# Boeing 727-1A7C

- Type: Aircraft model (FAA registry)
- Registry code: 13840X2
- Manufacturer (registry): BOEING
- Model: 727-1A7C
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 134
- Weight class: 20,000 lb and over
- Cruise speed: 435 mph
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-727-1a7c

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.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (118, newest 50)

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

- [SDR UPS07249687](https://openairdocs.org/sdr/UPS07249687), Apr 24, 2007: DUCT. BLOWN. EMERGENCY DECLARED, LWR AFT BODY OVERHEAT WARNING LIGHT ILLUM. ALL EPR INDICATIONS INOP. STDBY HYD OVERHEAT LT ILLUM. CAPT'S RADIO INTERMITTENT CREW WAS ASKED T
- [SDR UPS06247519](https://openairdocs.org/sdr/UPS06247519), Jul 26, 2006: WEB. CRACKED. CRACK FOUND ON I/B WEB OF REMOVABLE LEADING EDGE AT BS 740 RT. DAMAGED AREA REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS06247593](https://openairdocs.org/sdr/UPS06247593), Jul 14, 2006: SKIN. CORRODED. INSPECTION TYPE:C HTD B-NUT HAS FRETTED SKIN IN HYD BAY AT BS 1000 AT STR 23 LEFT. MEASURED AND EVALUATED FRETTED SKIN AND FOUND OUT OF LIMITS IAW SRM 53-30-01.
- [SDR UPS06247457](https://openairdocs.org/sdr/UPS06247457), Jul 14, 2006: CARRIAGE. WORN. INSPECTION TYPE:C WEAR IN NR 7 FLAP CARRIAGE SIDE ROLLER ASSY BRACKETS. FLAP CARRIAGE REPLACED IAW MM 27-51-13.
- [SDR UPS06247428](https://openairdocs.org/sdr/UPS06247428), Jul 14, 2006: LINK. CORRODED. INSPECTION TYPE:C NR 5 FLAP CARRIAGE BEARING LINK BEARING A DRIFT AND BUSHING CORRODED. CORROSION FOUND ON INNER SURFACE OF BEARING LINK. BEARING LINK ASSY AND 
- [SDR UPS06247460](https://openairdocs.org/sdr/UPS06247460), Jul 13, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE:C SEAT TRACK AT RBL 40 2 BETWEEN BS 740-760 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 51-30-02. REPLACED SEAT TRACK IAW SRM 51-30-02.
- [SDR UPS06247456](https://openairdocs.org/sdr/UPS06247456), Jul 13, 2006: CARRIAGE. WORN. INSPECTION TYPE:C NR 8 FLAP CARRIAGE AFT SIDE ROLLERS FWD ATTACH HOLES WORN. FLAP CARRIAGE REPLACED IAW MM 27-51-13.
- [SDR UPS06247436](https://openairdocs.org/sdr/UPS06247436), Jul 13, 2006: BEAM. CORRODED. INSPECTION TYPE:C SIDE LOAD BEAM AT RIGHT BS 740 CORRODED. ANGLE FABRICATED IAW DRWG 65-15940. INSTALLED SIDE LOAD BEAM ANGLE IAW B727-5310-7477.
- [SDR UPS06247434](https://openairdocs.org/sdr/UPS06247434), Jul 13, 2006: CARRIAGE. CORRODED. INSPECTION TYPE:C NR 4 FLAP CARRIAGE FWD LOWER FLANGE CORRODED. FLAP CARRIAGE REPLACED IAW MM 27-51-03.
- [SDR UPS06247386](https://openairdocs.org/sdr/UPS06247386), Jul 13, 2006: CARRIAGE. CORRODED. INSPECTION TYPE:C NR 5 FLAP CARRIAGE HAS CORROSION ON LWR FWD FLANGE UPPER AND LOWER SURFACES CARRIAGE REPLACED IAW MM 27-51-03.
- [SDR UPS06247385](https://openairdocs.org/sdr/UPS06247385), Jul 12, 2006: CARRIAGE. CORRODED. INSPECTION TYPE-C, 3 SEQUENCE CARRIAGE HAS CORROSION ON AFT UPPER LUGS SEQUENCE CARRIAGE REPLACED IAW MM 27-51-04.
