N674FE

Service difficulty reports · 345

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 = 'N674FE' 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 FDEA201102250759Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 64 BETWEEN SEAT TRACKS 4R AND 3R MILLED GRIP ON AFT FACE HAS A 1 INCH CRACK AT 2.25 INCH FROM TOP OF THE BEAM. CUT OUT DAMAGED AREA IAW SRM 53-10-15 FIG 211 PG 389. NDT CHECK COMPLIED WITH, NO CRACKS FOUND IAW NTM 51-10-08. REPAIFeb 25, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201102240758Seat Track · corrodedMAIN DECK NR 1 SEAT TRACK DOUBLER BETWEEN FR 27 AND FR 28 HAS .25 INCH SQ EXFOLIATION CORROSION AROUND SCREW HOLE. REMOVED LEVEL ONE CORROSION NR 1 SEAT TRACK BETWEEN FR 27 AND FR 28 IAW SRM 51-74-10. CHECK LIMITS AND FOUND TO BE OUT OF LIMITS (100 PERCENT MFeb 24, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102240757Plate · corrodedMAIN CARGO COMPARTMENT UNDERNEATH, 6 EA NUTPLATES HAVE CORROSION BETWEEN FR 26 AND FR 27 AND BETWEEN L2 AND L3 SEAT TRACKS. REMOVED LEVEL ONE CORROSION ON THRUSH PLATES BETWEEN FR 26 AND FR 27 AND SEAT TRACKS L2 (Y450) AND L3 (Y953) IAW SRM 51-74-10 PG 201.Feb 24, 2011 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201102240714Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, FR 73, SEAT TRACK 2R (-Y 450), CORRODED APPROX. 1" SQ IN ON OTBD FLANGE. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, PG 205, CHECKED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK -Y 450 AT FRFeb 24, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102240711Seat Track · corrodedMAIN CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT -Y 953 BETWEEN FRAMES 48 AND 49. REMOVE LEVEL 1 CORROSION IAW SRM 51-74-10, PG 205. CHECKED LIMITS, FOUND OUT OF LIMITS IAW SRM 53-10-16, FIG 101, REPAIRED SEAT TRACK -Y 953 BETWEEN FRAMES 48 AND 49 IAW Feb 24, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102220670Seat Track · corrodedMAIN CARGO COMPARTMENT SEAT TRACK 4L HAS CORROSION ON FLOOR PANEL LANDING AT FR 27 (ABOUT 3 SQUARE INCHES). REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, PAGE 205. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PAGE 103, FIG 101. REPAIRED SEAT TRFeb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102220669Seat Track · corrodedMAIN CARGO COMPARTMENT SEAT TRACK R2 HAS CORROSION BETWEEN FR 56 AND FR57. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16 FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 2R SECTION BETWEEN FR56 AND FR 57 IAW SRM 53-10 16, FIG 208 Feb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102220668Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM HAS A 0.25 INCH CRACK AT FR 31 BETWEEN SEAT TRACKS Y1456 AND Y1959. BLENDED CRACKED VERTICAL STIFFNER IAW SRM 53-10-15, FIG 212. NDT CHECK COMPLIED IAW NTM 51-10-08 VERIFIED ELIMINATION OF CRACK. REPAIRED CROSSBEAM AT R31Feb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201102220666Seat Track · gougedON SEAT TRACK 5L, 3 INCHES FWD OF FR 54.2 THE SCALLOP ARE GOUGED .3750 IN LONG, .2500 IN WIDE AND 0.090 INCH DEEP. CHECKED THE LIMIT FOR THE GOUGE ON THE SEAT TRACK 5L, FOUND TO BE OUT OF LIMIT IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK 5L BETWEEN FR 54 Feb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102220665Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FR 78 SEAT TRACK 2R CORRODED IN THE SCALLOP APPROX 1 SQ INCH. