N616FE
Service difficulty reports · 267
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 = 'N616FE' 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 = 'N616FE' 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 FDEA200907092547Door Frame · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 6 LWR JAMB FITTING AT HOLES B AND D. REPAIRED IAW EA 1-5310-132150.SDR FDEA200907092546Door Frame · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 6 LWR JAMB FITTING AT HOLE D. REPAIR IAW EA 1-5310-132150.SDR FDEA200907092545Door Frame · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 1 LWR JAMB FITTING AT HOLES A AND C. REPAIR IAW EA 1-5310-132150.SDR FDEA200902110508Terminal · brokenDURING POWER REDUCTION LEVEL 3 ENGINE 2 FIRE ALERT. BEGAN CHECKLIST ALERT/LIGHTS WENT AWAY. ENG 2 FIRE DET FAIL ILLUMINATED. FOLLOWED BY ENGINE FIRE, DETECT FAIL, DETECT FAULT. ALL ALERTS CLEARED EXCEPT ENG 2 FAULT (PREVIOUS WRITE-UP/MEL). ON RETURN, SAMESDR 08FDEA00108Door · chafedRT MLG FLIPPER DOOR FORWARD SIDE FOUND CHAFED. RT MLG FLIPPER DOOR FORWARD SIDE CHAFFED EDGE SMOOTHENED OFF AND FOUND WITHIN LIMIT AS PER SRM 52-00-01 FIGURE 1 VOLUME I. RT MLG AND GEAR WHEEL DOOR OPERATION CHECK CARRIED OUT AS PER AMM 32-31-00-700-803. SDR 08FDEA00107Longeron Splice · crackedCENTER CARGO COMPARTMENT, BILGE AREA, LONGERON SPLICE AT STA 5-123, L-52, FOUND CRACKED ABOUT 6 INCHES. CRACKED LONGERON SPLICE AT CENTER CARGO COMPARTMENT BILGE AREA STA 5-123, LONGERON 52, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFSDR 08FDEA00106Seat Track · corrodedMAIN DECK SEAT TRACK AT STA 1831 - 2007, -X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMENT. REPAIR CARRIED OUT AS PER E.A. 1-5340-117264, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA00105Seat Track · corrodedMAIN DECK SEAT TRACK AT STA 1831 - 2007, X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMENT. 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 08FDEA00075Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION SUPPORT FITTING FOUND CRACK. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2916Seat Track · crackedM/D CARGO LT SEAT TRACK (STA 695, LT, X=27.5) FOUND EDGE UNDER FLOOR CRACKED. REPAIR CARRIED OUT AT M/D CARGO, LH SEAT TRACK (STA 695, LT, X=27.5) PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA2808Skin · damagedCTR CARGO DOOR CUTOUT AFT LOWER SKIN REPAIR DOUBLER EDGE FOUND DAMAGED. REPAIR DOUBLER REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. NEW REPAIR DOUBLER FABRICATED PER SRM 53-50-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA2807Rib · crackedLEFT WING LOWER WINGLET FOUND RIB CRACK. RIB REMOVED AS PER SRM 51-33-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB7774 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA2794Doubler · crackedLEFT WING, LEFT RIB DOUBLER AT XOS 667 FOUND CRACK. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA2793Structure · crackedCRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER 9 AT WING STA XORS 819. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON LT WING TANK, END OF STRINGER 9, WING STA XORS 819 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS SDR 06FDEA2782Doubler · crackedRIGHT HAND WING FIXED L/E RIB DOUBLER FOUND CRACK AT XOS 667. REMOVED PER SRM 51-33-01 VOLUME II. NEW RIB DOUBLER FABRICATED PER DRAWING ARB3954 AND INSTALLED AS PER SRM 51 -33-01 VOLUME II. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.SDR 06FDEA2781Doubler · crackedRIGHT HAND WING FIXED L/E RIB DOUBLER FOUND CRACK AT XOS 667. REMOVED PER SRM 51-31- 01 VOLUME II. NEW RIB DOUBLER FABRICATED PER DRAWING ARB3954 AND INSTALLED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.SDR 06FDEA2780Structure · crackedCRACK FOUND DURING HFEC INSP ON RIGHT WING TANK AT THE END OF STRINGER 42 AT WING STA XORS 629. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RT WING TANK, END OF STRINGER 42, WING STA XORS 629 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIESDR 06FDEA2779Structure · crackedCRACK FOUND DURING HFEC INSP ON RT WING TANK AT THE END OF STRINGER 41 AT WING STA XORS 685. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RH WING TANK, END OF STRINGER 41, WING STA XORS 685 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED ASDR 06FDEA2777Structure · crackedCRACK FOUND DURING HFEC INSP ON RT WING TANK AT THE END OF STRINGER-11 AT WING STA XORS 704. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RH WING TANK, END OF STRINGER 11, WING STA XORS 704 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED ASDR 06FDEA2776Structure · crackedCRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-12 AT WING STA XORS 642. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON LT WING TANK, END OF STRINGER 12, WING STA XORS 642 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIEDSDR 06FDEA2775Structure · crackedCRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-11 AT WING STA XORS 704. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA2774Structure · crackedCRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-10 AT WING STA XORS 760. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA2773Skin · crackedRT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIRED AS PER FEDEX EA1-5730-103532, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA2772Skin · crackedLEFT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIR CARRIED OUT AT LH WING FIXED L/E TELESCOPING DUCT CUTOUT CRACK AS PER FEDEX EA 1-5730-103531. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 05FDEA02691Engine · fluctuatesNR 2 ENGINE DISPLAYED GRADUAL OIL LOSS TO AN INDICATION OF 1 QT JUST BEFORE DESCENT TO KIX. OIL PRESSURE BEGAN TO FLUCTUATE A LITTLE AND DURING DESCENT AN ALERT "OIL PRESS LO" DISPLAYED. PRECAUTIONARY SHUTDOWN PER QRH. NR 2 OIL PRESSURE WAS AROUND 35 PSI WISDR 05FDEA00939Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SKIN PLANK NR 3L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939SDR 05FDEA00926Support Bracket · corrodedFLOOR PANEL SUPPORT BRACKET AT STA 457 LBL 82 FOUND CORRODED. REMOVED IAW SRM 51-35-01 VOL II. FABRICATED NEW SUPPORT IAW DRAWING NR ABA8356 AND INSTALLED IAW SRM 51-33-01 VOL II.SDR 05FDEA00911Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82941.SDR 05FDEA00910Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.SDR 05FDEA00866Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 36L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.SDR 05FDEA00865Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 1R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR 1-5510-7-5000 HAS BEEN COMPLIED WITH.SDR 05FDEA00855Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 33R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.SDR 05FDEA00854Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 4L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.SDR 05FDEA00853Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 2L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.SDR 05FDEA00852Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR29R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.SDR 05FDEA00810Support · crackedRIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT RIGHT WING FIXED LSDR 05FDEA00808Support · crackedLEFT WING, FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT LEFT WING FIXED LEADINSDR 05FDEA00839Skin · corrodedCORROSION REMOVED ON NR 26R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.SDR 05FDEA00838Skin · corrodedCORROSION REMOVED ON NR 14R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.SDR 05FDEA00825Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 27R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.SDR 05FDEA00824Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 23R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.SDR 05FDEA00823Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 17R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.SDR 05FDEA00822Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 15R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.SDR 05FDEA00821Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 13R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.SDR 05FDEA00820Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 5R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82943.SDR 05FDEA00819Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 3R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.SDR 05FDEA00818Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 28L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.SDR 05FDEA00817Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 24L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.SDR 05FDEA00816Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 22L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.SDR 05FDEA00815Skin · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 20L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.
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