# Service difficulty reports: N275WA, cancelled Jan 30, 2014

A list on [N275WA, cancelled Jan 30, 2014](https://openairdocs.org/deregistered/N275WA-2014-01-30.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 WRLA20110823508](https://openairdocs.org/sdr/WRLA20110823508.md): Skin · corroded · Aug 23, 2011 · N275WA · Doug MD11F · Wing, Plate/Skin
  > CORROSION ON TOP OF CENTER TANK UPPER SKIN. REFERENCE EGAT NON-ROUTINE U05062; U05065; U05067; U05069; U05072; U05083. RE-WORKED CORROSION AREAS IAW EI W2011A57B-1770 REV. 01 AND REV. 02 FAA FORM 8100-9 SUBMITTED. SEE BOEING ACTIVITY NUMBER 1-WNM371 ALL WORK
- [SDR WRLA20110819507](https://openairdocs.org/sdr/WRLA20110819507.md): Skin · gouged · Aug 19, 2011 · N275WA · Doug MD11F · Fuselage Main, Plate/Skin
  > GOUGE- LEFT LOWER FUSELAGE OUTER SKIN STATION Y = 1150 TO Y = 1156 L44L. BLENDED AND OUT OF LIMIT. BLEND OUT GOUGE AND MEASURE RE-WORKED AREA AND THICKNESS, DETAIL DATA OUT OF LIMIT. REPAIRED DAMAGED AREA IAW SRM 53-40-01-2R-2. REPAIR NR 2 REV 46.
- [SDR WRLA20110818506](https://openairdocs.org/sdr/WRLA20110818506.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - MAIN DECK SEAT TRACK, STA 635, X10, FWD CARGO COMPARTMENT REF: EGAT N/R U05202. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 AND SRM 51-33-01 REV 46.
- [SDR WRLA20110818503](https://openairdocs.org/sdr/WRLA20110818503.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - MAIN DECK SEAT TRACK, STA 755, X48 FWD CARGO COMPARTMENT REF: EGAT N/R U05201. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1.
- [SDR WRLA20110818505](https://openairdocs.org/sdr/WRLA20110818505.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - MAIN DECK SEAT TRACK, STA 635, X48 FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.
- [SDR WRLA20110818504](https://openairdocs.org/sdr/WRLA20110818504.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - MAIN DECK SEAT TRACK, STA 755, X28, FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.
- [SDR WRLA20110818502](https://openairdocs.org/sdr/WRLA20110818502.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - MAIN DECK SEAT TRACK, STA 755, X76 FWD CARGO COMPARTMENT. REPAIRED THE EXISTING DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-1 REV 46 AND SRM 51-33-01 REV 46.
- [SDR WRLA20110818501](https://openairdocs.org/sdr/WRLA20110818501.md): Seat Track · cracked · Aug 18, 2011 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - AFT CARGO LT SIDE STATION 1944, SEAT TRACK. THE DAMAGED AREA AND RESULT ARE WITHIN ALLOWABLE LIMITS REF SRM 53-00-52 NDT VERIFIED NO CRACK. APPLIED PROTECTIVE COATING.
- [SDR WRLA20110812500](https://openairdocs.org/sdr/WRLA20110812500.md): Pan · cracked · Aug 12, 2011 · N275WA · Doug MD11F · Passenger Compartment Windows
  > DURING 2 C CHECK DATUM AIRCRAFT, CRACK WAS FOUND ON RETAINING PAN OF CABIN WINDOW PLUG ASSY. REFERENCE EGAT NON-ROUTINE U05111. REPAIRED DAMAGED AREA IAW EGAT EI NR W2011A56B-1756 PER REV 00, REV 01 REV 02 BOEING MSG EGA-WLD-11-00007-02B.
