N667FE

Service difficulty reports · 237

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 = 'N667FE' 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 FDEA201510053072Floor Panel · crackedMAIN DECK FLOOR PANEL 242UJ HAS CRACKED, BETWEEN FRAME 43 - 47, -Y450, -Y953. FABRICATED NEW PANEL 242UJ ON T15 1165069 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510053071Floor Panel · crackedMAIN DECK FLOOR PANEL 242QJ HAS CRACKED, BETWEEN FRAME 40 - 43, -Y450, -Y953. FABRICATED NEW PANEL 242QJ ON T15 1165070 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510053070Floor Panel · crackedMAIN DECK FLOOR PANEL 242BF HAS CRACKED, BETWEEN FRAME 30 - 34, -Y450, -Y953. FABRICATED NEW PANEL 242BF ON T15 1165122 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510053068Floor Panel · crackedMAIN DECK FLOOR PANEL 242MF HAS CRACKED, BETWEEN FRAME 37 - 38, -Y450 - Y953. FABRICATED NEW PANEL 242MF ON T15 1165121 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201506221956Panel · damagedDURING POST FLIGHT WALK AROUND, FOUND RT WING OTBD SPOILER PROTRUDING UP FROM THE SURFACE OF THE WING. R & R THE NR 5 SPOILER PANEL IAW MM 27-61-53-04.Jun 22, 2015 · N667FE · Airbus A300F4605R · SpoilersSDR FDEA201503060701Pcu · failedFLAPS BINDING AT APPROX 35 DEGREES ON APPROACH. COMPLIED WITH ECAM & QRH & LANDED. CREW STATED NO ASYMMETRY FAULTS RECEIVED & ACFT HAD NO ABNORMAL FLIGHT CHARACTERISTICS. VISUALLY INSPECTED FLAPS & SLATS FROM THE GROUND, NO ABNORMALITIES NOTED. INTERROGAMar 6, 2015 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201503040653Limiter · malfunctionedFLAPS STUCK AT ZERO ON APPROACH. CYCLED SLAT FLAP HANDLE, COULD NOT GET FLAPS TO FULLY EXTEND. WHILE ENG'S WERE STILL RUNNING, DEBRIEFED CREW OVER THE HEADSET. HAD THE CREW LOWER THE FLAP SLAT HANDLE, FLAPS WERE AGAIN STUCK AT 0. IAW TSM, BOTH SFCC 1 & 2 AMar 4, 2015 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201502100500Warning System · false activationFLAPS STUCK 15 RECYCLED & QRH NO HELP. TROUBLE SHOT FOUND SFCC 1 & 2 INDICATION FLAP JAM IAW TSM 27-50-00. INSPECTED TORQUE LIMITERS, NO FAULT INDICATIONS AT THIS TIME. INSPECTED SCREW JACKS, SYS OK. OPERATED FLAPS FULL EXTEND & FULL RETRACT TWICE IAW AMM Feb 10, 2015 · N667FE · Airbus A300F4605R · Trailing Flap Position Indicating SystemSDR FDEA201409102559Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311201 P1 WINGS BASIC WING STRUCTURE RT RIB 5 FWD LUG CORROSION.Sep 10, 2014 · N667FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201409092543Support Fitting · corrodedLEFT MLG RIB 5 FWD LUG BORE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0311222 P1 WINGS BASIC WING STRUCTURE LT MLG SUPPORT FITTING & RIB FWD LUG CORROSION.Sep 9, 2014 · N667FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201408242304Hydraulic System · overservicedHYD YELLOW RSVR OVERHEAT LIGHT AFTER TAKEOFF. LIGHT STAYED ON. FOUND YELLOW SYS OVER SERVICED. DRAINED BETWEEN 1.5 & 2.0 GALLONS OUT OF YELLOW SYS. THIS COULD POSSIBLY REMEDY PROBLEM, BUT NO TIME TO LET SYS RUN. NEEDS TESTING & POSSIBLY MORE TROUBLESHOOTAug 24, 2014 · N667FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201407031618Jackscrew · contaminatedON APPROACH TO MEM FLAPS STUCK AT 15 DEG. PER A300-600 TSM 27-50-00, BITE CHECK OF SFCC 1 AND 2 SHOW FAULT FOR BOTH SFCC. RESET BOTH SFCC. FOUND LEFT WING TORQUE LIMITER POPPED. LUBED ALL BALL NUTS FOR SCREWJACKS ON LEFT WING. FOUND WATER IN NR 2 BALL NUTJul 3, 2014 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201406201496Computer · malfunctionedFLAP SYS 1 & 2 FAULT DURING APPROACH. FOUND TORQUE LIMITER ON LT FLAPS TRIPPED. DRAINED & REFILLED ALL FLAP SCREWJACKS MM 12-13-27. OIL QUANTITIES IN SCREWJACKS WERE CORRECT, NO LEAKS NOTED. SFCC NR 1 & 2 CHANGED IAW WRI OPERATED FLAPS NUMEROUS TIMES OPEJun 20, 2014 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201404190763Ram Air Turb · deployedRAT WAS DEPLOYED AT BLOCK IN. RESTOWED RAT IAW A300-600 MM CH 29-25-00-03.Apr 19, 2014 · N667FE · Airbus A300F4605R · Hydraulic System, AuxiliarySDR FDEA201401160118Engine · leakingPRIOR TO DECENT, COURIERS NOTIFIED COCKPIT OF SMOKE IN CABIN. NO SMOKE DETECTORS OR ECAM WARNINGS IN COCKPIT OR ODOR OF SMOKE. RAN AIR CONDITIONING SMOKE CHECK LIST. DECLARED EMERGENCY LANDED. ON GROUND HAD ODOR IN COCKPIT. NR 1 ENGINE HAS DEBRIS IN SCRJan 16, 2014 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201401150107Unknown · smokePRIOR TO DESCENT INTO OKC COURIERS NOTIFIED COCKPIT OF SMOKE IN CABIN. NO SMOKE DETECTOR OR ECAM WARNING IN COCKPIT OR SMELL OF SMOKE. WITH NO ECAM OR SMOKE DETECTION RAN AIR CONDITIONING SMOKE CHECK LIST. DECLARED EMERGENCY LANDED NO PROBLEM. ONCE ON GND Jan 15, 2014 · N667FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA201311292892Seat Track · corrodedMDCC FR 66 - FR 67, Y 953 SEAT TRACK CORRODED. CUTOUT THE DAMAGED SEAT TRACK SECTION IAW SRM 51-40-21. MADE SEAT TRACK REPAIR PARTS IAW SRM 51-10-16 201. HEAT TREAT THE NAS 1097DD6 RIVETS SRM 51-25-00. WET INSTALLED THE SEAT TRACK REPAIR PARTS IAW SRM 51-Nov 29, 2013 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201311292891Seat Track · corrodedMDCC FR 65 - FR 66, Y 953 SEAT TRACK CORRODED CUT OUT THE DAMAGED SEAT TRACK SECTION IAW SRM 51-40-21. MADE SEAT TRACK REPAIR PARTS IAW SRM 51-10-16 201. HEAT TREAT THE NAS1097DD6 RIVETS IAW SRM 51-25-00. WET INSTALLED THE SEAT TRACK REPAIR IAW SRM 51-40-21Nov 29, 2013 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201311142780Stiffener · crackedDURING HFEC INSPECTION OF ZONE A & B OF FRAME 12A STIFFENER FITTING , FOUND A CRACK ABOUT 10MM IN LENGTH, REPAIRED IAW EO 6-5340-7-5002, P8.Nov 14, 2013 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201310022378Hose · leakingABOUT 45-50 MINUTES AFTER TAKE OFF, RECEIVED AN ECAM WARNING, HYD GREEN RESERVOIR LOW LEVEL INDICATION ON OVERHEAD PANEL AND RT ECAM WERE ALMOST ZERO. COMPLIED WITH ECAM AND QRH. R & R NR 2 ENGINE GREEN SYSTEM HYD PRESSURE LINE REF SMP & MM 29-11-32-04-02. Oct 2, 2013 · N667FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201308252028Landing Gear · multiple failAFTER TAKEOFF, LANDING GEAR WOULD NOT COME UP IN SYS 1 POSITION. SWITCHED TO NR 2 SYS AND LANDING GEAR CAME UP. RECEIVED