N456FE, cancelled Apr 23, 2020
Service difficulty reports · 79
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 = 'N456FE' AND deregistration_id = 'N456FE-2020-04-23' 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 = 'N456FE' AND deregistration_id = 'N456FE-2020-04-23' 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 FDEA201204011216Actuator · failedREJECTED TAKEOFF FOR SPEED BRAKE GROUND SPOILER DEPLOYMENT AT 110KTS. GROUND SPOILER NR1 ON LT WING SHOWED DEPLOYED AMBER CHEVRON AFTER REJECT. TROUBLESHOOTING BACK AT GATE SHOWED NR 1 GROUND SPOILER DEPLOYED ON ECAM BUT STOWED ON ACFT. ACFT HAD A PRIOR SPSDR FDEA201112035135Pressure Switch · failedREJECTED TAKE OFF AT 85KTS DUE TO ECAM WARNING WARNING, LOW OIL PRESSURE ENGINE NR 2. WARNING WENT AWAY WHEN THROTTLES RETARDED. CHECKED ALL ENGINE PARAMENTERS PRIOR TO 2ND TAKE OFF. ALL NORMAL, 2ND TAKE OFF NORMAL. R & R NR 2 ENGINE OIL PRESSURE TRAMSMISDR FDEA201012054591Regulator Valve · failedGOT HIGH OIL PRESSURE NR 2 ENG ON T/O ROLL. REJECTED T/O AT LOW SPEED. SECOND TAKEOFF NORMAL. 1ST T/O 62PSI, 2ND T/O 58 PSI. R & R 2 ENGINE OIL PRESSURE REGULATOR VALVE REF AMM 79-21-04-04-0. PERFORMED OIL PRESSURE TEST NR 7, REF 71-00-00, RAN NR2 ENGINE IAW SDR FDEA201012034558Oil Cooler · false activationGOT HIGH ENG OIL PRESSURE NR 2 ENG ON T/O ROLL. REJECTED T/O INDICATIONS WERE BACK TO NORMAL AFTER EXITING RUNWAY. RAN NR 2 ENG IAW JRH. NO DEFECTS NOTED. OIL NEVER ROSE ABOVE 58 PSI WITH THROTTLE ADVANCED AND WAS 50 TO 52 PSI AT IDLE. OIL TEMP WAS ALSO WISDR FDEA201011164395Skin · damagedLT WING - INBD FLAP - T/E SKIN FOUND DAMAGED. DUE TO NON APPROVED EXISTING REPAIRS THE T/E HAD TO BE REPLACED.SDR FDEA201011154373Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BTW RIB11/15 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.SDR FDEA201011154372Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BTW RIB4/5 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.SDR FDEA201011154371Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BETWEEN RIB13/15 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.SDR FDEA201011124326Skin · damagedPREVIOUS REPAIR FOUND AT LT INBD FLAP LOWER SKIN BTW STGR 13 & REAR SPAR AND RIBS 12/14. NEW REPAIR PERFORMED IAW EA 6-5750-144069. REPAIR NR2.SDR FDEA201011124320Skin · corrodedFWD CARGO COMPARTMENT DOOR - LOWER INTERNAL SKIN FOUND CORRODED. PANEL SKIN WAS REPLACED AS PER SRM 51-72-10.SDR FDEA201011104311Skin · crackedFWD CARGO DOOR - CRACK FOUND AT INNER PLATE AT LOWER AFT CORNER. INNER SKIN REPAIRED IAW 6-5230-144190.SDR FDEA201010284186Crossbeam · corrodedAFT CARGO COMPT FLOOR - TRANSVERSAL BEAM AT FR58 FOUND CORRODED. CROSSBEAM WAS REPLACED IAW 51-72-10.SDR FDEA201010254163Fitting · corrodedFITTING LOCATED AT L1 DOOR FOUND CORRODED. REPLACED BY A NEW ONE.SDR FDEA201010254162Crossbeam · damagedFWD CARGO COMPARTMENT - CROOSBEAM UPPER FLANGE AT FR36 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIGURE207.SDR FDEA201010254161Crossbeam · damagedFWD CARGO COMPARTMENT - CROSSBEAM UPPER FLANGE AT FR25 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIG 207.SDR FDEA201010214133Skin · dentedPREVIOUS REPAIRED DENTS NOT LISTED IN THE MCMRT AT RT FLAP INBD LOWER SKIN. DENT 1 - BTW RIB 5 & RIB 6 AND BTW FRONT SPAR & STRINGER 9. DENT 2 AND DENT 3 - BTW RIB 10 & RIB 11 AND STRINGER 11 & REAR SPAR. REPAIR OF THE DENTS IAW EA 6-5710-50143.SDR FDEA201010214132Frame · misrepairedFWD CARGO COMPARTEMENT - PREVIOUS REPAIR FOUND AT FR20A NOT IAW FAA APPROVED DATA. NEW REPAIR TO THE FR20A PERFORMED IAW EA 6-5310-144063.SDR