N308FE
Service difficulty reports · 98
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 = 'N308FE' 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 = 'N308FE' 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 FDEA201504261299Power Supply · failedWHILE PERFORMING PRE-DEPARTURE CHECK RECEIVED, EMER BAT 1 LOW ALERT, WHEN PERFORMING EMER LIGHT TEST. R & R EMER LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01-4-1. OPERATIONS CHECKED GOOD IAW MM 33-51-01-5. ACFT OK FOR SERVICE.SDR FDEA201405271199Skin · crackedDURING INSPECTION, THE RT WING FIXED LE FOUND A 1/2 INCH CRACK AT THE NR 2 SLAT TELESCOPING ANTI-ICE DUCT CUT OUT, UPPER OTBD RADIUS. PERFORMED HFEC ON RT WING, AT SUSPECTED CRACK LOCATION TO VERIFY CRACK IAW NTM PT 6. IAW SHEET METAL REQUEST, REMOVED RT WINSDR FDEA201405271200Skin · crackedON WALK AROUND FOUND A CRACK AT LT WING FUELING DOOR INBD SIDE. LT WING LWR LE CRACK VERIFICATION, PERFORMED HFEC OF SUSPECT CRACK AREA, CONFIRMED CRACK. CRACK ENDS AT RIVET HOLE. LT WING REFUEL & DEFUEL PANEL HAS BEEN REMOVED IAW SMP & PLACED IN THE COUSDR FDEA201405070960Engine · overtempPASSING 1200 FT, NR 3 ENGINE EGT WENT TO 969 C, PULLED THROTTLE BACK, TEMP STABILIZED, BUT WITHIN MINUTES STARTED FLUCTUATING INTO THE AMBER TOWARDS RED. PULLED THROTTLE TO IDLE & LT RED WITH THROTTLE AT IDLE. NR 3 ENGINE EGT EXCEEDANCE. ACCOMPLISH A BOROSCSDR FDEA201404290889Skin · crackedDURING WALK AROUND, FOUND ACRACK ON RT WING LE SKIN AT FWD LT CORNER OF FUELING PANEL. PERFORMED HFEC OF SUSPECT AREA, VERIFIED CRACK & IAW NTM PT6 20-30-00. REMOVED CRACK DAMAGE IAW SRM 57-10-00 FIG 68. INSTALLED REPAIR DOUBLER & COMPLIED WITH EA 8-5730SDR FDEA201403010427Door Frame · damagedR4 DOOR AREA UPPER DOOR FRAME HAS A DEEP GOUGES & CRACKED. REPAIRED IAW EA 8-5310-306410 PART 1SDR FDEA201307231637Pitot Tube · obstructedABORTED TAKE OFF DUE TO AIRSPEED DISCREPANCY OF 20 KTS, CAPTAIN`S AIRSPEED WAS 60 KNOTS WHEN F/O CALLED 80 KNOTS FOR AIRSPEED CHECK DURING TAKE OFF ROLL. REJECTED TAKE OFF AT 100 KTS HIGHEST BRAKE TEMP NR 2 AT 460 DEG. FOUND EVIDENCE OF INSECT NESTS IN CAPSDR FDEA201305110973Unknown · unknownDURING PREFLIGHT, DISPLAY UNITS 2,4 AND 5 INTERMITTENTLY WENT BLANK. DOWN POWERED ACFT FOR 10 MINS, POWERED ACFT. PERFORMED RTS ON ALL 3 VIA'S ALL TEST PASSED IAW MM 31-43-01-5. TSI ADDED TO REPLACED NR 1 VIA AND PERFORM ADJUSTMENT TEST ON ALL DU SWITCHINSDR FDEA201304180806Throttle · frozenNR 2 THROTTLE STUCK AT 87 TO 93 PERCENT. SHUTDOWN ENGINE TO LAND. THROTTLE MOVES FREELY IN CHOCKS. R & R NR 2 ENGINE THROTTLE PUSH-PULL CABLE IAW MM 76-11-01-2 (FOUND WATER IN CABLE, SUSPECT FREEZING IN FLIGHT) OPS CHECKED GOOD, OK FOR SERVICE.SDR FDEA201203281159Battery Pack · inoperativeDURING INSPECTION, EMERGENCY LIGHTS IN THE FLIGHT DECK AND COURIER AREA CEILING ARE INOPERATIVE. