N650FE

Service difficulty reports · 219

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N650FE' AND registry_match = 'registration'
  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 FDEA201011194427Valve · failedREJECTED TAKEOFF AT 60 KNOTS DUE TO ECAM MESSAGE- NR2 REVERSER PRESSURIZED. R & R NR 2 ENG PRESS REGULATING AND SHUTOFF VALVE REF MM 78-31-05-04.DUE TO REJECTED TAKEOFF. C/W HIGH PWR ENG RUN REF JRH CH 7 CKS GOOD.Nov 19, 2010 · N650FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201006182048Cadc · failedNO AIRSPEED ON CAPT'S PFD AT 80KT CALL. REJECTED TAKEOFF & COMPLETED CK. MTP SHOWED NO FAULTS. ADC BITE TEST IAW 34-10-00-5, CKD OK. REMOVED PITOT LINES FROM PRIMARY AND STBY PITOT PROBES AND BLEW AIR THROUGH PROBES NO BLOCKAGE NOTED. PERFORMED THE PITOT SJun 18, 2010 · N650FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR FDEA200910173598Uplock · damagedDURING GEAR RETRACTION THE NOSE GEAR DOOR DID NOT CLOSE. COMPLIED WITH THE ECAM AND QRH AND RETURNED TO MEM LT NOSE GEAR DOOR UPLOCK FOUND DAMAGED. REMOVED AND REPLACED LT NOSE GEAR DOOR UPLOCK ASSY 1257 IAW AMM 32-31-14-4. LK CKS OK. CKS OK IAW AMM 32-32Oct 17, 2009 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA200910093523Flap System · malfunctionedFLAPS WOULD NOT EXTEND BEYOND APPROX 17-18, SLATS, SYS 1 AND 2 FAULT ON OVERHEAD. NO SFPI INDICATOR. CHECKED SYS LOCKOUT AND ASYM BRAKE, NO FAULTS, RAN FLAPS TO BOTH DIRECTIONS AND FLAPS OPS CHECKS OK. SFCC HAD NO FAULTS DURING TESTS USING ELECTRIC PUMP ANDOct 9, 2009 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200910083514Jackscrew · wornGOT FLAP SYS 1 AND 2 FAULT, FLAPS STOPPED AT 15 DEG AT DESTINATION, SHORT RWY, RETRACTED FLAPS, DIVERTED. FLAPS FAULTED AT 30 DEG AT ALTERNATE. REMOVED AND REPLACED NR 2 SCREWJACK ASSY AMM 27-54-22-4. FLAPS OPS CK GOOD. REINSTALLED ALL FAIRINGS. COMPLETEDOct 8, 2009 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200905121635Transmitter · leakingECAM ALERT HYD SYS LOW QTY ON BLUE SYSTEM TURNED OFF BLUE PUMP AND SPOILER 7 ,4 AND 1. PLACED IN WORK PENDING FURTHER INVESTIGATION. FOUND BLUE HYDRAULIC PRESSURE TRANSMITTER LEAKING. REMOVED AND REPLACED BLUE SYS HYD PRESSURE TRANSMITTER IAW AMM 29-32-13-May 12, 2009 · N650FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA200902110506Flap System · unknownWHEN FLAPS WERE SELECTED TO FLAPS 20, FLAPS STUCK AT 15, GOT ASSOCIATED ECAM ADVISORY AND BOTH SYS 1 AND SYS 2 AMBER FAULT LIGHTS ILLUMINATED ON OVERHEAD PANEL. SFPI AMBER FLAP LIGHT WAS NOT ON. ACCOMPLISHED ASSOCIATED AMBER ECAM ITEM AND QRH PROCEDURES, NFeb 11, 2009 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200812185226Downlock Switch · out of adjustUNSAFE NOSE GEAR INDICATION ON INITIAL LOWERING OF THE GEAR HANDLE. COMPLIED WITH QRH PROCEDURES AND HAND CRANKED THE GEAR. STILL