N608FE
Service difficulty reports · 370
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 = 'N608FE' 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 = 'N608FE' 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 FDEA200904031242Fairing · damagedAFTER TO VIOLENT VIBRATION IN NOSE AREA WHEN ACCERATING THROUGH 230KTS.VIBRATION STOPPED WHEN DECCELATING TO 210KTS.276550 FLIGHT CREW ADVISED VIBRATION STARTED AFTER TAKEOFF AND ALL GEAR RETRACTED COMPLETELY. CHECKED A/C AROUND,LDG GEAR FOUND NO DEFECT NOTESDR FDEA200904031210Fairing · brokenAFTER TAKEOFF VIOLENT VIBRATION IN NOSE AREA WHEN ACCELERATING THROUGH 230KTS. VIBRATION STOPPED WHEN DECELERATING TO 210 KTS. FLIGHT CREW ADVISED VIBRATION STARTED AFTER TAKEOFF AND ALL GEAR RETRACTED COMPLETELY. CHECKED A/C AROUND, LANDING GEAR FOUND NO DSDR 08FDEA00810Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB BACKUP FITTING FOUND CRACKED. REMOVED AND REPLACED WITH A FABRICATED FITTING AS PER SRM 51-33-01 VOLUME II. FITTING FABRICATED AS PER EA 1-5300-112586, REPAIR CLASSIFIED AS MINOR PER GM 6-2-100.SDR 08FDEA00773Fitting · crackedMAIN DECK CARGO DOOR, LOWER JAMB SUPPORT FITTING AT NR 7 A POS HFEC CHECK FOUND FASTENER HOLE CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA1-5310-112585, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00673Seat Track · damagedMAIN DECK CARGO SEAT TRACK AT STA 5-33, RT = 75.25 UNDER FLOOR PANEL FOUND FLANGE DAMAGED. REPAIR CARRIED OUT AT MAIN DECK CARGO SEAT TRACK STA 5-33, RT=75.25 UNDER FLOOR PANEL FLANGE AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMSDR 08FDEA00651Seat Track · corrodedMAIN DECK CARGO, SEAT TRACK AT STA 555, RT X=27.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00623Splice · crackedHFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 LT SPLICE WITH CRACK LENGTH OF APPROX .25 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330-118768, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00622Splice · crackedHFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-2 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330- 118769, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00621Splice · crackedHFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330-118767, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00604Skin · cracked16 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING, LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS 690 AND XORS 700. REPAIR CARRIED OUT AS PER EA 1-5710-118761 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00603Skin · crackedFOUND SIX FASTENER HOLES CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-118760 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA00542Rib · crackedRIGHT WING, UPON REMOVAL OF NR 1 SLAT INBOARD CRUISE PERFORMANCE FILLET FOR NR 1 SLAT INBOARD LEADING EDGE METAL SEAL REPLACEMENT, FOUND OUTBOARD RIB NEAR ALIGNMENT AREA CRACKED. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS SDR 08FDEA00517Stiffener · crackedAFT FUSELAGE COMPT: AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT STA 2007, X=-10 UPPER END FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5310-117418, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA03392Strap · crackedRIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. RIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EA NR 1-5750-104780, TITLE: WINGS, RIGHT WING, OUTBOARD TRAILING EDGE FLAPSDR 06FDEA03272Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGSDR 06FDEA03271Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGS - SDR 06FDEA03270Bracket · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGSSDR 06FDEA03240Rib · crackedLEFT WING, AFTER REMOVAL OF NR 1 SLAT PERFORMANCE FAIRING FOUND FAIRING RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03239Longeron · corrodedRIGHT CENTER WING FUSELAGE LONGERON 28 LOWER SIDE OF R3 DOOR STA 1256 FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.250", REMOVED THICKNESS = 0.038", AND SDR 06FDEA03238Longeron · corrodedRIGHT CENTER WING FUSELAGE LONGERON 28 LOWER SIDE OF R3 DOOR STA 1305 FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.230", REMOVED THICKNESS = 0.063", AND SDR 06FDEA03237Panel · crackedLEFT WING NR 2 SLAT TRAILING EDGE PANEL OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03236Door Frame · corrodedMAIN DECK CARGO, FOUND R3 DOOR CUTOUT LOWER FORWARD AND AFT CORNER SEAL LAND LOCATION WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. ORIGINAL THICKNESS = 0.270", MATERIAL RESDR 06FDEA03235Door Frame · corrodedMAIN DECK CARGO, FOUND L3 DOOR CUTOUT LOWER FORWARD AND AFT CORNER SEAL LAND LOCATION WITH CORROSION. MAIN DECK CARGO LT HAND DOOR FORWARD AREA CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL THICKNESS = 0.270", REMAINING THICKNESS = 0.235", MATERIASDR 06FDEA03232Seat