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, CHECKED LIMITS, FOUND TO BE OUT OF LIMIT IAW SRM 53-10-16, PAGE 201. R & R SEAT TRACK 2R FROM FR 76 TO FR80 IAW SRM 53-10 16Feb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102220663Seat Track · corrodedMAIN CARGO COMPARTMENT SEAT TRACK 3L HAS CORROSION TOP SIDE FRAME 16. REMOVED LEVEL 1 CORROSION ON SEAT TRACK 3L AT FR 16 IAW SRM 51-74-10, PAGE 205, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PAGE 105, FIG 102. R & R SEAT TRACK 3L FROM FR 15 TO FR Feb 22, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102140563Seat Track · corrodedMAIN CARGO COMPARTMENT SEAT TRACK -Y1959 HAS CORROSION (7 SPOTS) BETWEEN FR 30 AND FR39. REMOVED LEVEL1 CORROSION FROM SEAT TRACK R5 IAW SRM 51-74-10 AT THE 7 SPOTS CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK 5R BEFeb 14, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102140561Seat Track · corroded6 INCH AFT OF FRAME 76, SEAT TRACK 2L CORRODED APPROX 1 SQ INCH. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-16, PAGE 103. REPAIRED SEAT TRACK 2L BETWEEN FR75 TO FR77 IAW SRM 53-10-16, FIG 208 SPLICE REPAIR SCFeb 14, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102130554Seat Track · corrodedSEAT TRACK 3L OTBD FLANGE, 7" FWD OF FR 60, CORROSION APPR 1 SQ". REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, PG 205. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK IAW SRM 53-10-16, PG 236, FIG 206 USING ANGLE AND FFeb 13, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102130553Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 28 BETWEEN SEAT TRACK 2R AND 3R, HAS 1" IN LONG CRACK ON T-CHORD. REMOVED THE DAMAGED SECTION FROM FLOORBEAM AT FR 28 BETWEEN SEAT TRACK 2R AND 3R IAW SRM 53-10-15, STEP 2 PG 394, NDT CHECK COMPLIED WITH IAW NTM 51-10-08, NO CRACK NOFeb 13, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201102130552Seat Track · gougedSEAT TRACK TOP SIDE HAS 2 GOUGES AT (Y 450) FR 32. BLENDED DAMAGED AREA IAW SRM 51-73-10, PG 207. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK AT FR 32 (Y 450) BY SPLICING THE SEAT TRACK IAW SRM 53-10-16, FIG 208.Feb 13, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102130551Seat Track · corrodedJUST AFT OF FR 77, SEAT TRACK 3L CORRODED APPR. 1 SQ" ON SCALLOP. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, PG 205. CHECKED LIMITS AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101, PG 103. R & R SEAT TRACK 3L BETWEEN FR 77 AND FR 80 IAW SRM 53-1Feb 13, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102090516Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM HAS CRACK AT FRAME 64 BETWEEN SEAT TRACK R-4 AND R-5 ( -Y1456 AND -Y1858) .5 IN LONG CUT OUT DAMAGED AREA IAW SRM 53-10-15, FIG 211, PG 389. TRIMMED FLOORBEAM IAW 53-10-15, PG 391-392. NDT CHECK FOR CRACKS IAW IAW NTM 51-10-0Feb 9, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201102050477Seat Track · corrodedMAIN CABIN FR 14B TO 15B, SEAT TRACK 2R HAS 6" INCHES OF CORROSION. REMOVED LEVEL 1 CORROSION ON SEAT TRACK 2R, BETWEEN FR 14B AND 15B IAW SRM 51-74-10, PG 205. CHECKED LIMITS IAW SRM 53-10-16, PG 103, FIG 101, FOUND TO BE OUT OF LIMIT. R & R SEAT TRACK 2R FFeb 5, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102050476Seat Track · corrodedMAIN CABIN FRAME 14B TO 15B, SEAT TRACK 2L HAS 6" INCHES OF CORROSION. REMOVED LEVEL 1 CORROSION ON SEAT TRACK 2L, BETWEEN FRAME 14B AND 15B IAW SRM 51-74-10, PG 205. CHECK AND FOUND OUT OF LIMITS IAW SRM 53-10-16, PG 103, FIG 101. R & R SEAT TRACK 2L FROM FFeb 5, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005141536Smoke Detector · false activationUPON APPLYING POWER AT T/O MAIN DECK SMOKE DETECTOR AFT B LOOP ILLUMINATED. LIGHT AND ECAM IMMEDIATELT WENT OFF WHEN T/O WAS ABORTED. ON SUBSEQUENT T/O LIGHT DID NOT ILLUMINATE AND THERE WAS NO ECAM ALERT. R & R MAIN DECK CARGO COMPARTMENT SMOKE DETECTION UMay 14, 2010 · N674FE · Airbus A300F4605R · Smoke DetectionSDR FDEA200904291468Pressure Switch · inoperativeIMMEDIATELY AFTER TAKEOFF GOT ECAM MSG ON BLUE HYDRAULIC SYSTEM LOW. COMPLIED WITH QRH. NEITHER QTY OR PRESSURE GOT TO ZERO. SERVICED BLUE SYSTEM HYD PER AIRBUS MM REF 12-12-29-0, OPERATED ELECT HYD PUMPS, OPERATED ALL FLIGHT CONTROLS AND CHECKED FOR