N807FD, cancelled Mar 2, 2024

Service difficulty reports · 79

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 = 'N807FD' AND deregistration_id = 'N807FD-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 FDEA2019060311203Sequence Valve · misaligned6685 ON GEAR EXTENSION RECEIVED UNSAFE INDICATION FOR RT MLG ON SYS 1 SYS 2. COMPLIED WITH QRH PROCEDURES AND LG GRAVITY EXTENSION CHECKLIST. GEAR DOORS REMAINED OPEN, UNEVENTFULL LANDING KLRD. (ON LOW APPROACH, TOWER CONFIRMED RT MLG HUNG UP). TROUBMay 31, 2019 · N807FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA2018042601120Power Supply · failedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD.Apr 25, 2018 · N807FD · Airbus A310324 · Emergency LightingSDR FDEA201705031343Jackscrew · lack of lubeWHEN SELECTING FLAPS TO 15, NOTICE BINDING LEAVING THE SLATS/FLAPS 15/0 GATE AT FLAPS 15 RECEIVED FLAP FAULT SYS 1 AND 2. CYCLED THE FLAP HANDLE, NO CHANGE. QRH PROCDURES COMPLETED. LANDED FLAPS 0. REMOVED AND REPLACED THE FLAP/SLAT HANDLE COMMAND SENSMay 3, 2017 · N807FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201612134398Floor Support · corrodedMAIN DECK FRAMES 12A - 14, Y953 FLOOR SUPPORT FOUND CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Dec 13, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612134397Skin · dentedFUSELAGE SKIN FOUND A DENTED BETWEEN FRAMES 65 - 66, STRINGER 36 - 37R. REPAIRED IAW SRM 53-10-12- 201 PARA 6 FIG225 SHEET 2 . MAJOR REPAIR IAW GMM 6-2-100.Dec 13, 2016 · N807FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201612094367Angle · crackedFRAME 47 RT INTERNAL ANGLE\ FOUND CRACKED. REPAIRED THE ANGLE IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612094366Angle · crackedANGLE AT FRAME 47 LT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612094369Angle · crackedTEE ANGLE AT STIFFENER 8 RT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100.Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612094368Angle · crackedTEE ANGLE AT STIFFENER 8 LT FOUND CRACK. REPAIRED THE TEE ANGLE IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612074345Attach Fitting · crackedAFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK BY HFEC INSPECTION. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.Dec 7, 2016 · N807FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201612074344Floor Support · corrodedMAIN DECK FR11-FR14 Y770 FLOOR SUPPORT CORRODED.Dec 7, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201612074343Attach Fitting · crackedFWD CARGO DOOR ACTUATOR ATTACH FITTING WITH CRACK SIGNAL. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.Dec 7, 2016 · N807FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201612074342Skin · crackedLEFT WING BOTTOM SKIN FOUND CRACKED AT 581AB CUTOUT. REPAIRED IAW EA 6-5730-T0330205 P1 AND DWG R57249152. MAJOR REPAIR IAW GMM 6-2-100.Dec 7, 2016 · N807FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201605021440Windshield · crackedDURING CRUISE FLIGHT AT FL 360, BEGAN TO SEE AN ORANGE GLOW IN LOWER LT CORNER OF CAPTAINS FWD WIND SCREEN. TURNED OUT TO BE WINDSHIELD HEAT ARCING, SO TURNED OFF CAPTAINS WINDSHIELD HEAT. ABOUT THE SAME TIME, CAPTAINS FWD, OUTER WINDSHIELD SHATTERED. REMOVMay 2, 2016 · N807FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201601240289Windshield · crackedCRACK ON CAPTAINS' OUTER FRONT WINDSHIELD. WINDOW HEAT WAS ON, BUT TURNED OFF ONCE CRACK DEVELOPED. R & R CAPTAINS WINDSHIELD. R & R LT WINDOW TEMP CONTROLLER -19DG. R & R LT WINDOW HEATING PROTECTION UNIT -87DG.Jan 24, 2016 · N807FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201410123118Skin · corrodedLEFT WING UPPER SURFACE SKIN FOUND CORROSION AT THE FRONT OF NR 2 SPOILER. REPAIRED LT WING UPPER SURFACE SKIN IAW EA 6-5730-T0311884 P1. TITLE WING PLATES & SKINS LHS WING TOP SKIN PANEL 2 TE OVERHANG