Airbus A310-324

Service difficulty reports · 1,439

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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 = 'A310324'
  ORDER BY difficulty_date DESC"

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SDR FDEA201009143394Floor Panel · puncturedBULK PIT FLOOR PANEL 161 GF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES & INSTALLED INSERTS IAW SRZ 25-005, REV "H". TRIMMED & BONDED METAL PLATE IAW SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143393Floor Panel · puncturedBULK PIT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143392Floor Panel · puncturedBULK PIT FLOOR PANEL 162 EF IS PUNCTURED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143391Panel · dentedBULK CARGO SLANT PANEL 162 CW HAS DENT DAMAGE. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS REF DWG SRZ 25- 005, REV "H". FABRICATED, TRIMED AND BONDED A METAL PLATE REF DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201009143390Floor Panel · puncturedBULK CARGO SLANT PANEL 161 CW IS PUNCTURED AND DENTED IN NUMEROUS PLACES. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 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 FDEA201009103337Skin · corrodedRT WING BOTTOM SKIN, LOWER SURFACE IS CORRODED AT RIB 31. REAR SPAR AREA. REMOVED CORROSION. ORIGINAL MATERIAL 0.150. MATERIAL REMAINING 0.091. MATERIAL LOSS 0.059 OUT OF LIMITS IAW SRM 57-20-12. RERPAIR AREA IAW EA 6-5710-136708, "WINGS - RT WING LOWSep 10, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201008263146Pitot Head · contaminatedF/O A/S INOP DURING T/O ROLL ABORTED T/O. PVG U CHECKED F/O PITOT TUBE FOUND A BUG INSIDE, CLEARED PITOT TUBE AND PERFORMED THE PITOT TUBE INSP ALL OK IAW AMM 34-11-15-6, PERFORMED AUTO LAND SYS TEST PASSED IAW AMM 22-00-00, ACFT REMAINED CAT 3III, ACFT OKAug 26, 2010 · N804FD · Airbus A310324 · Pitot/Static SystemSDR FDEA201008032783Slat System · malfunctionedSLOWING THRU 200 KTS TRIED TO EXTEND SLATS. AS SOON AS HANDLE MOVED FROM DETENT, GOT LOUD GRINDING NOISE. ALSO GOT ECAM WARNING FOR SLAT 1 & SLAT 2 FAULT. RECYCLED HANDLE. WARNINGS CLEARED; SLOWED TO 180 KTS, EXTENDED SLATS NORMALLY WITH NO WARNINGS AND Aug 3, 2010 · N815FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201007082424Shear Tie · crackedFWD CARGO DOOR STRUCTURE SKIN SUPPORT ANGLE AFT OF ACTUATOR HINGE FITTING LOWER END HAS 1 IN CRACK REMOVED DAMAGED ANGLE AND STRINGER CLIPS, FABRICATED REPLACEMENT ANGLE AND 2 EA STRINGER CLIPS IAW MFG DWG A52370111 AND DWG A52370142 AND INSTALLED REPLACEMENT Jul 8, 2010 · N402FE · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201007082423Priority Valve · failedON START OF T/O ROLL, RECEIVED ECAM FOR BLUE RSVR LO LEVEL, BLUE RSVR INDICATES EMPTY. TURNED OFF BLUE HYD ENG PUMP APPROX, 2 MINUTES AFTER ECAM ALERT. T/S AND FOUND ACTUALLEY BLUE RSVR HYD QTY INDICATED 1.5 G/L AND BLUE HYD MANIFOLD PRIORITY VALVE BROKEN.Jul 8, 2010 · N805FD · Airbus A310324 · Hydraulic System, MainSDR 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 FDEA201006252142Uplock · failedON TAKEOFF WITH GEAR HANDLE SELECTED UP- HEARD LOUD NOISE FROM UNDER ACFT AND NOSE GEAR DOOR LIGHT ON BOTH MAIN INDICATOR AND OVERHEAD INDICATOR. DURING AFTER TAKEOFF CHECKLIST WITH GEAR HANDLE POSITION TO NEUTRAL- NOSE GEAR CAME DOWN AND LOCKED. PUT HANJun 25, 2010 · N813FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201003301032B-Nut · leakingHYD GREEN SYS SERVICED WITHIN LIMITS, 10 MINUTES AFTER DEPARTURE, QTY IN AMBER BAN D. TURNED OFF NR 1 ENG HYD PUMP PRIOR TO TO RED DOT IN AMBER BAND AT FLT LEVEL 20. 