# Boeing 727-260 - Type: Aircraft model (FAA registry) - Registry code: 138408K - Manufacturer (registry): BOEING - Model: 727-260 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-fan - Seats: 134 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Holder: The Boeing Company - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-260 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026 - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2022-25-01](https://openairdocs.org/ad/2022-25-01): Wings · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 11 more. Effective Feb 16, 2023 - [AD 2021-03-09](https://openairdocs.org/ad/2021-03-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 31, 2021 - [AD 2020-06-19](https://openairdocs.org/ad/2020-06-19): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. 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 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 2014-04-09](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 2013-22-03](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 2013-21-07](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 2013-19-08](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 2013-15-15](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 2013-15-11](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 2013-14-03](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 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 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 - [AD 2008-11-09](https://openairdocs.org/ad/2008-11-09): Flight deck windows · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jul 3, 2008 - [AD 2008-08-02](https://openairdocs.org/ad/2008-08-02): Main landing gear (MLG) · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 19, 2008 Historical (superseded or no longer in force): - [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022 - [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013 - [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009 - [AD 2008-04-10](https://openairdocs.org/ad/2008-04-10) (historical): Fuel tank systems · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 28, 2008 - [AD 2007-11-08](https://openairdocs.org/ad/2007-11-08) (historical): Boost pump dry bay inspection · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jun 6, 2007 - [AD 2005-14-07](https://openairdocs.org/ad/2005-14-07) (historical): Carriage attach fittings on the foreflaps · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 15, 2005 - [AD 2001-24-02](https://openairdocs.org/ad/2001-24-02) (historical): Shoulder Restraint Harness Attachment · Boeing 707-100 Long Body, 707-100B Long Body, 707-300 Series (all) and 20 more. Effective Jan 4, 2002 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 - [AD 95-19-08](https://openairdocs.org/ad/95-19-08) (historical): Nose Cowl · Pratt and Whitney JT8D-217A, -217C, and -219 engines, related… (Rohr STC SA4363NM). Effective Oct 20, 1995 - [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995 - [AD 86-17-05 R1](https://openairdocs.org/ad/86-17-05-R1) (historical): Frame - Cargo Door Cutout · Boeing 727-200 Series. Effective Sep 3, 1987 All 279: https://openairdocs.org/model/boeing-727-260/ads.md ## Information bulletins (advisory) (7) - [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019 - [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014 - [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014 - [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010 - [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008 - [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006 - [SAIB NM-06-56](https://openairdocs.org/saib/NM-06-56): . Issued Jul 19, 2006 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20000321002159I](https://openairdocs.org/incident/20000321002159I), Mar 21, 2000: Boeing 727260 (N901PG), Pittsburgh, PA. (-23) Privacy data ommited. Incident no: IEA0300076. On March 21, 2000, at 0825E, a Boeing 727, s/n 