FDEA201010184101Fitting · misrepairedMAIN DECK FLOOR STRUCTURE - PREVIOUS REPAIR FOUND AT FITTING LOCATED BTWN FR11 & FR15A AT Y 1500. REPAIR DOES NOT CONFORM WITH AN EXISTING SRM REPAIR. FLOOR FITTING WAS REPLACED IAW SRM 51-72-10.SDR FDEA201010144063Skin · dentedRT WING - SLAT NR1 L/E - PREVIOUS DENT FOUND AT RIB 4. EVALUATED AND FOUND TO BE CONFORM WITH EA 6-5710-50155. DENT WAS FILLED USING THE GUIDELINES OF SRM 51-73-10.SDR FDEA201010144062Seat Track · corrodedSEAT TRACK Y954 FOUND CORRODED BTW FR18 & FR19. SEAT TRACK REPLACED BY A NEW ONE.SDR FDEA201009303810Skin · corrodedRT THS TOP SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT STGR9 FOUND CORRODED BTW RIB3 & RIB4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR FDEA201009303809Skin · corrodedRT THS TOP SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT STGR10 FOUND CORRODED BTW RIB3 & RIB4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR FDEA201009303808Skin · corrodedLT THS BOTTOM SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT STGR11 FOUND CORRODED BTW RIB3 & RIB4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR FDEA201009303807Skin · corrodedRT THS BOTTOM SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT STGR9 FOUND CORRODED BTW RIB3 & RIB4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR FDEA201009303806Skin · corrodedRIGHT THS TOP SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT S11 FOUND CORRODED BTW RIB 3 & RIB 4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR FDEA201009303805Skin · misrepairedBULK CARGO DOOR - PREVIOUS REPAIR FOUND AT INTERNAL SKIN, LOCATED BTW FR67 & FR69 AND BTW BEAM1 & BEAM4, NOT CONFORM WITH SRM. NEW REPAIR WAS PERFORMED IAW SRM 52-30-00, FIG 206.SDR FDEA201009273738Skin · debondedRT OTBD FLAP - LOWER SKIN BTW RIB2 AND RIB3 FOUND DEBONDED. REPAIRED IAW E.A. 6-5750-144062.SDR FDEA201009273737Skin · debondedFLAP OTBD RT - LOWER SKIN SURFACE BTW RIB7 AND RIB 9 FOUND DEBONDED. FLAP OUTBOARD DISBONDED AREA WAS REPAIR IAW EA 6-5750-144062.SDR FDEA201009273736Spacer · crackedRIGHT MLG W/W - SPACER WITH CRACK LOCATED AT FR54 AND AT Y-450 AND Z-1357. AFTER HFEC AND ROTOTEST THE CRACKS REPORTED BY THE VISUAL INSP WERE NOT CONFIRMED. IT WAS JUST A FLAW IN THE SURFACE PROTECTION SYS.SDR FDEA201009153656Skin · misrepairedFLAP INBD LT LOWER SKIN - PREVIOUS REPAIR FOUND BETWEEN RIB13/14 AND STGR 8/11. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO THE SRM. NEW REPAIR ACCOMPLISHED IAW EA 6-5750-144069 INSTRUCTIONS.SDR FDEA201009154251Skin · damagedRIGHT ELEVATOR BOTTOM SKIN - PREVIOUS REPAIR FOUND AT T/E AT STA 144/ER1. REPAIR REQUIRES EVALUATION. PREVOUS REPAIR FOUND DAMAGED (DEBONDED) AND IT WAS REMOVED. NEW REPAIR HAS BEEN ACCOMPLISHED IAW SRM 55-21-11, FIG 210.SDR FDEA201009144250Skin · damagedRT ELEVATOR TOP SKIN FOUND WITH DEBONDING AT T/E STA473/ER19. RT ELEVATOR HAS BEEN REPAIR IAW SRM 55-21-11, FIG 210.SDR FDEA201009143614Skin · dentedFUSELAGE SKIN - PREVIOUS DENT FOUND LOCATED BTW FR 2-3 IN LOWER SECTION. DENT WAS CUT-OFF AND REPAIRED IAW THE SRM 53-11-12, FIG 201 AND 53-10-12 FIG217.SDR FDEA201009133658Vane · misrepairedLT INBD FLAP VANE - T/E BOTTOM SKIN - PREVIOUS REPAIR FOUND BTW RIB 9-10. REPAIR WAS REMOVED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. FLAP VANE WAS REPLACED IAW AMM 27-50-15.SDR FDEA201009133657Vane · misrepairedLT INBD FLAP VANE - L/E SKIN WITH PREVIOUS REPAIR FOUND BETWEEN RIB 9-10. REPAIR WAS REMOVED AND FOUND NOT TO BE IAW THE SRM. FLAP VANE REPLACED AS PER AMM 27-50-15.SDR FDEA201009133615Skin · misrepairedFUSELAGE SKIN - PREVIOUS REPAIR