N595FE
Service difficulty reports · 389
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 = 'N595FE' AND registry_match = 'registration' 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 = 'N595FE' AND registry_match = 'registration' 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 FDEA200902020423Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127439, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020422Stanchion · corrodedFORWARD CARGO (UPON OPEN UP FOR THRUST REVERSER MODIFICATION) FOUND STA 6-70 X = 57, AFT BULKHEAD STANCHION LOWER SECTION CORRODED AROUND ANCHOR NUT. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW STANCHION REWORKED AS PER DRAWING A6A7094. REPAIR CLASDR FDEA200902020421Hinge Bracket · corrodedRIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127443, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200902020420Hinge Bracket · corrodedRIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127443, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA200902020419Hinge Bracket · corrodedLEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127442, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR FDEA200902020418Hinge Bracket · corrodedLEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127442, THIS REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100.SDR FDEA200902020417Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127438, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020416Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127438, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200902020415Hinge Bracket · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127438, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020414Hinge · corrodedLEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127444, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200902020413Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200902020412Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020411Hinge · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127440, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020410Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REPAIR 1-1. NEW BUSHING FABRICATED AND INSTALLED ON INBOARD ACTUATOR HOLE AS PER EA 1-5750-127440, THIS REPAIR SDR FDEA200901290397Rib · crackedLEFT WING LEADING EDGE COMPARTMENT CEILING UPPER SUPPORT RIB FOUND CRACKED AT APPROXIMATELY XORS 634 NEAR TO OUTBOARD SIDE OF NR 11 SLAT TRACK. REMOVED AS PER SRM 51-31-01 VOLUME II. RIB FABRICATED AS PER DRAWING ARB2923 AND INSTALLED AS PER SRM 51-31-01 VOLSDR FDEA200901290396Skin · dentedLOWER FUSELAGE AT STA 515 BETWEEN LONGERON 45L AND LONGERON 46L SKIN PANELS EXTERIOR SURFACE FOUND WITH DENT PREVIOUSLY BLENDED OUT. FOUND WITH OIL CANNING CONDITION. REPAIR CARRIED OUT AS PER E.A. 1-5310-127759, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2SDR FDEA200901290359Beam · crackedCRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE D, SECOND LAYER SKIN. CRACK INDICATION AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE D, SECONDSDR FDEA200901290358Support Fitting · crackedCRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE B, SECOND LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901290357Support Fitting · crackedCRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE A, SECOND LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901290356Support Fitting · crackedCRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE A, FIRST LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901290355Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901290354Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE B. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901290353Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE C AND D. REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200808253580Rectifier · inoperativeEMERGENCY PWR ON ALERT INFLIGHT. WHEN SELECTED OFF, DC3 DID NOT APPEAR POWERED. EMERGENCY PWR ARM AND ALERT STAYED ON. ADG DEPLOYED. ON SHORT FINAL DC3 UNPOWERED WITH LOSS OF ADG POWER RESULTING IN LOSS OF ASSOCIATED SYSTEMS. FLIGHT DIVERTED DFW AND LANDSDR 08FDEA03580Rectifier · malfunctionedEMERGENCY PWR ON ALERT INFLIGHT. WHEN SELECTED OFF, DC3 DID NOT APPEAR POWERED. EMERGENCY PWR ARM AND ALERT STAYED ON. ADG DEPLOYED. ON SHORT FINAL DC3 UNPOWERED WITH LOSS OF ADG POWER RESULTING IN LOSS OF ASSOCIATED SYSTEMS. FLIGHT DIVERTED DFW AND LANSDR 08FDEA01645Landing Gear · crackedFOUND CTR LANDING GEAR SHOCK STRUT CYLINDER CRACK FROM TOP DOWN ABOUT 33 INCHES. REMOVED AND REPLACE CENTER MAIN LANDING GEAR AND PERFORMED MLG RETRACTION TEST.SDR 07FDEA03297Bulkhead · corrodedREFERENCE TO SNRM N00486, CORROSION WAS DETECTED AFTER REMOVAL OF NR 3 PYLON AFT MOUNTING BEARING. COMPLIED WITH FEDEX EA NR 1-5410-112388, TITLE: NACELLES AND PYLONS, NR 3 PYLON AFT MOUNT BEARING HOUSING BORE, INTERIM (24 MONTHS) REPAIR. REPAIR CLASSIFIED ASDR 07FDEA03064Bearing Race · migratedNR 3 PYLON AFT MOUNT BEARING AFT FACE OUTER RACE FOUND MIGRATED. 08-31-07 REMOVED AND REPLACED AS PER FEDEX E.A. 1-5410-112388. