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 08FDEA01092Panel · damagedLEFT RUDDER PANEL, 25TH FASTENER FROM THE TOP OF THE RUDDER HAS 1 CELL OF WATER, MARKED IN WHITE MARKER. REPAIRED LT RUDDER PANEL 25TH FASTENER FROM TOP BY REMOVING DAMAGE & BONDING A NEW CORE & LAY-UP REPAIR PLIES IAW EA 6-5540-118453.Mar 21, 2008 · N803FD · Airbus A310324 · Rudder, Plate/SkinSDR 08FDEA01091Panel · damagedLEFT RUDDER PANEL, 2ND FASTENER FROM THE TOP HAS WATER IN 7 CONNECTED CELLS; 5 CONNECTED CELLS AND 5 INDIVIDUAL CELLS, (MARKED IN WHITE MARKER) AND DELAMINATION 3.3 INCH BY 1.9 INCH. REPAIRED LT RUDDER PANEL 2ND FASTENER FROM TOP BY REMOVING THE DAMAGED AREAMar 21, 2008 · N803FD · Airbus A310324 · Rudder, Plate/SkinSDR 08FDEA01067Smoke Detector · failedMIN EQUIPMENT BAY SMOKE INDICATION CAME ON INTERMITTENTLY, THEN STAYED ON CONSTANT. RAN ECAM ITEMS AND CHECKLIST (QRH). NO VISIBLE INDICATIONS OF SMOKE. PROBLEM CLEARED ITSELF AFTER ABOUT 2 MINS. REMOVED AND REPLACED MIN EQPT BAY SMOKE DET (12WA) PER M/Mar 19, 2008 · N814FD · Airbus A310324 · Smoke DetectionSDR 08FDEA01066Fitting · corrodedEDDIE CURRENT AND VISUAL INSPECTIONS INDICATE SURFACE CORROSION AT APPROX 45 PLACES ON THE SCUFF PLATE RETAINER BETWEEN FR 14B AND FR 16A; LT FWD DOOR CUTOUT. SEE ATTACHED FOR LOCATIONS. MARKED IN BLUE ON THE RETAINER. REMOVED CORROSION IAW A310-SRM 53-10-1Mar 19, 2008 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 08FDEA00951Fitting · damagedL-1 LOWER AFT SEALING SECTION CORNER HAS A DOUBLE DRILLED HOLE. REMOVED AND REPLACED WITH NEW FITTING PART NR A5361155629804; PO 611014.1 IAW A310 SRM 51-40-21; PG 7.Mar 14, 2008 · N803FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 08FDEA00950Skin · corrodedRIGHT WING UPPER SURFACE SKIN HAS AREAS OF CORROSION ALONG FRONT SPAR ATTACH ROW STA 556-565. REMOVED CORROSION IAW SRM 51-74-10 & WAS FOUND TO BE OUT OF LIMITS. ACCOMPLISHED HFEC OF HOLES IAW NTM 51-10-01. FLAT PEENED AREA IAW SRM 51-25-00. ALODINED IAW SRM Mar 14, 2008 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR 08FDEA00919Access Panel · crackedNR 1 PYLON, LEFT SIDE THRU ACCESS PANEL 413EL THE INTERNAL WEBBING IS CRACKED AT A PREVIOUS WELD. REMOVED INTERNAL DOUBLER IAW SRM 51-40-21; PG 7. PART MARKED IAW GMM 7-0-1001. INSTALLED IAW SRM 51-40-21; PG 7. MINOR REPAIRMar 13, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00896Skin · crackedNR 2 ENGINE AFT PYLON FAIRING; INBD MID SKIN IS CRACKED AT THREE PLACES. REMOVED DAMAGED SKIN AND DOUBLER. FABRICATED DOUBLER FROM .063 2024-0, PO 597274.1 IAW A310-300 SRM 51-26-10 AND 51-26-20; LOCATED HOLES IAW A310-300 SRM 51-40-40. ALODINED AND PRIMED Mar 11, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00877Guide · wornIN LT MLG AREA; ALL CABLE GUIDES INBD OF THE LT TRUNNION FOR THE AILERON CABLES ARE WORN. REMOVED AND INSTALLED 3 NEW CABLE GUIDES ON THE INBD SIDE OF THE LT MLG TRUNNION FOR THE