N664FE

Service difficulty reports · 307

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 = 'N664FE' 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 08FDEA03235Skin · dentedLEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. UPON FURTHER INVESTIGATION THE DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. FLAP SKIN WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00; PG 108. REPAIRED LOWER SKIN IAug 4, 2008 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03244Skin · gougedRIGHT WING INBD FLAP LOWER T/E SKIN IS GOUGED 7' FROM THE INBD END. REMOVED GOUGE IAW SRM 51-73-10. ORIGINAL MATERIAL 0.028 IAW SRM 57-50-00. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013. FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. REPAIRED AREA IAAug 4, 2008 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03242Skin · dentedRIGHT WING INBD FLAP LOWER SKIN HAS SEVERAL DENTS. SMOOTHED DENTS IAW SRM 51-73-10. ALL DENTS EXCEPT RIB 7. ORIGINAL MATERIAL IS 0.028. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013; FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. RIB 7 DENT 0.049 DEPTH.Aug 4, 2008 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03241Skin · dentedRIGHT WING INBD FLAP UPPER SKIN IS CREASED 3' FROM THE OUTBD END. SMOOTHED DENT IAW SRM 51-73-10. DENT DEPTH 0.049. ORIGINAL MATERIAL THICKNESS IS 0.031. NO MATERIAL LOSS NOTED, FOUND TO BE WITHIN LIMITS IAW SRM 57-50-00, FIG 101. DENT DIAMETER 1.25 INCH, Aug 4, 2008 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03234Skin · dentedLEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-73-10. FLAP SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00, PG 108. CUT OUT THE DAMAGED AREA IAW A300-600 SRAug 4, 2008 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03247Web · damagedCABIN RIGHT SIDE SUPPORT WEB IS CRACKED BETWEEN FRAME 38 AND FRAME 38.1; RBL 90 INCH CREASE BEAM AREA. REMOVED BROKEN SUPPORT WEB, LOCATED AND DRILLED THE NEW SUPPORT WEB IAW A300-600 SRM 51-40-21. ALODINED HOLES IN THE WEB IAW A300-600 SRM 51-21-10. PRIMEAug 4, 2008 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA03246Web · crackedRIGHT SIDE SUPPORT WEB IS CRACKED BETWEEN FRAME 38.1 AND FRAME 58.2, RBL 90 INCH, CREASE BEAM AREA. REPLACED CABIN RIGHT SIDE SUPPORT WEB BETWEEN FRAME 38.1 AND FRAME 38.2; RBL 90 IN REF TO TO AIRBUS A300-600 SRM 53-14-15.Aug 4, 2008 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA03209Retainer · gougedAFT CARGO DOOR CUT-OUT AFT SIDE SEAL LAND IS NICKED AND GOUGED IN SEVERAL PLACES AT BOTH TOP AND BOTTOM CORNERS. REMOVED AND REPLACED THE AFT CARGO DOOR SEAL LANDS (3EA) IAW A300-600 SRM 51-40-21.Aug 1, 2008 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA03213Attach Fitting · crackedTHE MAIN CARGO DECK FLOORBEAM TO FRAME AFT ATTACH LINK IS CRACKED AT FRAME 12A, RBL 79". REMOVED AND REPLACED THE FITTING IAW AS300-600 SRM 51-40-21.Aug 1, 2008 · N664FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 08FDEA03194Floorbeam · bentAFT CARGO COMPARTMENT, CABIN FLOORBEAM AT FRAME 60, LOWER FLANGE IS BENT AT APPROX BL -Y 1830. COMPLIED WITH EA 6-5310-123366 "FUSELAGE - C60 CROSSBEAM, PERMANENT REPAIR OF THE LOWER FLANGE DEFLECTION AT APPROX -Y 183.0.Jul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA03195Door Frame · crackedTHE AVIONICS COMPARTMENT DOOR HINGE FRAME IS CRACKED THROUGH, DOOR 121B, RIGHT HINGE. REMOVED AVIONICS COMPARTMENT DOOR TO FACILITATE THE REPAIR IAW AMM 52-41-14-4. REPAIRED THE CRACKED ANGLE IAW SRM 51-41-14; FIG 201. REMOVED AND REPLACED BRAKE FORM SECTIJul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR 08FDEA03193Stiffener · bentAFT CARGO DOOR CUTOUT, UPPER FWD CORNER, WEB PANEL IS BENT. REMOVED THE SURROUNDING STRUCTURE TO ACCESS THE DAMAGE IAW SRM 51-40- 21; PARA 5; 6 AND 7. REMOVED DAMAGED AREA IAW SRM 51-71-30; FIG 201. