N729FD

Service difficulty reports · 229

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 = 'N729FD' 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 FDEA201310022367Line · leakingDURING CRUISE, ECAM INDICATED LOSS OF GREEN SYS FLUID. OVERHEAD & ECAM CONFIRMED SAME ISSUE. PERFORMED QRH PROCEDURE & DIVERTED. EMERGENCY DECLARED. NR 1 ENGINE HAS RUNNING HYD LEAK. FOUND GREEN SYS EDP PRESSURE LINE CHAFED AND LEAKING. REMOVED AND REPOct 2, 2013 · N729FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201303120550Smoke Warning · false indicationMAIN DECK SMOKE, MID LOOP WARNING. COULD NOT DUPLICATE.Mar 12, 2013 · N729FD · Airbus A300B4622R · Fire DetectionSDR FDEA201212294395Oil System · lowSTAB JAMMED AT CRUISE FLT, 80 MACH, FLT LEVEL 320. COMPLIED WITH MANUAL, LANDED WITH NO MAJOR PROBLEMS. CAPTAIN STATED THAT DURING CRUISE, PITCH TRIM 1 & 2 DISCONNECTED. TRIED TO ENGAGED PITCH TRIM 1 & 2, BUT KICKED OFF AGAIN. FLT CREW ALSO STATED THAT MANDec 29, 2012 · N729FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA201203080819Skin · dentedLEFT AILERON UPPER SKIN HAS FOUR DENTS & AILERON LOWER SKIN HAS FOUR DENTS. LT AILERON FOUND ONE DENT ON BOTTOM SIDE FWD. AREA TO BE WITH IN LIMITS (NR 1). REPAIRED THREE DENTS ON LOWER SIDE NEAR T/E (NR 2, 3, 4) USING METAL DOUBLERS IAW SRM 57-61-11, PARA Mar 8, 2012 · N729FD · Airbus A300B4622R · AileronsSDR FDEA201203080818Skin · dentedLEFT AILERON UPPER SKIN HAS FOUR DENTS & AILERON LOWER SKIN HAS FOUR DENTS THAT REQUIRES EVALUATION. ON LT AILERON FOUND ONE DENT ON BOTTOM SIDE FWD. AREA TO BE WITH IN LIMITS (NR 1). REPAIRED THREE DENTS ON LOWER SIDE NEAR T/E ( NR 2, 3, 4) IAW SRM 57-61Mar 8, 2012 · N729FD · Airbus A300B4622R · AileronsSDR FDEA201203080816Skin · dentedRIGHT AILERON LOWER SKIN APPROX 3 INCHES FROM LT EDGE& 1.5" FWD OF AFT EDGE IS DENTED. DENT MEASURES APPROX 1.5" L X 1.5" W X 0.090" D. REPAIRED DENT ON RT AILERON LOWER SKIN APPROX 3" FROM LT EDGE & 1.5" FWD OF AFT EDGE USING METAL DOUBLER IAW SRM 57-61-11Mar 8, 2012 · N729FD · Airbus A300B4622R · AileronsSDR FDEA201203070799Failsafe · corrodedDURING VISUAL INSPECTION OF LT FWD CREW/COURIER DOOR AT LWR AFT CORNER RADIUS FAILSAFE RING, 1 SQ IN PITTED CORROSION FOUND. AFT CORNER FITING FOUND TO BE OUT OF LIMITS IAW DWG A53611556. R & R FITTING IAW SRM 51-40-21.Mar 7, 2012 · N729FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201203070798Wedge · corrodedLEFT LOWER ELEVATOR HAS NR 2 SPOT OF CORROSION 1 SQ" X 1 SQ" EACH. REMOVED CORROSION IAW SRM 51-74-10 PG 210 B, FOUND TO BE OUT OF LIMITS IAW SRM 55-20-00, PG 104. REMOVED DAMAGED WEDGE IAW SRM 51-40-44, PG 20. INSTALLED NEW WEDGE IAW SRM 51-40-21, PG 7. TRMar 7, 2012 · N729FD · Airbus A300B4622R · Elevator StructureSDR FDEA201203040774Skin · chafedLEFT WING, OTBD FLAP UPPER SURFACE BETWEEN BETWEEN TRACK 5 AND 6, A .5 INCH WIDE BY 1.5 INCH LONG CHAFE MARK INTO SKIN 2 INCHES ABOVE CHAFE SMOOTH AND BLEDED OUT CHAFE MARK AT OTBD FLAP UPPER SURFACE BETWEEN