AILERON CABLES IAW A310-300 AMM 20-21-12 AND AMM 27-10-00-6.Mar 11, 2008 · N803FD · Airbus A310324 · Aileron Control SystemSDR 08FDEA00865Seal Depressor · damagedFWD LWR CARGO PIT SEAL DEPRESSOR SCRATCHED AND WORN FWD AND AFT SIDES UPPER PORTION IN WORK.Mar 11, 2008 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 08FDEA00830Seat Track · damagedMAIN DECK CARGO FLOOR SEAT TRACK NR 1 RT SIDE, FR 61 HAS DAMAGE ON LOWER SURFACE, .545 IN ROUND BY .045 IN DEEP. REMOVED DAMAGED SEAT TRACK SECTION FROM FR 60.5 TO FR 61.5 AND REPAIRED IAW A310 SRM 53-10-16,FIG 208Mar 10, 2008 · N806FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00776Panel · crackedPYLON NR 1 LEFT SIDE LOWER SHIRT CLOSE OUT AT RIB 9 AND JUST FWD OF RIB 8, SHIRT IS CRACKED. REMOVED RUB STRIP, COVER PLATE, SHIRT PANEL AND ATTACH ANGLE IAW FEDEX A310-300 SRM 51-40-21, PG 6. LOCATED, DRILLED AND DEBURRED CLOSE OUT PANEL P/N A54610811600Mar 7, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00761Fairing · crackedNR 1 ENGINE AFT PYLON FAIRING; AFT WELDED SKIN IS CRACKED. STOP DRILLED THE CRACK IAW SRM 54-55-51 FIG 201.FABRICATED REPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. INSTALLED REPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. MINOR REPAIR.Mar 6, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00749Panel · chafedL/E NR 1 PYLON TOP PANEL P/N A572-44103-000 BACK SIDE HAS CHAFING MARKS IN NUMEROUS PLACES. BLENDED CHAFE MARKS IAW SRM 57-41-12 PG 102. MAT THICKNESS IS .035 IAW SRM 57-41-12, ITEM 60. MAT LOSS .006; MAT REMAINING .024, CHECKS TO BE OUT OF LIMITS IAW SRMMar 6, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00719Computer · malfunctionedUPON FLAP RETRACTION GOT SLAT SYS 1 AND SLAT SYS 2 FAULTS ALONG WITH FLAP SYS 1 FAULT. AT SAME TIME LOST ALL SPD LIMIT INDICATORS ON PFDS. ALL FAULTS RESET UPON LOWERING GEAR FOR PRECAUTIONARY LANDING. A/C IN WORK, IND MX. COULD NOT DUPLICATE FAULTS - JACMar 5, 2008 · N815FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR 08FDEA00737Floorbeam · corrodedTHE FLOORBEAM IS CORRODED AT THE CONNECTION TO FRAME 14 RT SIDE, Y - 1958. REMOVED DAMAGED SECTION OF THE FLOORBEAM IAW SRM 53-12-15. REMOVED FLOORBEAM END CONNECTORS, ATTACH ANGLES AND THE DUCT ATTACH BRACKET IAW SRM 53-12-15. RECEIVED MACHINED SECTION OF Mar 5, 2008 · N803FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 08FDEA00720Drain Pan · crackedNR 2 ENGINE PYLON HYDRAULIC/FUEL DRAIN PAN IS CRACKED IN 4 PLACES ON THE BOTTOM SIDE OF THE PAN. REMOVED DRIP PAN IAW AIRBUS A310 SRM 51-40-21; PG 7, WELD REPAIRED CRACKS IAW AEROSPATIALE DWG 41A54610805. REINSTALLED DRIP PAN IAW AIRBUS A310 SRM 51-40-21; PGMar 5, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00686Frame · corrodedFWD CARGO COMPT AT FR 36 AT RBL 29 FRAME CROSSBEAM IS CORRODED UNDER AND AROUND NUTPLATE. REMOVED CORROSION IAW SRM 51-74-10. BLENDED AREA FOUND TO BE OUT OF LIMITS. REMOVED