N725FD

Service difficulty reports · 221

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 = 'N725FD' 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 FDEA201508302720Floor Panel · damagedFORWARD CARGO COMPARTMENT, FLOOR PANEL 131 ZF DAMAGED. FABRICATED NEW PANEL ON T15 1157433 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 30, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272708Floor Panel · delaminatedFORWARD CARGO COMPARTMENT, FLOOR PANEL 132 HG DAMAGED. FABRICATED NEW PANEL ON T15 1157440 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272707Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 132 ZF DAMAGED. FABRICATED NEW PANEL ON T15 1157439 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272706Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 132 QF DAMAGED. FABRICATED NEW PANEL ON T15 1157438 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272711Floor Panel · delaminatedFORWARD CARGO COMPARTMENT, FLOOR PANEL 131RF DAMAGED. FABRICATED NEW PANEL ON T15 1157431 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272710Floor Panel · damagedFORWARD CARGO COMPARTMENT, FLOOR PANEL 132RF DAMAGED. FABRICATED NEW PANEL ON T15 1157437 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508272709Floor Panel · damagedFORWARD CARGO COMPARTMENT, FLOOR PANEL 132 JG DAMAGED. FABRICATED NEW PANEL ON T15 1157441 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS A MAJOR CAT A REPAIR.Aug 27, 2015 · N725FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201508042466Thermocouple · failedENGINE 1 OIL TEMP ADVISORY. OIL TEMP EXCEEDED T 177 DEG C. COMPLIED WITH QRH & SECURED ENG. OIL TEMP INDICATION FLUCTUATED APPROX 20 DEG C. ENG 2 INDICATION WAS STEADY. NR 1 NACELLE TEMP WAS 40 DEG C HIGHER THAN NR 2 NACELLE TEMP. R & R AIR & OIL HEAT EXAug 4, 2015 · N725FD · Airbus A300B4622R · Engine Oil TemperatureSDR FDEA201502190551Unknown · smokeAFTER DEICING IN THE GATE UNDER APU POWER, MAIN DECK CARGO SMOKE WARNING FROM AFT SENSOR MOVED FWD TO BOTH MID SECTIONS. MAIN CARGO COMPARTMENT FILLED WITH SMOKE. EMER EGRESS ACCOMPLISHED. INSP CARGO AREA WITH NO FAULTS FOUND, RAN APU & ENGS IAW JRH & HAD NOFeb 19, 2015 · N725FD · Airbus A300B4622R · Air Distribution SystemSDR FDEA201312102950Spar · crackedLT FUSELAGE CTR WING BOX REAR SPAR HOLE F CRACKED. COMPLIED WITH EA6-5710-T0303333.Dec 10, 2013 · N725FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201312102949Spar · crackedLT FUSELAGE CTR WING BOX REAR SPAR HOLE B CRACKED. COMPLIED WITH EA6-5710-T0303333.Dec 10, 2013 · N725FD · Airbus A300B4622R · Wing SparSDR FDEA201312102948Spar · crackedLT FUSELAGE CTR WING BOX REAR SPAR HOLE D CRACKED. COMPLIED WITH EA6-5710-T0303333.Dec 10, 2013 · N725FD · Airbus A300B4622R · Wing SparSDR FDEA201312102947Spar · damagedLT FUSELAGE CTR WING BOX REAR SPAR HOLE, A, ENLARGED. COMPLIED WITH EA6-5710-T0303333.Dec 10, 2013 · N725FD · Airbus A300B4622R · Wing SparSDR FDEA201312102946Spar · crackedRT FUSELAGE CTR WING BOX REAR SPAR HOLE, G, CRACKED. COMPLIED WITH