N816FD, cancelled Feb 6, 2024

Service difficulty reports · 54

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 = 'N816FD' AND deregistration_id = 'N816FD-2024-02-06'
  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 FDEA201312142981Jackscrew · lack of lubeON APPROACH, FLAPS DID NOT EXTEND. FLAPS SYS 1 & SYS 2 FAULT LIGHTS ILLUMINATED UPON MOVING FLAP HANDLE TO ANY EXTENDED POSITION. ALTITUDE 6200 FEET AT KGTF, TEMP -5C. RELIEVED LOAD ON LT FLAPS THEN RESET LT FLAP TO LIMITER. RT LIMITER OK IAW A310-300 AMMDec 14, 2013 · N816FD · Airbus A310304 · Trailing Edge Flap Control SystemSDR FDEA201304100772Door · damagedEXTENDING LANDING GEAR, RECEIVED ECAM WARNING THAT NLG DOOR WAS NOT CLOSED. BOTH PANELS SHOWED DOOR. FOLLOWED QRH LANDED UNEVENTFULLY. AFTER TAXING IN NOSE GEAR DOOR LIGHT EXTINGUISHED. FOUND AFT HINGE FITTING FOR RT AFT NOSE GEAR DOOR DAMAGED. REMOVED RTApr 10, 2013 · N816FD · Airbus A310304 · Landing Gear DoorsSDR FDEA201112155280Fuel Cell · leakingRT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304 PT3 AND EA 6-5710-149029 (FOR REPAIR OF FUEL TANK SEALING). THE REPAIR Dec 15, 2011 · N816FD · Airbus A310304 · Fuel StorageSDR FDEA201112155276Fuel Cell · leakingRT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND EA 6-5710-149029. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 15, 2011 · N816FD · Airbus A310304 · Fuel StorageSDR FDEA201112155274Canister · leakingRT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CANISTER IAW EO 6-5710-7-3304C PT1. RE-INSTALLED FUEL PNL 540BB, 540CB IAW AMM 28-11-22. LEAK CHDec 15, 2011 · N816FD · Airbus A310304 · Fuel StorageSDR FDEA201112025116Skin · dentedRT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 2, 2011 · N816FD · Airbus A310304 · Trailing Edge FlapsSDR FDEA201112025115Door · gougedFOUND CREW DOOR GOUGED. REPAIRED IAW EA 6-52-50-149021 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 2, 2011 · N816FD · Airbus A310304 · Fixed Inner DoorsSDR FDEA201111295067Fitting · crackedLEFT NOSE SECTION/ FR 12A STIFFENER FITTING WAS FOUND 1 EA CRACK ABOUT .7500" IN LENGTH . ON ZONE B,J AREA IAW NTM 51-10-08, PART 1. REMOVED STIFFENER FITTING AND JUNCTION FITTING. INSTALLED STIFFENER FITTING AND JUNCTION FITTING WITH NEW PART REFER TO EO 6Nov 29, 2011 · N816FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR FDEA201111224994Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 162AF HAS EDGE IMPACT DAMAGED. FOUND OUT OF LIMITS. REPLACED THE FLOOR PANEL BY FABRICATION OF A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20 & DWG A53279966. REPAIR MINOR PER GMM 6-2-100.Nov 22, 2011 · N816FD · Airbus A310304 · Fuselage Floor PanelSDR FDEA201110154538Power Supply · no testEMERGENCY LIGHTS WOULD NOT TEST PROPERLY. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM 33-51-14-04-09. OK FOR SERVICE.Oct 15, 2011 · N816FD · Airbus A310304 · Emergency LightingSDR FDEA200907022465Skin · dentedON WALK AROUND FOUND DENT ON LOWER FUSELAGEAFT OF RADOME BETWEEN FRAME O AND FRAME 1 CUT OUT DAMAGED AREA IAW A310 SRM 53-11-12 FIG. 201. INSTALLED PERMANENT REPAIR IAW A310 SRM 53-11-12 FIG. 201. BETWEEN FRAME 0 AND FRAME 1 AT FUSELAGE LOWER CENTERLINEJul 2, 2009 · N816FD · Airbus A310 · Fuselage Main, Plate/SkinSDR FDEA200907022464Skin · damagedLOWER AFT CORNER OF L - 1 DOOR HAS 3/16 INCH ARC CUT OUT DAMAGED AREA AND INSTALLED REPAIR OF OUTER SKIN IN CORNER AREA OF L-1 DOOR LOWER AFT CORNER,FR 17, STRINGER 25 LT IAW A310 SRM 52-11-00,FIG 206,PAGE 239/240Jul 2, 2009 · N816FD · Airbus A310304 · Passenger/Crew DoorsSDR 08FDEA01298Outflow Valve · failedUPON CLIMB-OUT CABIN VERTICAL SPEED EXCEEDED 2000FPM, AT 15000 ALT CAB ALT EXCEEDED 10,000. OUTBOARD EXTRACT VALVE FAULTED, UNABLE TO MANUALLY CONTROL CABIN PRESS. REACTIVATED SYSTEM. FAILED OPS CHECKED AS PER AMM 21-23-00-5, VALVE NEVER MOVED. T/S AS PER WDApr 4, 2008 · N816FD · Airbus A310304 · Pressure Regulator/Outflow ValveSDR 07FDEA02834Unknown · odorAFTER LIFT-OFF ACRID SMOKE ODOR AND EYES HAD BURNING SENSATION. LEVEL OFF AT 10,000 FT. NO CLEARING. OPENED RAM AIR ON DESCENT