N663FE
Service difficulty reports · 264
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 = 'N663FE' 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 = 'N663FE' 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 FDEA201208142998Floorboard · delaminatedMAIN DECK CARGO FLOORBOARD 242SF, DELAMIATED ALL AROUND THE CLEVIS ADAPTERS MOUNTING AREA. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201208142997Floorboard · damagedFLOORBOARD 241DF HAS FOUR AREAS 1INCH X 5 INCHES CRUSHED FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201208142996Floor Panel · damagedFLOOR PANEL 251WG BROKEN IN HALF. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208142995Floor Panel · crackedFLOOR PANEL 232G HAS TWO 9 INCH CRACKS, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208132973Floor Panel · crackedFLOOR PANEL 242RG HAS TWO 9 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208132972Floor Panel · crackedFLOOR PANEL 242EK HAS TWO 10 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208132971Floor Panel · crackedFLOOR PANEL 242GF HAS ONE 12 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208132970Floor Panel · crackedFLOOR PANEL 242QJ HAS TWO 10 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208112949Floor Panel · crackedFLOOR PANEL 252VF HAS TWO 9.5 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208112948Floor Panel · crackedFLOOR PANEL 242VG HAS ONE 9.5 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208112947Floor Panel · crackedFLOOR PANEL 232YG HAS A 9 INCH CRACK & TWO 4 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201208112946Floorboard · crackedFLOORBOARD 252UH HAS TWO 9.5 INCH CRACKS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201206142242Clevis · damagedLANDING GEAR WOULD NOT RAISE ON DEPARTURE TRIED SYS 2 WITH NO EFFECT, LOST THE FLIGHT DIRECTOR, PITCH DAMPNER, AUTOPILOT AND AUTO THROTTLES. PERFORMED ECAM AND QRH PROCEDURES. RETURNED TO DEPARTURE AS AN AIR TURN BACK. TROUBLESHOOTING PER TSM 32-61-00,PG 1SDR FDEA201204121384Jackscrew · contaminatedON APPROACH, FLAPS BECAME STUCK LESS THAN 15 DEG WITH SYS 1 & 2 FLAP FAULT LIGHTS ILLUMINATED. RECYCLED SLAT/FLAP HANDLE. FLAPS STILL STUCK LESS THAN 15 DEG ACCOMPLISHED QRH, UNEVENTFUL LANDING. INSPECTED & SERVICE TORQUE LIMITER, T-GEARBOX, NR 1 JACK SCSDR FDEA201108233438Rib · corrodedRT WING, RIB 5 MLG FITTING ATTACHMENT HOLE 4 HAL LIGHT PITTING CORROSION AT SPOT FACE DEFECT MEASURES .07 OF AN INCH SQ ON RT RIB 5, REMOVED CORROSION FROM SPOT FACE AT HOLE NR 47 IAW SRM 51-74-10. MEASURED SPOT FACES FOR ALL HOLES AND SUBMITTED TO MFG . CSDR FDEA201108233437Rib · corrodedRT WING, RIB 5 MLG FITTING ATTACHMENT HOLE NR 54 HAS PITTING CORROSION AT SPOT FACE . DEFECT MEASURES .25 OF AND IN SQ ON RT WING, RIB 5. REMOVED CORROSION FROM SPOT FACE FOR HOLE NR 54 IAW MFG SRM 51-74-10. MEASURED SPOT FACES FOR ALL HOLES AND SUBMITTEDSDR FDEA201108233436Rib · corrodedRT WING, RIB 5 MLG FITTING ATTACHMENT HOLE NR 54 HAS PITTING CORROSION AT SPOT FACE . DEFECT MEASURES .25 OF AND IN SQ ON RT WING, RIB 5, REMOVED CORROSION FROM SPOT FACE FOR HOLE NR 54 IAW SRM 51-74-10. MEASURED SPOT FACES FOR ALL HOLES AND SUBMITTED TO MSDR FDEA201108233435Rib · corrodedLT MLG RIG 5 HOLE LOCATION 47 HAS PITTING CORROSION ON FASTENER LANDING. ON LT RIB 5, REMOVED CORROSION FROM SPOTFACE FOR HOLE NR 47 IAW SRM 51-74-10 MEASURED SPOTFACE FOR ALL HOLES AND SUBMITTED TO MFG. COMPLIED WITH MFG TD 70551513/018 WITH NIL DEVIATIONS. SDR FDEA201102100531Frame · crackedDURING HFEC OPEN HOLE INSP, CRACK INDICATION FOUND AT LT FRAME 44, HOLE 'B' ON FRAME. REPAIRED PER E.A. 6-5310-143509, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 111.SDR FDEA201102100533Frame · crackedDURING HFEC OPEN HOLE INSPECTION, CRACK INDICATION FOUND AT RT FRAME 44, HOLE 'B' ON FRAME. REPAIR CARRIED OUT PER E.O. 6-5310-7-5006A1 PART 2, . REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101250355Spar · crackedDURING HFEC OPEN HOLE INSPECTION CRACK INDICATION FOUND AT RT CTR WING BOX OF REAR SPAR HOLE (I) ON SECOND LAYER EDGE FROM FWD APPROX 0.5" (L2) LONG. THE THIRD LAYER CRACK IS NOT A CRACK AT ALL. INSTEAD IT IS A STRAIGHT LINE BUTT-JOINT BETWEEN THE REAR SPAR SDR FDEA201101220333Mount · corrodedDURING NR 2 ENGINE PYLON MOUNT AFT HOLE CORROSION REMOVAL FOUND LOWER MATING FACE WITH CORROSION NEAR TO THE HOLE. REPAIRED IAW EA 6-5450-143832. DEEPEST REWORKED SURFACE: 0.019" AND MAXIMUM ALLOWABLE DEPTH: 0.0138" IAW SRM 54-51-81 CONFIGURATION 2, FIG 104,SDR FDEA201101210328Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (N) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201101210327Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (M) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2). REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVSDR FDEA201101210326Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (LT) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR GMM 6-2-100SDR FDEA201101210325Skin · corrodedRT WING OTBD FLAP OTD SIDE AT STATIC DISCHARGE BASE AREA FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-00, FIG 103 SHEET 5 REV 19. MATERIAL THICKNESS: 0.060", MATERIAL REMOVED: 0.040" AND MATERIAL REMAINING: 0.020". REPAISDR FDEA201101210324Skin · damagedLT WING - WING TIP T/E SEVERAL RIVET HOLES ELONGATED. REMOVED AS PER SRM 51-40-21 REVISION 19. ELONGATED HOLES REWORKED AS PER DRAWING A57247017 ISSUE M AND NEW RIVETS INSTALLED AS PER SRM 51-40-21 REVISION 19. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISSDR FDEA201101180279Mount · corrodedENGINE NR 2, PYLON FWD MOUNT AFT INBD HOLE LOWER AREA FOUND WITH CORROSION. AREA REWORKED AND FOUND WITHIN LIMIT IAW SRM 54-51-81, CONFIGURATION 2, FIG 202, REV 19. ORIGINAL HOLE DIAMETER: 0.9615", REWORKED HOLE DIAMETER: 0.9965" AND MAXIMUM HOLE DIAMETER: 0SDR FDEA201101180278Mount · corrodedENGINE NR 2, PYLON FWD MOUNT AFT OTBD HOLE LOWER AREA FOUND WITH CORROSION. REWORKED AND FOUND WITHIN LIMIT IAW SRM 54-51-81 CONFIGURATION 2, FIG 202, REV 19. ORIGINAL HOLE DIAMETER: 0.947", REWORKED HOLE DIAMETER: 0.9965" AND MAXIMUM HOLE DIAMETER: 0.997".SDR FDEA201101160183Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE. REPAIRED IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV I 111.SDR FDEA201101140173Skin · crackedDURING HFEC OPEN HOLE INSP, CRACK INDICATION FOUND AT LT WING LOWER SKIN PANEL INBD OF RIB 9, AFT OF REAR SPAR HOLE (G) 1 EA ON LOWER SKIN SIDE. REPAIR CARRIED OUT PER EA NR 6-5710-143824. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101140172Rib · crackedRIGHT WING OTBD OF RIB 23 FOUND L/E RIB CRACKED AT TWO LOCATIONS. CRACKED RIB AT RT WING OUTBOARD OF RIB 23 LEADING EDGE, REMOVED AND REPLACED PER SRM 51-40-21 REVISION 19. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101130129Skin · crackedRT WING LOWER SKIN PANEL INBD OF RIB 9 JUST INBD OF STIFFENER, FOUND WITH SUPPORT CRACK. REPAIR CARRIED OUT AS PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101120108Frame · crackedMAIN DECK CARGO COMPARTMENT, WITH REF TO EO NR6-5310-7-5006A1, PART 2, PAGE 21 OF 48 STEP 79, FRAME 44 RT HOLE B ABOVE STRINGER 26 FOUND WITH CRACK INDICATION. REPAIR CARRIED OUT PER EO NR 6-5310-7-5006 A1 PART 2. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201101120107Frame · crackedMAIN DECK CARGO COMPARTMENT, WITH REF TO EO 6-5310-7-5006A1 PART 1, PAGE 21 OF 48 STEP 79, FRAME 44 HOLE B ABOVE STRINGER 26, CRACK INDICATION FOUND. REPAIR CARRIED OUT PER EO NR 6-5310-7-5006 A1 PART 1. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISISDR FDEA201101120106Skin · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON RT WING LOWER BOTTOM SKIN PANEL INBD OF RIB NR 9. REPAIR CARRIED OUT PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101100096Attach Fitting · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON FWD CARGO DOOR ACTUATOR ATTACH FITTING AT FRAME 22A. REMOVED IAW SRM 51-40-21, REV 19 AND REPLACED WITH NEW FRAME SECTION IAW SRM 51-40-21, REV 19 AND EA 6-5230-143830. THIS REPAIR IS CLASSIFIED AS MAJOR SDR FDEA200912124434Warning System · malfunctionedEXECUTION OF EGPWS ESCAPE MANUVER. NO ENG PARAMETERS EXCEEDED. A/S 250KTS FIRE WALL PWR. 2000 AGL. SOME AIRFRAME BUFFET WAS FELT, RELAXED BACK PRESSURE, GOT TO APPOX 18 DEGREES NOSE HIGH, WARNING CEASED INDICATIONS WERE "TERRAIN, TERRAIN, WHOP WHOP" (NO PUSDR FDEA200903080865Proximity Sensor · failedLANDING GEAR WOULD NOT RETRACT AFTER T/O IN POS NR 1 SWITCHED TO NR 2 SYSTEM, STILL NO RETRACT. PROX BOX IS FAULTING ITSELF AND FAULT CODE 63. REMOVED AND REPLACED PROX BOX 54 GB PER MM 32-31-71-4. OPS CHECK OF BOX PER MM 32-31-71-4 CHECKED GOOD. FOUND LEVSDR 08FDEA04070Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK 2 RT HAS CORROSION AT FR 41,3 SQ IN. REMOVED LEVEL 1 CORROSION AT MDCC SEAT TRACK NR 2RT. REMOVED DAMAGED SECTION AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 40 AND FR 45,TRACK NR 2RT IAW A300-600 SRM 53-10-16, FISDR 08FDEA04069Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FR 31 FWD FACE UPPER SIDE HAS .100 IN CRACK, BETWEEN SEAT TRACKS NR 4 LT AND TRACK NR 5 LT REMOVED CRACK AT CROSSBEAM FR 31 AND INSTALLED CROSSBEAM CRACK REPAIR AT STIFFENER BETWEEN TRACKS NR 4 LT AND TRACK NR 5 LT IAW A300-600 FREISDR 08FDEA03955Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 RT HAS CORROSION 3 AREAS BETWEEN FR 51 AND FR 53 REMOVED LEVEL 1 CORROSION AND CUT OUT DAMAGED SECTION OF SEAT TRACK NR 2RT AND INSTALLED SPLICE REPAIR BETWEEN FR 51 AND FR 53 IAW SRM 53-10-16, FIG 205.SDR 08FDEA03954Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 RT HAS 4 SQ IN OF CORROSION AT FR 27 AND 4 SQ IN OF CORROSION AT FR 30. REMOVED LEVEL 1 CORROSION AND REMOVED DAMAGED SEAT TRACK SECTION AT TRACK NR 2RT AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 27 AND FR 30SDR 08FDEA03953Seat Track · corrodedMDCC SEAT TRACK CORRODED AT NR 3RT BETWEEN FRAME 41 AND FRAME 43, 4 SQ INCHES REMOVED LEVEL 1 CORROSION AND REMOVED AND REPLACED SEAT TRACK SECTION AT TRACK NR 3 RT, BETWEEN FR 40 AND FR44.5 IAW A300-600 SRM 51-72-10.SDR 07FDEA05116Windshield · crackedF/O`S R1 WINDOW SHATTERED AT CRUISE FL 300, QRH COMPLIED WITH. ACCOMPLISHED COMPLETION OF F/O'S WINDOW INSTALLATION IAW MM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4. SDR 07FDEA05111Window · crackedF/O`S R1 WINDOW SHATTERED AT CRUISE FL 300. QRH COMPLIED WITH. ACCOMPLISHED COMPLETION OF F/O'S WINDOW INSTALLATION IAW MM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4. SDR 07FDEA05110Windshield · crackedF/O`S R1 WINDOW SHATTERED AT CRUISE FL 300. QRH COMPLIED WITH. REMOVED AND REPLACE R1 WINDSHIELD PER AMM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4. PERFORMED WINDSHISDR 07FDEA00984Pump · unknownUPON RAISING LANDING GEAR AFTER TAKEOFF FROM MEM, GEAR STAYED DOWN WITH AMBER DOOR LIGHTS & GOT ECAM INDICATION OF COMPLETE GREEN SYSTEM FLUID LOSS. NO NOSE WHEEL STERRING ON ROLLOUT. REMOVED AND REPLACED THE NR 2 ENGINE GREEN SYSTEM HYDRAULIC PUMP PER A30SDR 07FDEA00134Proximity Sensor · failedAPPROACH TO GEG LOWERED LANDING GEAR, ECAM AND LANDING GEAR LIGHTS INDICATED UNSAFE NOSE GEAR. SAME INDICATION ON OVERHEAD PANEL. FOLLOWED QRH, MANUALLY LOWERED GEAR. C/W TSM A300-600-32-30-00 FIGURE 117 STEP 1 PREFORMED FREE FALL EXTENSION DOORS DID NOT FSDR 05FDEA01152Packing · leakingAT FL350 LOST QUANTITY IN THE GREEN HYD SYSTEM. ACCOMPLISHED ECAM ITEMS AND ADDITIONAL QRH ITEMS. MANUAL EXTENSION OF MAIN GEAR. EMERGENCY DECLARED FOUND LEAKAGE AT GREEN SYS PRESS TRANSMITTER ADDED MPN NSA8671-4 CPN 0114019 QTY 2 RING MSN 928916 ADDED MPN
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