanes. Control surface movements To insure proper operation of 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 in accordance with the following FAA-approved data: Boeing Drawing Numbers 727-200 727/727-100 and 727C/727-100C 65-56801 65-20801 Control Installation Aileron and Spoiler 65-56802 65-20802 Control Installation Elevator 65-56803 65-20803 Control Installation Rudder 65-56804 65-20804 Control Installation Stabilizer Trim 65-56805 65-20805 Control Installation Aileron Trim 65-56806 65-20806 Control Installation Rudder Trim 65-56808 65-20808 Control Installation Wing Flap 65-56816 65-20816 Control Installation Speed Flap Certification basis See Section I or Section II, as appropriate. Compliance with the following optional requirements has been established: CAR 4b.361, “Ditching Provision” CAR 4b.640, “Ice Protection” Production basis Production Certificate Number 700. 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 included in the type design data. See appropriate Weight and Balance Manuals and Note 8 for replacement passenger seats. Service information Boeing Report D6-4062, “Structural Repair Manual” is FAA-approved. Service bulletins and other service information when FAA-approved, will carry a statement to that effect. NOTE 1. Current weight and balance document, including list of equipment included in certificated weight empty and loading instructions, must be in each aircraft at the time of original certification and at all times thereafter, except in the case of operators having an approved weight control system. NOTE 2. The aircraft must be operated in accordance with the FAA Approved Airplane Flight Manual. NOTE 3. Reserved. NOTE 4. (a) The fuel controls approved for use with these engines are Hamilton Standard Models JFC 60-1 (JT8D-1, -1A, -7, -7A, and -7B), JFC 60-2 (JT8D-9, -11, -15, -15A, and -17, -17A), and JFC 60-3 (JT8D-17R, 17AR). (b) The anti-icing system airflow regulating valve approved for use with this engine is Pratt & Whitney Part No. 480888. P&WA Orifice Plate Part No. 528226 may be used in lieu of the valve. NOTE 5. (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. (b) Phillips 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. 9 A3WE NOTE 6. A list of the FAA-approved Interior Arrangement Drawings for all models of the Boeing 727 aircraft is contained in Boeing Document D6-6903. NOTE 7. Reserved. NOTE 8. The airplane design vertical load factors exceed TSO C-39 requirements at all fuselage stations for 727, 727-100, 727C, and 727-100C models and aft fuselage station 950D for 727-200 models: therefore, replacement passenger seats must be evaluated for compliance with CAR 4b.358(c) accordingly. NOTE 9. Combinations of engines which can be intermixed and their respective limitations are covered in the FAA Approved Flight Manuals or AFM Appendices. NOTE 10. Noise: Model 727, 727-100, 727C, 727-100C, 727-200 and 727-200F . Airplanes of these models that have not had any flight time before December 1, 1973, and are issued an original U.S. Standard Airworthiness Certificate after December 1, 1973, must show compliance with FAR Part 36. Configurations that meet the noise requirements are shown in Appendix 33 of the FAA Approved Airplane Flight Manual for the Model 727, 727-100, 727C, and 727-100C, and in Appendix 12 of the FAA Approved Flight Manual for the Model 727-200 and 727-200F. Model 727-200. Noise characteristics, approved type design configurations, including required acoustical treatment and certification status of Model 727-200 airplanes operated at brake release gross weight from 172,500 pounds to a maximum of 203,100 pounds approved before December 1, 1973, are shown in the FAA Approved Model 727-200 Airplane Flight Manual. NOTE 11. 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 D6-9825 titles “Service Bulletin 727.” 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. .....END..... ``` ## ADs (314, first 50, in force first) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. 