GE CF6-80A3

Service difficulty reports · 161

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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 engine_model_key = 'CF680A3'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA0239Repair · damagedSMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0328): FOUND REPAIR LOCATED RT FS 1605-1658 FR23-24. REPAIRS REQUIRES EJan 17, 2006 · N442FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04219Skin · crackedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPADec 10, 2005 · N424FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA04178Spar · corrodedLT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00541. REPAIRED LT UPPER IB THS SPAR CORD IAW A310-200 SRM 55-11-21 PARA 7.H PAGES 315TO, 320 FIG 211,213 AND 219 SHEET 2.Dec 8, 2005 · N423FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 05FDEA04166Spar · corrodedRT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00542. REPAIRED RT HORIZONTAL T/E UPPER SPAR CORD IAW SRM 55-11-21 PARA 7.H PAGES 315 TO 324 FIG SHEET 2 AND FIG 213.Dec 7, 2005 · N423FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 05FDEA04167Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00705. EVALUATION OF REPAIR REVEALED INCORRECT FASTENERS INSTALLED REPLACED REPADec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04168Panel · corrodedNOSE GEAR WELL, FWD WALL HAS 13 SPOTS OF LIGHT CORRODED AND SEVERAL SMALL SPOTS OF BARE METAL. REF N00747, REPAIRED NOSE LANDING GEAR BAY FORWARD PANEL BY REPLACING IAW REPAIR INSTRUCTION R53611077 AND NLG BAY PANEL REPLACEMENT, DWG R53610532. (K)Dec 7, 2005 · N423FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 05FDEA04169Repair · nonePREVIOUSLY REPAIR INSTALLED ON L/W NR 1 SLAT IB LEADING EDGE, SKIN BLIND FASTENER FLUSH. REPAIR WS RIB 2 TO RIB 3, NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00708. REPAIR EVALUATED AS GOOD IAW EA 6-5750-95471.Dec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04170Skin · corrodedBELLY OF AC RT SIDE FWD OF NR 2 PACK PORTABLE WATER SERVICE HAS CORROSION ON CUTOUT REF N00031. REPAIRED DAMAGE IAW EA 6-5330-94498 AND SRM 51-72-10 AND SRM 53-10-14.Dec 7, 2005 · N423FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA04171Doubler · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT EXT DOUBLER ABOVE AND AFT OF CAPT,S SIDE WINDOW, STA. 881 TO 904 FR 7 TO FR 8 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00696 REPAIR GOOD IAW EA 6-5330-95466.Dec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04146Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA, REF N00705. REPAIR REVEALED INCORRECT FASTENER INSTALLED REMOVED AND REPLACED REPAIR IAWDec 5, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04086Data Plate · missingDISCREPANCY (N0633 AND N0634): UNABLE TO VALIDATE MFG P/N AND S/N OF INSTALLED AIRFRAME LIFE LIMITED PARTS LT AND RT MLG RETRACT CYLINDERS DUE TO MISSING DATA PLATES. NSTALLED NEW DATA PLATE PER FEDEX DRWG. Z-20-001 REV. A AND AMM 11-22-32Dec 3, 2005 · N424FE · Airbus A310 · Placards and MarkingsSDR 05FDEA04087Repair · mismanufactured2PREVIOUS REPAIR INSTALLED AT LOWER FUSELAGE 6 O'CLOCK POSITION AT STA 771 TO STA 805, FR1 TO FR2. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUDec 3, 2005 · N424FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA04091Repair · mismanufacturedPREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE BELOW AOA SENSOR AT STA 1364 TO STA 1386, FR18 TO FR19, STR 39LT TO 44LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR Dec 3, 2005 · N424FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA04092Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 1923, FR35, STR 22LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR CONFORMS TO AN EXISTING FEDEX EDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04093Repair · unknownSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DIDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04094Repair · noneSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY Dec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA03982Roller Tray · corrodedRT OB MOST ROLLER TRAY AT FR 38.2 HAS CORROSION ON IB LEG FASTENER HOLE REF N 00466. REMOVED AND REPLACED ROLLER TRAY IAW SRM 53-10-15.Nov 28, 2005 · N423FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 05FDEA03984Repair · improperPREVIOUS REPAIRS ON MAIN DECK CARGO SEAT TRACK SPLICE FROM FR 58 TO 61 3RD TRACK LT OF CENTER LINE NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00725. FOUND REPAIR NOT IN CONFORMANCE OF SRM, 53-10-16 FIG 208 R7R REPAIR IAW SRMNov 28, 2005 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03985Repair · properPREVIOUS REPAIR 2 EA EXT DOUBLERS INSTALLED ON RT ELEVATOR IB UPPER SKIN NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00719. REPAIR IS IAW EA 6-2730-50500.Nov 28, 2005 · N423FE · Airbus A310203 · Elevator, Plate/SkinSDR 05FDEA04002Distributor Blk · malfunctionedVENT EXTRACT LOW FLOW RESET ONCE OK CAME ON DURING TAKEOFF ROLL. TRIPPED ATS LEVERS WITH HEAVY SMELL OF OVERHEAT.Nov 26, 2005 · N414FE · Airbus A310203 · Air Distribution SystemSDR 05FDEA03446Engine · leakingDURING CRUISE, NR 2 ENGINE TRIM LIGHT/ECAM ILLUMINATED NR 2 ENGINE, NOTICED N1 AND N2 INOP, OIL QUANTITY ZERO, OIL PRESSURE IN YELLOW, 14 PSI. ECAM ALERT FOR ENGINE SHUTDOWN, OIL PRESSURE ZERO. FLIGHT TIME ON ONE ENGINE -2 5 MINUTES. HYD LOW PRESS LIGHTS AOct 13, 2005 · N431FE · Airbus A310203 · Turbine Engine Oil SystemSDR 04FDEA02993Warning Light · illuminatedFUEL FILTER CLOG LIGHT ON T/O AT 60KTS. REJECTED T/O. ALL INDICATIONS NORMAL ON 60 PERCENT RUNUP FOR ENG ANTI-ICE. ECAM WARNING STOPPED STOPPED AS SOON AS POWER WAS REDUCED. I THINK IT WAS NR 1 ENG, BUT AM NO T POSITIVE. ENT BY: 001941 RPT BY: 119121 FAOct 25, 2004 · N410FE · Airbus A310 · Engine Fuel DistributionSDR 04FDEA02923Frame · dentedN00197, INCOMING CONDITION, JUST FORWARD OF FR 10 LT SIDE IS A DENT (2 INCH X 2 INCH X .090 INCH) WHICH IS OUT OF LIMITS IAW SRM TABLE 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER, FILLER IAW EA 6-5330-55382 AND SRM 51-71-70, EO-356-09-04-007-2/-4, DWG R536 Oct 12, 2004 · N410FE · Airbus A310 · Fuselage Main, FrameSDR 04FDEA02924Frame · dentedN00196 INCOMING CONDITION, JUST FORWARD OF FRAME 10 RT SIDE IS A DENT 1 INCH X .5 INCH X .050 INCH WHICH IS OUT OF LIMITS IAW SRM 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER AND FILLER C/W EA 6-5330-55381 AND SRM 51- 71-70, TECHNICAL REQUEST OE-356-09-Oct 12, 2004 · N410FE · Airbus A310 · Fuselage Main, FrameSDR 04FDEA02872Proximity Sensor · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLGOct 5, 2004 · N415FE · Airbus A310 · Landing Gear Position and WarningSDR 04FDEA02833Panel · damagedPANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02834Panel · damagedPANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02835Panel · damagedPANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02810Seat Track · crackedMAIN CABIN FR52 SEAT DUMMY TRACK (CLS ADAPTOR) AT TRACK 2R, 24 INCHES TO RT OF CTRIS, CRACKED UNDERNEATH AT BEND RADIUS APPROX 4 IN LONG. REMOVED AND REPLACED CLS ADAPTOR FR52 2R IN MAIN CABIN IAW SRM A310/200 51-40-21.Sep 23, 2004 · N410FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02724Seat Track · crackedMDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BENEATH LUGS) REMOVED DAMAGE AND FOUND TO BE CRACKED IAW SRM 51-73-10. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.Sep 17, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02689Floorbeam · corrodedAFT CARGO COMPARTMENT, BETWEEN FR 54 AND 54.2, FLOOR STRUCTURE RT SIDE, 3 AREAS OF CORROSION ON CLIP NUTS HOLE TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW A310 SRM 51-74-10, AND FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-15, TREATED PRIMED AND TOP COASep 16, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02691Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING ****Sep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02692Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D CSep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02693Floorbeam · crackedBULK CARGO COMPT FLOOR STRUCTURE ON FR67 AT RT SIDE CORNER UNDERNEATH NOTED CRACK. REMOVED AND REPLACED BEAM IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02694Seat Track · corrodedSEAT TRACK 0, SECTION BETWEEN FR73 TO FR80 HAS TWO DISCREPANT AREAS. TRACK 0 AT APPROX 12 INCHES AFT FROM FR 77 HAS 2 GOUGES INSIDE OF SCALLOPED AREA. TRACK 0 APPROX 10 INCHES AFT OF FR78 HAS CORROSION ON TOP OF TRACK AND IN SCALLOPED AREA. REMOVED CORROSIOSep 16, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02695Seat Track · gougedSEAT TRACK AT FR 36 AFT APPROX 8 INCHES IS GOUGED. BLENDED AREA PER A310 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS PER A310 SRM 53-10-16. REPAIRED BY REMOVING DAMAGED SECTION OF TRACK AND SPLICING IN A REPAIR SECTION PER A310 SRM 51-40-21 AND 53-10-16.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02696Adapter · crackedTRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02697Adapter · crackedTRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02698Floorbeam · crackedFWD CARGO FLOORBEAM STRUCTURE FR33 NOTED INDICATION OF CRACK. REMOVED DAMAGED AREA IAW A310 SRM 53-10-15, AND REPAIRED BY INSTALLING A DOUBLER IAW A310 SRM 53-10-15.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02678Seat Track · crackedMAIN CARGO DECK AT FRAME 47 BETWEEN TRACKS 1R AND 2R, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK AT FRAME 47 BETWEEN TRACKS 1R AND 2R IAW A310 SRM 51-40-21.**** S/D COMING ****Sep 14, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02679Seat Track · crackedDAMAGED SEAT TRACK ADAPTER AT FRAME 61 CENTER LINE REF EA 6-5320-81893. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21 AND EA 6-5320-81893. **** S/D COMING ****Sep 14, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02675Dummy Rail · crackedMCD AT FR 53 BETWEEN SEAT TRACKS 2L AND 3L, DUMMY TRACK IS CRACKED UNDERNEATH AT T-CAP RADIUS. REMOVED AND REPLACED CROSSBEAM, P/N A5381293420000 IAW A310 SRM 51-40-21.Sep 11, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02581Pan · corrodedREF. SNRM N00246 LWR FWD CARGO FR21 30 INCHES LT OF CENTER DATUM FLOOR CARGO ELECTRIC ROLLER PAN HAS CORROSION. REMOVED AND REPLACED WITH NEW ROLLER PAN IAW A310/200 SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02582Dummy Rail · crackedREF. SNRM N00261 MAIN DECK CARGO COMPT. AT FR 42 BETWEEN L1 AND L2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02583Dummy Rail · crackedMAIN DECK CARGO COMPT AT FR 40/41 BETWEEN R1 AND R2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02584Dummy Rail · crackedREF. SNRM N00257 MAIN DECK CARGO COMPT. AT FR 46 DUMMY TRACK IS CRACKED BETWEEN R1 AND R2 SEAT TRACKS. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02585Dummy Rail · crackedMAIN DECK CARGO COMPT. AT FR53 BETWEEN R1 AND R2 SEAT TRACK DUMMY TRACK IS CRACKED . REMOVED AND REPLACED DUMMY TRACK IAW A310-200 SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02586Dummy Rail · crackedMAIN DECK CARGO COMPT. AT FR 45 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02587Dummy Rail · crackedREF. SNRM N00259, MAIN DECK CARGO COMPT. AT FR 43 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02543Connector · corrodedNR 1 MLG DOOR WOULD NOT CLOSE ON GEAR RETRACTION. PUT GEAR DOWN IAW ECAM, RETURNED FOR LANDING. PERFORMED BITE CHECK OF PROX DET UNIT REF A310 M/M 32-31-71-4, RECEIVED BOX FAULT CODE (BOX LIGHT ON) CODE 64= 28VDC POWER SUPPLY NR 4 OR NR 3,SEE A310 TSM 32-Aug 22, 2004 · N442FE · Airbus A310203 · Electrical Connectors
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