N805FD, cancelled Mar 2, 2024
Service difficulty reports · 70
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 = 'N805FD' AND deregistration_id = 'N805FD-2024-03-02' 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 = 'N805FD' AND deregistration_id = 'N805FD-2024-03-02' 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 FDEA201609133211Slat · lack of lubeDURING APPROACH, SLATS WOULD NOT EXTEND, COMPLIED WITH PHASE 1, ECAM & QRH - SLATS CONFIRMED STUCK. DID NO SLAT/FULL FLAP LANDING IAW QRH. CREW CALLED IN FIRETRUCKS FOR SAFETY PRECAUTION. ACCOMPLISHED SFCC 1 AND 2 BITE TEST IAW AMM TSM 27-80-00 FOUND SFCCSDR FDEA201606131980Computer · faultyAPPROX 60 NM FROM DESTINATION, GOT FUEL ADV ON ECAM. LT OUTER 6K, LT INNER 11.0, CTR WAS 0, TRIM TANK WAS 0, RT INNER STARTED AT 11, THEN 10, THEN 9, THEN 8, ALL THE WAY TO ZERO. RIGHT WAS 4.0 AND DECREASING. DIVERTED. WITH T/O OF 57, FUEL USED COUNTER WASSDR FDEA201407191860Stringer · corrodedAFT CARGO STRINGER 46R FRAME 63 - 64 STRINGER CORRODED. REPAIRED THE STRINGER PER A310 SRM 53-10-14 PB201 FIG201HSDR FDEA201207262710Engine · failedUPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MODE FAULT AND ATS LEVER KICKED OFF. NOTICED ENG 1 EGT GAUGE INOP AT "0". ENG 1 N1 BEGAN UNCOMSDR FDEA201204051259Fuel Cell · leakingLEFT WING INNER TANK LOWER SURFACE 1 EA BOLT FUEL SEEPING NEAR REAR SPAR RIB 8 POSITION. USED OPTIONAL INSP METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND RESEALANT ON THE NUT IAW SRM 51-49-00. APPLIED NEW SDR FDEA201204051258Fuel Cell · leakingRIGHT OUTER TANK REAR SPAR, FUEL SEEPING AT NR 6 SPOILER BLOCK VALVE SUPPORT FITTING LWR RT FITTING FASTENERS. USED OPTIONAL INSPECTION METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND SEALANT ON THE NUT IAW SRSDR FDEA201203190997Floor Support · corrodedFWD MAIN DECK, COURIER FLOOR AREA, FOUND FLOOR SUPPORT CORRODED LOCATION FROM FR 11 TO 13A AND Y-724. R & R THE FLOOR SUPPORT IAW SRM 51-72-10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201203160965Floor Panel · damagedMAIN DECK FLOOR PANEL 241NK DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201203130909Skin · dentedNOSE SECTION RT LOWER HALF SKIN PLATE EXTERNAL GOT A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR 2 AND FR 3 POSITION.SDR FDEA201109264124Skin · scratchedLEFT WING OTBD FLAP UPPER SURFACE NEAR FLAP TRACK NR 3, FOUND SURFACE WITH 8" SCRATCH MARK UNDER RUBSTRIP. REPLACED THE O/B FLAP PER AMM 27-50-12-04-0SDR FDEA201106122214Thrust Reverser · malfunctionedAT APPRX 70KTS, NR 2 THRUST REVERSER UNLOCK AMBER LIGHT ON. REJECTED T/O, AFTER STOWING THRUST REVERSER, LIGHT OUT. REVERSER APPEARED TO OPERATE NORMAL. RELEASED FOR SERVICE PER MEL. PERFORMED TROUBLESHOOTING AS PER AMM 78-30-00-02. CARRIED OUT RIGGINGSDR FDEA201007082423Priority Valve · failedON START OF T/O ROLL, RECEIVED ECAM FOR BLUE RSVR LO LEVEL, BLUE RSVR INDICATES EMPTY. TURNED OFF BLUE HYD ENG PUMP APPROX, 2 MINUTES AFTER ECAM ALERT. T/S AND FOUND ACTUALLEY BLUE RSVR HYD QTY INDICATED 1.5 G/L AND BLUE HYD MANIFOLD PRIORITY VALVE BROKEN.SDR FDEA201001130093Stringer · misrepairedPREVIOUS STR REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETWEEN FRAMES 72 TO 74 HAS 2 EACH REPAIR ANGLES AND 1 EACH STR REPAIR SECTION. PREVIOUSLY INSTALLED REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETSDR FDEA201001110078Fairing · shearedNR 2 PYLON FAIRING 485AL INBD AFT SECTION MOUNTING RIVETS SHEARED NOT GOING THROUGH REINFORCING STRINGER REMOVED REINFORCING ANGLE. REPAIRED SKIN USING SPLICING METHOD IAW EA 6-5480-137727. REPLACED REINFORCING ANGLE IAW SRM 51-72-10.SDR FDEA200912294540Skin · dentedLT SIDE LWR FUSELAGE SKIN AT FRAME 67 STR 50L DENT MEASURING 12 INCHES X 1 INCH X .188 DEEP. REPAIRED SKIN PN A53974208200 AT FRAME 67 BETWEEN STRINGERS 49L AND 50L USING DOUBLER AND FILLER IAW SRM 53-10-12 FIG. 225 PAGES 357 THROUGH 366.SDR FDEA200912234512Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STRINGER 36 LT BETWEEN FRAMES 20 TO 22 HAS 1 EACH REPAIR SPLICE MEASURING 7.2" LONG AND 1 EACH STRINGER REPAIR SPLICE MEASURING 24.3" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT FWD CARGO ON STRINGER 36 LT BETWSDR FDEA200808263598Computer · failedDURING APPROACH WITH THE LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURSDR FDEA200808263597Computer · malfunctionedDURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAINSDR FDEA200808263602Limiter · failedDURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR SDR 08FDEA03602Limiter · malfunctionedDURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR SDR 08FDEA03598Slat System · failedDURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGASDR 08FDEA03597Slat System · malfunctionedDURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGASDR FDEA200807122844Jackscrew · leakingSLATS STUCK AT 0 DEG, C/W QRH. EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4.SDR 08FDEA02844Jackscrew · stuckSLATS STUCK AT O DEG, C/W QRH, EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4.SDR 07FDEA05026Stringer · corrodedFWD PIT BETWEEN FR 39 AND FR 38.2 STGR 53 LT HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-10-14. FAB`D STRINGER DOUBLER IN T7/711755. REMOVED AND REPLACED STRG DOUBLER AND COUPLING IAW 51-40-44.SDR 07FDEA04854Stringer · corrodedFWD CARGO BETWEEN FR 38.1 AND FR 38.2 STGR 48 RT HAS CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. CUT OUT DAMAGE AREA STR 48 RT FR 37-38.1 IAW SRM 53-10-14. REMOVED SHEAR TIE TR 37 STR 47 RT. FAB STRINGER DOUBLER IAW MAE TRAVESDR 07FDEA04488Skin · corrodedFOUND CORROSION AT WEDGE C 70, P56-57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04485Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 65, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04483Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P48, C 68-69 AND C 70-71. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04451Skin · dentedFOUND DENT AT SLAT NR 2 LT OUT OF LIMIT. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11 FIG 202.SDR 07FDEA04446Lug · corrodedFOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RAS/BAE/1000347/2005 ISS A.SDR 07FDEA04467Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 56, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04466Stringer · corrodedFOUND CORROSION AT STRINGER P 48 LT, C 69-70 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04465Fitting · corrodedFOUND CORROSION AT CORNER FITTING P 44 LT, C64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04464Frame · damagedFOUND ENLARGED HOLES AT C 26/32 BETWEEN P 13-22 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04463Fitting · corrodedFOUND CORROSION AT CORNER FITTING C 33 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04462Channel · dentedLT AFT CREW DOOR LOWER CHANNEL HAS A NOTCH OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04461Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 56 LT, C 80 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04460Skin · misrepairedFOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 57-2055.SDR 07FDEA04459Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 72, P 48 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04458Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 72, 45 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04457Flange · corrodedFOUND FLANGE C61-62, AD CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04456Fitting · corrodedFOUND CORROSION AT RUN OUT FITTING P44 LT/RT, C17 REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440.SDR 07FDEA04455Fitting · corrodedFOUND FITTING AT C13-13A, P26 LT CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04454Seat Track · corrodedFOUND SEAT TRACK C 15A-19, Y-953 CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04453Skin Panel · corrodedFOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING OF TWO DOUBLERS IAW DRAWING R573-10011 AT BEAM 4 AND 6, C 44-2 AND C 44 LT/RT IAW EA 6-5710-81129 AND RAS/AS/0036/2005 ISS A.SDR 07FDEA04452Rib · damagedFOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055.SDR 07FDEA04450Skin · wornFOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.SDR 07FDEA04449Skin · wornFOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.SDR 07FDEA04448Skin · damagedRT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND RELEASED IAW FAA FORM 8130-3 NR 05/1145.
Back to N805FD, cancelled Mar 2, 2024