N806FD, cancelled Mar 2, 2024

Service difficulty reports · 65

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 = 'N806FD' AND deregistration_id = 'N806FD-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.

SDR FDEA201401030016Sequence Valve · failedRIGHT MLG WOULD NOT GO DOWN. UTILIZED CRANK HANDLE & RT MLG LOWERED. RT MLG SEQUENCE VLV LOCKED UP & WOULD NOT MOVE. R & R RT MLG SEQUENCE VLV IAW AMM A310-300 32-31-37-04. OPERATIONS CHECK & LEAK CHECKED GOOD.Jan 3, 2014 · N806FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201312253039Sequence Valve · out of rigGEAR LEVER RAISED, RT MAIN GEAR DID NOT RETRACT. GREEN DOWN INDICATION, GEAR DOOR AMBER. PUT GEAR HANDLE BACK DOWN ALL INDICATIONS BACK TO NORMAL FOR DOWN & LOCKED. JACKED ACFT, SWUNG RT MAIN GEAR, GEAR DID NOT RETRACT. FOUND RT MAIN GEAR SEQUENCE VALVEDec 25, 2013 · N806FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201206272374Actuator · faultedPRIOR TO THRUST SET FOR TAKEOFF, RECEIVED NR 1 ENGINE FADEC CHANNEL A FAULT AND FADEC CHANNEL B FAULT. REJECTED TAKEOFF AT 45-50 KNOTS. FOLLOWED QRH PROCEDURES. SHUTDOWN AND RESTARTED NR 1 ENGINE, ATTEMPTED TAKEOFF AND RECEIVED SAME FAULTS AT SLIGHTLY HIJun 27, 2012 · N806FD · Airbus A310324 · Fuel Controlling SystemSDR FDEA201205041733Skin · crackedNR 1 ENGINE PYLON LT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR FDEA201205041732Skin · crackedNR 1 ENGINE PYLON RT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR FDEA201205011687Skin · crackedONE CRACK FOUND, LENGTH 13MM AT RT WING BOTTOM SKIN LANDING PLATE AREA. REPAIRED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 1, 2012 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201204271627Floor Support · corrodedFWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORROSION LOCATION FROM FR 11 TO FR 13A AND Y-724. R & R FLOOR SUPPORT WITH NEW IAW SRM 51-72-10. THE REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Apr 27, 2012 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201204181477Floor Panel · damagedAVIONICS BAY FLOOR PANEL 122PF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-27- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 12 A53210216. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10-Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181476Floor Panel · damagedBULK CARGO BAY FLOOR PANEL 162HF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 17 A53279962. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10-35Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181475Floor Panel · damagedBULK CARGO BAY FLOOR PANEL 161JF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35- 04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 17 A53279960. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL COApr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181474Floor Panel · damagedAFT CARGO COMPARTMENT FOUND FLOOR PANEL 151AF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 10 A25772831. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181473Floor Panel · damagedFWD CARGO BAY FLOOR PANEL 132RF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL, FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG A53272792. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-29-Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201105171851Transmitter · leakingLOST YELLOW SYS HYD ENROUTE. COMPLIED WITH ECAM & QRH. HYD FLUID LEAKING FROM YELLOW HYD SYS PRESSURE TRANSMITTER 16WV HSG CAP & CGO DOOR HYD SELECTOR VALVE 10MJ THE CONTROL SHAFT. R & I 16WV & 10MJ ASSY, REPLENISH YELLOW HYD RESERVOIR & LEAK CHECKED OK, May 17, 2011 · N806FD · Airbus A310324 · Hydraulic Indicating SystemSDR FDEA201007062366Skin · misrepairedAN EXISTING FUSELAGE SKIN REPAIR IS AT FR52-53, BELOW STRINGER 18L. THERE ARE 5 ROWS OF 11 RIVETS ATTACHING THE SKIN (A53870003220) TO THE PLATE (A53870004218). THERE IS NO CUTOUT OR DOUBLER. IAW EA 6-5330-141519, REMOVED RIVETS IAW SRM 51-40-21 AND ROTO-TESJul 6, 2010 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 08FDEA00830Seat Track · damagedMAIN DECK CARGO FLOOR SEAT TRACK NR 1 RT SIDE, FR 61 HAS DAMAGE ON LOWER SURFACE, .545 IN ROUND BY .045 IN DEEP. REMOVED DAMAGED SEAT TRACK SECTION FROM FR 60.5 TO FR 61.5 AND REPAIRED IAW A310 SRM 53-10-16,FIG 208Mar 10, 2008 · N806FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04991Windshield · crackedA/C HAS DIVERTED INTO CUN DUE F/O WINDSHIELD HAS SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD A310-300 M/M 56-11-11-4, OPN CHECK IS GOOD. OK FOR SVC. REPLACED WINDSHIELD TEMP REGULATOR AS A PRECAUTION AMM 30-42-11-4 REPLACED WINDOW HEAT