MULTIPLE FAULTS AT SAME TIME. R & R PROXIMITY UNIT. R & R LANDING GEAR NORMAL CONTROL SWITCH. R & R BOGIE SENSORS 8GA AND 12 GA RT MLG.Aug 25, 2013 · N667FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201308121837Unknown · malfunctionedREPORT 1 OF 2 FLAP SYS 1 & 2 FAULT ON APPROACH, CYCLED FLAPS, RAN QRH. DID NOT GAIN NORMAL FLAPS. TROUBLESHOOTING IN WORK BITE DISPLAY FAULT CODE NR 1 SFCC FLAP 00111(FAULT CODE NOT LISTED ON TSM) NR 2 SFCC FLAP 01111 (JAMMED) NR 1 SFCC SLAT 00010 ( LT KRUGEAug 12, 2013 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201308081839Flap System · inoperativeFLAP SYS 1 & 2 FAULT ON APPROACH SAN, CYCLED FLAPS, RAN QRH. DID NOT GAIN NORMAL FLAPS. TROUBLESHOOTING IN WORK BITE DISPLAY FAULT CODE 1 SFCC FLAP 00111 (FAULT CODE NOT LISTED ON TSM) NR 2 SFCC FLAP 01111(JAMMED) 1 SFCC SLAT 00010 (LT KRUGER RETRACT S/W) NAug 8, 2013 · N667FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201112065176Altimeter · failedF/O'S ALTIMETER INOPERATIVE. NAV ADC F/O'S FAULT ON ECAM. SWITCHING F/O ADC INSTRUMENT DOES NOT RECOVER, INSTRUMENT RED OFF FLAG IN F/O'S ALTIMETER. R & R F/O'S ALTIMETER IAW MM 34-12-21-04. OPS CHECKED GOOD, ACFT OK FOR SERVICE.Dec 6, 2011 · N667FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA201105312033Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR ALONG SEAT TRACK Y-450 BETWEEN FR76 AND FR77. CORROSION FOUND ON TRACK CROWN. CORROSION REMOVED AS PER SRM 51-74-10 REV 20, MATERIAL REMOVED 0.039" (L-3" W-0.5") AND FOUND OUT OF LIMIT AS PER SRM 53-10-16 FIG 102. REPAMay 31, 2011 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105251977Frame · failedDURING ACCOMPLISHMENT OF EO 6-5310-7-5006, PART 3, FIG 10 WORK STEP 2 AT CABIN FRAME 44 LT SIDE STRINGER 27 TO STRINGER 28 FOUND UNABLE TO COMPLY TO FRAME FOOT CUTOUT DIMENSIONS IAW FIG 8, SHEET 1. COMPLIED WITH EA NR 6-5310-143580 TITLE: FUSELAGE -CENTER SECMay 25, 2011 · N667FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201105251976Floor Panel · delaminatedBULK CARGO COMPARTMENT FLOOR PANEL, NR 161AF, FOUND DELAMINATED. R & R BULK CARGO COMPARTMENT FLOOR PANEL, NR 161AF, IAW AMM 53-10-35-04, REV 52.0. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 112.May 25, 2011 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201105251975Floor Panel · delaminatedFWD CARGO COMPARTMENT FLOOR PANEL, NR 131KG, FOUND DELAMINATION. R & R FWD CARGO FLOOR PANEL, NR 131KG IAW AMM 53-10-29-04, REV 52.0. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 112.May 25, 2011 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201105241957Floor Panel · crackedMAIN DECK CARGO COMPARTMENT RT OB BETWEEN FR 55 & FR 57.1 FLOOR PANEL FOUND CRACKED. MAIN DECK CARGO COMPARTMENT RT O/B BETWEEN FR 55 AND FR 57.1 FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-10-23 REV 52.0. FLOOR PANEL FABRICATED AS PER DRAWING SRZ 25-005 May 24, 2011 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201105201904Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR ALONG SEAT TRACK Y-450 BETWEEN FR74 AND FR75, CORROSION FOUND AT TRACK CROWN. CORROSION REMOVED AS