Track · wornMAIN DECK CARGO, FOUND WORN SEAT TRACK AT STA 715 RBL 27. REPAIR CARRIED OUT AT STA 715 RBL 27 AS PER SRM 53-70- 00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00661 FOR REPAIR DETAILS.SDR 06FDEA03220Hinge Fitting · crackedEMPENNAGE, FORWARD TAILCONE LEFT FORWARD HINGE FITTING FOUND CRACKED (LOCATED AT AFT ACCESSORY COMPARTMENT AFT BULKHEAD AREA). REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03219Seat Track · wornMAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 755 RBL 33.SDR 06FDEA03218Skin · crackedLEFT WING, FIXED LEADING EDGE SKIN AT TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103504, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03217Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 682 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103502, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03216Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 737 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103501, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03215Seat Track · wornMAIN DECK CARGO, FOUND SEAT TRACK WORN AT RBL 67 JUST AFT OF LAVATORY LOCATION. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 7 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03187Seat Track · wornMAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 700 RBL 55. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00591 FOR REPAIR DETAILS.SDR 06FDEA03186Seat Track · wornMAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 675 RBL 55. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03185Seat Track · wornMAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 755 LBL 33. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03184Skin · crackedRIGHT WING, FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103503, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03183Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. REPAIRED AS PER FEDEX E.A 1-5730-103500, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03182Spar Cap · corrodedCORROSION OBSERVED ON RIGHT WING REAR SPAR UPPER CAP AT XORS 683. RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 683 CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I AND FEDEX EA NR 1-5710-104779.SDR 06FDEA03177Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING STRINGER 14 END AT XORS 521. RIGHT HAND WING STRINGER 14 END AT XORS 521 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03176Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING STRINGER 12 END AT XORS 642. CRACKED STRINGER END ON RIGHT HAND WING, STRINGER 12 END AT XORS 642 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS SDR 06FDEA03175Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON LT WING STRINGER 13 END AT XORS 577. LT HAND WING STRINGER 13 END AT XORS 577 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03174Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON LEFT WING STRINGER 12 END AT XORS 642. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03173Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON LEFT WING STRINGER 10 END AT XORS 760. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03172Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON LEFT WING STRINGER 7 END AT XORS 952. REPAIRED AS PER FEDEX EA 1-5720-100697, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03171Trunnion · crackedRIGHT NOSE LANDING GEAR TRUNNION FITTING FOUND WITH CRACK ON LOWER FORWARD SIDE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-100699.SDR 06FDEA03170Trunnion · crackedLEFT NOSE LANDING GEAR TRUNNION FITTING FOUND WITH CRACK ON LOWER FORWARD SIDE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-104776,SDR 05FDEA01157Thrust Reverser · crackedNR 1 ENGINE, LEFT THRUST REVERSER COWL, UPPER TORQUE BOX FORWARD FRAME CHAMPFER FOUND CRACKED P/N 683L213G04 S/N R591-085. REPAIRED PER DRAWING SRZ-78-002.SDR 05FDEA01142Stringer · crackedRT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 9, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10.SDR 05FDEA01141Stringer · crackedRIGHT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 8, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10.SDR 05FDEA01131Seat Track · wornSNRM NO.: N0592 - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1139 TO Y= 6- 60, X= 47 CROWN ELONGATED A5A7082-1. REWORKED AND INSTALLED IAW SRM 53-70-01 VOLUME I, FIGURE 1.SDR 05FDEA01124Seat Track · wornMAIN DECK, FLOOR SEAT TRACK AT STA Y= 794, Y=800 AND Y= 908, X= -27 CROWN ELONGATED ADA8389-1. REMOVED IAW SRM 51-33-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA01121Seat Track · wornMAIN DECK, FLOOR SEAT TRACK AT STA Y= 904 TO Y= 1059, X= 47 CROWN ELONGATED ADA8389-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.
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