- [SDR WRLA20110505476](https://openairdocs.org/sdr/WRLA20110505476.md): Nose Cowl · cracked · May 5, 2011 · N275WA · Doug MD11F · Engine Air Intake System
  > NR 2 ENGINE NOSE COWL INLET LOWER LIP FOUND CRACKS EMANATING FROM SEVERAL FASTENERS FROM THE 4 TO 8 O'CLOCK POSITION. PERFORMED HFEC INSPECTION AND FOUND EXISTENCE OF CRACKS MENTIONED ABOVE IAW NDT MANUAL PART 6. REF: CARD WM-445 AND NON-ROUTINE 046. REMOVED
- [SDR WRLA20100120333](https://openairdocs.org/sdr/WRLA20100120333.md): Stringer · cracked · Jan 20, 2010 · N275WA · Doug MD11F · Wing, Longeron/Stringer
  > CRACK - STRAP XORS 987.2 & XOS 993.3 LT WING FIXED L/E. REPAIRED CRACK IAW EI W201057B-143 REV 00 2. COND CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20100105330](https://openairdocs.org/sdr/WRLA20100105330.md): Stop Fitting · cracked · Jan 5, 2010 · N275WA · Doug MD11F · Trailing Edge Flaps
  > DURING 01C CHECK FOUND RIGHT WING OUTBOARD FLAP STOP RIB (P/N:ARC4125-502) CRACKED AT XOF 563.244. NRC U05078 ISSUED. PER EI:W2010A57B-072 REV00 AND AMM REV66, RMV THE FLAP, RPL THE LEADING EDGE RIB, RE-INST THE FLAP. PFM AMM SUBTASK 27-50-30-830-003 TO ADJ
- [SDR WRLA20100105331](https://openairdocs.org/sdr/WRLA20100105331.md): Fitting · cracked · Jan 5, 2010 · N275WA · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > DURING 01C CHECK FOUND NOSE GEAR TRUNNION LT FITTING P/N ACA7017-502 CRACKED.
- [SDR WRLA20100105329](https://openairdocs.org/sdr/WRLA20100105329.md): Membrane · cracked · Jan 5, 2010 · N275WA · Doug MD11F · Fuselage Miscellaneous Structure
  > DURING 01C CHECK FOUND Y=360 X=-2 Z=-10 MEMBRANE ABA 7202-117 DEFORM AND 2EA CRACK, L=0.9" AND L=1.2" ON LIGHTENING HOLE. NRCU05014 ISSUED. ACCOMPLISHED THE REPAIR PER EI: W2010A53B-050 REV 00, 01,02: CUT THE DAMAGED AREA AS SHOWN IN W2010A53B-050 FIG 1, FA
- [SDR WRLA20090810196](https://openairdocs.org/sdr/WRLA20090810196.md): Skin · damaged · Aug 10, 2009 · N275WA · Doug MD11F · Fuselage Main, Plate/Skin
  > DAMAGE TO THE FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE UPPER CARGO DOOR CUTOUT. REPAIRED IN ACCORDANCE WITH WOA ERA 09-53-103.
- [SDR WRLA2008069A](https://openairdocs.org/sdr/WRLA2008069A.md): Doubler · cracked · Aug 20, 2008 · N275WA · Doug MD11F · Fuselage Main, Structure
  > DURING INSPECTION FOUND CRACK ON CLG WHEEL WELL LT AND RT DOUBLER AT Y=1381, X=31.5 AND -31.5. REPAIRED CRACK AREA IAW EI W2008A53B-761 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)
- [SDR WRLA2008067](https://openairdocs.org/sdr/WRLA2008067.md): Seat Track · cracked · Aug 5, 2008 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y=760, X=47.6. REPAIRED CRACK SET TRACK IAW MD-11SRM VOL 1 53-70-00 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)
- [SDR WRLA2008066](https://openairdocs.org/sdr/WRLA2008066.md): Seat Track · cracked · Aug 5, 2008 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > DURING "C" CHECK INSPECTION IN TPE FOUND CRACK IN THE MAIN DECK SEAT TRACK AT Y=760, X=47.5. (S)
