N652FE
Service difficulty reports · 320
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 = 'N652FE' 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 = 'N652FE' 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 FDEA201812143502Floor Panel · damagedFLOOR PANEL 122JF FWD CORNER HAS EDGE DAMAGE. FABRICATED NEW PANEL PER SRZ-25-005 REV P.SDR FDEA201803040597Seat Track · damagedSEAT TRACK DAMAGE AT 8L & 7L. SEAT TRACK ADAPTER DAMAGE IN POSITION 8L & 7L NEAR RESTRAINT D1458 & C1467. REMOVED OLD SEAT TRACK CUT NEW SEAT TRACK AND SPLICE PIECES TO FIT DRILLED PILOT HOLES AND CLECOED INTO PLACE ALODINED PRIMED AND PAINTED ALL BARE METAL SDR FDEA201702230639Connector · damagedAFTER LANDING ROLLOUT, THE NOSE WHEEL STEERING ALMOST FROZEN IN A SMALL, APPROX 10 DEGREE RANGE NEAR CENTER. USED DIFFERENTIAL BRAKING TO CLEAR RUNWAY. NO OTHER INDICATIONS OR ADVERSE FACTORS. TOWED TO THE GATE. THE ACFT HAS LESS THAN 10 DEGREES OF TILLER MOSDR FDEA201609223347Floorbeam · crackedMAIN DECK CARGO FRAME 31 CROSSBEAM CRACKED, BETWEEN Y1456 AND Y1959. REPAIRED IAW SRM 53-10-15 FIGURE 212. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223346Rib · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND OUTER FLAP RIB 3 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0328395 PT1 MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223345Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.2 AND 2.3. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223344Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223343Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 21 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223342Stiffener · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223341Stiffener · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223340Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 19 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223339Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223338Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 17 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223337Stiffener · crackedLEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609223336Stiffener · crackedLEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 11 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609193311Pressure Deck · crackedHORIZONTAL PRESSURE DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y953 AND Y1456. REPLACED THE PRESSURE DECK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201609193310Pressure Deck · crackedHORIZONTAL PRESSURE DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y0 AND Y-450. REPAIRED IAW SRM 53-15-15-201 PARA.5 FIG.201. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201602190665Warning System · false activationON TAKEOFF ROLL, BETWEEN 60-70 KTS, GOT A LOW GREEN HYD PRESS SYS 1 & 2. FOLLOWED BY NR 6 SPOILER FAULT. REJECTED TAKEOFF, CLEARED RUNWAY, RAN QRH. ENGS RAN IAW JRH, REF AMM 29-10-00-05 MAIN HYD POWER NORMAL AT THIS TIME, NO HISTORY & ACFT OK FOR SERVICE. SDR FDEA201602190648Warning System · false activationON TAKEOFF ROLL, BETWEEN 60 - 70 KTS, GOT A LOW GREEN HYD PRESS SYS 1 & 2. FOLLOWED BY NR 6 SPOILER FAULT. REJECTED TAKEOFF, CLEARED RUNWAY, RAN QRH. ENGS RAN IAW JRH, REF AMM 29-10-00-05 MAIN HYD POWER NORMAL AT THIS TIME, NO HISTORY & ACFT OK FOR SERVICESDR FDEA201512254078Hmu · malfunctionedAT TOP OF DESCENT, NR 1 ENG STARTED A SERIES OF 6 - 7 STALLS. FOLLOWED THE QRH & OPERATED AT IDLE. N1 STARTED TO DECREASE & EGT CLIMBED TO 622 AT SHUTDOWN. PARAMETERS AT SHUTDOWN N1 29.5, EGT 622, N2 66.6 WIND MILLING TIME WAS 10 MIN PERFORMED BORESCOPE INSDR FDEA201508092521Pump · failedNUMBER 1 GREEN ENG PUMP FAILED ON TAKEOFF. COMPLIED WITH ECAM. PUMP WAS RUN FOR 3 MINS BEFORE TURNED OFF. PUMP SWITCH WAS OFF WITH ENG RUNNING FOR A MIN, AIR TIME PLUS TAXI. COMPLETED INSTALLATION OF NR 1 ENG GREEN HYD PUMP IAW AMM 29-11-32-04-02. BLEEDISDR FDEA201409302877Lug · corrodedRIGHT RIB 5 MLG FWD LUG HAS CORROSION IN BORE, FWD FACE & AFT FACE. COMPLIED WITH EA 6-5710-T0311735 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201409302875Rib · corrodedLEFT RIB 5 MLG FWD LUG CORROSION IN BORE, FWD FACE & AFT FACE. COMPLIED WITH EA 6-5710-T0311735 P1 WINGS BASIC WITH STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201406171479Seat Track · corrodedMAIN DECK SEAT TRACK FRAME 48 - 49, Y-1456 CORRODED. REPAIRED SEAT TRACK IAW EA 6-5310-T0308972. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201406111394Floorbeam · crackedMAIN DECK CARGO FLOORBEAM CRACKED AT FRAME 30, -Y450-Y953. REPAIRED IAW EA 6-5310-T0308932 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201301170120Apu · leakingON TAXI OUT, MAIN DECK CARGO SMOKE WARNING RETURNED. TROUBLESHOT SYS REF TSM 26-19-00. UPON ARRIVAL AT ACFT. MAIN CARGO DECK AND FLIGHT DECK HAD A VERY STRONG ODOR OF DEICE FLUID. INSPECTED PACKS AND FOUND DEICE FLUID IN LT PACK. OPENED AND CLEANED COALESSDR FDEA201301160105Coalescer Bag · contaminatedDEPARTING, PASSING THROUGH 2000 FT, RECEIVED RED ECAM AND ASSOCIATED OVERHEAD INDICATION FOR MAIN DECK CARGO SMOKE AFT. ACCOMPANIED BY SMOKE IN COCKPIT. AFTER LANDING, OPENED COCKPIT DOOR TO SEE FORWARD COMPARTMENT FILLED WITH SMOKE. ACFT WAS DEICED FOR 20 SDR FDEA201301150119Coalescer Bag · dirtyON TAKEOFF, MID 1 AND AFT SMOKE DETECTOR LOOP A'S FAULT LIGHTS CAME ON FOR APPROX 10 SECS, THEN EXTINGUISHED. PERFORMED CARGO COMPARTMENT SMOKE DETECTION TEST, REF AMM 26-16-00-05-01. NO DEFECTS NOTED AT THIS TIME. PERFORMED MAIN DECK CARGO COMPARTMENT SSDR FDEA201301120086Warning Light · false activationAFTER TAKEOFF GOT MID 1 AND MID 2 MAIN CARGO SMOKE WARNING. RETURNED TO DEPARTURE. DETECTOR 7WU, MID 2 DETECTOR 11WU, MID 1 DETECTOR CONTROL UNIT AND MID 2 DETECTOR CONTROL UNIT IAW TSM 26-19-00 AND REF 26-19-12-04. R & R 4WU, 8WU AND 12WU MAIN DECK SMOKE SDR FDEA201210303774Union · strippedDURING TAKE OFF, CAPT'S AIRSPEED 60KTS F/O 120KTS, REJECTED TAKE OFF. FOUND UNION STRIPPED AT CAPTAIN'S PITOT TUBE WHILE REMOVING FITTING. RAN DRY NITROGEN THROUGH TUBING FROM ADC TO CONNECTION AT PITOT TUBE. R & R CAPTAIN'S PITOT TUBE IAW MM 34-11-15-04. SDR FDEA201112285450Spar · wornNR 1 PYLON AFT SIDE LOWER SPAR HYD RESERVOIR PRESSURE LINE HOLE ELONGATED BETWEEN RIB 19 AND 20. R & R WEB IAW SRM 51-40-21, PARA 6A.SDR FDEA201112235441Shear Plate · corrodedMAIN CABIN LT SIDE FR 25 TO FR 30 BETWEEN SEAT TRACKS 5L AND 6L 21EA AREAS OF CORROSION (THRUST PLATES) MAIN CABIN LT SIDE FR 25 THROUGH 30 SEAT TRACKS 5L AND 6L, R & R 5EA THRUST PLATES.SDR FDEA201112235440Shear Plate · corrodedMAIN CABIN LT SIDE FR 25 TO FR 30 BETWEEN SEAT TRACKS 5L AND 6L 21EA AREAS OF CORROSION (THRUST PLATES) MAIN CABIN LT SIDE FR 25 THROUGH 30 SEAT TRACKS 5L AND 6L, R & R 5EA THRUST PLATES.SDR FDEA201112225422Thrust Plate · corrodedMAIN CARGO LT SIDE FR 26 & FR 27 BETWEEN SEAT TRACKS 4L & 5L THRUST PLATE HAS 3 EA AREAS OF CORROSION. R & R THRUST PLATE AT FR 26 TO FR27 BETWEEN SEAT TRACKS 4L & 5L IAW SRM 51-72-10 AND SRM 51-40-21 PARA'S 6 AND 7. APPLIED PROTECTIVE COATING IAW SRM 51-7SDR FDEA201112215412Attach Fitting · corrodedNR 2 ENGINE PYLON TO WING LOWER ATTACH FITTING AT RIB NR 18 HAS 4 SQ IN OF CORROSION AT INNER RACE. R & R RIB 18 FITTING ON NR 2 PYLON IAW AMM 54-51-75-04-02.SDR FDEA201112205380Adapter · corrodedMDCC