# Service difficulty reports: N271WA, cancelled Nov 24, 2014

A list on [N271WA, cancelled Nov 24, 2014](https://openairdocs.org/deregistered/N271WA-2014-11-24.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 3 · 144 reports

- [SDR WRLA20130401588](https://openairdocs.org/sdr/WRLA20130401588.md): Connector · unsecure · Apr 1, 2013 · N271WA · Doug MD11 · Light System Wiring
  > UPON ARRIVAL AT STATION KTIK, FWD ZONE EMERGENCY LIGHTS CAME ON AND WOULD NOT SHUT OFF. PROBLEM WAS CORRECTED BY RESECURING OF THE EMERGENCY BATTERY CONNECTOR. NO FURTHER FAULTS NOTED.
- [SDR WRLA20130111578](https://openairdocs.org/sdr/WRLA20130111578.md): Unknown · odor · Jan 11, 2013 · N271WA · Doug MD11 · Air Distribution System
  > ELECTRICAL BURNING ODOR DURING, SMOKE/ FUME CHECKLIST COMPLIED WITH, ODOR DISSIPATED WHEN ELEC/AIR SWITCH PLACED TO THE 3/1 POSITION. MAINTENANCE RETURNED ALL ELECTRICAL SYSTEMS TO NORMAL ACCOMPLISHED INSPECTION OF THE FWD AVIONICS BAY ELECTRICAL BOXES NO AB
- [SDR WRLA20121117564](https://openairdocs.org/sdr/WRLA20121117564.md): Web · cracked · Nov 17, 2012 · N271WA · Doug MD11 · Fuselage Miscellaneous Structure
  > CRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT WEB PN: ACA3804-27 AT AIR CONDITION DOOR JAMB, STA Y=555, L-36. REPAIRED PER EGAT EI: W2012A53B-2619, R00,R01. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121117563](https://openairdocs.org/sdr/WRLA20121117563.md): Skin · cracked · Nov 17, 2012 · N271WA · Doug MD11 · Nacelle/Pylon, Plate/Skin
  > CRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACKS ON RIGHT FAIRING SKIN OF TAIL PYLON LWR AFT SECTION. REPAIRED PER EGAT EI: W2012A54B-2664,R01. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121117562](https://openairdocs.org/sdr/WRLA20121117562.md): Seat Track · corroded · Nov 17, 2012 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CABIN SEAT TRACK CORROSION AT STA 1351, X= -75.25. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-52, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121117561](https://openairdocs.org/sdr/WRLA20121117561.md): Seat Track · corroded · Nov 17, 2012 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CABIN SEAT TRACK CORROSION AT STA 460, X= -27.5. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-52, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121117559](https://openairdocs.org/sdr/WRLA20121117559.md): Longeron · corroded · Nov 17, 2012 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > CORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND LONGERON 51LT LOCATED AT STA 1701 TO STA 1721 ON CENTER CARGO COMPT. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-05, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121117558](https://openairdocs.org/sdr/WRLA20121117558.md): Cargo Track · corroded · Nov 17, 2012 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND LONGERON SURFACE LOCATED ON CENTER CARGO UNDER FLOOR AT LONGERON 51 LEFT AT STA 1601 TO STA 1621. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-05, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121116565](https://openairdocs.org/sdr/WRLA20121116565.md): Skin · dented · Nov 16, 2012 · N271WA · Doug MD11 · Fuselage Main, Plate/Skin
  > DENT - DURING C04 CHECK, EGAT MECHANIC FOUND TWO DENTS ON FUSELAGE SKIN BETWEEN STA Y -495 AND Y=515, L-25L AND L-28L. REPAIRED PER EGAT EI: W2012A53B-2668, R00, R01, R02, R03. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20121116560](https://openairdocs.org/sdr/WRLA20121116560.md): Frame · cracked · Nov 16, 2012 · N271WA · Doug MD11 · Fuselage Main, Frame
  > CRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACKS ON FRAME (P/N: AGA7098-3) AND CAP (AGA7098-7) AT STA Y=1841.
- [SDR WRLA20121110566](https://openairdocs.org/sdr/WRLA20121110566.md): Web · corroded · Nov 10, 2012 · N271WA · Doug MD11 · Fuselage Miscellaneous Structure
  > CORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CORROSION ON HORIZONTAL WEB (P/N: NCA6048-3) OF NOSE WHEEL WELL AT STA Y=515. REPAIRED PER EGAT EI:W2012A53B-2699, R00, R01, R02. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20110826509](https://openairdocs.org/sdr/WRLA20110826509.md): Battery · discharged · Aug 26, 2011 · N271WA · Doug MD11 · Emergency Lighting
  > EMER LT 1L TEST FAIL. REMOVED AND REPLACED EMER LIGHT BATT SYSTEM, OPS CHECK GOOD MM 33-50.
