# Boeing 727-2A1

- Type: Aircraft model (FAA registry)
- Registry code: 138407F
- Manufacturer (registry): BOEING
- Model: 727-2A1
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 134
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-727-2a1

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 (2)

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 20010406012429I](https://openairdocs.org/incident/20010406012429I), Apr 6, 2001: Boeing 7272A1 (N286SC), Toledo, OH. (-23)Crew declared emergency during taxi for takeoff due to smoke in the cockpit. Aircraft taxied back to ramp without incident. Maintenance found the smoke…
- [Incident 19881017059019I](https://openairdocs.org/incident/19881017059019I), Oct 17, 1988: Boeing 727200 (N214UP), Omaha, NE. Took off and returned twice. Smoke in cockpit due to bad seal between cooling fand duct. Anti ice overheat light.

## Service difficulty reports (502, newest 50)

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

- [SDR C8GA20120406005](https://openairdocs.org/sdr/C8GA20120406005), Apr 3, 2012: GENERATOR. FAILED. AFTER TAKEOFF, ALL COCKPIT LIGHTS FLICKERED FOLLOWED BY NR 2 GENERATOR OVER EXCITATION FOLLOWED BY PHASE IMBALANCE. NR 3 BUSS TIE TRIPPED FOLLOWED BY NR 3 GEN I
- [SDR C8GA20120321004](https://openairdocs.org/sdr/C8GA20120321004), Mar 20, 2012: FLOORBEAM. CORRODED. DURING 18 MONTH CPCP INSPECTION, CORROSION WAS FOUND ON OTBD END OF LT FLOORBEAM AT FS 910, AND WL 70. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED 
- [SDR C8GA2011000009](https://openairdocs.org/sdr/C8GA2011000009), Jun 30, 2011: RELAY. INOPERATIVE. DURING CLIMB OPERATION THE FO'S CDI NEEDLE DID NOT DEVIATE WITH COURSE CHANGES WITH THE VOR SELECTED. ALSO, THE CAPTAINS CDI WAS UNREADABLE ON LOCALIZER, SHOWED
- [SDR C8GA2011000001](https://openairdocs.org/sdr/C8GA2011000001), Mar 23, 2011: CONTROL CABLE. OUT OF ADJUST. DURING APPROACH, WITH THE GEAR LEVER PLACED IN THE DOWN POSITION, THE GREEN LANDING GEAR INDICATION LIGHTS WERE ILLUMINATED AS WELL AS THE RED INDICATION LIGHTS
- [SDR FOTR2102212390](https://openairdocs.org/sdr/FOTR2102212390), Mar 18, 2011: SKIN. DEBONDED. RT WING T/E NR 11 SPOILER UPPER SKIN IS DEBONDED OTBD END. REMOVED DAMAGED AREA DIM 10" X 6.25" IAW SRM 51-40-20 PARA 7,11,14,15 AND FABRICATED FILLER DIM 10" X
- [SDR FOTR2102212391](https://openairdocs.org/sdr/FOTR2102212391), Mar 18, 2011: SKIN. DEBONDED. RT WING T/E NR 13 SPOILER UPPER SKIN IS DISBONDED. REMOVED DAMAGED AREA DIM 12" X 7.75" IAW SRM 51-40-20, PARA 7,11,14,15 AND FABRICATED FILLER DIM 12" X 7.75" 
- [SDR FOTR2102212508](https://openairdocs.org/sdr/FOTR2102212508), Mar 18, 2011: SKIN. DEBONDED. RT ELEVATOR TAB T/E IS DISBONDED. REMOVED DAMAGED AREA DIM 6.5" X 6.5" IAW SRM 51-40-20, PAGE 12-14, PARA 7. FABRICATED REPAIR FILLER 6.5" X 6.5" AND DOUBLER DI
- [SDR FOTR2102212576](https://openairdocs.org/sdr/FOTR2102212576), Mar 15, 2011: TAB. DEBONDED. LT OTBD AILERON TAB HAS DISBOND ON INBD END. REMOVED DAMAGE ON AILERON INBD END DIM 7" X 3" IAW SRM 51-40-20, PAGE 12, PARA 7. FABRICATED REPAIR CORE IAW SRM 51
- [SDR FOTR2102212575](https://openairdocs.org/sdr/FOTR2102212575), Mar 15, 2011: TAB. DEBONDED. LT OTBD AILERON TAB HAS DISBOND ON OTBD END. REMOVED DAMAGE ON AILERON TAB DIM 2" X 2" IAW SRM 51-40-20, PAGE 12, PARA 7. FABRICATED REPAIR CORE IAW SRM 51-40-2