- [SDR UPS06247373](https://openairdocs.org/sdr/UPS06247373), Jul 12, 2006: FLOOR SUPPORT. CRACKED. INSPECTION TYPE-C AND SI FLOOR SUPPORT CRACKED AT BS 850 RBL 24.75. FLOOR SUPPORT REMOVED IAW SRM 51-30-02. NEW FLOOR SUPPORT FABRICATED I AW SRM 51-40-03. FLOO
- [SDR UPS06247433](https://openairdocs.org/sdr/UPS06247433), Jul 11, 2006: FLAP TRACK. CORRODED. INSPECTION TYPE:C CORROSION IN \1 FLAP TRACK HOLES E, D AND C. BUSHING FABRICATED IAW AAAE EO 2006-042-005. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SO
- [SDR UPS06247429](https://openairdocs.org/sdr/UPS06247429), Jul 11, 2006: FLAP TRACK. CORRODED. INSPECTION TYPE:C CORROSION IN NR 6 FLAP TRACK HOLES G AND F. BUSHINGS FABRICATED IAW AAAE-EO-2006-042-08. HEAT TREATED IAW 06-42-03. CAD PLATED IAW SOPM 20-42-
- [SDR UPS06247375](https://openairdocs.org/sdr/UPS06247375), Jul 11, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE-C AND SI CORROSION ON UPPER SURFACE OF FLOORBEAM UPPER FLANGE REPAIR AT BS 560 LBL 37. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUT OF 
- [SDR UPS06247353](https://openairdocs.org/sdr/UPS06247353), Jul 11, 2006: SUPPORT. CORRODED. INSPECTION TYPE: C AND SI CORROSION ON INTERCOSTAL SUPPORT CONTROL CABIN FLOOR, BL 0, FS 277 TO 29 4.5. CORROSION CLEANED AND SUPPORT FOUND TO BE OUTSIDE LIMITS
- [SDR UPS06247568](https://openairdocs.org/sdr/UPS06247568), Jul 10, 2006: STRUCTURE. CORRODED. INSPECTION TYPE:C EVIDENCE OF CORROSION AT BS 850 RT UNDER STR 18A. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06. FASTENER REINSTALLED 
- [SDR UPS06247463](https://openairdocs.org/sdr/UPS06247463), Jul 10, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE:C EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 690-720 RBL 65. CORROSION OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REP
- [SDR UPS06247432](https://openairdocs.org/sdr/UPS06247432), Jul 10, 2006: ATTACH FITTING. CORRODED. INSPECTION TYPE:C CORROSION ON NR 7 FLAP TRACK ATTACH PAD HOLE E. BUSHING FABRICATED IAW EO 2006-042-0009. HEAT TREATMENT REFERENCE 06-4 2-03. CAD PLATED IAW SO
- [SDR UPS06247431](https://openairdocs.org/sdr/UPS06247431), Jul 10, 2006: ATTACH FITTING. CORRODED. INSPECTION TYPE:C NR 8 FLAP TRACK ATTACH PAD HAS CORROSION IN HOLES E, D AND C. BUSHINGS FABRICATED FOR HOLES IAW AAAE EO 2006-042-10. HEAT TREATMENT REFERENCE 
- [SDR UPS06247381](https://openairdocs.org/sdr/UPS06247381), Jul 10, 2006: WEB. CRACKED. INSPECTION TYPE-C SI RT WING STRUCTURE INNER WEB CRACKED AT NR 8 SLAT ACTUATOR CUTOUT, REPAIR OR REPLACE. REPAIRED IAW SRM 51-40-02 FIG 1.
- [SDR UPS06247365](https://openairdocs.org/sdr/UPS06247365), Jul 10, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE-C AND SI EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 5 92 RBL 45. NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW
- [SDR UPS06247364](https://openairdocs.org/sdr/UPS06247364), Jul 10, 2006: SEAT TRACK. CRACKED. INSPECTION TYPE-C AND IS CRACKED ON SEAT TRACK TOP BS 397 RBL 23 NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90, SRM 5 1-10-2 AND 51-30-2.