- [SDR WRLA2008065](https://openairdocs.org/sdr/WRLA2008065.md): Longeron · corroded · Aug 2, 2008 · N275WA · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING "C" CHECK INSPECTION IN TPE, FOUND CENTER CARGO LONGERON 49R CORROSION AT STA Y=1707. REPAIRED THE CTR CARGO LONGERON 49R AT STA Y -1707 PER MD-11 SRM 53-10-00 REV. 40. CONDITION CHECK NORMAL AND JOB COMPLETED. (S)
- [SDR WRLA2008061](https://openairdocs.org/sdr/WRLA2008061.md): Wedge · debonded · Jul 31, 2008 · N275WA · Doug MD11F · Ailerons
  > DURING 4C CHECK INSPECTION DISBOND WAS FOUND ON THE LT WING OUTBOARD AILERON BETWEEN T/E CORE AND THE UPPER SKIN ASSEMBLY. BOEING HAS AUTHORIZED A TEMPORARY REPAIR WITH A-CHECK REINSPECTIONS AND C-CHECK PERMANENT REPAIR. (A)
- [SDR WRLA2008062](https://openairdocs.org/sdr/WRLA2008062.md): Fairing · dented · Jul 30, 2008 · N275WA · Doug MD11F · Nacelle/Pylon, Main Frame
  > DURING C CHECK INSPECTION DENT FOUND NR 3 ENGINE NOZZLE FAIRING SKIN DENT AT NAC BETWEEN 3O`CLOCK AND 4O`CLOCK POSITION. (LOOKING FORWARD). REPAIRED NR3 ENG NOZZLE FAIRING SKIN IAW EI W2008 A54B-687 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (A) (S)
- [SDR WRLA2008063](https://openairdocs.org/sdr/WRLA2008063.md): Structure · cracked · Jul 29, 2008 · N275WA · Doug MD11F · Leading Edge Devices
  > DURING C CHECK INSPECTION CRACK-FOUND RT WING LE INBD SLAT NR 1 AFT SIDE HAD CRACK 11.5 INCHES LONG AT XIS 247. REMOVED THE RT INBD NR 1 SLAT ASSY COMPLETED PER AMM 27-80-20-000-801 REV 62. REPAIRED THE DAMAGED AREA IAW MD-11 SRM VOL ONE 57-10-00 REV. 40. I
- [SDR WRLA2008069](https://openairdocs.org/sdr/WRLA2008069.md): Fuel/Oil Cooler · cracked · Jul 16, 2008 · N275WA · Doug MD11F · Engine Fuel/Oil Cooler
  > PRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXED IN YELLOW ON SHUT DOWN. OIL TEMP 105C OIL PRESSURE 148 PSID AT FL 280 THROTTLE IDLE, N2 69.3. RAN ENG AND FOUND LEAK AT EXISTING WELD ON FUEL/OIL COOLER. REMOVED AND R
- [SDR WRLA2008059](https://openairdocs.org/sdr/WRLA2008059.md): Engine · oil consumption · Jul 16, 2008 · N275WA · Doug MD11F · Turbine Engine Oil System
  > GEC8284 EDDP/K JFK 07/16 ITEM: PRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXED IN YELLOW ON SHUT DOWN. OIL TEMP 108C OIL PRESSURE 146PSID AT FL 280 THROTTLE IDLE, N2 69.5. OPEN. (S)
- [SDR WRLA2007087](https://openairdocs.org/sdr/WRLA2007087.md): Skin · damaged · Aug 23, 2007 · N275WA · Doug MD11F · Trailing Edge Flaps
  > DURING 3C+12A, EGAT MECHANIC FOUND CRACK ON INBOARD FLAP SKIN AT STA XIFH 198, YIFH 40 ON LEFT HAND WING. 09-26-07 PERFORM NDT/ET FOR CUTOUT AREA REF JC31896, NO CRACK FOUND. REPAIR CRACK AREA PER MD11 SRM VOL.157-10-00 REV.40
- [SDR WRLA2007089](https://openairdocs.org/sdr/WRLA2007089.md): Doubler · cracked · Aug 23, 2007 · N275WA · Doug MD11F · Wing, Longeron/Stringer
  > DURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LOWER LEADING EDGE STRINGER DOUBLER AT STA XOS 906. 09-26-07 REPAIRED PER MD-11 SRM 57-10-00 FIG.18 VOL.1 REV.40.
- [SDR WRLA2007088](https://openairdocs.org/sdr/WRLA2007088.md): Skin · cracked · Aug 23, 2007 · N275WA · Doug MD11F · Wing, Plate/Skin
  > DURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LEADING EDGE NOSE SKIN AT STA XOS=906. 09-26-07 PERFORM NDT/ET FOR REWORK AREA REF JC 0032337. REPAIR CRACK AREA PER MD-11 SRM 57-10-00 FIG.41 VOL.1 REV.40.