PROTECTION CONDec 4, 2007 · N806FD · Airbus A310324 · Flight Compartment WindowsSDR 07FDEA04407Skin Panel · damagedFOUND DURING P TO F CONVERSION A CUT (10MM) AT SKIN PANEL C 35, P 35 LT REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A FLUSH REPAIR WITH NEW STRAP AND COUPLING IAW EA 6-5314-82877 AND RAS/DABRE/7005190/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04406Fitting · chafedFOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Attach FittingsSDR 07FDEA04405Skin Panel · dentedFOUND NICK ON SKIN PANEL NR 3 C 18-19, P 33 RT REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5313-82859 AND RAS/DABRE/7005143/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04404Skin · delaminatedFOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A.Oct 1, 2007 · N806FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04403Fitting · damagedFOUND MISDRILLED HOLES IN CORNER FITTING C59, P 44 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04402Doubler · corrodedFOUND CORROSION AT DOUBLER C71-72, P 47-48 LT REPAIR PERFORMED BYREWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-82856 AND RAS/DATLS/0002522/2005 ISS B.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04401Stringer · corrodedFOUND CORROSION AT STRINGER P52 LT, C70-71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04400Fitting · crackedFITTING AT P 48, C78 LT CRACKED (ABOUT 8MM). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04399Fitting · corrodedFOUND CORROSION AT FITTING C 63, P44-46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04398Spar · damagedSHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH IAW EA 6-5720-82852 AND RAS /BAE/1000689/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Wing SparSDR 07FDEA04397Floorbeam · damagedFOUND OLD MISDRILLED HOLE AT CROSSBEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04396Stringer · damagedFOUND MISDRILLED HOLES AT STRINGER 41 LT, C33-34 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04395Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04394Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04393Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04392Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04391Stringer · corrodedFOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04390Stringer · corrodedFOUND CORRODED STRINGER SEGMENT P 57 AT C 72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04389Floorbeam · corrodedFOUND CROSSBEAM C 63 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04388Flange · corrodedFOUND CORRODED FLANGE AT C61-62, P 56 RT-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04387Stringer · corrodedFOUND CORRODED STRINGER P 21 LT, BETWEEN 55/58-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04386Panel · crackedFOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 07FDEA04370Plate · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR. 33 LT REPLACEMENT OF WEB PLATE IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04369Plate · damagedDAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR 39 LT AND RT. REPLACEMENT OF WEB PLATES LT AND RT IAW SRM 51-72-10Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04368Fitting · corrodedCORROSION ON UPPER RUN OUT FITTING BETWEEN FRAME 16A-17, STRG 44 RT, AFTER REWORK NO REMAINING THICKNESS WAS EXISTED. REPLACEMENT OF UPPER RUN OUT FITTING IAW. REPAIR DRW R536-10440 ISSUE C.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04367Skin · chafedFOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB 27 OTHER ASNA0081A FASTENERS ARE INSTALLED ACC TO DRW A578-44242/SHEET 16, IAW AI-STATEMENT 942-03Sep 28, 2007 · N806FD · Airbus A310324 · Leading Edge DevicesSDR 07FDEA04365Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NEW SKIN INSERT IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04364Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04363Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04362Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 1 AND SLAT TRACK 2, LEADING EDGE SKIN, RT WING. NOSE SKIN REPAIR RENEWED, NEW REPAIR SKIN IAW SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04360Skin · chafedFOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41-12/FIG 203, 204.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04359Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04358Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous StructureSDR 07FDEA04357Plate · crackedFOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10.Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous Structure
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