N277WA, cancelled Aug 26, 2015
Service difficulty reports · 86
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 = 'N277WA' AND deregistration_id = 'N277WA-2015-08-26' 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 = 'N277WA' AND deregistration_id = 'N277WA-2015-08-26' 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 WRLA20111226529Ballast · defectiveELECTRICAL 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 POSDR WRLA20111118525Light · inoperativeEMERGENCY 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 WRLA20110920510Skin · dentedAIRCRAFT 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 WRLA20110730497Pin · defectiveFLOOR 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 WRLA20110308474Fan · faultyMX 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 WRLA20101217456Battery Pack · faultedEMERGENCY LIGHT TEST FAIL: NR 1 BATTERY PACK FAULTED. REMOVED AND REPLACED NR 1 BATTERY PACK.SDR WRLA20101206455Light · inoperativeDURING T-10 FOUND EMERGENCY FLOOR LIGHTING INOP FOR B ZONE ROW 14 THRU 18 LT SIDE.SDR WRLA20100619418Battery Pack · failedEMERGENCY 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 WRLA20100616414Shear Tie · corrodedCORROSION - STA 1986 L50L TO L50R, LOWER SHEAR TIE P/N AGA8007-9 CORROSION. NRC U05110 ISSUED.SDR WRLA20100607417Web · crackedCRACK - IN CTR CARGO AT STA 1841 X = -62 VERTICAL WEB P/N AGA7125-3 CRACK. NRC U05084 ISSUED.SDR WRLA20100607416Stop Fitting · crackedCRACK - IN CTR CARGO STA 1841 X=-62 STOP FITTING P/N AGA71971 CRACK. NRC U05083 ISSUED.SDR WRLA20100607415Frame · corrodedCORROSION - STA 1986 L50L TO L50R LOWER FRAME CORROSION, NRC U05111 ISSUED.SDR WRLA20100607413Tee Fitting · corrodedCORROSION - 1EA TEE P/N AGA800219 LOC STA1975 BETWEEN L50L AND L50R CORROSION, NRC U05072 ISSUED.SDR WRLA20100607412Cargo Track · corrodedCORROSION - MAIN DECK FLOOR STA 495 X=-75 RT CURVED SEAT TRACK CORROSION.SDR WRLA20100607411Seat Track · corrodedSTA 495 X=75 LT CURVED SEAT TRACK CORRODED.SDR WRLA20100607410Seat Track · corrodedCORROSION AT X=785 Y=104 SEAT TRACK S4929148 CORROSION.SDR WRLA20100607409Skin · crackedCRACKED NR 2 INLET LIP OUTER SKIN CRACK AT 5-7 O'CLOCK.SDR WRLA20100607408Skin · dentedDENT AT STA 430-440 L36R-S38R DENT ON SKIN.SDR WRLA20100607407Skin · crackedCRACK AT NR 2 ENG INLET LIP INNER SKIN INNER SURFACE CRACK AT 6 O'CLOCK.SDR WRLA20100607406Pan · corrodedCORROSION AT STA 19 S51L-51R WASTE TANK DRAIN PAN CORROSION.SDR WRLA20100506356Battery Pack · dischargedEMERGENCY LIGHT TEST FAILED NR 4 BATTERY PACK. REMOVED AND REPLACED NR 4 BATTERY PACK.SDR WRLA2009195Engine · failedDURING 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 WRLA2009189Engine · vibrationNR 1 ENGINE HI VIBRATION/LOW RPM IN INITIAL CLIMB OUT. HIGH EGT 917C. DURING SHUTDOWN ENGINE FIRE AGENT DISCHARGED.SDR WRLA2009092Floor Support · corrodedDURING 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 0SDR WRLA2009091Floor Support · corrodedDURING 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 4SDR WRLA2009089Web · crackedDURING 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 NOSDR WRLA2009090Doubler · crackedDURING 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 CUTOUSDR WRLA2009088Angle · crackedDURING 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 WRLA2009087Stiffener · crackedDURING 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 ENSDR WRLA2009086Stiffener · crackedDURING 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 ENSDR WRLA2009085Rib · crackedDURING 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 NORMALSDR WRLA2009084Seat Track · corrodedDURING 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 WRLA2009083Door · crackedDURING 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, REINSTALLEDSDR WRLA2009082Door · crackedDURING 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-INSDR WRLA2009081Step · crackedDURING 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 & CSDR WRLA2009080Support Bracket · deformedDURING 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 THISDR WRLA2009079Support Bracket · crackedDURING 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, INSTALLESDR WRLA2009078Doubler · crackedDURING 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, INSTSDR WRLA2009077Doubler · crackedDURING 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 WRLA2009076Doubler · crackedDURING 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 SRMSDR WRLA2009075Doubler · crackedDURING 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 SRMSDR WRLA2009074Step · crackedDURING 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 WRLA2009073Rib · crackedDURING 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 DOSDR WRLA2009072Fitting · crackedDURING 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 COMPLETEDSDR WRLA2009071Seal · crackedDURING 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 WRLA2009070Rib · crackedDURING 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 WRLA2009069Seat Track · corrodedDURING 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 WRLA2009068Vane · debondedDURING 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 27-50-22SDR WRLA2009067Wedge · debondedDURING 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 57-5SDR WRLA2009063Fitting · crackedDURING 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
Back to N277WA, cancelled Aug 26, 2015