FOUND LOCATED AT FR25A BTW S48-50R. EXISTING REPAIR WAS NOT IN COMPLIACE WITH THE SRM. NEW REPAIR ACCOMPLISHED IAW SRM 53-10-12, FIG 228.SDR FDEA201009094249Skin · damagedRT ELEVATOR - TOP SKIN FOUND DEBONDED AT THE T/E STA 323/ER11. RT ELEVATOR HAS BEEN REPAIRED IAW SRM 55-21-11, FIG 210.SDR FDEA201005241624Lug · corrodedRT MLG RIB 5 FWD LUG EXCEEDED ALLOWABLE LIMITS IAW DWG AFTER REMOVAL OF LEVEL 1 CORROSION. FABRICATED AND INSTALLED NEW BUSHING IAW EA 6-5710-135199.SDR 08FDEA03641Pressure Switch · failedYELLOW HYD PUMP FAILED AT FLAP RETRACTION. PERFORMED NR 2 ENGINE RAN,VERIFIED YELLOW HYD SYS PRESSURE IS 2900 PSI ON ECAM, YELLOW SYS LOW PRESS LIGHT FLICKER MOMENTARILY DURING FLAPS EXTENSION AND RETRACTION, NEED PRESS SWITCH CPN 0030767, MPN BSG0001-5505 NSDR 08FDEA02965Skin · delaminatedRT WING, INBD FLAP TRAIL EDGE UPPER AND LOWER SURFACE DELAMINATED AT 15.0 INCH FROM INBD EDGE, MEASURING 5.0 BY 2.0 INCH REPAIRED THE DELAMINATED WEDGE PER EA NR 6-5720-117366.SDR 08FDEA02640Longeron · corrodedLT PAX/CREW DOOR LONGERON POSITION NR 2 WITH MILD/EXFOLIATION CORROSION BETWEEN FR15A-16. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. MEASURED REMAINING THICKNESS PER NTM 51-10-04. THE ORIGINAL THICKNESS IS 0SDR 08FDEA02641Floor Support · corrodedFR 12 - FR 12A Y1456 LONGERON FOR SUPPORTING OF MAIN DECK FLOOR CORRODED. REPAIRED THE DAMAGE PER EA NR 5310-117358.SDR 08FDEA02618Roller · inoperativeRT INBD FLAP TRACK NR 2, UPON REMOVAL OF INBD FLAP FOUND 2 FRONT CARRIAGE ROLLER AND 1 REAR CARRIAGE ROLLER SEIZED. DISASSEMBLED ROLLERS PER CMM 27-51-54, CLEANED AND INSPECTED, FOUND ROLLERS WITH SURFACE CORROSION ON MATING SURFACE. REMOVED THE ROLLERS PESDR 08FDEA02588Floorbeam · corrodedMAIN DECK CROSSBEAM C14(FR14) -Y1220 TO -Y1300 LOWER FREE FLANGE WITH EXFOLIATION CORROSION. REMOVED THE PULLEY BRACKET PER AMM 20-29-11-0. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. MEASURED REMAINING THICKNSDR 08FDEA02587Arm · corrodedNR 1 RUDDER HINGE ARM FORWARD ATTACH AREA FORWARD OF BEARINGS EXFOLIATED. REMOVED CORROSION AND POLISHED REWORK AREA PER SRM 51-76-10, APPLIED ALODINE TO THE REWORK AREA PER SRM 51-21-10. PERFORM HFEC TO REWORK AREA FOR CRACK, NO CRACK FOUND PER NTM 51-10-09SDR 08FDEA02491Web · crackedWEB CRACKED OUTBOARD OF PRECOOLER NR 1 PYLON. DRILLED CRACK STOP HOLES PER SRM 54-52-31. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLER AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB AND THE DOUBLER PER SDR 08FDEA02489Rib · crackedWEB CRACKED LOWER END FORWARD OF RIB 18 RIGHT SIDE NR 2 PYLON. DRILLED CRACK STOP HOLES PER SRM 54-52-31. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLERS AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB ANSDR 08FDEA02488Rib · crackedWEB CRACKED LOWER END FORWARD OF RIB 18 LEFT SIDE NR 2 PYLON. DRILLED CRACK STOP HOLES PER SRM 51-40-21. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLER AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB AND SDR 08FDEA02492None · noneNR 2 PYLON REPAIR INSTALLED ON PRECOOLER WEB DOES NOT MEET REQUIREMENTS PER SRM. REMOVED THE ORIGINAL REPAIR PART PER SRM 51-40-21. DRILLED CRACK STOP HOLES (4.8MM) PER SRM 54-52-31. FABRICATED REPAIR PART PER SRM 54-52-31. DRILLED FASTENER HOLES TO THE RESDR 08FDEA02500Floorbeam · corrodedMAIN DECK CROSSBEAM C14, LBL 55.0, INNERGRANULAR CORROSION ON LOWER FLANGE. REMOVED CORROSION PER SRM 51-74-10. MEASURED REMAINING THICKNESS PER NTM 51-10-04. FOUND WITHIN LIMIT (REMAINING THICKNESS: 0.096 INCH). APPLIED FLAP PEENING PER SRM 51-29-00. REP
Back to N456FE, cancelled Apr 23, 2020