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 FDEA201304090756Limit Switch · failedCLIMBING THROUGH 5,100 METERS RECEIVED ECAM ALERT. FORWARD CARGO DOOR UNLOCK, PROCEEDED ACCORDING WITH ECAMS SET LANDING ELEVATION AT 10,000 ALERT WENT AWAY AND CAME BACK IN FINAL AGAIN. EXECUTED OVER WEIGHT LANDING IAW QRH. GROUND CHECKED THE FWD CARGO DApr 9, 2013 · N811FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201303120549Rib · crackedLT WING T/E AT 284.85, SUPPORT RIB CRACKED, JUST BETWEEN SPOILER NR 5 AND SPOILER NR 6.Mar 12, 2013 · N808FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201303030491Floorboard · delaminatedAFT CARGO BAY FLOORBOARD BETWEEN 1R AND 2R RAIL TRACKS, 2 FEET FWD OF BALL MAT HAS 24"OF DELAMINATION. FLOORBOARD WAS DAMAGED BEYOND ECONOMICAL REPAIR. FABRICATED A REPLACEMENT FLOORBOARD IAW DWG SRZ-25-005, REV J.Mar 3, 2013 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201302270475Ferrule · crackedNR 2 PYLON FERRULE IS CRACKED COMPLIED WITH EA 6-5450-T0300139 REV NR PS P1 - NACELLES/PYLON PRECOOLER FERRULE CRACK ON NR 2 PYLON REF WR 54-50 6954.Feb 27, 2013 · N803FD · Airbus A310324 · Nacelle/Pylon, Main FrameSDR FDEA201302190374Frame · corrodedFUSELAGE AFT PRESSURE BULKHEAD FWD FACE LWR RIM FR 80/82 HAS 3 EA AREAS OF EXFOLIATED CORROSION & 1 EA AREA OF CORROSION EXTENDING INTO THE CLEAT PROFILE. DEFECT MEASURES 15"SQ. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND ANGLES TO BE OUT OF LIMITS IAW SRMFeb 19, 2013 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201302080306Skin · dentedRT WING OTBD FLAP L/E APPROX WING RIB 25 HAS A DENT WITH FIELD REPAIR APPROX 1.5 X 1.5 X .200D. CUT OUT DAMAGED AREA. FABRICATED, HEAT TREATED, LOCATE AND DRILLED REPAIR PARTS IAW SRM 57-53-12, FIG 213. PROTECTED REPAIR PARTS AND THE CUT OUT AREA ON RT FLAPFeb 8, 2013 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201302060288Floorboard · delaminatedMLG BAY LT AFT WALKWAY PANEL 148 BF HAS 60 SQ" AREA OF DELAMINATION. FABRICATED REPLACEMENT PANEL 148 BF IAW DWG SRZ 25-005, REV J.Feb 6, 2013 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201301170121Connector · failedCAPTAIN'S RA DOES NOT PROPERLY AGREE WITH FO'S RA. DURING TROUBLESHOOTING NR 1 R/A WOULD FLUCTUATE BETWEEN 150FT AND 450FT, THEN GO ABOVE 2500FT. DISCONNECTED BOTH TRANSMIT AND RECEIVING ANTENNAS AND METERED BOTH COAX CABLES FROM NR 1 R/A RACK CONNECTOR (1Jan 17, 2013 · N812FD · Airbus A310324 · Ground Proximity SystemSDR FDEA201212244367Skin · delaminatedRIGHT WING INBD LOWER FLAP T/E MID SECTION FOUND DELAMINATED. REMOVED DELAMINATED DOUBLER & DAMAGED HONEYCOMB CORE IAW SRM 57-52-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-52-12/201. MADE HONEYCOMB CORE PLUG SRM 57-52-12/201. INSTALLED HONEYCOMB CORE PLUG ANDec 24, 2012 · N812FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201212244368Skin · delaminatedLEFT WING OTBD FLAP T/E LOWER SURFACE FOUND DELAMINATED, FROM INBD TO OTBD 2000 MM, DIM:16" X 7". REMOVED DELAMINATED LOWER SKIN IAW SRM 57-53-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-53-12/201. FILLED THE HONEYCOMB CORE WITH COMPOUND IAW SRM 57-53-12/201. Dec 24, 2012 · N812FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201212154307Fitting · corrodedLEFT WING-MLG FITTING-INSPECTION OF RIB 5 FORWARD LUG CORROSION EXCEED LIMITS. REMOVED CORROSION IAW REPAIR DWG R57249389, ISSUE B, STEP 1B. IAW EA6-5710-163164. PENETRANT INSPECT THE LUG BORE IAW NTM 51-90-00 TO CONFIRM ALL DAMAGED COMPLETELY REMOVED. IAW Dec 15, 2012 · N812FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA201212144299Spar · crackedCENTER WING RT REAR SPAR NR 61 HOLE FOUND CRACKED. REAMED HOLE AT 0.4MM THROUGH ALL LAYERS PER EA6-5710-163167. INSPECTED PER NTM51-10-01,NO CRACK FOUND. REAMED UP THE HOLE ON ALL LAYERS TO 15.836-15.875MM IN TRANSITION FIT PER EA6-5710-163167. WET INSTALLDec 14, 2012 · N812FD · Airbus A310324 · Wing SparSDR FDEA201212144297Plate · crackedFOUND A CRACK ABOUT 5MM IN LENGTH, 1MM IN DEPTH INITIATED FROM THE NR 2 FASTENER HOLE OF THE RT WING UPPER CORNER ANGLE AT FR40. REAMED NR 2 HOLE AT 0.4MM THROUGH ALL LAYERS PER EA6-5710-163166. INSPECTED PER NTM51-10-01,NO CRACK FOUND. REAMED HOLE ON ALL LDec 14, 2012 · N812FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201207262710Engine · failedUPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MODE FAULT AND ATS LEVER KICKED OFF. NOTICED ENG 1 EGT