- [SDR FOTR2102212307](https://openairdocs.org/sdr/FOTR2102212307), Mar 15, 2011: SPAR. CRACKED. NR 1 SLAT ACTUATOR OTBD MOUNT SUPPORT ON LT WING FRONT SPAR CRACKED. REMOVED CRACKED WEB FROM L/E LT WING SLAT STA 398.1 IAW SRM 51-30-2. FABRICATED NEW WEB FRO
- [SDR FOTR2102212335](https://openairdocs.org/sdr/FOTR2102212335), Mar 14, 2011: TAB. DEBONDED. LT WING OTBD AILERON TAB IS DISBONDED AT 4 EA PLACES. REMOVED DAMAGED ON LT OTBD AILERON TAB 30" FROM OTBD END, DIM 7" X 4" IAW SRM 51-40-20-PAGE 12, PARA 7. FA
- [SDR FOTR2102212574](https://openairdocs.org/sdr/FOTR2102212574), Mar 14, 2011: TAB. DEBONDED. LT OTBD AILERON TAB HAS DISBOND ON UPPER SURFACE 15" FROM OTBD END. REMOVED DAMAGED ON LT OTBD AILERON TAB, FABRICATED REPAIR CORE, BONDED REPAIR CORE, FABRICAT
- [SDR FOTR2102212539](https://openairdocs.org/sdr/FOTR2102212539), Mar 14, 2011: SKIN. DEBONDED. RT INBD MID FLAP T/E UPPER OTBD END HAS AREA DISDOND. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR 7, REPAIRED RT INBD MID-F
- [SDR FOTR2102212489](https://openairdocs.org/sdr/FOTR2102212489), Mar 14, 2011: SKIN. DEBONDED. RT WING NR 11 SPOILER UPPER SKIN IS DISBONDED INBD END. REMOVED DAMAGED, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, FABBED REPAIR PARTS, 2 PCS, 1 FILLER
- [SDR FOTR2102212487](https://openairdocs.org/sdr/FOTR2102212487), Mar 14, 2011: WEDGE. DEBONDED. LT INBD FLAP T/E WEDGE, UPPER INBD END IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR7, REPAIRED LT INBD MID FLA
- [SDR FOTR2102212485](https://openairdocs.org/sdr/FOTR2102212485), Mar 14, 2011: WEDGE. DEBONDED. RT INBD MID FLAP T/E WEDGE, LWR INBD NR 1 TRACK IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20 PARA NR 7, REPAIRED RT INB
- [SDR FOTR2102212402](https://openairdocs.org/sdr/FOTR2102212402), Mar 14, 2011: SKIN. GOUGED. RT WING NR 5 SLAT T/E SKIN BY INBD HOOK IS GOUGED. CLEANED AREA ON NR 5 SLAT IAW MM12-40-00, FOUND AREA OF GOUGE TO BE OUT OF LIMITS IAW SRM 57-50-1, FIG 2. FRA
- [SDR FOTR2102212361](https://openairdocs.org/sdr/FOTR2102212361), Mar 14, 2011: SEAT TRACK. CORRODED. BL-O-SEAT TRACK CORRODED STA 610. REMOVED BL-O- SEAT TRACK STA 590-730 IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK FROM 40456, 7178T6511 PO 9007703 DIM 120" IAW S
- [SDR FOTR2102212349](https://openairdocs.org/sdr/FOTR2102212349), Mar 14, 2011: SKIN. DAMAGED. DRILL STARTS IN FUSELAGE AT STR 2R STA 400. FOUND AREA TO HAVE A SMALL DELAMINAION ON TEAR STRAP AT STR 2R-3R, L1 = .5 PERCENT = 5 PERCENT, FOUND TO BE WITHIN L
- [SDR FOTR2102212339](https://openairdocs.org/sdr/FOTR2102212339), Mar 14, 2011: SKIN. CRACKED. LT WING OTBD FLAP, AFT FLAP HAS CRACK AT L/E, JUST INBD OF MOST OTBD TRACK. CUT OUT DAMAGED AREA DIM 1.2" X 1" ON LT WING OTBD FLAP L/E IAW SRM 57-50-4, FIG 9. 
- [SDR FOTR2102212322](https://openairdocs.org/sdr/FOTR2102212322), Mar 14, 2011: FENCE. CRACKED. 4 SLAT FENCE CRACKED LWR DRAIN HOLE SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-9 PARA. 7. APPLIED REPAIR TO PREPPED AREA IAW SRM 51-40-9, PARA 7 AND REFINIS
- [SDR FOTR2102212315](https://openairdocs.org/sdr/FOTR2102212315), Mar 14, 2011: SKIN. CRACKED. NR 2 SLAT LWR SKIN CRACKED AT INBD TRACK TO SKIN ATTACH FASTENERS. CUT OUT DAMAGED AREA DIM 3.3" X 5.55" IAW SRM 57-50-3, FIG 1. FABRICATED REPAIR DOUBLER FROM 
