N421FE, cancelled Feb 18, 2016
Service difficulty reports · 97
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 = 'N421FE' AND deregistration_id = 'N421FE-2016-02-18' 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 = 'N421FE' AND deregistration_id = 'N421FE-2016-02-18' 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 FDEA200904171573Frame · damagedAFT CARGO COMPARTMENT, EXISTING HOLES WRONGLY DRILLED AT FR 63A, STGR 27 RT. THE FRAME WAS REPAIRED AS PER SRM 53-17-13 FIG 203.SDR FDEA200904061439Seat Track · corrodedSEAT TRACK WITH CORROSION BTW FR 72 AND FR 73 AT Y0. SEAT TRACK REPAIRED AS PER SRM 53-10-16 FIG 202.SDR FDEA200904061427Seat Track · corrodedSEAT TRACK WITH CORROSION BETWEEN FR 76 AND FR 77 AT Y1448. SEAT TRACK REPLACED AS PER SRM 51-72-10.SDR FDEA200904031552Seat Track · corrodedSEAT TRACK WITH SPOTS OF CORROSION BETWEEN FR72-73 AT Y-1456. THE SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200904021444Skin · damagedFUSELAGE, EVALUATE BLENDING AT STGR 43 LT BTW FR 20 AND FR 21. SKIN WAS REPAIRED AS PER SRM 53-10-12 FIG 216 SHEET 1.SDR FDEA200904021438Seat Track · corrodedSEAT TRACK WITH SPOTS OF CORROSION BTW FR 69-FR 70 AT Y-450. SEAT TRACK REPAIRED BTW FR 68-69 AS PER SRM SUPP 53-10-16 FIG 202.SDR FDEA200904021436Seat Track · corrodedSEAT TRACK WITH SPOTS OF CORROSION BTW FR58-69 AT Y-953. SEAT TRACK WAS REPAIRED BTW FR 62-63 AND BETWEEN FR 64-65 AS PER SRM 53-10-16 FIG 202.SDR FDEA200904021435Seat Track · corrodedSEAT TRACK WITH SPOTS OF CORROSION BTW FR 69-71, AT Y-953. THE SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903311709Floorbeam · corrodedN1322 AFT CARGO COMPT - FLOORBEAM WITH CORROSION AT FR 63 AND BTW 44-55 LH. THE BEAM WAS REPLACED IN ACCORDANCE WITH 51-72-10.SDR FDEA200903301737Hinge Fitting · corrodedAFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 63. THE FITTING WAS REPAIRED AS PER EA 6-5310-129288.SDR FDEA200903301736Hinge Fitting · corrodedAFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 62. THE FITTING WAS REPAIRED AS PER FEDEX EA 6-5310-129288.SDR FDEA200903301429Seat Track · wornSEAT TRACK WITH WEAR BETWEEN FR62-63 AT Y0. SEAT TRACK REPAIRED BTW FR 62 AND FR 63 AND BETWEEN FR 64 AND FR 65 AS PER SRM SUPP 53-10-16 FIG 202.SDR FDEA200903301426Seat Track · corrodedSEAT TRACK WITH CORROSION AND WEAR BETWEEN FR 54.2 AND FR 58 AT Y450. THE RELEVANT SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903271554Roller Track · corrodedTRACK AT ROLLERS LT SIDE BTW FRAMES 54.2 TO 55 AT STGR 43 WITH CORROSION. ROLLER TRACK REPAIRED AS PER SRM 53-10-15 FIG 203.SDR FDEA200903261407Fitting · corrodedRT WING FLAP OTBD, FITTING AT BUSHINGS OF NR 4 TRUNNION WITH CORROSION. THE CORROSION WAS BLENDED AS PER EA 6-5710-127419.SDR FDEA200903251742Skin · corrodedCENTER WING BOX LOWER SKIN EXTERNAL SURFACE FOUND WITH SEVERAL SPOTS OF CORROSION - REFER TO EA6-5710-129280 FOR DETAILS. REPAIR WAS ACCOMPLISHED AS PER EA 6-5710-129280.SDR FDEA200903251425Crossbeam · crackedCROSSBEAM AT FR36 CRACKED AT Y-953. CROSSBEAM AT FR 36 WAS REPAIRED AS PER SRM SUPP 53-10-15 FIG 201 SHEET2A.SDR FDEA200903251406Floorbeam · corrodedZONE 100 - FUSELAGE - PREVIOUS REPAIR AT FLOORBEAM LOCATED AT FR 55/58 AT Y-1200. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS REMOVED BECAUSE THE FLOORBEAM WAS REPLACED AS PER THSDR FDEA200903241734Beam · corrodedRT FWD PAX DOOR - SPOTS OF CORROSION AT BEAM 3. BEAM 3 WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903241668Beam · corrodedRT FWD PAX DOOR, SPOTS OF CORROSION AT BEAM 3. BEAM 3 WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903241442Track · corrodedNR 1 PYLON, RIB 18, LUG ATTACHMENT WING TO PYLON WITH CORROSION AT ATTACHMENT ROLLER TRACK OF BEARING. REPAIR ACCOMPLISHED AS PER FEDEX EA 6-5450-127411.SDR FDEA200903231708Floorbeam · corrodedN938 AFT CARGO COMPT - FLOORBEAM AT FRAME 55/58 WITH SEVERAL SPOTS OF CORROSION BTW STGR 44 AND 45LH- THE FLOORBEAM WAS REPLACED IN ACORDANCE WITH SRM 51-72-10.SDR FDEA200903231437Fitting · corrodedFWD COMPT, CORROSION FOUND BETWEEN FRAMES 24 TO 25 AND STGR 55 RT TO 53 LT. THE FITTING WAS REPAIRED AS PER EA 6-5310-127421.SDR FDEA200903231434Skin · crackedCOCKPIT PLATE FOUND CRACKED AT COCKPIT FLOOR NEXT TO Y-790 BTW FR 0 AND FR 1. THE CRACKED PANEL WAS REPAIRED AS PER FEDEX EA 6-5310-127415.SDR FDEA200903231430Seat Track · wornSEAT TRACK NEXT TO Y0, NEXT TO FR 33 FOUND WORN. SEAT TRACK REPAIRED AS PER FEDEX EA 6-5310-127412.SDR FDEA200903231402Floor Support · corrodedBULK CARGO COMPT, RT FLOOR PANELS LONGITUDINAL SECTION WITH CORROSION AT FR 67 AND FR 65 UNDER STRINGER 49. SECTION LONGITUDINAL WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903211404Floorbeam · corrodedBULK COMPT, CORROSION AT BULK CARGO COMPT FLOORBEAM AT FR 65 ABOVE STRINGER 49 RT. FLOORBEAM REPLACED AS PER SRM 51-72-10.SDR FDEA200903211403Floorbeam · corrodedBULK COMPT - CORROSION AT BULK COMPT FLOORBEAM OF FR 64 ABOVE STRINGER 49 RT. FLOORBEAM WAS REPLACED AS PER SRM 51-72-10.SDR FDEA200903191551Skin · dentedRT WING AILERON, LOWER SKIN FOUND DAMAGED. LOWER SKIN OF AILERON REPAIRED IN ACCORDANCE WITH SRM 57-61-12 FIG 201.SDR FDEA200903191555Track · misrepairedPREVIOUS REPAIR (DUMMY TRACK) FOUND LOCATED BETWEEN FR 38.1 AND FR 40 AT Y0. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPSDR FDEA200903191209Stringer · misrepairedAREA 100, FUSELAGE, PREVIOUS STRINGER REPAIR FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 51 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPSDR FDEA200903191208Stringer · misrepairedAREA 100 - FUSELAGE - PREVIOUS REPAIR AT STRINGER FOUND LOCATED BTW FR21 AND FR 22 AT STGR 50 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRMSDR FDEA200903191207Stringer · misrepairedAREA 100, FUSELAGE, PREVIOUS REPAIR (STRINGER) FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 49 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTSDR FDEA200903191206Stringer · misrepairedAREA 100, FUSELAGE, PREVIOUS REPAIR FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 48 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEWSDR FDEA200903171433Skin · wornLT WING FIX LEADING EDGE BTW SCREWJACK 3 AND