CENTER GUIDE; ROLLER TRAY AND LATERIAL WEB TO FOM IAW SRM 51-40-21. WEIGH DAMAGMar 4, 2008 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR 08FDEA00682Panel · corrodedRT WING PANEL 650 MB; INTERIOR SURFACE HAS FRETTING AROUND THE FASTENER HOLES. CLEANED AREAS AROUND THE FASTENER HOLES; CHECKED THE LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A5735003900000; PO6Mar 3, 2008 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR 08FDEA00681Panel · corrodedRT WING VENT TANK PANEL 650 LB, HAS FRETTING AT THE INTERIOR FASTENER HOLES. CLEANED FRETTING AROUND THE FASTENER HOLES; CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A5735003900000 PO 61028Mar 3, 2008 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR 08FDEA00665Channel · fracturedNR 2 PYLON AFT POWER FAIRING 485 AL AFT SUPPORT CHANNEL HAS A FRACTURE AT THE OUTBD EDGE. REMOVED CHANNEL & FABRICATE WEB & CHANNEL ON OPS 00748 & 00749. ASSEMBLED & INSTALLED TO NR 2 PYLON IAW SRM 51-40-01 PG 7.Feb 29, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00664Attach Angle · crackedPYLON NR 1 LEFT SIDE, FWD ATTACH ANGLE FOR PANEL 413 CL IS CRACKED. REMOVED AND REPLACED BRACKET PER A310-300 SRM 51-40-21, PG 7.Feb 29, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Attach FittingsSDR 08FDEA00649Skin · crackedON THE NR 1 ENG AFT PYLON FAIRING, O/B MID SKIN PANEL ASSY IS CRACKED AT THE MID FRAME. REMOVED MID FRAME IAW SRM 51-40-21; PGS 22 & 23; PARA 6. MATERIAL ID 2024- O .063 FOR THE PATCH & 2024-0 .071 FOR THE DOUBLER IAW SRM 54-55-51; PG 202. HEAT TREATEDFeb 28, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00632Fairing · tornEMPENNAGE RT LOWER FAIRING IS TORN. REMOVED AND REPLACED THE FAIRING IAW MM 55-15-11-4. MINOR REPAIR.Feb 27, 2008 · N803FD · Airbus A310324 · Horizontal Stabilizer StructureSDR 08FDEA00631Angle · bentEMPENNAGE FR 87 TO 88 APPROX STRINGER 29, THE INTERCOSTAL IS BENT. REMOVED INTERCOSTAL FOR FOM IAW SRM 51-40-21. REMOVED DAMAGED ANGLE FROM THE INTERCOSTAL IAW SRM 51-40-21. RECEIVED ANGLE. INSTALLED ANGLE AND INTERCOSTAL IAW SRM 51-40-21. MINOR REPAIR.Feb 27, 2008 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 08FDEA00619Angle · bentEMPENNAGE FR 87 TO FR 88 APPROX AT STRINGER 26, THE INTERCOSTAL IS BENT. REMOVED INTERCOSTAL FOR FOM IAW SRM 51-40-21. REMOVED DANAGED ANGLE FROM THE INTERCOSTAL IAW SRM 51-40-21. RECEIVED NEW ANGLE. INSTALLED NEW ANGLE & INTERCOSTAL IAW SRM 51-40-21. MINFeb 26, 2008 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 08FDEA00615Intercostal · cracked.25 INCH CRACK IN MAIN CABIN INTERCOSTAL BETWEEN FRAME 79 AND FRAME 80/82 AND STRINGER 26L. REMOVED AND REPALCED WEB IAW A310-300 SRM 51-20-41. MINOR REPAIRFeb 26, 2008 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 08FDEA00614Seat Track · gougedMAIN CABIN FLOOR BETWEEN FS 54.2 AND FS 54.3; 37 INCHES RIGHT OF CENTER LINE SEAT TRACK IS GOUGED/WORN. REPAIRED