N655FE
Service difficulty reports · 219
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 = 'N655FE' 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 = 'N655FE' 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 FDEA200912084381Adapter · crackedMAIN CABIN ADAPTER IS CRACKED AT FRAME 59; LBL 50. DRILLED AND TRIMMED PART AS NEEDED; ALODINED; PRIMED AND PAINTED. INSTALLED WET; IAW FREIGHTER SRM 53-10-15, FIG 207, SHEET 36, PGS 327 / 328 "MAIN DECK CARGO CROSSBEAM REPAIR (FR,59). INSTALLED FLOOR PANSDR FDEA200912084380Support · crackedAVOINICS COMPARTMENT BATTERY RACK HORIZ SUPPORT IS CRACKED ON THE UPPER INBD END. COMPLIED WITH EA 6-2570-135519.SDR FDEA200912084379Intercostal · crackedAVOINICS COMPARTMENT BATTERY RACK SUPPORT LONGITUDINAL INTERCOSTAL IS CRACKED AT ATTACH FASTENER AT FRAME 15 AND STR 15. REMOVED BATTERY RACK SUPPORT IAW SRM 51-72-10, PARA 5A AND SRM 51-40-21, PARA 5, PG 7. DRILLED BATTERY REAC SUPPORT PN A9242053522200 ISDR FDEA200912084377Skin · damagedFUSELAGE EXTERIOR SKIN IS CREASED IN 2 PLACES AFT OF THE FWD CARGO DOOR CUTOUT AT FRAME 25B, STR 38R. REPAIRED IAW SRM 53-13-12, PGS 227/228.SDR FDEA200912084376Skin · damagedFUSELAGE EXTERIOR SKIN HAS PREVIOUS DAMAGE FWD OF THE FWD LWR CARGO DOOR CUTOUT AT FRAME 19 FROM STR 42R TO STR 43R. REPAIRED IAW EA 6-5330-136175.SDR FDEA200912074371Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 QH IS DAMAGED. FABRICATED FLOOR PANEL 251 QH IAW DWG SRZ 25-005, REV "H".SDR FDEA200912074370Seat Track · corrodedMAIN CABIN SEAT TRACK AT FRAME 49; RBL 60 HAS CORROSION ON THE INBD FLANGE. REPLACED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201 AT RBL 40 FROM FRAME 45 TO 54.SDR FDEA200912074369Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD YH IS PUNCTURED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGE AND POTTED EDGES, CURED AND SANDED EDGES, APPLIED NON-SKID TASDR FDEA200912074363Seat Track · crackedAFT CARGO COMPARTMENT; DUMMY SEAT TRACK; OVERHEAD MAIN CABIN FLOOR STRUCTURE IS CRACKED IN THE RADIUS AT FRAME 60. STR 30R. REMOVED DUMMY SEAT TRACK IAW AMM 51-40-21, PG 7. LOCATED AND DRILLED HOLES IN THE NEW SEAT TRACK PN A5327828820300, PO NR 592553.5 IAW SDR FDEA200912074362Rib · gougedRIGHT WING T/E AREA; SPOILER NR 5 HINGE SUPPORT RIB IS GOUGED AT WS 1260. SMOOTHED OUT GOUGED AREA IAW SRM 51-73-10. ORIGINAL THICKNESS WAS 0.145. REMAINING THICKNESS TAPERS FROM 0.145 TO 0.052. ACCOMPLISHED HFEC OF BLENDED AREA NTM 51-10-08. NO CRACKS NOSDR FDEA200912044357Floor Panel · damagedMAIN CABIN FLOOR PANEL NR 252 WH IS DAMAGED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGE AND POTTED EDGES, CURED AND SANDED EDGES, APPLIED NON-SKID TAPE AND PART MARSDR FDEA200912044356Seat Track · crackedFWD CARGO COMPARTMENT MAIN CABIN FLOOR SEAT TRACK IS CRACKED AT FRAME 29; LBL 30. REMOVED FLOORBOARDS 231UG; HH; JH AND YG IAW AMM 53-10-23-4. REMOVED SUBSTRUCTURE ANGLES; SPLICES AND DAMAGED SECTION OF SEAT