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Effective Jun 22, 2020 - [AD 2019-23-04](https://openairdocs.org/ad/2019-23-04): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Feb 4, 2020 - [AD 2019-24-18](https://openairdocs.org/ad/2019-24-18): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 11 more. Effective Feb 3, 2020 - [AD 2018-25-15](https://openairdocs.org/ad/2018-25-15): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jan 22, 2019 - [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018 - [AD 2018-20-05](https://openairdocs.org/ad/2018-20-05): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 2 more. Effective Nov 2, 2018 - [AD 2018-17-20](https://openairdocs.org/ad/2018-17-20): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 4, 2018 - [AD 2017-19-02](https://openairdocs.org/ad/2017-19-02): Doors · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 19, 2017 - [AD 2016-19-16](https://openairdocs.org/ad/2016-19-16): Doors · Boeing 707-300 Series, 707-300B Series, 707-300C Series and 3 more. Effective Jan 9, 2017 - [AD 2014-21-09](https://openairdocs.org/ad/2014-21-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 3, 2014 - [AD 2014-16-09](https://openairdocs.org/ad/2014-16-09): Oxygen · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 16 more. Effective Sep 23, 2014 - [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014 - [AD 2014-12-10](https://openairdocs.org/ad/2014-12-10): Fuselage · Boeing 727-100 Series. Effective Jul 28, 2014 - [AD 2014-04-09](https://openairdocs.org/ad/2014-04-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 2, 2014 - [AD 2014-05-14](https://openairdocs.org/ad/2014-05-14): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 1, 2014 - [AD 2014-03-21](https://openairdocs.org/ad/2014-03-21): Fuselage · Boeing 727-200 Series and 727-200F Series. Effective Mar 31, 2014 - [AD 2013-24-15](https://openairdocs.org/ad/2013-24-15): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jan 8, 2014 - [AD 2013-21-07](https://openairdocs.org/ad/2013-21-07): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 5, 2013 - [AD 2013-22-03](https://openairdocs.org/ad/2013-22-03): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 5, 2013 - [AD 2013-19-08](https://openairdocs.org/ad/2013-19-08): JASC Code 3418, Stall Warning System · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 18 more. Effective Nov 6, 2013 - [AD 2013-16-17](https://openairdocs.org/ad/2013-16-17): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 27, 2013 - [AD 2013-15-11](https://openairdocs.org/ad/2013-15-11): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 20, 2013 - [AD 2013-15-15](https://openairdocs.org/ad/2013-15-15): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 20, 2013 - [AD 2013-14-02](https://openairdocs.org/ad/2013-14-02): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 26, 2013 - [AD 2013-14-03](https://openairdocs.org/ad/2013-14-03): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 26, 2013 - [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011 - [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011 - [AD 2011-12-05](https://openairdocs.org/ad/2011-12-05): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jul 15, 2011 - [AD 2011-02-05](https://openairdocs.org/ad/2011-02-05): Fuselage. · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 1, 2011 - [AD 2011-01-05](https://openairdocs.org/ad/2011-01-05): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Feb 14, 2011 - [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011 - [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010 - [AD 2008-04-10 R1](https://openairdocs.org/ad/2008-04-10-R1): Fuel tank · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 30, 2009 - [AD 2009-20-08](https://openairdocs.org/ad/2009-20-08): Fuel system · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Nov 5, 2009 - [AD 2009-20-03](https://openairdocs.org/ad/2009-20-03): Kickboard beam · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Nov 3, 2009 - [AD 2009-20-01](https://openairdocs.org/ad/2009-20-01): Auxiliary fuel tanks · Boeing 727-200 Series with STC SA3449NM. Effective Oct 26, 2009 - [AD 2009-06-10](https://openairdocs.org/ad/2009-06-10): Lower skin and the upper fastener row of the upper skin · Boeing 727-100 Series and 727-200 Series. Effective Apr 28, 2009 - [AD 