SEAT TRACK IAW A310-300 SRM 53-10-16; FIG 101.Feb 26, 2008 · N803FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00613Structure · corrodedLEFT ELEVATOR LEADING EDGE INTERIOR; FWD OF THE OUTBOARD ACTUATOR IS CORRODED. REMOVED AND REPLACED IAW AMM 27-31-24. PERFORMED A FUNCTIONAL TEST OF THE ELEVATOR REF AMM 27-31-00; TEST GOOD. REMOVED AND REINSTALLED ACCESS PANELS 335AB; 335BB; 335CB; 33Feb 26, 2008 · N803FD · Airbus A310324 · Elevator StructureSDR 08FDEA00574Skin · corrodedEXTERIOR SKIN AT THE AFT EDGE OF THE NOSE WW CUTOUT TRIPLER IS CORRODED AT FR 17, BETWEEN STR 55 R AND STR 54 R. BLENDED AFT EDGE OF THE NOSE W/W CUTOUT TRIPLER IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 53-12-12, DIAGRAM 102. ALODINED IAW SRM 51-2Feb 22, 2008 · N803FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 08FDEA00573Stringer · crackedNR 2 ENG AFT PYLON FAIRING (STRINGER), INBD INTERNAL, AFT SIDE AT NUTPLATES HAS 5 CRACKS. RECEIVED FROM STOCK P/N A545152411500 PO 569792.1. NEW MEMBER TO BE INSTALLED ON CARD 44T0512-2.Feb 22, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Longeron/StringerSDR 08FDEA00567Flap Track · crackedPARTS RACK, FLAP TRACK FAIRING 632 CB, AFT WEB IS CRACKED. REMOVED AND REINSTALLED WEB ASSEMBLY AND REPLACED WEB IAW A310-300 SRM 51-40-21.Feb 22, 2008 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR 08FDEA00575Support Angle · corrodedNR 2 PYLON, ACCESS PANEL 484 BR CUTOUT, 2 AFT VERTICAL SUPPORT ANGLES HAVE CORROSION AROUND THE NUTPLATES AND FASTENER HOLES. REMOVED AND REPLACED GUSSET IN REF TO SRM 51-40-21; PG 7.Feb 22, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00572Stringer · crackedNR 2 ENG AFT PYLON FAIRING (STRINGER), OUTBD SIDE, AFT CORNER IS CRACKED. REMOVED EXISTING DOUBLER FROM THE ADJACENT AREA TO FOM IAW SRM 51-40- 10. FABRICATED NEW REPAIR IAW SRM 54-55-51; FIG 201 & EA 06-5480-118441. STOP DRILLED THE CRACK & REMOVED THE DFeb 22, 2008 · N803FD · Airbus A310324 · Nacelle/Pylon, Longeron/StringerSDR 08FDEA00566Relay · inoperativeDISCHARGE AGENT 2 LIGHT FOR THE CARGO FIRE BOTTLES FAILS TEST. DISCHARGE AGENT 2 LIGHT DID NOT ILLUMINATE UNTIL 75 MINUTES. REMOVED AND REPLACED RELAY 14WM REF ESPM 20-46-50. DISCHARGE AGENT 2 REMINDER LIGHT OPS CHECK GOOD REF AMM 26-23-00-5.Feb 22, 2008 · N803FD · Airbus A310324 · Fire DetectionSDR 08FDEA00565Lug · corrodedRT HORIZIONTAL STAB NR 6 ELEVATOR HINGE ARM LUG AT THE ELEVATOR IS CORRODED UPPER INBD. REMOVED AND REPLACED IAW AMM 55-16-45-1. FUNCTIONAL TEST GOOD IAW AMM 27-31-11.Feb 22, 2008 · N803FD · Airbus A310324 · Horizontal Stabilizer, Attach FittingsSDR 08FDEA00564Skin · delaminatedRT ELEVATOR UPPER SURFACE IS DELAMINATED APPROX 8 INCHES FROM TE TO TE FROM NR 1 HINGE ARM TO NR 6 HINGE ARM APPROX 8 FT. UPON FURTHER INSPECTION; THE ELEVATOR WAS FOUND TO BE SERVICEABLE. THE AREA NOTED IN THE DISCREPANCY IS NOT DELAMINATED.Feb 22, 2008 · N803FD · Airbus A310324 · Elevator, Plate/SkinSDR 08FDEA00544Wire · damagedAFTER START GOT OVERBOARD VALVE FAULT COMPLIED WITH ECAM QRH AND CHECKED MEL. DURING CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AVIONICS EXTRACT VALVE TO FOM AV LINE C/B'S 60HR, 61HR PULLED AND COLLARED. FOUND WIRE BUNDLE CUT, FOR AV EXTRACT VALVE. Feb 21, 2008 · N808FD · Airbus A310324 · Air Conditioning System WiringSDR 08FDEA00131Outflow Valve · failedAFTER T/O, OVERBOARD VALVE FAULTED. REMOVED AND REPLACED OVERBOARD EXTRACT VALVE (75HR) IAW MM 21-23-13-4. OPS CHK NORMAL.Jan 15, 2008 · N815FD · Airbus A310324 · Pressure Regulator/Outflow ValveSDR 08FDEA00047Window · crackedCAPT FRONT COCKPIT WINDOW CRACKED REMOVED AND REPLACED WINDOW HEAT PROTECTION NR 1 IAW MM 30-42-11-4. PERFORMED OPS CHECK AS PER MM 30-42-00-5. ALL TEST PASSED.Jan 6, 2008 · N802FD · Airbus A310324 · Flight Compartment WindowsSDR 07FDEA05026Stringer · corrodedFWD PIT BETWEEN FR 39 AND FR 38.2 STGR 53 LT HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-10-14. FAB`D STRINGER DOUBLER IN T7/711755. REMOVED AND REPLACED STRG DOUBLER AND COUPLING IAW 51-40-44.Dec 11, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04991Windshield · crackedA/C HAS DIVERTED INTO CUN DUE F/O WINDSHIELD HAS SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD A310-300 M/M 56-11-11-4, OPN CHECK IS GOOD. OK FOR SVC. REPLACED WINDSHIELD TEMP REGULATOR AS A PRECAUTION AMM 30-42-11-4 REPLACED WINDOW HEAT PROTECTION CONDec 4, 2007 · N806FD · Airbus A310324 · Flight Compartment WindowsSDR 07FDEA04854Stringer · corrodedFWD CARGO BETWEEN FR 38.1 AND FR 38.2 STGR 48 RT HAS CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. CUT OUT DAMAGE AREA STR 48 RT FR 37-38.1 IAW SRM 53-10-14. REMOVED SHEAR TIE TR 37 STR 47 RT. FAB STRINGER DOUBLER IAW MAE TRAVENov 19, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04703Structure · contaminatedCTR TANK FUEL QUANTITY FLUCTUATES IN FLIGHT FROM 60 LBS TO 1080 LBS. SHOWED 1.0 IN CTR FOR TAKEOFF. STAB TRIM WAS ADJUSTED ACCORDINGLY. NOSE WAS VERY LIGHT ON TAKEOFF ROLL AND TOOK EXCESSIVE NOSE DOWN TRIMMING TO GET AIRCRAFT IN TRIM. ONCE IN FLIGHT RECHEOct 26, 2007 · N815FD · Airbus A310324 · Fuselage Main, StructureSDR 07FDEA04722Skin · delaminatedLT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293.Oct 11, 2007 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04735Arm · corrodedNR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04733Arm · corrodedNR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04732Arm · corrodedNR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04723Skin · debondedRT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293.Oct 9, 2007 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04488Skin · corrodedFOUND CORROSION AT WEDGE C 70, P56-57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/Skin
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