# Boeing 727-277

- Type: Aircraft model (FAA registry)
- Registry code: 138408S
- Manufacturer (registry): BOEING
- Model: 727-277
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 189
- 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: 1
- Page: https://openairdocs.org/model/boeing-727-277

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-727-277/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 (1)

- [N727HL](https://openairdocs.org/aircraft/N727HL): [Aviation Sales And Charter LLC](https://openairdocs.org/faa-owner/AVIATION%20SALES%20AND%20CHARTER%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), S/N 22642

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (10)

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 20140626011349I](https://openairdocs.org/incident/20140626011349I), Jun 26, 2014: Boeing 727-277 (N251FL), Laredo, TX, Substantial damage. Third crew member on aircraft was the flight engineer, [privacy data omitted], dob is [privacy data omitted]. His hire date is [privacy data omitted], total…
- [Incident 20040323003849I](https://openairdocs.org/incident/20040323003849I), Mar 23, 2004: Boeing 727277 (N245FE), Great Falls, MT. (-23) On March 24, 2004, at approximately 0058 UTC, fed ex, flight 542, a B727 landed at gtf and was notified by the tower, that the aircraft's right brake was…
- [Incident 20030107005959I](https://openairdocs.org/incident/20030107005959I), Jan 7, 2003: Boeing 727277 (N244FE), Indianapolis, IN. (-23) On 01/07/03 fedex flight 1609 declared an emergency due to a loss of the system a hydraulic fluid. Maintenance personnel found that the right outboard…
- [Incident 19980331009899I](https://openairdocs.org/incident/19980331009899I), Mar 31, 1998: Boeing 727277 (N246FE), Des Moines, IA. Narrative: aircraft landed on runway 31R & subsequently slid off departure end and taxiway D6. Dsm ATC stated observed FL 1500 making approach, landing, and…
- [Incident 19940629028909I](https://openairdocs.org/incident/19940629028909I), Jun 29, 1994: Boeing 727277 (N241FE), Rochester, NY. On climbout strip of sealing tape came loose and flapped against windshield returned and replaced.
- [Incident 19901018054419I](https://openairdocs.org/incident/19901018054419I), Oct 18, 1990: Boeing 727277 (N240FE), Memphis, TN. ATC requested pilot to expedite rollout. Lost control, veered and struck lights. Runway had ungrooved patches.
- [Incident 19900518032509I](https://openairdocs.org/incident/19900518032509I), May 18, 1990: Boeing 727277 (N246FE), Minor damage. Two bullet holes found in cargo compartment and fuselage during post flight inspection.
- [Incident 19880411022379I](https://openairdocs.org/incident/19880411022379I), Apr 11, 1988: Boeing 727277 (N274WC), Kansas City, MO. Pilot failed to follow the yellow line. Turned too soon. Right gear became stuck in the mud.
- [Incident 19851012060689I](https://openairdocs.org/incident/19851012060689I), Oct 12, 1985: Boeing 727277 (N275WC), Omaha, NE. Passenger became ill and unscheduled landing was made.
- [Incident 19850619032439I](https://openairdocs.org/incident/19850619032439I), Jun 19, 1985: Boeing 7272M7 (N276WC), Omaha, NE. Unscheduled landing made to remove ill passenger.

## Service difficulty reports (627, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR VGCA20140624004](https://openairdocs.org/sdr/VGCA20140624004), Jun 24, 2014: FAIRING. DAMAGED. FAIRING ADJACENT TO LEFT PACK COOLING DOOR DAMAGED.
- [SDR FDEA201306151306](https://openairdocs.org/sdr/FDEA201306151306), Jun 15, 2013: UNKNOWN. UNKNOWN. ENROUTE, BOTH ALTIMETERS SHOWED LEVEL AT FL350 ATC STATED THE RETURN WAS SHOWING 400' HIGH. TRANSPONDER WAS SELECTED NR 1. PERFORMED TEST ON NR 1 & 2 TRANSPONDE
- [SDR VGCA20130528005](https://openairdocs.org/sdr/VGCA20130528005), May 28, 2013: SUPPORT BEAM. CORRODED. CORROSION ON LT MLG BEAM AT NR 4 FLAP TRACK ATTACH POINT AROUND BOLTS.