EA6-5710-T0303333.Dec 10, 2013 · N725FD · Airbus A300B4622R · Wing SparSDR FDEA201312092935Cylinder · damagedRT MLG INNER CYLINDER CHROMIUM COAT MISSING. REPLACED THE RT MAIN LANDING GEAR PER WORK CARD 32T0008.Dec 9, 2013 · N725FD · Airbus A300B4622R · Main Landing Gear Strut/Axle/TruckSDR FDEA201312092934Cylinder · damagedLT MLG INNER CYLINDER CHROMIUM COAT MISSING. REPLACED THE LT MAIN LANDING GEAR PER WORK CARD 32T0007.Dec 9, 2013 · N725FD · Airbus A300B4622R · Main Landing Gear Strut/Axle/TruckSDR FDEA201312052919Spar · crackedA CRACK AT HOLE NR 3 WAS FOUND IN THE REAR SPAR AT TENSION FITTING ATTACHMENT, MLG RIB 5 LT WING. ACCOMPLISHED IAW EA 6-5710 T0304448.Dec 5, 2013 · N725FD · Airbus A300B4622R · Wing SparSDR FDEA201311212847Frame · corrodedAV COMPARTMENT FRAME 17 RT BOTTOM CORNER FOUND CORROSION. BLENDED OUT THE CORROSION IAW SRM51-74-10. REPAIRED THE BLENDED OUT AREA IAW EA 6-5310-T0303479.Nov 21, 2013 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201311212846Frame Splice · crackedLT FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24L & 26L FOUND HOLE H CRACKED. REPAIRED THE CRACK PER EA6-5310-T0303310.Nov 21, 2013 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201311212845Rib · crackedLT WINGS MLG FITTING OF RIB 5 FWD LUG CORRODED. REMOVED THE CORROSION PER DWG 57240425 ISSUE B. PERFORMED INSPECTION TO THE LUG BORE PER NTM57-51-34 BLOCK 901 FOUND CRACK. REPLACED THE RIB5 PER EA6-5710-T0303522.Nov 21, 2013 · N725FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201311212844Rib · crackedRT WINGS MLG FITTING OF RIB 5 FWD LUG CORRODED. REMOVED THE CORROSION PER DWG 57240425 ISSUE B. PERFORMED INSPECTION TO THE LUG BORE PER NTM57-51-34 BLOCK 901 FOUND CRACK. REPLACED THE RIB5 PER EA6-5710-T0303523Nov 21, 2013 · N725FD · Airbus A300F4622R · Wing, Rib/BulkheadSDR FDEA201311202830Doubler · crackedCRACKS WERE FOUND ON HOLE NR 1 & NR 2 AT CTR WING BOX FRAME 44 BEAM RT CUTOUT DOUBLER Y212. REMOVED THE CRACK, INSTALLED THE BUSHING FOR HOLE NR 1, COMPLETED WITH EA6-5710-T0303307.Nov 20, 2013 · N725FD · Airbus A300B4622R · Wing, Center BoxSDR FDEA201106062132Rudder · delaminatedRUDDER FAILS MOISTURE NDT CHECK. RUDDER REMOVED AND REFITTED IAW AMM 27-21-21. REPAIRS CARRIED OUT IAW SRM 55-41-12, PARA 12 AND PARA 31.Jun 6, 2011 · N725FD · Airbus A300B4622R · Rudder StructureSDR FDEA201106032109Skin · chafedSCRATCHES AND SCUFFS X 4 ON THE LT FUSELAGE SKIN FR72 STR26-27 AREA. REPAIR CARRIED OUT IAW EA6-5330-149783 AND SRM 53-10-12 FIG 228.Jun 3, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201106032107Keelbeam · chafedKEELBEAM UPPER SURFACE DAMAGE AT FR51 LT REPAIR CARRIED OUT TO LT KEELBEAM IAW EA 6-5310-149778.Jun 3, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, KeelSDR FDEA201106012074Skin · misrepairedREWORK OBSERVED FR76-77 STR27-30 RT FUSE SKIN EXT DOUBLER REPAIR CARRIED OUT ON RT FUSELAGE SKIN AFT OF FR76 STR28 IAW SRM 53-10-12. FIG 224 SHT 2. ORIGINAL SKIN THICKNESS 1.6MM DOUBLER 1.8MM SECTION 18. REPAIR CLASSED AS MAJOR WITH REPEAT