TRACK FROM FRAME 26.5 TO FRAME 29.5, LBL 30 IAW SRSDR FDEA200912024326Skin · dentedBULK CARGO DOOR OUTER SKIN HAS 2 LARGE DENTS, PREVIOUSLY FILLED. INTERIOR SKIN BENEATH THE DENTS ARE BULGING. CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-00, PARA 5, FIG 103, PARA B. MATERIAL ID 2024-T3 0.071 PO NR 618569.1 IAW SRM 52-34-00, FIGSDR FDEA200911304258Seat Track · gougedMAIN CABIN SEAT TRACK IS GOUGED AT FRAME 28; LBL 71. BLENDED OUT GOUGE AREA IAW SRM 53-10-16. REMOVED 0.009 OF MATERIAL. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.040. REMAINING MATERIAL WITHIN ALLOWABLE LIMITS IAW 53-10-16, FIG 102. ALODINED AND PRIMED IAW SRSDR FDEA200911304257Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AT FRAME 20; LBL 88. REMOVED CORROSION IAW SRM 53-10-16. REMOVED 0.019 OF MATERIAL. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.040. REMAINING MATERIAL IS WITHIN ALLOWABLE LIMITS IAW SRM 53-10-16, FIG 101. ALODINED & PRIMED IAWSDR FDEA200911304256Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED FROM BS 3692 TO BS 3695; LBL 18. REMOVED CORROSION IAW SRM 53-10-16. REMOVED 0.019 OF MATERIAL. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.040. REMAINING MATERIAL IS WITHIN ALLOWABLE LIMITS IAW A300-600 SRM 53-10-16, FIG 101.SDR FDEA200911304255Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED FROM BS 4927 TO BS 4932; LBL 0. REMOVED CORROSION IAW SRM 53-10-16. REMOVED 0.019 OF MATERIAL. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.040. REMAINING MATERIAL IS WITHIN ALLOWABLE LIMITS IAW SRM 53-10-16, FIG 101. ALODINED SDR FDEA200911304267Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 232 YG IS CRACKED. FABRICATED FLOOR PANEL 232 YG IAW DWG SRZ 25-005, REV "H".SDR FDEA200911304266Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 252 VF IS CRACKED IN 3 AREAS FROM FRAME 62 TO FRAME 65; RBL 18 TO RBL 37. FABRICATED FLOOR PANEL 252 VF IAW DWG SRZ 25-005, REV "H".SDR FDEA200911304265Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 252 UH IS CRACKED FROM FRAME 60 TO FRAME 62; RBL 37. FABRICATED FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".SDR FDEA200911304264Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 252 PH IS CRACKED AT FRAME 58; RBL 35. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGE AND POTTED EDGES, CURED AND SANDED EDGES,SDR FDEA200911304263Floorboard · delaminatedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 232 HG IS DELAMINATED. FABRICATED FLOOR PANEL 232 HG IAW DWG SRZ 25-005, REV "H".SDR FDEA200911304262Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 242 QT IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGE AND POTTED EDGES, CURED AND SANDED EDGES, APPLIED NON-SKSDR FDEA200911304261Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 242 BF IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGES, POTTED EDGES, CURED AND SANDED EDGES, APPLIED ANTI-SKISDR