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-71-30;Jul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA03198Seat Track · bentTHE MAIN CABIN SEAT TRACK AT FRAME 30, LBL 40 INCH HAS A BENT FLANGE. REMOVED DAMAGED SEAT TRACK PER SRM 51-41-21. LOCATED AND DRILLED TRACK PER SRM 53-10-16. INSTALLED SEAT TRACK AND SPLICES PER SRM 51-41-02, SRM 53-10-16 AND DWG A53781911. APPLIED CIC PJul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03197Seat Track · corrodedMAIN CARGO SEAT TRACK HAS LIGHT CORROSION IN THE CENTER OF THE TRACK AT FRAME 78; RBL 18 INCH. REMOVED CORROSION; BLENDOUT IS WITHIN LIMITS PER A300-600 SRM 53-10-16. TREATED, PRIMED AND PAINTED AREA PER A300-600 SRM 51-23-10.Jul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03196Seat Track · corrodedMAIN CARGO SEAT TRACK IS CHAFFED AT FRAME 78; BL "0". REMOVED CORROSION; BLENDOUT IS WITHIN LIMITS PER SRM 53-10-16. TREATED, PRIMED AND PAINTED AREA PER SRM 51-23-10.Jul 31, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03169Floor Panel · damagedMAIN CABIN FLOOR PANEL NR 242 HK IS CRACKED. FABRICATED NEW FLOORBOARD NR 242 HK IAW FEDEX DWG SRZ 25-005; REV "G".Jul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03179Floorbeam · crackedMAIN CABIN FLOORBEAM AT FRAME 30 IS CRACKED AT THE VERTICAL STIFFENER BETWEEN Y- 450 AND Y-953. REPAIRED FLOORBEAM IAW SRM 53-10-15; FIG 212.Jul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA03175Seat Track · crackedMAIN CABIN SMALL LATERAL SEAT TRACK AT FRAME 30; LBL 30 FLANGE IS CRACKED. REMOVED CRACKED LATERAL SEAT TRACK IAW SRM 51-40-21; PARA 7. RECEIVED NEW LATERAL SEAT TRACK, PO 617060.2. LOCATED AND DRILLED THE LATERAL SEAT TRACK IAW SRM 51-40-40. INSTALLED NEWJul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03176Seat Track · crackedMAIN CABIN CROSS SEAT TRACK AT FRAME 29; LBL 30 IS CRACKED. REMOVED THE CROSS SEAT TRACK AT FRAME 29 IAW A300-600 SRM 51-40-21. LOCATED AND DRILLED AND COUNTERSUNK HOLES FOR THE NEW CROSS SEAT TRACK P/N A5370617920000, PO 627372.1 IAW A300-600 SRM 51-40-10Jul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03177Seat Track · crackedMAIN CABIN CROSS SEAT TRACK AT FRAME 30; LBL 30 IS CRACKED. REMOVED AND REPLACED THE ADAPTER ASSEMBLY IN REF TO SRM 51-40-21; PARA 7. APPLIED CIC PROTECTION IN REF TO AMM SUP 51-22-00-0.Jul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03178Seat Track · crackedMAIN CABIN CROSS SEAT TRACK AT FRAME 28, LBL 35 IS CRACKED. REMOVED CROSS SEAT TRACK AT FRAME 28, RBL 35 IAW SRM 51-40-21, PARA 7. DRILLED AND COUNTERSUNK HOLES FOR THE NEW CROSS SEAT TRACK ADAPTER P/N A5378193720100, PO 627374.2 IAW SRM 51-40-21, PARA 7. AJul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03173Seat Track · damagedMAIN CABIN SMALL LATERAL SEAT TRACK AT FRAME 30; LBL 56 INCH HAS A BROKEN SCALLOP. REMOVED SEAT TRACK ADAPTER IAW SRM 51-40-21. DRILLED AND COUNTERSUNK A NEW SEAT TRACK ADAPTER P/N A5378193620200, PO 627374.3 IAW A300-600 51-40-40. INSTALLED SEAT TRACK ADAPJul 30, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03141Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCHES TO 97 INCHES IS BROKEN. THIS SDR WAS GENERATED IN ERROR. FOR DETAILS SEE SDR TRACKING NR 08-3140.Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03147Floorboard · damagedCABIN FLOOR BOARD HAS A DENT FROM FRAME 26 TO 28 AND RBL 47 INCHES TO 67 INCHES. FABRICATED NEW FLOORBOARD NR 232 VH IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03145Floor Panel · damagedMAIN DECK FLOORBOARD NR 232 TG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 TG IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03144Floor Panel · damagedMAIN DECK FLOOR BOARD NR 232 YG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 YG IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03143Floor Panel · damagedMAIN DECK FLOORBOARD, RIGHT SIDE NR 252 CF IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 CF IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03142Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 30; LBL 30 INCH IS CRUSHED. FABRICATED NEW FLOORBOARD NR 231 YG IAW DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03140Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCH TO 97 INCH IS BROKEN. FABRICATED NEW FLOORBOARD NR 241 LK IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03138Floor Panel · damagedMAIN CABIN FLOOR PANEL BETWEEN FRAMES 40 TO 43 AND LBL 57 INCH TO 77 INCH IS BROKEN. FABRICATED NEW FLOOR BOARD NR 241 TH IAW DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA03134Seat Track · gougedCABIN SEAT TRACK HAS A GOUGE BETWEEN FRAMES 27 AND 28, RBL 87 INCH. REMOVED THE DAMAGED SECTION OF SEAT TRACK AND INSTALLED THE NEW SECTION AND SPLICES IN REF TO SRM 53-10-16; FIG 201; 201A AND SRM 51-40-21, PARA 7; AND DWG A53781941. ALODINED, PRIMED AND TJul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03137Seat Track · wornMAIN CABIN SEAT TRACK BETWEEN FRAMES 43 AND 44 AT RBL 77 INCH HAS WORN SCALLOPS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DWG A53610365 AND SRM 51-40- 21. FABRICATED SEAT TRACK IAW DWG A53610365.Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03139Seat Track · wornMAIN CABIN SEAT TRACK BETWEEN FRAMES 49 AND 47 AT RBL 57 INCH HAS WORN SCALLOPS. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21. RECEIVED NEW SEAT TRACK P/N A5327400500053, PO 617932.1 IAW A300-6Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03146Seat Track · gougedCABIN SEAT TRACK HAS A GOUGE BETWEEN FRAMES 27 AND 28, RBL 37 INCH. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM FRAME 27 - 31 IAW SRM 51-40-21, PARAGRAPH 7 AND SRM 53-10-16, FIG 201/201A, SRM 51-21-10 AND SRM 51-23-10. WORKED IN CONJUNCTION WITH SNRJul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03133Seat Track · corrodedMAIN CABIN SEAT TRACK AT RBL 17 INCH HAS CORROSION BETWEEN FRAMES 47 AND 48. REMOVED OLD SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW A300-600 SRM 57-40-21. MATERIAL ID FOR THE NEW TRACK IAW A300-600 SRM 53-15-16. FABRICATED A NEW SEAT TRACK IAW DWG A53812Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03126Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 30 AND FRAME 31; RBL 37 INCHES. REMOVED CORROSION IAW AMM 51-74-10-8; PGS 1-2. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED DAMAGED SEAT TRACK, DRILLED IAW SRM 51-40-21 PARA 7 AND SRM 53-10-16 FIG 201/201Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03135Seat Track · damagedCABIN SEAT TRACK IS DAMAGED AT FRAME 38.1, RBL 67. SEAT TRACK FOUND TO BE OUT OF LIMITS PER A300-600 SRM 53-10-16. REMOVED THE DAMAGED TRACK PER A300-600 51-41-21. MATERIAL ID FOR THE NEW TRACK P/N A5327400500053, PO 617932.1. MATERIAL ID FOR THE SPLICES Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03132Seat Track · corrodedMAIN CABIN SEAT TRACK AT APPROX RBL 37 INCH; BETWEEN FRAMES 43 AND 44 HAS CORROSION. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK IAW SRM 51-40-21. IN REF TO SRM 53-15-16 AND SM NSA348076. CUT SEAT TRACK AND DRILLED Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03131Seat Track · corrodedMAIN CABIN SEAT TRACK AT APPROX RBL 37 INCH, BETWEEN FRAMES 41 AND 42 HAS CORROSION IN THE TRACK. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. TOOL USED T8492F. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21. MATERIAL ID OR NEW SEAT TRACK Jul 29, 2008 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03095Floor Support · corrodedMAIN CARGO DECK FLOOR SUPPORT HAS CORROSION 4 INCH AFT OF FRAME 13; LBL 31 INCHES. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.079. MATERIAL REMOVED 0.013. MATERIAL REMAINING 0.066. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVEJul 28, 2008 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA03040Door · damagedNR 2 ENGINE INBD REVERSER LOWER DOOR FLANGE IS DAMAGED. EVALUATED 6 WORN AREAS. 2 HAD MATERIAL LOSS OF .005 AND 2 EA HAD MATERIAL LOSS OF 0.010. THESE 4 AREAS ARE WITHIN LIMITS REF MRA CMM 78-32-02. 1 AREA HAD A MATERIAL LOSS OF 0.045 & 1 AREA HAD 100% MATJul 24, 2008 · N664FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA04894Processing Unit · inoperativeGEAR FAILED TO RETRACT ON TAKEOFF. INDICATION 3 GREEN, 3 RED "UNLKD" ON LOWER AND UPPER PANEL. MAX AIRSPEED 225 KIAS THE DET SYS 2 WAS UNABLE TO RETRACT THE GEAR. DID NOT TRY THE DET SYS 1. REMOVED BOOGIE BEAM PROX SENSOR PROX MOUNT REMOVED FOR ACCESS OF 1Nov 21, 2007 · N664FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 07FDEA00661Ram Air Turb · unwanted deployDURING WALKAROUND, FOUND RAT DEPLOYED, NOT SURE OF WHEN (INFLIGHT OR TAXI IN) RAT DEPLOYED. FLT CREW UNAWARE, CONTROLS WERE STILL SAFETIED IN C/P. VISUALLY INSP RAT FOR DEFECTS PER AMM 29-25-00-6. NO DEFECTS NOTED AT THIS TIME. STOWED RAT PER AMM SUP 29-25Mar 6, 2007 · N664FE · Airbus A300F4605R · Hydraulic System, AuxiliarySDR 07FDEA00325Bleed Valve · leakingREPORT OF NR 1 FIRE INDICATION ON LANDING ROLLOUT AT KROC. AML LOGPAGE FROM FLIGHT CREW TO FOLLOW REFER TO WRI 72-00-9550 FOR ACTION TAKEN ON THIS ITEM. BLEED AIR TO NR 1 ENG DUCTING. FOUND BLEED VALVE VENT FITTING LEAKING EXCESSIVELY, VERIFIED THIS TO BEFeb 5, 2007 · N664FE · Airbus A300F4605R · Compressor Bleed ValveSDR 07FDEA00072Uplock · damagedON GEAR RETRACTION ECAM INDICATED GEAR DOOR FAULT WITH NOSE GEAR DOOR. REMOVED AND REPLACED RT NOSE GEAR DOOR UPLOCK ASSY PER A300 AMM 32-31-14-4. COMPLETED STEPS UP TO PAGE 407. COMPLETED RIGHT HAND NOSE DOOR UPLOCK INSTALLATION, AND REINSTALLED NOSE DJan 10, 2007 · N664FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 06FDEA2548Floorbeam · crackedDURING THE PRIMARY INSPECTION [FEDEX TASK CARD 61S5043CP] A 0.90 INCH LONG CRACK WAS FOUND ON THE FR65 FLOOR CROSS BEAM (P/N A53275350200). THE CRACK IS LOCATED NEAR AN EXISTING REPAIR (REF FEDEX EA 6-5310-87889 FIGURE 1 OF THIS EA PROVIDES THE LOCATION AND DJul 12, 2006 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 06FDEA2438Support Fitting · crackedMDCC UNDER FLOOR STRUCTURE SEAT TRACK VERTICAL SUPPORT FITTING INBD LWR EAR LUG CRACKED, FS 48 LBL 57.5Jul 2, 2006 · N664FE · Airbus A300* · Fuselage Main, Attach FittingsSDR 06FDEA2437Intercostal · crackedFOUND AFT FUSELAGE BETWEEN C86-87 RBL 30 FRAME INTERCOASTAL UPPER CHORD CRACKED.Jul 2, 2006 · N664FE · Airbus A300* · Fuselage Miscellaneous StructureSDR 06FDEA2410Rib · crackedRT WING FIXED L/E RIB LWR CHORD IS CRACKED, LOCATED OUTBD OF KRUGER FLAP ACTUATOR.Jun 26, 2006 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR 06FDEA2409Dummy Rail · damagedDUMMY SEAT TRACK NR 5R UPPER SCALLOP LUG BROKEN AT FR39, RBL77.Jun 26, 2006 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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