INSPECTION/SMR REJun 1, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201106012078Skin · dented2 SKIN DENTS OBSERVED ON LT FUSE SKIN DENTS PAINT STRIPPED, REPAIRED IAW EA - 6-5330-149782. MINOR REPAIR NO REPEAT INSPECTION.Jun 1, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201106012077Skin · damagedLEFT FUSELAGE SKIN AREA OF SURFACE FINISH DETERIORATED AROUND FASTENER HEAD FR21/ STR 41. REPAIR CARRIED OUT IAW SRM 53-10-12, FIG 225, SH3, SRI 53-10-12-2-005-00 TABLE TO BE EMBODIED. INITIAL AT 42500FC OR89000FH, SUBSEQUENT AT TO BE DECIDED. INSP METHJun 1, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201106012075Skin · misrepairedREWORK OBSERVED FR76-77 STR27-30 RT FUSE SKIN EXT DOUBLER REPAIR CARRIED OUT ON RT FUSE SKIN AFT OF FR76 STR28 IAW SRM 53-10-12 FIG224 SHT 2. ORIGINAL SKIN THICKNESS 1.6MM DOUBLER 1.8MM SECTION 18. REPAIR CLASSED AS MAJOR WITH REPEAT INSPECTION/SMR REQUIREMEJun 1, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105272003Seat Track · chafedCHAFING MARK FOUND ON SEAT TRACK Y4156, FR60-61. BLENDED OUT AND FOUND TO BE OUT OF SRM LIMITS. SEAT TRACK SECTION REPLACED IAW SRM 53-10-16 PG 243 PARA 10.May 27, 2011 · N725FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105272002Skin · misrepairedAFT CREW DOOR PREVIOUS REPAIR NOT IAW SRM REPAIR PROCEDURES. REPAIRED IAW SRM AND RE-INSTALLED IAW AMM 52-13-11/52-13-20. SRM 52-10-00 FIG 204 PARA 7. REPAIR IS MAJOR,May 27, 2011 · N725FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA201105272001Skin · damagedLEFT SKIN DAMAGE FR 16/17 STR 27/28. AFFECTED AREA INSPECTED IAW SRM 53-10-12 AND NTM 51-10-07 PT6 WITH NO DEFECTS FOUND.May 27, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105272000Keelbeam · damagedTOOLING DAMAGE ON KEEL BEAM UPPER SURFACE FR 51 LT AND RT. DAMAGE REPAIR ACCOMPLISHED ON EA 6-5310-149778. NDT INSPECTION REQUIREMENTS CONCLUDES NO DEFECTS APPARENT. JPF STAGES 1 TO 14 ATTCHED REFER. MAJOR REPAIR CARRIED OUT.May 27, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, KeelSDR FDEA201105271998Skin · damagedFWD PAX CREW DOOR CUT OUT UPPER CORNERS SKIN DAMAGE. SURFACE FINISH DETERIORATION ON BOTH FWD PAX/CREW DOOE CUTOUT SKIN UPPER CORNERS INVESTIGATED AND CORROSION REMOVED IAW SRM 51-22-00. REPAIRS ON FWD LH AND RH ACCOMPLISHED ON EA 6-5310-149768 WITH STAGEMay 27, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105271997Frame · damagedDENT AT FRAME 70 STR 26/27 LT. DAMAGE ASSESSED IAW SRM 53-10-12 AND FOUND TO BE OUT OF LIMITS DUE TO DAMAGE PROXIMITY TO FRAME. REPAIR CARRIED OUT IAW SRM 53-10-12 FIG 225/53-10-14 PARA 4B FIG 102. JPF STAGES 1 TO 9 REFER. MAJOR REPAIR CARRIED OUT, ORIGINMay 27, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201105271999Skin · dentedDENT IN FUSELAGE FR 57.3 STR 16LHMay 27, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105261992Skin · corrodedFWD PAX/CREW DOOR CUT OUT SKIN UPPER CORNERS HAVE MINOR SURFACE FINISH DETERIORATION. CORROSION REMOVED IAW SRM 51-22-00. REPAIRS ON FWD LT AND RT ACCOMPLISHED ON EA 