GAUGE INOP AT "0". ENG 1 N1 BEGAN UNCOMJul 26, 2012 · N805FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR FDEA201206272374Actuator · faultedPRIOR TO THRUST SET FOR TAKEOFF, RECEIVED NR 1 ENGINE FADEC CHANNEL A FAULT AND FADEC CHANNEL B FAULT. REJECTED TAKEOFF AT 45-50 KNOTS. FOLLOWED QRH PROCEDURES. SHUTDOWN AND RESTARTED NR 1 ENGINE, ATTEMPTED TAKEOFF AND RECEIVED SAME FAULTS AT SLIGHTLY HIJun 27, 2012 · N806FD · Airbus A310324 · Fuel Controlling SystemSDR FDEA201206172253Hydraulic System · warning messageDURING CLIMB, HAD GREEN SYS OVERHEAT ECAM. COMPLIED WITH CHECKLIST, MANUALLY EXTENDED LANDING GEAR TOWED OFF RUNWAY. DRAINED AND SERVICED GREEN SYS HYD RESERVIOUR PER MM 29-14-00-03. RAN NR 1 AND 2 ENGINES IAW JRH. ALL INDICATIONS AND PARAMETERS NORMAL. Jun 17, 2012 · N810FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201205041733Skin · crackedNR 1 ENGINE PYLON LT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR FDEA201205041732Skin · crackedNR 1 ENGINE PYLON RT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR FDEA201205011687Skin · crackedONE CRACK FOUND, LENGTH 13MM AT RT WING BOTTOM SKIN LANDING PLATE AREA. REPAIRED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 1, 2012 · N806FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201205011689Angle · crackedLEFT FRAME40 PICK UP ANGLE FOUND CRACK EXTENDED FURTHER THAN STOP HOLE (EXTENDED CRACK LENGTH:0.2INCHES) COMPLY WITH EA 6-5310-161218, PART 1.May 1, 2012 · N808FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201204271627Floor Support · corrodedFWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORROSION LOCATION FROM FR 11 TO FR 13A AND Y-724. R & R FLOOR SUPPORT WITH NEW IAW SRM 51-72-10. THE REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Apr 27, 2012 · N806FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201204271661Slide · partial deployINADVERTENT OPENING OF R1 CABIN DOOR STARTED INITIATION OF SLIDE DEPLOYMENT. INSTALLED R1 ESCAPE SLIDE IAW MM 25-61-20-02, AND ADJUSTMENT AND TEST IAW MM 25-61-20-05-01. OP'S CHECKED NORMAL, INSTALLED R1 PNEUMATIC EMERGENCY DOOR ASSIST BOTTLE ARMING LEVER,Apr 27, 2012 · N801FD · Airbus A310324 · Escape SlideSDR 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 FDEA201204181477Floor Panel · damagedAVIONICS BAY FLOOR PANEL 122PF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-27- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 12 A53210216. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10-Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181476Floor Panel · damagedBULK CARGO BAY FLOOR PANEL 162HF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 17 A53279962. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10-35Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181475Floor Panel · damagedBULK CARGO BAY FLOOR PANEL 161JF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35- 04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 17 A53279960. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL COApr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181474Floor Panel · damagedAFT CARGO COMPARTMENT FOUND FLOOR PANEL 151AF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 10 A25772831. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204181473Floor Panel · damagedFWD CARGO BAY FLOOR PANEL 132RF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL, FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG A53272792. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-29-Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201204051259Fuel Cell · leakingLEFT WING INNER TANK LOWER SURFACE 1 EA BOLT FUEL SEEPING NEAR REAR SPAR RIB 8 POSITION. USED OPTIONAL INSP METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND RESEALANT ON THE NUT IAW SRM 51-49-00. APPLIED NEW Apr 5, 2012 · N805FD · Airbus A310324 · Fuel StorageSDR FDEA201204051258Fuel Cell · leakingRIGHT OUTER TANK REAR SPAR, FUEL SEEPING AT NR 6 SPOILER BLOCK VALVE SUPPORT FITTING LWR RT FITTING FASTENERS. USED OPTIONAL INSPECTION METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND SEALANT ON THE NUT IAW SRApr 5, 2012 · N805FD · Airbus A310324 · Fuel StorageSDR FDEA201203301200Hydraulic System · multiple failDURING CRUISE FLIGHT, HYD GREEN SYS RESERVOIR OVERHEAT ILLUMINATED ON ECAM. GREEN HYD PUMPS SECURED UNTIL APPROACH. TURNED BACK ON LOW POWER LIGHTS ILLUMINATED, NO GREEN HYD