HAD AN UNSAFE INDICATION AFTER ALL STEPS WERE COMPLETED. EXECUTED HIGH "G" MANEUVER AND NOSE GEAR CAME DOWN SHORTLY THEREAFTDec 18, 2008 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA200812125136Uplock · failedON FINAL NLG BOTH SYSTEMS SHOWED UNSAFE, GO AROUND TO HOLDING TO USE GRAVITY EXTEND PROCEDURES. THREE GREEN SAFE LIGHTS AFTER PROCEDURE WITH NORMAL LANDING, AND TOW IN CREW STATED GOT 3 UNLOCK (AMBER) RED LIGHT AND 2 GREEN LOCK LIGHTS ON MLG`S ON BOTH SYSTEMSDec 12, 2008 · N650FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA200810154372Jackscrew · damagedAFTER TAKEOFF, UPON ATTEMPTING TO RAISE THE FLAPS, FLAPS FAULTED. COMPLIED WITH ECAM AND RED TABS AND RETURNED TO KATL. UPON CONFIG FOR LANDING FLAPS DID GO TO 40 FOR A NORMAL LANDING. FLAPS THEN RETRACTED TO 0 UPON LANDING. REMOVED AND REPLACED NR 6 RT FOct 15, 2008 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR 08FDEA04372Flap System · malfunctionedREPEAT, AFTER TAKEOFF, UPON ATTEMPTING TO RAISE THE FLAPS, FLAPS FAULTED. COMPLIED WITH ECAM AND RED TABS AND RETURNED TO KATL. UPON CONFIG FOR LANDING FLAPS DID GO TO 40 FOR A NORMAL LANDING. FLAPS THEN RETRACTED TO 0 UPON LANDING.Oct 15, 2008 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200810094293Proximity Sensor · failedON TAKEOFF LANDING GEAR RETRACTED. THEREAFTER ECAM DISPLAYED LANDING GEAR RETRACTION FAULT. SELECTED POSITION DET 1 AND 2 GEAR RETRACTION FAULT REMAINED ON ECAM. FLAPS WOULD NOT RETRACT, STAYED AT 15/20 ONCE LANDING GEAR DOWN ALL FLAP OPERATION RETURNED TO Oct 9, 2008 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 08FDEA04293Proximity Sensor · failedON TAKEOFF LANDING GEAR RETRACTED. ECAM DISPLAYED LANDING GEAR RETRACTION FAULT. SELECTED POSITION DET 1 AND 2 GEAR RETRACTION FAULT REMAINED ON ECAM. FLAPS WOULD NOT RETRACT, STAYED AT 15/20 ONCE LANDING GEAR DOWN ALL FLAP OPERATION RETURNED TO NORMAL. LOST Oct 9, 2008 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA200810084278Limiter · malfunctionedFLAPS STUCK AT 20 DEG WOULD NOT RETRACT. FOLLOWED RED TABS FLAPS DID EXTEND TO 30/40 ON LANDING FLAPS RETRACTED AFTER LANDING. BOTH SYS 1 AND SYS 2 FLAP FAULT LIGHT ON IN FLIGHT. PERFORMED SERVICING OF RT WING JACKSCREWS AND TORQUE LIMITER PER AMM 12-13-27Oct 8, 2008 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR 08FDEA04278Limiter · malfunctionedFLAPS STUCK AT 20 DEG. WOULD NOT RETRACT. FOLLOWED RED TABS FLAPS DID EXTEND TO 30/40 ON LANDING FLAPS RETRACTED AFTER LANDING. BOTH SYS 1 AND SYS 2 FLAP FAULT LIGHT ON IN FLT. PERFORMED SERVICING OF RT WING JACKSCREWS AND TORQUE LIMITER PER AMM 12-13-27-0.Oct 8, 2008 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR 08FDEA04284Target · out of alignmentON T/O LDG RETRACTED. ECAM DISPLAYED LDG RETRACTION FAULT. SELECTED POS DET 1 AND 2. GEAR RET