- [SDR UPS06247626](https://openairdocs.org/sdr/UPS06247626), Jul 8, 2006: SKIN. DAMAGED. INSPECTION TYPE:C SMALL NICK ON FUSE SKIN, DAMAGE LOCATED AT BASE OF C, D WINDOW POST. FASTENERS REMOVED FROM REPAIR AREA AND DAMAGE BLENDED OUT IAW SRM 53-30 -
- [SDR UPS06247462](https://openairdocs.org/sdr/UPS06247462), Jul 8, 2006: STIFFENER. CORRODED. INSPECTION TYPE:C CORROSION ON FLOOR STRUCTURE STIFFENER AT RT SIDE AT BS 230 RBL 36. STIFFENER REPLACED IAW SRM 51-30-02.
- [SDR UPS06247374](https://openairdocs.org/sdr/UPS06247374), Jul 8, 2006: INTERCOSTAL. CORRODED. INSPECTION TYPE-C AND SI CORROSION AROUND ANCHOR NUT HOLE UNDER COCKPIT DOOR SILL BS 303. REMOVED INTERCOSTAL UNDER COCKPIT DOOR IAW SRM 51-30-02. FABRICATED I 
- [SDR UPS06247352](https://openairdocs.org/sdr/UPS06247352), Jul 8, 2006: INTERCOSTAL. GOUGED. INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 328 AND 334 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LI
- [SDR UPS06247351](https://openairdocs.org/sdr/UPS06247351), Jul 8, 2006: INTERCOSTAL. GOUGED. INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 312 - 328 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMI
- [SDR UPS06247520](https://openairdocs.org/sdr/UPS06247520), Jul 7, 2006: RIB. CRACKED. SUSPECT CRACK ON NR 6 SLAT ON 4TH RIB OB OF ACTUATOR AT UPPER AFT CORNER RIB REPLACED IAW SRM 51-30-02.
- [SDR UPS06247518](https://openairdocs.org/sdr/UPS06247518), Jul 7, 2006: RIB. CRACKED. SUSPECT CRACK ON NR 6 SLAT ON 1ST RIB O/B OF I/B TRACK ALONG AFT FLANGE. RIB REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247437](https://openairdocs.org/sdr/UPS06247437), Jul 7, 2006: RIB. CRACKED. INSPECTION TYPE:C SUSPECT CRACK ON NR 5 SLAT 3RD RIB O/B OF IB TRACK AT AFT UPPER CORNER. SLAT REPLACED.
- [SDR UPS06247366](https://openairdocs.org/sdr/UPS06247366), Jul 7, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE-C AND SI CORROSION ON SEAT TRACK TOP CHORD BS 590-630 LBL 45.5 NEW SEAT TRACK FABRICATED, PAINT AND INSTALLED IAW MM 51-20-90, SRM 51- 30-2, 53-
- [SDR UPS06247636](https://openairdocs.org/sdr/UPS06247636), Jul 6, 2006: WEDGE. DELAMINATED. RT O/B AILERON HAS DELAM ON TRAILING EDGE WEDGE. AILERON BEYOND REPAIRABLE LIMITS, AILERON REPLACED IAW MM 27-10-14.
- [SDR UPS06247569](https://openairdocs.org/sdr/UPS06247569), Jul 6, 2006: STRUCTURE. CORRODED. INSPECTION TYPE:C SURFACE CORROSION AT BOTH I/B STATIC DISCHARGERS LEFT WING TIP T/E. CORROSION REMOVED IAW SRM 51-10-01 AND FASTENERS REMOVED IAW SRM 51-3 0-02
- [SDR UPS06247566](https://openairdocs.org/sdr/UPS06247566), Jul 6, 2006: FITTING. CRACKED. INSPECTION TYPE:C BS 740 TERMINAL FITTING REQUIRES REPLACING. FITTING REPLACED IAW EO B727-5310-7477 AND DRWG 65C13724.
