N654FE

Service difficulty reports · 237

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 = 'N654FE' 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.

SDR FDEA201106302505Seat Track · gougedSEAT TRACK NR1 HAS GOUGE ON SCALLOP AT FR54.2 CLS ADAPTER. R & R CLS ADAPTER IAW SRM 51-40-21 AND REPROTECTED CLS ADAPTER IAW SRM 51-75-10.Jun 30, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106262430Frame · dentedFRAME 21 SPLICE AND FRAME HAVE DENT 4 IN LONG BETWEEN S8-9R. REMOVED DAMAGED SPLICE ANGLE. CUT OUT CRACKED FRAME SECTION IAW OE-738-06-11-009. FABRICATED NEW REPAIR ANGLE AND FILLERS IAW OE-738-06-11-009. INSTALLED REPAIR PARTS IAW OE 738-06-11-009. NDT VERIJun 26, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201106222387Skin · dentedRIGHT CENTER FLAP HAS 3 DINGS, DEPRESSIONS ON LOWER SURFACE,OTBD OF NR 3 TRACK, APPROX 15 IN AFT OF L/E. FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00,PG 216. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-50-00, PG 219.Jun 22, 2011 · N654FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201106152278Intercostal · damagedMAIN CABIN RT SIDE INTERCOSTAL AT SEAT TRACK 6R FRAME STA 38.2 ATTACH POINTS (6 EA) HOLES HAVE TOOL MARKS. FABRICATED REPLACEMENT PART PER DRAWING A5381317O REPROTECTED PART IAW SRM PG 202,203Jun 15, 2011 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201106092175Seat Track · corrodedSEAT TRACK 4L HAS CORROSION ON FLANGE BETWEEN FRAMES 27-29, 5EA AREAS. REMOVED LEVEL ONE CORROSION IAW SRM 51-74-10 PAGE 204/208. CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 103 FIG 101. REMOVED DAMAGED SECTION SEAT TRACK MDCC, 4L, IAW SRMJun 9, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106092173Seat Track · corrodedSEAT TRACK 5L HAS CORROSION ON OTBD FLAGE BETWEEN FR-49 AND FR-50, ABOUT 6-SQ INCHES. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND SEAT TRACK SECTION OUT OF LIMITS IAW SRM 53-10-16.REMOVED AND REPLACED SEATRACK SECTION IAW SRM 53-10-16 FIG 205.Jun 9, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106082163Frame · dentedMDCC AT FRAME 22 SPLICE AND FRAME HAS A DENT 3 IN. LONG BETWEEN STRINGER 8R AND 9R. R & R SPLICE ANGLE AT FRAME 22 BETWEEN STR 8R AND 9R IAW SRM 51-72-10.Jun 8, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201106042115Seat Track · corrodedSEAT TRACK 4L HAVE 5 PLACES OF CORROSION ON OTBD SIDE WALL ABOUT 0.5" SQUARE EACH BETWEEN FR34 AND FR37. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101 PG 103. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10 PG 1,2 AND 3.Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106042116Seat Track · corrodedSEAT TRACK 6L HAS CORROSION ON FLANGE AT FRAME 27. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICES REF IAW SRM 53-10-16 FIG 201A PAGE 208A / 208B.Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106042117Seat Track · corrodedSEAT TRACK 2R HAS CORROSION ON FLANGE BETWEEN FRAME 30 -32. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK 2R WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201.Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106042114Seat Track · corrodedSEAT TRACK 3R HAS CORROSION ON FLANGE AT FR 27. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 103, FIG 101. LOCATED DRILLED AND INSTALLED SEAT TRACK. REPAIR SECTION IAW SRM 53-10-16, PG 207/208, FIG 201.Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106042113Floorbeam · crackedMAIN CABIN RT SIDE AT STA C59 BETWEEN 3R AND 4R SEAT TRACK FLOORBEAM HAS CRACK, AFT SIDE MIDDLE STIFFENER. REMOVED CRACK NDT VERIFIED NO CRACKS EXIST IAW NTM 51-10-08. INSTALLED REPAIR ANGLE IAW SRM 53-10-15, FIG 211.Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201106042111Floorbeam · crackedCRACK AT FWD FACE OF MAIN DECK FLOORBEAM RBL 24. 1" BELOW UPPER FLANGE, FRAME 21. REMOVED CRACK AT FLOORBEAM RBL24, FR21 IAW SRM 53-10-15, FIG 212. PERFORMED NDT TO VERIFY CRACK FREE CONDITION AND SHOWS NO CRACK INDICATION AFTER TRIMMED OUT, PERFORMED REPAIR Jun 4, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201106022099Seat Track · corrodedMAIN CABIN LT SIDE AT FR 58 TO FR 59 SEAT TRACK 1 HAS CORROSION ON OTBD SIDE. REMOVED LEVEL 1 CORROSION ON SEAT TRACK 1 AT FR 58 TO FR 59 AND WAS FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201.Jun 2, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105272012Floorbeam · crackedMAIN DECK FLOORBEAM FWD FACE STIFNER AT UPPER FLANGE CRACKED (0.25") AT FR26 BETWEEN SEAT TRACK 2R AND 3R. ROUTED OUT CRACK ON FLOORBEAM FWF FACE OF FR 25 IAW SRM 53-10-15 PG 394 ITEM 3. NDT VERIFIED NO CRACK EXISTS IAW NTM 51-10-08. FABRICATED AND INSTALLMay 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201105272013Floorbeam · crackedAFT FUSELAGE FR60 FLOORBEAM CRACKED AT VERTICAL STIFFENER BETWEEN SEAT TRACK 4 AND 5R. CUT OUT DAMAGED AREA IAW SRM 53-10-15 FIG 211 NDT VERIFIED NO CRACKS IAW NTM 51-10-08. LOCATED DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 53-10-15 FIG 211.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201105272006Seat Track · corrodedMDC SEAT TRACK 2R HAS 1" SQUARE OF CORROSION ON INBD FLANGE AT FR14A. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10 PG 1-3.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105272009Floor Support · crackedMDCC FLOOR SUPPORT STRUCTURE BETWEEN FR38.1 AND FR38.2, OB OF SEAT TRACK 6R IS CRACKED (ABOUT 2"). REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE BETWEEN FR 38.1 AND FR 38.2 O/B OF SEAT TRACK 6R IAW SRM 51-40-21 PARA 7May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201105272007Seat Track · corroded6 AREA OF CORROSION ON MCD SEAT TRACK 2L SCALLOP FROM 7" FWD OF FR19 TO 19" FWD OF FR17. FOUND TO BE OUT OF LIMITS.REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10 PG 1-3.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105272005Seat Track · corroded5" SQUARE OF EXFOLIATION COROSSION ON MDC SEAT TRACK 3L INBD FLANGE, 6" FWD OF FR19 TO 11" FWD OF FR19. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK 3L FR 15 TO FR 19 IAW SRM 51-72-10 PG 1-3.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105272011Floor Support · corrodedBULK CARGO PIT FLOOR FR63 FLOOR SUPPORT UNDERNEATH ROLLER TRAY 30 IN RT OF C/L HAS 1 SQ IN EXFOLIATED CORROSION. AFTER REMOVAL OF LEVEL 1 CORROSION, FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. R & R FLOOR SUPPORT REPAIR SECTION STRUCTURE IMay 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201105272010Floorbeam · crackedAFT FUSELAGE FR66 FLOOR BEAM CRACKED AT VERTICAL STIFFENER BETWEEN SEAT TRACK 3 AND 4L.