Airbus A310-304

Service difficulty reports · 238

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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 aircraft_model_key = 'A310304'
  ORDER BY difficulty_date DESC"

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SDR CA110420006Cover · missing(CAN) UPON ARRIVAL AT DESTINATION AIRPORT IT WAS DISCOVERED THAT THE FWD CARGO DOOR FWD LOCKS COVER WAS MISSING, PANEL 811AR. SUSPECT THAT IT WAS STRUCK DURING CLOSING OF THE DOOR BY LOADING EQUIPMENT AT THE DEPARTURE AIRPORT.Apr 10, 2011 · Airbus A310304 · Cargo/Baggage DoorsSDR CA110408004Wire · damaged(CAN) LEFT OUTER TANK BOOST PUMP 1 & 2 INDICATE LOW PRESS & LT INNER TANK BOOST PUMP NR 2 INDICATES LOW PRESS. FOUND WIRING DAMAGED IN LT WW JUST ON TOP OF GREEN HYD HP MANIFOLD AT FEED THROUGH NR 31VP, 6 WIRES FOUND DAMAGED & SHORTED & CUT AT SPLICE 116VS & Mar 22, 2011 · Airbus A310304 · Fuel System WiringSDR CA110204007Wire Harness · damaged(CAN) GEAR INDICATION SYSTEM 2 WAS UNDER MEL ON FLT, SYSTEM 1 WAS SELECTED AND DURING GEAR EXTENSION ON FLT BACK TO BASE. SYSTEM 1 FAILED AND NO GREEN LIGHT ON NLG. DURING GEAR SWING FOUND, SWITCH WAS JUMPERED AND FAULT DISAPPEARED, ELECTRICAL LOOM FABRICATEDFeb 1, 2011 · Airbus A310304 · Landing Gear System WiringSDR CA110203007Panel · delaminated(CAN) MCC CONTACTED AIRPORT AUTHORITIES REGARDING PIECE OF ALUMINUM FOUND ON THE RUNWAY POSSIBLY FROM A/C OR ANOTHER A/C THAT DEPARTED SINCE THE LAST FOD INSPECTION CARRIED OUT. MCC NOTIFIED STATION AND INSPECTION WAS CARRIED OUT, BUT NO ABNORMALITIES WERE FOJan 19, 2011 · Airbus A310304 · Engine Thrust ReverserSDR CA101223006Rod End · separated(CAN) DURING OVERNIGHT ROUTINE MAINTENANCE AND TROUBLESHOOTING AN OPEN MEL ITEM FOR NR 2 & 3 SPOILER FAULT THAT WAS PLACED ON MEL (SYSTEM DEACTIVATED) PRIOR TO AIRCRAFT ARRIVAL, MAINTENANCE DISCOVERED THE NR 2 RT SPOILER ACTUATOR THREADED ROD END ASSEMBLY HAD Dec 10, 2010 · Airbus A310304 · Drag Control ActuatorSDR CA101208006Switch · burned(CAN) UPPER BEACON LIGHT C/B K73 POPPING AND SWITCH SMELL BURNED. ANTI-COLLISION SWITCH 2LV REPLACED CHECK SERVICEABLE.Nov 4, 2010 · Airbus A310304 · Exterior LightingSDR CA101026002Duct · damagedDURING WALK AROUND, LEAK SOUND FROM NR 2 ENG - FOUND DUCT BESIDE PRSOV CRACKED. DUCT BLEED ELBOW CRACKED. DUCT HAS BEEN REPLACED.Oct 25, 2010 · Airbus A310304 · Pneumatic Distribution SystemSDR FDEA201010204122Seat Track · corrodedMAIN CARGO DECK , FWD CABIN SEAT TRACK NR3 LT HAS CORROSION FR 15 TO FR16. REMOVED CORROSION WITH 55 PERCENT MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-10-16, PAGE 108, FIG 101 . R & R SEAT TRAC 3L BETWEEN FR15 AND FR16 IAW SRM 53-10-16 PAGE 108, FIG 101 ANOct 20, 2010 · N815FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010124011Seat Track · gougedSEAT TRACK 4L BETWEEN FRAME 62 AND FRAME 65 HAS 2 AREAS OF GOUGES AROUND SCALLOPS, APPROX .009" DEEP. REMOVED DAMAGED AREAS BY BLENDING OUT GOUGES ON SCALLOPS OF SEAT TRACK 4L BETWEEN FRAME 62 AND FRAME 65 IAW SRM 51-73-10, PGS 7 THRU 10. CHECKED LIMITS ANDOct 12, 2010 · N815FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR CA100917003Tube · chafedFUEL VBV ACTUATOR TUBE AND HOSE FOUND CHAFING - PN 113254-3 (IPC 72-00-00, FIG 4, ITEM 80) ON VBV FEEDBACK CABLE. THIS CHAFING CAUSED A FUEL LEAK THAT WAS FOUND DURING THE WALKAROUND. TUBE AND HOSE FUEL VBV HAS BEEN REPLACED IAW AMM 75-32-01 AND ESM 72-00-00Sep 13, 2010 · Airbus A310304 · Engine Fuel DistributionSDR CA100630004Hook · wornDURING PERFORMANCE OF MPD TASK 292500-05-1, (GENERAL INSP OF CONTROL LINKAGE FOR CORROSION AND DAMAGE), RAT FAILED TO DEPLOY FROM BOTH THE CAPT`S OR F/O`S RELEASE LEVER. PROBLEM WAS IDENTIFIED TO BE WITH THE UPLOCK ACTUATOR. A NOTCH HAD WORN IN THE HOOK ASSYJun 22, 2010 · Airbus A310304 · Hydraulic System, AuxiliarySDR FDEA201002090367Bellcrank · dirtyLT MAIN GEAR DOOR WOULD NOT CLOSE ON T/O. RETURNED TO DEPARTURE. OPS CHECKED LT MLG DOOR IAW MM 32-12-11-5. OPS CHECKS NORMAL. DURING TROUBLESHOOTING, WERE ABLE TO DUPLICATE THIS PROBLEM BY OPERATING DOOR WITH GROUND CONTROL HANDLE, AFTER DISASSEMBLING, CLFeb 9, 2010 · N817FD · Airbus A310304 · Landing Gear Door Retract SectionSDR CA091109004Generator · cracked(CAN) ON CHECKING APU OIL QUANTITY, MX FOUND THE APU COMPARTMENT OIL SOAKED. HSG OF THE APU GENERATOR WAS FOUND CRACKED AND LEAKING. UNIT HAS BEEN REPLACED.Nov 3, 2009 · Airbus A310304 · AC Generator-AlternatorSDR 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 FDEA200907012422Idg · underservicedON T/O ROLL AT APPROX 80 KNOTS RECEIVED ECAM ALERT, NR 1 IDG OIL PRESS W/ GEN 1 FAULT. RTO AND RETURNED TO BLOCKS. GEN 1 FAULT CLEARED BUT IDG NR1 FAULT KEPT FLICKERING. SERVICED NR 1 ENG IDG IAW AMM 12-13-24-0. RAN NR 1 ENG IAW JRH CHAP 5. NO LEAKS NOTED, Jul 1, 2009 · N817FD · Airbus A310304 · Alternator-Generator DriveSDR CA090505003Bracket · damaged(CAN) THE ACFT WAS RELEASED FROM YUL UNDER MEL FOR LT MLG MECHANICAL DOWNLOCK INDICATOR. AFTER LG EXTENSION ON APPROACH, FLIGHT REPORT CREW REPORTED THEY DID NOT HAVE DOWNLOCK INDICATION ON BOTH LT LG POSITION INDICATORS AND DECLARED EMERGENCY LANDING. AFTER Apr 29, 2009 · Airbus A310304 · Main Landing GearSDR CA090325001Landing Gear · malfunctioned(CAN) BEFORE LANDING, THE CREW REPORTED ON VHF THAT THEY HAD TO C/O A MANUAL EXTENSION OF THE NOSE LANDING GEAR DUE TO NO GREEN LIGHT INDICATION FOR THE NOSE GEAR. REFERENCE TO ACFT DEFECT LOG 1030911. TROUBLESHOOTING IS GOING ON AT THIS TIME.Mar 24, 2009 · Airbus A310304 · Nose/Tail Landing GearSDR CA090327003Actuator · faulty(CAN) DURING TAXI OUT CREW LOST YELLOW HYD SYS. FOUND AT FAULT RT NR 4 SPOILER ACTUATOR. ACTUATOR REPLACED, YELLOW HYD SYS FILLED AND TESTED SERVICEABLE.Mar 23, 2009 · Airbus A310304 · Drag Control ActuatorSDR CA090407015Wire · damaged(CAN) SPOILER NR5 FAULT AFTER TAKEOFF AND CB S64 POPPED. FOUND WIRES DAMAGED AT ROUTE 4A UNDER PANEL 572CB, WIRES NR 2711-5042, 5043, 5060, 5061, 2842-5011, 2212-5025, 2213-5025. TEMPORARY REPAIR CARRIED OUT. COAX CABLE FOR RT OUTER FUEL TANK INDICATION DAMAGMar 22, 2009 · Airbus A310304 · Electrical Power System WiringSDR CA090112009Wire · arced(CAN) MECHANIC NOTICED FLASH OF LIGHT FROM LEFT WHEEL