- [SDR UPS06247464](https://openairdocs.org/sdr/UPS06247464), Jul 6, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE:C CORROSION ON SEAT TRACK TOP CHORD AT BS 950-962 RBL 62.5. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02
- [SDR UPS06247461](https://openairdocs.org/sdr/UPS06247461), Jul 6, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 950 RBL 51-56. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06 AND 53-1001. FLOORBEAM TOP CHORD
- [SDR UPS06247455](https://openairdocs.org/sdr/UPS06247455), Jul 6, 2006: PANEL. DELAMINATED. INSPECTION TYPE:C LT WING UPPER SURFACE PANEL FWD OF NR 5 AND 6 SPOILERS DELAM AT PREVIOUS REPAIR. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-40-20. PANEL REPL
- [SDR UPS06247430](https://openairdocs.org/sdr/UPS06247430), Jul 6, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 420 RBL 52-55. SPLICE ANGLE AND FILLER INSTALLED IAW SRM 53-10-8.
- [SDR UPS06247384](https://openairdocs.org/sdr/UPS06247384), Jul 6, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE-C CORROSION ON SEAT TRACK TOP BS 418-427 RBL 45.5. SEAT TRACK REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.
- [SDR UPS06247369](https://openairdocs.org/sdr/UPS06247369), Jul 6, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 328 LBL 27-31 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. NEW FLOOBEAM TOP CHORD FABRICAT
- [SDR UPS06247368](https://openairdocs.org/sdr/UPS06247368), Jul 6, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 344 LBL 16-23 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. FLOORBEAM TOMP P CHORD FABRICAT
- [SDR UPS06247354](https://openairdocs.org/sdr/UPS06247354), Jul 6, 2006: FITTING. CRACKED. INSPECTION TYPE: C AND SI CRACKS DETECTED ON BS 740 STR 18R - STR 24R. ON INVESTIGATION CRACKS FOUND TO BE OUTSIDE LIMITS IAW SB 727-53-0062. REFERENCE NRC 1003
- [SDR UPS06247567](https://openairdocs.org/sdr/UPS06247567), Jul 5, 2006: CHANNEL. CORRODED. INSPECTION TYPE:C AFT SUPPORT CHANNEL FOR APU EXHAUST ON THE LOWER SIDE UPPER WING PANEL IS CORRODED. CHANNEL REPLACED IAW SRM 51-20-01.
- [SDR UPS06247383](https://openairdocs.org/sdr/UPS06247383), Jun 11, 2006: SEAT TRACK. CORRODED. INSPECTION TYPE-C CORROSION ON SEAT TRACK, TOP CHORD BS 481 RBL 45.5 CORROSION FOUND OUTSIDE LIMITS IAW SRM 53-10-1. SEAT TRACK AND CONNECT OR REPLACED IAW SRM 
- [SDR UPS06247382](https://openairdocs.org/sdr/UPS06247382), Jun 11, 2006: FLAP TRACK. CORRODED. INSPECTION TYPE-C CORROSION IN NR 5 FLAP TRACK HOLE G. CORROSION REMOVED IAW OHM 57-40-01. MPI CARRIED OUT IAW BSOPM 20-20-0 1. BUSHING FABRICATED IAW EO 20065-
- [SDR UPS05243879](https://openairdocs.org/sdr/UPS05243879), Feb 3, 2005: ANGLE. CRACKED. LT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02.
- [SDR UPS05243890](https://openairdocs.org/sdr/UPS05243890), Feb 2, 2005: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT BS 680 LBL 56 FOUND ON REMOVAL OF FLOOR PANELS FOR DOOR SILL INSPECTION. REPAIR CARRIED OUT IAW SRM 51-10-2, 53-10-8, 51-20-4 AND AAAE
- [SDR UPS05243888](https://openairdocs.org/sdr/UPS05243888), Feb 1, 2005: ANGLE. CRACKED. AFT AIRSTAIRS ANGLE CRACKED AT FORWARD SIDE OF BS 1203 FRAME LT AT S13L. STOP DRILLED CRACK IAW 51-10-1. HFEC CARRIED OUT IAW NDTM PT6 51-00 -00, CRACK CONTAINE
- [SDR UPS05243878](https://openairdocs.org/sdr/UPS05243878), Feb 1, 2005: CASTING. CRACKED. NR 8 SPOILER I/B END HINGE CASTING IS CRACKED AT FASTENER HOLE. HINGE CASTING REPLACED IAW SRM 51-30-2.

All 118: https://openairdocs.org/model/boeing-727-1a7c/reports.md

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