N717FD

Service difficulty reports · 155

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 = 'N717FD' 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 FDEA201107262948Frame · crackedCRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON CABIN LT SIDE FRAME 40 CENTER TENSION BOLT HOLE 'B'. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.Jul 26, 2011 · N717FD · Airbus A300F4622R · Fuselage Main, FrameSDR FDEA201107262947Frame · crackedCRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT. OPEN HOLE INSP ON CABIN LT SIDE FRAME 40 LOWEST TENSION BOLT HOLE 'C'. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 26, 2011 · N717FD · Airbus A300F4622R · Fuselage Main, FrameSDR FDEA201107262946Hinge · crackedAVIONICS COMPARTMENT DOOR, FOUND RT HINGE CRACKED. PERFORMED REPAIR PER A300-600 SRM 52- 41-14 FIG 201 REV 75. AVIONICS COMPARTMENT DOOR REMOVED AND RE-INSTALLED AFTER REPAIR COMPLETED PER AMM 52-41-14-04 REV 52.0 AVIONICS COMPARTMENT DOOR ADJUSTMENT TESJul 26, 2011 · N717FD · Airbus A300B4622R · Fuselage, Door HingeSDR FDEA201107212875Floor Panel · corrodedBULK CARGO FLOOR PANEL 162DF FOUND CORRODED. FLOOR PANEL REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ 25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 21, 2011 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201107212874Floor Panel · corrodedBULK CARGO FLOOR PANEL 162CF FOUND CORRODED. FLOOR PANEL REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ-25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 21, 2011 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201107212873Floor Panel · corrodedBULK CARGO FLOOR PANEL 161CF FOUND UNDER CORRODED. REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ 25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Jul 21, 2011 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201107192800Frame · corrodedAFT CARGO DOOR HANDLE FWD FRAME FOUND CORROSION. REMOVED AND NEW FRAME INSTALLED PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Jul 19, 2011 · N717FD · Airbus A300F4622R · Cargo/Baggage DoorsSDR FDEA201107082611Frame · damagedDURING ACCOMPLISHMENT OF EO 6-5310-7-5017 A5 PART 4, HOLES A-N AT FRAME 47 RT FOUND TO BE IN OVERSIZED CONDITION. ACCOMPLISHED REPAIR PER EA 6-5310-143612, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Jul 8, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107082610Frame · damagedDURING ACCOMPLISHMENT OF EO 6-5310-7-5017 A5 PART 3, HOLES A-N AT FRAME 47 LT ARE FOUND TO BE IN OVERSIZED CONDITION. REPAIRED PER EA 6-5310-143612, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Jul 8, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107052574Roller Tray · corrodedAFT CARGO ROLLER TRAY AT ABOUT 140 MILLIMETER TO THE LT AND RT FROM THE MIDDLE AT FRAME 60 FOUND CORROSION AROUND FASTENER AREA. REMOVED ASSY AMM 25-52-24-04, REV 52.0. NEW TRAY REWORKED (FABRICATED) IAW DWG NR A25772926 ISSUE F. FABRICATED NEW PART, INSTJul 5, 2011 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201107042562Fitting · corrodedENGINE NR 2 PYLON FORWARD MOUNT FORWARD LT BOLT BORE HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 6-5450-152689.Jul 4, 2011 · N717FD · Airbus A300B4622 · Nacelle/Pylon, Attach FittingsSDR FDEA201107042561Fitting · nickedENGINE NR 2 PYLON ENGINE FORWARD MOUNT FORWARD RT BOLT BORE HOLE FOUND NICKED. REPAIRED AS PER EA 6-5450-152689.Jul 4, 2011 · N717FD · Airbus A300B4622 · Nacelle/Pylon, Attach FittingsSDR FDEA201107042560Fitting · corrodedENG NR 1 PYLON FORWARD MOUNT FITTING LT AFT BOLT BORE HOLES FOUND WITH CORROSION. REPAIRED AS PER EA 6-5450-152690.Jul 4, 2011 · N717FD · Airbus A300B4622 · Nacelle/Pylon, Attach FittingsSDR FDEA201107012520Frame · crackedDURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 16TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012519Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 15TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012518Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND 13TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012517Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 11TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012516Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 10TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012515Frame · crackedCABIN - DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 8TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012514Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 5TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012513Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 17TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012512Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012511Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. REPAIRED IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012510Frame · damagedDURING HFEC OPEN HOLE INSPECTION ON LT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE TOP 2ND HOLE DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012509Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 5TH HOLE COUNT FROM THE TOP WITH THE CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REV112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012508Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 49, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107012507Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 48, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292491Frame · damagedCABIN - DURING HFEC OPEN HOLE INSP ON LT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE TOP 