21978, operating as (S84A) sky trek international airlines,… ## Service difficulty reports (70, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA150506005](https://openairdocs.org/sdr/CA150506005), May 5, 2015: ROLLER CAM. SHEARED. (CAN) DURING DAILY MAINTENANCE, THE AFT LOWER ROLLER CAM ON THE MAIN ENTRANCE DOOR WAS FOUND SHEARED OFF. THE ROLLER CAM WAS REPLACED IAW THE AMM AND FUNCTION C - [SDR CA150505008](https://openairdocs.org/sdr/CA150505008), Apr 21, 2015: ROLLER CAM. SHEARED. (CAN) WHILE CLOSING MAIN ENTRANCE DOOR, THE UPPER AFT CRANK ROLLER CAM SHAFT SHEARED. THE SHEARED CRANK ROLLER CAM WAS REPLACED AND CHECKED IAW THE AMM. THE ACF - [SDR CA150224030](https://openairdocs.org/sdr/CA150224030), Feb 23, 2015: MOUNT. MISALIGNED. (CAN) DURING ROUTINE MAINTENANCE INSPECTION THE NR 2 ENGINE RT FORWARD ISOLATOR MOUNT ALIGNMENT MARKS WERE FOUND MISALIGNED AND BONDING STRAP SHEARED. - [SDR CA120817009](https://openairdocs.org/sdr/CA120817009), Jul 31, 2012: SLIDING WINDOW. CRACKED. (CAN) R2 WINDOW OUTER PANE FAILED IN CRUISE, ACFT LANDED WITHOUT INCIDENT MAINTENANCE REPLACED WINDOW ASSY. - [SDR CA120112007](https://openairdocs.org/sdr/CA120112007), Jan 4, 2012: DUCT. CRACKED. (CAN) ON DECENT CREW OBSERVED NR 2 ENGINE FIRE WARNING INDICATION. COMPLETED FIRE DRILL, FIRE LIGHT STAYED ON, FIRE BOTTLE DISCHARGED. DECLARED EMERGENCY, LANDE - [SDR CA111212015](https://openairdocs.org/sdr/CA111212015), Dec 8, 2011: MODULE. BYPASSING. (CAN) DURING TAXI WHEN FLAPS EXTENDED HYD A SYS PRESS WENT TO 1500 PSI & BOTH A SYS LOW PRESS LIGHTS CAME ON. UPON REMOVAL OF RUDDER MODULE FOUND TEFLON BACK UP - [SDR CA091022004](https://openairdocs.org/sdr/CA091022004), Oct 20, 2009: WINDSHIELD. CRACKED. (CAN) DURING CRUISE AT FL320, THE CAPTAINS L1 WINDOW OUTER PANE CRACKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND THE WINDOW WAS REPLACED BY MAINTENANCE - [SDR CA090526008](https://openairdocs.org/sdr/CA090526008), Mar 3, 2009: ACTUATOR. CORRODED. (CAN) UNIT REMOVED FOR SCHEDULED OVERHAUL. UPON DISASSEMBLY, INTERNAL COMPONENTS BADLY CORRODED AND CONTAMINATED WITH WATER. UNIT SCRAPPED. THERE WERE NO INFLIG - [SDR CA080905003](https://openairdocs.org/sdr/CA080905003), Sep 3, 2008: CONTROLLER. MALFUNCTIONED. (CAN) AT FL300, TOP OF DESCENT, AS THRUST REDUCTION COMMENCED, LARGE BANG WAS EXPERIENCED BY THE FLIGHT CREW WITH FLUCTUATIONS IN NR 2 ENGINE PARAMETERS. ENGINE - [SDR CA080423004](https://openairdocs.org/sdr/CA080423004), Apr 16, 2008: WINDSCREEN. BURNED. (CAN) AFTER COCKPIT SETUP SMOKE AND FLAME WAS OBSERVED BY THE FLIGHT CREW FROM THE TOP LT CORNER OF THE R1 WINDOW. WHEN THE R1 WINDOW HEAT WAS SELECTED OFF THE - [SDR CA070911012](https://openairdocs.org/sdr/CA070911012), Sep 5, 2007: STUD. DISLODGED. (CAN) DURING CRUISE, THE NR 2 OIL QUANTITY SLOWLY DECREASED TO ZERO. WHEN THE OIL QUANTITY WENT BELOW THE GREEN ARC THE FLIGHT CREW SHUTDOWN THE ENGINE USING TH - [SDR CA070531003](https://openairdocs.org/sdr/CA070531003), May 30, 2007: PITOT SYSTEM. OBSTRUCTED. (CAN) THE AIRCRAFT BEGAN THE TAKEOFF ROLL WHEN THE FLIGHT CREW NOTICED A LAG IN THE FIRST OFFICERS AIR SPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAF - [SDR CA070518005](https://openairdocs.org/sdr/CA070518005), May 16, 2007: DUCT. RUPTURED. (CAN) WHILE PERFORMING THE DAILY INSPECTION, MAINTENANCE PERSONNEL HEARD A LOUD BANG, WHICH WAS FOLLOWED BY A DROP IN APU DUCT PRESSURE TO 0 PSI. UPON INSPECTIO - [SDR CA050718008](https://openairdocs.org/sdr/CA050718008), Jul 12, 2005: FIRE LOOP. FAILED. DURING CLIMB AT FL120, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND ASSOCIATED WARNING HORN SOUNDED INTERMITTENTLY. CREW FOLLOWED ENGINE FIRE EMERGENCY CHECKL - [SDR CA050512004](https://openairdocs.org/sdr/CA050512004), May 5, 2005: CONTROLLER. FAILED. DURING DESCENT FROM FL290 TO FL270, THE 'OFF SCHEDULE' DESCENT LIGHT ILLUMINATED. CABIN ALTITUDE WAS QUICKLY INCREASING WITH CABIN DIFFERENTIAL QUICKLY DECREASI - [SDR CA050105003](https://openairdocs.org/sdr/CA050105003), Dec 