QUANTITY INDICATED. R & R NR 1 AND NR 2 ENGINE PUMPS OF GREEN SYS IAW MM 29-11-32-0Mar 30, 2012 · N810FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201203190997Floor Support · corrodedFWD MAIN DECK, COURIER FLOOR AREA, FOUND FLOOR SUPPORT CORRODED LOCATION FROM FR 11 TO 13A AND Y-724. R & R THE FLOOR SUPPORT IAW SRM 51-72-10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 19, 2012 · N805FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201203160965Floor Panel · damagedMAIN DECK FLOOR PANEL 241NK DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 16, 2012 · N805FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201203130909Skin · dentedNOSE SECTION RT LOWER HALF SKIN PLATE EXTERNAL GOT A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR 2 AND FR 3 POSITION.Mar 13, 2012 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201202160589Spar · damagedRT PYLON SPIGOT RECEPTACLE FITTING FOUND A MISDRILLED BOLT HOLE. REPAIRED IAW AMM 54-50-00 AND AMM 20-21-12Feb 16, 2012 · N804FD · Airbus A310324 · Nacelle/Pylon, Main FrameSDR FDEA201202100542Skin · contaminatedTWO WATER TRAPPED AREAS WERE FOUND AT RT RUDDER NR 27 SCREW (5.5" X 5") AND NR 38 SCREW (3" X 1.5") (EO 6-5530-7-5004, PART 2) NDT INSPECT L/E AND T/E. THE OUTER SKIN AND EVLUATED THE DIMENSION OF THE DAMAGED AREA ARE 5.5"X5" (NR 27 SCREW) AND 3"X1.5" (NFeb 10, 2012 · N804FD · Airbus A310324 · Rudder, Plate/SkinSDR FDEA201202100543Skin · corrodedRIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 4 AND RIB 6. PERFORMED THE REPAIR IAW EA 6-5730-1490. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201202100541Skin · corrodedLEFT WING BOTTOM SKIN UPPER SURFACE CORRODED AT RIB 5 REINFORCING BEHIND REAR SPAR AREA. REMOVED CORROSION IAW EA 6-5730-149035. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201202040470Skin · dentedNOSE SECTION RT LOWER HALT SKIN PLATE EXTERNAL HAS A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR2 AND FR3 POSITION 1. PAIN REMOVED IAW SRM 51-75-20. CUT OUT THE DAMAGED AREA. REPAIRED THE REWORK AREA WITH FASTENERS AND DOUBLER REFER TO SRM 53-Feb 4, 2012 · N804FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201201110095Skin · corrodedRIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND WITHIN THE ALLOWABLE DAMAGE LIMIT IAW SRM 57-20-12. RESTORED SURFACE PROTECTION IAW SRM 51-49-00 AND Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110094Skin · corrodedRIGHT WING UPPER SKIN NEAR MIDDLE SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 ANDJan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110096Floor Support · corrodedFWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORRODED FROM FR 12 TO FR 14 BETWEEN Y 383 AND Y 953. REPLACED WITH NEW SUPPORT IAW SRM 51-40-21 AND 51-72-10. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 11, 2012 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201201110093Skin · corrodedRIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION AT RIB 7. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51-21-10. REPAIRJan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110091Skin · corrodedRIGHT WING UPPERSKIN NEAR FRONT SPAR FOUND CORRODED, POSITION BETWEEN RIBS 16 AND 17. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51-Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110090Skin · corrodedRIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 20 AND RIB 21. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED SURFACE PROTECTION IAW SRM 51-49-00 AND 5Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110089Skin · corrodedRIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 25 AND RIB 26. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51-2Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110088Skin · corrodedRT WING UPPER SKIN FOUND CORROSION POSITION ABOUT RIB 27 BESIDE THE OTBD JET FUEL PANEL. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110086Skin · corrodedRT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 28 AND RIB 29. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FOUND WITHIN THE ALLOWABLE DAMAGE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201080046Seat Track · chafedMAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y0. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16 A53274256. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
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