LEAKApr 29, 2009 · N674FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200812175192Proximity Sensor · failedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF IN POSITION DET SYS 1 OR SYS 2. REPLACED RELAY 20ES FOUND BAD ON PREVIOUS T/S. SWUNG GEAR IN SYSTEM 1 AND 2 REF AMM 32-61-00-5. BOTH SYSTEMS CHECK GOOD. DOWN JACKED ACFT , NEEDS PROX BOX DET BITE TEST WHEN POWEDec 17, 2008 · N674FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 08FDEA02889Floorboard · damagedMAIN CARGO FLOOR PANEL 242 RG IS CRACKED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F.Jul 15, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02862Fitting · gougedRIGHT MLG DOOR UPPER ACTUATOR ATTACH FITTING BRACKET IS GOUGE BY THE SEQUENCE VALVE. REMOVED DAMAGED FITTING IAW SRM 51-41-21. LOCATED & DRILLED NEW FITTING P/N A5381077100195, PO 624364.1 IAW DWG A53810906. INSTALLED IAW DWG A53810906. LANDING GEAR FUNCTIJul 14, 2008 · N674FE · Airbus A300B4605R · Main Landing GearSDR 08FDEA02872Bolt · crackedLEFT WING NR 1 SLAT, NR 2 TRACK LOWER BOLT IS CRACKED. REMOVED AND REPLACED IAW A300-600 AMM 27-80-12-4.Jul 14, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02870Bolt · crackedRIGHT WING NR 2 SLAT, NR 5 TRACK LOWER BOLT IS CRACKED. REMOVED AND REPLACED BOLT ON THE RIGHT WING NR 2 SLAT, NR 5 TRACK IAW FEDEX A300-600 AMM 27-80-12-4.Jul 14, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02871Bolt · crackedRIGHT WING NR 2 SLAT, NR 7 TRACK LOWER MOUNT BOLT IS CRACKED. REMOVED RIGHT WING NR 2 SLAT, NR 7 TRACK LOWER MOUNT BOLT AND INSTALLED NEW NR 2 SALT; NR 7 TRACK LOWER MOUNT BOLT IAW FEDEX A300-600 AMM 27-80-12-4.Jul 10, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02763Slat Track · crackedLEFT WING NR 2 SLAT; NR 5 TRACK LOWER MOUNT BOLT IS CRACKED. REMOVED DAMAGED BOLT AND REPLACED WITH A NEW BOLT IAW A300-600 AMM 27-80-12-4. TOOL NR T8342K.Jul 8, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02762Slat Track · crackedRIGHT WING NR 2 SLAT; NR 6 TRACK LOWER MOUNT BOLT IS CRACKED AND THE NUT IS CORRODED.Jul 8, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02744Slat Track · crackedRIGHT WING NR 3 SLAT; NR 8 TRACK LOWER LUG BOLT IS CRACKED. REMOVED NR 3 SLAT; NR 8 TRACK LOWER BOLT AND INSTALLED A NEW BOLT FOR THE NR 3 SLAT; NR 8 TRACK IAW FEDEX A300-600 AMM 27-80-12-4.Jul 8, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02743Slat Track · crackedRIGHT WING NR 3 SLAT; NR 9 TRACK LOWER LUG BOLT IS CRACKED REMOVED AND REPLACED BOLT ON THE RIGHT WING NR 3 SLAT NR 9 TRACK IAW FEDEX A300-600 AMM 27-80-12-4; PG 2; STEP D-4.Jul 8, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02729Slat Track · crackedRIGHT WING NR 3 SLAT NR 10 TRACK LOWER LUG BOLT IS CRACKED. REMOVED AND REPLACED RIGHT WING NR 3 SLAT; NR 10 TRACK LOWER BOLT IAW FEDEX A300-600 AMM 27-80-12-04; PG 2; STEP D-4.Jul 7, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02728Fairing · crackedNR 2 PYLON AFT FAIRING LT FWD OF 483 CL CUTOUT; METAL PLATING IS CRACKED AT THE LOWER END. REMOVED METAL PLATE REINFORCEMENT IAW A300-600 SRM 51-40-00. FABBED REPAIR DOUBLER IAW A300-600 SRM 54-50-10; PG 214. STOP DRILLED THE CRACK IAW A300-600 SRM 54-50-00Jul 7, 2008 · N674FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA02727Web · corrodedTHE CABIN FLOOR WEB FROM FRAME C26 - C28; LBL 78 - 98 HAS CORROSION. REMOVED PANEL IAW A300-600 SRM 51-40-2. LOCATED AND DRILLED PANELS IAW A300-600 SRM 51-40-21 AND SRM 51-40-40;PG1. INSTALLED PANELS IAW A300-600 SRM 51-40-22. REMOVED AND REINSTALLED SEJul 7, 2008 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02726Web · corrodedTHE CABIN FLOOR WEB AT FRAME C28 - C30 LBL 78-98 HAS CORROSION. REMOVED PANELS (2EA) IAW A300-600 SRM 51-40-22. LOCATED AND DRILLED PANELS (2EA) IAW A300-600 SRM 51-40-21 AND SRM 51-40-40; PG 1. MACHINED A WEB IAW AIRBUS DWG