- [SDR WRLA20110720494](https://openairdocs.org/sdr/WRLA20110720494.md): Battery Pack · failed · Jul 20, 2011 · N271WA · Doug MD11 · Emergency Lighting
  > NR 1 EMERGENCY BATTERY FAILED TEST. REMOVED AND REPLACED NR 1 EMERGENCY LT BATTERY PACK ALL TEST PASSED.
- [SDR WRLA20110506479](https://openairdocs.org/sdr/WRLA20110506479.md): Spacer · cracked · May 6, 2011 · N271WA · Doug MD11 · Wing Miscellaneous Structure
  > CRACK: LT WINGLET AFT FITTING SPACER PN: ARB7602-3 CRACK, NRC U05087 ISSUED.
- [SDR WRLA20110506478](https://openairdocs.org/sdr/WRLA20110506478.md): Support Fitting · cracked · May 6, 2011 · N271WA · Doug MD11 · Trailing Edge Flaps
  > CRACK ON INBD HINGE SUPPORT OF LT OTBD T/E FLAP.
- [SDR WRLA20110506477](https://openairdocs.org/sdr/WRLA20110506477.md): Fitting · cracked · May 6, 2011 · N271WA · Doug MD11 · Wing Miscellaneous Structure
  > RT LOWER WINGLET FWD FITTING CRACKED.
- [SDR WRLA20091003251](https://openairdocs.org/sdr/WRLA20091003251.md): Support Fitting · cracked · Oct 3, 2009 · N271WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FOUND CRACK ON CABIN FLOOR FRAME SUPPORT CLIP AT STA Y=1119, X=-65. FABRICATE PART IAW EI W2009P53B-1110 REV 00. REPLACE GUSSET PER MD-11 61-35-02 REV 41.
- [SDR WRLA20090926247](https://openairdocs.org/sdr/WRLA20090926247.md): Skin · delaminated · Sep 26, 2009 · N271WA · Doug MD11 · Trailing Edge Flaps
  > DURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE LEFT WING INBOARD FLAP VANE LOWER SKIN DISBOND (7 *17) AT XIFH 192. CUT OUT DENT SKIN SANDED AROUND THE AREA AND CLEAN BONDED FIBERGLASS FABRIC USE WET LAY-UP AT 200 OF CURE FOR 220 MINS WITH VACUUM PRESSUR
- [SDR WRLA20090926246](https://openairdocs.org/sdr/WRLA20090926246.md): Skin · delaminated · Sep 26, 2009 · N271WA · Doug MD11 · Trailing Edge Flaps
  > DURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE RIGHT WING INBOARD FLAP VANE LOWER SKIN DISBOND 12 *19 AT XIFH210. REMOVED RIGHT WING INBOARD FLAP VANE (J/C ATTACHING SHEET NR 088958 ITEM 01). REPAIRED THE DISBOND DAMAGE AREA IAW EGAT EI NR W2009A57B-113
- [SDR WRLA20090926224](https://openairdocs.org/sdr/WRLA20090926224.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1249, X=107.25. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926222](https://openairdocs.org/sdr/WRLA20090926222.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1121-1127, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV 41.
- [SDR WRLA20090926234](https://openairdocs.org/sdr/WRLA20090926234.md): Beam · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Wing Main, Frame Structure
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LT WING FIXED INNER T/E LOWER BEAM, STA XW200,L=14. JOB COMPLETED IAW EI NR W2009A57B-1122 REV00 AND REV01.
- [SDR WRLA20090926230](https://openairdocs.org/sdr/WRLA20090926230.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 532-559, X=73. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR1 REV41. APPLY PROTECTION COATING MD-11 SRM 51-21-01 REV41.
- [SDR WRLA20090926229](https://openairdocs.org/sdr/WRLA20090926229.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 909-929, X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 52-21-01 REV41.
- [SDR WRLA20090926223](https://openairdocs.org/sdr/WRLA20090926223.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1239-1250, X=-107.25. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.
- [SDR WRLA20090926218](https://openairdocs.org/sdr/WRLA20090926218.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 6-30, X=8.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV41.
- [SDR WRLA20090926216](https://openairdocs.org/sdr/WRLA20090926216.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1870, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 REPAIR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.