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA201105272008Floorbeam · crackedAFT CARGO COMPT AT FR58 FLOORBEAM IS CRACKED APPROX 1/4 INCH LONG BETWEEN SEAT TRACKS 3 AND 2 RT, BELOW CLS ADAPTOR. REMOVED CRACKED FLOORBEAM & REPLACED WITH NEW SECTION IAW SRM 53-10-15, FIG 207.May 27, 2011 · N654FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200908193051Indication Sys · malfunctionedACFT WAS LOADED WITH 30.1 FUEL, SHORTLY AFTER T/O GOT ECAM ALERT, BOTH CTR FUEL TANKS FAULT- DIRECTED US TO TURN OFF BOTH CTR FUEL PUMPS. TOTAL FUEL DROPPED TO 17.0 AND LT OUTER TANK INDICATED 2.1. TURNED BACK TO DEPARTURE, LOWEST FUEL TOTAL WAS 15- WITH AAug 19, 2009 · N654FE · Airbus A300F4605R · Fuel Indicating SystemSDR FDEA200904151305Landing Gear · lack of lubeAT 170 KIAS,WHEN GEAR LOWERED NOSE GEAR INDICATED UNSAFE FOR APPROX 15 SECONDS( BOTH GEAR INDICATOR PANELS) SAFE INDICATION ACCOMPANIED BY GEAR MOVEMENT /LOCKING SOUNDS. LUBED GEAR PER MM 12-22-32-0 COMPLED WITH NORMAL NOSE GEAR EXTENSION PER MM 32-31-00-5Apr 15, 2009 · N654FE · Airbus A300F4605R · Nose/Tail Landing GearSDR 08FDEA04906Skin · damagedRT WING CENTER FLAP T/E HAS DAMAGE REMOVED DAMAGED SKIN IAW SRM 57-50-00 FIG 206. PERFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATION NOTED. FABRICATED REPAIR DOUBLER IAW SRM 57-50-00 FIG 206. TREATED REPAIR PARTS IAW SRM 51-21-10. PRIMED REPAIR PARTSNov 18, 2008 · N654FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA04899Mount · corrodedNR 1 PYLON ENGINE PYRAMID MOUNT ALIGNMENT PIN HOLE IS PITTED. CHECKED ALLOWABLE LIMITS OF SPIGOT FITTING IAW SRM 54-51-81. ORIGINAL HOLE DIAMETER OF 1.350. FOUND TO BE OUT OF LIMITS DIAMETER WAS 1.371. REAMED HOLE IN STEPS OF 1.389-1.410, TO 1.409-1.428 WNov 17, 2008 · N654FE · Airbus A300F4605R · Engine Mount SectionSDR 08FDEA04872Nose Cowl · gougedNR V 1 NOSE COWL HAS A MINOR SCRATCH AT 10 O'CLOCK POSITION LEADING EDGE. REMOVED DAMAGED SKIN AREA IAW SRM 54-10-00 REPAIR NR 9. FABRICATED SKIN PATCH AND DOUBLER IAW SRM 54-10-00, LOCATED AND DRILLED PATCH AND DOUBLER IAW SRM 51-40-44. HEAT TREATED PATCHNov 13, 2008 · N654FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA04848Skin · damagedLOWER FUSELAGE HAS LIGHTNING STRIKE ON STR 54L 4TH FASTENER FWD OF FR 34. CUT-OUT DAMAGE IAW SRM 53-10-12 FIG 207, PERFORMED HFEC OF CUT-OUT AREA IAW NTM 51-10-08 PT6. NO CRACK INDICATIONS NOTED. FABRICATED DOUBLER FROM 2024-T3 .071C IAW SRM 53-10-12 FIG 20Nov 11, 2008 · N654FE · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 08FDEA04844Seat Track · corrodedMAIN CARGO DECK SEAT TRACK RBL 58 HAS CORROSION 7 INCH FWD OF FRAME 49. REMOVED AND REPLACED SEAT TRACK FROM FR 45 TO FR 54 IAW SRM 51-40-21- AND 51-40-44.Nov 11, 2008 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04832Seat Track · corrodedMAIN CARGO DECK SEAT TRACK RBL 18 HAS CORROSION 3 INCHES FWD OF FRAME 42. REMOVED AND REPLACED SEAT TRACK FROM FR 40 TO FR 44 IAW SRM 51-40-41AND 51-40-44.Nov 10, 2008 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04828Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 47, 3 INCHES BELOW STR 12L REPAIR COMPLIED WITH ON EA 6-5310-133939.Nov 10, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04789Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 47 3 INCH BELOW STR 12R BLENDED AREA IAW SRM 51-73-10, FOUND TO BE WITHIN LIMITS. PERFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATIONS NOTED. TREATED AND PRIMED IAW SRM 51-23-20.Nov 7, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04786Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 54 3 INCH BELOW STR.12L BLENDED AREA IAW SRM 51-73-10, FOUND TO BE WITHIN LIMITS. PERFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATIONS NOTED, TREATED AND PRIMED IAW SRM 51-23-20.Nov 7, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04785Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 54 3 INCHES BELOW STR 12R. BLENDED AREA IAW SRM 51-73-10, FOUND WITHIN LIMITS. HFEC IAW SRM 51-10-08 PT6, NO CRACKS FOUND. TREATED AND PRIMED IAW SRM 51-23-20.Nov 7, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04783Frame Splice · damagedMAIN CARGO DECK HAS DAMAGE ON FRAME 21 TRUSS SPLICE BETWEEN STR 8R AND STR 9R WITH SHEARED RIVETS ON STR 9R. REMOVED AND REPLACED TRUSS SPLICE AT FRAME 21 STR 8, STR 9, AND STR 13 IAW SRM 51-40-21. FABRICATED PARTS ON TRAVELERS T8/765472, T8/765399, T8/76547Nov 7, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04769Frame · gougedMAIN CARGO DECK HAS DAMAGE ON FRAME 24 TRUSS SPLICE BETWEEN STR 8R AND STR 9R. REMOVED DAMAGED SPLICE IAW SRM 51-40-21AND REWORKED IAW SRM 51-26- 00, PERFORMED NDT CRACK TEST IAW NTM 51-10-08 PT 6. NO CRACK INDICATION NOTED, TREATED AND PRIMED IAW SRM 51-21Nov 6, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04762Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 4.5 INCHES ABOVE STR 22L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04761Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 1 INCH BELOW STR 19L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04759Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 2.125 INCH BELOW STR 18L, REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04758Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 3 INCHES ABOVE STR 18L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04751Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 1 INCH ABOVE STR17 L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04743Frame · gougedMAIN CARGO DECK HAS GOUGE ON FR 28, 2.5 INCH ABOVE STR 14L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04741Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME 28, 2.5 INCH ABOVE STR 21L. REPAIR COMPLIED WITH ON EA 6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04738Frame · gougedMAIN CARGO DECK HAS GOUGE ON FR 28, 1 INCH ABOVE STR 20L. REPAIR COMPLIED WITH ON EA6-5310-123938.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04732Frame · bentMAIN CARGO DECK FR 59 BENT BELOW STR 13L 2 INCH TO 4 INCH. REWORKED THE UPPER FLANGE SECTION IAW SRM 51-26-00, PERFORMED HFEC INSPECTION IAW NTM 51-10-08 PT 6. NO CRACK INDICATIONS NOTED.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04731Frame · bentMAIN CARGO DECK HAS BENT FRAME 58 FROM STR 13L 4.5 INCH TOWARD STR 14L. REWORKED THE UPPER FLANGE SECTION IAW SRM 51-26-00, PERFORMED HFEC INSPECTION IAW NTM 51-10-08 PT 6. NO CRACK INDICATION NOTED.Nov 5, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04692Splice · damagedMAIN CARGO DECK HAS DAMAGE ON FRAME 22 TRUSS SPLICE BETWEEN STR 8R AND STR 9R WITH SHEARED RIVETS ON STR 9R. REMOVED AND REPLACED PROFILE AND SPLICE IAW SRM 51-40-21.Nov 4, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR 08FDEA04704Frame · gougedMAIN CARGO DECK HAS 2 GOUGES ON FR 24 2.75 INCH BELOW STR13R AND 2.5 INCHES BELOW STR 14. REMOVED AND REPLACED FRAME SECTION BETWEEN STR 13R AND 21R IAW SRM 51-40-21. FABRICATED FRAME SECTION ON TRAVELER T8/ 765475.Nov 4, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA04702Frame · gougedMAIN CARGO DECK FR 20 HAS GOUGE 2.5 INCHES BELOW STR 12R. REPAIR COMPLIED WITH ON EA 6-5310-124032.Nov 4, 2008 · N654FE · Airbus A300F4605R · Fuselage Main, Frame
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