# Service difficulty reports: N277WA, cancelled Aug 26, 2015

A list on [N277WA, cancelled Aug 26, 2015](https://openairdocs.org/deregistered/N277WA-2015-08-26.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 86 reports

- [SDR WRLA20111226529](https://openairdocs.org/sdr/WRLA20111226529.md): Ballast · defective · Dec 26, 2011 · N277WA · Doug MD11 · Passenger Compartment Lighting
  > ELECTRICAL SMOKE SMELL IN A ZONE. PULLED CEILING LIGHTS OUTBOARD CIRCUIT BREAKER AND THE SMELL WENT AWAY. FWD CABIN LIGHT INOP. ITEM PUT IN DMI LOG DMI M33DE2011-214 MEL 33-10-01-01 CAT "C", DUE ON -01-12 C ON BALLAST DISC AND C/B PULLED ON CEILING LIGHT PO
- [SDR WRLA20111118525](https://openairdocs.org/sdr/WRLA20111118525.md): Light · inoperative · Nov 18, 2011 · N277WA · Doug MD11 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING INOP AT 4-6 HJK. ITEM PLACED ON MEL - DMI REF NO NM31101811-103 DUE DATE 28 NOV 2011, PLACARD INSTALLED CAT-C MX CONT NOTIFIED.
- [SDR WRLA20110920510](https://openairdocs.org/sdr/WRLA20110920510.md): Skin · dented · Sep 20, 2011 · N277WA · Doug MD11 · Fuselage Main, Plate/Skin
  > AIRCRAFT DAMAGE FOUND AT SCHEDULE A-6 CHECK INITIAL WALKAROUND, DENT ON FUSELAGE FORWARD OF L-2 DOOR BETWEEN Y715 AND Y736, AT Z27. DENT WAS 4 INCH LONG, 0.750 WIDE, 0.145 DEEP. BEING REPAIRED PER SRM 53-00-01.
- [SDR WRLA20110730497](https://openairdocs.org/sdr/WRLA20110730497.md): Pin · defective · Jul 30, 2011 · N277WA · Doug MD11 · Light System Wiring
  > FLOOR EMERGENCY LIGHTS, ZONE B, LIT, SEAT 19D AND FWD INOP. CLEANED ALL CONNECTIONS ON FLOOR AND REPLACED AP5660023 PINS ON WIRES FRH-20WH. LIGHTS CHECK NORMAL PER MM 33-52, TROBLESHOOTING PER WDM 33-52-06.
- [SDR WRLA20110308474](https://openairdocs.org/sdr/WRLA20110308474.md): Fan · faulty · Mar 8, 2011 · N277WA · Doug MD11 · Air Distribution Fan
  > MX IS INVESTIGATING THE ODOR OF ELECTRICAL BURNING IN THE CABIN. NO SMOKE, ONLY A SMELL. PAX BOARDING IS BEING DELAYED FOR THIS. FOUND NR 2 RECIRC FAN AT FAULT.
- [SDR WRLA20101217456](https://openairdocs.org/sdr/WRLA20101217456.md): Battery Pack · faulted · Dec 17, 2010 · N277WA · Doug MD11 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL: NR 1 BATTERY PACK FAULTED. REMOVED AND REPLACED NR 1 BATTERY PACK.
- [SDR WRLA20101206455](https://openairdocs.org/sdr/WRLA20101206455.md): Light · inoperative · Dec 6, 2010 · N277WA · Doug MD11 · Emergency Lighting
  > DURING T-10 FOUND EMERGENCY FLOOR LIGHTING INOP FOR B ZONE ROW 14 THRU 18 LT SIDE.
- [SDR WRLA20100619418](https://openairdocs.org/sdr/WRLA20100619418.md): Battery Pack · failed · Jun 19, 2010 · N277WA · Doug MD11 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL NR 3 BATTERY. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY SUPPLY IAW MD-11 AMM 33-51-01. OPS CHECK GOOD.
- [SDR WRLA20100616414](https://openairdocs.org/sdr/WRLA20100616414.md): Shear Tie · corroded · Jun 16, 2010 · N277WA · Doug MD11 · Fuselage Internal Mounting Structure
  > CORROSION - STA 1986 L50L TO L50R, LOWER SHEAR TIE P/N AGA8007-9 CORROSION. NRC U05110 ISSUED.
- [SDR WRLA20100607417](https://openairdocs.org/sdr/WRLA20100607417.md): Web · cracked · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > CRACK - IN CTR CARGO AT STA 1841 X = -62 VERTICAL WEB P/N AGA7125-3 CRACK. NRC U05084 ISSUED.