FDEA200911304260Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 241 DF IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGES, POTTED EDGES, CURED AND SANDED EDGES, APPLIED ANTI-SKISDR FDEA200911304259Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOOR BOARD 231 TG IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, LOCATED FASTENER HOLES, COUNTERBORED AND POTTED INSERTS, CUT BACK CORE EDGE AND POTTED EDGES, CURED AND SANDED EDGES, APPLIED NON-SKISDR FDEA200911304252Hinge · bindingR-1 DOOR GUIDE ROLLERS CAUSING DOOR TO BIND UP DURING OPENING AND CLOSING. FOUND R-1 DOOR SUPPORT ARM HINGE BOLT WORN AND DOOR HINGE ARMS BUSHINGS WORN. SUPPORT ARM HINGE BOLT AND BUSHINGS REPLACED ON W/C N00121. DOOR HINGE ARMS BUSHINGS REPLACED ON W/C N00SDR FDEA200911304251Cylinder · failedR-1 DOOR EMERGENCY ACTUATING CYLINDER FAILED TO OPEN DOOR DURING THE OPS TEST OF THE DOOR ESCAPE SLIDE. PRESSURIZED BOTTLE DISCHARGED BUT DOOR REQUIRED TO BE MANUALLY OPENED FAR ENOUGH FOR THE SLIDE TO DROP OUT AND INFLATE. INFLATION OF SLIDE WAS NORMAL FRSDR FDEA200911123934Connector · looseON INITIAL CLIMB OUT PASSING FL 230, RECEIVED ECAM INDICATION OF THE LT CREW ENTRY DOOR UNLOCKED. F/O CONFIRMED PARTIAL UNLOCK CONDITION OF THE DOOR. RETURN TO DEPARTURE. PASSING FL1800 UNLOCKED INDICATION WENT AWAY. CREW DEBRIEFED THAT THE DOOR WAS CONFISDR FDEA200906122045Panel · separatedAFTER TAKEOFF TOWER REPORTED SEEING "SOMETHING" FALL OFF THE AIRPLANE. DIVERTED WHEN TOLD IT MAY HAVE BEEN A GEAR DOOR. REPLACED MISSING PANEL A2551030700260Y (LT MLG BAY FWD BULKHEAD).SDR FDEA200905141657Gcu · failedWITH NR 2 GEN DEFERRED, GOT APU GEN FAULT ON TAKEOFF AT 90KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 24-23-01 CATEGORY: C EXPIRATION: 24MAY09 "MEL 24-23-01: APU GEN SYSTEM - INOP." REF: SDR NR 09-1656 AND WRI 24-20/1826 FOR OTHER DISCREPANCY.SDR FDEA200905141656Gcu · failedNR 2 GEN FAULT ON START . REPLACED NR 2 GENERATOR CONTROL UNIT PER AMM 24-22-12-4. PERIODIC TEST GOOD PER AMM 24-41-00-0. NR 2 GEN CKS GOOD ON ENG RUN. OK FOR SERVICE. REF: WRI 24-20/1825, FOR OTHER DISCREPANCY.SDR FDEA200903210981Wire Harness · failedAT TOP OF DESCENT NR 2 ENG OIL PRESS INDICATED 0 PSI ON ECAM AND MECHANICAL GAUGE. SHUT DOWN ENGINE. WINDMILLED FOR 33 MINUTES INDICATING 0 OIL PRESSURE OIL TEMPS MATCHED PRIOR TO SHUTDOWN. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE HARNESS (224W9722) IAW MSDR 08FDEA00359Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR 32 LBL 67 FWD SIDE, REWORKED CRACKED FLOORBEAM IAW 53-10-15 FIG 212 SHEET 2.SDR 08FDEA00358Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR 31 LBL67 FWD SIDE REWORKED CRACKED AREA IAW SRM 53-10-15 AND SRM 51-22-0, FINISHED REWORKED AREA IAW 51-75-10.SDR 08FDEA00357Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR31 LBL67 FWD SIDE REWORKED CRACKED AREA IAW SRM 53-10-15 AND SRM 51-22-0, FINISHED REWORKED AREA IAW 51-75-10.SDR 08FDEA00355Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR30 