3RD HOLE DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292490Frame · crackedCABIN DURING OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 5TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292489Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 13TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292488Frame · crackedCABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 7TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292487Frame · crackedCABIN - DURING HFEC HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 49, FOUND THE 17TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292486Frame · crackedCABIN - DURING HFEC INSP ON RT REINFORCE BASES JUNCTION AT FRAMES 49, FOUND THE 5TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106292485Frame · crackedDURING HFEC HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 48. FOUND THE 5TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 29, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106282458Attach Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSP ON FORWARD CARGO DOOR ACTUATOR ATTACH FITTING, FOUND CRACKED. REMOVED AND NEW FITTING INSTALLED PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Jun 28, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, Attach FittingsSDR FDEA201106282464Floor Support · corrodedFLOOR SUPPORT BETWEEN FRAME 12A TO FRAME 13A Y953, CORRODED. REMOVED AS PER SRM 51-74-00 REV 75, MATERIAL REMOVED 0.053", MATERIAL REMAINED 0.025", MATERIAL THICKNESS 0.078" AND FOUND OUT OF LIMIT AS PER SRM 53-12-15 FIG 101 REV 75. DAMAGED FLOOR SUPPORT REJun 28, 2011 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201106282462Floor Support · corrodedMAIN DECK - LOWER OF LAVATORY UNIT BETWEEN FRAME 11 TO FRAME 12A AT FLOOR SUPPORT, CORROSION. REMOVED AS PER SRM 51-74-10 REV 75. MATERIAL REMOVED 0.061", MATERIAL REMAINED 0.017", MATERIAL THICKNESS 0.078" AND FOUND OUT OF LIMIT AS PER SRM 53-12-15 FIG 101Jun 28, 2011 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201106282477Frame · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT REINFORCE BASE JUNCTION AT FRAME 48 FOUND THE HOLE NR 17 FROM TOP WITH CRACKED INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 28, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106282476Frame · damagedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LT REINFORCE BASE JUNCTION AT FRAME 49 FOUND THE FIRST HOLE FROM TOP DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jun 28, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201106212352Stringer · corrodedFORWARD CARGO AT ABOUT FR 38.2 STRINGER 45L FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-10-14 FIG 201 REV 75. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 21, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR FDEA201102020455Line · leakingLOSS YELLOW HYD SYS PRESSURE AND QUANTITY. R & R YELLOW PRESSURE HOSE IAW SPM CHAP 20 AND AMM 12-12-29-00 .Feb 2, 2011 · N717FD · Airbus A300B4622 · Hydraulic System, MainSDR FDEA200904081222Pickup · malfunctionedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF A300-66 MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.Apr 8, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051226Shaft · wornDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. INSTALLED NEW NR 1 RT SLAT JACKSCREW AND INBD SECTION OF TORQUE TUBE WITH NEW U-JOINT REF AMM 27-84-22-4 AND SMP, STILL REQUIRES RII FOR INSTALLATION AND OPS CK.Apr 5, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051225Shaft · shearedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. FOUND RT WING NR 2 SLAT OTBD J/S, INBD SIDE TRANS SHAFT "U" JOINT SHEARED IN TWO. REMOVED AND REPLACED CHA1237-004A, S/N 0158, R & R FPPU REF MM 27-81-19-4. RII FOR INSTALApr 5, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051224Universal Joint · failedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. OPENED RT WING LOWER L/E PANELS TO INSPECT FOR FAULTS. FOUND RT WING NR 2 SLAT OTBD J/S, INBD SIDE TRANS SHAFT "U" JOINT SHEARED IN TWO. REMOVED JOINT FROM SHAFT AND PART OApr 5, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051223Pickup · malfunctionedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF A300-66 MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.Apr 5, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051220Pickup · malfunctionedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.Apr 5, 2009 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA200904051182Control Unit · malfunctionedDURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG. WOULD NOT RETRACT. FOUND THE FEEDBACK PPU, (FPPU) & LT WING (APPU) READING INCORRECTLY. REMOVED AND REPLACED FPPU REF MM 27-81-19-4. STILL REQUIRES RII FOR INSTALL & OPERATIONAL TEST REF 27Apr 5, 2009 · N717FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA200902020424Jackscrew · unknownAFTER TAKEOFF, FLAP RETRACTION, FLAPS WOULD NOT RETRACT (FROM 15/20) UNTIL AFTER LANDING. THEREBY CAUSING AN UNSCHEDULED RETURN TO CWF. TROUBLESHOT IAW TSM 27-50-02 FIG 101/102/103/104. AT ON SITE REP REQUEST SWAPPED NR`S 3/5/6 FLAP SYSTEM JACKSCREWS FROM LTFeb 2, 2009 · N717FD · Airbus A300B4622 · Trailing Edge Flap Control SystemSDR FDEA200901130189Floor Support · crackedMAIN DECK CARGO COMPARTMENT VERTCAL FLOOR SUPPORT INBD TANG CRACKED 2 IN LONG AT FR 49, BELOW SEAT TRACK 4RT. REMOVED AND REPLACED VERTICAL FLOOR SUPPORT AT FR 49 BELOW SEAT TRACK 4RT IAW A300-600 SRM 51-72-10.Jan 13, 2009 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
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