FAULT REMAINED ON ECAM. FLAPS WON'T RETRACT, FROM 15/20 ONCE GEAR DOWN ALL FLAP OPS NORMAL. LOST ALL AUTOMATION ON GEAR RET RETURNED TO NORMAL WITH GEAR EXTENSIONOct 7, 2008 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 08FDEA04264Target · misalignedON CLIMB, LANDING GEAR RETRACTED. ECAM DISPLAYED LANDING GEAR RETRACTION FAULT. SELECTED POSITION DET 1 AND 2 GEAR RETRACTION FAULT REMAINED. FLAPS WOULD NOT RETRACT, STAYED AT 15/20, ONCE LANDING GEAR DOWN ALL FLAP OPERATION RETURNED TO NORMAL. LOST ALL AUTOct 7, 2008 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 08FDEA03871Floor Panel · delaminatedUPPER CARGO FLOORBOARD IS BULGED AT THE TRACK FITTING (251 QH) REMOVED DAMAGED FLOOR PANEL 251 QH IAW SRM 51-40-21. MATERIAL ID FOR THE NEW PANEL A402H144 IAW DWG SRZ 25-005; REV "G". FABBED A NEW FLOOR PANEL 251 QH IAW DWG 25-005; REV "G". INSTALLED PANEL Sep 15, 2008 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03775Panel · chafedLEFT WING LOWER T/E PANEL 575 FB LAND AND AIRFRAME MATING SURFACE IS CHAFFED AND HAS BARE METAL. REMOVED CAMLOCKS AND SEAL TO FOM IAW SRM 51-40-00. FABRICATED A REPAIR DOUBLER IAW EA NR 6-5720-123627. PREPPED PANEL SKIN AND DOUBLER FOR BONDING IAW SRM 51-21Sep 8, 2008 · N650FE · Airbus A300F4605R · Wing, Plate/SkinSDR 08FDEA03618Flap Track · wornRIGHT WING FLAP FAIL SAFE BOLT PIN PLATING IS WORN, (FWD BOLT). REMOVED AND REPLACED THE RIGHT WING INBD FLAP FAIL SAFE BOLT REF AMM 57-20-24-4.Aug 28, 2008 · N650FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03628Fitting · corrodedRUST AT THE R-1 DOOR SLING ADAPTER HOLES (2 PLACES). REMOVED AND REPLACED HOIST FITTING (2EA) IAW FE A300-600 SRM 51-40-21.Aug 28, 2008 · N650FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 08FDEA03552Frame · gougedBULK CARGO DOOR, LOWER SECTION, FRAME IS GOUGED. REMOVED AND REPLACED THE BULK CARGO DOOR LOWER FRAME SECTION IAW SRM 51-72-10 AND SRM 51-40-21.Aug 22, 2008 · N650FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA03556Web · crackedNR 1 ENGINE OUTBD T/R FWD UPPER WEB IS CRACKED. FABBED DOUBLER IAW A300-600 MRA CMM 78-32-02. MATERIAL ID 2024-T3, 0.063. LOCATED HOLES IAW A300-600 MRA CMM 78-32-02. ALODINED, PRIMED AND INSTALLED DOUBLER IAW A30-600 MRA CMM 78-32-02. MATERIAL PO NR 614Aug 22, 2008 · N650FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA03555Web · crackedNR 1 ENGINE INBD T/R FWD UPPER WEB IS CRACKED. STOP DRILLED CRACK; NDT'D AREA FOR CRACK PROPAGATION AT THE CRACK END IAW A300 NTM 51-90-00 PT 9. FABBED A NEW DOUBLER IAW MRA CMM 78-32-01. TREATED DOUBLER AND AREA IAW A30-600 SRM 51-1-23 AND MRA CMM 78-32-01Aug 22, 2008 · N650FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA03554Floor Panel · damagedMAIN CABIN FLOORBOARD 241 BF HAS DAMAGE ON THE FWD CORNER. FABRICATED NEW FLOOR PANEL 241BF, POTTED