CLEVIS ADAPTER BETWEEN SEAT TRACKS 2R AND 3R AT FR 47 HAS A GOUGED SCALLOP AND 2EA AREAS OF CORROSION. R & R CLEVIS ADAPTER AT FR 47 IAW SRM 51-72-10, PARA 6, PAGES 1-3.SDR FDEA201112175330Bulkhead Web · corrodedFWD FUSELAGE AT FR 1 RADOME BULKHEAD FWD FACE, INSULATION SUPPORT WEB NR2 HAS 7 AREAS OF CORROSION. REMOVED LEVEL 1 CORROSION ON NR 2 WEB, 3 AREAS OUT OF LIMITS IAW SRM 53-10-00, PG 106, FABBED REPAIR ANGLES AND DOUBLER AND INSTALLED IAW SRM 51-71-30, PG 203,SDR FDEA201112165319Seat Track · wornSEAT DUMMY TRACK RT NR 4 AT FR.38.2 - 40 WEAR GAP VALUE (A) MEASUREMENT IS MORE THAN .0157 BUT LESS THAN .0846 ACTUAL MEASUREMENT .019. REMOVED TRACK 4R IAW SRM 51-40-2. REPAIRED DAMAGED AREA IAW SRM 53-15-16. RE-INSTALLED TRACK IAW SRM 51-40-21.SDR FDEA201112165318Adapter · gougedFLOOR CLEVIS ADAPTER CROWN INBD AND OTBD ENDS HAVE GOUGES FR 62 BETWEEN 2L AND 3L SEAT TRACKS. R & R CLEVIS ADAPTER IAW SRM 51-72-10 PARA 5 AND 6.SDR FDEA201112165314Skin · chafedFWD CARGO DOOR CUTOUT EXTERNAL SKIN AND EDGE HAS CHAFED 6.0 INCHES LONG, LOCATED AT FWD LOWER CORNER BETWEEN S39-42R FR 20. REPAIRED IAW EA 6-5310-156062.SDR FDEA201112155307Skin · crackedRIGHT NR 3 SPOILER HAS A ONE INCH CRACK ON INBD L/E TAB. REPAIRED CRACK IAW SRM 57-72-11 PARA 12. RESTORED SURFACE PROTECTION IAW SRM 51-75-10, PARA 3. COMPLIED WITH EA 6-5750-145699.SDR FDEA201112145265Floorbeam · misrepairedFLOORBEAM FR 64 BETWEEN SEAT TRACKS 3L YA53 AND 4L Y1456, HAS 1EA REPAIR ANGLE ON AFT UPPER FLANGE 12.4" LONG X 2.2" TALL IS INSTALLED WITH INCORRECT MATERIAL THICKNESS. COMPLIED WITH EA 6-5310-157802 PT1 BY REMOVING REPAIR ANGLE AND REINSTALLED REPAIR ANGLSDR FDEA201112145264Floorbeam · corrodedPROFILE LANDING BETWEEN SEAT TRACK 3R AND 4R FR. 54 HAS 1 SQ IN OF CORROSION AT FASTENER HOLE. R & R PROFILE AT FR 54 BETWEEN SEAT TRACKS 3R AND 4R IAW SRM 51-72-10.SDR FDEA201112135257Skin · dentedLEFT WING AILERON HAS NUMEROUS DENTS ON UPPER AND LOWER T/E SKIN SURFACES MEASURING .003" TO .028" DEEP. R & R LT WING AILERON T/E WEDGE IAW SRM 51-72-10, 51-40-21 AND DWG A57661002/A57661001. PROTECTED SURFACES IAW SRM 51-75-10.SDR FDEA201112125249Seat Track · damagedMID SEAT TRACK 2R OTBD FLANGE HAS 8 EA. SCREW HOLES THAT DO NOT HAVE ADEQUATE ED FROM FRAME 45 TO FRAME 51. SEAT TRACK 2R AT FR 45 TO FR 51. R & R IAW SRM 51-72-10 PAGES 1-3. APPLIED PROTECTIVE COATINGS IAW SRM 51-75-10.SDR FDEA201112105239Retainer · deformedFWD CARGO DOOR CUTOUT MID PROFILE PANEL RETAINER DEFORMED. R & R RETAINER IAW SRM 51-72-10, PGS 1-3.SDR FDEA201112045141Seat Track · corrodedSEAT TRACK 2R HAS CORROSION BETWEEN FR 40 & FR 45. DEFFECT MEASURES 8 SQ INCHES. AFTER REMOVING LEVEL 1 CORROSION FROM SEAT TRACK IAW SRM 51-11-10 PAR 3, MATERIAL LOSS AND LIMIT CHECKED IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW SDR FDEA201112045149Fitting · crackedFR 49, TRACK 4L VERTICAL SUPPORT LEG IS CRACKED ON BOTTOM INBD FLANGE. R & R FITTING ON FR 49 TRACK 4L VERTICAL SUPPORT LEG IAW SRM 51-40-21, PARA 5, PG 7 AND IAW SRM 51-72-10.SDR FDEA201112025126Seat Track · corrodedMID MDCC SEAT TRACK 5L CORRODED AT 2 LOCATIONS BETWEEN FR 30 AND FR 32. AFTER REMOVAL OF LEVEL 1 CORROSION ON SEAT TRACK 5L AT 2 LOCATIONS, BETWEEN FR 30 AND FR 32, IAW AMM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 102. FOUND TO BE OUT OF LIMIT. R & R SDR FDEA201112025130Seat Track · corrodedMAIN CARGO CABIN AT FRAME 27 & 28 RT SIDE SEAT TRACK 3R INBD FLANGE HAS 3 EA AREAS WITH CORROSION. REMOVED CORROSION IAW SRM 51-74-10. CORRODED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. R & R SEAT TRACK IAW SRM 51-72-10, 53-10-16, AND 51-40-
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