TRACK 5 AND 6 ON LT WING IAW SRM 51-73-10. CHECKEDMar 4, 2012 · N729FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA201203040773Floorboard · delaminatedAFT FUSELAGE TAIL SECTION FLOORBOARD 312AF HAS 7 INCH X 7 INCH AREA OF DELAM ON FWD SIDE OF PULLEYS COVER. FABRICATED FLOORBOARD IAW DWG SRZ-25-005, REV J.Mar 4, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201203020736Skin · dentedLEFT HORIZONTAL STAB LWR SURFACE 8TH RIB FROM OTBD END OF PANEL 331CB AND 8 INCHES FROM L/E HAS A DENT 4.5"L X 4.0" W AND APPOX 0.15 DEEP. REMOVED AND REINSTALLED L/E PANEL 331CB IAW SRM 51-40-02. REPAIRED DENT BY ROUTING OUT DAMAGE IN SKIN 4.5" X 4.6", ROUMar 2, 2012 · N729FD · Airbus A300B4622R · Horizontal Stabilizer, Plate/SkinSDR FDEA201202240682Floorboard · crackedFLOORBOARD 252 RG CRACKED, 12 INCHES LONG AT CTR POSITION. FABRICATED REPLACEMENT FLOORBOARD IAW DWG, SRZ 25-005, REV J.Feb 24, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201202230671Floorboard · delaminatedTHS COMPT FLOORBOARD 312 AF DELAMINATED AT EDGE 10 SQ.IN FABRICATED FLOORBOARD 312 AF IAW DWG SRZ 25-005, REV J.Feb 23, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201202230670Floorboard · crackedFLOORBOARD 252ZF CRACKED 10.5" LONG, EXTENDING FROM CLEVIS ADAPTER CUT OUT. FABRICATED REPLACEMENT FLOORBOARD 252ZF IAW SRZ 25-005, REV J.Feb 23, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201202230669Floor Panel · damagedAFT CARGO FLOOR PANEL 152AF HAS CRUSHED CORE 4 PLACES 32 SQ IN. FABRICATED REPLACEMENT FLOOR PANEL 152AF IAW DWG SRZ 25-005, REV J.Feb 23, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201202230668Floor Panel · damagedAFT CARGO FLOOR PANEL 151 AF HAS CRUSHED CORE 24 SQ IN, FABRICATED REPLACEMENT FLOOR PANEL 151AF IAW DWG SRZ-25-005, REV J.Feb 23, 2012 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201202220647Seat Track · gougedSEAT TRACK 4L BETWEEN FR 61- 62 HAS TWO GOUGES AT SCALLOPS. REMOVED SEAT TRACK IAW SRM 51-40-21 PG 7. FABRICATED, LOCATED AND DRILLED SEAT TRACK IAW SRM 53-10-16 PG 213-214 FIG 202 AND SRM 51-40-44 PG 7 TABLE 8. APPLIED ALODINE IAW SRM 51-21-10. PG 7 TABLE Feb 22, 2012 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201202200625Seat Track · gougedMAIN CABIN AT FR37 & FR38 SEAT TRACK 2R HAS 2EA SCALLOPS WITH GOUGES. REMOVED GOUGES AND CHECKED LIMITS IAW SRM 51-74-10. MATERIAL LOSS IS .025". FOUND TO BE WITHIN TOLERANCES IAW SRM 53-10-16. ALODINED, PRIMED AND TOPCOATED IAW SRM 51-21-10, 51-23-10 ANDFeb 20, 2012 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201202200624Seat Track · corrodedMAIN CABIN AT FR 54.3 & FR 55 SEAT TRACK 3R HAS CORROSION. (SCALLOPS) MAIN CABIN AT FR54.3 TO FR 55 SEAT TRACK 3R, REMOVED CORROSION AND CHECKED LIMITS IAW SRM 51-74-10. MATERIAL LOSS IS .034". FOUND TO BE WITHIN TOLERANCES IAW SRM53-10-16. ALODINED, PRIMED Feb 20, 2012 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201202200623Seat Track · corrodedMDCC SEAT TRACK 2R HAS 3EA AREAS