N809FD, cancelled Mar 2, 2024

Service difficulty reports · 115

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 = 'N809FD' AND deregistration_id = 'N809FD-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 FDEA201909112203Gearbox · failedPDIS 809 27-80 2171 11SEP19 SAT OPEN U LOGPAGES:2553291 DURING EXTENSION OF FLAPS AT 40 DEGREES, RECEIVED SLATS FAULT SYS 1 AND 2. CYCLED PER ECAM, FAULT REILLUMINATED. FOLLOWED ECAM AND QRH PROCEDURES. DECLARED EMERGENCY IN SAT. LANDED WITHOUT Sep 11, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201909102197Computer · faultyPDIS 809 27-80 2168 10SEP19 AFW OPEN U DURING ARRIVAL TO KAFW WHILE EXTENDING THE SLATS HAD SLATS 1&2 FAULT. SLATS WERE STUCK AT 5 DEGREE. RETRACTED SLATS AND IMMEDIATELY GOT SLATS 1&2 FAULT. THE SLATS WERE STUCK AT 0 DEGREES. FOLLOWED QRH AND LANSep 10, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201811053107Tee Fitting · crackedCNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 RT SIDE FWD HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR RIB1 INTERNAL ANGLE/TEE FITTING AT FR44 RH SIDE FWD HOLE(#34A). MAJOR REPAIR IAW FEDEX GMM6-2-Nov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201811053106Tee Fitting · crackedCNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 LT SIDE MID HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR RIB1 INTERNAL ANGLE/TEE FITTING AT FR44 LH SIDE MID HOLE(#35A). CATEGORY "B" REPAIR.FIRST INSPENov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201810202960Support Beam · damagedMDCC FWD UTILITY AREA FR14-FR17, -Y1456 LONGITUDINAL SUPPORT BEAM FOUND 1EA HOLE ENLARGED REFER TO SRM 53-12-15 FIG. 207 REPAIRED THE -Y1456 LONGITUDINAL SUPPORT BEAM AT MDCC FWD UTILITY AREA BETWEEN FR14-FR17. THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECT AOct 20, 2018 · N809FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201706011556Indication Sys · intermittentR1 ENTRY DOOR SLIDE ARMED INDICATOR DOES NOT SHOW ARMED ON ECAM. CLEANED CONNECTOR ON 14WN RT DOOR ESCAPE SLIDE ARM SWITCH. CLOSED AND ARMED R1 DOOR SLIDE AND SLIDE ARM INDICATION CHECKS NORMAL ON ECAM IAW ASM 52-73-00. ACFT OK FOR SERVICE.Jun 1, 2017 · N809FD · Airbus A310324 · Door Warning SystemSDR FDEA201704261272Power Supply · inoperativeR1 DOOR SLIDE FAIL TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BATTERY 1 IAW AMM 52-73-18-04, BITE TESTED OK, R1 SLIDE INDICATION CHECKS OK IAW AMM 52-73-00.Apr 26, 2017 · N809FD · Airbus A310324 · Emergency EquipmentSDR FDEA201703040774Line · leakingLOST ALL GREEN SYSTEM HYD FLUID LEAVING FL 320. USED LANDING GEAR GRAVITY EXTENTION PROCEDURE. HYD SYS CIRCUIT BREAKERS HAVE BEEN COLLARED IN E/E BAY. FOUND A PIN HOLE IN LT GREEN HYD RETURN LINE, REMOVED AND REPLACED THE LINE IAWSMP 20-23-11-00, & 20-23-12-Mar 4, 2017 · N809FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201612064330Flap System · malfunctionedFLAPS STUCK AT 0 DURING APPROACH. COMPLIED WITH ECAM & QRH. NO RELIEF IN CYCLE. LANDED SLATS 30 FLAPS 0. TSM 27-50, BOTH SFCC'S INDICATE FLAP JAMB, LEFT FLAP SYSTEM TORQUE LIMITER TRIPPED. SRM 27-50-02 FIG 101 BLOCK 2, ALL SCREW JACK TORQUE LIMITERS INSPDec 6, 2016 · N809FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201603100888Gcu · malfunctionedREJECTED TAKE OFF AT 90 KNOTS, AC BUS 2 OFF, GEN 2 FAULT. PERFORMED BITE CHECK ON GND POWER CONTROL UNIT & FOUND, RT GEN POWER SYS, FAULTED. R & R NR 2 GEN CONTROL UNIT IAW AMM 24-22-12-04. RAN NR 2 ENG IAW JRH WITH NO FAULTS NOTED. ALSO PERFORMED ADJUSTMEMar 10, 2016 · N809FD · Airbus A310324 · AC InverterSDR FDEA201602120510Sequence Valve · faultyRIGHT MLG DID NOT EXTEND DURING NORMAL EXTENSION. GEAR EXTENDED TO DOWN & LOCKED WITH