- [SDR WRLA2007086](https://openairdocs.org/sdr/WRLA2007086.md): Door Frame · cracked · Aug 16, 2007 · N275WA · Doug MD11F · Wing Main, Frame Structure
  > RIGHT WING FIXED LEADING EDGE ANTI-ICING TELESCOPING DUCT DOOR CUT OUT CORNER FOUND CRACK AT STA XOS464 AND XOS470. 09-26-07 PERFORM NDT/ET FOR REWORK AREA REF JC0032000. REPAIR DAMAGE PER MD-11 SRM 57-10-00 VOL.1 REV.40 AND EI NR 2006P20A-124 REV.00. REF
- [SDR WRLA2007085](https://openairdocs.org/sdr/WRLA2007085.md): Bellmouth · cracked · Aug 16, 2007 · N275WA · Doug MD11F · Turbine Engine Air Inlet Section
  > THREE EA CRACKS AT NUMBER 2 ENGINE BELLMOUTH BETWEEN 6-7 O'CLOCK POSITION. REPLACED NR 2 ENGINE BELLMOUTH ASSYWITH NEW PARTS AS PER AMM 71-11-04-000-868/71-11-04-400-868 REV.59
- [SDR WRLA2007083](https://openairdocs.org/sdr/WRLA2007083.md): Seat Track · cracked · Aug 14, 2007 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN WORN AT STA Y=585, X=27.50. REPAIR IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40.
- [SDR WRLA2007084](https://openairdocs.org/sdr/WRLA2007084.md): Seat Track · cracked · Aug 14, 2007 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK SEAT TRACK CROWN WORN AT STA Y=625, X=75.25. REPAIRED IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40
- [SDR WRLA2007082](https://openairdocs.org/sdr/WRLA2007082.md): Frame · cracked · Aug 14, 2007 · N275WA · Doug MD11F · Landing Gear Doors
  > DURING 3C+12A CHECK, EGAT MECHANIC FOUND RT CENTERLINE LANDING GEAR DOOR FORWARD FRAME EXISTING DOUBLER CRACK AT STA Y=1378.225. 09-26-07 REPLACED THE CRACKED FRAME WITH NEW PART PER MD-11 SRM VOL.II 51-35-01 & 51-33-01 REV.40
- [SDR WRLA2006107](https://openairdocs.org/sdr/WRLA2006107.md): Seat Track · broken · Dec 11, 2006 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO SEAT TRACK STATION 595 TO 655 LT DAMAGED BY LOADING FREIGHT. SEAT TRACK REPLACED REF SRM 51-30-00 VOL.2 REV. 38.
- [SDR WRLA2006085](https://openairdocs.org/sdr/WRLA2006085.md): Barrel Nut · corroded · Sep 12, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 9. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WRLA2006083](https://openairdocs.org/sdr/WRLA2006083.md): Barrel Nut · corroded · Sep 12, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 6. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WRLA2006084](https://openairdocs.org/sdr/WRLA2006084.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 8. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WRLA2006092](https://openairdocs.org/sdr/WRLA2006092.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST RT BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WRLA2006091](https://openairdocs.org/sdr/WRLA2006091.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST RT BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WRLA2006089](https://openairdocs.org/sdr/WRLA2006089.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 34. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATE
- [SDR WRLA2006087](https://openairdocs.org/sdr/WRLA2006087.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 21. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATE
- [SDR WRLA2006086](https://openairdocs.org/sdr/WRLA2006086.md): Barrel Nut · corroded · Sep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 17. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATE
- [SDR WRLA2006090](https://openairdocs.org/sdr/WRLA2006090.md): Barrel Nut · corroded · Sep 8, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > ITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 35. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FAB
- [SDR WRLA2006088](https://openairdocs.org/sdr/WRLA2006088.md): Barrel Nut · corroded · Sep 8, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer Structure
  > DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 32. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED
- [SDR WLDA200489](https://openairdocs.org/sdr/WLDA200489.md): Computer · inoperative · Aug 16, 2004 · N275WA · Doug MD11 · Autopilot System
  > UNCOMMANDED ELEV MOVEMENT. CONSIDERABLE CONTROL COLUMN PULL FORCE REQUIRED DURING INITIAL ROTATION TO ATTAIN REQUIRED T/O CLIMBOUT PITCH ATTITUDE UNTIL 500-800 FT AGL. AFTER FLAP RETRACTION, FORCE REQUIRED RETURNED TO NORMAL, CNTRL COLUMN OSCILLATED(TWICE) BE
- [SDR WRLA200417](https://openairdocs.org/sdr/WRLA200417.md): Solenoid · smoke · Apr 29, 2004 · N275WA · Doug MD11F · Passenger/Crew Doors
  > DURING CLIMB AFTER 3 MINUTES THE FLIGHT CREW SMELLED SMOKE IN THE COCKPIT. RETURNED BACK TO KDAY, THE CREWS HAD TO DUMP FUEL TO PERFORM A SUCCESSFUL LANDING. THE CAUSE OF THE SMOKE WAS DETECTED BY THE FIRE DEPARTMENTS USE OF INFRA RED HEAT UNIT TO BE AROUND
- [SDR WRLA200413](https://openairdocs.org/sdr/WRLA200413.md): Wire · burned · Mar 18, 2004 · N275WA · Doug MD11F · Electrical Power System Wiring
  > CENTER CARGO COMPT. PDU WIRE BUNDLE HAVE 6 WIRES BURNED AND BROKEN (WIRE NO:G110-663-20, G110-667-20, G110-665-20, G110-668-20, G110-666-20 AND G110-094-16) REPAIR THE WIRES WITH SPLICE PER SWPM 20-10-03. WIRES CONTINUITY AND INSULATION CHECK PER WDM 30-29-01
- [SDR WRLA200319](https://openairdocs.org/sdr/WRLA200319.md): Cooler · failed · Sep 20, 2003 · N275WA · Doug MD11F · Engine Fuel/Oil Cooler
  > AFTER TWO HRS INTO FLT LVL 2 HIGH OIL TEMP ON NR 3 ENG MAX TEMP 163 FOR APPROXIMATELY 3 MINUTES POWER REDUCED TO REDUCE TEMP. DEU'S WERE CHECKED FOR EXCEEDENCES NONE WERE NOTED. NR 3 ENGINE EEC CH A/B CHECKED FOR RELATED OIL SYTEM CONTROL OR SENSING FAULTS
- [SDR WRLA200329](https://openairdocs.org/sdr/WRLA200329.md): Screen · failed · Sep 19, 2003 · N275WA · Doug MD11F · Turbine Engine Oil System
  > FOUND ENGINE NR 3 OIL TEMPERATURE HIGH ILLUMINATED IN FLIGHT. ENGINE WAS SHUTDOWN WHEN TEMPERATURE REACH 177 DEGREES. OIL TEMPERATURE HIGH ILLUMINATED FOR 4 MINUTES. AS PER 72-00-04 PAGE 610 TABLE 606, NO MAINTENANCE REQUIRED. REPLACED NR 3 MAIN OIL SCREEN
- [SDR WRLA200222](https://openairdocs.org/sdr/WRLA200222.md): Pin · backed out · Sep 13, 2002 · N275WA · Doug MD11F · Aileron Control System
  > AILERON DEFLECT DISAGREE UPON FLAP RETRACTION, AIRCRAFT RETURNED TO DEPARTING STATION PANC. REPAIRED CONNECTOR PIN AT P1-1667. PIN E AND ALL FCC FLAP SYSTEMS PASSED RETURN TO SERVICE. (M)
- [SDR 2002F00059](https://openairdocs.org/sdr/2002F00059.md): Fmu · defective · Sep 17, 2001 · N275WA · Doug MD11F · Fuel Controlling System
  > ON CLIMB-OUT FROM JFK, NR 2 WAS SHUT DOWN FOR LOW RPM. NO RESTART OF NR 2 ENGINE WAS ATTEMPTED. THE AIRCRAFT WAS POSITIONING FROM JFK TO XNA FOR A SCHEDULED A-CHECK. REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT. LEAK AND OPERATION CHECK GOOD IAW MD-

Next page: https://openairdocs.org/deregistered/N275WA-2014-01-30/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 = 'N275WA' AND deregistration_id = 'N275WA-2014-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N275WA-2014-01-30/reports

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