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01-4 AND 33-51-01-5.SDR FDEA201203251095Panel · missingDURING WALKAROUND, FOUND NR 3 PYLON MISSING PIE SHAPED PANEL AFT OF ENGINE PYLON. REPLACED SUPPORT ANGLE AUB7036-4 USING SRM. FINAL CLOSED.SDR FDEA201203231066Light · shortedDURING PRE-DEPARTURE INSPECTION, WHILE PERFORMING EMERGENCY EXIT POWER LIGHT TEST, ALL CEILING LIGHTS IN FLIGHT DECK AND COURIER AREA INOPERATIVE. TROUBLESHOT SYS AND FOUND POWER BEING DRAWN TO A GROUND FROM POWER SUPPLY NOT PROVIDING ENOUGH VOLTAGE TO LIGSDR FDEA201109093785Wire Harness · failedENG NR3 FIRE INDICATION AT FL 350 INDICATION WENT OUT WHEN THROTTLE PULLED TO IDLE. FOLLOWED CHECKLIST AND SHUTDOWN ENG UNEVENTFUL LANDING. R & R NR 3 ENGINE CORE FIRE DET WIRE HARNESS IAW SMP CHAPTER 20. FDCU OPS CHECKED GOOD IAW MM 26-11-01-5. NR 3 ENG FISDR FDEA201105241958Switch · inoperativeDURING T/O ROLL ENGINES WERE SURGE USING MAX POWER AND AUTO THROTTLES. THROTTLES WERE MOVING BACK AND FORTH ABOUT ONE KNOB. ENGINE 2 EXCEEDANCE AT 110 KNOTS 121.3 N1, 109.6 N2. REJECTED TAKEOFF. PERFORMED VISUAL INSPECTION TO ENGINES AS PER MM 72-00-00-SDR FDEA201104261625Engine · malfunctionedON TAKEOFF ROLL. MAX POWER AT 90KIAS THE ENGINE FAIL LIGHT, ENGINE 2 N1 EXCEEDANCE 120.1 (T/O LIMIT 115.8) REJECTED T/O. PERFORMED FAN (N1) OVERSPEED INSP, FAN ROTOR FREE FOR ROTATION, FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FSDR FDEA201101250345Light · inoperativeACFT EMERGENCY LIGHTS SYS INOP. (PLACED ON MEL)SDR FDEA201004071093Sensor · failedDURING TAKEOFF RETRACTED GEAR RECEIVED A RED UNSAFE INDICATION OF THE LT MAIN GEAR IN BOTH THE PRIMARY AND SECONDARY GEAR POSITION INDICATORS. CYCLED GEAR IAW QRH SAFE DOWN INDICATION, UNSAFE UP. CONTINUED TO DEST AT 250 KNTS. R & R LT MLG POSITION DOWN AND SDR FDEA200903140921Cylinder · failedHEARD THUMP FOLLOWED BY HYD QTY LOW THEN IMMEDIATELY FOLLOWED BY LVL FAIL ALERT JUST PRIOR TO TOUCHDOWN, FOUND LT NWS STEERING ACT HOUSING SHEARED. REPLACED LT NWS STEERING ACT REF AMM 32-52-01-2, OPS CK OK. LEAK CK OK. ALSO INSP NWS STEERING COLLAR AREA ASDR 08FDEA00079Frame · crackedUPPER FUSELAGE ENTRY WAY CRACK ON FITTING SUPPORT (P/N AWE8001-503 ). REPAIRED FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL I.SDR 07FDEA05050Seat Track · crackedAFTER REMOVAL CEILING PANELS WITH J/C "2552C120-2JR" FWD CARGO COMPT BELOW SEAT TRACK FOUND CRACK. REPAIRED SEAT TRACK IAW SRM 53-70-01 FIG 1 VOL I.SDR 07FDEA05049Floor Support · corrodedAFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 VOL I FIG 13.SDR 07FDEA05048Support · corrodedAFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 FIG 13 VOL I.SDR 07FDEA05047Web · crackedLOWER AFT FUSELAGE COMPT CRACK ON WEB, UPPER TORQUE BOX PLANE. REPAIRED WEB IAW SRM 51-40-00 FIG 41 VOL I.SDR 07FDEA04978Skin · dentedLOWER EXT FUS FOUND DENT .50" BY .50" DEPTH .04" ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.SDR 07FDEA04850Spar Cap · crackedDURING SPAR CAP INSP, FOUND 1 1/2 INCH CRACK. ACCOMPLISHED EA 8-5510-111624.SDR 07FDEA04773Skin · crackedDURING INSP OF CONSTANT SECTION UPPER AND LOWER INTERIOR SKIN PANEL FOUND CRACK IN FLYABLE LIMITS.SDR 06FDEA2436Pump · malfunctionedAFTER T/O, NR 2 HYD LT EDP OVERPRESS, APPROX 4KPSI, PER QRH SHUT OFF THAT PUMP NOTICED NR 2 HYD TEMP WAS HI 70 DEG AND RISING FOLLOWED QRH NO HELP, RECEIVED LT TEMP HI ON NR 2 SYS. FOLLOWED QRH, NO HELP. TEMP KEPT RISING ON NR 2 SYS AT 120 DEG, SHUTDOWN NR 2SDR 05FDEA00087Retainer · brokenAT FL350 WHEN WING ANTI-ICE WAS TURNED ON THE NR 1 PNEU PRESSURE WENT TO FULL SCALE AND BOTH WING ANTI-ICE DISAGREE LIGHTS CAME ON. THE CONFIG WAS NR 1 AND NR 2 PNEU SUPPLIES OPEN 1-3 ISO VALVE OPEN, 1-2 CLOSED AND NR 1 PACK ON. NR 3 PNEU SUPPLY WAS DEFERREDSDR 04FDEA02359Warning Light · false indicationRT MAIN GEAR LIGHT ON S/O PANEL SHOWED UNSAFE AFTER GEAR RETRACTION. F/O PANEL SHOWED NORMAL. IAW RED TABS RECYCLED LANDING GEAR. LANDING GEAR EXTENDED NORMAL WITH 4 GREEN ON BOTH PANELS. FOLLOWING RETRACTION RT MAIN RED LIGHT ON S/O PANEL STILL STAYED ILSDR 03FDEA01657Hinge · gougedCOMPLY WITH EA 8-5240-71005. DOORS-SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC7011-1. CLOSING ACTION ON 09/25/03.ON N/R S00013.COMPLIED WITH EA 8-5240-71005. DOORS SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC 7011-1.SDR 03FDEA01655Cap · gougedCOMPLY WITH EA 8-5710-72305. WINGS-MAIN FRAME-GOUGE REPAIR XORS 562.390 (LT) FLAP BULKHEAD LWR CAP. CLOSING ACTION ON 09/26/03. ON N/R S00015. COMPLIED WITH EA 8-5710-72305.WINGS, MAIN FRAME, GOUGE REPAIR STA XORS 562.390.SDR 03FDEA01654Adapter · chafedEXHAUST THRUST REVERSER HAS A CHAFED UPPER ADAPTER. COMPLIED WITH E.A.8-7832-71004.EXHAUST THRUST REVERSER CHAFED UPPER ADAPTER.SDR 03FDEA01656Flap Track · corrodedIB FLAP TRACK AND DRIVE SUPPORT BORE HAS CORROSION. COMPLIED WITH EA 8-5750-72297. RT WING IB FLAP TRACK AND DRIVE SUPPORT BORE CORROSION.SDR 02FDEA00352Windshield · crackedCAPTAINS FRONT WINDSHIELD (OUTER PANE) CRACKED. REMOVED AND REPLACED NR 1 CAPTAINS WINDSHIELD IAW M/M CHAPTER 56-11-00-2. DUE TO BROKEN WIRE ON TERMINAL BLOCK R5-1071. PERFORM ANTI-ICE/DEFOG TEST IAW M/M CHAPTER 30-42-00 PAGE 201. INSTALLED TERMINAL BLOCK SDR 02FDEA00337Valve · failedON CLIMB NR 2 PNEU TEMP HI LIGHT ILLUM'D. SHUTDOWN PNEU SUPPLY