SCREWJACK 4 WITH WEAR. FIX L/E REPAIRED AS PER EA 6-5710-127425.SDR FDEA200903161574Roller Track · misrepairedPREVIOUS REPAIR FOUND ON ROLLER TRACK LOCATED BTW FR 22-23 AT Y-100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WASDR FDEA200903161564Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED BETWEEN FR 38.1 AND 38.2, BTW STGR 54 LT AND 50 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING APPROVED SDR FDEA200903161553Skin · misrepairedPREVIOUS REPAIR AT INBD FLAP LOWER SKIN LOCATED BETWEEN RIB 7 AND RIB 9. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WASDR FDEA200903161443Structure · misrepairedFUSELAGE, PREVIOUS REPAIR FOUND LOCATED BTW FR 23 AND FR 24 BTW STGR 49 RT AND 52 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR EVALUATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING FEDEX EASDR FDEA200903161440Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED BETWEEN FR 20 ANBD FR 21 STGR 47 LT AND STGR 51 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NESDR FDEA200903161432Skin · corrodedTHS - SUPERFICIAL CORROSION AT BASE OF HOLES NR 2 AND NR 3 OF GROUP A, RT SIDE. CORROSION BLENDED OUT AS PER EA 6-5510-127414.SDR FDEA200903161431Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED AT FR 13 STGR 28 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NO TO CONFORM TO AN SRM REPAIR, NEW REPAIR WAS ACCOMPLISHED AS PER SDR FDEA200903161405Floorbeam · corrodedAREA 100 - PREVIOUS REPAIR AT FLOORBEAM FOUND LOCATED AT FR 63 BTW Y420 AND Y-420. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS REMOVED BECAUSE THE FLOORBEAM WAS REPLACED DUE TO SSDR FDEA200903161401Crossbeam · misrepairedN542 - FUSELAGE - PREVIOUS REPAIR IN CROSSBEAM LOCATED BETWEEN FR 36 AT Y1680. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAISDR FDEA200903161400Crossbeam · misrepairedN544 - FUSELAGE - PREVIOUS REPAIR AT CROSSBEAM LOCATED BETWEEN FR 37 AT Y1680. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW RSDR FDEA200901150215Dampener · leakingAIR TURN BACK DUE TO GEAR WOULD NOT RETRACT IN SYS 1 OR 2. ECAM L/G RETRACTION FAULT, LANDED AT 266.9 NOT OVERWEIGHT. ON WALK AROUND FOUND RT PITCH DAMPNER TRIPPED. ACFT BEING MOVED TO THE HANGAR FOR JACKING. REMOVED AND INSTALLED SERVICEABLE RT MLG PITCH SDR FDEA200810154371Engine · failedNUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPROVSDR 08FDEA04371Engine · hung startNUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPSDR 07FDEA01075Floorbeam · corrodedMDCC FLOORBEAM AT FR 14 LT 64 INCHES FROM CENTER HAS 1 SPOT OF CORROSION ON FORWARD BOTTOM FACE 15" LONG BY 1" WIDE. REMOVED CORROSION IAW SRM 51-74-10 CHECKED LIMITS IAW SRM 53-12-15, OUT OF LIMITS. FABBED REPAIR IAW A310/200 SRTM 53-12-15 PB210 FIG 201. RSDR 07FDEA01074Floor Support · crackedUPON REMOVAL OF CEILING PANEL 131EC FOR AGING ACFT INSPECTION, FOUND MDCC FLOOR SUPPORT C36 BETWEEN L4 AND L5 SEAT TRACK TO BE CRACKED TOP OF VERTICAL STIFFENER LENGTH OF CRACK .400 INCH ROUTED OUT CRACK IAW A310/200 SRM 53-10-15. FABRICATED 2 REPAIR ANGLES
Back to N421FE, cancelled Feb 18, 2016