OF CORROSION BETWEEN 57 & 57.1 TOTAL DEFECT MEASURES 3 SQ INCHES. REMOVED CORROSION AT SEAT TRACK 2R BETWEEN FR 57 TO FR57.1 IAW SRM 51-74-10. MECHANICALLY MEASURED MAXIMUM MATERIAL LOSS .006" USING DEPTH GAUGE FOUND WITHIN LFeb 20, 2012 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201202200622Seat Track · corrodedSEAT TRACK 3R CORRODED BETWEEN FR 54.1 TO FR 54.2 AS MARKED, REMOVED CORROSION AT SEAT TRACK 3R BETWEEN FR 54.1 TO FR54.2 IAW SRM 51-74-10. MECHANICALLY MEASURED MAXIMUM MATERIAL LOSS .009" FOUND WITHIN LIMIT IAW SRM 53-10-16. TREATED THE AREA IAW SRM 51-21-Feb 20, 2012 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908143017Floor Panel · delaminatedFWD CARGO COMPARTMENT FLOOR PANEL 131 QF IS DELAMINATED. FABRICATED FLOOR PANEL 131 QF IAW DWG SRZ 25-005, REV "H".Aug 14, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908122981Skin · dentedTHE BULK CARGO DOOR IS DENTED AT THE FWD LOWER CORNER. REPAIRED BULK CARGO DOOR DENT IAW EA 6-5230-127982, "BULK CARGO DOOR OUTER SKIN LOWER FWD CORNER DENT".Aug 12, 2009 · N729FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA200908102967Floor Panel · damagedFLOOR PANEL 242 VG HAS THE END OF THE PANEL BROKEN OFF. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "H".Aug 10, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908072963Floorboard · dentedAFT CARGO PIT BALLMAT PANEL 151 RF IS PUNCTURED ON THE BOTTOM SIDE. REMOVED OLD SKIN IAW SRM 51-40-21; PARA 6 & 13. DRILLED NEW SKIN IAW SRM 51-72-10, PG 2. ALODINED IAW SRM 51-21-10, PG 1. PRIMED & PAINTED IAW SRM 51-23-10, PG 1. INSTALLED SKIN IAW SRM 5Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908072962Floorboard · dentedAFT CARGO PIT BALLMAT PANEL 1561 MF HAS BULGES ON THE BOTTOM SKIN. REMOVED OLD SKIN IAW SRM 51-40-21; PARA 6 & 13. DRILLED NEW SKIN IAW SRM 51-72-10, PG 2. ALODINED IAW SRM 51-21-10, PG 1. PRIMED & PAINTED IAW SRM 51-23-10, PG 1. INSTALLED SKIN IAW SRM 5Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908072944Profile · crackedFWD CARGO COMPARTMENT BALL MAT 132 TG INTERNAL PROFILE IS CRACKED. REMOVED & REPLACED PROFILE IAW SRM 51-72-10, PARA 6. PO # 651190.2. ALODINED; PRIMED; TOP COATED & APPLIED ANTI-SKID IAW SRM 51-23-10, PGS 1 - 4. INSTALLED PROFILE IAW SRM 51-72-10, PG 2.Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200908072943Floorboard · damagedFWD CARGO COMPARTMENT BALL MAT 132 XG IS DAMAGED. REMOVED PROFILE IAW SRM 51-72-10, PARA 5A. LOCATED & DRILLED PROFILE IAW SRM 51-72-10, PARA 6A. TOP COATED IAW SRM 51-23-10. INSTALLED PROFILE IAW SRM 51-72-10, PARA 6. APPLIED NON-SKID IAW SRM 51-23-10.Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908072941Profile · crackedAFT CARGO COMPARTMENTUPPER DOOR CUTOUT RT PROFILE IS CRACKED. REMOVED CRACKED PROFILE IAW SRM 51-40-21, PARA ,6 ; PG 7 AND PARA 7, PG 24. DRILLED & LOCATED THE NEW PROFILE IAW SRM 51-40-44; 51-72-10& 51-17-18 PG 45. INSTALLED IAW 51-40-21 PARA 6, PG Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200908072940Support · crackedAFT CARGO COMPARTMENT UPPER DOOR CUTOUT R/H SIDE PROFILE IS CRACKED. REMOVED CRACKED PROFILE IAW SRM 51-40-21, PARA ,6 ; PG 7 AND PARA 7, PG 24. DRILLED & LOCATED THE NEW PROFILE IAW SRM 51-40-44; 51-72-10& 51-17-18 PG 45.Aug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200908072939Floorbeam · corrodedAFT CARGO COMPARTMENT BILGE AREA FLOORBEAM IS CORRODED ON THE LOWER SURFACE OF FRAME 63; LBL 1405 TO RBL 300. CLEANED AFT CARGO COMPARTMENT FLOORBEAM AT FRAME 63; LBL 1405 TO RBL 300 PER SRM 51-74-10; PG 201. REMOVED CORROSION IAW SRM 51-74-10 AND FOUND TOAug 7, 2009 · N729FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200908052914Floorbeam · corrodedFORWARD CARGO COMPARTMENT INTERNAL INTERCOSTAL IS CORRODED AT FRAME 30; BL-18R. REMOVED CORROSION IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG 106, ITEM K. REMOVED & REPLACED ROLLER IAW AMM 25-51-24-4, PGS 3&4; PARA B&D. REMOVED & RAug 5, 2009 · N729FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200908052915Support · crackedAVIONICS COMPARTMENT; UNDER PANEL 121 TF; THE ELECTRICAL WIRES SUPPORT STRUCTURE (TUBE) IS CRACKED FROM FRAME 17 TO FRAME 18 AND RBL 0 TO RBL 6. REMOVED; LOCATED; DRILLED AND INSTALLED ELECTRICAL WIRES SUPPORT STRUCTURE IAW SRM 51-72-10.Aug 5, 2009 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200908032877Floor Panel · crackedFLOOR PANEL IS CRACKED FROM FRAME 51 TO FRAME 54; APPROX LBL 20. FABRICATED FLOORBOARD IN REF TO DWG SRZ 25-005, REV "H".Aug 3, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908032876Floor Panel · damagedMAIN CABIN FLOOR PANEL 262 YF IS DAMAGED FROM FRAME 78 TO FRAME 79 AND FROM RBL 32 TO RBL 45. FABRICATED FLOORBOARD IN REF TO DWG SRZ 25-005, REV "H".Aug 3, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200908032875Floor Panel · crackedCABIN FLOOR PANEL 251 XH FWD END IS CRACKED BETWEEN FRAME 63 & FRAME 64; LBL 96. FABRICATED FLOORBOARD IN REF TO DWG SRZ 25-005, REV "H".Aug 3, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907312855Bracket · bentAFT CARGO COMPARTMENT BILGE AREA, BRACKET BENT FR 57.3 - FR 58, S52-53R REMOVED AFT CARGO COMP BRACKET BETWEEN FRAME 57.3 & FRAME 58 AT STRINGER 52R PER SRM 51-40-21; PG 46. FABRICATED A NEW BRACKET PER DWG 10A93584232A. INSTALLED NEW BRACKET IN AFT CARGJul 31, 2009 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200907312856Rack · crackedAVIONICS COMPARTMENT, BATTERY RACK, INBD RAIL CRACKED, FR16A - FR16A. REPLACED BATTERY RACK SUPPORT RAIL IAW SRM 51-72-10; REF DWG A92420535. REINSTALLED 3 A/C BATTERIES PER AMM 24-31-11-4. OPS CHECK GOOD PER AMM 24-31-00-5.Jul 31, 2009 · N729FD · Airbus A300B4622R · Battery Box StructureSDR FDEA200907272776Skin · crackedCRACK IN LT WING BOTTOM SKIN PANEL, JUST FWD OF OTBD FWD CORNER OF ACCESS PANEL 575FB. FOUND DURING HFEC INSPECTION. ACCOMPLISHED REPAIR ON WORK CARD E6-5710-7-5013 PT5; E.O. 6-5710-7-5013 PART 5.Jul 27, 2009 · N729FD · Airbus