- [SDR WRLA20100607416](https://openairdocs.org/sdr/WRLA20100607416.md): Stop Fitting · cracked · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Main, Structure
  > CRACK - IN CTR CARGO STA 1841 X=-62 STOP FITTING P/N AGA71971 CRACK. NRC U05083 ISSUED.
- [SDR WRLA20100607415](https://openairdocs.org/sdr/WRLA20100607415.md): Frame · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Main, Frame
  > CORROSION - STA 1986 L50L TO L50R LOWER FRAME CORROSION, NRC U05111 ISSUED.
- [SDR WRLA20100607413](https://openairdocs.org/sdr/WRLA20100607413.md): Tee Fitting · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > CORROSION - 1EA TEE P/N AGA800219 LOC STA1975 BETWEEN L50L AND L50R CORROSION, NRC U05072 ISSUED.
- [SDR WRLA20100607412](https://openairdocs.org/sdr/WRLA20100607412.md): Cargo Track · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION - MAIN DECK FLOOR STA 495 X=-75 RT CURVED SEAT TRACK CORROSION.
- [SDR WRLA20100607411](https://openairdocs.org/sdr/WRLA20100607411.md): Seat Track · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > STA 495 X=75 LT CURVED SEAT TRACK CORRODED.
- [SDR WRLA20100607410](https://openairdocs.org/sdr/WRLA20100607410.md): Seat Track · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT X=785 Y=104 SEAT TRACK S4929148 CORROSION.
- [SDR WRLA20100607409](https://openairdocs.org/sdr/WRLA20100607409.md): Skin · cracked · Jun 7, 2010 · N277WA · Doug MD11 · Nacelle/Pylon, Plate/Skin
  > CRACKED NR 2 INLET LIP OUTER SKIN CRACK AT 5-7 O'CLOCK.
- [SDR WRLA20100607408](https://openairdocs.org/sdr/WRLA20100607408.md): Skin · dented · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Main, Plate/Skin
  > DENT AT STA 430-440 L36R-S38R DENT ON SKIN.
- [SDR WRLA20100607407](https://openairdocs.org/sdr/WRLA20100607407.md): Skin · cracked · Jun 7, 2010 · N277WA · Doug MD11 · Nacelle/Pylon, Plate/Skin
  > CRACK AT NR 2 ENG INLET LIP INNER SKIN INNER SURFACE CRACK AT 6 O'CLOCK.
- [SDR WRLA20100607406](https://openairdocs.org/sdr/WRLA20100607406.md): Pan · corroded · Jun 7, 2010 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > CORROSION AT STA 19 S51L-51R WASTE TANK DRAIN PAN CORROSION.
- [SDR WRLA20100506356](https://openairdocs.org/sdr/WRLA20100506356.md): Battery Pack · discharged · May 6, 2010 · N277WA · Doug MD11 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED NR 4 BATTERY PACK. REMOVED AND REPLACED NR 4 BATTERY PACK.
- [SDR WRLA2009195](https://openairdocs.org/sdr/WRLA2009195.md): Engine · failed · Jul 21, 2009 · N277WA · Doug MD11 · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT, NR 1 ENGINE FAILED CAUSING DAMAGE TO THE LEFT INBOARD AILERON AND LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE. REPLACED NR 1 ENGINE, LEFT INBOARD AILERON, AND LEFT OUTBOARD SECTION OF THE HORIZONTAL STABILIZER LEADING EDGE.
- [SDR WRLA2009189](https://openairdocs.org/sdr/WRLA2009189.md): Engine · vibration · Jul 13, 2009 · N277WA · Doug MD11 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE HI VIBRATION/LOW RPM IN INITIAL CLIMB OUT. HIGH EGT 917C. DURING SHUTDOWN ENGINE FIRE AGENT DISCHARGED.