20, 2004: CONTROL SYSTEM. FAILED. (CAN) DURING CLIMB FLAPS/SLATS SELECTED UP. FLAPS INDICATED UP, SLAT AMBER REMAINED ON AND AIRCRAFT ROLLED TO THE RT. SECOND OFFICERS PANEL INDICATED NR6 SLAT S - [SDR CA041214007](https://openairdocs.org/sdr/CA041214007), Dec 9, 2004: INDICATOR. UNRELIABLE. (CAN) DURING CLIMB ENGINE NR 2 OIL QUANTITY DECREASED RAPIDLY TO ZERO, FOLLOWED BY A RISE IN OIL TEMP. CREW SHUTDOWN THE ENGINE ANDRETURNED TO AIRPORT. MAINTENA - [SDR CA040625006](https://openairdocs.org/sdr/CA040625006), Jun 24, 2004: SHUTOFF VALVE. LEAKING. (CAN) DURING CLIMB NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. OPS CHECKLIST CARRIED OUT. AIRCRAFT WAS RETURNED TO BASE DUE TO SECOND INCIDENT IN 2 DAYS. DURI - [SDR CA040625002](https://openairdocs.org/sdr/CA040625002), Jun 24, 2004: FIRE LOOP. MALFUNCTIONED. (CAN) DURING FLIGHT, NR 3 ENGINE FIRE WARNING INDICATION WAS ACTIVATED. BELL WAS INTERMITTENT BUT BECAME A LITTLE MORE STEADY. EMERGENCY PROCEDURES WERE INITIAT - [SDR CA040625005](https://openairdocs.org/sdr/CA040625005), Jun 22, 2004: MODULATING VALVE. LEAKING. (CAN) DURING CLIMB IT WAS OBSERVED THAT THE NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. IAW OPS CHECKLIST, SYSTEM CHECK CARRIED OUT AND FLIGHT CONTINUED WITHOUT I - [SDR CA040402006](https://openairdocs.org/sdr/CA040402006), Apr 1, 2004: WIRE HARNESS. INOPERATIVE. (CAN) DURING START UP, IT WAS OBSERVED THAT AC PACK WATER SEPARATOR CB POPPED FOLLOWED BY A PACK TRIP. A BURNING ODRO WAS SENSED. ENGINES WERE SHUTDOWN. MAINTEN - [SDR CA040209002](https://openairdocs.org/sdr/CA040209002), Feb 5, 2004: WINDOW. CRACKED. (CAN) DURING CLIMB, THE F/O OBSERVED THE R2 SLIDING WINDOW WAS CRACKED. THE DECISION WAS MADE TO RETURN TO BASE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE R2 WI - [SDR CA040112003](https://openairdocs.org/sdr/CA040112003), Jan 9, 2004: BRAKE PADS. DAMAGED. (CAN) DURING TAXI, CREW REPORTED THAT THERE WAS SOME DRAGGING FELT WHEN THE BRAKES WERE APPLIED. THE AIRCRAFT RETURNED TO THE BLOCKS. A DETAILED INSPECTION WAS - [SDR CA031202003](https://openairdocs.org/sdr/CA031202003), Nov 29, 2003: TRANSPONDER. FAULTY. (CA) WAS NOTIFIED THAT SEARCH AND RESCUE WAS RECEIVING AN ELT RESPONSE FROM A COMPANY AIRCRAFT. INSPECTED AND IT WAS DETERMINED THIS AIRCRAFT WAS AT FAULT. THE - [SDR CA031103002](https://openairdocs.org/sdr/CA031103002), Oct 30, 2003: ISOLATION VALVE. FAILED. (CAN) DURING CLIMB, IT WAS OBSERVED THAT CABIN PRESSURE WAS NOT CONSISTENT WITH FLIGHT LEVEL. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. AIRCRAFT WAS DISPATCHE - [SDR CA021114006](https://openairdocs.org/sdr/CA021114006), Nov 12, 2002: BOLT. CRACKED. (CAN) AT C-CHECK. WHILE PERFORMING FWD MLG TRUNION FITTING REPLACEMENT ON THE RT MLG. TECH NOTICED NO SHIMS WERE INSTALLED BETWEEN FWD TRUNNION BEARING AND TRUN - [SDR CA020429002](https://openairdocs.org/sdr/CA020429002), Apr 26, 2002: TIE BOLT. SHEARED. (CAN) DURING AIRCRAFT SERVICE CHECK FOUND NR 3 MAIN WHEEL ASSEMBLY WITH ONE SHEARED TIE BOLT NR 3 MAIN WHEEL ASSEMBLY. REPLACED IAW MM 32-45-1. MAIN WHEEL ASSEM - [SDR CA020422005](https://openairdocs.org/sdr/CA020422005), Apr 18, 2002: BOLT. BROKEN. (CAN) DURING SERVICE CHECK, NR 2 MAIN WHEEL TIRE FOUND DEEPLY CUT AND ONE TIE BOLT BROKEN ON MAIN WHEEL HUB ASSY. NR 2 MAIN WHEEL ASSY REPLACED PER MM. MAIN WHE - [SDR CA020412013](https://openairdocs.org/sdr/CA020412013), Apr 8, 2002: HINGE PIN. LOOSE. (CAN) DURING B CHECK INSPECTION, MAIN CARGO DOOR HINGE PIN WAS FOUND MIGRATING AFT APROX. 