15 MINUTES LATER RESERVOIR EMPTY. COMPLIED WITH QRH. SAFE LANDING. FOUND FLUID LEAKING OMar 30, 2010 · N812FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201003160837Thrust Reverser · malfunctionedON TAKEOFF AT 60 KIAS, THE NR 2 THRUST REVERSER UNLOCKED LIGHT WITH ACCOMPANIED ECAM WARNING ILLUMINATED. TAKEOFF REJECTED, ECAM AND QRH CHECKLISTS COMPLETE. MEL 16MAR10 RELEASED FOR SERVICE PER MEL: 78-30-01-C CATEGORY: C EXPIRATION: 26MAR10, "MEL 78-30-Mar 16, 2010 · N815FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201003090706Indicator · intermittentSHORTLY AFTER LEVELOFF AT 380 LT OUTER FUEL INDICATED "XX" WITH TOTAL FUEL READING "XX" AND ALSO GW AND CG READING "XX" ON ECAM. LT OUTER FUEL QUANTITY ON OVERHEAD WAS BLANK. MEL 28-21-09 ALREADY HAD AUTO FUEL FEED SYSTEM DE-ACTIVATED FUEL ON LT INNER TANK Mar 9, 2010 · N803FD · Airbus A310324 · Fuel Indicating SystemSDR FDEA201003070672Jackscrew · failedRECEIVED SLAT SYS 1 AND SYS 2 FAULT. SLAT STUCK AT APPROX 2 DEG, LANDED SLATS 2 DEG AND FLAPS 40 DEG, REPEAT WRITE UP. CYCLED ON THE GROUND PRIOR TO DEPARTURE AND THEY WORKED OK. CYCLED AIRBORN AND THEY STUCK. APPEAR TO BE AIRLOAD RELATED, CYCLED AT 210 KTMar 7, 2010 · N812FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201001130093Stringer · misrepairedPREVIOUS STR REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETWEEN FRAMES 72 TO 74 HAS 2 EACH REPAIR ANGLES AND 1 EACH STR REPAIR SECTION. PREVIOUSLY INSTALLED REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETJan 13, 2010 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201001110078Fairing · shearedNR 2 PYLON FAIRING 485AL INBD AFT SECTION MOUNTING RIVETS SHEARED NOT GOING THROUGH REINFORCING STRINGER REMOVED REINFORCING ANGLE. REPAIRED SKIN USING SPLICING METHOD IAW EA 6-5480-137727. REPLACED REINFORCING ANGLE IAW SRM 51-72-10.Jan 11, 2010 · N805FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR FDEA200912294540Skin · dentedLT SIDE LWR FUSELAGE SKIN AT FRAME 67 STR 50L DENT MEASURING 12 INCHES X 1 INCH X .188 DEEP. REPAIRED SKIN PN A53974208200 AT FRAME 67 BETWEEN STRINGERS 49L AND 50L USING DOUBLER AND FILLER IAW SRM 53-10-12 FIG. 225 PAGES 357 THROUGH 366.Dec 29, 2009 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA200912234512Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STRINGER 36 LT BETWEEN FRAMES 20 TO 22 HAS 1 EACH REPAIR SPLICE MEASURING 7.2" LONG AND 1 EACH STRINGER REPAIR SPLICE MEASURING 24.3" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT FWD CARGO ON STRINGER 36 LT BETWDec 23, 2009 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA200912104401Skin · misrepairedPREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT UPPER NOSE SKIN BETWEEN RIBS 14 TO 17 MEASURES 11.7 INCHES X 9.8 INCHES. PREVIOUSLY INSTALLED REPAIR LOCATED AT LT WING NR 2 SLAT UPPER NOSE SKIN BETWEEN RIBS 14 TO 17 WAS DETERMINE NOT TO BE IAW EA6-5710-8101Dec 10, 2009 · N804FD · Airbus A310324 · Leading Edge DevicesSDR FDEA200912104400Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RT SIDE FUSELAGE SKIN AT FRAME 74 AND BETWEEN STRINGERS 39 TO 41 RT MEASURES 9 INCHES X 7.2 INCHES, WITH A SKIN CUTOUT BETWEEN STRINGERS 39 AND 40 RT MEASURES 2.7 INCHES X 1.7 INCHES. PREVIOUSLY INSTALLED REPAIR LOCADec 10, 2009 · N804FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA200912084382Computer · malfunctionedON CLIMB OUT, FLAPS AND SLATS UP, CAPT MAX SPEED INDICATOR (ZIPPER) REMAINED AT 245 KTS. F/O SPD LIMIT REMAINED "ON". R & R NR 2 SFCC DUE TO FAULT AND R & R NR 1 SFCC AS A PRECAUTION IAW AMM 27-51-18-4 AND TESTED IAW AMM 27-51-00-0, BITE TESTS PASS NO FAULTDec 8, 2009 · N808FD · Airbus A310324 · Speed-Attitude Correction SystemSDR FDEA200912074364Skin · corrodedLT WING UPPER SURFACE GRAVITY FUEL PORT INBD HAS LEVEL 1 CORROSION AROUND CUT-OUT EXTENDING UNDER SKIN APROX 1" TO 1.5" REPAIRED UPPER WING SKIN AROUND LT UPPER FUEL PORT IAW EA NR 6-5730-135142 AND A/B DWG R57349265 AND RAS NR RAS/BAE/1011485/2009 ISSUE 'A DUDec 7, 2009 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA200911244150Coalescer Bag · dirtyOIL ODOR IN THE COCKPIT AFTER DEPARTURE THAT DID NOT SUBSIDE. RETURNED TO DEPARTURE. R & R NR 1 & 2 WATER SEPARATOR COALESCER BAGS AS PRECAUTION TO REMOVE ANY RESIDUE THAT MIGHT CAUSE ODOR IN COCKPIT IAW AMM 21-51-16-3. AFTER REPLACEMENT, PERFORMED AN AIR CNov 24, 2009 · N815FD · Airbus A310324 · Humidity Control SystemSDR FDEA200911204098Brake Sys · malfunctionedDURING TRO WITH MAX BRAKES SELECTED, ONLY WHEEL BRAKES ON NR1,2,5,6 (LT SIDE) OPERATED NORMALLY. ACFT STARTED ABRUPT PULL TO LT DESELECTED AUTO BRAKES AND STOPPED USING MANUAL BRAKES. MEL 20NOV09 14:24 GRR RELEASED FOR SERVICE IAW MEL: 32-42-05 CATEGORY:Nov 20, 2009 · N812FD · Airbus A310324 · Landing Gear Brake SystemSDR FDEA200911204097Anti-Ice System · faultedDURING T/O POWER APPLICATION, WHEN TOGA PWR WAS SELECTED THE GREEN A/THR LIGHT ILLUMINATED HOWEVER THE THROTTLES WOULD NOT MOVE. ACCOMPLISHED RTO AT 25 KTS. VERIFIED AT BLOCK IN NR1 ENGINE ANTI ICE WAS FAULTING IN ECAM. RELEASED FOR SERVICE IAW MEL: 22-30-01Nov 20, 2009 · N812FD · Airbus A310324 · Engine Anti-Icing SystemSDR FDEA200911204095Anti-Ice Valve · faultedDURING TAKEOFF ROLL AT 85KTS ECAM WARNING "ENG NAC ANTI ICE VALVE". ACCOMPLISHED RTO (ENG NR1) ENG ANTI ICE WAS ON DURING TAKE OFF. VERIFIED AT BLOCK IN NR 1 ENG ANTI ICE WAS FAULTING IN ECAM. VERIFIED AT BLOCK IN NR 1 ENG ANTI ICE WAS FAULTING IN ECAM. "MENov 20, 2009 · N812FD · Airbus A310324 · Air Intake Anti/De-Ice SystemSDR FDEA200911204093Anti-Ice Valve · warning messageDURING TAKEOFF ROLL WITH ANTI-ICE ON, RECEIVED ECAM MESSAGE "ENG NR1 ANTI-ICE NAC VALVE". ACCOMPLISHED RTO AT 70 KTS. (RTO 1 OF 2) SEE WRI 30-20/3659 FOR DEFERRAL OF NR1 ENG NAC A/I VALVE. FAULT CLEARED WHEN REDUCING POWER, NO FURTHER FAULTS. CREW TAXIED Nov 20, 2009 · N812FD · Airbus A310324 · Air Intake Anti/De-Ice SystemSDR FDEA200911033799Pitot Tube · malfunctionedNO AIRSPEED INDICATION AT 80/KTS. REJECTED TAKEOFF, RETURNED TO GATE FOR FUEL. SUSPECT BAD ADC. FAC ORDERED TO MSN 1151676 AND THE ADC IS ORDERED TO MSN 1151673. NOTE THAT THE INFORMATION ON F/O SIDE IS GOOD. THE STANDBY AIRSPEED INDICATORS INFORMATION ANNov 3, 2009 · N803FD · Airbus A310324 · Pitot/Static 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 FDEA200908133009Floorbeam · corrodedAFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y-140. BEAM REPLACED IAW SRM 51-40-21.Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200908133008Floorbeam · corrodedAFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y1470. REPLACED IAW SRM 51-40-21.Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200908073165Skin · delaminatedLT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10.Aug 7, 2009 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA200908033100Structure · crackedCOCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.Aug 3, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907303099Structure · crackedCOCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y-1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.Jul 30, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907293007Fitting · corrodedFWD CARGO COMPT - MANHOLE FITTING - CORROSION FOUND BTW FR38.1&FR38.2. CORROSION REMOVED IAW SRM 51-74-10. MANHOLE WAS REPAIRED IAW A310 SRM 53-14- 12 FIG.203.Jul 29, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907292910Skin · corrodedRIGHT WING - SPOTS OF CORROSION AT UPPER SKIN SURFACE AT REAR SPAR LOCATION, BTW RIBS 4 AND 5. CORROSION WAS BLENDED OUT AND REMAINING THICKNESS FOUND ACCEPTABLE AS PER EA 6-5710-131042.Jul 29, 2009 · N802FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA200907273108Beam · corrodedAFT CARGO COMPT, CORROSION ON BEAM OF CARGO COMPT FLOOR AT FRAME 63 BTW Y805 AND Y1740. THE BEAM WAS REPLACED IAW SRM 51-72-10.Jul 27, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907233102Trunnion · damagedLT WING - NR 3 EXTERIOR TRUNNION FOUND DAMAGED. TRUNNION NR 3LH WAS REPAIRED IAW CMM 57-53-12.Jul 23, 2009 · N802FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA200907032470Brake · burnedNR 8 BRAKE TAXING INTO GATE WENT ABOVE 300 DEGS WITH ALL OTHER TEMPS BETWN 50-75 DEGS. ON ARRIVAL, WERE INFORMED BY GRD CREW THE BRAKES WERE VERY HOT, SMOKING AND LATER CAUGHT FIRE. ECAM SHOWED TEMP ABOVE 600 DEGREES. BRAKE FANS WERE ACTIVATED BEFORE GATE AJul 3, 2009 · N802FD · Airbus A310324 · Landing Gear Brake SystemSDR FDEA200906292427Fitting · corrodedCORROSION WAS FOUND ON MANHOLE FITTING AT FR 23-24. REPAIR EVALUATED AND FOUND WITH CORROSION AT FWD MANHOLE INTEGRAL FITTING. MANHOLE REPLACEMENT PLUS REPAIR WERE ACCOMPLISHED IAW EA 6-5310-131032.Jun 29, 2009 · N801FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA200906232556Cargo Track · crackedAFT CARGO COMPT - TRACK ROLLER NR 4 BTW FR55/58 AND 63 CRACKED AND WITH CORROSION AT DRAIN AREA. THE TRACK WAS REPAIRED IAW SRM 53-10-15 FIG 202.Jun 23, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906232436Skin · dentedRIGHT WING FLAP OUTBOARD UPPER SKIN SURFACE WITH DEEP DENT AT FRICTION PLATE SEATING AREA BETWEEN RIB 2.5 AND RIB 3. REPAIRED IAW E.A. 6-5710-131025.Jun 23, 2009 · N801FD · Airbus A310324 · Wing Main, Frame StructureSDR FDEA200906222519Floorbeam · corrodedAFT CARGO COMPT- FR60 CROSSBEAM WITH CORROSION BTW Y1300 AND Y1390. BEAM REPAIRED IAW SRM 53-10-15 FIG 207.Jun 22, 2009 · N801FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200906192472Arm · corrodedVERTICAL STABILIZER RUDDER HINGE ARM NR 4 FOUND WITH CORROSION AT VERTICAL STABILIZER CONNECTION. RUDDER HINGE ARM REPAIRED AS PER EA 6-5510-131027.Jun 19, 2009 · N801FD · Airbus A310324 · Horizontal Stabilizer StructureSDR FDEA200906192468Skin · damagedRIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030Jun 19, 2009 · N801FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA200906162513Track · misrepairedPREVIOUS REPAIR FOUND LOCATED AT ROLLER TRACK LT, ON FWD CARGO COMPT BTW FR38- 38.1 AT STA Y140. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200906162473Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR76-77 AT ATGR 23LH-25LH, NEXT TO AFT DOOR LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Plate/Skin
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