Airbus A310

Service difficulty reports · 606

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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 = 'A310'
  ORDER BY difficulty_date DESC"

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SDR FDEA200812205247Floor Panel · damagedFWD CARGO PIT FLOOR PANEL 131 ZF IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLS PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRDec 20, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812195238Seat Track · gougedCABIN SEAT TRACK GOUGED BETWEEN FR 18 & FR 19 AT RBL 63. REMOVED DAMAGE AND CHECKED LIMITS REF SRM 53-10-16. ALODINED REF SRM 51-21-10. PRIMED & PAINTED REF SRM 51-23-10.Dec 19, 2008 · N428FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812195234Fitting · corrodedNR 2 PYLON TO WING ATTACHMENT FITTING LUG INNER RACE BEARING AT RIB 18 RUSTED. R & R AFT ATTACH FITTING IAW AMM 54-51-75-4-02 TW - T8312G.Dec 19, 2008 · N428FE · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR FDEA200812195235Seat Track · corrodedSEAT TRACK AT RBL 35 AND FR47/48 HAS CORROSION ON OTBD FLANGE AT FASTENER HOLE, LOWER SURFACE. BLENDED CORROSION ON SEAT TRACK. ORIGINAL THICKNESS 0.078. THICKNESS REMAINING 0.054. MATERIAL LOSS 0.024. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; FIG 101. Dec 19, 2008 · N428FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR CA081219004Engine · making metal(CAN) DURING FLIGHT, NR 1 ENGINE FILTER CLOG LIGHT + ECAM WARNING. THE CREW C/O THE QRH PROCEDURE & STATUS OF WARNING DID NOT CHANGE. NR 1 ENG. IN-FLIGHT S/DOWN WAS C/O THE ACFT RETURNED TO YUL FOR FURTHER INVESTIGATION. FOUND ENGINE FILTER CONTAMINATED WITH Dec 18, 2008 · Airbus A310 · Engine (Turbine/Turboprop)SDR FDEA200812185201Floor Panel · damagedFLOOR PANEL BROKEN ON THE END ( 232HG ). REPAIRED FLOOR PANEL 232 HG BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ".Dec 18, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812185200Floor Panel · crackedFLOORBOARD 252YG IS CRACKED. FR 62 - 65 RT. REPAIRED FLOORBOARD BY FABRICATING A NEW FLOORBOARD FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ".Dec 18, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812185199Floor Panel · damagedFLOOR PANEL BETWEEN FR 45 - 46 & BETWEEN RBL 71 - 91 IS BROKEN ON THE EDGE. 242SK REPAIRED FLOOR PANEL BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ".Dec 18, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812185198Floorbeam · damagedFLOORBOARD 251FG BROKE AT CORNER FROM FRAME 69 TO FRAME 71 LT SIDE. REPAIRED FLOORBOARD BY FABRICATING A NEW FLOORBOARD FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ".Dec 18, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812185197Floorbeam · delaminatedFLOORBOARD 252WG IS DELAMINATED ON THE LWR SURFACE FROM FRAME 62 TO FRAME 65 R/H. REPAIRED FLOOR PANEL 252 WG BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ20-005; REV " G ".Dec 18, 2008 · N428FE · Airbus A310 · Fuselage Floor PanelSDR FDEA200812175227Switch · failedON APPROACH, BEFORE LANDING CHECK LIST COMPLETE, AT 200' ABOVE THE GROUND WE HAD A "TO LOW GEAR]" ALERT FWD PANEL SHOWED 3 GREEN, OVERHEAD INITIALLY SHOWED 3 GREEN BUT NOW SHOWED NO NOSE GEAR GREEN. WENT AROUND AND THE ACFT SHOWED 3 GREEN ON BOTH PANELS THRDec 17, 2008 · N815FD · Airbus A310 · Landing Gear Position and WarningSDR 08FDEA04730Skin · damagedTHERMOGRAPHY