N274WA
Service difficulty reports not matched to an aircraft · 129
They name N274WA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N274WA' AND registry_match IS NULL 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 = 'N274WA' AND registry_match IS NULL 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 WRLA20110608491Structure · crackedAPU DOOR INNER STRUCTURE CRACKED NEAR SNUBBER FITTING.SDR WRLA20110603489Support Fitting · crackedRT NLG SUPPORT FITTINGS 15MM CRACKED.SDR WRLA20110601490Nose Cowl · crackedENGINE NR 2 FRONT SPAR OF NOSE COWL INSIDE CRACKED 0400 POS. LIP SKIN ON POSITION 12/3/6/9 CLOCK POS. FOUND SEVERAL NEW CRACKS NEXT TO EXISTING DOUBLER.SDR WRLA20110601488Longeron · corrodedLT SIDE LONGERON 28 BELOW OVERWING DOOR CORRODED.SDR WRLA20110601487Longeron · corrodedRT SIDE LONGERON 28 BELOW OVERWING DOOR ON TWICE POSITIONS CORRODED.SDR WRLA20091119326Fitting · corrodedFOUND LT WING OUTBOARD FLAP INBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 5 EA. REPAIRED THE 5EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET 1 AND REF JOB CARD ATTACHING SHEET 087985, 070668.SDR WRLA20091119325Seat Track · wornWORN - SEAT TRACK CROWN, STA 675, X=107.5 IN M/D CARGO FLOOR. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV 41.SDR WRLA20091116323Doubler · brokenBROKEN - LWR DOUBLER OF LT WING FIXED L/E NOSE SECTION XOS 487. FABRICATED PART IAW EGAT EI W2009P57B-1344 REV 00. INSTALLED PART IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091116322Skin · corrodedEXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR WRLA20091116321Seat Track · wornWORN - SEAT TRACK CROWN, STA 1887 X=47.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53.00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116320Seat Track · wornWORN - SEAT TRACK CROWN, STA 735 X=107.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116319Seat Track · wornWORN - SEAT TRACK CROWN, STA 716 X=-46, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116318Hinge Fitting · corrodedFOUND RT WING OUTBOARD FLAP OUTBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-01-000-801 REV 65 RMV THE RT WING OUTBOARD FLAP OUTBOARD FWD HINGE. SEND TO SHOP FOR RPR REF J/C ATTACHING SHEET 070610, 070611. IAW SDR WRLA20091116317Support Fitting · corrodedFOUND RT WING OUTBOARD FLAP OUTBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 3 EA. REPAIRED THE 3EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET 1 AND REF JOB CARD ATTACHING SHEET 087986. COND CHECK SATISFACTORY AND JOB COMPLETED.SDR WRLA20091116316Mount · corrodedFOUND RT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL 7 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE RT WING OUTBOARD FLAP INBOARD AFT HINGE. SEND TO SHOP FOR REPAIR REF J/C ATTACHING SHEET 070608. IAW AMM 20-20-01-400-801 REV 65 RE-INSDR WRLA20091116315Skin · corrodedCORROSION - SKIN Y=1226~1228 X=57~61 EXFOLIATION AROUND FASTENERS HEAD CTR WING TANK UPPER SURFACE TOTAL: 3 AREAS. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR WRLA20091116314Seat Track · wornWORN - SEAT TRACK CROWN, STA 1887 X=27.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116313Seat Track · wornWORN - SEAT TRACK CROWN, STA 638 TO STA 650, X=42, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116312Seat Track · wornWORN - SEAT TRACK CROWN, STA 645 X=24, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116311Seat Track · wornWORN - SEAT TRACK CROWN, STA 1163, X=-8.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091116310Seat Track · wornWORN - SEAT TRACK CROWN, STA 1289, X= -47, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD1 SRM 51-21-01 REV 41.SDR WRLA20091116309Seat Track · wornWORN - SEAT TRACK CROWN BETWEEN STA 630 AND 635 X= 8.5 INCHES IN MID CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091114308Mount · corrodedFOUND LT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL: 3 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE LT WING OUTBOARD FLAP INBOARD AFT HINGE. SEND TO SHOP FOR REPAIR REF EGAT NRC U05182 J/C ATTACHING SHEET 070607. IAW AMM 20-50-02-90SDR WRLA20091114307Mount Fitting · corrodedFOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-04-000-801 REV 65, REMOVED THE LT WING OUTBOARD FLAP INBOARD FWD HINGE. SEND TO SHOP FOR REPAIR REF EGAT NRC U05183 J/C ATTACHING SHEETSDR WRLA20091105306Panel · crackedCRACK PANEL RUDDER REAR CENTER SPAR TO REAR SPAR LWR PANEL RT SIDE. REPAIRED THE CRACK AREA IAW MD11 SRM 55-30-02 FIG 201 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091105305Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 546. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105304Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 560 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105303Doubler · crackedCRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLE IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105302Doubler · crackedCRACK - BEADED DOUBLER FINED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 11 INCH. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091105327Seat Track · wornWORN - SEAT TRACK CROWN, BETWEEN STA 1661. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41. JOB COMPLETED AND COND CHECK NORMAL.SDR WRLA20091101287Fitting · crackedCRACK - FITTING RT WING LOWER WINGLET STRUCTURE, DIMENSION =2.6 INCH QTY 1 EA. IAW AMM 57-31-00-000-801 REV 65 REMOVED THE RT LOWER WINGLET. REFERENCE THE EI W2009A57B-1483 REV 01 TO REPAIR THE WINGLET. IAW AMM 57-31--00-400-801 REV 65 INSTALL THE RT WING LSDR WRLA20091101301Fitting · crackedCRACK - ONE CLIP CRACKED ABOUT 1 INCH Y=1341, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY=1. FABRICATED PART IAW EGAT EI W2009P53B-1375 REV 00. INSTALLED WITH NEW PARTS IAW MD11 SRM 51-33-01.SDR WRLA20091101300Fitting · crackedCRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND SRM 51-33-01 FIG 2 REV 41.SDR WRLA20091101299Intercostal · crackedCRACK - INTERCOSTAL, STA Y=6-50, L-42R, FWD CARGO COMPARTMENT L=0.1 INCH. REPAIRED INTERCOSTAL CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.SDR WRLA20091101298Bracket · damagedCRACK - BRACKET TAIL CONE WORK PLATFORM DOOR LOCK/UNLOCK SENSOR SUPPORT ATTACHED AFT FUSELAGE BULKHEAD AFT FACE, Y=2164, Z=73, LENGTH =.5 INCH. REPLACED DAMAGE BRACKET IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101297Skin · deformedDEFORMED - EDGE OF SKIN FWD LOWER CORNER OF CENTER CARGO DOOR. MEASURE DEFORMED AREA DIMENSION (LXWXD = 1.5"X1.5"X0.03") AND NDT CHECK NORMAL AND IAW MD11 SRM 53-00-01 REV 41 WITHIN LIMITATION.SDR WRLA20091101296Bracket · crackedCRACK - BRACKET OF TAIL CONE WORK PLATFORM LIGHT BOTH OF AFT FUSELAGE BULKHEAD ABOUT 1 INCH QTY = 2EA. REPLACED NEW BRACKET IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101295Support Angle · crackedCRACK - NR 3 ENG PRECOOLER COMPARTMENT WIRE SUPPORT ANGLE CRACK ABOUT 2 INCHES. REPAIRED THE CRACK AREA IAW MD11 SRM 54-00-00 FIG 208 REV 41.SDR WRLA20091101294Retainer · crackedCRACK - RETAINER STA 1521 LBL 49 PRESSURE BULKHEAD OF CENTER CARGO COMPARTMENT QTY =1EA. REPLACED WITH NEW RETAINER IAW EGAT EI W2009P53B-1374 REV 00.SDR WRLA20091101293Retainer · crackedCRACK - RETAINER STA 1521 LBL 11 PRESSURE BULKHEAD CENTER CARGO COMPARTMENT DIMENSION: 1 INCH. REPLACED WITH NEW RETAINER IAW MD11 SRM 53-00-01 REV 41.SDR WRLA20091101292Seat Track · crackedCRACK - SEAT TRACK STA 635 X=8 M/D CARGO FLOOR L=3". REPAIRED THE SEAT TRACK IAW ME11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091101291Seat Track · crackedCRACK - SEAT TRACK STA 755 X=47.5 M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.SDR WRLA20091101290Intercostal · crackedCRACK - INTERCOSTAL 3 AIR CONDITION DOOR L=0.5" QTY =1 AREA. REPLACED INTERCOSTAL IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101289Intercostal · crackedCRACK - INTERCOSTAL 2 AIR CONDITION DOOR L=5", QTY = 1 AREA. REPLACED WITH NEW INTERCOSTAL ON 2 AIR CONDITION DOOR IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101286Support Bracket · crackedCRACK - THE SUPPORT BRACKET OF FUEL PIPE AT Y=1441, L32L, LEFT UPPER FUSELAGE, CRACKED ABOUT .25 INCH. FABRICATED NEW PART IAW EGAT EI W2009P53B-1353 REV 00. INSTALLED NEW PART IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101285Angle · crackedCRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091101284Web · crackedCRACK - WEB, LT WING TO BODY FAIRING SUPPORT STRUCTURE, L=1.5", Y=1341. REPAIRED WEB CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.SDR WRLA20091101283Web · crackedCRACK - WEB, LT OF FWD UPPER HORIZONTAL STAB COMPARTMENT ACCESS CUTOUT Y = 2042,, X=14, LENGTH = .375 INCH. REPAIRED THE CRACK AREA IAW MD11 SRM 53-00-00 FIG 211 REV 41.SDR WRLA20091101282Stiffener · crackedCRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.SDR WRLA20091101281Stiffener · crackedCRACK - STIFFENER, STA 1841, RBL 38 LWR SIDE WEB OF FLOORBEAM, AFT CARGO COMPARTMENT L=0.5 INCH. REPLACED WITH NEW STIFFENER IAW MD11 SRM 51-33-01 FIG 2 REV 41.
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