GE CF6-80A3

Service difficulty reports · 161

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201009113345Cargo Track · crackedMAIN CARGO DECK FLOOR SUPPORT STRUCTURE FR 54.2 RT SIDE NR 5 SEAT TRACK HAS 3.5 INCH CRACK ON LOWER PART OF SEAT TRACK. REMOVED DAMAGED TRACK SECTION BETWEEN FR 54.2 AND FR 55/58 AND INSTALLED NEW REPLACEMENT TRACK SECTION AT TRACK NR5 RT IAW SRM 51-75-10,53Sep 11, 2010 · N425FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009113346Skin · dentedL 2 DOOR EXTERIOR SKIN 20.5 INCHES FROM AFT END OF DOOR SKIN,12.5 INCHES FROM BOTTOM OF DOOR SKIN HAS SM DENT,10 MM W X .014 IN DEEP CUT OUT DAMAGED SECTION OF EXTERIOR DOOR SKIN AT FR 75 BETWEEN STR 24 LT AND STR 25 LT AND INSTALLED REPAIR EXTERNAL DOUBLER Sep 11, 2010 · N425FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201008213075Stringer · misrepairedPREVIOUS STR REPAIR LOCATED IN AFT CARGO ON STRINGER 52 LT BETWEEN FRAMES 62 TO 63 HAS 1 EACH STRINGER REPAIR SECTION FROM FR 60 TO 63 MEASURING 43IN LONG AND 1EA REPAIR SPLICE 7.6 IN LONG. PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201, Aug 21, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008213076Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 45 LT BETWEEN FR 60 AND FR 61 HAS 1 EA STRINGER REPAIR SECTION FROM FR 55/58 TO 62 MEASURING 51IN LONG AND 1EA REPAIR SPLICE 8IN LONG. PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201,Aug 21, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008213077Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 47 LT BETWEEN FR 59 AND FR 60 HAS 1EA STRINGER REPAIR SECTION FROM FR 55/58 TO 60 MEASURING 29.4IN LONG AND 1EA REPAIR SPLICE 7.9 INCH LONG. PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-10-14, FIAug 21, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008213078Skin · misrepairedPREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT NOSE SKIN BETWEEN RIB 13 AND 15 JUST BELOW UPPER GIRDER MEASURES 5.4 X 5.8 INCH PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 57-43-11, FIG 202, SHEET 3, PAGES 209 TO 213 AND PAGE 216 DUE TO 64 EA BLIND FASAug 21, 2010 · N425FE · Airbus A310203 · Leading Edge DevicesSDR FDEA201008203064Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 51 RT BETWEEN FRAMES 60 TO 62 HAS 1 EA, STRINGER REPAIR SECTION MEASURING 15.1 INCH LONG AND 2 EA. REPAIRS SPLICES 8.1 INCH LONG PREVIOUSLY REPAIRS DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201, DUE TAug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203065Stringer · misrepairedPREVIOUS STRINGER REPAIR IN FWD CARGO ON STR 45 RT BETWEEN FR 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.8 INCH LONG AND THE STR SECTION WAS CUT ONLY TO REMOVE FOR ACCESS ORIGINAL STR INSTALLED PREVIOUS REPAIR DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201 ONAug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203068Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STR 47 RT BOTTOM FRAMES 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.9 INCH LONG AND THE STRINGER SECTION WAS CUT ONLY TO REMOVE FOR ACCESS , ORIGINAL STRINGER INSTALLED. PREVIOUS REPAIR DETERMINED NOT TO BE IAW SAug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203069Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STR 46 RT BETWEEN FRAME 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.8 INCH LONG AND THE