INSPECTION OF RUDDER S/N HF1005 SHOWS 3 AREAS OF POSSIBLE DEFECTS, LT SIDE- CONFIRMED BY ULTRASONIC INSP. DEFECTS AT NEAR FASTENERS 9,13 AND 20 COUNTED FROM TOP OF RUDDER REMOVED DAMAGED AREAS AND REPAIRED LT SIDE OF RUDDER IAW EA 6-5540-118Nov 5, 2008 · N420FE · Airbus A310 · Rudder, Plate/SkinSDR 08FDEA04111Floor Panel · crackedMAIN CABIN FLOOR PANEL 242 VJ IS CRACKED. FABRICATED A NEW FLOORBOARD 242 VJ IAW FEDEX DWG SRZ 25-005; REV G.Sep 29, 2008 · N450FE · Airbus A310 · Fuselage Floor PanelSDR CA080926005Connector · damaged(CAN) DURING STATION TRANSIT, CABIN CREW REPORTED SMOKE COMING FROM AFT GALLEY, WITH SMOKE WARNING, WHEN GALLEY ELECTRICAL PWR WAS PUT ON. GALLEY POWER WAS REMOVED FROM THE AFT GALLEY. DURING MX INVESTIGATION, THE GALLEY CONNECTOR 38 MC WAS FOUND DAMAGED WITSep 25, 2008 · Airbus A310 · Equipment/Furnishings WiringSDR 08FDEA03901Skin · dentedTHE FUSELAGE SKIN IS DENTED AROUND RIVETS T FRAMES 70 - 72; STRINGER 22R. RE-EVALUATED THE AREA & FOUND TO BE OUT OF LIMITS IAW SRM 53-17-12 & SRM 53-10-00. REMOVED DAMAGED AREA IAW SRM 53-10-12. FABRICATED THE FILLER & DOUBLER REPAIR IAW SRM 53-10-12. Sep 16, 2008 · N450FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 08FDEA03902Seat Track · damagedSEAT TRACK IS DAMAGED AT FRAME 54; RBL 18. REMOVED THE DAMAGED TRACK & INSTALLED A NEW TRACK WITH SPLICE IAW SRM 53-10-16.Sep 16, 2008 · N450FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02947Control Unit · malfunctionedNORMAL BEFORE T/O CHCK LIST, CLEARED FOR T/O RWY 77C DFW PASSING 40 KIAS GOT RED ECAM PARKING BRAKE SET. ABORTED T/O. PARKING BRAKE HANDLE CHECKED STOWED, BUT MOVED FURTHER DOWN 1/8 INCH /- NO DRAGGING BRAKI NG FELT ON INITIAL ROLL . HOWEVER CLEAR OF RWY BJul 17, 2008 · N407FE · Airbus A310 · Landing Gear Brake SystemSDR 08FDEA01918Floor Panel · damagedTHERE IS A BROKEN FLOOR FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 65, RBL 57 TO RBL 74. MATERIAL ID IS A402H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 6May 20, 2008 · N815FD · Airbus A310 · Fuselage Floor PanelSDR 08FDEA01839Panel · chafedLT WING FUEL PANEL ASSY 550 AT CLAMP RING HAS AREAS OF FRETTING. REMOVED & REPLACED THE CLAMP RING IAW SRM 57-20-16.May 13, 2008 · N815FD · Airbus A310 · Wing, Plate/SkinSDR 08FDEA01848Skin · delaminatedFOUND EVIDENCE OF A CRACK STARTING AT A FASTENER HOLE ON THE RIGHT EXTERNAL SIDE OF THE FUSELAGE SKIN BETWEEN STRINGER 21R & STRINGER 22R & FRAMES 40 TO 41. BLENDED AREA IN REF TO SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.061 IAW SRM 53-14-12. MATERIAL RMay 12, 2008 · N815FD · Airbus A310 · Fuselage Main, Plate/SkinSDR 08FDEA01826Panel · chafedNR 2 PYLON AFT LOWER FAIRING PANEL 485 AL; FWD UPPER RT ATTACH PLATE IS CHAFED ON THE INNER SURFACE. REMOVED ATTACH PLATE & INSTALLED A NEW ATTACH PLATE PER SRM 51-40-21 PARA 6. LOCATED & DRILLED HOLES PER SRM 51-40-21 PARA 6. ALODINED PER SRM 51-21-10. PMay 12, 2008 · N815FD · Airbus A310 · Nacelle/Pylon, Plate/SkinSDR 08FDEA01818Bleed Valve · faultedAT FL 370 BLEED VALVE NR 2 FAULTED. TURNED IT OFF AND OPENED BLEED CROSS FEED. APPROX 1 MIN LATER BLEED VALVE NR 1 FAULTED. TURNED IT OFF, TRIED RESETTING AND WOULD NOT RESET. DURING DESCENT, NR 1 BLEED VALVE DID RESET. BY 10,000 BOTH BLEED VALVES RESET May 11, 2008 · N450FE · Airbus A310 · Compressor Bleed ValveSDR 08FDEA01803Longeron · chafedNR 1 PYLON AFT LOWER FAIRING PANEL 475 