6 INCHES. HINGE PIN REPOSITIONED AND SAFETIED. - [SDR CA020205007](https://openairdocs.org/sdr/CA020205007), Feb 4, 2002: HINGE PIN. CORRODED. (CAN) DURING INSPECTION OF HORIZONTAL STABILIZER HINGE PINS, FOUND THE RT SIDE OUTER PIN THREADS AND THREAD RELIEF AREA CORRODED. THE OUTER AND INNER PINS WILL - [SDR CA020103007](https://openairdocs.org/sdr/CA020103007), Dec 28, 2001: ENGINE. FAILED. (CAN) NR 3 ENGINE SHUT DOWN IN FLIGHT DUE VIBRATION. REPAIR FACILITY EVALUATION: EXTENSIVE IMPACT DAMAGE WAS NOTED ON THE 7-12 STAGE STATOR VANES AND THE 7-13 S - [SDR CA011119003](https://openairdocs.org/sdr/CA011119003), Nov 7, 2001: ENGINE. FAILED. (CAN) ON DESCENT, THRUST AT IDLE, NR 3 START LEVER VIBRATED IN DETENT. NR 3 EGT 100 DEGREES HIGHER THAN ENGINES NR 1 AND 2. "WHINING NOISE" AND VIBRATION FELT I - [SDR CA010724026](https://openairdocs.org/sdr/CA010724026), Jul 14, 2001: WHEEL. CRACKED. (CAN) DURING SERVICE CHECK, NR 1 MAIN WHEEL TIRE PRESSURE FOUND TO BE 40 PSI PRESSURE DETECTED TO BE LEAKING AT WHEEL HUB. NR 1 AND 2 MAIN WHEEL ASSEMBLIES REPL - [SDR CA010628001](https://openairdocs.org/sdr/CA010628001), Jun 19, 2001: WIRE. BROKEN. (CAN) WHEN LANDING GEAR EXTENDED, R/H MAIN GEAR DOOR LIGHTS DO NO ILLUMINATE. INSPECTED RT MAIN GEAR DOOR CANNON PLUG, WIRE PIN 6 BROKEN, REPAIRED WIRE TO PIN 6 - [SDR CA000907027](https://openairdocs.org/sdr/CA000907027), Aug 22, 2000: ENGINE. FAILED. (CAN) PRIOR TO DESCENT INTO YYC LOW OIL PRESSURE LIGHT ON FOR NR 2 ENGINE OIL PRESSURE DECREASING AND OIL QUANTITY DECREASING.ENGINE FAILURE AND SHUTDOWN FOLLOW - [SDR CA000215019](https://openairdocs.org/sdr/CA000215019), Feb 4, 2000: ACTUATOR. FAILED. (CAN) A/C TURNBACK DUE TO LE FLAP ACTUATOR WOULD NOT RETRACT. NR 2 LE FLAP INDICATES DOWN WHEN FLAP IN RETRACT POSITION. REPLACED. - [SDR S84A008](https://openairdocs.org/sdr/S84A008), Feb 3, 2000: TRANSMITTER. FAILED. ON TAXI OUT, SPLIT FLAP BETWEEN INBOARD AND OUTBOARD 0 DEGREES THROUGH 15 DEGREES. ADJUSTED LEFT OUTBOARD FLAP POSITION TRANSMITTER. OPS CHECK GOOD IAW MM 27-52 - [SDR S84A007](https://openairdocs.org/sdr/S84A007), Jan 28, 2000: SWITCH. LEAKING. NR 2 ENGINE QTY DECREASED TO ZERO. OIL PRESSURE DOWN TO 38 PSI OIL TEMP 80 DEGREES CELSIUS. ENGINE WAS SHUTDOWN AT 0158Z. ENGINE WINDMILLED AT 17 PSI 80 DEGREES - [SDR S84A006](https://openairdocs.org/sdr/S84A006), Jan 22, 2000: WARNING LIGHT. ILLUMINATED. NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED, SHUTDOWN ENGINE PER AFM. DEFERRED AS PER MEL 79-2 ACCOMPLISHED DPPG 79-2. NO CONTAMINANTS FOUND ON INSPECTION OF OIL F - [SDR CA991209038](https://openairdocs.org/sdr/CA991209038), Nov 6, 1999: LINE. MISINSTALLED. (CAN) ON ONE OCCASION BRAKE CHATTER APPEARS ON RT SIDE. FOUND TWO HYDRAULIC LINES CROSSED, REPAIRED. - [SDR CA991209037](https://openairdocs.org/sdr/CA991209037), Nov 1, 1999: FITTING. CRACKED. (CAN) NR 3 FORWARD ENGINE SUPPORT FITTING CRACKED, REPLACED. REF 97-05-08. - [SDR CA991209036](https://openairdocs.org/sdr/CA991209036), Oct 27, 1999: INDICATOR. FAILED. (CAN) COULD NOT RETRACT INBOARD FLAPS PAST 2, USED ALTERNATE FLAPS TO RETRACT, CONTINUED FLIGHT AND AT LANDING USED NORMAL SYSTEM WITHOUT INCIDENT, ON GROUND CY - [SDR CA991007087](https://openairdocs.org/sdr/CA991007087), Sep 25, 1999: BRACKET. CRACKED. (CAN) NLG ACTUATOR UPPER SUPPORT BRACKET CRACKED AT TRUNNION SUPPORT LT AND RT LOWER ATTACH HOLES CRACKED. REPLACED. - [SDR 2000ZZZX24](https://openairdocs.org/sdr/2000ZZZX24), Sep 7, 1999: SPAR. CORRODED. SJO - REPAIRED LEFT WING FRONT SPAR LOWER CHORD PLATE LEADING EDGE BETWEEN FSS 124 AND FSS 152 DUE TO WEAR AND CORROSION IAW COOPESA EO COO-2-57-549-99 DATED 9- - [SDR 99ZZZX3641](https://openairdocs.org/sdr/99ZZZX3641), Aug 16, 1999: LIGHT. INOPERABLE. VARIOUS FLOOR 'E' PATH LIGHTS INOPERABLE. RELAMPED 3 PATHWAY LIGHTS. OPS CHECKED GOOD. - [SDR 99ZZZX3640](https://openairdocs.org/sdr/99ZZZX3640), Aug 16, 1999: LIGHT. INOPERABLE. EMERGENCY LIGHT (INTERIOR) OVER R2 GALLEY DOOR INOPERABLE. REMOVED AND REPLACED BATTERY PACK PN 9505-42, SN OFF 25262; S/N ON 7071. - [SDR 99ZZZX3639](https://openairdocs.org/sdr/99ZZZX3639), Aug 16, 1999: BULB. FAILED. ONE BULB INOPERABLE ON EMERGENCY LIGHT ON AFT CARGO DOOR. RELAMPED. OPS CHECKED GOOD. - [SDR 99ZZZX3638](https://openairdocs.org/sdr/99ZZZX3638), Aug 16, 1999: BULB. FAILED. ONE BULB INOPERABLE ON RIGHT OVERWING FORWARD EMERGENCY LIGHT. RELAMPED. OPS CHECK GOOD. - [SDR CA990715029](https://openairdocs.org/sdr/CA990715029), Jul 