N665FE
Service difficulty reports · 201
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 = 'N665FE' 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 = 'N665FE' 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 08FDEA02360Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 UH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 UH BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED; SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-005 REV F.SDR 08FDEA02359Floorboard · damagedMAIN CABIN FLOOR PANEL 241 NF IS DAMAGED. FABRICATED NEW FLOORBOARD; POTTED EDGES; LOCATED HOLES; INSTALLED INSERTS; CURED; APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F.SDR 08FDEA02369Floor Panel · crackedMAIN CABIN FLOOR PANEL 262 VF IS CRACKED AND DAMAGED. MATERIAL ID FOR THE REPAIR IS 2024-T3, 056; PO 609852.1 IAW A300-600 SRM 53-52-00; FIG 703. FABRICATED REPAIR IAW A300-600 SRM 53-52-00; FIG 7003. ALODINED IAW A300-600 SRM 51-21-10; PG 3. PRIMED IAW A3SDR 08FDEA02350Seat Track · corrodedMDCC SEAT TRACK HAS CORROSION ON THE UPPER SURFACE BETWEEN FRAME 14C AND FRAME 17; LML 99.06 CM.SDR 08FDEA02349Skin · dentedTHE RIGHT INBD FLAP LOWER SURFACE HAS DENTS. LIMITS CHECKED AND THE DENTS WERE FOUND TO BE WITHIN LIMITS AT DOTS C528, 0.029 AND P745, 0.029 IAW A300-600 SRM 57-50-00 PGS 104; 105 AND 106; FIGURE D USING DEPTH GAUGE T8410B. DOT NR C527 WAS FOUND TO BE OUT OF SDR 08FDEA02348Panel · crackedRIGHT WING L/E PANEL 613 AB CUTOUT FWD OUTBD FASTENER HOLE IS CRACKED. MATERIAL ID FOR THE REPAIR IS 2024-T3, 0.056, PO 609852.1 IAW A300-600 SRM 53-52-00; FIG 703. FABRICATED THE REPAIR IAW A300-600 SRM 53-52-00; FIG N703. ALODINED IAW A300-600 SRM 51-21-1SDR 08FDEA02313Panel · corrodedTHE BULK CARGO COMPARTMENT LEFT TRANSITION PANEL IS CORRODED AROUND THE FASTENER RECEPTICALS FROM FRAME 67 TO FRAME 69. REMOVED THE CORROSION; FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-00. REMOVED TRANSITION PANEL. FABRIATED A NEW TRANSITION PANEL IASDR 08FDEA02311Panel · gougedBULK CARGO COMPARTMENT LEFT TRANSITION PANEL IS GOUGED FROM FRAME 63 TO FRAME 64; LBL 53 TO LBL 62. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW A300-600 SRM 53-10-00. REMOVED TRANSITION PANEL IAW A300-600 SRM 51-40-21. MATERIAL ID 2024-T3, 0.063, PO 619567.SDR 08FDEA02293Support · crackedLEFT WING T/E SPAR AREA; NR 4 SPOILER OUTBD HINGE INNER WEB HAS A REPAIR INSTALLED THAT IS CRACKED IN THE RADIUS. THE NR 4 SPOILER IS REALLY THE NR 2 OUTBD. REMOVED SKIN SUPPORT IAW A300-600 SRM 51-40-21; PG 7. LOCATED; DRILLED AND DEBURRED SKIN SUPPORT P/NSDR 08FDEA02225Seat Track · corrodedTHE CABIN SEAT TRACK HAS CORROSION AT FRAME 39; LBL 18. THIS SDR WAS GENERATED IN ERROR. FOR DETAILED INFORMATION SEE SDR TRACKING NUMBER 08-2224. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.1SDR 08FDEA02224Seat Track · corrodedTHE CABIN SEAT TRACK HAS CORROSION AT FRAME 39; LBL 18. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.134. MATERIAL LOSS 0.020. MATERIAL REMAINING 0.114. ALODINED; PRIMED AND TOPCOATED THE AREASDR 08FDEA02223Seat Track · corrodedTHE CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 32 AND FRAME 33; LBL 58. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.134. MATERIAL LOSS 0.025. MATERIAL REMAINING IS 0.109. DEPTH GAUGE USED WAS TSDR 08FDEA02227Floorbeam · crackedMAIN DECK FLOOR; FRAME 64; RIGHT 46 INCH FROM CENTERLINE; THE FLOORBEAM IS CRACKED.SDR 08FDEA02222Shim · crackedNR 1 PYLON RIB 3-A STA 615 INBD SIDE SHIM HAS A .75 INCH CRACK.SDR 08FDEA02221Shim · crackedNR 1 PYLON RIB 3-A; STA 615, THE OUTBD SIDE SHIM HAS A 3/4 INCH CRACK.SDR 08FDEA02205Shear Web · crackedRIGHT FLOOR STRINGER SHEAR WEB IS CRACKED JUST AFT OF FRAME 79 AT THE MAIN CARGO DECK FLOOR LEVEL. REMOVED AND REPLACED WITH A NEW WEB P/N A5398111320100; PO 616322.4 IAW SRM 51-40-21; PGS 6 AND 7. RESTORED CIC IAW SRM 51-22-00.SDR 08FDEA02204Shear Web · crackedLEFT FLOOR STRINGER SHEAR WEB IS CRACKED JUST AFT OF FRAME 79 A; AT THE MAIN CARGO DECK FLOOR LEVEL REMOVED AND REPLACED WITH A NEW WEB IAW SRM 51-40-21; PG 7.SDR 08FDEA02206Floorbeam · crackedTHE BULK CARGO COMPARTMENT CEILING AREA MAIN DECK FLOOR SUPPORT ANGLE IS CRACKED AT THE FWD FACE OF FRAME 69 AND LBL 60.SDR 08FDEA02163Intercostal · bentTHE INTERCOSTAL FROM EMPENNAGE FRAME 86 TO FRAME 87; AT STRINGER 34R IS BENT. REMOVED INTERCOSTAL IAW A300-600 SRM 51-40-21. REPLACED INTERCOSTAL CHORD IAW A300-600 SRM 51-40-21 AND SRM 51-72-10. INSTALLED INTERCOSTAL IAW A300-600 SRM 51-40-21.SDR 08FDEA02144Rib · crackedNR 2 PYLON RIB 8A; STA 726 OUTBD SIDE SHIM HAS A .75 INCH CRACK.SDR 07FDEA00229Unknown · unknownNR 2 ENG REVERSER PRESSURIZED LIGHT ON ECAM ILLUMINATED AT GEAR RETRACTION ON TAKEOFF COMPLIED WITH E-CAM AND QRH ATB. R&R DIR. PILOT VALVE, HARNESS FOR T/R, PRESS REG. S/O VALVE,DIODE UNIT 20KM,MOD BLOCK 204VT, RELAYS 6KM&16KM, AWAITING FINAL OPS CHECK & ESDR 07FDEA00187Unknown · unknownON TAKEOFF AT APPROX, 60 KIAS LT ECAM (W/O CHIME) ALERTED US TO "ENG 2 REVERSER PRESSURIZED" AFTER CONSULTING TO W/MX, CYCLED NR 2. REVERSER ON THEN OFF THIS TEMPORARILY SOLVES THE PROBLEM AS THE THROTTLE ADVANCE ON NR 2 ENG FOR TAXI PROBLEM RESURFACED ACN RSDR 06FDEA2650Ecu · malfunctionedAFTER TAKEOFF APPROXIMATELY AT 500' AGL, GOT A MASTER CAUTION ECAM MESSAGE FOR FADEC 2 FAULT. COMPLIED WITH CHECKLIST. RETURNED TO KMEM BECAUSE OF KBTR SHORT RW AND CAUTION ABOUT OVERBOOST WITH REVERSE THRUST. REMOVED AND REPLACED NR 2 ENGINE ECU REF A300-SDR 06FDEA1564Seat Track · crackedSEAT TRACK CRACKED ON SEAT TRACK 4 LT FR 31 LT SIDE REF N00537. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.SDR 06FDEA1563Seat Track · corrodedSEAT TRACK - ZONE 240 TRACK 3R AT FR 52 FR 40-41 AND FR 30-31 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-10, 2 AREAS IN LIMITS OF SRM 53-10-16, 1 AREA OUT OF LIMITS OF SRM 53-10-16 FR 40-41. REMOVED AND REPLACED SEAT TRACK RAIL IAW SRM 51-72-10.SDR 04FDEA03237Thrust Reverser · out of rigDURING T/O, NR 2 ENGINE ECAM "THRUST REVERSER UNLOCKED" RTO POWER SETTING 70 PERCENT N1 AIRSPEED 30 KTS. ENT BY: 299976 RPT BY: 096807 FACT 26NOV04 23:59 EWR R RE-RIGGED NR 2 ENGINE THRUST REVERSER PER AMM 78-31-00-5-F. RE-RIGGED NR 2 ENGINE THRUST REVSDR 04FDEA02073Crossbeam · deformedAFTER REMOVAL OF CLS ADAPTER AT FR65 BETWEEN LT SEAT TRACK 3 & 4. DEFORMATION OF CROSS BEAM FLANGE WAS FOUND TO BE AT .250 INCH, REF A300/600 SRM 53-10-15 FIG 205, MAX DEFORMATION IS .197 INCH, REF SNRM N00405. REPAIRED IAW FED EX EA 6-5310-80084.SDR 04FDEA02076Frame · dentedFRAME 20A AT FWD CARGO PIT DOOR, FWD SIDE DENTED 4 X 2 X .125 INCH. CUT OUT DAMAGE AND REPAIRED IAW A300600 SRM 51-40-21 AND FED EX SRM 30-53-001.SDR 04FDEA02075Seat Track · corrodedCOMPT RT NR 2 SEAT TRACK BETWEEN FR45 AND 54 HAS CORROSION AT FR45, 46.2, 49, 53.8, 52. REF SNRM N00454. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW A 300/600 SRM 51-72-10.SDR 04FDEA02074Floorbeam · crackedFWD CARGO COMPT UPPER FLOORBEAM AT FR29 O/B OF 1ST SEAT TRACK FROM CENTER IS CRACKED. REF SNRM N00276. REMOVED DAMAGE, NO CRACK NOTED. INSTALLED REPAIR ANGLES, AND SHIM AND TREATED AND PRIMED, AND TOP COATED IAW A33/600 SRM 53-10-15 AND 51-75-10.SDR 04FDEA02072Seat Track · corrodedSEAT TRACK NR 2 RT BETWEEN FR26 AND FR38.2 HAS CORROSION ON FR 26.8, FR 28.5, FR30.2, AND 32.7. REF SNRM N00401. REMOVED AND REPLACED SEAT TRACK IAW A300/600 SRM 53-10-16.SDR 04FDEA02053Seat Track · corrodedMAIN CARGO COMPT RIGHT NR 5 SEAT TRACK BETWEEN FR 45 AND FR 54 HAS CORROSION AT FR 48.7, 50.8, 53, 53.6 AS MARKED. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 PARA 5.0 FIG 205.SDR 04FDEA02052Seat Track · corrodedMAIN CARGO COMPT RIGHT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRACK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16.SDR 04FDEA02051Seat Track · corrodedMAIN CARGO COMPT RT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRACK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16.SDR 04FDEA02050Floorbeam · crackedFWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TREATED, PRIMED, AND TSDR 04FDEA02049Floorbeam · crackedFWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TREATED, PRIMED, AND TSDR 04FDEA02048Seat Track · damagedMAIN CABIN SEAT TRACK NR 5 LEFT OF CENTER LINE AT FR 