- [SDR VGCA20130528004](https://openairdocs.org/sdr/VGCA20130528004), May 28, 2013: SUPPORT BEAM. CORRODED. CORROSION ON BOTTOM SIDE OF RT MLG SUPPORT BEAM AT NR 5 FLAP TRACK ATTACH POINT.
- [SDR VGCA20130528003](https://openairdocs.org/sdr/VGCA20130528003), May 28, 2013: SUPPORT FITTING. CORRODED. CORROSION ON LT WING FUSELAGE TERMINAL FITTING.
- [SDR VGCA20130528002](https://openairdocs.org/sdr/VGCA20130528002), May 28, 2013: FUEL TANK. CORRODED. RIGHT SIDE AFT UPPER SURFACE OF FUEL TANK AT FS 850 CORRODED.
- [SDR VGCA20130528001](https://openairdocs.org/sdr/VGCA20130528001), May 28, 2013: SUPPORT FITTING. CORRODED. CORROSION ON LT WING FUELAGE TERMINAL FITTING.
- [SDR VGCA20121010](https://openairdocs.org/sdr/VGCA20121010), Oct 10, 2012: SKIN. DAMAGED. UPPER FUSELAGE SKIN DAMAGED.
- [SDR VGCA20120207](https://openairdocs.org/sdr/VGCA20120207), Feb 7, 2012: DOOR FRAME. CRACKED. THREE INCH CRACK FOUND ON NR 3 CARGO DOOR FWD FRAME AT S-26R ON FRAME 1090 WHILE COMPLYING WITH AD2006-13-01/SB 53A0169.
- [SDR FDEA201108173307](https://openairdocs.org/sdr/FDEA201108173307), Aug 17, 2011: LIGHT. INOPERATIVE. FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. R & R FLIGHT DECK EMERGENCY EXIT LIGHT REF MM 33-50-101-2-0. OPS CHECKED NORMAL.
- [SDR FDEA201107303035](https://openairdocs.org/sdr/FDEA201107303035), Jul 30, 2011: FLEX HOSE. LEAKING. AT ABOUT 60-70 KNOTS ON TAKEOFF ROLL S/O CALLED A-SYS HYD QTY WAS ZERO. REJECTED TAKEOFF. PRESSURE ON A SYS WAS NORMAL UNTIL THE RUNWAY CLEARED, THEN LOST HYD P
- [SDR FDEA201107232914](https://openairdocs.org/sdr/FDEA201107232914), Jul 23, 2011: THERMAL SWITCH. FAILED. DURING CRUISE AT FL360 ENGINE 3 BLEED AIR TRIP OFF LIGHT ILLUMINATED AND THE NR 3 BLEED AIR VALVE CLOSED, SYS WOULD NOT RESET VIA QRH PROCEDURES ( LIGHT STAYED 
- [SDR FDEA201010224147](https://openairdocs.org/sdr/FDEA201010224147), Oct 22, 2010: ENGINE. FAILED. WHILE ADVANCING POWER FOR TAKEOFF, AT 80 PERCENT N1 ON ENG NR 2. EPR SLOW TO INCREASE, COMPRESSOR STALL OCCURED. TOWER WITNESSED FLAMES FROM NR 2 ENGINE. R & R 
- [SDR FDEA201008203055](https://openairdocs.org/sdr/FDEA201008203055), Aug 20, 2010: RECEIVER. FAILED. VOR'S CHECKED GOOD ON PREFLIGHT. DURING CLIMBOUT BOTH VOR'S SHOWED A 30 DEGREE SPLIT ON VOR STA COULD NOT CTR EITHER CDI ON VOR STATION. TRIED ANOTHER VOR STA, 
- [SDR FDEA201001150180](https://openairdocs.org/sdr/FDEA201001150180), Jan 15, 2010: SEAT TRACK. CORRODED. CABIN SEAT TRACK AT STA 695 RBL 24 INBD FLANGE AND SPLICE CORRODED REMOVED SEAT TRACK SECTION BETWEEN STA 690 TO 740 RBL24 AND 1 EA SPLICER IAW SRM 51-30-2, FAB
