N631FE
Service difficulty reports · 360
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 = 'N631FE' 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 = 'N631FE' 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 FDEA201508192612Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER BARREL NUTS HOLE SURFACE CORROSION. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508172596Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.205", FINAL HOLE DIAMETER 1.223", MAX ALLOWABLE DIAMETER 1.220". BUSHING FABRISDR FDEA201508172595Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.253", FINAL HOLE DIAMETER 1.258", MAX ALLOWABLE HOLE DIAMETER 1.254". OVERSISDR FDEA201508172594Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOUSDR FDEA201508172593Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.703", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOSDR FDEA201508172592Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION AT HOLE 4 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 2.311", FINAL HOLE DIAMETER 2.318", MAX ALLOWABLE HOLE DIAMETER 2.3135". OVERSIZED BUSHISDR FDEA201508172591Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-08. EXISTING THICKNESS UPPER 0.376", LOWER 0.376", MATERIAL REMOVED UPPER 0.007", LOWER: 0.007", REMAINING THICKNESS UPPER 0.369", LOWER 0.369SDR FDEA201508172590Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHISDR FDEA201508172589Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHINGSDR FDEA201508172588Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.408", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATESDR FDEA201508172587Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.407", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATEDSDR FDEA201508172586Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 10 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.668", FINAL HOLE 0.691", MAXIMUM ALLOWABLE HOLE 0.667". OVERSSDR FDEA201508172585Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-09. EXISTING THICKNESS UPPER 0.426", LOWER 0.448", MATERIAL REMOVED UPPER 0.006", LOWER 0.006", REMAINING THICKNESS UPPER 0.420", LOWER 0.442SDR FDEA201508172584Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.328", MATERIAL REMOVED 0.013", REMAINING THICKNESS 0.315", MINIMUM ALLOWABLE THICKNESS 0.320SDR FDEA201508172583Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED BSDR FDEA201508172582Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.258", FINAL HOLE 1.282", MAXIMUM ALLOWABLE HOLE 1.258". OVESDR FDEA201508172581Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257, MAXIMUM ALLOWABLE HOLE 1.220". OVERSDR FDEA201508172580Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.365", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.361", MSDR FDEA201508172579Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.357", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.353", MSDR FDEA201508172578Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.522", FINAL HOLE 0.591", MAXIMUM ALLOWABLE HOLE 0.584". SSDR FDEA201508172577Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.723", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.717", MISDR FDEA201506081721Pitot Tube · obstructedAFTER 80KT SPEED CHECK ON TAKEOFF ROLL, FIRST OFFICER LOST AIRSPEED WITH FIRST OFFICER`S SPEED IN RED FOOT. FIRST OFFICER HAD 40 KT ERROR IN V INDICATION. ROTATED & CLIMBED ON PITCH POWER. RAN QRH & DUMPED 20K FUEL, CAPTAIN`S SIDE NORMAL. LANDED 18C BOTH ASDR FDEA201504201268Elt · faultySUSPECT OUR ELT IS ACTIVE. HAVE BEEN LISTENING TO A STRONG ELT SIGNAL ON 121.5 FOR MOST OF FLIGHT. DUPLICATED TONE PRESENT ON BLOCK IN, WHILE LISTENING TO 121.5. ACCESSED ELT UNIT & PLACED SWITCH TO OFF, TONE CEASED ON 121.5. R & R ELT UNIT IAW M/M 23-25-0SDR FDEA201501070064Gearbox · failedDURING CLIMB, PASSING APPROX 9000 FEET, RECEIVED A LEVEL 2 MASTER CAUTION LIGHT FOR LOW OIL PRESSURE IN NR 2 ENGINE. REFERRED TO QRH. NR 2 OIL WAS IN THE RED INDICATING -2. IAW QRH NR 2 ENGINE WAS SHUTDOWN. ENGINE REMAINED SHUTDOWN FOR REMAINDER OF FLIGHT.SDR FDEA201311252866Indicator · inoperativeMDIS 63125-60 0009630 23NOV13 ANC CLOSE R1 DOOR SLIDE REMOTE PRESS INDICATOR INOPERATIVE. FACT 23NOV13 22:53. ANC R RELAMPED R1 DOOR REMOTE PRESS INDICATOR IAW MM 25-61-04-4, OK FOR SERVICE.SDR FDEA201309162236Tray · damagedFWD CARGO LATCH TRAY DAMAGED AT BS 609, X= 43. REPAIRED IAW EA 1- 5320- T0302535 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 117.SDR FDEA201309122189Support Fitting · crackedDURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, NR 7 LOWER DOOR FRAME SUPPORT FITTING, FOUND HOLE "D" CRACKED. AFTER REWORK TO SIZE 0.560" CRACK STILL EXISTS. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED ASDR FDEA201309122188Support Fitting · crackedDURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND LOWER DOOR FRAME SUPPORT FITTING FOUND HOLE "A" CRACKED. REWORKED TO SIZE 0.560" CRACK STILL EXISTS. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED AS MAJORSDR FDEA201309082161Seat Track · corrodedSEAT TRACK AT BS 935, X=8.5 FOUND CORRODED AT CROWN AREA. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 909 - 949, IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117SDR FDEA201212094271Line · leakingHYDRAULIC LEAKING NR 6 BRAKE. R & R HYD BRAKE LINE AND COUPLING, OPS AND LEAK CHECKED GOOD. REF MM 32-43-21-4 AND SMP.SDR FDEA201112305462Warning Light · illuminatedFSS DISCHARGE LIGHT ILLUMINATED ON OVERHEAD PANEL AFTER L1 DOOR CLOSED. 2L RED INDICATOR ILLUMINATED ON CONTROL PANEL. COMPLIED WITH EA 1-2624-155778, REV NO A POS.SDR FDEA201109294204Skin · misrepairedSKIN MISREPAIRED AT BS 715-735 LONGERON 47-48 RT. CARRIED OUT REPAIR AS PER SRM 53-00-01 REPAIR 1 FIG 201 REV 47. CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201109274152Frame · dentedFRAME BS 1701 L12R, FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 FIG. 201 REPAIR 2 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201109274151Frame · dentedFRAME BS 1681, L12R, FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REV 112.SDR FDEA201109274150Spar · crackedNR 2 ENGINE RT AIR INTAKE REAR SPAR INTERIOR SUPPORT STRUCTURE FOUND CRACKED.SDR FDEA201109234076Finger Doubler · crackedLT WING CAVITY OTBD OF NR 11 SLAT TRACK, FINGER DOUBLER FOUND CRACKED. REPAIR CARRIED OUT PER SRM 57-40-02 FIG. 203 REPAIR 9 REV 47. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.SDR FDEA201109234077Beam · crackedR3 DOOR , AFT SIDE NR 1 STOP FITTING , HORIZONTAL BEAM FOUND CRACKED. REMOVED AND REPLACED WITH NEW BEAM AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201109173927Engine · malfunctioned2 HRS AFTER TAKEOFF, NR 2 ENGINE ROLLED BACK. RPM AND EGT ROLLEDBACK, PERFORMED ENGI 2 SHUTDOWN IN FLIGHT. CHECKED NR 2 EEC A & B, NO CURRENT FAULTS. CARRIED OUT DETAIL AND WINDMILLING INSPECTION, CHECKED ALL MAGNETIC CHIP DETECTORS, NO ABNORMALITIES FOUND. SDR FDEA201108223399Engine · failedNR 3 ENGINE OIL QUANTITY INDICATED BOXED AMBER SHOWING 1 GAL OIL. TEMP INCREASED TO 135 DEGREE C. OIL PRESSURE INDICATED 80 PSI. SHUTDOWN ENGINE & LANDED. ENGINE OPERATED AT WINDMILLING RPM FOR APPROX 30 MINUTES, OIL QUANTITY APPROX 1 GAL. ALL OTHER INSDR FDEA201102240732Oil Cooler · malfunctionedAFTER TAKEOFF, RECEIVED LEVEL 2 " ENG 1, OIL TEMP HI" ALERT C/W QRH & RETARDED THROTTLE. TEMP PEAKED AT 168 & DROPPED BELOW 163 IN ABOUT 6-7 MIN. IT STABILIZED APPROX 10 MINS BEFORE DECREASING TO 110 DEGREES MATCHING NR 2 & NR 3 OIL TEMPS. DURING LEVEL FLT SDR FDEA201012164697Transducer · inoperative1 HOUR AFTER TAKEOFF, AT FL300 RECEIVED HYD PRESS 3 LOW LEVEL 1 ALERT, NR 3 HYD PRESSURE INDICATED 0 & NR 3 HYD QTY INDICATED 10.9 GALS, TURNED ON BOTH RMPS, NO HELP NR 3 PRESSURE STILL 0. DURING LANDING PHASE-RECEIVED HYD 3 PRESS LOW & HYD NR 3 FAIL LEVEL 2SDR FDEA201011104290Lamp · inoperativeSERVICE CHECK FOUND LT ENTRY DOOR SLIDE PRESSURE INDICATOR LIGHT INOP. CK FOUND LT ENTRY DOOR SLIDE PRESSURE INDICATOR LIGHT ASSY INOP. R&R LAMP, RELEASED FOR SERVICE IAW MEL: 25-61-02SDR FDEA200911204079Beam · crackedMAIN DECK LT OVERWING PASSENGER DOOR PLUG NR 5 BEAM FWD STOP FITTING FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 51-31-01 REV 42 AND EA 1-5210-132274. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 108.SDR FDEA200911184018Frame · dentedMAIN DECK UPPER SIDEWALL FRAME AT LT STA 1621, 13L FOUND DENTED. MAIN DECK DENTED FRAME AT LT STA 1621 13L REPAIRED IAW SRM 53-00-07 FIG. 201. REPAIR 2 REV 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9.500 CYCLES TO BE CASDR FDEA200911184017Frame · dentedMAIN DECK UPPER SIDEWALL FRAME AT LT STA 1741, 13L FOUND DENTED. MAIN DECK DENTED FRAME AT LT STA 1741 13L REPAIRED IAW SRM 53-00-07 FIG 201, REPAIR 2 REV 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9.500 CYCLES TO BE CARRSDR FDEA200911184016Frame · dentedMAIN DECK UPPER SIDEWALL FRAME AT LT STA 1761, 13L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 2 REV 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9.500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG 201 REPAIR 2, SDR FDEA200911184015Frame · dentedMAIN DECK UPPER SIDEWALL AT LT STA 1661, 15L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIG. 201, REPAIR 2 REV 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07 FIG. 201 REPAIR 2, REVSDR FDEA200911184014Skin · damagedRT WING - NR 5 L/E SLAT UPPER SURFACE INBD EDGE FOUND EDGE CUT. REPAIR CARRIED OUT IAW EA 1-5740-132271. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911173994Skin · crackedCRACKS FOUND ON FASTENER HOLES DURING HFEC OPEN HOLE INSP ON LT WING LWR SKIN PANEL OUTER WING ACCESS DOOR. REPAIR CARRIED OUT EA 1-5710-132277. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911173993Skin · crackedCRACK FOUND ON THE FASTENER HOLES DURING HFEC OPEN HOLE INSP ON RT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR. REPAIR CARRIED OUT IAW EA 1-5710-132278. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.
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