SEL. PERFORMED RED TAB PROC. REMOVED AND REPLACED THE NR 3 PACK FLOW VALVE AND THE NR 1 PNEU PRESS REGULATOR VALVE. ALL CHECK OK.SDR 02FDEA00218Flap · malfunctionedWRI 27-50-7942 WITH FLAPS SEL AT 50 DEG LEFT TAPE IND 45 DEG IN FLT ON GRD FLAP TAPE GO TO 50 DEG. REMOVED AND REPLACED O/B FLAP PER MM 27-50-02-4.SDR 01FDEA00662Radar · faultyREPEAT WRITE UP NR 1 RADAR SYS UNSATISFACTORY WITH HEAVY SIDE RETURNS.SDR 01FDEA00661Antenna · malfunctionedREPEAT WRITE UP WX RADAR RETURNS BOTH SYS SHOW BLANK AREA IN A SPOKE PATTERN. REMOVED AND REPLACED ANTENNA PER IAW MD DC10-30 AMM 34-41-01-2.SDR 01FDEA00663Radar · malfunctionedAFT 38 MIN RADAR STARTED SPOKING. REMOVED AND REPLACED RADOME MM 53-51-00-2. REMOVED AND REPLACED WX RADAR ANTENNA PEDESTAL MM 34-41-01-2.SDR 01FDEA00629Radar · malfunctionedRADAR SPOKING BOTH SYSTEMS ALL RANGES ALL GAINS SETTINGS REPEAT WRITEUP.SDR 01FDEA00628Antenna · malfunctionedBOTH CAPT AND F/O RADAR DISPLAY BEGAN TO SPOKE. REMOVED AND REPLACED WEATHER RADAR ANTENNA AND PLATE AS PER MM 34-41-01-2. GROUND CHECK OK.SDR 01FDEA00124Bracket · crackedAFT FUSELAGE COMPARTMENT ZONE 312 STA Y2046.000 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, REPLACED AND FAB PER DRW AJC 7021, SRM 51-31-01 VOL 11.SDR 01FDEA00123Bracket · crackedAFT FUSELAGE COMP ZONE 312 STA Y2069.440 CAN''T TOP ANGLE BRACKET LT CORNER CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW DRW AJC 7029, SRM 51-31-01 VOL 11.SDR 01FDEA00122Bracket · crackedAFT FUSELAGE COMP ZONE 312 STA Y2092.880 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, REPLACED AND FAB PER IAW DRW AJC 7028, SRM 51-31-01 VOL 11.SDR 99FDEA00266Trim Cylinder · malfunctioned99-162 - GEAR HANDLE WOULD NOT RAISE AFT T/O. RED TAB RAN BUT STILL DID NOT WORK. GOOD HYDS ON ALL 3 SYS. NO PINS FND. BLED/RESET TRIM CYLINDER INTERLOCK FUSE PRECAUTIONARY PER DC-10 MM 32-31-06-2. A/C OK FOR RETURN TO SERVICE.SDR 97FDEA00817Actuator · failedWHEN LANDING GEAR WAS DEPLOYED FOR LANDING AT PDX, A LOUD AND HEAVY THUMP WAS HEARD AND FELT AS THE CTR. GEAR IMMEDIATELY CAME DOWN. THE REMAINING GEAR SEEMED TO TAKE MORE TIME THAN USUAL. FOUND RETRACT CYLINDER ROD END STRIPPED OUT AND DAMAGED CENTER LANDISDR 97FDEA00401Engine · flamed outNR 1 ENGINE FAIL AFTER T/O, HIGH EGT 999+, AFTER THROTTLE RETARD FUEL FLOW AND EGT REMAIN EXCESSIVE. WHILE DUMPING FUEL ENGINE FLAMED OUT. RETURNED TO ANC. *S/D* REMOVED AND REPLACED NR 1 ENG AS PER MM 71-00-00-4 RUN UP LC CK NR 1 ENG. ALL CKS OK TDS 9822SDR 97FDEA00221Bracket · crackedLT WING, O/B L/E SLAT DRIVE MECHANISM, OUTER BRACKET ASSY HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. EDDY CURRENT INDICATION.
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