N599FE
Service difficulty reports · 318
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 = 'N599FE' 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 = 'N599FE' 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 FDEA200903160924Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1.5 INCH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAPS AREA. REPAIRED AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 REVISION 107.SDR FDEA200903160923Hinge Bracket · corrodedRIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG OUTBOARD BORE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127487, NEW BUSHING INSTALLED AS PER EA 1-5750-127487. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200903160922Hinge · corrodedRIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG INBOARD BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127487, BUSHING FABRICATED AS PER MD 11 CMM 57-52-03 REVISION 63 AND NEW BUSHING INSTALLED AS PER E.A. NO. 1-5750-127487. REPAIR CLASSIFIED SDR FDEA200903120903Frame · deformedMAIN DECK, AT STA 1701 LONGERON 12 LEFT, FRAME FOUND DEFORMED. REPAIRED AS PER SRM 53-30-00 FIGURE 1, VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-0SDR FDEA200903110900Seat Track · corrodedMAIN DECK, AT STATION 1006, X = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 989 TO STA 1029, X = 8.5, AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.SDR FDEA200903110899Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME I I REVISION 40. REPSDR FDEA200903110897Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II SDR FDEA200903110896Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION SDR FDEA200903110895Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES NR A, NR B AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION SDR FDEA200903110894Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVSDR FDEA200903110893Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION SDR FDEA200903110892Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. RESDR FDEA200903110891Skin · chafedLEFT INBOARD FLAP UPPER SURFACE FOUND CHAFED THROUGH ON SKIN AT 9 INCHES OUTBOARD OF INBOARD END. TRIMMED OFF AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISION 40. REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISSDR FDEA200903110890Skin · crackedLEFT WING LEADING EDGE SLAT TRACK NR 14 CUTOUT FOUND CRACKED AT CORNER EDGE. OUT CRACKED CORNER EDGE, TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.SDR FDEA200903110889Skin · crackedRIGHT WING LEADING EDGE SLAT TRACK NR 14 CUTOUT FOUND CRACKED AT CORNER EDGE. OUT CRACKED CORNER EDGE, TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.SDR 08FDEA03457Uplock Sensor · malfunctionedRT MAIN LDG GEAR WOULD NOT RETRACT ON FIRST ATTEMPT. SLOWED TO <230KIAS AND RECYCLED GEAR. 2ND RETRACT ATTEMPT WAS SUCCESSFUL. AS CREW BRIEF, DID NOT SEE SECONDARY MAIN LANDING GEAR INDICATION WHEN HAD NOT RETRACT. ALSO THEY COULD NOT FEEL ACTUAL DRAG. PESDR 08FDEA03269Proximity Switch · malfunctionedDURING APPROACH TO LFPG EXPERIENCED A LEVEL NR 2 "SLAT DISAGREE" ALERT DURING SLAT EXTENSION. COMPLIED WITH QRH AND CONDUCTED A FLAP/RETRACT LANDING TO RUNWAY 26R AT LFPG. LANDING WEIGHT WAS REDUCED AS MUCH AS POSSIBLE AND NO FURTHER PROBLEMS WERE ENCOUNTESDR 07FDEA04224Skin · dentedRT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA04221Skin · dentedLT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA04189Longeron · corrodedRT WING TO FUSELAGE BODY FAIRING ENCLOSED AREA FOUND LONGERON 28 AT STA 1289 WITH CORROSION. 10-04-07 CORROSION REMOVED AS PER SRM 51-31-012 VOLUME II. HOLES PICKED UP ON NEW LONGERON AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPIAR CLASSIFIED AS MASDR 07FDEA04149Seat Track · crackedMAIN DECK CABIN SEAT TRACK AT STA 635, X = 27.5 LT FOUND WITH CRACK. FOUND AFTER REMOVAL OF LOWER FWD CARGO CEILING PANEL. 10-04-07 REPAIRED BY SECTION A SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10SDR 07FDEA04148Frame · dentedMAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED OUT AS PER SRM 53-30-0SDR 07FDEA04147Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1741 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED OUT AS PER SRM 53-30-SDR 07FDEA04146Frame · dentedMAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIE OUT AS PER SRM 53-30-00SDR 07FDEA04145Frame · dentedMAIN DECK CARGO COMPARTMENT, MAINFRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-0SDR 07FDEA03981Attach Fitting · crackedLEFT MAIN LANDING GEAR WHEEL WELL, FOUND STRUT ATTACHMENT FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER SRM 52-10-00 FIGURE 18 VOLUME I. OPS CHECK CARRIED OUT AS PER AMM 32-31-00-700-803 FOUND 'SAT'. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2SDR 07FDEA03977Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK STA 770, X = 75.25 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA03974Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X = 47.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA03971Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X= 8.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA03888Strut · crackedRIGHT MAIN LANDING GEAR WHEEL WELL FOUND STRUT ATTACHING FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER SRM 52-10-00 FIGURE 18 VOLUME I. OPERATIONS CHECK OF RIGHT HAND MAIN LANDING GEAR FLIPPER DOOR CARRIED OUT AS PER AMM 32-31-00-700-803 FOUND 'SDR 07FDEA03886Stop Fitting · crackedLEFT WING OUTBOARD FLAP SECONDARY UPSTOP FITTING FOUND CRACKED. 10-04-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA03884Structure · crackedRIGHT WING NR 3 SLAT TELESCOPIC DUCT CUTOUT FOUND CRACKED. 10-04-07 REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA03883Stringer · crackedRIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. 10-04-07 STRINGER REPAIRED AS PER FEDEX E.A. 1-5710-113193. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA03202Unknown · odorPASSING 9000FT AFTER T/O CAPT NOTICED FAINT BURNT PAPER ODOR. NO OTHER INDICATIONS, F/O WENT TO COURIER AREA NO FUMES BUT NOTICED EMERGENCY LIGHT ON. CAPT MADE DECISION TO RETURN TO HKG. DECLARED EMERGENCY, UNEVENTFUL LANDING. PANELED SHUTDOWN ENGS TO REMSDR 06FDEA1936Bracket · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759, WINGS RT OUTBOARD TRAILING EDGE FLAP, INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE CORROSION REPAIR. REPAIR CLASSISDR 06FDEA1935Bracket · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759 WINGS RT OUTBOARD TRAILING EDGE FLAP. INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE, CORROSION REPAIR. REPAIR SDR 06FDEA1934Strut · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97760, WINGS OUTBOARD TRAILING EDGE FLAP RT INBD SUPPORT STRUT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR 06FDEA1933Strut · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-97760, TITLE, WINGS OUTBOARD TRAILING EDGE FLAP. RIGSDR 06FDEA1919Fitting · corrodedRT WING - OUTBOARD FLAP, INBOARD HINGE FITTING, INBOARD AFT BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMESDR 06FDEA1918Fitting · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-5SDR 06FDEA1917Fitting · corrodedFOUND RIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING INBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MMSDR 06FDEA1925Strut · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. LEFT HAND WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING AFT HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638, TITLE: WINGS OUTBOARD TRAILING EDGE FLAP, LEFT INBOARD SDR 06FDEA1924Strut · corrodedFOUND LEFT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638. WINGS OUTBOARD TRAILING EDGE FLAP, LEFT HAND ISDR 06FDEA1923Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LT OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORES CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FESDR 06FDEA1922Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD AFT HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FLAP HINGE FORWARD FITTING OUTBOARD AFT HOLE CORROSION REPAIRED AS PER FEDEX E.A. NR 1-5750-99639, TITLE: WINGS LEFT OUTBOARD TRSDR 06FDEA1921Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LH OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GSDR 06FDEA1920Bracket · corrodedFOUND LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99639, TITLE: WINGS LEFTSDR 06FDEA1916Skin · scratchedFORWARD CARGO DOOR CUTOUT, FUSELAGE SKIN ON FORWARD DOOR JAMB FOUND WITH SCRATCHES AT LONGERON 40R. SCRATCH MARK AT FORWARD CARGO DOOR CUT-OUT FUSELAGE SKIN ON FORWARD DOOR JAMB TRIMMED OUT AND CARRIED OUT. REPAIR AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPSDR 06FDEA1914Fitting · corrodedRIGHT WING - OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD LOWER BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MSDR 06FDEA1913Spar Cap · corrodedFOUND LEFT WING, REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. FOUND CORRODED. CORROSION AT LEFT WING REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. REPAIRED AS PER FEDEX EA NR 1-5710-97758, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CEN
Back to N599FE