STRINGER SECTION WAS CUT ONLY FOR ACCESS ORIGINAL STRINGER INSTALLED PREVIOUSLY INSTALLED REPAIR DETERMINED TO NOT IAW SAug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203070Seat Track · misrepairedPREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR1 Y0 BETWEEN FRAMES 61 TO 62, HAS 1 EA REPAIR ANGLE ON LT SIDE UPPER FLANGE MEASURING 9.3 INCHES LONG X 1.7 IN TALL AND 1 EA UPPER FLANGE REPAIR FILLER FOR CUT MEASURING 3.1 INCHX 0.900 IN PREVIOUSLY INSTALLEDAug 20, 2010 · N425FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008203071Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 LT BETWEEN FRAMES 66 TO 67 HAS 1 EA STRINGER REPAIR SECTION FROM FR 65 TO 67 MEASURING 33.5 INCH LONG AND 1 EACH REPAIR SPLICE 8.2 INCH LONG PREVIOUSLY INSTALLED REPAIR WAS DETERMINED NOT TO BE IAAug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203072Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 55 R/H BETWEEN FR66 AND FR67 HAS 1 EACH STRINGER REPAIR SECTION FROM FR 65 TO 67 MEASURING 32 INCH LONG AND 1 EACH REPAIR SPLICE 8.1 INCH LONG. PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-1Aug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203073Stringer · misrepairedPREVIOUS STR REPAIR LOCATED IN BULK CARGO ON STR 54 R BETWEEN FR 66 AND FR67 HAS 1 EA STR REPAIR SECTION FROM FR 65 TO FR 67 MEASURING 32 IN LONG AND 1EA REPAIR SPLICE 8.1 INCH LONG PREVIOUS INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201Aug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008203074Stringer · misrepairedPREVIOUS STR REPAIR LOCATED IN AFT CARGO ON STR 46 LT BETWEEN FRAMES 61 TO 62 HAS 1EA STR SECTION FROM FR 55/58 TO 62 MEASURING 71.7 INCH LONG AND 1EA REPAIR SPLICE 7.9 INCH LONG. PREVIOUS REPAIR WAS DETERMINED NOT TO BE IAW SRM 53-10-14, FIG 201, PAGES 203 Aug 20, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008112937Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK 4 LT HAS 3 EA AREAS OF CORROSION ON SCALLOPS AND FLANGE, ABOUT 30 SQ IN BETWEEN FR 74 AND FR 76. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK, FABRICATED REPLACEMENT SECTION OF SEAT TRACK, 4 LT BETWEENAug 11, 2010 · N425FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008112938Attach Angle · crackedNR 1 PYLON-TO-ENGINE FWD ATTACH MOUNT OTBD UPPER ATTACH ANGLE IS CRACKED. REMOVED BLEED AIR DUCT, LOWER NR 1 PYLON TO GAIN ACCESS. R & R NR 1 PYLON OTBD FWD ATTACH MOUNT, UPPER ATTACH ANGLE SHEET IAW SRM 51-40-21. REINSTALLED BLEED AIR VALVE IAW AMM 20-21Aug 11, 2010 · N417FE · Airbus A310222 · Nacelle/Pylon, Attach FittingsSDR FDEA201008112939Skin · delaminatedNR 2 RT WING SPOILER LOWER SURFACE T/E IS DEBONDED AT THE OTBD HALF. REPAIRED DEBOND OF T/E ON NR2 SPOILER BY INJECTING AND RIVETING AREA IAW SRM 57-70-00 AND EA 6-5750-136689, " WINGS - RT NR2 SPOILER T/E DELAMINATED".Aug 11, 2010 · N417FE · Airbus A310222 · SpoilersSDR FDEA201007012302Skin · corrodedRT ELEVATOR LWR SURFACE CTR SPLICE HAS CORROSION 8 IN FWD FROM AFT EDGE APPROX 1.5 SQ IN APPROX STA ER21. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND LWR SURFACE CTR SPLICE OUT OF LIMITS IAW SRM 55-10-00. REMOVED DAMAGE, FABRICATED REPAIR PARTSJul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201007012303Skin · corrodedRT ELEVATOR UPPER SURFACE HAS APPROX 1.5 SQ IN OF CORROSION AT APPROX. ER36 1 IN. FWD OF AFT EDGE REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND UPPER SURFACE 1 IN FWD OF AFT EDGE, OUT OF LIMITS IAW SRM 55-10-00 FABRICATED REPAIR PARTS AND INSTALLJul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201007012305Floorbeam · corrodedMDCC FLOORBEAM HAS CORROSION ON UPPER SURFACE AT FR 14 6IN. BETWEEN SEAT TRACK 3L AND 4L. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND CROSSBEAM SECTION OUT OF LIMITS IAW SRM 51-74-10 AND SRM 53-10-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201007012311Floorbeam · crackedMAIN DECK FLOORBEAM FWD FACE HAS 0.188 INCH CRACK , ON FR 38 , 67 INCHES FROM CTR LINE, LT SIDE. TRIMMED OUT DAMAGE AREA IAW SRM 53-10-15, FIG 201, NDT CHECK IAW NTM 51-10-08. FOUND CRACK EXTENDS TO 1.0 INCH. CUT OUT CRACK DAMAGE AREA IAW SRM 53-10-15, FIG Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201007012312Floor Support · corrodedMDCC SEAT TRACK 5L HAS A 4 SQ INCH AREA OF CORROSION BENEATH FLOOR PANEL FR 16A. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-10-15 FIG 101 FOUND TO BE OUT OF LIMITS . REPLACED SEAT TRACK 5L , AT FR 16A. IAW SRM 51-40- 21 AND 51-72-10.Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201007012313Skin · corrodedRT ELEVATOR LWR SURFACE SKIN HAS CORROSION 56 INCHES FROM OTBD END, 6 INCHES FWD OF AFT EDGE APPROX 5 SQ IN TOTAL , APPROX ER 34 REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10 , FOUND LOWER SURFACE OUT OF LIMITS IAW SRM 55-10-00. FABRICATED REPAIR PARTS AND INSTAJul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201006141986Seat Track · corrodedSEAT TRACK 6R AT FRAME 47 HAS 1 HOLE WITH EXPOSED METAL WITH CORROSION PRESENT ON TOP AND BOTTOM OF MOUNT HOLE. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-16. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 205.Jun 14, 2010 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006141994Seat Track · corrodedCORROSION ON SEAT TRACK RT SIDE MAIN UPPER DECK CARGO FR 16 TO FR 18 TRACK NR 4 REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK NR 4 RT, FABRICATED REPLACEMENT PART IAW DWG 53610798 AND REPLACED SEAT TRACK NR 4 RT SECTION BETWEEEN FR 16 AND FJun 14, 2010 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006141995Fitting · corrodedAVIONICS COMPT FR 15A TO FR 17,STR 44 RT HAS CORROSION ALONG VERT LEG AND BASE. REMOVED LEVEL 1 CORROSION. R & R 2 EA FITTINGS TO FRAME ATTACHMENT AT FR 15A AND FR 17, STR 44RT IAW SRM 51-40-21. FITTING P/N'S A5361060720793 AND A5361060720501.Jun 14, 2010 · N403FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201006041822Skin · delaminatedLT INBD FLAP T/E AT MIDSPAN HAS 2EA DISBONDED AREAS ON TOP AND BOTTOM SKINS APPROX 24" (INCHES) LENGTH TOTAL. REMOVED PREVIOUS REPAIR DOUBLER, LT INBD FLAP T/E UPPER SKIN MIDSPAN IAW SRM 51-77-11. CUT OUT DISBONDED UPPER SKIN IAW SRM 57-53-12, PAR 13 B(5). CJun 4, 2010 · N404FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201005291734Beam · corrodedAFT CARGO DOOR LOWER TORQUE BOX, UPPER LONGITUDINAL BEAM IS CORRODED ON INSIDE SURFACE, JUST FWD OF FRAME 60. (APPROX 2 SQ. INCHES) R & R AFT CARGO DOOR LOWER DOOR SILL BEAM IAW DWG R53970189 FROM FRAME 59R TO 64R.May 29, 2010 · N404FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201005291735Floorbeam · corrodedAFT CARGO FLOORBEAM FRAME 60, 45" RT OF CTRLINE, UPPER CHORD LOWER SURFACE IS EXFOLIATED AROUND FASTENER HOLE APPROX 4 SQ IN TOTAL. R & R FR 60 CROSSMEMBER SEC BEAM RT AT AFT CARGO DOOR SILL BEAM IAW SRM 51-72-10.May 29, 2010 · N404FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201005291736Skin · chafedEXTERNAL FUSELAGE SKIN AT FR 38 AND STR 42R HAS 1 EA TOOL MARK SURROUNDING FASTENER 1 IN LENGTH X 1 IN WIDTH X 0.007 IN DEPTH. TOOL MARK BLENDED, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. DAMAGE CUTOUT AND WAS NDT INSPECTED IAW NTM 51-10-08 AND NO CRACKS FMay 29, 2010 · N404FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201005251625Stringer · corrodedAFT CARGO BILGE STR 47R HAS CORROSION ON VERTICAL LEG JUST FWD OF FRAME 59 APPROX 2 SQ IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 TABLE 6. REPAIRED STRINGER 47R BETWEEN FRAME 59 AND 58 IAW May 25, 2010 · N404FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201005251626Stringer · corrodedAFT CARGO BILGE STR 50 R HAS CORROSION ON VERTICAL LEG FROM FRAME 55/58 TO FRAME 59 APPROX 20 SQ IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, TABLE 102 DAMAGE CODE C. REPAIRED STR 50 R May 25, 2010 · N404FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201005251627Stringer · corrodedAFT CARGO BILGE STR 48 R HAS CORROSION ON VERTICAL LEG AND TOP LEDGE FROM FR 55/58 TO FR 59, APPROX 8 SQ IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10 PAGE 205. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 TABLE 102 DAMAGE CODE C. REPAIRED STRMay 25, 2010 · N404FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201005231617Stringer · corrodedAFT CARGO COMPT BILGE,FRAME RF64-FR65,STR 51R HAS CORROSION ON VERTICAL LEG. REMOVED CORROSION ON STR 51R BETWEEN FR64-FR65 CHECK FOUND TO BE OUT OF LIMIT IAW SRM 53-10-00, FIG 106, TABLE 2 R & R DAMAGE STR 51R, BETWEEN FR FR64-FR65 IAW SRM 53-10-14 PARA 2 May 23, 2010 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201005161546Seat Track · corrodedUPPER DECK SEAT TRACK 4R HAS CORROSION ON INBD FLANGE AT FRAME 26, 12". (APPROX 2 SQ IN TOTAL). R & R SEAT TRACK AT FRAME 26, 12" 4R IAW SRM 53-10-16 PG 244.May 16, 2010 · N404FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005161547Seat Track · corrodedMDCC LT SEAT TRACK Y450, 3" FWD OF FRAME 80 THERE IS ONE AREA OF CORROSION INSIDE THE SCALLOPED AREA (APPROX .7500 SQ INCH). ONE AREA OF CORROSION ON TOP OF A SCALLOP EAR (APPROX .5 SQ. INCH.). REPAIRED SEAT TRACK LT Y450 USING SPLICING METHOD BETWEEN FRAME May 16, 2010 · N404FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005161548Floorbeam · corrodedBULK CARGO PIT FLOOR , FRAME 66 AT CTR LINE FLOORBEAM TOP SURFACE CORRODED. R & R FLOORBEAM AT FR 66 IAW SRM 51-72-10 PAGE 1-2 AND SRM 53-17-15, PAGE A68, FIG 11.May 16, 2010 · N404FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201005161549Floorbeam · corrodedBULK CARGO PIT FLOORBEAM FR 64 TOP L/E OF FLANGE CORRODED 1.5 SQ INCH. LT OF CTR LINE. REMOVED CORROSION IAW SRM 51-74-10 , FOUND OUT OF LIMITS IAW SRM 53-10-00, FIG 104, TABLE 102. REPAIRED FLOORBEAM IAW SRM53-10-15, FIG 207May 16, 2010 · N404FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201005151544Structure · crackedNR 1 PYLON LT FWD SIDE SKIRT HAS 0.125" CRACK AFT EDGE UPPER CORNER OF LT FAN COWL. STOP DRILLED CRACK IAW SRM 54-56-10 FIG 201, NDT VERIFIED NO CRACK INDICATIONS IAW NTM 51-60-00 BEYOND STOP DRILL. FABRICATED, LOCATED, AND DRILLED DOUBLER IAW SRM 54-56-May 15, 2010 · N404FE · Airbus A310203 · Nacelle/Pylon, Main FrameSDR FDEA201005151545Skin · crackedNR1 PYLON OTBD LATERAL WALL AT RIB 4A PRECOOLER HAS 1 EA CRACK. REPAIRED NR1 PYLON PRECOOLER LATERAL WALL AT RIB 4A IAW SRM 54-52-31, PB201, FIG 202.May 15, 2010 · N404FE · Airbus A310203 · Nacelle/Pylon, Plate/SkinSDR FDEA200901090106Filter · dirtyNR 2 ENG FUEL FILTER CLOG LIGHT & ECAM INDICATION ON CLIMB-OUT PASSING 2000 FT. POWER REDUCED & ECAM INDICATIONS WENT AWAY. TRIED ADVANCING THROTTLE AGAIN & ECAM INDICATIONS BACK ON. REMOVED & INSPECTED NR 2 ENGINE FUEL FILTER FOR CONTAMINATION. FOUND SMJan 9, 2009 · N429FE · Airbus A310203 · Engine Fuel DistributionSDR FDEA200804161426Skin · damagedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LOWER CTR FUSELAGE SKIN MANHOLE FITTING CUTOUT AT FRAMES 23 TO 24 AND BETWEEN STRINGERS 48 RT TO 52 RT, MEASURES 24.4 IN X 15 IN WITH 4 EA INTERNAL POCKET REPAIRS BETWEEN STRINGERS 54 LT TO 49 RT REPAIR NOT IAW SRMApr 16, 2008 · N445FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA200804161427Seat Track · misrepairedPREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT -Y1456 BETWEEN FRAMES 62 TO 63, HAS 2 EACH REPAIR SPLICES MEASURING 7 IN LONG X 3 IN TALL AND 1 EA REPAIR SECTION 52 IN LONG FROM FRAME 65 TO BETWEEN FRAMES 62 AND 63 REPAIR NOT IAW SRM REQUIREMENTS.REMOApr 16, 2008 · N445FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200804161428Rib · corrodedTHE RIB 5 FWD BORE ON THE LT MLG IS CORRODED ON THE INSIDE, FOUND AFTER BUSHING WAS REMOVED. THE MAX DIAMETER OF 4.8405 HAS BEEN REACHED, REMOVED LEVEL 1 CORROSION, AND REPAIRED LT MLG RIB 5 IAW EA 6-5710-118108. THIS IS A REPAIR WITH NO ASSIGNED PN.Apr 16, 2008 · N445FE · Airbus A310203 · Wing, Rib/BulkheadSDR 08FDEA00800Engine · vibrationCLIMBING THROUGH FL 320 TO FL 350 WITH ALL CONDITION NORMAL, ACFT SHUDDERED AND SWERVED SLIGHTLY, THEN BEGAN CONTINUOUS THUMPS, BOTH AUDIBLE AND CLEARLY FELT THROUGH AIRFRAME. THERE WERE NO ECAM ADVISORIES, BUT NR 1 ENGINE N1 DECREASED TO APPROX 60 PERCENT. Mar 9, 2008 · N423FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR 07FDEA02435Main Bearing · leakingDIVERTED - PIT AT FL340 NOTICED A FAINT BURN ODOR. THIS WAS FOLLOWED BY A ECAM [MAIN DECK CARGO LOOP FAULT] W/ASSOCIATED LOOP "A" LIGHT AFT. 15-20 SECONDS LIGHT EXTINGUISHED. NEXT LOOP "A/B" LIGHTS ILLUMINATED W/RED SMOKE (AFT) ILLUMINATED FOLLOWED BY LOOP Jul 11, 2007 · N414FE · Airbus A310203 · Turbine Engine Oil SystemSDR 06FDEA03606Control Unit · failedAUTOBRAKES WORKED FINE TIL TOP OF DESCENT, WITH GEAR HANDLE NEUTRAL TRIED TO ARM (MED) AUTOBRAKES. GREEN PN CAME ON FOLLOWED IMMEDIATE W/AUTO BRAKES INOP. TRIED SEVERAL RESETS. GOC DIRECTED KMSP RETURN DUE TO SHORT DLH RWY. BSCU SHOWED CODE FOR ALT SERVO Oct 10, 2006 · N445FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 06FDEA0237Placard · correctA/C DATA PLATE SHOWS DATE OF MFG AS 9 JAN 1985. RECORDS SHOW DATE F MFG AS 26 OCT 1984 THERE APPEARS TO BE A CONFLICT. VERIFIED AIRCRAFT DATAPLATE DAY OF MFG TO BE 9 JAN 1985. AIRCRAFT RECORDS NOTIFIED.Jan 17, 2006 · N442FE · Airbus A310 · Placards and MarkingsSDR 06FDEA0238Repair · correctSMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0324 FOUND REPAIR LOCATED LT FS1067AND FS1091 FR 12 AND FR12A EXT DOJan 17, 2006 · N442FE · Airbus A310 · Aircraft Structures
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