2009-05-03](https://openairdocs.org/ad/2009-05-03): Ground fault interrupter (GFI) · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Apr 3, 2009 - [AD 2008-22-12](https://openairdocs.org/ad/2008-22-12): Elevator side fitting/hinge fitting joint · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 17, 2008 - [AD 2008-23-09](https://openairdocs.org/ad/2008-23-09): Insulation blanket · Boeing 727-200 Series, 727-200F Series, 737-200 Series and 18 more. Effective Dec 15, 2008 - [AD 2008-22-01](https://openairdocs.org/ad/2008-22-01): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727 Series and 17 more. Effective Nov 26, 2008 - [AD 2008-17-14](https://openairdocs.org/ad/2008-17-14): Elevator rear spar · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 2, 2008 - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [AD 2008-12-03](https://openairdocs.org/ad/2008-12-03): Auxiliary fuel tanks · Airbus BAC 1-11 400 Series, 707-100 Long Body, 707-100B Long Body and 15 more. Effective Jul 9, 2008 All 314: https://openairdocs.org/tcds/A3WE/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Boeing 727-223](https://openairdocs.org/model/boeing-727-223): 9 aircraft (registry code 1384074) - [Boeing 727-227](https://openairdocs.org/model/boeing-727-227): 4 aircraft (registry code 1384078) - [Boeing 727-225](https://openairdocs.org/model/boeing-727-225): 2 aircraft (registry code 1384077) - [Boeing 727-200](https://openairdocs.org/model/boeing-727-200): 1 aircraft (registry code 138407E) - [Boeing 727-200F](https://openairdocs.org/model/boeing-727-200f): 1 aircraft (registry code 1384060) - [Boeing 727-212](https://openairdocs.org/model/boeing-727-212): 1 aircraft (registry code 138407G) - [Boeing 727-230](https://openairdocs.org/model/boeing-727-230): 1 aircraft (registry code 1384080) - [Boeing 727-232](https://openairdocs.org/model/boeing-727-232): 1 aircraft (registry code 1384082) - [Boeing 727-243](https://openairdocs.org/model/boeing-727-243): 1 aircraft (registry code 138408D) - [Boeing 727-247](https://openairdocs.org/model/boeing-727-247): 1 aircraft (registry code 138408F) - [Boeing 727-264](https://openairdocs.org/model/boeing-727-264): 1 aircraft (registry code 138408M) - [Boeing 727-277](https://openairdocs.org/model/boeing-727-277): 1 aircraft (registry code 138408S) - [Boeing 727-281](https://openairdocs.org/model/boeing-727-281): 1 aircraft (registry code 138408N) - [Boeing 727](https://openairdocs.org/model/boeing-727): 0 aircraft (registry code 1384001) - [Boeing 727-100](https://openairdocs.org/model/boeing-727-100): 0 aircraft (registry code 1384036) - [Boeing 727-100C](https://openairdocs.org/model/boeing-727-100c): 0 aircraft (registry code 1384037) - [Boeing 727-108C](https://openairdocs.org/model/boeing-727-108c): 0 aircraft (registry code 1384039) - [Boeing 727-109](https://openairdocs.org/model/boeing-727-109): 0 aircraft (registry code 1384033) - [Boeing 727-109C](https://openairdocs.org/model/boeing-727-109c): 0 aircraft (registry code 1384034) - [Boeing 727-113C](https://openairdocs.org/model/boeing-727-113c): 0 aircraft (registry code 1384038) - [Boeing 727-114](https://openairdocs.org/model/boeing-727-114): 0 aircraft (registry code 1384040) - [Boeing 727-116](https://openairdocs.org/model/boeing-727-116): 0 aircraft (registry code 1384043) - [Boeing 727-116C](https://openairdocs.org/model/boeing-727-116c): 0 aircraft (registry code 1384046) - [Boeing 727-121C](https://openairdocs.org/model/boeing-727-121c): 0 aircraft (registry code 138404I) - [Boeing 727-123](https://openairdocs.org/model/boeing-727-123): 0 aircraft (registry code 138404G) - [Boeing 727-134](https://openairdocs.org/model/boeing-727-134): 0 aircraft (registry code 1384041) - [Boeing 727-134C](https://openairdocs.org/model/boeing-727-134c): 0 aircraft (registry code 138404H) - [Boeing 727-151C](https://openairdocs.org/model/boeing-727-151c): 0 aircraft (registry code 138404V) - [Boeing 727-155C](https://openairdocs.org/model/boeing-727-155c): 0 aircraft (registry code 138404Z) - [Boeing 727-162](https://openairdocs.org/model/boeing-727-162): 0 aircraft (registry code 1384056) - [Boeing 727-172C](https://openairdocs.org/model/boeing-727-172c): 0 aircraft (registry code 1384058) - [Boeing 727-173C](https://openairdocs.org/model/boeing-727-173c): 0 aircraft (registry code 1384059) - [Boeing 727-180C](https://openairdocs.org/model/boeing-727-180c): 0 aircraft (registry code 138406G) - [Boeing 727-185C](https://openairdocs.org/model/boeing-727-185c): 0 aircraft (registry code 138406N) - [Boeing 727-191](https://openairdocs.org/model/boeing-727-191): 0 aircraft (registry code 1384063) - [Boeing 727-193](https://openairdocs.org/model/boeing-727-193): 0 aircraft (registry code 138406Z) - [Boeing 727-208](https://openairdocs.org/model/boeing-727-208): 0 aircraft (registry code 1384070) - [Boeing 727-214](https://openairdocs.org/model/boeing-727-214): 0 aircraft (registry code 138407R) - [Boeing 727-217](https://openairdocs.org/model/boeing-727-217): 0 aircraft (registry code 1384061) - [Boeing 727-221](https://openairdocs.org/model/boeing-727-221): 0 aircraft (registry code 1384071) - [Boeing 727-222](https://openairdocs.org/model/boeing-727-222): 0 aircraft (registry code 1384073) - [Boeing 727-224](https://openairdocs.org/model/boeing-727-224): 0 aircraft (registry code 1384076) - [Boeing 727-228](https://openairdocs.org/model/boeing-727-228): 0 aircraft (registry code 1384083) - [Boeing 727-231](https://openairdocs.org/model/boeing-727-231): 0 aircraft (registry code 1384079) - [Boeing 727-233](https://openairdocs.org/model/boeing-727-233): 0 aircraft (registry code 138408A) - [Boeing 727-235](https://openairdocs.org/model/boeing-727-235): 0 aircraft (registry code 138408B) - [Boeing 727-251](https://openairdocs.org/model/boeing-727-251): 0 aircraft (registry code 138408H) - [Boeing 727-254](https://openairdocs.org/model/boeing-727-254): 0 aircraft (registry code 138408L) - [Boeing 727-256](https://openairdocs.org/model/boeing-727-256): 0 aircraft (registry code 1384062) - [Boeing 727-259](https://openairdocs.org/model/boeing-727-259): 0 aircraft (registry code 138408J) All 63: https://openairdocs.org/tcds/A3WE/aircraft.md ## STCs approved under this data sheet (1,246, first 50) - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems - [STC ST12412CH](https://openairdocs.org/stc/ST12412CH): Installation of the Dual FreeFlight Systems RA-6500 Radio Altimeter. IFL Group Inc. - [STC ST00736SE](https://openairdocs.org/stc/ST00736SE): Installation of new flight crew oxygen masks and holders. B/E Aerospace, Inc. - FSI - [STC ST00020AT](https://openairdocs.org/stc/ST00020AT): Installation of expanded parameters flight data recorder.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST02992AT-D](https://openairdocs.org/stc/ST02992AT-D): Installation of Rockwell Collins WXR-2100 Multiscan Weather Radar. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON LLC d/b/a MASS Systems - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc. - [STC ST02771SE](https://openairdocs.org/stc/ST02771SE): Installation of Improved Radio Altimeter System. AeroMech Incorporated - [STC ST02646AT](https://openairdocs.org/stc/ST02646AT): Installation of an AudioVideo In-Flight Entertainment System (IFE) per ARC Avionics Master Drawing List (MDL) ARC-VIDE-001-MDL latest FAA approved revision.. ARC145 LLC - [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net.. Satco Inc. - [STC ST03450AT](https://openairdocs.org/stc/ST03450AT): Installation of a horse stall system. Gregory Jackson - [STC SA2348WE](https://openairdocs.org/stc/SA2348WE): Installation of emblem lights.. The Boeing Company - [STC ST09113AC](https://openairdocs.org/stc/ST09113AC): Installation of Tail Floodlights on Boeing 727 Engine Pylons. The Boeing Company - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC SA1026NW](https://openairdocs.org/stc/SA1026NW): Installation of centerline life raft stowage compartments.. Safran Cabin Inc. - [STC SA1045NW](https://openairdocs.org/stc/SA1045NW): Installation of Spacemaker I-A interior kit.. Safran Cabin Inc. - [STC SA1078NW](https://openairdocs.org/stc/SA1078NW): Installation of C&D coat closet, L.H. forward unit.. Safran Cabin Inc. - [STC SA1086NW](https://openairdocs.org/stc/SA1086NW): Installation of C&D coat closet, R.H. forward unit.. Safran Cabin Inc. - [STC SA1174NW](https://openairdocs.org/stc/SA1174NW): Installation