N613FE
Service difficulty reports · 422
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 = 'N613FE' 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 = 'N613FE' 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 04FDEA02109Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TSDR 04FDEA02108Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.395 AND REPAIRED AS PER EA NR 1SDR 04FDEA02107Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.096 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE ANDSDR 04FDEA02106Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.507, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EA NR 1-575SDR 04FDEA02105Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.511, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.508 AND REPAIRED AS PER EA 1-5750-77943. SDR 04FDEA02104Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED.SDR 03FDEA00150Spar Cap · corrodedLT WING FWD OF NR 4 SPOILER AREA REAR UPPER SPAR CAP FOUND RIVET PULLED. SNRM NR 112 : WINGS - OUTER WING / REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIR CARRIED OUT AS PER EA 1-5720-67571, PART 1.SDR 03FDEA00149Skin · bulgedLT WING FWD OF NR 5 SPOILER AREA WING REAR UPPER SPAR CAP FOUND SKIN BULGED. OUTER WING/REAR SPAR TRAILING EDGE LT REAR SPAR UPPER CAP REPAIR CARRIED-OUT AS PER FEDEX EA 1-5720-67571 PART 1.SDR 03FDEA00159Skin · corrodedRT WING, TOP SKIN JUST FWD OF FUEL DUMP VALVE PIPE FOUND WITH CORROSION. CENTER OUTER WING, UPPER SKIN CORROSION REWORK CARRIED OUT IAW EA 1-5720-67573.SDR 03FDEA00160Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD BORE FITTING, FOUND CORROSION. TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIR CARRIED-OUT IAW EA 1-5750-67572.SDR 03FDEA00164Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END, OUTBOARD FITTING FOUND CORROSION . WING TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD. FLAP OUTBOARD HINGE BRACKET REPAIR CARRIED OUT IAW E.A. 1-5750-67572.SDR 03FDEA00162Rib · crackedLT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. LT WING LEADING EDGE AND LEADING EDGE DEVICES, RIB INBOARD SLAT TRACK NR 16. SUPPORT FABRICATION CARRIED OUT IAW EA 1-5740-67574. CRACKED RIB REMOVED IAW SRM 51-31-01 VOL. II. AND REPLACED NEW FABSDR 03FDEA00161Rib · crackedRT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. REMOVED AND REPLACED INBOARD STRUCTURAL RIB IAW SRM 51-31-01 SHT.1 VOL. II.SDR 02FDEA00757Tire · damagedAFTER T/O GEAR RETRACTED- NLG MADE LOUD ROTATIONAL NOISE WITH STRONG VIBRATION. PRESSURE 196/199. UP INDICATION OK. FOUND RT NOSE TIRE DAMAGE, (MISSING CORD). R&R RT NOSE TIRE AS REQUIRED.SDR 02FDEA00011Bolt · looseDURING PFM NR 44 CHECK FOUND RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE.SDR 00FDEA00710Seat Track · crackedMAIN DECK SEAT TRACK FOUND CRACK AT BS 635 X = 47.5 RT. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III AND SRM 53-70-00 VOL I.SDR 00FDEA00709Cargo Track · crackedCABIN MAIN DECK CARGO COMPT SEAT TRACK ALONG X = 47 & Y = 635 FOUND WITH LWR FLANGE CRACKED. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III AND SRM 53-70-00 VOL I.SDR 99FDEA00366Seat Track · crackedSNRM 419 MAIN DECK FORWARD CABIN DOOR WAY SEAT TRACK AT BS 655 FOUND CRACKED, X=107-25. CRACK LENGTH APPROX 1 INCH. ** S/D ** AREA SMOOTH AND PROTECTED AS PER SRM 51-21-01 VOL 2. NDT INSP CARRIED OUT. NO CRACK EVIDENT.SDR 98FDEA00276Cadc · malfunctionedSNRM N01247 AT NRT: DURING CLIMB-OUT OF KIX GOT A GPWS TERRAIN WARNING AT 10,000 FT. ESCAPE MANUVER BEGAN FOLLOWED W/WINDSHEAR ALERT. CREW THEN GOT THE STICK SHAKER AND PITCH LIMIT IND. A/C DIVERTED, DUMPED FUEL AND LANDED IN NRT. REMOVED AND REPLACED THSDR 98FDEA00233Air Supply · brokenON CLIMBOUT, ENG NR 1 FIRE WARNING CAME ON. WARNING WENT OUT UPON ENG SHUTDOWN. RETURNED TO RAMP. FOUND TUBE-RS HP RECOUP AIR SUPPLY WAS BROKEN AND MANIFOLD-HPT ACTIVE CLEARANCE CONTROL WAS CRACKED. ALSO, CLAMP JAW WAS BROKEN. REPLACED ABOVE PARTS AND RANSDR 98FDEA00228Duct · cracked98-0083 - ON CLIMB-OUT FROM ANC THROUGH FL 400 ENG 1 FIRE ALERT CAME ON. FOLLOWED EMERGENCY PROCEDURE AND RETURNED TO ANC. ALL ENGINE, HYDRAULIC, PNEUMATIC AND ELECTRICAL SYSTEMS NORMAL. SUSPECT BLEED AIR LEAK IN ENG NR 1. FOUND DUCT IN PYLON CHAFFED BY T/SDR 97FDEA00323Fitting · crackedDURING ROUTINE SERVICE, INSPECTED FWD CARGO COMPARTMENT OMNI ROLLER SUPPORT FITTINGS AT STA Y=943.000. FOUND ONE FITTING WITH AN APPROX .125 INCH LONG CRACK AT FILLET RADIUS. RET DAC SB MD-11-25-212. REMOVED AND REPLACED WITH A NEW OMNI ROLLER SUPPORT FITTIN
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