MANUAL EXTENSION. FREE FALL EXTENSION SYS RETURNED TO NORMAL CONDITION IAW AMM 32-33-00-2. INSPECTED MAIN LG DOOR & WW AREA & NO DEFECT FOUND. JACKED UP ACFT IAW AMM 07-1Feb 12, 2016 · N809FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201601130138Skin · delaminatedRIGHT SIDE RUDDER PANEL, FOUND DELAMINATED AT TE RR 48 - RR 49, APPROX 6" X 6". REMOVE THE OUTER SKIN IN THE DAMAGED AREA IAW SRM 55-41-12 PARA 31. PERFORM A TAP TEST AROUND THE DAMAGE AREA TO MAKE SURE NO DELAMINATION IAW NTM 51-10-19, NO DAMAGE. PERFORM Jan 13, 2016 · N809FD · Airbus A310324 · Rudder, Plate/SkinSDR FDEA201601120125Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 60 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR Jan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120124Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 62 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Jan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120123Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 60 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IJan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120122Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 46 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IJan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120121Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 41 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAJan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120120Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 31 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IJan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120119Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 14 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Jan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120118Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 62 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Jan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601120117Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 61 WITH CRACK SIGNAL, RT SIDE. REPAIRED THE CRACKED HOLE IAW EA6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS AJan 12, 2016 · N809FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201601040021Stringer · corrodedAFT CARGO BAY STRINGER 54R, FOUND CORRODED BETWEEN FRAMES 59 - 63. REPAIR THE STRINGER IAW SRM 53-10-14-201 FIG 201 VIEW F & G. MAJOR REPAIR IAW GMM 6-2-100.Jan 4, 2016 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201601040020Stringer · corrodedAFT CARGO BAY, STRINGER 55R, FOUND CORRODED BETWEEN FRAMES 64 - 65. REPAIRED THE STRINGER IAW SRM 53-10-14-201 FIG 201 VIEW F & G. MAJOR REPAIR IAW GMM 6-2-100.Jan 4, 2016 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512304106Beam · corrodedCENTER WING FUEL TANK, BOTTOM SKIN LONGITUDINAL BEAM 4RT OTBD ATTACHED SPLICE FITTING, CORRODED AT FRAME 40. BLENDED OUT & SMOOTHED THE CORRODED AREA IAW SRM 51-74-10. THE DAMAGE WAS OUT OF THE DESIGN THICKNESS TOLERANCE IAW DWG A57112070. REPLACED IAW SRM Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA201512304105Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 44R CORRODED BETWEEN FRAMES 38 - 38.1. REPAIRED THE STRINGER IAW SRM 53-10-14-201 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512304104Stringer Splice · corrodedAFT CARGO BAY STRINGER 54L, STRINGER SPLICE FITTING FOUND CORRODED AT FRAME 65. REPLACED THE SPLICE FITTING IAW SRM 51-40-21. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512264080Stringer · corrodedEXISTING REPAIR ON FUSELAGE STRINGER 55 LT SIDE, BETWEEN FRAME 59 & 61 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & CORROSION WAS FOUND AT THE REPAIR AREA. THE EXISTING SPLICE REPAIR WAS REMOVED & PERFORMED AGAIN IAW SRM 53-10-14 FDec 26, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512013845Door · departedON DEPARTURE, MAIN WW FWD LEFT & CENTER DOORS DEPARTED ACFT.Dec 1, 2015 · N809FD · Airbus A310324 · Service DoorsSDR FDEA201506231983Proximity Sensor · failedLANDING GEAR WOULD NOT RETRACT USING SYSTEM 1. REMOVED AND REPLACED THE LEFT MAIN GEAR TORQUE LINK PROXIMITY DETECTOR IAW AMM 32-00-00-04.Jun 23, 2015 · N809FD · Airbus A310324 · Landing Gear Position and WarningSDR FDEA201505031377Sensor · failedMLG WOULD NOT COME UP DURING DEPARTURE IN SYS 1 & SWITCHED TO SYS 2 & STILL WOULD NOT COME UP. ALSO HAD ADC 1 FAULT, PITCH TRIM NR 1 FAULT, CAPTAIN PROBABLY HEAT, MULTIPLE TIMES. THE JET THOUGHT IT WAS STILL ON THE GND. ALSO CABIN PRESSURE NR 1 FAULT. ALSOMay 3, 2015 · N809FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201405281215Support · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0308476 P1 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION, LT RIB 5.May 28, 2014 · N809FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA201405281214Support · corrodedRIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0308476 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION, RT RIB 5.May 28, 2014 · N809FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA201311122736Skin · corrodedLEFT WING UPPER SKIN INBD JET FUEL GROUND CONNECTOR POINT AROUND AREA HAS SLIGHT CORROSION AT STR 7 AND STR 8 POSITION. REPAIRED IAW EA 6-5720-T0303769. REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 12, 2013 · N809FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201311012663Beam · crackedONE CRACK WAS FOUND ON THE NR 33 FASTENER OF THE INNER LONGERON BEAM FLANGE AT STRINGER 11 BETWEEN FRAMES 73A AND 75A (LT SIDE). CRACK LENGTH IS 1INCH IAW E6-5310-7-3314, PT3. DRILLED OUT AFFECTED FASTENER AND CUT OUT DAMAGE PORTION OF BEAM FLANGE. NDI WAS Nov 1, 2013 · N809FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA201310152506Limiter · trippedDURING FINAL, TRIED LOWERING FLAPS AND RECEIVED A FLAPS 1/2 SYS FAULT. CYCLED HANDLE NO FLAPS EXTENDED. FOUND WHEEL WELL TORQUE LIMITER FOR RT WING FLAP DRIVE TRIPPED. RESET LIMITER. INSPECTED RT WING FLAP TRANSMISSION TORQUE LIMITERS NOT TRIPPED. NR 1 SFOct 15, 2013 · N809FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201106062200Battery · inoperativeCOURIER COMPARTMENT EMERGENCY LIGHT TEST INOP. R & R 29WL1 POWER SUPPLY BATTERY IAW MM 33-55-00-05, NO HELP, REINSTALLED ORIGINAL BATTERY, SUSPECT POWER SUPPLY UNIT 29WL1 BAD. R & R PWR SUPPLY MM 33-55-00-05. NO HELP, SUSPECT BATTERY. PREMATURE REMOVAL/IJun 6, 2011 · N809FD · Airbus A310324 · Emergency LightingSDR FDEA201105292020Skin · delaminatedTHERMOGRAPHY AND ULTRASONIC INSP CARRIED OUT FOUND TRAPPED WATER ON RT RUDDER SKIN AT T/E BELOW NR 37 SCREW LINE AREAS APPROX 600 SQ MM. ACCOMPLISHED EA 6-5540-150322.May 29, 2011 · N809FD · Airbus A310324 · Rudder, Plate/SkinSDR FDEA201105141841Stringer · corrodedFUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR 31 FOUND STRINGER END TOP SURFACE WITH CORROSION FUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR 31 STRINGER END CORRODED PART REMOVED AND REPALCED PER A310-300 SRM 51-40-21 AND SRMay 14, 2011 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201105141840Stringer · corrodedFUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR28 FOUND STRINGER END TOP SURFACE WITH CORROSION FUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGH HAND STGR28 CORRODED STRINGER END REMOVED AND REPLACED GER SRM 51-40-21 AND 51-72-10 REV 79. May 14, 2011 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201010194103Warning