- [SDR WRLA2009092](https://openairdocs.org/sdr/WRLA2009092.md): Floor Support · corroded · Mar 30, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CORROSION ON THE PANEL SUPPORT OF CABIN FLOOR AT STA Y=860 & X=61 (REF EGAT N/R U05037). REMOVED THE DAMAGED PANEL SUPPORTS PER MD-11 SRM 51-35-01 VOL 2 REV 40. FABRICATE NEW SUPPORT IAW EGAT EI W2009P53B-374 REV 0
- [SDR WRLA2009091](https://openairdocs.org/sdr/WRLA2009091.md): Floor Support · corroded · Mar 30, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CORROSION ON THE PANEL SUPPORT OF CABIN FLOOR AT STA Y=775 & X=85 (REF EGAT N/R U05038). REMOVED THE DAMAGED PANEL SUPPORTS PER MD-11 SRM 51-35-01 VOL 2 REV 40. REPLACE NEW SUPPORT PER MD-11 SRM 51-35-01 VOL 2 REV 4
- [SDR WRLA2009089](https://openairdocs.org/sdr/WRLA2009089.md): Web · cracked · Mar 30, 2009 · N277WA · Doug MD11 · Nacelle/Pylon Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 1 ENG PYLON INTERNAL WEB CRACK AT STA 300 (REF GET N/R U05024). REPAIRED THIS CRACKED AREA PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40 AND JOB CARD ATTACH SHEET 079586. JOB COMPLETED AND CONDITION CHECK NO
- [SDR WRLA2009090](https://openairdocs.org/sdr/WRLA2009090.md): Doubler · cracked · Mar 30, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON THE DB DOUBLER FASTENER AREA OF THE LEFT WING OUTBOARD FIXED CAVITY AT STA XOS627 (REF EGAT N/R U05035). REPAIR THIS CRACKED AREA B PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. PERFORM ET INSPECTION FOR CUTOU
- [SDR WRLA2009088](https://openairdocs.org/sdr/WRLA2009088.md): Angle · cracked · Mar 28, 2009 · N277WA · Doug MD11 · Nacelle/Pylon Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 3 ENG PYLON INTERNAL ANGLE AT STA 180 (REF GET N/R U05032). REPLACED THE INTERNAL ANGLE PER MD-11 SRM 51-35-01 VOL 2 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA2009087](https://openairdocs.org/sdr/WRLA2009087.md): Stiffener · cracked · Mar 28, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF LT WING FIXED L/E UPPER PNL 516ET (REF EGAT N/R U05031). REMOVED THE DAMAGED STIFFENERS (ARB2440-503/503) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT EN
- [SDR WRLA2009086](https://openairdocs.org/sdr/WRLA2009086.md): Stiffener · cracked · Mar 28, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF RT WING FIXED L/E UPPER PNL 616ET (REF EGAT N/R U05027). REMOVED THE DAMAGED STIFFENERS (ARB2440-504/506) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT EN
- [SDR WRLA2009085](https://openairdocs.org/sdr/WRLA2009085.md): Rib · cracked · Mar 28, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON RIGHT WING FIXED L/E CAVITY XOS1025 - LOWER RIB CRACKED FROM FASTENERS AREA (REF EGAT N/R U50534). REPAIR THIS CRACKED RIB PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL
- [SDR WRLA2009084](https://openairdocs.org/sdr/WRLA2009084.md): Seat Track · corroded · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C3 CHECK IN TPE INSPECTION FOUND SEAT TRACK CORROSION AT STA 859. REPAIRED THIS CORRODED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA2009083](https://openairdocs.org/sdr/WRLA2009083.md): Door · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Landing Gear Doors
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON FLIPPER DOOR FWD EDGE OF RT MLG GR - ABOUT.5 INCH (REF EGAT N/R U05029). REMOVED THIS CRACKED FLIPPER DOOR PER AMM 32-14-08-000-801, REPAIRED THE FLIPPER DOOR IAW SRM VOL 1 52-10-00 FIG 18 REV 40, REINSTALLED
- [SDR WRLA2009082](https://openairdocs.org/sdr/WRLA2009082.md): Door · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Landing Gear Doors
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON FLIPPER DOOR FWD UPPER EDGE OF LT MLG GR - ABOUT.5 INCH (REF EGAT N/R U05028). REMOVED THIS CRACKED FLIPPER DOOR PER AMM 32-14-08-000-801, REPAIRED THE FLIPPER DOOR IAW SRM VOL 1 52-10-00 FIG 18 REV 40, RE-IN
- [SDR WRLA2009081](https://openairdocs.org/sdr/WRLA2009081.md): Step · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON STEP PANEL OF AVIONICS COMPARTMENT LADDER AT STA 348 (REF EGAT N/R U05026). REMOVED AND FABRICATED NEW PANEL IAW EGAT EI W2009P57B-351 REV 00, INSTALLED PANEL IAW SRM 51-35-01 VOL 2 REV 40, AND JOB COMPLETE & C
- [SDR WRLA2009080](https://openairdocs.org/sdr/WRLA2009080.md): Support Bracket · deformed · Mar 21, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND DEFORM ON THE GND JACKS SUPPORT BRACKET INSIDE OF RT WING FUELING STATION (REF EGAT N/R U05025). REMOVED BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLED THI