EDGES, COMPLETED CURE AND LIGHTLY SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED THE PANEL IAW DWG SRZ 25-005; REV "G".Aug 22, 2008 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03553Floor Panel · damagedMAIN CABIN FLOORBOARD 241 DF IS DAMAGED ON THE UPPER SURFACE. FABRICATED NEW FLOOR PANEL 241DF, POTTED EDGES, COMPLETED CURE AND LIGHTLY SANDED EDGE POTTING, INSTALLED INSERTS. APPLIED NON-SKID AND PART PARKED THE PANEL IAW DWG SRZ 25-005; REV "G".Aug 22, 2008 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03487Attach Fitting · crackedMAIN CARGO FLOOR SUPPORT AND WEB, LOWER OUTBD ATTACH FITING IS CRACKED AT FRAME 48, FLOOR LOCATION -Y 1456. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-40-21; PARA 10-B.Aug 18, 2008 · N650FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 08FDEA03489Floorbeam · crackedMAIN CABIN FRAME 48 SUB-FLOOR AT Y 145.6 FLOORBEAM WEB LOWER INBD MOUNT IS CRACKED. REMOVED AND REPLACED THE FITTING IAW A300-600 SRM 51-40-21;PARA 10-B.Aug 18, 2008 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA03488Attach Fitting · crackedMAIN CARGO FLOOR SUPPORT WEB, LOWER OUTBD ATTACH FITTING IS CRACKED AT FRAME 49; FLOOR LOCATION -Y 145.6. REMOVED AND REPLACED ATTACH FITTING IAW A300-600 SRM 51-40-21; PARA 10-B.Aug 18, 2008 · N650FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 08FDEA03485Structure · damagedAFT CARGO DOOR BETWEEN LOCKING HOOKS NR 4 AND 35 WEB IS PUNCTURED. REMOVED DAMAGE PER A300-600 SRM 52-32-11. ACCOMPLISHED BHEC INSPECTION OF THE DAMAGED AREA PER NTM 51-10-01. NO DEFECTS NOTED. GENERATED RFTS NR N650FE -1-31253. RECEIVED FINAL RFTS N650FEAug 18, 2008 · N650FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA03409Pitot Line · leakingSTAND-BY PITOT SYSTEM FAILS THE LEAK TEST. TROUBLE SHOOT SYSTEM IAW AMM 34-10-00. FOUND DAMAGED UNION AT THE STANDBY PITOT TUBE. REMOVED AND REPLACED THE UNION IAW 34-11-15-4. TESTED AND LEAK CHECKED THE STANDBY PITOT SYSTEM IAW AMM 34-10-00-5. NO LEAKAug 13, 2008 · N650FE · Airbus A300F4605R · Pitot/Static SystemSDR 08FDEA03375Connector · disconnectedWHILE PERFORMING THE RESIDUAL CABIN PRESSURE WARNING SYSTEM OPS CHECK THE LIGHT ON THE L-1 DOOR DOES NOT COME ON. FOUND LIGHT 73 WN DISCONNECTED ON THE L-1 DOOR. RECONNECTED THE CONNECTOR. OPS CHECK WAS GOOD IAW A300-600 AMM 52-73-15.Aug 11, 2008 · N650FE · Airbus A300F4605R · Door System WiringSDR 07FDEA05058Pin · shearedBOLT/PIN BROKEN ON RT MLG AT DRAG LINK/MAIN STRUT ASSY, ATTACH'S SUPPORT ASSY FOR DOWN LOCK SENSORS. REMAINDER OF SHEARED OFF PIN EXTRACTED FROM GEAR ASSY BY LAX MACHINE SHOP EMP'S NR 213560/519905. REPLACED BOLT FOR RT MAIN GEAR TORQUE LINK DOWN LOCK SENSORDec 14, 2007 · N650FE · Airbus A300F4605R · Main Landing GearSDR 07FDEA05051Pin · shearedF/O TAT FAILED, CAUSING SECONDARY LOSS OF NR 2 PITCH TRIM, NR 2 