PER SRM 51-74-10 REV 20. MATERIAL REMOVED 0.037" (L-2.5" W-0.5") AND FOUND OUT OF LIMIT AS PER SRM 53-10-16 FIG 102 REV 20May 20, 2011 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105201903Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR ALONG CTR SEAT TRACK Y0 AT FR78, CORROSION FOUND AT TRACK CROWN. CORROSION REMOVED AS PER SRM 51-74-10 REV 20 MATERIAL REMOVED 0.039" (L-25" W-0.5") AND FOUND OUT OF LIMIT AS PER SRM 53-10-16 REV 20 FIG 102. REPAIR CARRIEDMay 20, 2011 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105201902Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR ALONG Y0 CTR SEAT TRACK BETWEEN FR58 AND FR59, CORROSION FOUND ON FLANGE. REMOVED AS PER SRM 51-74-10 REV 20. MATERIAL REMOVED 0.035" (L-3" W-1") AND FOUND OUT OF LIMIT AS PER SRM 53-10-16 FIG 102 REV 20. REPAIR CARRIED OMay 20, 2011 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105121823Frame · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AND FOUND HOLE NR 1 WITH CRACK INDICATION AT LEFT FRAME STATION 44. LEFT FRAME STATION 44 CARRIED OUT REPAIR AS PER E.A. 6-5310-143580 AND E.A. 6-5310-143578, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-May 12, 2011 · N667FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201105121827Skin · crackedCRACK INDICATION FOUND DURING OPEN HOLE PER WORKCARD E6-5710-7-5013 02 PT6. WORK STEP 6D ON BOTTOM SKIN HOLE 'G'. CRACK ON BOTTOM SKIN HOLE "G" PERFORMED REPAIR PER DRAWING R57340199 ISSUE E AND EA 6-5710-150321 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6May 12, 2011 · N667FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201105121826Stiffener · crackedRIGHT WING LOWER SKIN SUPPORT JUST IN FRONT OF ACCESS DOOR 675FB FOUND STIFFENER CRACKED. PERFORMED REPAIR PER DRAWING R57340199 ISSUE E AND EA 6-5710- 150321 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.May 12, 2011 · N667FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201105121825Skin · crackedHFEC SURFACE INSPECTION CARRIED OUT AND FOUND CRACK ON LT WING LOWER SKIN PANEL INBOARD OF RIB 9 AROUND 01EA FASTENER WITH LENGTH APPROXIMATELY 1/4IN LONG. CRACK ON LT WING LOWER SKIN PANEL INBOARD OF RIB 9 AROUND 01EA FASTENER, PERFORMED REPAIR PER DRAWIMay 12, 2011 · N667FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201105121824Stiffener · crackedLT WING LOWER SKIN SUPPORT JUST FRONT OF ACCESS DOOR 575FB FOUND STIFFENER CRACKED. LT WING LOWER SKIN SUPPORT JUST IN FRONT OF ACCESS DOOR 575FB FOUND STIFFENER CRACKED, PERFORMED REPAIR PER DRAWING R57340199 ISSUE E AND FEDEX EA 6- 5710-150320 PART 1. May 12, 2011 · N667FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR 08FDEA04902Guide · wornCOMPLY WITH EA NR 2550-116540, "EQUIPMENT/FURNISHINGS, MAIN DECK CARGO COMPARTMENT, CARGO SYSTEM, REMOVAL OF AFT "Y" GUIDES. COMPLIED WITH EA 6-2550-116540 "EQUIPMENT/FURNISHINGS, MAIN DECK CARGO COMPARTMENT, CARGO SYSTEM, REMOVAL OF "AFT" GUIDES.Nov 17, 2008 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA04652Strap · unknownAFT CARGO DOOR CUT-OUT AT STRINGER 41R; FRAME 59A; STRAP P/N/A5397333620000 HAS A PREVIOUS BLEND OUT ON THE