- [SDR FDEA200908072929](https://openairdocs.org/sdr/FDEA200908072929), Aug 7, 2009: INDICATOR. FAILED. STANDBY ADI PRECESSED 20 MIN. AFTER TAKE OFF, AT CRUISE. RECAGED BUT 2-3 MIN. LATER, PRECESSED AGAIN. 20-30 DEG RIGHT BANK, 10 DEG NOSE HIGH. REMOVED AND REPLAC
- [SDR FDEA200906011866](https://openairdocs.org/sdr/FDEA200906011866), Jun 1, 2009: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM BS 312, LBL 6 IS EXFOLIATED ON AFT LIP OF UPPER CHORD. CUT OUT DAMAGED AREA 2 BY 1 INCH IAW DWG NR SR27-53-017 REV A. FABRICATED 2 REPAIR A
- [SDR FDEA200905311899](https://openairdocs.org/sdr/FDEA200905311899), May 31, 2009: SKIN. DAMAGED. RT WING INBD FOREFLAP, OUTBD END, PREVIOUS REPAIR IS GOUGED REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4 AND 57-50-4
- [SDR FDEA200905301857](https://openairdocs.org/sdr/FDEA200905301857), May 30, 2009: FUEL TANK. DAMAGED. DAMAGE AT STA 744 ON CTR TANK WEB RBL 60. REPAIRED CENTER TANK WEB IAW EA 7-5710-126825. REPAIR BY CUTTING OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IA
- [SDR FDEA200905301858](https://openairdocs.org/sdr/FDEA200905301858), May 30, 2009: STRINGER. CORRODED. AFT CARGO COMPARTMENT, CORROSION AROUND FASTENERS IN STRINGER 30 AT BS 990. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED NEW STRINGER SECTION, FABRICAT
- [SDR FDEA200905291863](https://openairdocs.org/sdr/FDEA200905291863), May 29, 2009: RIB. CRACKED. NR 5 SLAT HAS CRACKED RIB ON INBOARD SIDE OF ACTUATOR FORWARD MOUNT. REMOVED AND REPLACED RIBS WITH NEW RIBS IAW SRM 51-30-2.
- [SDR FDEA200905291846](https://openairdocs.org/sdr/FDEA200905291846), May 29, 2009: STRINGER. CORRODED. STRINGER 27L CORRODED STA'S 950F TO 1030 REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER SECTIONS. FABRICATED RE
- [SDR FDEA200905271940](https://openairdocs.org/sdr/FDEA200905271940), May 27, 2009: FRAME. DAMAGED. STATION 520 FRAME DAMAGED AT STRINGER 21L TO 26L. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, HEAT TREATED TO T6 CONDITION, AND INSTALLED PARTS IAW SRM 51-30-2
- [SDR FDEA200905271898](https://openairdocs.org/sdr/FDEA200905271898), May 27, 2009: SKIN. CRACKED. RMLG WING DOOR SKIN CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB 727-32-318 HFEC SHOWS AREA OF CUT OUT FREE OF CRACKS IAW NDTM 51-00-00 FIG 
- [SDR FDEA200905271865](https://openairdocs.org/sdr/FDEA200905271865), May 27, 2009: SEAT TRACK. CORRODED. SEAT TRACK CORRODED STA 690-720 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW ONE, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-
- [SDR FDEA200905271815](https://openairdocs.org/sdr/FDEA200905271815), May 27, 2009: SHEAR TIE. CORRODED. FWD PIT BS 720C BETWEEN ST 25RT TO 26RT SHEAR TIE CORRODED.