TO CLEAR AIR. SHUT OFF NR 2 PACK AS IT HAD A HIGH TEMP 55 DEG C. NO OTHER WARNINGS. REPLACED CHECK VALVES 291394,293388,291388Aug 12, 2007 · N816FD · Airbus A310304 · Air Distribution SystemSDR 07FDEA02911B-Nut · leakingAFTER ENGINE START CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE CASPER VENTS. FOUND HYDRAULIC RETURN LINE B NUT LEAKING AT PYLON ON NR 1 ENGINE. SECURED AND OPERATED ENGINE WITH NO LEAKS REMOVED AND REPLACED NR 1 PACK COALESCER BAG PER MM 21-51-16-3. Aug 9, 2007 · N816FD · Airbus A310304 · Hydraulic System, MainSDR 07FDEA01311Frame · crackedDEVIATION TO EO 6-5310-7-5020-SB A310-53-2124- AD 2006-020-06, CRACKS IN FRAME FEET C43, C46 RT REPAIR PERFORMED BY REMOVING THE CRACKS THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS. AApr 4, 2007 · N816FD · Airbus A310304 · Fuselage Main, FrameSDR 07FDEA01310Frame · crackedDEVIATION TO EO 6-5310-7-5020, SB A310-53-2124, AD 2006-02-06, CRACKS IN FRAME FEET , C45, C46 LT REPAIR PERFORMED BY CRACK REMOVING THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS A.Apr 4, 2007 · N816FD · Airbus A310304 · Fuselage Main, FrameSDR 07FDEA01253Rib · crackedFOUND OLD CRACK REPAIR ON INBOARD FLAP RT, RIB 21 (POCKET REPAIR). REPAIR WAS PERFORMED BY REPLACEMENT OF RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-106443.Apr 3, 2007 · N816FD · Airbus A310304 · Trailing Edge FlapsSDR 07FDEA01159Fairing · crackedCRACKED SHIM PLATE AT INNER SIDE AFT AREA OF LT NR 3 FLAP TRACK FIXED FAIRING. REPAIR PERFORMED BY WET LAY-UP PER SRM 57-20-35 AND INSERT INSTALLATION, APPROVED BY EA 6-5720-106421 AND RAS/FOK/016/2007 ISS. AMar 28, 2007 · N816FD · Airbus A310304 · Wing Miscellaneous StructureSDR 07FDEA01158Attach Fitting · corrodedFOUND CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.Mar 28, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01157Attach Fitting · corrodedCORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.Mar 28, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01129Fairing · damagedREPAIR DAMAGE TO FAIRING 577EL REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW EA 6-5317-106416 AND RAS/DAHAM/4021689/2007 ISS.AMar 26, 2007 · N816FD · Airbus A310304 · Aerodynamic FairingsSDR 07FDEA01128Skin · damagedOLD EXTERNAL DOUBLER REPAIR AT C38/38A, P44 RT REPAIR WAS PERFORMED IAW LHT SDR 0226/007536, APPROVED BY EA 6-5314-106414 AND RAS/DABRE/7005488/2005 ISS.AMar 26, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA01111Frame · crackedMILLED FRAME CRACKED, C22, P26, RHS REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW EA 6-5313-106374 AND RAS/DABRE/7007381/2007 ISS. A.Mar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, FrameSDR 07FDEA01110Bulkhead · gougedSOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049380/2007 ISS. AMar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, BulkheadSDR 07FDEA01103Skin Panel · gougedTWO MISDRILLED HOLES THROUGH THE SKIN PANEL, INTERNAL DOUBLER, C17 FLANGE AND CONNECTING FITTINGS AT P44 LT. REPAIR PERFORMED BY REPLACING CONNECTING FITTINGS P44 BY NEW ONES; INSTALLING STEEL REPAIR BUSHES IN SKIN PANEL, INTERNAL DOUBLER C17 FLANGE AND C17 FMar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA01053Frame · crackedDEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6-5710-106423 AND RAS/049817/013/2007 ISSUE "A".Mar 21, 2007 · N816FD · Airbus A310304 · Wing SparSDR 07FDEA01052Mount · chafedOLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANGLE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441.Mar 21, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01050Fitting · damagedMISDRILLED HOLES IN C17 AT P44 LT. REPAIR WAS PERFORMED BY BUSHING REPAIR AND NEW FITTING INSTALLATION (P/N A536-10607-206-93, A536- 10607-207-93) IAW EA 6-5312-106418 AND RAS/AS/006/2007 ISSUE "A".Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Attach FittingsSDR 07FDEA01036Skin · scratchedOLD SCRATCH REPAIR ON EXTERNAL SKIN BETWEEN C75/76, P27. REPAIR VERIFICATION, PERFORMED IAW SRM 53-18-12/FIG 102 EA FOR TRACKING: 6-5318-106413.Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00990Skin · chafedCHAFE MARKS ON C38.1, P14-15 LT SIDE. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-106417 AND RAS/DATLS/0003560/2007 ISS. BMar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00989Skin · damagedDOUBLE HOLE ON FUSELAGE SKIN AT C67, P35 RHS REPAIR WAS PERFORMED BY BUSH REPAIR IAW SRM 51-40-51, APPROVED BY EA 6-53176-106410 AND RAS/DAHAM/4021719/2007 ISS. AMar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/SkinSDR 07FDEA00987Vane · damagedCHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED.Mar 19, 2007 · N816FD · Airbus A310304 · Trailing Edge FlapsSDR 07FDEA00955Attach Fitting · damagedV/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.)Mar 16, 2007 · N816FD · Airbus A310304 · Vertical StabilizerSDR 07FDEA00954Floor Support · corrodedCORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT, CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00. PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR 07FDEA00953Floor Support · corrodedFOUND CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT (CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00). PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR 07FDEA00952Crossbeam · corrodedFOUND CORRODED CROSSBEAM AT C67, Y-1070-1115. PART REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, StructureSDR 07FDEA00951Beam · damagedTWO LONGITUDINAL BEAMS BETWEEN C64-65, -Y 525 AND Y 805 WITH WRONG EXISTING HOLES. PARTS REPLACED IAW SRM 51-72-10.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, StructureSDR 07FDEA00948Stiffener · damagedRT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER.Mar 16, 2007 · N816FD · Airbus A310304 · Wing Miscellaneous StructureSDR 07FDEA00947Skin · crackedRT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R572-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED).Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Plate/SkinSDR 07FDEA00946Rib · chafedKRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT.Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Rib/BulkheadSDR 07FDEA00945Web · chafedCHAFING MARK AT BACK WALL OF KRUEGER FLAP CHAMBER. REPAIR WAS PERFORMED BY BLEND OUT AND REPROTECT.Mar 16, 2007 · N816FD · Airbus A310304 · Leading Edge DevicesSDR 07FDEA00944Attach Fitting · chafedPYLON NR 2, CHAFING MARKS ON INBOARD SIDE OF PYLON-TO-ENGINE ATTACH FITTING. REPAIR WAS PERFORMED BY BLEND OUT AND RESTORE PROTECTION.Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Nacelle/Pylon Attach FittingsSDR 07FDEA00938Longeron · bentAPU ACCESS DOOR LT/RT LOWER LONGERON, OLD BENT REPAIR. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLATION OF NEW LONGERON SECTION.Mar 16, 2007 · N816FD · Airbus A310304 · APU Cowling/ContainmentSDR 07FDEA00936Floorbeam · corrodedAFT CARGO COMP FLOORBEAM AT C63 LT, Y 445 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207 BY LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Floor BeamSDR 07FDEA00933Stringer · chafedOLD CHAFING MARKS BETWEEN C44-45, P45 LT. REPAIR PERFORMED BY BLEND OUT IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Longeron/StringerSDR 07FDEA00932Skin · dentedOLD DENT REPAIR ON BULK CARGO DOOR OUTER SKIN BETWEEN BEAM 1-2 AND BEAM 4-5. REPAIR WAS PERFORMED BY INSTALLING EXTERNAL DOUBLER BETWEEN BEAM 4-5 AND BLEND OUT BETWEEN BEAM 1-2 IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage DoorsSDR 07FDEA00931Skin · chafedTWO OLD NICK/CHAFING MARKS AT THE INTERNAL SKIN OF FWD CARGO DOOR C20A-25A, LONGERON 4-5. REPAIR WAS PERFORMED BY INSTALLING A DOUBLER IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage DoorsSDR 07FDEA00930Shaft · chafedOLD CHAFING MARK ON PAX DOOR NR 1 RT AT LOCKING CONTROL SHAFT. REPAIR WAS PERFORMED BY BLEND OUT IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Passenger/Crew DoorsSDR 07FDEA00929Skin · delaminatedOLD REPAIR ON LT MLG DOOR, DELAMINATED SKIN. REPAIR WAS PERFORMED BY FILL OUT THE DELAMINATED AREA IAW LHT SDR.Mar 16, 2007 · N816FD · Airbus A310304 · Landing Gear Doors
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