N651FE
Service difficulty reports · 421
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 = 'N651FE' 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 = 'N651FE' 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 FDEA201506121774Seat Track · damagedMAIN DECK SEAT TRACK Y1959 SCALLOPS DAMAGED FR54.2 REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21.SDR FDEA201506111770Seat Track · corrodedCORROSION ON SEAT TRACK BETWEEN FRAMES 26 - 27 Y953. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM-53-10-16 FIG. 101, REMOVED AND REPLACED THE SEAT TRACK IAW SRM-53-10-16 PG. 207, FIG. 201. CAT"A" MAJOR REPAIR.SDR FDEA201506111769Floor Panel · damagedFLOOR PANEL AT FRAME 13A AND BETWEEN FLOORBEAMS YE AND YD HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW-DWG SRZ-25-005 CATEGORY "A" MAJOR REPAIR.SDR FDEA201506111768Floor Panel · damagedCOURIER AREA FLOOR PANEL 221 PF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 CATAGORY "A" MAJOR REPAIR.SDR FDEA201506111767Floor Panel · damagedCOURIER AREA FLOOR PANEL 221LF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW-DWG SRZ-25-005, CATAGORY "A" MAJOR REPAIR.SDR FDEA201506111764Floor Panel · damagedCOURIER AREA FLOOR PANEL 221RF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 CATAGORY "A" MAJOR REPAIR.SDR FDEA201506111762Floor Panel · damagedCOURIER AREA FLOOR PANEL 222QF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 CAT "A" MAJOR REPAIR.SDR FDEA201506111760Floor Panel · damagedCOURIER AREA FLOOR PANEL 222RF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 CAT"A" MAJOR REPAIR.SDR FDEA201503090746Processing Unit · failedAFTER TAKEOFF CAPTAIN ADC FAILED. AFTER TAKEOFF & AFTER SLAT RETRACTION 15/0 TAKEOFF GOT A SYS 1 FLAP FAULT. CYCLED THE SLATS & FLAPS 15. BOTH MOVED BUT FLAPS WERE SLOW. ON APPROACH PS 20 BOTH FLAP SYS 1 & 2 FAULTED & A FLAP 20 LANDING WAS MADE. PERFORMEDSDR FDEA201408082118Gimbal Joint · contaminatedON FINAL SELECTED FLAPS 20 & IMMEDIATELY GOT 2 FLAP SYS 1 & 2 FAULT LIGHTS. ELECTED TO GO AROUND & FOLLOWED ECAM & QRH PROCEDURES. AFTER LANDING, FLAP HANDLE SELECTED UP & THEY RETRACTED NORMALLY. FOUND TRACK 1 AND 2 GIMBLES ON BOTH WINGS WITH WATER UNDER SDR FDEA201407081669Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & IN FWD & AFT SPOT FACES. COMPLIED WITH EA 6-5710-T0309480 P-1 WING BASIC WING STRUCTURE RT RIB 5 FWD LUG CORROSION.SDR FDEA201407081668Rib · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE & AFT SPOT FACE REPAIRED LT RIB 5 FWD LUG IAW DWG R57240425 ISSUE C & EA 6-5710-T0309453.SDR FDEA201406061322Transmitter · leakingHYDRAULIC SYS BLUE LO PRESS IN FLT, COMPLIED WITH QRH. FOUND HYDRO FLUID LEAKING FROM AFT LT WW AREA. TROUBLESHOOTING IN PROGRESS TO ISOLATE. CREW REPORTED BLUE PUMP WAS TURNED OFF 30 SECONDS AFTER LOW PRESS INDICATION. BLUE HYD QTY IS JUST INSIDE THE BOTTSDR FDEA201401170121Spring · failedAFTER TAKEOFF, NOSE GEAR DOOR DID NOT CLOSE. BOTH SYSTEMS SHOWED DOOR UNSAFE, FOLLOWED ECAM. FOUND DOOR UPLOCK HOOK RETURN SPRINGS FOR LT NLG MAIN DOOR BOTH FAILED. R & R LT UP LOCK ASSEMBLY IAW MM 32-31-14-04. ACFT OK FOR SERVICE.SDR FDEA201401160117Spring · failedAFTER TAKEOFF, NOSE GEAR DOOR DID NOT CLOSE. BOTH SYSTEMS SHOWED DOOR UNSAFE, FOLLOWED ECAM. FOUND DOOR UPLOCK HOOK RETURN SPRINGS FOR LT NLG MAIN DOOR FAILED. R & R LT UPLOCK ASSEMBLY IAW MM 32-31-14-04.SDR FDEA201306071221Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION IAW EO 6-5710-7-3305, PART 4, STEP 11 OF HOLE 'C' AT RT WING REAR SPAR FOUND CRACK INDICATION AT 6 O'CLOCK TOWARDS AFT. REPAIRED IAW EA 6-5710-T0300640 REV A, P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201306041187Skin · misrepairedRT WING T/E CENTER FLAP UPPER SURFACE BETWEEN RIB 12 AND RIB 13 MISREPAIRED. REPAIRED IAW EA 6-5750-167168. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306041185Frame · misrepairedFORWARD CARGO COMPARTMENT DOOR CUT OUT AT FRAME 20A BETWEEN STRINGER 37 AND 41 RT MISREPAIRED. REPAIRED IAW DWG 13 R53706085, ISSUE C. REPAIR CLASSIFIED MAJOR IAW GMM6-2-100, REV 116.SDR FDEA201306041184Floor Panel · delaminatedMAIN DECK FWD UTILITY AREA LT DOORWAY FLOOR PANEL 221QF FOUND DELAMINATED. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100, REV 116. FLOOR PANEL R & R AMM 53-10-25, REV 55.2.SDR FDEA201306041183Mount · corrodedNR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING MATING SURFACE FOUND RUST. REWORKED IAW SRM 54-51-81, CONFIG 2, FIGURE 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR FDEA201306041182Mount · corrodedNR 2 ENGINE PYLON FORWARD ENGINE MOUNT FITTING AFT OTBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED AND FOUND WITH LIMITS IAW SRM 54-51-81, CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA NR 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA201306041181Mount · corrodedNR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING AFT INBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED IAW SRM 54-51-81 CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR FDEA201305251085Seat Track · misrepairedSEAT TRACK AT MAIN DECK BETWEEN FRAME 29 AND FRAME 30, Y =0 MISREPAIRED. REPAIRED IAW SRM 51-40-21, REV 23 & SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305251087Floor Panel · delaminatedAIR CONDITIONING COMPARTMENT FWD LT FLOOR PANEL FOUND DELAMINATED. REMOVED FLOOR PANEL AND INSTALLED IAW AMM 20-21-12, REV 55.2 , NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116 .SDR FDEA201305251086Crossbeam · crackedMAIN DECK CARGO COMPARTMENT CROSSBEAM FOUND CRACKED AT STATION FRAME 31 BETWEEN SEAT TRACK Y1456 AND Y1959. CRACKED CROSSBEAM REPAIRED IAW SRM 53-10-15, FIG 212, REV 23 AND EA 6-5310-T0300636. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305221059Seat Track · misrepairedMAIN DECK CARGO TRACK -Y450, BETWEEN FRAME 32 AND 33 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305221061Cargo Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT Y1456, BETWEEN FRAME 53 AND FRAME 54, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-10, REV 23. FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 102, REV 23. DAMAGED CARGO TRACK REMOVED IAW SRM 51-40-21, REV 23. NESDR FDEA201305221060Cargo Track · corrodedMAIN DECK CARGO TRACK AT Y450, BETWEEN FRAME 52 AND FRAME 53, FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT IAW SRM 53-10-16, FIG 102, REV 23. R & R IAW SRM 51-40-21, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305221058Crossbeam · crackedMAIN DECK CARGO BAY CROSSBEAM FOUND CRACKED AT STATION FRAME 30 BETWEEN SEAT TRACK Y1456 AND Y1959. ACCOMPLISHED REPAIR AS IAW SRM 53-10-15, FIG 212 AND EA 6-5310-T0 300636 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305201035Crossbeam · misrepairedMAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 27 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305201034Crossbeam · misrepairedMAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 29 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305201032Crossbeam · misrepairedMAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 30 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 116.SDR FDEA201305201040Seat Track · misrepairedMAIN DECK CARGO SEAT TRACK BETWEEN FRAME 32 AND 33, -Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 202, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305201038Seat Track · misrepairedMAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 33 AND FRAME 