of a windscreen.. Safran Cabin Inc. - [STC SA1305NM](https://openairdocs.org/stc/SA1305NM): Installation of coat closet, L. H. forward unit.. Safran Cabin Inc. - [STC SA1306NM](https://openairdocs.org/stc/SA1306NM): Installation of coat closet, R. H. forward unit. (727-232). Safran Cabin Inc. - [STC SA1370NM](https://openairdocs.org/stc/SA1370NM): Installation of class divider-closet units and curtain header. (727-235). C & D Zodiac Inc. - [STC SA1419NM](https://openairdocs.org/stc/SA1419NM): Installation of overhead life raft stowage containers.. Safran Cabin Inc. - [STC SA1442NM](https://openairdocs.org/stc/SA1442NM): Installation of Spacemaker interior kit. Safran Cabin Inc. - [STC SA1662NM](https://openairdocs.org/stc/SA1662NM): Installation of overhead stowage Quikbin retrofit kits.. Safran Cabin Inc. - [STC SA2474NM](https://openairdocs.org/stc/SA2474NM): Installation of 3 coat closets and one class divider.. Safran Cabin Inc. - [STC SA2480NM](https://openairdocs.org/stc/SA2480NM): Installation of divider assembly, closet assembly, cabinet assembly, coatroom assembly.. Safran Cabin Inc. - [STC SA3111NM](https://openairdocs.org/stc/SA3111NM): Installation of C&D Plastics closet, P/N 1891001-103; cabinet, P/N1871001-501; class divider, P/N 1851001-102.. Safran Cabin Inc. - [STC SA3299NM](https://openairdocs.org/stc/SA3299NM): Installation of an overhead life raft stowage compartment kit.. Safran Cabin Inc. - [STC SA3457NM](https://openairdocs.org/stc/SA3457NM): Installation of cabin divider.. Safran Cabin Inc. - [STC SA469NW](https://openairdocs.org/stc/SA469NW): Installation of coat closet unit.. Safran Cabin Inc. - [STC SA5169NM](https://openairdocs.org/stc/SA5169NM): Installation of Aerobin interior modification kits.. Safran Cabin Inc. - [STC SA5172NM](https://openairdocs.org/stc/SA5172NM): Installation of modular lavatory components.. Safran Cabin Inc. - [STC SA547NW](https://openairdocs.org/stc/SA547NW): Installation of Mark I interior conversion kit. Safran Cabin Inc. - [STC SA6051NM](https://openairdocs.org/stc/SA6051NM): Installation of Galley, G6A.. Safran Cabin Inc. - [STC SA816NW](https://openairdocs.org/stc/SA816NW): Installation of spacemaker interior modification kit.. Safran Cabin Inc. - [STC ST00147LA](https://openairdocs.org/stc/ST00147LA): Installation of closet and curtain header.. Safran Cabin Inc. - [STC ST00577SE](https://openairdocs.org/stc/ST00577SE): Installation of SpaceLine Interior Kits. Safran Cabin Inc. - [STC ST01437LA](https://openairdocs.org/stc/ST01437LA): Installation of a reinforced cockpit door.. Safran Cabin Inc. - [STC ST00556CH](https://openairdocs.org/stc/ST00556CH): Installation of a single or dual Honeywell/Trimble HT9100 Global Navigation System.. Amphenol Cable and Interconnect Technologies Inc. - [STC SA3141NM](https://openairdocs.org/stc/SA3141NM): Installation of floor proximity emergency escape path. Bruce Aerospace Inc. - [STC SA2932SO](https://openairdocs.org/stc/SA2932SO): Installation of a Fairchild or Sundstrand Digital Flight Data Recorder. Acron Aviation Inc. - [STC ST00771AT](https://openairdocs.org/stc/ST00771AT): Installation of expanded parameters Digital Flight Data Recorder from 6 parameters to 24 parameters. L3 Communications/Aviation Recorders - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc. - [STC ST01271CH](https://openairdocs.org/stc/ST01271CH): Installation of Automatic Dependent Surveillance-Broadcast (ADS-B) Provisions and a single Honeywell Mode-S transponder.. Amphenol Cable and Interconnect Technologies, Inc. - [STC ST04515AT](https://openairdocs.org/stc/ST04515AT): Installation of Auxiliary Fuel Tank Ignition Mitigation Reticulated Polyurethane Foam in Boeing 727-223 Series. AerSale Inc. - [STC ST01395LA](https://openairdocs.org/stc/ST01395LA): Approved for model 727-100, serial number 19860 and 20279; for model 727-200, serial number 21082, 21494, and 21495. Installation of BAE Systems (formerly Canadian Marconi) Dual CMA-900 Flight Management System.. Aero Technik Inc. - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC All 1,246: https://openairdocs.org/tcds/A3WE/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.