15, 1999: ALTIMETER. FAILED. (CAN) FIRST OFFICER'S ALTIMETER READS 100 FEET HIGHER THAN CAPTAIN'S ALT AT DECISION HEIGHT. FO'S ALTIMETER REPLACED AND SERVICEABLE. - [SDR CA990707059](https://openairdocs.org/sdr/CA990707059), Jun 29, 1999: DRIVE UNIT. INOPERATIVE. (CAN) OUTBOARD FLAP ALTERNATE SYSYEM INOPERABLE. OUTBOARD FLAPS ALT DRIVE UNIT REPLACED. All 70: https://openairdocs.org/model/boeing-727-260/reports.md ## STCs that may be installed (OpenAirDocs) (837, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 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 SA3299NM](https://openairdocs.org/stc/SA3299NM): Installation of an overhead life raft stowage compartment kit. Safran Cabin Inc. Lists 727 Series - [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 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 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 - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST01641AT](https://openairdocs.org/stc/ST01641AT): Installation of a photoluminescent floor proximity emergency escape path marking system. STG Aerospace Inc - [STC ST00399SE](https://openairdocs.org/stc/ST00399SE): The above boeing model which has incorporated Raisbeck Commercial Air Group Inc Master Drawing List 96B-1001, Revision D, dated September 2, 1997, or later FAA approved revision, complies iwth FAR Part 36, Stage 3 noise limits. Raisbeck Engineering Inc - [STC ST00553SE](https://openairdocs.org/stc/ST00553SE): Incorporation of the Raisbeck Commercial Air Group inlet acoustical treatment and associated structure on certain engine nose cowls. Raisbeck Engineering Inc - [STC ST00555SE](https://openairdocs.org/stc/ST00555SE): Modification in the leading edge slat and flap configurations. Raisbeck Engineering Inc All 837: https://openairdocs.org/model/boeing-727-260/stcs.md ## PMA parts (OpenAirDocs) (over 1,000, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [CN0940-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191263023320261023152340.0001): Connecting Components fuel and old quantity systems 10-60479. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces 10-60479-12 · Oct 6, 2026 - [CN0940-126](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142363876520261023152341.0001): Connecting Components fuel and old quantity systems 10-60479. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces 10-60479-126 · Oct 6, 2026 - [9781-2IKT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110484692620260909135544.0001): Latch Assy. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9781-2 · Aug 31, 2026 - [BACC45FT16C24S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176521662720260930182727.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16C24S · Aug 27, 2026 - [BACC45FT14-15S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142993650720260930182705.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-15S · Aug 27, 2026 - [BACC45FT14-7S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138551737320260930182709.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-7S · Aug 27, 2026 - [BACC45FT18A14P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132144449920260930182733.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT18A14P · Aug 27, 2026 - [BACC45FT16-24P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123899478520260930182718.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16-24P · Aug 27, 2026 - [BACC45FT14A7S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123337052020260930182713.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14A7S · Aug 27, 2026 - [BACC45FT16A24P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122635290020260930182721.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16A24P · Aug 27, 2026 - [BACC45FT14-7P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104300287920260930182707.