CORROSION REPAIR BETWEEN RIBS 5 - 7. MAJOR REPAIR IAW GOct 12, 2014 · N807FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201410113111Tee Fitting · crackedCENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312253 TITLE WINGS BASIC WING STRUCTURE SB A310-57-2047 FRAME 47 HOLES CRACKED. MAJOR REPAIR IAW GMM 6-2-100.Oct 11, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201410062974Bracket · crackedLEFT AILERON OTBD HINGE PANEL BRACKET CRACKED REPAIRED LT AILERON OTBD HINGE PANEL BRACKET IAW EA 6-5750-T0312135. WINGS FLIGHT SURFACES FRONT SPAR LOWER DOUBLER BROKEN AT LT AILERON LOWER SURFACE LE MAJOR REPAIR IAW GMM 6-2-100.Oct 6, 2014 · N807FD · Airbus A310324 · AileronsSDR FDEA201410032930Fitting · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201410032929Angle · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201410032928Angle · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Wing Main, Frame StructureSDR FDEA201410032927Angle · crackedREAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 1 FASTENER HOLE WITH A CRACK SIGNAL. REPAIREDSPAR ANGLE & TEE FITTING IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201409302860Floorbeam · corrodedFORWARD CARGO COMPARTMENT FLOORBEAM TEE CORRODED AT FRAME 37, Y140 - Y805. REPAIRED THE FLOORBEAM IAW EA 6-5310-T0311889. MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201409272822Floorbeam · delaminatedAFT CARGO BAY FLOORBEAM TEE FOUND DELAMINATION AT FRAME 60 Y-805 - Y-1470. CUT THE DELAMINATED BEAM IAW SRM 53-10-15 FIG 207 CHECKED THE CRACKS TO CUTOUT PER NTM 51-10-08 MADE THE REPAIR PARTS IAW SRM 53-10-15 FIG 207 WET INSTALLED THE REPAIR IAW SRM 51-4Sep 27, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201409242751Fitting · crackedCENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE PER EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100Sep 24, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201404010608Rib · corrodedRT RIB 5 BORE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0307063 P 1 WINGS & BASIC WING STRUCTURE, RT RIB 5 LUG CORROSION.Apr 1, 2014 · N807FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201404010606Rib · corrodedLT RIB 5 HAS CORROSION IN BORE & FACE. COMPLIED WITH EA 6-5710-T0307003 WINGS & BASIC STRUCTURE, LT RIB 5 LUG CORROSION.Apr 1, 2014 · N807FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201402070285Fuel · contaminatedEN ROUTE LT OUTER PUMP 1 & PUMP 2 FAILED IN FLIGHT. BOTH PUMPS SHOWED LOW PRESS. FOLLOWED ECAM TO TURNOFF. THAWED LO FUEL PUMPS & TANK WITH 3 COLD BUSTERS FOR 5 HOURS. PERFORMED LO TANK PUMPS OPERATIONAL TESTED IAW AMM IAW 28-21-00-05, BOTH PUMPS CHECKED NFeb 7, 2014 · N807FD · Airbus A310324 · Engine Fuel DistributionSDR FDEA201311302913Floor Support · crackedMDIS 807 53-00 0008007 30NOV13 BQN CLOSE R FOUND FWD FUSELAGE FLOOR SUPPORT MEMBER BETWEEN C9 & C10, ONE FRAME LT 09 88 WITH SEVERAL CRACKS. A536 11977200 ID WEB IAW SRM 53-11-15 PAGE 4 ITEM 475 PN A53611977200 & ATTACHED FITTING ITEM 185 PN A53610270220. Nov 30, 2013 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201204241547Fitting · crackedPERFORMED NDT IAW E6-5710-7-3324 A PT2 , CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 RT UPPER CORNER FITTING.Apr 24, 2012 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201204241546Fitting · crackedPERFORMED NDT IAW E6-5710-7-3324 A PT1, CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 LT UPPER CORNER FITTING.Apr 24, 2012 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201108273530Power Supply · failedL1 & R1 DOORS ESCAPE SLIDE RELEASE WARNING LIGHTS SYSTEM INOPERATIVE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN). OPS CHECKED GOOD REF MM 52-73-18-04. OK FOR SERVICE.Aug 27, 2011 · N807FD · Airbus A310324 · Door Warning SystemSDR FDEA201104182042Battery · failedON