AL; UPPER LT ATTACH ANGLE IS CHAFED ON THE INNER SURFACE. BLENDED CHAFED AREA PER SRM 51-77-10. FOUND TO BE OUT OF LIMITS PER SRM 54-55-51 TABLE 101 SHEET 1. ORIGINAL MATERIAL 0.071. MATERIAL REMAINING 0.047. MATERIAL REMay 8, 2008 · N815FD · Airbus A310 · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA01640Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RIGHT SIDE FUSELAGE SKIN BETWEEN FRAMES 16A TO 18 AND BETWEEN STRINGERS 41 AND 43 RT MEASURES 11 INCH BY 8.1. "REPAIR NOT IAW WITH SRM 53-12-12 FIG 201, REPAIR NOT APPLICABLE TO AREA. REMOVED AND REPLACED REPAIR IAApr 28, 2008 · N445FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 08FDEA01421Door Frame · gougedAFT PIT DOOR, LWR FWD CORNER, GOUGED. FOUND GOUGE TO BE OUT OF LIMITS IAW SRM 51-10-00. REMOVED AND REPLACED EDGE SECTION IAW SRM 51-40-21. FOR ADJUSTMENT AND CHECK SEE WC 41X5114ALI.Apr 16, 2008 · N425FE · Airbus A310 · Cargo/Baggage DoorsSDR 08FDEA01420Structure · gougedAFT PIT DOOR, NEAR AFT HOOK, STRUCTURE DENTED. NO DENTS ALLOWED IAW SRM 51-10-00. REMOVED AND REPLACED EDGE SECTION IAW SRM 51-40-21. FOR ADJUSTMENT AND CHECK SEE WC 41X5114ALI.Apr 16, 2008 · N425FE · Airbus A310 · Cargo/Baggage DoorsSDR 08FDEA01030Fitting · corrodedAVIONICS COMPARTMENT STRINGER 44L END FITTING IS CORRODED FWD OF FR 17. FITTING REMOVED IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MAT 0.067. MAT REMOVED 0.014. MAT REMAINING 0.053. OUT OF LIMITS IAW SRM 53-10-00 & DWG A53610607. REMOMar 18, 2008 · N425FE · Airbus A310 · Fuselage Main, Longeron/StringerSDR 08FDEA00944Fairing · dentedRT WING FAIRING 634 AT IS DENTED AND DELAMINATED. REPAIRED IAW SRM 57-20-35.Mar 14, 2008 · N425FE · Airbus A310 · Wing StructureSDR CA080213001Generator · cracked(CAN) DURING TROUBLESHOOTING FOR HIGH OIL CONSUMPTION ON THE APU, FOUND A 7 INCHES CRACK ON THE GENERATOR HOUSING. THE IDG WAS REPLACED AND THE UNIT WAS SENT TO THE VENDOR FOR INVESTIGATION. (TC NR 20080213001)Feb 8, 2008 · Airbus A310 · AC Generator-AlternatorSDR 08FDEA00334Tip Cap · crackedLT HORIZONTAL STAB TIP, TRAILING EDGE, CRACKED. REMOVED DAMAGE & APPLIED FIBERGLASS WET LAY UP IAW 55-14-11 FIGURE 203, DWG A551- 76100 & EA 6-5510-113014.Jan 30, 2008 · N416FE · Airbus A310 · Horizontal Stabilizer StructureSDR 07FDEA04967Switch · failedRECEIVED AN AUDIBLE "TOO LOW-GEAR" WNG ON SHORT FINAL. ALL GEAR INDS SHOWED GREEN/DOWN, SWITCHED TO POS1, REATTEMPT LANDING ALL SYS WORK NORMAL. ACN RELEASED FOR SVC. BRIEF INCREASED ALTITUDE AND TERRAIN AWARENESS." R&R MICROSWITCH 79GB IN REF TO MM 32-Nov 29, 2007 · N412FE · Airbus A310 · Landing Gear Position and WarningSDR 07FDEA04643Attach Fitting · crackedMAIN CABIN FR45 RT SIDE ADAPTER CRACKED OVER WING BOX REPLACED FR45 ADAPTER IAW SRM 51-40-21 P7 AND AMM 20-21-12.Oct 18, 2007 · N402FE · Airbus A310 · Fuselage Main, Attach FittingsSDR 07FDEA03515Beam · corrodedCORROSION ON FWD PAX DOOR 31 LT AT BEAM NR 1 OUT OF LIMIT REPAIR PERFORMED IAW SRM 52-11-00 FIG 213, APPROVED BY EA 6-5210-79568.Sep 11, 2007 · N432FE · Airbus A310 · Passenger/Crew DoorsSDR 07FDEA02998Control Unit · failedAFTER T/O, NR 5 SPOILER FAULTED W/RT WING NR 5 SPOILER INDICATING UP. RAN QRH PROCEDURE NO RELIEF. REMOVED AND REPLACED NR 1 AND 2 EFCU'S IAW A310-200 MM 27-61-34-4. OPS CK GOOD, PERFORMED GROUND SPOILER OPS TEST IAW 27-61-00-5. SUPPLIED FROM AIRBUS WEB SIAug 21, 2007 · N435FE · Airbus A310 · Drag Control SystemSDR 