- [SDR WRLA20090926250](https://openairdocs.org/sdr/WRLA20090926250.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=3, STA 5-123, L51L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1132 REV00. INSTALL NEW LONGERON SP
- [SDR WRLA20090926249](https://openairdocs.org/sdr/WRLA20090926249.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=2, STA 5-123, L38L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1131 REV 00. INSTALL NEW LONGERON S
- [SDR WRLA20090926248](https://openairdocs.org/sdr/WRLA20090926248.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=1, STA 5-123, L34L. REMOVED DAMAGE LONGERON SPLICE IAW SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1130 REV 00. INSTALL NEW LONGERON SPLICE
- [SDR WRLA20090926245](https://openairdocs.org/sdr/WRLA20090926245.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=2, STA 5-123, L50R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1133 REV 00. INSTALLED NEW LONGERON
- [SDR WRLA20090926241](https://openairdocs.org/sdr/WRLA20090926241.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=1, STA 5-126, L38R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1129 REV00. INSTALL NEW LONGERON SP
- [SDR WRLA20090926240](https://openairdocs.org/sdr/WRLA20090926240.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=1, STA 123, L35R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1128 REV 00. INSTALL NEW LONGERON SPL
- [SDR WRLA20090926239](https://openairdocs.org/sdr/WRLA20090926239.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=4, STA 123, L37L. REMOVED DAMAGE LONGERON SPLICE IAW SRM 51-33-01 REV 41. ABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1127 REV00. INSTALL NEW LONGERON SPLICE IAW
- [SDR WRLA20090926238](https://openairdocs.org/sdr/WRLA20090926238.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CENTER CARGO, L=5, STA 123, L49R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1126 REV 00. INSTALL NEW LONGERON SPL
- [SDR WRLA20090926237](https://openairdocs.org/sdr/WRLA20090926237.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CTR CARGO, L=1, STA 5-123, L44L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1125 REV 00. INSTALL NEW LONGERON SPL
- [SDR WRLA20090926236](https://openairdocs.org/sdr/WRLA20090926236.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CTR CARGO, L=4, STA 123, L49L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1124 REV 00. INSTALL NEW LONGERON SPLICE
- [SDR WRLA20090926235](https://openairdocs.org/sdr/WRLA20090926235.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG, CTR CGO, L=1, STA 5-123, L45L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NO W2009P53B-1123 REV 00. INSTALL NEW LONGERON SPLIC
- [SDR WRLA20090926233](https://openairdocs.org/sdr/WRLA20090926233.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1398, X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR 1 REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV41.
- [SDR WRLA20090926232](https://openairdocs.org/sdr/WRLA20090926232.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1240-1247, 5142 X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51.21.01 REV 41.
- [SDR WRLA20090926231](https://openairdocs.org/sdr/WRLA20090926231.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 830-882, X=8.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926225](https://openairdocs.org/sdr/WRLA20090926225.md): Beam · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Main Landing Gear Strut/Axle/Truck
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN. REMOVED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20-000-908 REV 65. INSTALLED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20
- [SDR WRLA20090926221](https://openairdocs.org/sdr/WRLA20090926221.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 925-968, X=-75.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926220](https://openairdocs.org/sdr/WRLA20090926220.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 840-870, X=-27.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926217](https://openairdocs.org/sdr/WRLA20090926217.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 820-864, X=-8.50. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926214](https://openairdocs.org/sdr/WRLA20090926214.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D FLOOR SUPPORT AT STA 1880, X=36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926211](https://openairdocs.org/sdr/WRLA20090926211.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D CABIN FLOOR SUPPORT, STA 1878 X=-36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.
- [SDR WRLA20090926254](https://openairdocs.org/sdr/WRLA20090926254.md): Longeron Splice · cracked · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON LONGERON SPLICE FITTING, CENTER CARGO, STA 5-123, L4R. PART REPLACED PER WOA EI W2009P53B-1134 REV 00.
- [SDR WRLA20090926219](https://openairdocs.org/sdr/WRLA20090926219.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 457, X=-33.5. CLEAN-UP CORROSION AREA MEASURE THE ORIGINAL AND REWORK THICKNESS RESULT: 0.090-0.082" (REF JOB CARD ATTACHING SHEET 074291) WITHIN LIMITS PER MD-11 SRM 53-00-00 PAGE 206 RE
- [SDR WRLA20090926209](https://openairdocs.org/sdr/WRLA20090926209.md): Seat Track · corroded · Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 453-455, X=-27.5. CLEAN-UP CORROSION AREA MEASURE THE TRACK AREA THICKNESS: 0.100" (REF JOB CARD ATTACHING SHEET 074290) WITHIN LIMITS PER SRM 53-00-52 REV 41. APPLY PROTECTION COATING P

Next page: https://openairdocs.org/deregistered/N271WA-2014-11-24/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 = 'N271WA' AND deregistration_id = 'N271WA-2014-11-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N271WA-2014-11-24/reports

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