N596FE
Service difficulty reports · 417
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 = 'N596FE' 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 = 'N596FE' 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 FDEA200903301105Fitting · corrodedCORROSION, HOLE FOR OTBD FLAP VANE FITTING D ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128674. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301104Fitting · corrodedCORROSION, HOLE FOR OTBD FLAP VANE FITTING F ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128673. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301100Fitting · corrodedCORROSION-HOLE FOR OUTBD FLAP VANE FITTING E ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128671. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301099Fitting · corrodedCORROSION-HOLE FOR OUTBD FLAP VANE FITTING C ECENTRIC ADJUST RETAINER. REPAIR CARRIED OUT AS PER EA 1-5750-128672. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200903291097Seat Track · crackedCRACK-MAIN DECK SEAT TRACK AT STA 635 X=-8.5. CARRIED OUT SECTIONAL REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903271090Fuel Tank · corrodedCABIN, CENTER TANK UPPER SKIN AT STA 1229 X= -80 TO -90 FOUND CORROSION. REPAIRED AS PER EA 1-5710-128664. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903271089Fuel Tank · corrodedCABIN, CENTER TANK UPPER SKIN AT STA 1234 X= -70 TO -80 FOUND CORROSION. REPAIRED AS PER EA 1-5710-128664. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903271088Fuel Tank · corrodedCABIN, CENTER TANK UPPER SKIN AT STA 1229 X= -70 TO -80 FOUND CORROSION. REPAIRED AS PER EA 1-5710-128664. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.SDR FDEA200903271087Fuel Tank · corrodedCABIN, CENTER TANK UPPER SKIN AT STA 1229 X= -50 TO -60 FOUND CORROSION. REPAIRED AS PER EA 1-5710-128664. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.SDR FDEA200903271086Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE OUTBD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA NR 1-5750-128663. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903271085Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE INBD ACTUATOR HOLE FOUND CORROSIONS. REPAIRED AS PER E.A. 1-5750-128663. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903261049Longeron Splice · crackedCRACK, LONGERON SPLICE FITTING STA 5-123 S-7L AROUND FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW LONGERON SPLICE FITTING FABRICATED AS PER DRAWING A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISIONSDR FDEA200903261048Longeron Splice · crackedCRACK, LONGERON SPLICE FITTING STA 5-123 S-24R AROUND FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW LONGERON SPLICE FITTING FABRICATED AS PER DRAWING A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISIONSDR FDEA200903261047Longeron Splice · crackedCRACK, LONGERON SPLICE FITTING STA 5-123 S-25R AROUND FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW LONGERON SPLICE FITTING FABRICATED AS PER DRAWING A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISIONSDR FDEA200903261046Longeron Splice · crackedCRACK LONGERON SPLICE FITTING STA5-123 S-6L AROUND FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW LONGERON SPLICE FITTING FABRICATED AS PER DRAWING A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION SDR FDEA200903261045Frame · dentedDENT, MAIN FRAME STA5-73 BETWEEN S-12R TO S-13R. REPAIRED AS PER