WELL. FOUND POWER SUPPLY WIRE BUNDLE UNDER SUPPORT CLAMP ON AFT WALL OF LEFT WHEEL WELL. SYSTEM WAS DEACTIVATED AND PUT ON MEL 29-2. HARNESS WILL BE REPLACED AT THE NEXT AVAILABLE DOWNTIME AND HARNESS WIJan 9, 2009 · Airbus A310304 · Electrical Power System WiringSDR CA090108002Uplock · failed(CAN) IN DESCENT TO LGW, FLIGHT CREW REPORTED, L/G NOSE WHEEL UNSAFE INDICATION. PERFORMED L/G GRAVITY EXTENT ION. NLG UPLOCK ASSY WAS REPLACED AND OPERATIONAL CHECK WAS CARRIED OUT SERVICEABLE. AS SAFETY PRECAUTION, BOTH NOSE LANDING GEAR DOOR SEQUENCE VALDec 29, 2008 · Airbus A310304 · Landing Gear Position and WarningSDR FDEA200812065096Bushing · damagedMAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FABRICATED REPLACEMENT REPAIR BUSHING AND INSTALLED IAW FEDEX EA 6-5310-99725A, RELEASE DATE 07/20/06.Dec 6, 2008 · N817FD · Airbus A310304 · Fuselage, Landing Gear Attach FittingsSDR 08FDEA04961Seat Track · damagedMAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-21.Nov 22, 2008 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR CA080808001Attach Fitting · broken(CAN) ON LDG GEAR UP SELECTION NOSE GEAR SHOWED UNSAFE DOOR NOT UP. ECAM/QRH CARRIED OUT. ACFT RETURNED TO THE STATION. FOUND NLG UP LOCK ACTUATOR ATTACHMENT FITTING ASSY P/N A5341130500200 WITH BROKEN LUGS. NEW ATTACHMENT FITTING INSTALLED.Aug 7, 2008 · Airbus A310304 · Landing Gear ActuatorSDR CA080804001Flasher · burned(CAN) UPPER SLOWER BEACON AND STROBE LIGHTS INOP. FOUND FLASHER UNIT U/S (RECEPTACLE CONNECTOR BURNED & PARTIALLY MELTED INSIDE). CONNECTING ELECTRICAL PLUG INSULATION SLIGHTLY BURNED AND PINS DAMAGED. CONNECTOR P/N E0052R14B15SNE AND TIMER UNIT REPLACED. PARTJul 31, 2008 · Airbus A310304 · Exterior LightingSDR CA080728004Oven · dirty(CAN) FLIGHT RETURNED TO THE STATION DUE TO CABIN SMOKE FROM FWD OVEN (DARK SMOKE). CABIN DETECTOR ACTIVATED. BOTH FWD OVENS INSPECTED AND ELECTRICAL CONNECTION CHECKED AND FOUND SERVICEABLE. LT OVEN INSERTS FOUND DIRTY (FOOD RESIDUE). OVEN REPLACED AND SERVICJul 8, 2008 · Airbus A310304 · Buffet/GalleysSDR 08FDEA01724Transmitter · inoperativeON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN HYD PUMPS. FAULTS ON OVERHEAD WERE AS FOLLOWS: GREEN SYS SERVO (GREEN PUMPS OFF), SLAT SYS 1 AND 2, SPOILER NR 5. DID GO AROUND FOUND RT MMay 1, 2008 · N817FD · Airbus A310304 · Hydraulic Indicating SystemSDR 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 CA080409001Wire · burnedIN CRUISE AFT GALLEY RT COFFEEMAKER BURNED. ALL C/B’S WERE PULLED. HALON FIRE EXTINGUISHER WAS USED AS A PRECAUTIONARY MEASURE. C/B ON COFFEE MAKER FOUND POPPED. FOUND WIRES TO PRESSURE SWITCH BURNED AND DISCONNECTED. NO OTHER WIRING DAMAGE ON THE COFFEE Mar 25, 2008 · Airbus A310304 · Equipment/Furnishings WiringSDR CA080305001Pressure Switch · malfunctionedDURING CLIMB AT 18000 FEET, NR 1 ENGINE OIL FILTER CLOGGED LIGHT CAME ON. AS PER QRH, NR 1 ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO STATION WITH NO FURTHER PROBLEM. THE OIL FILTER WAS REPLACED. NO SIGNIFICANT CONTAMINATION WAS NOTICED. THE OIL SYSTEM WAMar 3, 2008 · Airbus A310304 · Turbine Engine Oil SystemSDR CA080304005Line · splitWHILE AIRCRAFT WAS UNDER MAINTENANCE IN THE HANGAR, THE HYDRAULIC RETURN LINE FOR YELLOW SYSTEM ALTERNATE BRAKE FAILED WITH A SPLIT IN THE TUBING APPROX 1.5 INCHES IN LENGTH. AT THE TIME OF THE FAILURE THERE WAS NO HYDRAULIC PRESSURE OR OPERATION OF THE SYSTEFeb 27, 2008 · Airbus A310304 · Hydraulic System, MainSDR 08FDEA00192Hydraulic System · lowREJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE.Jan 18, 2008 · N817FD · Airbus A310304 · Hydraulic System, MainSDR CA071127001Pump · cracked(CAN) DURING CRUISE, THE YELLOW HYD SYS OVERHEAT ECAM MESSAGE CAME ON. LATER THE HYD RESERVOIR (LO LEVEL) WARNING CAME ON THE ECAM. NORMAL QRH PROCEDURE WAS PERFORMED. DURING INVESTIGATION, MAINT FOUND YELLOW HYD PUMP LEAKING. HYD PUMP CASING WAS CRACKED. PUMPNov 20, 2007 · Airbus A310304 · Hydraulic Pump (Electric/Engine), MainSDR 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 CA070424002Fan · odor(CAN) DURING FLIGHT CABIN CREW REPORTED ELECTRICAL BURN ODOR FROM THE AFT CABIN. FAULT ISOLATED TO THE AFT RT FAN HEATER FIN NR 28HC. CB’S WERE PULLED AND ODOR DISAPPEARED. SYSTEM WAS PLACED ON MEL DUE PART IS NIL STOCK. (TC NR 20070424002)Apr 21, 2007 · Airbus A310304 · Air Distribution FanSDR CA070424001Ptu · leaking(CAN) DURING FLIGHT, CREW NOTICED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. FLIGHT DIVERTED TO MAIN MAINTENANCE BASE FOR INVESTIGATION. DURING INVESTIGATION, THE GREEN/YELLOW SYSTEM PTU WAS FOUND LEAKING AT THE CHECK VALVE DUE TO A DAMAGED O RING. PTU UNIT WAS REPApr 20, 2007 · Airbus A310304 · Hydraulic System, MainSDR CA070424003Unknown · unknown(CAN) DURING CRUISE, CREW NOTICES A FUEL DISCREPANCY OF ONE TON BETWEEN FUEL ON BOARD AND FUEL USED. AFTER RECALCULATION SHORTLY THEREAFTER THE FUEL DISCREPANCY HAD GROWN TO 1.4 TONS. CREW PROCEEDED WITH QRH PROCEDURES AND SPOTTED FUEL SPAYING FROM THE RIGHT WApr 12, 2007 · Airbus A310304 · Aircraft Fuel SystemSDR CA070411002Switch · sticking(CAN) DURING CLIMB THE AIRCRAFT HAD A (KRUGER) FAULT ECAM WARNING.QAH CARRIED OUT BUT WARNING REMAINED ON. AIRCRAFT RETURNED TO THE STATION. DURING TROUBLESHOOTING THE BITE TEST ON THE SFCC 1 AND 2 FAULTED THE RT RETRACT SWITCH. THE SWITCH WAS FOUND DIRTY AND Apr 5, 2007 · Airbus A310304 · Landing Gear Retraction/Extension SystemSDR CA070404004Hose · punctured(CAN) GREEN HYDRAULIC ECAM MESSAGE LOW LEVER WARNING CAME ON AFTER TAKE OFF. ON ARRIVAL, MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE HOSE LEAKING. FOUND HOLE IN FLEX LINE. FLEX LINE WAS REPLACED WITH BOTH HYDRAULIC PUMPS, CASE DRAINApr 4, 2007 · 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 07FDEA01303Attach Fitting · crackedFUSELAGE CRACKED LT NLG DOOR ACTUATOR ATTACH FITTING (EO 6-5340-7-5001). COMPLIED WITH EA 6-5340-102027 PT1 FUSELAGE CRACKED LT NLG DOOR ACTUATOR ATTACH FITTING (EO 6-5340-7-500 1) IAW SB A310-53-2065 REV 04.Apr 3, 2007 · N414FE · Airbus A310304 · Fuselage Main, Attach FittingsSDR 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, Frame
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