- [SDR WRLA2009079](https://openairdocs.org/sdr/WRLA2009079.md): Support Bracket · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR PANEL SUPPORT BRACKET OF RIGHT WING T/E AT STA XOSP465.027 (REF EGAT N/R U05023). REMOVED SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLE
- [SDR WRLA2009078](https://openairdocs.org/sdr/WRLA2009078.md): Doubler · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789 (REF EGAT N/R U05018). REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INST
- [SDR WRLA2009077](https://openairdocs.org/sdr/WRLA2009077.md): Doubler · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INSTALLED THIS DOUBLER IAW
- [SDR WRLA2009076](https://openairdocs.org/sdr/WRLA2009076.md): Doubler · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-355 REV 00, INSTALLED THIS DOUBLER IAW SRM
- [SDR WRLA2009075](https://openairdocs.org/sdr/WRLA2009075.md): Doubler · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-357 REV 00, INSTALLED THIS DOUBLER IAW SRM
- [SDR WRLA2009074](https://openairdocs.org/sdr/WRLA2009074.md): Step · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON RT STEP SUPPORT OF CAC COMPARTMENT. REMOVED SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-339 REV 00, INSTALLED THIS SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV
- [SDR WRLA2009073](https://openairdocs.org/sdr/WRLA2009073.md): Rib · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR CHORD OF LT WING FIXED L/E NOSE CAVITY NEARBY FASTENER AT STA XOS546. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-338 REV 00, INSTALLED THIS DO
- [SDR WRLA2009072](https://openairdocs.org/sdr/WRLA2009072.md): Fitting · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON 1EA RT CLIP OD CAC COMPARTMENT. REMOVE THIS DAMAGED CLIP PER SRM 51-33-01 VOL 2 REV 40, FABRICATE THIS CLIP PER EGAT EI W2009P53B-354 REV 00, INSTALLED THIS CLIP PER SRM 51-33-01 VOL 2 REV 40, AND JOB COMPLETED
- [SDR WRLA2009071](https://openairdocs.org/sdr/WRLA2009071.md): Seal · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LEFT WING T/E BEAM SEAL LAND Y=1474 Z=-100. REPLACE THIS CRACK SEAL LAND IAW SRM 51-35-01 AND 51-33-01 VOL 2 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA2009070](https://openairdocs.org/sdr/WRLA2009070.md): Rib · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON RT RIB OF RT MLG GR JAMB INSTALLED AT Y-1474 Z=-100. REMOVE RT RIB OF RT MLG JAMB PER SRM 51-33-01 VOL 2 REV 40, INSTALLED NEW RIB PER MD-11 SRM 31-33-01 VOL 2 REV 40, JOB COMPLETED AS NORMAL.
- [SDR WRLA2009069](https://openairdocs.org/sdr/WRLA2009069.md): Seat Track · corroded · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C3 CHECK IN TPE INSPECTION FOUND CABIN SEAT TRACK HAD CORROSION AT STA 846 X=43. REPAIRED THIS CORRODED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA2009068](https://openairdocs.org/sdr/WRLA2009068.md): Vane · debonded · Mar 21, 2009 · N277WA · Doug MD11 · Trailing Edge Flaps
  > DURING C3 CHECK IN TPE INSPECTION FOUND LT INBOARD FLAP VANE HAS DISBOND AT XIFH196 AND XIFH249. PER AMM 27-50-22-000-081 & 27-50-24-000-081 REV 63. REMOVED THIS DISBONED FLAP VANE, REPAIRED THE FLAP VANE AS JOB CARD ATTACHMENT SHEET 079554, PER AMM 27-50-22
- [SDR WRLA2009067](https://openairdocs.org/sdr/WRLA2009067.md): Wedge · debonded · Mar 21, 2009 · N277WA · Doug MD11 · Ailerons
  > DURING C3 CHECK IN TPE INSPECTION FOUND EGAT LT OUTBOARD AILERON WEDGE DISBOND AT XOA 842. REMOVE AND CLEANUP AREA. REPAIR THIS WEDGE PER DRAWING SG11570003. CHECK REPAIRED AREA WAS SATISFIED, CALCULATED THE REWORK BALANCE MOMENT IS 66.65 LB-IN PER SRM 57-5
- [SDR WRLA2009063](https://openairdocs.org/sdr/WRLA2009063.md): Fitting · cracked · Mar 21, 2009 · N277WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON 1EA RT CLIP OD CAC COMPARTMENT. REMOVE THIS DAMAGED CLIP PER SRM 51-33-01 VOL 2 REV 40, FABRICATE THIS CLIP PER EGAT EI W2009P53B-354 REV 00, INSTALLED THIS CLIP PER SRM 51-33-01 VOL 2 REV 40, AND JOB COMPLETED

Next page: https://openairdocs.org/deregistered/N277WA-2015-08-26/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N277WA' AND deregistration_id = 'N277WA-2015-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N277WA-2015-08-26/reports

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