CABIN PRESS REGULATOR 34-62 0508. NR 2 INTERMITTENT FOUND PROX SYS FAULTING SENSOR. REF:MDIS 32 10 0511, BOLT/PIN BROKEN ON RT MLG AT DRAG LINK ATTACHMENT FOR GEAR SENSORS. REMOVED AND REPLACDec 13, 2007 · N650FE · Airbus A300F4605R · Rate of Climb IndicatorSDR 04FDEA01618Floor Support · corrodedAT FRAME 51 BETWEEN SEAT TRACKS 1 AND 2L FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-00, FABRICATED NEW PART IAW DWG A53812989, INSTALLED FABBED PART IAW SRM 53-40-21.Jun 4, 2004 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 04FDEA01568Seat Track · corrodedNR 2 RT TRACK BETWEEN FR 45 & 54, LEVEL 2 CORROSION IN TRACK, AND FR 47 & 48, 2EA AREAS, FR 46 & 47 2EA AREAS OF LEVEL 2 CORROSION, FR 48 & 49 2EA AREAS BROKEN RIVETS AND BARE METAL ALONG FLANGE. REMOVED DAMAGED TRACK, FABBED NEW TRACK AND INSTALLED IAW SRM'SJun 2, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01567Seat Track · chippedSEAT TRACK 5L 4 INCHES FWD OF FRAME 23 HAS CHIPPED SCALLOP. REMOVED DAMAGED SECTION OF TRACK, FABBED REPAIR SPLICE IAW SRM 53-10-16, AND INSTALLED SPLICE IAW SRM'S 51-10-08, 51-35-00, AND 51-40-21.Jun 2, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01551Floorbeam · crackedFWD CARGO OVERHEAD FLOORBEAM AT FR 27, 27 INCHES RIGHT OF CENTERLINE ON THE FWD SIDE IS CRACKED ON UPPER VERTICAL LEG. REWORKED CRACK AT FR 27 IAW A300-600 SRM 51-27-00, NDT VERIFIED CRACK, REMOVED CRACK IN WEB IAW 53-10-15 P207. NDT VERIFIED NO CRACK FOUND.Jun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 04FDEA01550Seat Track · gougedMAIN CABIN TRACK 3R: 1) A WORN SCALLOP AT FR 24. 2) GOUGES ON TOP OF SCALLOPS AT FR 22. 3) GOUGED SCALLOPS AT FR 20 TO 21. BLENDED AREAS 2 AND 3 IAW A300-600 SRM 51-73-10, WITHIN LIMITS PER SRM 53-10-16. FOR AREA 1 AT FR 24 REF EA 6-5320-78360 FOR REPAIR,Jun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01549Seat Track · corrodedSEAT TRACK 3R HAS 6 EA AREAS OF CORROSION. 1) 8 INCHES FWD OF FR27. 2) 4 INCHES FWD OF FR27. 3) 6 INCHES AFT OF FR30. 4) 8 INCHES AFT FR32. 5) 10 INCHES AFT OF FR33. 6) 4 INCHES AFT OF FR38.1. REMOVED CORROSION 6 AREAS IAW A300-600 SRM 53-10-16, AREA 3 Jun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01545Seat Track · corrodedBETWEEN FR 28 AND FR 29 AT TRACK 2L THERE IS AREAS OF CORROSION (MAIN CARGO) AND FROM FR 30 TO FR 38, 12 EA AREA OF CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MEASURED MAT'L LOSS, CHECKED MAT'L LIMITS PER SRM 53-10-16 FIG 102, REPAIRED SEAT TRACKJun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01544Seat Track · corrodedMAIN DECK CARGO COMP BETWEEN FR 45 AND FR 54, L4 SEAT TRACK HAS 6 AREAS OF CORROSION. 1) 6 INCHES AFT OF FR 45. 2) 12 INCHES AFT OF FR47. 3) 5 INCHES FWD OF FR49. 4) 2 INCHES FWD OF FR50. 5) 7 INCHES FWD OF FR 53. 