N621FE
Service difficulty reports · 288
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 = 'N621FE' 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 = 'N621FE' 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 FDEA200908052904Web · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE B. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.SDR FDEA200908052903Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.SDR FDEA200908052902Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 6 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.SDR FDEA200908052901Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 5 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.SDR FDEA200908052900Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 3 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.SDR FDEA200908052899Web · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SUPPORT FITTING HOLE A. COMPLIED WITH EA1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV.107.SDR FDEA200908042892Vane · delaminatedRIGHT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING - INBD FLAP VANE ASSY REMOVED AND REPLACED IAW AMM 27-50-22-4, REV.64. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV. 64.SDR FDEA200908042891Support · crackedRIGHT WING LEADING EDGE INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB FOUND CRACKED. RT WING L/E INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. NEW RIB SUPPORT FABRICATED IAW DWG ARB2850 REV G. SDR FDEA200901150208Unknown · vibrationAFTER TAKEOFF PASSING 13000 FT IN CLIMB PWR NR 1 ENG STARTED VIBRATING. AT LEVEL OFF PULLED NR 1 THROTTLE TO IDLE AND WHEN PASSING BELOW 80 PERCENT N1 VIBRATION WENT DOWN SIGNIFICANTLY AND AT IDLE NO VIBRATION NOTED. KEPT THROTTLE BELOW 80 PERCENT TO REMAINDSDR 08FDEA00528Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND SEVERAL DENTS AT XIFH 244. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR SDR 08FDEA00466Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = 47.50" CRACKED. 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 08FDEA00465Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -27.50 INCH CRACKED. 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 08FDEA00464Seat Track · corrodedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -8.50" CRACKED. 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 08FDEA00463Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF LOWER CARGO CEILING PANEL FOUND SEAT TRACK AT STA 635, X = 8.50 INCH CRACKED. 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 08FDEA00462Floor Support · crackedMAIN DECK COMPARTMENT, STA 1989, X= 55 FLOOR SUPPORT FOUND CRACKED. SUPPORT REMOVED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA00461Frame · damagedMAIN DECK, FRAME DOUBLER AT RIGHT STA 1701 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES AS PER SRM 53-30-00 FIGURE 1SDR 08FDEA00460Skin · dentedRIGHT WING, INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE FOUND WITH DENT. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT RT WING INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE AS PER SRM 57-10-00 FIGURESDR 06FDEA03097Block · corrodedCENTER LANDING GEAR, LT PILLOW BLOCK AT FORWARD NUT SIDE FOUND SPOTFACE WITH CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK AT FORWARD NUT SIDE SPOTFACE CORROSION REMOVED AND FOUND WITHIN LIMITS PER SRM 53-40-00 VOLUME I, FIGURE 15. THICKNESS OF FSDR 06FDEA03098Trunnion · corrodedCENTER LANDING GEAR, RT TRUNNION AFT HOLE UPPER SURFACE FOUND CORRODED. COMPLIED WITH FEDEX E.A 1-5340-103487, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03092Attach Fitting · corrodedCENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING FOUND MATING SURFACE WITH FITTING CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING MATING SURFACE - PITTING CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER 53-40-00SDR 06FDEA03067Trunnion · crackedNOSE LANDING GEAR, LEFT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECTED CRACKED SNRM NO.: N00556. COMPLIED WITH FEDEX EA NR 1-5310-103482, FUSELAGE, LT NOSE LANDING TRUNNION WEB CRACK. STOP DRILL DEVIATION FROM SRM. REPAIR CLASSIFIED AS MINOR PER GMM 6-2SDR 06FDEA03084Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT. MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1721 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAT INSPECTION RESDR 06FDEA03083Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT SNRM NO.: N00660, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1581 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEASDR 06FDEA03082Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT SNRM NO.: N00659, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1641 LONGERON 12R REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEASDR 06FDEA3084Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT AFA7799-1.SDR 06FDEA3083Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT AFA7819-1.SDR 06FDEA3082Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT AFA7817-1.SDR 06FDEA3067Trunnion · crackedNLG, LT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECT CRACK.SDR 06FDEA03027Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521 SNRM NO.: N00284, LT WING TANK STRINGER 14 AT STA XORS 521 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MSDR 06FDEA03026Stringer · crackedRT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NR N00285, RT WING TANK AT WING STA XORS 704 STRINGER 11, CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED ASDR 06FDEA03025Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 SNRM NO.: N00283, LT WING STA XORS 819 STRINGER 9 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME 1, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GSDR 06FDEA03024Stringer · crackedLT WING, CRACK FOUND APPROX 9" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NO.: N00282, LT WING TANK STA XORS 704 STRINGER 11 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR SDR 06FDEA3024Stringer · crackedLT WING, CRACK FOUND APPROX 9" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 ARB7511.SDR 06FDEA3025Stringer · crackedFOUND LT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 (ARB7509).SDR 06FDEA3026Stringer · crackedRT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704.SDR 06FDEA3027Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC. INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521.SDR 06FDEA03022Skin · crackedRIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED. RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT REPAIR CARRIED OUT PER FEDEX EA NR 1-5730-1013480, WINGS RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING SDR 06FDEA03021Skin · crackedLEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED, SNRM NR N00183. LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA NR 1-5730-103497, WINGS, LT WING LEADING EDGE SKIN CRACKSDR 06FDEA3021Structure · crackedLEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.SDR 06FDEA3022Structure · crackedRIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.SDR 05FDEA01372Panel · corrodedHORIZONTAL STABILIZER RIGHT HAND FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83008.SDR 05FDEA01296Spar Cap · corrodedHORIZONTAL STABILIZER RIGHT HAND AFT SPAR CAP NR 36R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83007.SDR 05FDEA01295Panel · corrodedHORIZONTAL STABILIZER RT FORWARD PLANK NR 14R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.SDR 05FDEA01286Bulkhead · crackedCENTER CARGO STA 1841 FLOOR AREA BULKHEAD APPROX X= -23 WEB FOUND CRACKED. CRACKED WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= -23 CUT AT STA 1841 X= -23 AND REMOVED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR WEB AND DOUBLER FABRICATED AND INSTALLSDR 05FDEA01284Stiffener · crackedCENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= -25 VERTICAL STIFFENER FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW STIFFENER FABRICATED AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED AS MINOR SDR 05FDEA01285Bulkhead · crackedCENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= 3 WEB FOUND CRACKED. CRACKED AREA OF WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= 3 TRIMMED OUT AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRMSDR 05FDEA01269Seat Track · crackedMAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 05FDEA01268Splice · crackedCENTER CARGO - RIGHT HAND UTILITY TUNNEL AT STA 1531 L-37 RIGHT HAND LONGERON SPLICE FOUND CRACK. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED MAJSDR 04FDEA03133Warning Light · illuminatedON CLIMB-OUT AT 14K MSL ENG 2 A-ICE DUCT LEVEL 3 ALERT WITH AURAL WARNING. FOLLWED QRH CHECKLIST AND SHUTDOWN NR 2 ENGINE RETURN TO ONT. OPENED NR 2 ENGINE COWLS FOR INSPECTION, REMOVED ANTI-ICE VALVE HEAT SHIELD, AND REMOVED TWO DUCT ELBOW JOINT HEAT SHIELDSDR 04FDEA02658Detector · burstON T/O, PRIOR TO FLAP RET, A/C DISPLAYED A MOMENTARY LVL 3 ENG 2 A-ICE DUCT ALERT. AS THROTTLE WAS BEING MOVED TO IDLE ALERT WENT AWAY. CLIMB TO FL 290 WAS UNEVENTFUL UNTIL 30 MIN INTO FLT WHEN A/C DISP LVL-1 ENG 2 A-ICE OFF ALERT, WITH A CONS OF ENG 2 A-
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