- [SDR FDEA200905271814](https://openairdocs.org/sdr/FDEA200905271814), May 27, 2009: SHEAR TIE. CORRODED. FWD PIT BS 720C BETWEEN STR 25L TO 26L SHEAR TIE CORRODED
- [SDR FDEA200905261900](https://openairdocs.org/sdr/FDEA200905261900), May 26, 2009: SKIN. CRACKED. LEFT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB B727-32-318 AND SRM 51-30-2 HFEC SHOWS AREA FREE OF CRACKS IAW NDTM 51-00-00
- [SDR FDEA200905231868](https://openairdocs.org/sdr/FDEA200905231868), May 23, 2009: STRINGER SPLICE. CORRODED. CORROSION ON STRINGER SPLICE AT STRINGER 30, BS 950. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE PN 69-44177-1 IAW SRM 51-30-2, AND 51-30-5.
- [SDR FDEA200905231867](https://openairdocs.org/sdr/FDEA200905231867), May 23, 2009: FITTING. CORRODED. CORROSION ON STRINGER 29L KEELBEAM EXTENSION FITTING AT BS 950. FOUND OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PART NR 69-5
- [SDR FDEA200905211765](https://openairdocs.org/sdr/FDEA200905211765), May 21, 2009: SEAT TRACK. CORRODED. MAIN CABIN FUSELAGE SEAT TRACK AT BS 1110, LBL 24 IS CORRODED. REMOVED CORRODED SECTION OF SEAT TRACK IAW 51-30-2 FABRICATED NEW SECTION IAW DRAWING 53FX976 REV
- [SDR FDEA200905211760](https://openairdocs.org/sdr/FDEA200905211760), May 21, 2009: STRINGER. CORRODED. ART PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 950E-950F. REMOVED CORROSION IAW SRM 51-10-6. UT INSPECTED AREA FOUND OUT OF LIMITS. CUT OUT DAMAGE AREA IAW SRM 
- [SDR FDEA200905211759](https://openairdocs.org/sdr/FDEA200905211759), May 21, 2009: STRINGER. CORRODED. AFT PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 970-990. REMOVED CORROSION IAW SRM 51-10-6. INSPECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-10-1. FIG 1. CUT OU
- [SDR FDEA200905191757](https://openairdocs.org/sdr/FDEA200905191757), May 19, 2009: SKIN. CRACKED. L-1 DOOR LOWER HINGE SKIN DOUBLER IS CRACKED. REPAIRED L-1 DOOR LOWER HINGE SKIN IAW EO 7-5330-7-2345 PART 2.
- [SDR FDEA200905191741](https://openairdocs.org/sdr/FDEA200905191741), May 19, 2009: FRAME. CRACKED. FORWARD CARGO DOOR, STA 540, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME, FABRICATED NEW ONE AND INSTALLED IAW SRM SRM 51
- [SDR FDEA200905191740](https://openairdocs.org/sdr/FDEA200905191740), May 19, 2009: FRAME. CRACKED. FORWARD CARGO DOOR, STA 520, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME AND INSTALLED NEW FABRICATED ONE IAW SRM 51-30-2
- [SDR FDEA200905191739](https://openairdocs.org/sdr/FDEA200905191739), May 19, 2009: FRAME. CRACKED. FORWARD CARGO DOOR, STA 500, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.
- [SDR FDEA200905191738](https://openairdocs.org/sdr/FDEA200905191738), May 19, 2009: FRAME. CRACKED. FORWARD CARGO DOOR, STA 560, STRINGER 21-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME EXTENSION, FABRICATED NEW STUB FRAME, HEAT TREATE
- [SDR FDEA200905181842](https://openairdocs.org/sdr/FDEA200905181842), May 18, 2009: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BS 1110-1116 LBL47. CORROSION ON SEAT TRACK OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51
- [SDR FDEA200905181713](https://openairdocs.org/sdr/FDEA200905181713), May 18, 2009: STRINGER. CORRODED. FWD PIT CORROSION ON STR 26 L STA 720B. CUT OUT DAMAGE AREA IAW SRM 53-10 3 FIG 1. FABRICATED REPAIR PART AND 2 SPLICES IAW SRM 53-10-2 FIG 1 AND 53-10-2 FIG 9.