34, -Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 202, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305201030Crossbeam · misrepairedMAIN DECK CARGO CROSSBEAM, FRAME 30 BETWEEN Y450 AND Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 212, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D, PART 1.SDR FDEA201305191026Crossbeam · misrepairedMAIN DECK CARGO COMPARTMENT CROSSBEAM 28 BETWEEN-Y450 AND-Y953 MISREPAIRED. CARRIED OUT REPAIR IAW EA NR 6-5310-167620.SDR FDEA201305191025Skin · misrepairedFUSELAGE SKIN FRAME 85 TO FRAME 86, BETWEEN STRINGER 13-15R. REPAIRED IAW SRM 53-10-12, FIG 208 AND 51-40-44, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D PART 1.SDR FDEA201305191024Seat Track · misrepairedSEAT TRACK BETWEEN FRAME 74 AND FRAME 76, Y =0 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305191023Skin · misrepairedFUSELAGE SKIN FRAME 77 TO FRAME 78, BETWEEN STRINGER 39 - 43R MISREPAIRED. REPAIRED IAW SRM 53-10-12, FIG 208, SHEET 1, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D, PART 1,SDR FDEA201209133317Floorboard · damagedMAIN DECK CARGO FLOORBOARD 231DH BETWEEN FR 19 & FR 21 SEAT TRACK 3 L & 4L HAS 15 " X1' AREA OF DAMAGE ON UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201105031703Outflow Valve · inoperativeDURING CLIMBOUT PASSING 10,000 FT, CABIN PRESS REG 1 FAULTED, COMPLIED WITH ECAM AND TURNED IT OFF. 1 MINUTE LATER, CABIN PRESS REG 2 FAULTED AND WE WERE IN MAN PRESSURE. IT APPEARED THAT THE AFT OUTFLOW VALVE WAS NOT PROGRAMMING PROPERLY.SDR FDEA201103161027Skin · crackedRT WING LOWER SKIN JUST IN FRONT AND OTBD EDGE OF ACCESS DOOR NR 675FB FOUND INTERIOR SUPPORT STIFFENER CRACKED. REPAIRED AS PER E.A. 6-5710-143870 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.SDR FDEA201103020828Rib · crackedLT WING INBD FLAP, T/E OF RIB 25A, 03 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT LT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201103020827Rib · crackedRT WING INBD FLAP, T/E OF RIB 25A, 02 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT RT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201103010808Crossbeam · damagedFORWARD CARGO COMPARTMENT AT FRAME 32 CROSS BEAM BETWEEN LONGERON 3 AND 4 FOUND 04 FASTENERS MISSING. FASTENERS INSTALLED AS PER E.A. 6-5310-92946, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201102210652Skin · crackedRT WING FIXED L/E SKIN UPPER CUTOUT FOR NR 2 SLAT INBD JACKSCREW, FOUND CRACKED. REPAIRED AS PER SRM 57-41-12 FIGURE 203, REVISION 19. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112. REPAIR CLASSIFIED CATEGORY B. TO PERFORMED DETAILED VISUAL INSPESDR FDEA201102210656Skin · crackedRT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 675FE FOUND CRACKED, APPROX 0.250 INCH LONG DURING HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED AS PER EA 6-5710-143870 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112SDR FDEA201102210654Skin · crackedLT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 575FE FOUND CRACKED APPROX 0.375 IN LONG DURING HIGH FREQUENCY EDDY CURRENT INSP. REPAIRED AS PER EA 6-5710-143871 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.SDR FDEA201102170584Frame · crackedCABIN RT SIDE FRAME 42 HOLE "B" FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP THROUGH WORK CARD E6-5310-7-5006A2, PT2. REPAIR CARRIED IAW EO NR E6 -5310 -7- 5006A2, PT2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201102160573Attach Fitting · crackedAFT CARGO COMPARTMENT DOOR ACTUATOR ATTACH FITTING AT FRAME 61A FOUND APPROX 1.2 IN LENGTH CRACKED DURING HIGH FREQUENCY EDDY CURRENT INSP. R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
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