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-7P · Aug 27, 2026 - [69-38947EV-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136065364220260930205555.0001): Yoke Clip. EVCO, LLC · PMA PQ00044CB · Replaces 69-38947-21 · Aug 12, 2026 - [69-38947EV-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105135663220260930205555.0001): Yoke Clip. EVCO, LLC · PMA PQ00044CB · Replaces 69-38947-13 · Aug 12, 2026 - [BACC45FN16-24P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197713128720260826222320.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24P6 · Jul 15, 2026 - [BACC45FT10C5P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193996168620260826222355.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT10C5P · Jul 15, 2026 - [BACC45FT12-12S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193814563120260826222400.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-12S · Jul 15, 2026 - [BACC45FN22-19P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189121516320260826222338.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-19P · Jul 15, 2026 - [BACC45FN18-8P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189112308220260826222330.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN18-8P · Jul 15, 2026 - [BACC45FT12-12P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181604367920260826222358.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-12P · Jul 15, 2026 - [BACC45FN22-55P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181107411820260826222341.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-55P · Jul 15, 2026 - [BACC45FN20-25S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175722890620260826222332.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN20-25S · Jul 15, 2026 - [BACC45FT10C5S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166448010820260826222357.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT10C5S · Jul 15, 2026 - [BACC45FN8-3P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161773834720260826222352.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN8-3P · Jul 15, 2026 - [BACC45FS14-7P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161191738820260826222355.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, THREADED COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FS14-7P · Jul 15, 2026 - [BACC45FN16-24P7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152017518420260826222321.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24P7 · Jul 15, 2026 - [BACC45FT12-12P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150919908320260826222359.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-12P6 · Jul 15, 2026 - [BACC45FN16-24P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143397069520260826222319.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24P · Jul 15, 2026 - [BACC45FN18-14P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136438137320260826222326.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN18-14P · Jul 15, 2026 - [BACC45FN18-31P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134751538220260826222328.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN18-31P · Jul 15, 2026 - [BACC45FN16-24S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108180098920260826222324.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24S · Jul 15, 2026 - [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172200643320260909221022.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026 - [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148776985720260909221013.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026 - [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133606371820260909221004.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026 - [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116339893920260909220945.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026 - [BACC45FN12-12P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176703190220260826222409.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN12-12P6 · Jun 10, 2026 - [BACC45FN14-15P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176140837920260826222418.