AFT END OF THE STRAP. REMOVED & REPLACED PER SRM 51-40-23.Oct 31, 2008 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA04651Skin · gougedAFT CARGO DOOR, FWD LOWER DOOR JAMB IS GOUGED. FOUND TO BE OUT OF LIMITS PER SRM 53-17-12. REPAIRED PER SRM 53-17-12. TREATED ALL AREAS PER 51-21-10. APPLY LUBRICANT CORROSION INHIBITOR PER 51-23-00.Oct 31, 2008 · N667FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 08FDEA04577Mount · corrodedNR 1 ENGINE FWD ENGINE MOUNT IN SPIGOT HOLE HAS RUST. REMOVED SPIGOT FITTING IAW DWG 41A54612646; REV "B". REPAIRED DAMAGED BORE HOLE IAW SRM 54-51-81; FIG 101. CAD PLATED IAW SRM 51-21-10. PRIMED IAW SRM 51-21-10. RE-INSTALLED SPIGOT FITTING IAW DWG 41AOct 27, 2008 · N667FE · Airbus A300F4605R · Engine Mount SectionSDR 08FDEA04572Floor Panel · corrodedFLOOR PANEL 241 RJ IS CRACKED. LOCATED & COUNTER BORED PANEL. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSERTS. PART MARKED & APPLIED THE NON-SKID TAPE IAW DWG SRZ 25-005.Oct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04571Floor Panel · brokenFLOOR PANEL 242 SF IS BROKEN. LOCATED & COUNTER BORED PANEL. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSERTS. PART MARKED & APPLIED THE NON-SKID TAPE IAW DWG SRZ 25-005.Oct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04570Floor Panel · damagedCABIN FLOOR PANEL BETWEEN RBL 85 - 78 AND FRAMES 45-46 HAS A HOLE IN THE BOTTOM. FABBED NEW PANEL 242 XJ USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSERTS. PART MARKED & Oct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04568Floor Panel · damagedCABIN FLOOR PANEL BETWEEN FRAMES 31 - 34 AND LBL 78 - 97 HAS HOLES ON THE BOTTOM. FABBED NEW PANEL 241 EF USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSERTS. PART MARKED & AOct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04566Floorboard · brokenMAIN CABIN FLOOR BOARD 241 HK IS BROKEN. FABBED NEW FLOOR PANEL 241 HK BY USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED HILES. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSERTS. PART MARKED & APPLIED THE NON-SKID TAPE IAW DWG SRZ 25-0Oct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04564Floor Panel · crackedFLOOR PANEL 242 QJ IS CRACKED THROUGH THE UPPER SURFACE. FABBED NEW PANEL 242 QJ USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSERTS. PART MARKED & APPLIED NON-SKID TAPE IAOct 27, 2008 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA04502Seat Track · crackedTHE EXPANSION SEAT TRACK BETWEEN FRAME 54 AND 54.2, RBL 90 IS CRACKED LOCATED; DRILLED AND INSTALLED SEAT TRACK P/N A5381313020000; S/N 758464 IAW SRM 51-40-21.Oct 23, 2008 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04404Floorbeam · crackedAFT PIT AT FRAME C61; RBL 64 FLOOR ANGLE SUPPORT IS CRACKED. REMOVED & REPLACED FLOOR ANGLE IAW SRM 51-40-21.Oct 17, 2008 · N667FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA04422Seat Track · crackedMAIN CABIN SEAT TRACK SUPPORT FITTING AT FRAME 49, STA 3089, LBL 48 IS CRACKED.Oct 17, 2008 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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