A53781984 (1 EA). ALODINED AJul 7, 2008 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02725Skin Panel · damagedA FASTENER IN THE FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT THE LEFT SKIN LOWER FLAP SPLICE BETWEEN FRAME 2 AND FRAME 3. REMOVED FASTENER IAW A300-6003-10-12. COLD WORKED THE HOLE A300-600 SRM 51-40- 49. INSTALLED A NEW FASTENER IN THE LEFT SKIN LOWER SPJul 7, 2008 · N674FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 08FDEA02655Bearing · wornNR 1 PYLON; AFT CENTER PYLON ATTACH BEARING HAS PLAY IN ALL DIRECTIONS. REMOVED AND INSTALLED A NEW BEARING ASSEMBLY REF A300-600 AMM 54-51-75-4.Jul 3, 2008 · N674FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR 08FDEA02653Bolt · corrodedRIGHT WING NR 1 SLAT; NR 2 TRACK FWD BOLT IS PITTED. REMOVED AND REPLACED THE BOLT ON THE RIGHT WING NR 1 SLAT; NR 2 TRACK FWD BOLT IAW FEDEX A300-600 AMM 27-80-11-4.Jul 3, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02869Bolt · crackedLEFT WING NR 2 SLAT, NR 7 TRACK LOWER BOLT ID CRACKED. REPLACED DAMAGED BOLT WITH A NEW LOWER BOLT IAW A300-600 AMM 27-80-12-4.Jul 1, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02868Bolt · crackedNR 4 GUIDE TRACK LOWER KNUCKLE BOLT (NR 10) IS CRACKED AT THE HEAD END. THE ECCENTRIC BOLT WASHER IS GROOVED. REMOVED DAMAGED LOWER BOLT AND REPLACED WITH NEW. REMOVED DAMAGED WASHER AND REPLACED WITH NEW IAW A300-600 AMM 27-80-12-4. TORQUE WRENCH T8342MJul 1, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02585Slat Track · crackedLEFT WING NR 2 SLAT NR 4 TRACK LOWER ATTACH BOLT IS CRACKED. REMOVED DAMAGED BOLT AND REPLACED IT WITH A NEW ONE IAW A300-600 AMM 27-80-12-4.Jun 30, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02584Skin · gougedLEFT INBD FLAP LOWER SKIN; FWD OUTBD; HAS A PAINTED OVER GOUGE. BLENDED DAMAGE IAW A300-600 SRM 57-50-00. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00. INSTALLED REPAIR IAW A300-600 SRM 57-50-00; PG 218; FIG 205.Jun 30, 2008 · N674FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA02583Skin · chafedRIGHT WING CENTER FLAP UPPER SKIN HAS A WORN AREA APPROXIMATELY 70 INCH FROM THE INBD END AND 23 INCHES FROM THE AFT EDGE. BLENDED AREA AND FOUND AREA OUT OF ALLOWABLE LIMITS IAW A300-600 SRM 57-50-00; FIG SHEET 5; NOTE 1. FABBED REPAIR DOUBLER; TREATED; PRJun 30, 2008 · N674FE · Airbus A300F4605R · Leading Edge DevicesSDR 08FDEA02549Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 252 UH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL 252 UH, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F.Jun 27, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02548Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 252 YG IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 252 YG, LOCATED HOLES FROM THE OLD PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F.Jun 27, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02547Floor Panel · damagedMAIN CARGO FLOOR PANEL 251 QH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 251 QH, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F.Jun 27, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02546Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 251 BH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F.Jun 27, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02545Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 251 AH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 251 AH, LOCATED HOLES FROM THE OLD PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F.Jun 27, 2008 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02544Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 251 XG IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTTED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F.Jun 27, 2008 · N674FE · Airbus A300B4605R · Fuselage Floor Panel
Back to N674FE