- [SDR FOTR2102212546](https://openairdocs.org/sdr/FOTR2102212546), Mar 14, 2011: SKIN. DENTED. EVALUATE EXISTING DENT ON FUSELAGE SKIN AT BS 1336 ABOVE STRINGER 26L. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1, FIG 1, DETAIL 2. DEBONDED A
- [SDR C8GA201000009](https://openairdocs.org/sdr/C8GA201000009), Apr 16, 2010: BUSHING. DEFECTIVE. FLT 716 FROM CVG TO MEM. WHILE CLIMBING THROUGH 15,000 FEET ACCELERATING THROUGH 280 KTS A HIGH FREQUENCY AERODYNAMIC VIBRATION DEVELOPED. CREW WAS UNABLE TO ID
- [SDR FOTR20006NR2095](https://openairdocs.org/sdr/FOTR20006NR2095), Feb 24, 2010: SKIN. DENTED. (FOTR) DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006. N/R 02095- R & R PREVIOUS REPAIR TO LT FUSELAGE SKIN AT STA 1319 STR 9L IAW SRM 53-30
- [SDR FOTR20006NR2059](https://openairdocs.org/sdr/FOTR20006NR2059), Feb 13, 2010: SKIN. DEBONDED. RT WING INBD AILERON TAB LOWER SURFACE DISBONDED 22 INCHES FROM OTBD END. REPAIRED ON FASI WO 20006, N/R 02059. REPAIRED RT WING INBD AILERON TAB AT WBL 280 BY 
- [SDR FOTR20006NR2054](https://openairdocs.org/sdr/FOTR20006NR2054), Feb 12, 2010: STRUCTURE. CRACKED. RT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION 
- [SDR FOTR20006NR2033](https://openairdocs.org/sdr/FOTR20006NR2033), Feb 10, 2010: SKIN. DEBONDED. RT WING NR 9 SPOILER LOWER SURFACE HAS DISBONDED DOUBLER JUST AFT OF ACTUATOR ATTACH FITTING. REPAIRED ON FASI WO 20006, N/R 02033. REPAIRED RT WING NR 9 SPOILE
- [SDR FOTR20006NR2031](https://openairdocs.org/sdr/FOTR20006NR2031), Feb 10, 2010: SKIN. DEBONDED. LT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFA
- [SDR FOTR20006NR2028](https://openairdocs.org/sdr/FOTR20006NR2028), Feb 10, 2010: SKIN. PUNCTURED. RT ELEVATOR LOWER SKIN WORN THRU AT ELEV STA 78 NEAR CENTER OF ELEVATOR. REPAIRED ON FASI WO 20006, N/R 02028. INSTALLED REPAIR DOUBLER ON RIGHT ELEVATOR LOWER 
- [SDR FOTR20006NR2027](https://openairdocs.org/sdr/FOTR20006NR2027), Feb 9, 2010: FRAME. DAMAGED. UPPER CABIN FRAME DAMAGED AT BS 380 STR 5L. REPAIRED ON FASI WO 20006. N/R 02027. INSTALLED REPAIR ANGLE TO FUSELAGE FRAME AT BS 380, STR 5L IAW B727 SRM 53-10-
- [SDR FOTR20006NR2023](https://openairdocs.org/sdr/FOTR20006NR2023), Feb 8, 2010: SKIN. DEBONDED. RT OTBD AILERON TAB, UPPER SURFACE INBD END HAS AREA OF DISBOND. REPAIRED ON FASI WO 20006. N/R 02023, INSTALLED HOT BONDED REPAIR TO RT OTBD AILERON TAB UPPER 
- [SDR FOTR20006NR2021](https://openairdocs.org/sdr/FOTR20006NR2021), Feb 8, 2010: SKIN. PUNCTURED. RT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-
- [SDR FOTR20006NR2020](https://openairdocs.org/sdr/FOTR20006NR2020), Feb 8, 2010: STRINGER CLIP. PUNCTURED. FRAME TO STR. BRACKET HAS HOLE IN RADIUS AT STA. 672 STR. 13L. REPAIRED ON FASI W/O NR 20006, N/R 02020- R & R SUPPORT ANGLE AT STA 672 STR 13L IAW SRM 51-30-2,
- [SDR FOTR20006NR2016](https://openairdocs.org/sdr/FOTR20006NR2016), Feb 8, 2010: SKIN. GOUGED. LT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.
- [SDR FOTR20006NR2013](https://openairdocs.org/sdr/FOTR20006NR2013), Feb 8, 2010: WEDGE. DELAMINATED. RT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERO
- [SDR FOTR20006NR2012](https://openairdocs.org/sdr/FOTR20006NR2012), Feb 8, 2010: SKIN. DELAMINATED. RT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/
