N598FE
Service difficulty reports · 281
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 = 'N598FE' 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 = 'N598FE' 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 FDEA200911153974Beam · chafedLT MLG STRUT DOOR AFT JAMB FOUND CHAFED. LT MLG STRUT DOOR AFT JAMB CHAFED REPAIR CARRIED OUT IAW EA 1-5710-135652, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.SDR FDEA200911103919Tee Fitting · corrodedRT WING OTBD FLAP, FLAP VANE "T" FITTING FOUND CORROSION. REWORKED AS PER EA 1-5750-135651. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 108.SDR FDEA200911103918Tee Fitting · corrodedRT WING OTBD FLAP, FLAP VANE FITTING NR3 FOUND CORROSION. TEE FITTING REWORKED AS PER EA 1-5750-135650. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 108.SDR FDEA200911103917Tee Fitting · corrodedRT WING OTBD FLAP, FLAP VANE "T' FITTING NR 2 FOUND CORROSION. FITTING REWORKED AS PER EA 1-5750-135649. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 108.SDR FDEA200911103916Tee Fitting · corrodedRT WING OTBD FLAP, FLAP VANE TEE FITTING NR1 FOUND CORROSION. REWORKED AS PER EA 1-5750-135648. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 108.SDR FDEA200911083904Skin · crackedVERTICAL STABILIZER LT SURFACE FOUND CRACKED AT FWD OF REAR SPAR PLANE AT APPROX ZFR 540 AREA. REPAIR CARRIED OUT ON VERT STAB LT SURFACE SKIN AT FWD OF REAR SPAR PLANE AT APROX ZFR 540 IAW EA 1-5530-135661. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 1SDR FDEA200911073885Doubler · crackedCTR LANDING GEAR WHEEL WELL FWD BULKHEAD RT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED IAW SRM 51-33-01 REV 41. NEW DOUBLER MACHINED IAW DWG EA 0526 REV NC. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.SDR FDEA200911063872Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD HOLE FOUND CORROSION. LT INBD FLAP AFT OTBD HINGE PIVOT OTBD HOLE REWORKED IAW EA 1-5750-135627. BUSHING FABRIACTED AND INSTALLED IAW EA 1-5750-135627. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVSDR FDEA200911063870Bushing · wornRT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG INBD BORE BUSHING FOUND WORN. RT INBD FLAP AFT OTBD HINGE PIVOT LUG INBD BORE REWORKED IAW EA 1-5750-135628. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135628. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA200911063869Hinge Bracket · corrodedRT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT FWD AND AFT SPOT FACE FOUND CORROSION. RT OTBD FLAP FWD INBD HINGE LWR MOUNT FWD AND AFT SPOTFACE REWORKED IAW EA 1-5750-135630. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.SDR FDEA200911063868Hinge Bracket · corrodedRT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OTBD LUG, HOLE FOUND CORROSION. RT OTBD FLAP HINGE ACTUATOR HOLE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 65. REPAIR FOUND TO BE ACCEPTED IAW EA 1-5750-76656. BUSHING FABRICATED ANSDR FDEA200911063867Hinge Bracket · corrodedRT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG, HOLE FOUND CORROSION. RT OTBD FLAP FWD OTBD ACTUATOR INBD HOLE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV65. REPAIR FOUND TO BE ACCEPTED IAW EA 1-5750-76656 IAW EA 1-5750-766SDR FDEA200911063866Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD BORE FOUND CORRODED. LT OTBD FLAP FWD INBD HINGE UPPER HINGE UPPER MOUNT INBD BORE REMOVED IAW EA 1-5750-135631. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135631. REPAIR CLASSIFIED AS MAJOR IAW GMSDR FDEA200911063865Bushing · wornLT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR OTBD BORE FOUND BUSHING WORN. LT WING OTBD FLAP FWD OTBD HINGE ACTUATOR OTBD BORE REWORKED IAW EA 1-5750-135629. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135629. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR FDEA200911063864Hinge Bracket · corrodedLT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR, ATTACHMENT INBD LUG, HOLE FOUND CORROSION. LT OTBD FLAP FWD OTBD HINGE ACTUATOR INBD LUG BORE REWORKED IAW EA NR 1-5750-135629. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135629. REPAIR CLASSIFIED ASSDR FDEA200911053863Frame · crackedMAIN DECK CARGO COMPARTMENT RT SIDEWALL STRUCTURE FRAME CRACKED AT STA 1701, LONGERON 12 RT. UPPER CARGO COMPT. RH SIDEWALL STRUCTURE, CRACKED FRAME REPAIR AT STA 1701, L-12R, REPAIR AS PER SRM 53-00-07 FIG. 201 REPAIR 2 REV. 41. REPETITIVE INSPECTION REQSDR FDEA200911053862Frame · dentedMAIN DECK CARGO COMPARTMENT LT SIDEWALL STRUCTURE FRAME DENTED AT STA 1701, LONGERON 12 LT. MAIN DECK CARGO COMPT, LT SIDEWALL STRUCTURE DENTED FRAME AT STA. 1701 L12L, REPAIR CARRIED OUT AS PER SRM 53-00-07 FIG. 201 REPAIR 2 REV. 41. REPETITIVE INSPECTION SDR FDEA200911033805Skin · dentedRT WING NR 1 SLAT LWR SKIN FOUND DENT. RT WING NR1 SLAT LWR SKIN DENT REPAIR SCHEME CARRIED OUT IAW SRM 57-40-01, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108. RT WING NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5 REV 64 FOUND SASDR FDEA200911033807Tee Fitting · corrodedRT WING OTBD FLAP VANE NR 4 TEE SUPPORT FITTING FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5750-135646. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911033806Support Fitting · corrodedRT WING OTBD FLAP VANE NR 2 TEE SUPPORT FITTING FOUND CORROSION. REPAIR CARRIED OUT IAW EA 1-5750-135646. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911023793Skin · dentedRT WING INBD FLAP UPPER SURFACE AT L/E AREA FOUND DENTED AT APPROX X1FH 183.300 AS MARKED. RT WING INBD FLAP UPPER SURFACE AT L/E APPROX XIFH183.300, DENTED AREA MEASURED, DEPTH = 0.065", LENGTH = 1.5" FOUND WITHIN LIMIT IAW SRM 57-00-00 FIG. 206 REV. 41, SDR FDEA200911023792Beam · crackedR3 DOOR FWD LOWEST BEAM FWD STOP FITTING CRACKED. R3 DOOR, CRACKED LOWEST BEAM REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.SDR FDEA200911023791Spar Cap · crackedCRACK INDICATION FOUND DURING HFEC INSP ON LT OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT ON LT LWR VERTICAL STABILIZER FWD OF UPPER REAR SPAR CAP IAW SRM 55-30-02. REPAIR 3 REV 41 AND EA 1-5530-135661. REPAIR CLASSISDR FDEA200809073757Unknown · unknownAFTER TAKEOFF R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIGHT WENT OUT.SDR 08FDEA03757Warning Light · false activationAFTER T/O R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIGHT WENT OUT.SDR FDEA200808153432Cylinder · malfunctionedDURING GEAR RETRACTION- RED GEAR INDICATION REMAINED ILLUMINATED FOR RT MAIN GEAR APPROX 5 SECONDS LONGER THAN OTHER GEAR. REMOVED AND REPLACED RETRACT CYL IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK) CYL REF MM 32-33-02-4. ACCOMPLISHED DSDR 08FDEA03432Cylinder · damagedDURING GEAR RETRACTION RED GEAR INDICATION REMAINED ILLUMINATED FOR RIGHT MAIN GEAR APPROXIMATELY FIVE SECONDS LONGER THAN THE OTHER GEAR. REMOVED AND REPLACED RETRACT CYLINDER IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK) CYLINDER REF MM 32SDR FDEA200807303181Unlock Cylinder · failedGEAR RETRACT AFTER TAKEOFF, RT MAIN UNSAFE ON PRIMARY AND SECONDARY. TOWER STATED RT MAIN GEAR STILL DOWN, OTHERS UP. RAN CHK LIST, NO HELP AFTER GEAR RECYCLE. SETTING UP FOR RTN TO ORIGINAL, HEARD SOUND OF GEAR DOOR CLOSING, UNSAFE LIGHT OUT, GEAR NORMAL OSDR 08FDEA03181Unlock Cylinder · malfunctionedGEAR RETRACT AFTER T/O, RT MAIN UNSAFE A ON PRIMARY AND SECONDARY. TWR STATED RT MAIN GEAR STILL DOWN, OTHERS UP. RAN CHK LIST, NO HELP AFTER GEAR RECYCLE. SETTING UP FOR RTN TO ORIGIN, HEARD SOUND OF GEAR DOOR CLOSING, UNSAFE LIGHT OUT, GEAR NORMAL ON CONFSDR FDEA200807293130Proximity Switch · failedPDIS: AFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK LIST, NO HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHSDR 08FDEA03130Proximity Switch · failedAFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK LIST, NO HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHECK ADSDR 08FDEA02375Trunnion · corrodedDURING CENTER LANDING GEAR REMOVAL FOR REPLACEMENT, THE RIGHT TRUNNION FITTING AFT ATTACHMENT BOLT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5310-122488, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA02302Skin · corrodedAFTER REMOVAL OF LEFT OVERWING FLOOR PANELS FOR WIRING INSPECTION ACCESS FOUND CENTER WING TANK LEFT UPPER TORQUE BOX SKIN APPROXIMATELY AT STA Y1371, XCW113 WITH EXFOLIATION CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA NR 15710-122479, TITLE: WINGS CENTER WSDR 08FDEA02251Fitting · damagedMAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES "B" AND "C" FOUND WITH CRACK FREE CONDITION AFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52". MAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-0SDR 08FDEA02234Seat Track · damagedMAIN DECK SEAT TRACK AT STA 525, X = -8 FOUND HOLE ELONGATED. DAMAGED SEAT TRACK AT MAIN DECK STA 525 TO STA 555, X = -8 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA02233Skin · chafedFORWARD CARGO DOOR CUTOUT LOWER AFT FOUND WITH CHAFFING. CHAFFED MARK ON FORWARD CARGO DOOR CUTOUT LOWER AFT SKIN EDGE BLENDED OUT AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. MATERIAL REMOVED AT EDGE 0.023 INCH. REPAIR CLASSIFIED AS MINORSDR 08FDEA02232Skin · chafedCENTER CARGO DOOR LOWER AFT CUTOUT FOUND CHAFED. CHAFED MARK AT CENTER CARGO DOOR LOWER AFT CUTOUT REPAIRED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA02241Fitting · crackedAFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52 INCH ON MAIN DECK CARGO DOOR SPOOL FITTING NR 2 MOUNTING BOLT HOLE "D" FOUND 2ND LAYER OF DOOR JAMB WITH CRACK INDICATION. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-122486, TITLE: FUSELAGE MAIN CARGO DOOR LOWSDR 08FDEA02240Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 7 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 7 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUTSDR 08FDEA02239Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE C. MAIN DECK CARGO DOOR SPOOL FITTING NR 6 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS SDR 08FDEA02238Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 5 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE D. MAIN DECK CARGO DOOR SPOOL FITTING NR 5 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS SDR 08FDEA02237Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 3 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 3. REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OSDR 08FDEA02236Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 2 FOUND 3RD LAYER CRACK INDICATIONS AT FITTING MOUNTING BOLT HOLES A, C, AND D. MAIN DECK CARGO DOOR SPOOL FITTING NR 2 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARSDR 08FDEA02235Fitting · crackedMAIN DECK CARGO DOOR SPOOL FITTING NR 1 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 1 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10SDR 07FDEA00099Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD CENTER HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00098Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00097Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00096Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00095Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00094Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER CMM 57-52- 04. FLAP ADJUSTMENT REFER TO FEDEX EO 1-5720-7-5001 PT2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
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