6-5310-149768 WITH STAGES 1 TO 20 ON ATTACHED JPF. NDT INSPECTION CONCLUDES NO APPARENT FMay 26, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105131837Skin · dentedRIGHT INBD FLAP UPPER SURFACE HAS A DEEP GOUGE DAMAGED AREA BLENDED OUT AND HFEC INSPECTION COMPLETED. DAMAGED AREA CUTOUT AND REPAIR CARRIED OUT TO COVER BOTH DAMAGED AREAS IN ACCORDANCE WITH SRM 57-50-00. MINOR REPAIR CARRIED OUT AS PER GMM 6-2-100May 13, 2011 · N725FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201105131838Structure · misrepairedREPAIR ON FWD CREW DOOR FOUND TO BE NOT IAW SRM 52-10-00 FIG 204. REPAIR REPLACED IAW SRM 52-10-00, FIG 204, PARA 7.May 13, 2011 · N725FD · Airbus A300B4622 · Passenger/Crew DoorsSDR FDEA1105131837ASkin · dentedGOUGE AND DENT FOUND ON LT FUSE SKIN BETWEEN FR9 TO FR10 8 O'CLOCK POS.May 13, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201105131836Structure · misrepairedDOOR REPAIR FOUND TO BE NOT IAW SRM REPAIR PROCEEDURE IAW SRM 52-10-10, FIG 204. REPAIR CARRIED OUT IAW SRM 52-10-00-FIG 204, PARA 7 REPAIR IS MAJOR CAT B.May 13, 2011 · N725FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA201105131835Rib · corrodedRT KREUGER FLAP LOWER FLAP OTBD RIB HAS CORROSION. RIB REPLACED IAW DWG A53510208.May 13, 2011 · N725FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201104251630Panel · corrodedFWD LAV SERVICE PANEL DOOR IS CRACKED AND CORRODED. REPLACEMENT CARRIED OUT IAW AMM 52-42-11, PB401. DOOR OPERATION AND CLOSURE AS EXPECTED.Apr 25, 2011 · N725FD · Airbus A300B4622R · Service DoorsSDR FDEA201104251616Service Panel · corrodedFWD LAV SERVICE PANEL DOOR IS CRACKED AND CORRODED. REPLACEMENT CARRIED OUT IAW AMM 52-42-11 PB401. DOOR OPERATION AND CLOSURE AS EXPECTED.Apr 25, 2011 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA04454Skin · corrodedSUB-SURFACE CORROSION FOUND ON THE RT WING SKIN UPPER PANEL COMPLIDE WITH EA NR 6-5710-125470.Oct 21, 2008 · N725FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA04339Skin · gougedFLAP INBD RT UPPER SKIN AT FLAP ZONE OF RIB 1 BETWEEN STR 2.1 / STR 2.2 WITH SMALL GOUGE WAS REPAIRED IAW EA 6-5710-121707 AND SRM 57-50-00.Sep 18, 2008 · N725FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04407Spar · crackedRT WING RIB 5 NEXT CENTER SPAR FWD ZONE FOUND WITH CRACK (RIB 5 TO TOP SKIN). RIB 5 REPAIRED IAW EA 6-5710-121705.Sep 16, 2008 · N725FD · Airbus A300B4622R · Wing SparSDR 08FDEA04390Skin · damagedRT WING, INBD FLAP WITH ACCESS HOLE AT RIB 7 OVER DIMENSIONAL AT INNER LOWER SKIN SURFACE, IT WAS REPAIRED IAW EA 6-5750-121702.Sep 16, 2008 · N725FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04338Spar · wornLEFT WING FLAP INBD W/ HOLES OVALIZED AT FRONT SPAR OF RIB 7 THE FRONT SPAR WAS REPAIRED IAW EA 6-5750-121702.Sep 16, 2008 · N725FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04303Skin · gougedSKIN DAMAGE LOCATED AT FR43/44 S40L. REPAIRED AS PER EA 6-5330-121701.Sep 9, 2008 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
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