- [SDR FOTR20006NR2011](https://openairdocs.org/sdr/FOTR20006NR2011), Feb 8, 2010: SKIN. DELAMINATED. RT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW
- [SDR FOTR20006NR1992](https://openairdocs.org/sdr/FOTR20006NR1992), Feb 6, 2010: SKIN. DENTED. RT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT 
- [SDR FOTR20006NR1984](https://openairdocs.org/sdr/FOTR20006NR1984), Feb 5, 2010: STRINGER. CORRODED. AFT AIRSTAIR AT BS 1323 CENTER STRINGER AT LOWER END CORRODED. REPAIRED ON FSAI W/O NR 20006, N/R 01984. REPAIRED STRINGER AT AFT STAIRS STA 1323 IAW B727 SRM 5
- [SDR FOTR20006NR1976](https://openairdocs.org/sdr/FOTR20006NR1976), Feb 5, 2010: WEB. CRACKED. LT SIDE OF FUSELAGE INTERIOR WEB CRACKED JUST ABOVE NR 2 ENG "S" DUCT AT BS 1303. REPAIRED ON FASI W/O NR 20006, N/R 01976. INSTALLED REPAIR DOUBLER TO CRACKED 
- [SDR FOTR20006NR1972](https://openairdocs.org/sdr/FOTR20006NR1972), Feb 5, 2010: DOUBLER. CRACKED. L1 DOOR UPPER HINGE SKIN DOUBLER CRACKED LOWER CORNER. REPAIRED ON FASI W/O NR 20006, N/R 01972. REPLACED EXTERNAL DOUBLER AT LEFT FORWARD ENTRY DOOR UPPER HING
- [SDR FOTR20006NR1971](https://openairdocs.org/sdr/FOTR20006NR1971), Feb 5, 2010: SHEAR TIE. CRACKED. STA 600 STR 16L SHEAR TIE CRACKED. REPAIRED ON FASI W/O NR 20006, NR 01971, REPLACED CRACKED SHEAR TIE AND DOUBLER AT BS 680, STR 16L IAW B727 SRM 53-20-2 FIG 3
- [SDR FOTR20006NR1969](https://openairdocs.org/sdr/FOTR20006NR1969), Feb 5, 2010: STRINGER CLIP. CRACKED. STA 700 STR. 16L STR CLIP CRACKED. REPAIRED ON FASI W/O NR 20006,NR 01969. REPLACED CRACKED STRINGER CLIPS AT BS 700 STR 16L IAW DRAWING NR 66-11809 REV B AND B
- [SDR FOTR20006NR1965](https://openairdocs.org/sdr/FOTR20006NR1965), Feb 5, 2010: FRAME. DENTED. STA 720A STR 16R FRAME IS DENTED. REPAIRED ON FASI W/O NR 20006, NR 01965. INSTALLED REPAIR DOUBLER TO FRAME AT BS 720A, STR 16R, DUE TO DENT, IAW B727 SRM 53-1
- [SDR FOTR20006NR1962](https://openairdocs.org/sdr/FOTR20006NR1962), Feb 5, 2010: FRAME. GOUGED. LEFT UPPER CABIN FRAME GOUGED AT BS 670 BETWEEN STR 5L AND 6L. REPAIRED ON FASI W/O 20006, N/R 01962. REMOVED AND REPLACED FUSELAGE FRAME AT BS 670 BETWEEN STR 
- [SDR FOTR20006NR1862](https://openairdocs.org/sdr/FOTR20006NR1862), Feb 4, 2010: FRAME. BENT. STA 420 FRAME BENT AT STR 7R. REPAIRED ON FASI W/O NR 20006, NR 01862. INSTALLED REPAIR DOUBLER TO FRAME AT BS 420, STR 7R, DUE TO DENT, IAW B727 SRM 53-10-2 FI
- [SDR FOTR20006NR1850](https://openairdocs.org/sdr/FOTR20006NR1850), Feb 4, 2010: STRUCTURE. PUNCTURED. RT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SUR
- [SDR FOTR20006NR5780](https://openairdocs.org/sdr/FOTR20006NR5780), Feb 3, 2010: WEB. CORRODED. LT MOP SILL CORRODED UNDERSIDE STA 1130 BELOW FLOOR. REPAIRED ON FASI WO 20006, N/R 05780. REMOVED AND REPLACED WEB BETWEEN STA 1110 TO 1130 IAW B727 SRM 53-10-
- [SDR FOTR20006NR5718](https://openairdocs.org/sdr/FOTR20006NR5718), Feb 3, 2010: FLOORBEAM. CRACKED. MAIN CABIN OVERWING FLOORBEAM T-CHORD CRACKED AT BS 760 RBL.45.5. REPAIRED ON FASI W/O NR 20006, N/R 05718. REMOVED AND REPLACED MAIN CABIN FLOORBEAM T-CHORD AT

All 502: https://openairdocs.org/model/boeing-727-2a1/reports.md

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