N275WA, cancelled Jan 30, 2014
Service difficulty reports · 144
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WRLA20110823508Skin · corrodedCORROSION 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 WORKSDR WRLA20110819507Skin · gougedGOUGE- 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 WRLA20110818506Seat Track · crackedCRACK - 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 WRLA20110818503Seat Track · crackedCRACK - 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 WRLA20110818505Seat Track · crackedCRACK - 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 WRLA20110818504Seat Track · crackedCRACK - 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 WRLA20110818502Seat Track · crackedCRACK - 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 WRLA20110818501Seat Track · crackedCRACK - 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 WRLA20110812500Pan · crackedDURING 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 WRLA20110505476Nose Cowl · crackedNR 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. REMOVEDSDR WRLA20100120333Stringer · crackedCRACK - 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 WRLA20100105330Stop Fitting · crackedDURING 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 ADJSDR WRLA20100105331Fitting · crackedDURING 01C CHECK FOUND NOSE GEAR TRUNNION LT FITTING P/N ACA7017-502 CRACKED.SDR WRLA20100105329Membrane · crackedDURING 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, FASDR WRLA20090810196Skin · damagedDAMAGE 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 WRLA2008069ADoubler · crackedDURING 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 WRLA2008067Seat Track · crackedDURING 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 WRLA2008066Seat Track · crackedDURING "C" CHECK INSPECTION IN TPE FOUND CRACK IN THE MAIN DECK SEAT TRACK AT Y=760, X=47.5. (S)SDR WRLA2008065Longeron · corrodedDURING "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 WRLA2008061Wedge · debondedDURING 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 WRLA2008062Fairing · dentedDURING 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 WRLA2008063Structure · crackedDURING 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. ISDR WRLA2008069Fuel/Oil Cooler · crackedPRECAUTIONARY 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 RSDR WRLA2008059Engine · oil consumptionGEC8284 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 WRLA2007087Skin · damagedDURING 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.40SDR WRLA2007089Doubler · crackedDURING 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 WRLA2007088Skin · crackedDURING 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 WRLA2007086Door Frame · crackedRIGHT 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 WRLA2007085Bellmouth · crackedTHREE 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.59SDR WRLA2007083Seat Track · crackedDURING 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 WRLA2007084Seat Track · crackedDURING 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.40SDR WRLA2007082Frame · crackedDURING 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.40SDR WRLA2006107Seat Track · brokenMAIN 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 WRLA2006085Barrel Nut · corrodedDURING 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, FABRICATEDSDR WRLA2006083Barrel Nut · corrodedDURING 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, FABRICATEDSDR WRLA2006084Barrel Nut · corrodedDURING 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, FABRICATEDSDR WRLA2006092Barrel Nut · corrodedDURING 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, FABRICATEDSDR WRLA2006091Barrel Nut · corrodedDURING 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, FABRICATEDSDR WRLA2006089Barrel Nut · corrodedDURING 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, FABRICATESDR WRLA2006087Barrel Nut · corrodedDURING 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, FABRICATESDR WRLA2006086Barrel Nut · corrodedDURING 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, FABRICATESDR WRLA2006090Barrel Nut · corrodedITEM: 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, FABSDR WRLA2006088Barrel Nut · corrodedDURING 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, FABRICATEDSDR WLDA200489Computer · inoperativeUNCOMMANDED 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) BESDR WRLA200417Solenoid · smokeDURING 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 WRLA200413Wire · burnedCENTER 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 WRLA200319Cooler · failedAFTER 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 FAULTSSDR WRLA200329Screen · failedFOUND 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 SCREENSDR WRLA200222Pin · backed outAILERON 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 2002F00059Fmu · defectiveON 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-
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