07FDEA02033Unknown · unknownSHORTLY AFTER T/O A/C ACTED AS IF THERE WAS GROUND SENSING PROBLEM, MALFUNCTIONS TO INCLUDE; ATS 1, PITCH TRIM 1, ALL THREE PITOT PROBE, CAPT TAT, BOTH PRESS CONTROLERS: GEAR WOULD NOT RETRACT SYS 1, A/P 1&2 INOP. INSTALLED NEW NOSE STRUT SENSOR 55GB PRMay 31, 2007 · N449FE · Airbus A310 · Auto Flight SystemSDR 07FDEA01858Skin · dentedLOWER EXTERNAL FUSELAGE SKIN HAS DENT BETWEEN FR 67 TO FR68 STRG 53R TO STRG 54R APPROX 4" REPAIRED IAW SRM 53-10-12 FIG. 225May 20, 2007 · N432FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 07FDEA01552Frame · corrodedCORROSION ON FRAME CONNECTION , C80, P`36 REPAIR PERFORMED BY REPLACEMENT OF CORRODED SECTIONS (A539-87426-212/-211) AND INSTALLING BOLTS NAS 6603-5 INSTEAD OF RIVETS, APPROVED BY EA 6-5319-99170 AND RAS/DAHAM/4020596/2006 ISSUE A.Apr 24, 2007 · N809FD · Airbus A310 · Fuselage Main, FrameSDR 07FDEA01529Longeron · corrodedHEAVY CORROSION ON LONGERON BETWEEN C11-C15 CABIN FLOOR STRUCTURE. REPAIR PERFORMED IAW SRM53-12-15 / FIG 207.Apr 20, 2007 · N809FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01477Attach Fitting · corrodedCORROSION ON PYLON NR 2 BEARING HOLE ON RIB 18 LOWER ATTACH FITTING. REPAIR PERFORMED BY REAM UP HOLE AND CHAMFER ON EACH SIDE IAW SB: A310-54-2021 AND EA 6-5451-103241.Apr 12, 2007 · N810FD · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01470Skin · dentedOLD DENT ON BULK CARGO DOOR LOWER LT CORNER WITH RAS/DATLS/0002170/2004 WITH TEMPORARY LIMIT OF ONE UNPRESSURIZED FERRY FLIGHT. PERMANENT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW. EA 6-5234-101283 AND RAS/DABRE/7006682/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Cargo/Baggage DoorsSDR 07FDEA01468Stringer · corrodedCORRODED STRINGER P44 LT AND RT, C16A-C17. STRINGER REPAIR PERFORMED IAW. SRM 53-12-14 / FIG.201. (RUN OUT FITTING INSTALLATION; PN A536-10607-206, -207)Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01466Floorbeam · corrodedCORRODED TOP CAP FLOORBEAM AT C33 LT. REPAIR PERFORMED BY SPLICING IAW SRM 53-10-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Floor BeamSDR 07FDEA01464Longeron · corrodedCORRODED LONGERON C11-C15A, Y-450. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01463Longeron · corrodedCORRODED LONGERON C12A-C14, Y1959. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG 207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01462Longeron · corrodedCORROSION ON LONGERON C11-C15A, Y-1456. REPAIR PERFORMED BY T-SPLICE REPAIR IAW SRM 53-12-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01460Seat Track · corrodedCORROSION ON SEAT TRACK, C15A-C19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 71-52-10.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01459Longeron · corrodedCORROSION FOUND ON LONGERON A536-11644-220, C11-C14, Y 770. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01457Panel · delaminatedDELAMINATION AT VERTICAL STABILIZER L/E PANEL NR 3. REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW. SRM 51-77-12 / FIG.211, APPROVED BY EA 6-5532-101302 AND RAS/DAHAM/4020826/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Vertical Stabilizer, Plate/SkinSDR 07FDEA01456Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Wing, Plate/SkinSDR 07FDEA01455Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Wing, Center Box
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