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 07FDEA00093Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD CENTER BOLT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00074Skin · crackedRIGHT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. CRACK AREA ON THE RIGHT WING TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX EA NR 1-5710-107767, TITLE: WINGS, RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR. REPAIRSDR 07FDEA00068Frame · dentedCABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND CRACKED. CABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYSDR 07FDEA00067Frame · dentedCABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CSDR 07FDEA00066Frame · dentedCABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCSDR 07FDEA00065Frame · dentedCABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCSDR 07FDEA00064Frame · dentedCABIN RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN, RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYSDR 07FDEA00058Seat Track · crackedCABIN STA 755 X = -8.5 SEAT TRACK LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00057Duct · crackedLEFT WING TELESCOPIC DUCT OUTBOARD CUTOUT FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX E.A. #1-5710-107766, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00053Stringer · crackedDURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 13" IN LENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00052Stringer · crackedDURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 13 (XORS 577) WITH APPROX 8" IN LENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00051Stringer · crackedDURING HFEC INSPECTION AT THE RIGHT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 11" IN LENGTH. TRIMMED OUT AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR 05FDEA03257Bearing · wornUPON GEAR EXTENSION DURING APPROACH ALL FOUR GEARS INDICATED UNSAFE AND NO EXTENSION. GEAR HANDLE RECYCLED UP AND DOWN AGAIN WITH GEAR EXTENSION BEING ABOUT ONE FOURTH THE SPEED OF NORMAL GEAR EXTENSION. SEQUENCE OF DOWN AND LOCKED INDICATIONS WERE NOSE, CENSDR 05FDEA02095Skin · delaminatedRIGHT WING, INBOARD FLAP, FLAP VANE INBOARD LOWER SKIN FOUND DELAMINATED. DELAMINATION MEASURES 40.00 INCHES IN LENGTH BY 17.00 INCHES IN WIDTH. REPAIRED IN ACCORDANCE WITH FEDEX EA 1-5750-87555.SDR 05FDEA02076Frame · chafedNR 1 ENGINE, RIGHT HAND THRUST REVERSER COWL T-FRAME AT LOWER 2 BUMPER AREA FOUND WITH CHAFING MARK. CARRIED OUT REPAIR PER FEDEX EA 1-7830-87557. ENGINE THRUST REVERSER - NR 1 ENGINE, RIGHT HAND TEE FRAME WEAR AT 4 AND 5 O' CLOCK POSITIONS - REPAIR. REPAIRSDR 05FDEA02024Static Port · failedFUSELAGE INTERIOR, LT PRIMARY STATIC PORT FAILED WAVINESS TEST. REMOVED AND REPLACED AS PER AMM 34-11-03-4.SDR 05FDEA02004Nose Cowl · damagedNR 1 ENGINE, NOSE INLET COWL INNER BARREL FROM 3, 9 AND 12 O' CLOCK POSITION FOUND DOUBLER WITH SHEARED RIVETS. NR 1 ENGINE, NOSE INLET COWL REMOVED AND REPLACED AS PER AMM 71- 11-01-4.SDR 05FDEA02003Nose Cowl · damagedNR 3 ENGINE, NOSE INLET COWL INNER BARREL FROM 6 TO 9 O' CLOCK POSITION FOUND WITH CORROSION. NR 3 ENGINE, NOSE INLET COWL REMOVED AND REPLACED PER AMM 71-11- 01-4.SDR 05FDEA01983Frame · dentedRT MAIN DECK AFT FUSELAGE FRAME AT STA 1641, BETWEEN LONGERONS L12 AND L13 FOUND WITH DENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 05FDEA01960Seat Track · crackedMAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= - 8.5 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFID AS MAJOR PER GMM 6-2-100.SDR 05FDEA01961Seat Track · crackedMAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= -27 FOUND WITH CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 05FDEA01959Seat Track · crackedMAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= 47 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR 05FDEA01941Seat Track · elongatedMAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK CROWN AT STA 645, X= -47 FOUND ELONGATED.SDR 05FDEA01901Skin · crackedRT WING, LEADING EDGE SKIN AT STA XORS 797 FOUND WITH 17 IN CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 VOLUME I, FIGURE 37.SDR 04FDEA01116Rib · crackedRIGHT WING - NR 16 SLAT TRACK INBOARD RIB SUSPECTED CRACK AS MARKED. RIGHT WING - NR 16 SLAT TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL 2.SDR 04FDEA00965Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE T-FITTING (SECOND FROM INBOARD SIDE) FOUND WITH HOLES CORRODED. TEE FITTING (SECOND FROM INBOARD SIDE) REPAIRED AS PER EA 1-5750-76008.SDR 04FDEA00964Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658.SDR 04FDEA00963Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658.SDR 04FDEA00962Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502, SHT.4, ZONE 40.SDR 04FDEA00961Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOTFACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658, CORROSION REMOVAL AND REPAIR.SDR 04FDEA00960Skin · dentedLT WING DENT MARK FOUND ON OUTBOARD NOSE SURFACE AREA OF SLAT NR 6. DENTED AREA AT LH WING OUTBOARD NOSE SURFACE OF SLAT NR 6 TRIMMED AS PER SRM 57-00-01, FIG.7, VOL. I. REPAIR PARTS FABRICATED & INSTALLED AS PER SRM 57-00-01, FIG.7, VOL.I & SRM 51-35-01,SDR 04FDEA00898Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.SDR 04FDEA00897Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED.SDR 04FDEA00896Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BOLT HOLE AREA SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.SDR 04FDEA00895Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD UPPER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WINGS OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.SDR 04FDEA00894Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD UPPER MOUNT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIRSDR 04FDEA00893Hinge · corrodedRIGHT AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 AND REPAIRED AS PER EA 1-5750-76657 PART 1. INBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (FLAP SIDE) CORROSION REMOVAL ANDSDR 04FDEA00871Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00870Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00869Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DRAWING ARC0502, SHT.4, ZONE 40.SDR 04FDEA00868Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00842Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643, TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00841Hinge · corrodedLT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00840Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BORE SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00839Hinge · corrodedLT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD LOWER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00830Longeron · crackedCENTER CARGO COMPARTMENT CRACKED ON LONGERON SPLICE 51L, STA 5- 123. CRACKED LONGERON SPLICE REMOVED AND REPLACED PER SRM 51-33- 01 VOL IISDR 04FDEA00829Hinge · corrodedLT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR.SDR 04FDEA00828Hinge · corrodedLEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1SDR 04FDEA00827Hinge · corrodedLT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654, LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.SDR 04FDEA00826Hinge · corrodedLEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.
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