SRM 53-30-00 FIGURE 1, VOLUME I, REVISION 40. REPETITIVE INSPECTION REQUIRE. INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1, VOSDR FDEA200903251033Longeron Splice · crackedCRACK-LONGERON SPLICE FITTING AT STA5-123 S33R IN CENTRE CARGO COMPARTMENT. CARRIED OUT REPAIR BY SECTIONAL LONGERON REPLACEMENT AS PER SRM 53-10-00 FIGURE 2, VOLUME I, REVISION 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903251032Longeron Splice · crackedCRACK-LONGERON SPLICE FITTING AT STA5-123 S38R IN CENTRE CARGO COMPARTMENT.SDR FDEA200903251031Longeron Splice · crackedCRACK-LONGERON SPLICE FITTING AT STA1531/5-123 S37R IN CENTRE CARGO COMPARTMENT. REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-33-01 VOLUME II, REVISION 40. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7114, REVISION J. REPAIR CLASSIFIED SDR FDEA200903241021Skin · dentedDENT, RT INBD FLAP LEADING EDGE AT XIFH284. SMOOTHENED AS PER SRM 51-21-01 VOL. II REV. 40 AND FOUND WITHIN LIMIT AS PER SRM 57-00-01 FIG. 2 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903241020Seat Track · wornWORN, SEAT TRACK AT MAIN DECK STA1431 X= 47.5. REPAIRED BY SECTIONAL REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903241019Seat Track · corrodedCORROSION, SEAT TRACK AT MAIN DECK STA 1361 TO STA 1371 X= 75.5. REPAIRED BY SECTIONAL REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903241018Seat Track · wornWORN, SEAT TRACK AT MAIN DECK STA5-48 X= 47.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200903241017Seat Track · corrodedCORROSION, SEAT TRACK AT STA1355 X=-75.5. REPAIR AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40 (MAJOR REPAIR).SDR FDEA200903231011Longeron Splice · crackedCRACKED LONGERON SPLICE FITTING AT STA 1991 48L OF WASTE FITTING. FITTING REPLACED AS PER SRM 51-31-01 VOL 2 REV 40 (MAJOR REPAIR).SDR FDEA200903231010Hinge Bracket · corrodedCORROSION, OTBD HOLE AT LOWER MOUNT OF LT WING OUTBD FLAP OTBD HINGE. REPAIRED AS PER EA 1-5750-127793. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903231009Hinge Bracket · corrodedCORROSION, HOLE AT INBD ACTUATOR HOLE OF LT WING OTBD FLAP OTBD HINGE. REPAIR AS PER CMM 57-44-09 REV 63 (MINOR REPAIR).SDR FDEA200903231008Hinge Bracket · corrodedCORROSION, HOLE AT OTBD ACTUATOR HOLE OF RT WING OTBD FLAP INBD HINGE. REPAIRED AS PER EA NR 1-5750-127794. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903231007Hinge Bracket · corrodedCORROSION AT STRUCTURE AT INBD ACTUATOR ATTACH OF RT WING OTBD FLAP INBD HINGE. REPAIRED AS PER EA 1-5750-127794. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200903231006Seat Track · crackedCRACK, SEAT TRACK AT STA635 X=47.5. REPAIR AS PER SRM 53-70-00 FIG1 VOL1 REV40 (MAJOR REPAIR).SDR FDEA200903231005Seat Track · crackedCRACK, SEAT TRACK AT STA 755 X=8.5. REPAIR AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40 (MAJOR REPAIR).SDR FDEA200903231004Support Fitting · crackedCRACK, HOLES AT SUPPORT FITTING NR 7 OF MAIN DECK CARGO LOWER DOOR JAMB. FITTING REPLACED AS PER SRM 51-31-01 VOL2 REV40 (MAJOR REPAIR).SDR FDEA200903231003Support Fitting · crackedCRACK, HOLES AT SUPPORT FITTING NR 6 OF MAIN DECK CARGO LOWER DOOR JAMB. FITTING REPLACED AS PER SRM 51-31-01 VOL2 REV40 (MAJOR REPAIR).SDR FDEA200903231002Support Fitting · crackedCRACK, HOLES AT SUPPORT FITTING NR 5 OF MAIN DECK CARGO LOWER DOOR JAMB. FITTING REPLACED AS PER SRM 51-31-01 VOL2 REV40 (MAJOR REPAIR).SDR FDEA200903231001Support