20 HAS 2 EA BROKEN LUGS. REPAIRED MAIN CABIN SEAT TRACK 35 LT OF CENTERLINE AT FR 20 IAW A300-600F SRM 53-10-16 FIG 201.SDR 04FDEA01914Seat Track · corrodedMAIN CABIN SEAT TRACK 4L HAS 2EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS BETWEEN FR 75 & 76 AND BETWEEN FR 74 & 75. REMOVED CORRODED SECTION AND REPAIRED IAW A300-600 SRM 53-10-16, INSTALLED 1EA TRACK 4 FT 9 INCHES AND 2 EA SPLICES.SDR 03FDEA00047Bearing · wornON ROTATION FOR TAKEOFF ELEVATOR RESPONSE WAS VERY SLUGGISH AS IF A/P WAS ON IN CONTROL WHEEL STEERING. NO CHANGE IN HOW THE ELEV FELT AT 250 KIAS AND 320 KIAS. NO WARNING LIGHTS ILLUMINATED AT ANY TIME. DURING APPROACH ELEV RESPONSE FELT THE SAME FOUND CAPT SDR 02FDEA00202Thrust Reverser · malfunctionedDURING T/O N1 GOT NR 1 THRUST REVERSER PRESSURIZED ON LEFT ECAM REJECT AT LOW SPEED. PERFORMED FUNCTION CHECK CND.SDR 02FDEA00038Smoke Detector · activatedON CLIMBOUT BOTH DETECTORS MID 1 & ONE INDICATED SMOKE IN CARGO COMPT.SDR 01FDEA01002Fire Warning · activatedRECEIVED MAIN CARGO DECK 1 & 2 FIRE IND. SHUTDOWN A/C AND INSP APU.SDR 01FDEA00846Smoke Warning · illuminatedCARGO SMOKE WARNING CAME ON. RELEASE PER MEL, NO CARGO TO BE CARRIED IN MAIN DECK.SDR 01FDEA00448Smoke Detector · false indicationDURING TAXI BOTH MID 2 MAIN DECK CARGO SMOKE LIGHT ILLUM TRIGGERING MC DECK CARGO VALVE, ISO VALVE, ETC. PERF SMOKE TEST NO FAULTS FOUND. RERACKED SMOKE MODULES AND ALL 3 PASSED SELF TEST PER TSM 28-19-00.SDR 01FDEA00387Smoke Detector · looseAFT T/O MAIN DECK CARGO SMOKE WARNING ON ECAM ILLUM. NR 2 UPPER DECK SMOKE DETECTOR UNIT LOOSE, TIGHTENED HOLDING NUT AND PERF SMOKE DETECTOR SYS TEST PER IAW AMM 26-19-00-5, ALL TEST OK FOR SERVICE.SDR 01FDEA00382Smoke Detector · activatedAFTER GEAR RETRACT AVIONICS SMOKE ON ECAM. OPERATED SNIFFER FAN, NO SMOKE DETECTED.SDR 00FDEA00875Pilot Valve · faulty00-356 ECAM MSG NR 1 PRESSURIZED AFT T/O. R&R DIRECTIONAL PILOT VALVE AND PRESS SW MM 78-31-06-2. OPS CK GOOD AND LK CK GOOD.SDR 00FDEA00871Control Valve · malfunctioned00-352 ECAM MSG NR 1 T/R PRESSURIZED. R&R DIRECTIONAL PILOT CONTROL VALVE AND PRESSURE SWITCH PER MM 78-31-06-2.SDR 00FDEA00481Proximity Switch · failedON GEAR RETRACTION (NR 2 SYS) GEAR IND NOT RETRACTED ECAM ANNOUNCED LAND GEAR RETRACTION SYS INOP. GEAR AND DOOR LIGHT WERE ON. REMOVED AND REPLACED PROXIMITY UNIT PER AMM 32-31-71-4 PRECAUTIONARY. OLD PROX BOX SHOW NO FAULTS.SDR 99FDEA00500Warning Light · illuminatedLANDING GEAR DOWN NR 3 WAS UNSAFE WARNING AFT MISSED APPROACH, GOT THREE GROUND LIGHTS (BOTH PNLS SAME) LEVEL. RECYCLED THE GEAR AND ALL OK. INSP RT GEAR ALL LINKS, SWITCHES NORM. PER PROX BOX TEST PER TSM 32-61-00 101 THRU 105. NO FAULTS DISPLAYED. MEMOR
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