- [SDR FDEA200905181712](https://openairdocs.org/sdr/FDEA200905181712), May 18, 2009: STRINGER. CORRODED. FWD PIT - CORROSION ON STR 26 L BETWEEN STA 700 AND 720. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER AND 1 SPLICE IAW SRM 53-10-2 FIG 9. TREA
- [SDR FDEA200905181714](https://openairdocs.org/sdr/FDEA200905181714), May 18, 2009: FITTING. CORRODED. CORROSION ON STRINGER 29 R KEEL BEAM EXTENSION FITTING AT BS 950. FOUND CORROSION ON FITTING OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED N
- [SDR FDEA200905171699](https://openairdocs.org/sdr/FDEA200905171699), May 17, 2009: SKIN. CRACKED. RT WING INBD MID FLAP AFT LOWER ANGLE HAS 2 CRACKS, WBL 90. REMOVED R / WING I/B MID FLAP LOWER INNER SKIN PANEL IAW SRM 51-30-2. CUT OUT DAMAGE AREA ANGLE SECT
- [SDR FDEA200905171702](https://openairdocs.org/sdr/FDEA200905171702), May 17, 2009: ANGLE. CRACKED. NR 3 SLAT AFT LOWER ANGLE IS CRACKED AT ACTUATOR ATTACHMENT. UPON FURTHER INVESTIGATION SLAT REPAIR NOT FEASIBLE, SLAT REMOVED AND REPLACED.
- [SDR FDEA200905171701](https://openairdocs.org/sdr/FDEA200905171701), May 17, 2009: SPAR. CRACKED. LT WING FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. CUTOUT SECTION, FABRICATED NEW SECTION, FABRICATED WEB, FABRICATED 2 ANGLES, HEAT TREAT ANGLES IAW FASI ER
- [SDR FDEA200905171700](https://openairdocs.org/sdr/FDEA200905171700), May 17, 2009: KEELBEAM. CRACKED. LT W/W, LT KEEL BEAM IS CRACKED AT 2ND FASTENER STA 875, LBL 6. TRIMMED OUT CRACK DIMS 2 INCH X 1 INCH, FABRICATED DOUBLER, HEAT TREATED AND CADMIUM PLATED DOUB
- [SDR FDEA200905171697](https://openairdocs.org/sdr/FDEA200905171697), May 17, 2009: SKIN. CORRODED. RT WING LEADING EDGE HAS BULGING SEALANT AND CORROSION AT WS 510 UPPER SURFACE ABOVE SPAR. FABRICATED REPAIR FILLERS & DOUBLER IAW B727 SRM 57-30-4 FIG 6. TREAT
- [SDR FDEA200905161690](https://openairdocs.org/sdr/FDEA200905161690), May 16, 2009: SKIN. DAMAGED. FUSELAGE SKIN AT STA 300 STRINGER 21LT IS GOUGED BLENDED OUT DAMAGED AREA IAW SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2, CUT OUT DAMAGE
- [SDR FDEA200905161693](https://openairdocs.org/sdr/FDEA200905161693), May 16, 2009: ANGLE. CRACKED. NR 6 SLAT AFT LOWER CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD REMOVED NR 6 SLAT COVE ACCESS PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRIC
- [SDR FDEA200905151681](https://openairdocs.org/sdr/FDEA200905151681), May 15, 2009: SKIN. CRACKED. RIGHT FOREFLAP, INBOARD WBL 124, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER & FILLER IAW SRM 57

All 627: https://openairdocs.org/model/boeing-727-277/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-727-277/stcs.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 727-287](https://openairdocs.org/model/boeing-727-287): 0 registered aircraft, registry code 1384020

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