Fitting · crackedCRACK, HOLES AT SUPPORT FITTING NR 4 OF MAIN DECK CARGO LOWER DOOR JAMB. BUSHING REPAIR AS PER SRM 53-50-00 VOL1 REV40 (MINOR REPAIR).SDR FDEA200903231000Support Fitting · crackedCRACK, HOLES AT SUPPORT FITTING NR 3 OF MAIN DECK CARGO LOWER DOOR JAMB. FITTING REPLACED AS PER SRM 51-31-01 VOL2 REV40 (MAJOR REPAIR).SDR FDEA200903220998Support Fitting · crackedCRACK, AT SUPPORT FITTING NR 1 OF MAIN DECK LOWER DOOR JAMB. FITTING REPLACED AS PER SRM 51-31-01 VOL2 REV40 (MAJOR REPAIR).SDR FDEA200903190971Skin · dentedDENT, RT WING INBD FLAP LEADING EDGE AT XIFH167. MINOR REPAIR AS PER EA 1-5750-127809.SDR FDEA200902250724Door · missingON ARRIVAL FROM BOM FOUND RT AFT CTR GEAR DOOR MISSING AND LT AFT CENTER MLG DOOR AND GEAR BAY SHIELD DAMAGED. REPLACED MISSING RT CENTER MLG DOOR. R & R LT CENTER MLG DOOR IAW MM 32-17-04. R & R CENTER MLG DEFLECTOR IAW MM 32-17-06-4 REPLACED MISSING FASDR FDEA200902240681Downlock · failedON DEPARTURE RT MAIN GEAR SHOWED UNSAFE. YAW WAS PRESENT. ONCE GEAR WAS CYCLED TO DOWN POSITION GEAR IMMEDIATELY INDICATED GREEN. ALL INDICATIONS WERE THAT GEAR REMAINED IN DOWN POSITION ON DEPARTURE WITH GEAR HANDLE IN THE UP POSITION. BOTH GREEN/RED GEARSDR FDEA200902150521Restrictor Valve · failedAFTER TAKEOFF RT MLG SHOWED RED WITH GEAR HANDLE UP. BOTH PRIMARY AND SECONDARY INDICATIONS. ALSO RECEIVED VISUAL CONFORMATION FROM ANOTHER AIRCRAFT THE GEAR WAS FULLY DOWN. RAN THE QRH PROCEDURES AND LOWERED THE GEAR AND THE RT MAIN IMMEDIATELY SHOWED GRESDR 07FDEA04479Skin · dentedLEFT WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE FOUND DENT. 10-12-07 REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA04385Seat Track · corrodedCABIN, LBL 8 STA 1885 SEAT TRACK FOUND CORRODED. 10-12-07 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 07FDEA04384Frame · chafedMAIN DECK COMPARTMENT AT STA 1701 STRINGER 12R AREA FRAME EDGE FOUND CHAFED. 10-9-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTIONS REQUIRED AT EVERYSDR 07FDEA04383Frame · chafedMAIN DECK CARGO COMPARTMENT AT STA 1761 STRINGER 12L AREA FRAME FOUND CHAFED. 10-9-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 9,500 SDR 07FDEA04379Doubler · crackedRIGHT WING FIXED LEADING EDGE LOWER ANGLE DOUBLER AT XOS 546 FOUND CRACKED. 10-16-07 RT WING FIXED LEADING EDGE LOWER ANGLE CRACKED DOUBLER AT XOS 546 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.SDR 07FDEA04378Access Panel · crackedRIGHT WING LEADING EDGE ACCESS PANEL 618GB INBOARD SUPPORT FOUND CRACKED. 10-16-07 RIGHT HAND WING LEADING EDGE ACCESS PANEL 618GB CRACKED INBOARD SUPPORT STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX SDR 07FDEA04377Skin · dentedLEFT WING INBOARD FLAP, INBOARD SEGMENT LOWER SKIN FOUND DENT MARKS. 10-9-07 DENTED AREA MEASURED, DIAMETER = 2" AND DEPTH = 0.058" FOUND ACCEPTABLE AS PER SRM 57-10-00 FIGURE 17 VOLUME I. HFEC INSPECTION CARRIED PER DAC SPM REV13, 06-10-01.001 AND NO CSDR 07FDEA04376Skin · dentedLEFT WING INBOARD FLAP, INBOARD SEGMENT UPPER SKIN FOUND DENT MARKS. 10-9-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.SDR 07FDEA04375Angle · crackedLT WING FIXED LEADING EDGE, XOS 602, LOWER ANGLE FOUND CRACKED. 10-9-07 REMOVED ANGLE AS PER SRM 51-33-01 VOLUME II AND FABRICATED NEW ANGLE DOUBLER AS PER DRAWING ARB 2933. INSTALLED NEW ANGLE DOUBLER AT LT WING FIXED LEADING EDGE , XOS 602, LOWER
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