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA02971Longeron · crackedAFT CARGO, LONGERON 51L SPLICE END AROUND STA 1956 FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA02955Longeron · crackedFUSELAGE, LEFT EXTERIOR SURFACE LONGERON END CAP FITTING AT STA 1521 LONGERON 30L FOUND CRACKED. 08/31/07 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE END CAP FITTING FABRICATED AS PER DOUGLAS DRAWING AEA7643 AND INSTALLED AS PER SRM 51-33-01 VOLUMESDR 07FDEA02903Rib · crackedRIGHT WING SLAT TRACK NR 16 RIB FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51- 35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA02902Structure · dentedRIGHT WING NR 6 SLAT FOUND WITH DENTS. 08-31-07 MEASURED AND FOUND 4 AREAS EXCEEDED LIMIT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. ALL DENT AREAS REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA02901Structure · noneRIGHT WING NR 7 SLAT FOUND WITH DENTS. CARRIED OUT AS PER DAC NDT SPM REV. 13 06- 10-01.001 AND FOUND NO CRACKS ON DENTS. ALL DENT MARKS MEASURED AND FOUND WITHIN LIMIT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. REWORKED AREA PROTECTED AS PER SRM 51-21-01 VSDR 07FDEA02900Structure · crackedLEFT WING FIXED LEADING EDGE SLAT TRACK COVER CUTOUT OUTBOARD CORNER AT STA XOS = 832, FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE STA XOS = 889 SLAT TRACK COVER CUTOUT AREA AS PER SRM 57-100-00 FIGURE 21 VOLUME I. REPAIR CLASSISDR 07FDEA02899Structure · crackedLEFT WING FIXED LEADING EDGE SLAT COVER CUTOUT OUTBOARD CORNER AT STA XOS = 774 FOUND CRACKED. 08-31-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MISDR 07FDEA01126Control Valve · unknownPDIS: FLAPS FROZE AT 22-23 DEG ON RETRACTION, RETURN FLAP HANDLE TO 25DEG FLAPS EXTENDED BACK TO 25 DEG, NO ASYMMETRY NOTED, ON 2ND ATTEMPT TO RETRACT FLAPS, FLAPS MOVED SLOWER THAN NORMAL AND FLAPS FULLY RETRACTED. ON LANDING FLAPS EXTEND NORMALLY. AFTER LASDR 07FDEA01125Computer · failedPDIS : FLAPS DID NOT RETRACT WHEN FLAP HANDLE RAISED AFTER T/O, PER QRH, MATCHED FLAP HANDLE TO INDICATED POSITION (15DEG) BUT FLAP INDICATION SHOWED FLAPS CONTINUING TO COME UP. EVENTUALLY INDICATED "0", MATCHED FLAP HANDLE AGAIN. RTB WITH NO PROBLEM ON FLASDR 07FDEA01027Tire · damagedNR 9 TIRE FAIL ALERT ON LNDG ROLLOUT CDG. NO OTHER INDICATIONS. FOUND NR 9 TIRE EXPOSED. FOUND BRAKE NR 10 HYD PRESS LINE CUT, AND BRAKE NR 9 HID FITTING BENT, NEED TO REPLACE NR 9 BRAKE. REMOVED AND REPLACED BRAKE NR 10 HYD PRESS LINE AS PER SUMP. LEAK SDR 06FDEA1350Bracket · corrodedFOUND CORROSION LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE . CORROSION AT LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE. REPAIRED AS PER FEDEX EA NR 1-5750-95810, TITLE: "WINGS - LT OUTBOARD TRAILING EDGE FLAP, I/B BRACSDR 06FDEA1349Support Fitting · corrodedLT WING O/B FLAP I/B HINGE SUPPORT FITTING (ARC4009) O/B NR 3 BOLT HOLE FOUND CORROSION. LT WING O/B FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30- 4. OPERATIONAL CHECK AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.SDR 06FDEA1348Fitting · crackedRT WING O/B FLAP SECONDARY UP STOP SUSPECT CRACK. RT WING O/B FLAP SECONDARY UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.SDR 06FDEA1356Frame · dentedFOUND MAIN DECK CARGO, AT STA 1721 RT FRAME, HAS A DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1721 RT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDESDR 06FDEA1355Frame · dentedFOUND MAIN DECK CARGO AT STA 1681 LT, FRAME HAS DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1681 LT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDEX ESDR 06FDEA1354Frame · dentedFOUND MAIN DECK CARGO AT STA 1661 LT FRAME HAS A DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1661 LT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDEX SDR 06FDEA1351Skin · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE FOUND DELAMINATED. LEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE REPAIRED AS PER FEDEX EA NR 1-5790-95674, TITLE: WINGS, OUTBOARD AILERON, REPAIR LEFT OUTBOARD AILERON DELAMINASDR 06FDEA1325Skin · crackedLT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACKED. CRACK AT LT WING FIXED L/E TELESCOPING DUCT CUTOUT REPAIRED AS PER FEDEX EA NR 1-5730-95669, TITLE: "WINGS - STRUCTURE. LEFT LEADING EDGE SKIN CRACKS AT ANTI-ICE TELESCOPING DUCT CUTOUT". REPAIR CLASSSDR 06FDEA1338Stringer · crackedHFEC INSPECTION CARRIED OUT, FOUND CRACK ON END OF LEFT HAND WING STRINGER 10. LEFT HAND WING TANK AT THE END OF STRINGER 10 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA1330Stringer · crackedCRACK FOUND IN LEFT WING TANK AT END OF STRINGER 14 DURING HFEC INSPECTION. LEFT WING AT THE END OF STRINGER 14 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA1329Stringer · crackedCRACK FOUND IN LEFT WING TANK AT END OF STRINGER 13 DURING HFEC INSPECTION. LEFT WING TANK AT THE END OF STRINGER 13 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA1328Stringer · crackedHFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER-14 END. RIGHT WING STRINGER 14 END CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
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