PREDISPATCH CK, FOUND ON COURIER COMPARTMENT EMERGENCY LT TEST INOP. REMOVED AND REPLACED EMG POWER SUPPLY UNIT AND EMERGENCY SUPPLY BATTERY, REF MM 33-51-14-04-09. OPS CK GOOD. OK FOR SERVICE. (CLOSED)Apr 18, 2011 · N807FD · Airbus A310324 · Emergency LightingSDR 2011FA0000222Jackscrew · out of positionDURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMBLED ON THE OPPOSITE POSITION COMPARED TO THE SPEC MENTIONED ON THE CMM 27-44-13. LETTER LT-S9-11-10Feb 18, 2011 · N807FD · Airbus A310324 · Stabilizer Control SystemSDR FDEA200910213626Skin · damagedACCOMPLISH TERMINATING ACTION REPAIR OF RUDDER. NEW REVISION "C" PART 2 OF EA 6-5540-118407 ACCOMPLISHED TERMINATING ACTION REPAIR OF RUDDER IAW EA NR 6-5540-118407 C PT2 AND RAS/DAHAM/4024327/2008 ISSUE A DATED OCT 20, 2009Oct 21, 2009 · N807FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04039Skin · misrepairedOLD EXTERNAL DOUBLER REPAIR ON INBOARD FLAP RT ON LOWER SIDE BETWEEN RIB 10-11, NOT CONFORM TO OLD RECORDS AS PER SRM 57-52-12/FIG 204: EXTERNAL DOUBLER IS ON LOWER SURFACE INSTEAD OF UPPER SURFACE, NO FILLER ON UPPER SURFACE INSTALLED AND NO RIVETS ON TRAILINSep 19, 2007 · N807FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04037Door Frame · damagedDURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPAIR PERFORMED BY CUT OUT OF LOWER BEAM WEB IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE A.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04036Door Frame · damagedDURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPLACEMENT OF STRINGER 26 COUPLING BY NEW ONE IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE ASep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04034Skin Panel · misrepairedFOUND OLD DOUBLER REPAIR BETWEEN FRAME 11-11A, STRG 27-28 LT, NOT CONFORM TO REPAIR REFERENCE AS PER SRM 53-12-12/FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-12-12/FIG 201.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04033Rib · noneOLD REPAIR ON RT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.Sep 19, 2007 · N807FD · Airbus A310324 · Standard Practices/StructuresSDR 07FDEA04032Rib · noneOLD REPAIR ON LT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.Sep 19, 2007 · N807FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04029Stringer · corrodedDURING NON ROUTINE DR0115, FOUND CORROSION ON STRINGER 51 LT, BETWEEN FRAME 54.1-54.2. PARTIAL STRINGER REPLACEMENT WITH SPLICE REPAIR PERFORMED, BETWEEN FRAME 54.1-54.2 IAW SRM 53-10-14/FIG 201 AND 54.2-54.3 (DR0115).Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04026Stringer Splice · corrodedCORROSION ON CONNECTING SEGMENT STRG 51 LT, BETWEEN FRAME 54.2-54.3. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04024Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 63 RT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04022Floor Support · corrodedHEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 AD, BULK CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04021Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM AT FRAME 69 LT, BULK CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04019Frame · damagedOLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED AND AFTER REWORK OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING NEW REPAIR ANGLE AT OLD REPAIR AS PER PRINCIPLE IN SRM 53-10-13.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04015Shear Plate · crackedCRACKED SHEAR PLATE AT STR 26 LT, BETWEEN FRAME 79-80. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04014Stringer · corrodedCORROSION ON STRINGER 42 RT, BETWEEN FRAME 72-73. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04013Stringer · damagedOLD DAMAGE ON STRINGER 30 RT, BETWEEN FRAME 54.2-54.3. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
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