Message · false indicationON TAKEOFF ROLL APPROX 80 KTS GOT ECAM WARNING FOR PITCH FEEL SYS 1 AND 2 AND RUDDER TRAVEL SYS 1 AND 2 FAULTS. ALL 4 LIGHTS WERE ILLUMINATED ON OVHD PANEL. ABORTED TAKEOFF, COMPLETED APPROPRIATE CHECKLISTS AND RETURNED TO BLOCKS. ACCOMPLISHED AFS/LAND TEOct 19, 2010 · N809FD · Airbus A310324 · Central WarningSDR FDEA201009303820Pickup · malfunctionedON FINAL APPROACH, WHEN FLAPS WERE SELECTED TO 40 DEG RECEIVED ECAM. FLAPS STUCK. ALSO RECEIVED SYS 1 AND 2 FAULT LIGHT ON OVERHEAD PANEL. FLAPS STUCK BETWEEN 20 DEG -40 DEG. COMPLIED WITH QRH AND ECAM. REPLACED LT APPU 29CV PER AMM 27-56-11-04. PERFORMED OSep 30, 2010 · N809FD · Airbus A310324 · Trailing Flap Position Indicating SystemSDR FDEA201009143386Jackscrew · damagedON FINAL SLATS/FLAPS STUCK 20/17: RECYCLED AND SLAT/FLAP STUCK LIGHT EXTINGUISHED. SELECTED SLAT/FLAP 20/20 TO LAND AND LIGHT REILLUMINATED, THE SECOND TIME. RAN QRH AND LANDED AT SLAT/FLAPS 20/17. ALL HYD'S WERE GOOD. REPLACED NR 3 FLAP JACKSCREW IAW AMMSep 14, 2010 · N809FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR 08FDEA04951Frame · corrodedEMPENNAGE FRAME 84 AT STRINGER 13 L, THE FRAME LOWER CHORD IS CORRODED AT AND UNDER THE CROSSBEAM. REMOVED CORROSION FROM THE FRAME FLANGE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, FIG 105 AND TABLE 102. REMOVED THE FLANGE IAW SRM 51-40-Nov 21, 2008 · N809FD · Airbus A310324 · Fuselage Main, FrameSDR 08FDEA04898Floor Panel · crackedFLOOR PANEL 232 LG IS CRACKED. FABBED NEW FLOOR PANEL 231 LG USING THE OLD PANEL AS A TEMPLATE. POTED & CURED INSERTS; POTTED; CURED & SANDED THE EDGES. APPLIED NON-SKID TAPE & PART MARKED PANEL IAW FEDEX DWG SRX 25-005; REV "G".Nov 17, 2008 · N809FD · Airbus A310324 · Fuselage Floor PanelSDR 08FDEA04897Floor Panel · crackedFLOOR PANEL 232 TG IS CRACKED. FABBED NEW FLOOR PANEL 232 TG USING THE OLD PANEL AS A TEMPLATE. POTED & CURED INSERTS; POTTED; CURED & SANDED THE EDGES. APPLIED NON-SKID TAPE & PART MARKED PANEL IAW FEDEX DWG SRX 25-005; REV "G".Nov 17, 2008 · N809FD · Airbus A310324 · Fuselage Floor PanelSDR 08FDEA04871Floor Panel · delaminatedFWD CARGO PIT FLOOR PANEL NR 131QF IS DAMAGED FABRICATED NEW PANEL FWD CARGO PIT FLOOR PNL 131QF PER DWG SRZ 25-005 REV G AND AMM 20-31-00-0 PG 58.Nov 13, 2008 · N809FD · Airbus A310324 · Fuselage Floor PanelSDR 08FDEA04877Fitting · crackedBULK CARGO DOOR FITTING UNDERNEATH SPRING MECHANISM IS CRACKED. REMOVED CRACKED FITTING IAW A310-300 SRM 51-72-10. LOCATED; DRILL & INSTALLED NEW FITTING P/N A5237807900000 IAW A310-300 SRM 51-72-10.Nov 12, 2008 · N809FD · Airbus A310324 · Cargo/Baggage DoorsSDR 08FDEA04853Floor Panel · damagedBULK CARGO PIT FLOOR PANEL NR 161 GF IS DAMAGED. FABRICATED NEW PANEL IAW DWG. SRZ 25-005. FABBED TOP SHEET IAW SRZ DWG. 25-005. ATTACHED TOP SHEET IAW DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000.Nov 11, 2008 · N809FD · Airbus A310324 · Fuselage Floor PanelSDR 08FDEA04834Failsafe · corrodedLEFT AFT PASSENGER DOOR EXTERNAL SKIN IN THE SCUFF PLATE AREA AND FAIL/SAFE RING HAS SEVERAL AREAS OF CORROSION. REMOVED LIGHT SURFACE CORROSION AS REQUIRED FROM SCUFF PLATE AREA & FAILSAFE RING IAW SRM 51-74-10. ALODINE AND PRIME ACCOMPLISHED ON W/C 41X5067ANov 10, 2008 · N809FD · Airbus A310324 · Passenger/Crew DoorsSDR 08FDEA04833Failsafe · corrodedRIGHT AFT PAX DOOR FAIL/SAFE RING LOWER SECTION HAS CORROSION ON THE SKIN AROUND THE FASTENER HEADS. REMOVED LIGHT SURFACE CORROSION AS REQUIRED ON R/H AFT ENTRY DOOR FRAME, FAILSAFE RING IAW SRM 53-18-12 FIG. 102 & 5140-47. ALODINE & PRIME APPLICATION REFENov 10, 2008 · N809FD · Airbus A310324 · Passenger/Crew Doors
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