A300B4622 · Wing, Plate/SkinSDR FDEA200907272790Bracket · dentedAVIONICS COMPARTMENT ACCESS DOOR BRACKET IS DENTED. REMOVED DAMAGED DOOR BRACKET IAW SRM 51-40-21. FABRICATED NEW BRACKET IAW DWG A53612000. ALODINED NEW DOOR BRACKET IAW SRM 51-23-10. PART MARKED IAW GMM 7-0-1001. INSTALED DOOR BRACKET IAW SRM 51-40-21, Jul 27, 2009 · N729FD · Airbus A300B4622R · Electrical/Electronic Compartment DoorsSDR FDEA200907272789Floorboard · puncturedPARTS RACK, FWD CARGO COMPARTMENT BALLMAT 132DF, BOTTOM SKIN IS PUNCTURED. REMOVED & REINSTALLED BALL UNIT IAW AMM 25-52-23-4, PARA 3B & 3D. REMOVED BOTTOM SKIN & SEATING LEDGES IAW SRM 51-72-10, PARA 5. LOCATED & DRILLED BOTTOM SKIN 51-72-10, PARA 6A. Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272788Floorboard · puncturedPARTS RACK, FWD CARGO COMPARTMENT BALLMAT 132XG, BOTTOM SKIN IS PUNCTURED. REMOVED & REINSTALLED BALL UNITS IAW AMM 25-52-23-4, PARA 3B & 3D. REMOVED BOTTOM SKIN & SEATING LEDGES IAW SRM 51-72-10, PARA 5A. BOTTOM SKIN ID 2024-T3 ,0.025 IAW DWG A25771864Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272787Floorboard · puncturedFWD CARGO COMPARTMENT BALLMAT 132SG, BOTTOM SKIN IS PUNCTURED. REMOVED BOTTOM SKIN IAW SRM 51-72-10, PARA 5A. BOTTOM SKIN MATERIAL ID 2024-T3, 0.025 IAW AIRBUS DWG A25771864. LOCATED & DRILLED IAW SRM, 51-72-10, PARA 6A. ALODINED IAW SRM 51-21-10, PG 3, Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272786Floorboard · puncturedFWD CARGO COMPARTMENT BALL MAT 132TG, BOTTOM SKIN IS PUNCTURED. DRILLED & DEBURRED SKIN IAW DWG 10A25771870, ISSUE "F". ALODINED; PRIMED & TOP COATED IAW A300-600 SRM 51-21-10, PG 6 & 51-23-10, PG 5. INSTALLED SKIN; SEATING LEDGES & BALL UNITS IAW SRM 51- Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272785Floorboard · puncturedPARTS RACK, FWD CARGO COMPARTMENT FLOORBOARD 132RF TOP SKIN IS PUNCTURED. REPAIRED FLOOR PANEL IAW DWG SRZ 25-005; REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272784Floorboard · damagedPARTS RACK, FWD CARGO COMPARTMENT FLOORBOARD 131 RF HAS EDGE DAMAGE. REPAIRED FLOOR PANEL IAW DWG SRZ 25-005; REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272783Floorboard · crackedPARTS RACK, FWD CARGO COMPARTMENT FLOORBOARDS 132HG IS CRACKED. FABRICATED NEW FLOOR PANEL 132 HG IAW DWG SRZ 25-005, REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272782Floorboard · damagedPARTS RACK, FWD CARGO COMPARTMENT FLOORBOARD 132YF HAS A DAMAGED CORNER. REPAIRED IAW DWG SRZ 25-005; REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272781Floorboard · puncturedPART RACK, FWD CARGO COMPARTMENT FLOORBOARD 132JG BOTTOM IS PUNCTURED. REPAIRED IAW DWG SRZ 25-005; REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200907272780Floorboard · puncturedPARTS RACK, FWD CARGO COMPARTMENT FLOORBOARD 132ZF BOTTOM IS PUNCTURED. REPAIRED IAW DWG SRZ 25-005; REV "H".Jul 27, 2009 · N729FD · Airbus A300B4622R · Fuselage Floor Panel
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