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN14-15P · Jun 10, 2026 - [BACC45FN12-12P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174312460620260826222407.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN12-12P · Jun 10, 2026 - [BACC45FN14-7S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153623499520260826222422.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN14-7S · Jun 10, 2026 - [BACC45FN12-12S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152683497720260826222411.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN12-12S · Jun 10, 2026 - [BACC45FN14-15S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114007333220260826222419.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN14-15S · Jun 10, 2026 - [AF201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193338846020260717175322.0001): Duct Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026 - [J-082269-7TMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188457935320260616141004.0001): Ball Transfer Unit. Source Manufacturing Inc · PMA PQ1549CE · Replaces J-082269-7 · Apr 10, 2026 - [BACC45FT10-5P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191951809220260309212953.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT10-5P · Mar 7, 2026 - [BACC45FT10-5S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168149589820260309212957.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT10-5S · Mar 7, 2026 - [BACC45FN10-5S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133201637820260309212949.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN10-5S · Mar 7, 2026 - [BACC45FN10-5P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107300513420260309212944.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN10-5P · Mar 7, 2026 - [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140279722720260325180521.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026 - [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113446375620260325172402.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026 - [HR1287-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155529214120251124233301.0001): Repair Kit. HRD Aerosystems Inc · PMA PQ1451NM · Replaces R1287-101 · Oct 15, 2025 - [SP2514-06-1175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106892706220251119194842.0001): CAP ASSEMBLY. Soundair Aviation Services · PMA PQ2540NM · Replaces 383-0271-1 · Oct 1, 2025 All of them: https://openairdocs.org/model/boeing-727-260/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Boeing 727-223](https://openairdocs.org/model/boeing-727-223): 9 registered aircraft, registry code 1384074 - [Boeing 727-227](https://openairdocs.org/model/boeing-727-227): 4 registered aircraft, registry code 1384078 - [Boeing 727-225](https://openairdocs.org/model/boeing-727-225): 2 registered aircraft, registry code 1384077 - [Boeing 727-200](https://openairdocs.org/model/boeing-727-200): 1 registered aircraft, registry code 138407E - [Boeing 727-212](https://openairdocs.org/model/boeing-727-212): 1 registered aircraft, registry code 138407G - [Boeing 727-230](https://openairdocs.org/model/boeing-727-230): 1 registered aircraft, registry code 1384080 - [Boeing 727-232](https://openairdocs.org/model/boeing-727-232): 1 registered aircraft, registry code 1384082 - [Boeing 727-243](https://openairdocs.org/model/boeing-727-243): 1 registered aircraft, registry code 138408D - [Boeing 727-247](https://openairdocs.org/model/boeing-727-247): 1 registered aircraft, registry code 138408F - [Boeing 727-264](https://openairdocs.org/model/boeing-727-264): 1 registered aircraft, registry code 138408M - [Boeing 727-281](https://openairdocs.org/model/boeing-727-281): 1 registered aircraft, registry code 138408N - [Boeing 727-277](https://openairdocs.org/model/boeing-727-277): 1 registered aircraft, registry code 138408S --- 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.