LBL 27 FWD SIDE REWORKED AREA IAW 51-75-10 53-10-15 FIG 212, FINISHED REPAIR IAW 51-75-10-8.SDR 08FDEA00354Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR25 RBL27 FWD SIDE REWORKED REPAIR AREA IAW 53-10-15, SRM 51-21-10 AND SRM 51-75-10, FINISHED REPAIR IAW SRM 51-40-21.SDR 08FDEA00353Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR25 RBL27 FWD SIDE REWORKED REPAIR AREA IAW 53-10-15, SRM 51-21-10 AND SRM 51-75-10, FINISHED REPAIR IAW SRM 51-40-21.SDR 08FDEA00352Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR23 RBL27 FWD SIDE REPAIRED FLOORBEAM IAW 53-10-15 FIG 212, RESTORE FINISH IAW 51-21-10.SDR 08FDEA00351Floorbeam · crackedMCD FLOORBEAM HAS CRACK AT FR 30 LBL 67 FWD SIDE REWORKED AREA OF FLOORBEAM IAW SRM 51-10-15 FIG 212, RESTORED AREA IAW SRM 51-710.SDR 08FDEA00299Seat Track · corrodedMAIN DECK SEAT TRACK HAS COROSION BETWEEN FR 69 AND FR 70, LBL18. INSTALLED NEW SEAT TRACK SECTION P/N NR A53274005. FABRICATED FROM MATERIAL DAN200IT79511, BATCH NR 0000993114, IAW SRM 53-10-16 AND 53-23-00.SDR 08FDEA00298Seat Track · corrodedMAIN CARGO SEAT TRACK AT RBL 57 BETWEEN FR 58 AND FR 60 HAS 4 PLACES WITH CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK FABRICATED FROM A532-74005-200, MATERIAL DAN200IT79511IAW SRM53-10-16 AND 51-23-00.SDR 07FDEA01779Connector · looseNR 2 ENGINE THRUST REVERSER DEACTIVATED DUE TO MEL OF NR 2 ENGINE HP VALVE (MEL 36-11-03). MEM MX FAILED TO SECURE ALL CONNECTORS PER MEL 78-30-01-A. MX SECURED ALL C/P'S PER MEL AND FLT CONTINUED.SDR 07FDEA00489Door · unlatchedCLIMBIMG THRU FL 220, ECAM WARN LEFT CABIN DOOR UNLATCHED. VISUAL INSPECTION SHOWED BOTH LATCH INDICATIONS FULL RED, RETURNED TO MEMPHIS. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01. CATEGORY: C EXPIRATION: 24FEB07 "MEL 52-71-01: (IDENTIFY) L1 DOOR CLOSED ANSDR 06FDEA03891Drain · leakingON TAKEOFF ROLL, NOTED FIRST OFFICER'S AIRSPEED INDICATION ON HIS PFD WAS NOT INCREASING. ABORTED TAKEOFF APPROX 100KTS. PRESSURIZED PITOT SYS REF MM 34-10-00-5, SEPARATED AND CAPPED PITOT TUBING RUN AS NECESSARY TO ISOLATE LEAK. FOUND CULPRIT TO BE SYSTEM SDR 05FDEA03239Landing Gear · malfunctionedRIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.SDR 05FDEA03193Rib · crackedLT NR 5 SPOILER, LT CENTER HINGE, HINGE PIN HEAD HAS ROTATED AND CRACKED THE FLANGE OF THE SUPPORT RIB ABOVE IT. VIEW FROM TOP OF WING THROUGH ACCESS PANEL BETWEEN CENTER HINGES. FABBED AND INSTALLED ANGLE AND STOP BLOCKS IAW EA NR 6-5710-91294.SDR 05FDEA03118Limit Switch · malfunctionedL1 DOOR ESCAPE SLIDE WARNING LIGHT (13WN) DOES NOT ILLUMINATE DURING TEST. REPLACED SWITCH NSA932030-02SDR 04FDEA02360Seat Track · corrodedFWD MAIN DECK BETWEEN FR 12-13 FWD OF RT SEAT TRACK 2 AND 3 T-CAP IS CORRODED. REMOVED AND REPLACED TRACK (T-CAP) AT MAIN DECK BETWEEN FR 12-13 FWD OF SEAT TRACK NR 2 AND 3 IAW A300-600 SRM 51-40-21.
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