6) 12 INCHES AFT OF FR53. REMOVED CORROJun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01543Seat Track · corrodedSEAT TRACK 1 (CENTER TRACK) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 1) 10 INCHES AFT OF FR 71 AT PRODUCTION BREAK. 2) BETWEEN FR 73 & FR 74. 3) BETWEEN FR 75 & FR76. 4 & 5) BETWEEN FR 75 & 76. 6) 2 INCHES AFT OF FR 78. REMOVED DISCREJun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01542Seat Track · corrodedSEAT TRACK 4R HAS 1 EA AREA ON AND UNDER SCALLOP WITH CORROSION 10 INCHES AFT OF FR 74. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MAT'L LOSS OUT OF LIMITS. REMOVED DAMAGED SECTION SEAT TRACK, LOCATED DRILLED, AND INSTALLED SEAT TRACK SECTION IAW A300-600 Jun 1, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01516Seat Track · corrodedSEAT TRACK 5R FROM 8 INCHES FWD OF FR 45 TO FR 54 HAS 3 EA AREAS OF CORROSION, ONE AREA OUTBOARD FLANGE WITH GOUGES AT FR 47, AND 7 AREAS OF ELONGATED HOLES WITH GOUGES ON INBOARD FLANGE BETWEEN FR 48 TO FR 51. REMOVED CORROSION AND GOUGES IAW A300-600 SRM 51May 28, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01515Seat Track · corrodedTRACK 3L SECTION FROM 10 INCHES AFT OF FR 71 TO 10 INCHES FWD OF FR 74 HAS 4 AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS, AT FR 72, BETWEEN FR 72 AND 73, 2 INCHES AFT OF FR 74. REMOVED SEAT TRACK, FABRICATED REPLACEMENT TRACK, TREATED, PRIMED AND TOP CMay 28, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01514Track · corrodedMAIN CABIN CROSS TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R HAS ONE EA AREA OF CORROSION. REMOVED AND REPLACED CABIN CROSS TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R IAW A300-600 SRM 51-72-10.May 28, 2004 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 04FDEA01513Seat Track · corrodedSEAT TRACK NR 4L SECTION FROM FR 74 TO FR 80/82 HAS 3 EA AREAS OF CORROSION, INCLUDING ON AND UNDER SCALLOPS, BETWEEN FR 74 AND FR 75, 10 INCHES AFT OF FR 75, 3 INCHES FWD OF FR 76. REMOVED CORROSION FROM SEAT TRACK, MAT'L LOSS AT AREAS AND ARE OUT OF LIMITS May 28, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01448Seat Track · corrodedUPPER FUSELAGE STA 1870 FR 28 I/B SIDE OF TRACK 5R UNDER FLOOR PANEL 232VH LEVEL 1 CORROSION 1.2 L X 1.0 INCH W. DEPTH UNDERMINE WITHOUT BLENDOUT, ALSO FR 29 LIGHT SURFACE CORROSION 1 EA AREA, BETWEEN FR 30 & 31, 1 EA AREA LIGHT SURFACE CORROSION, FR 38 AND FMay 25, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01441Seat Track · corrodedSEAT TRACK 3R SECTION (10 INCHES FWD OF FR 74 TO JUST AFT OF FR 80/82) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 6 INCHES FWD OF FR 74, BETWEEN FR 74 AND FR 75, BETWEEN FR 75 AND 76, 1 INCH FWD OF FR 76, 1 INCH AFT OF FR 76, AND 7 INCHES AFMay 25, 2004 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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