N720FD, cancelled Jun 28, 2024

Service difficulty reports · 51

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 = 'N720FD' AND deregistration_id = 'N720FD-2024-06-28'
  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 FDEA201412244177Power Supply · inoperativeL1 & R1 DOOR ESCAPE SLIDE RELEASE WARNING LIGHTS INOPERATIVE. BUZZERS OPS NORMAL. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW AMM 52-73-18-04. OPS CHECKED GOOD. PTT BUTTONS ILLUMINATE RED WARNING LIGHTS ON BOTH L1 & R1 DOORS.Dec 24, 2014 · N720FD · Airbus A300B4622 · Door Warning SystemSDR FDEA201412194178Power Supply · inoperativeAFTER BLOCK IN, R1 DOOR SLIDE ARMED NOT ON ECAM. FIRST OFFICER SAID DOOR WAS ARMED, RECYCLED ARM HANDLE, STILL NO CHANGE, NO "SLIDE" ILLUMINATED. R & R R1 DOOR LIMIT SWITCH IAW AMM 52-71-11-04-01. OPS CHECK SHOWED DOOR CLOSED ON ECAM BUT DID NOT SHOW THAT Dec 19, 2014 · N720FD · Airbus A300B4622 · Door Warning SystemSDR FDEA201211184069Frame · damagedMAIN DEC CARGO FR 28 S8-20 LT FRAME DAMAGED, BLEND OUT THE DAMAGE IAW SRM 51-73-10, COMPLIED WITH EA 6-5310-163149.Nov 18, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201211154022Skin · delaminatedRIGHT WING OTBD FIXED L/E OTBD TRAILING SECTION DELAMINATED. REMOVED THE ORIGINAL T/E DOUBLER IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201 FIG 215. INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215.Nov 15, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/SkinSDR FDEA201211144014Skin · damagedLOWER FUSELAGE SKIN FR38, S35-36R FOUND ONE LIGHTNING STRIKE. REMOVED DAMAGE IAW SRM 51-73-10. EXCEED LIMITS IAW SRM 53-10-12/101, DIAGRAM 112, REPAIRED IAW SRM 53-10-12/201 FIG 225.Nov 14, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201211144007Skin · delaminatedRT WING OTBD FIXED T/E UPPER SURFACE DELAMINATED. REMOVED THE DAMAGE T/E SKIN IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201, FIG215 WET INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215 SEALED THE EDGE WITH SEALANT IAW SRMNov 14, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/SkinSDR FDEA201211133986Skin · delaminatedSKIN DOUBLER AT RT WING TIP UPPER SKIN UNDERNEATH STATIC DISCHARGE DELAMINATION FOUND AROUND THE ORIGINAL DOUBLER AT RT WING TIP UPPER SKIN. UNDERNEATH STATIC DISCHARGE, REPAIRED IAW SRM 57-51-12/201, FIG 215 AND CLASSFIED AS MAJOR IAW GMM6-2-100.Nov 13, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/SkinSDR FDEA201211013798Floor Support · corrodedFLOOR SUPPORT CORRODED AND DELAMINATED BETWEEN FR11 TO FR13A. REPLACED FLOOR SUPPORT PER SRM51-40-21.Nov 1, 2012 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201210243735Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "F" OF LT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center BoxSDR FDEA201210243734Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "F" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center BoxSDR FDEA201210243733Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "C" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center BoxSDR FDEA201210243732Frame · crackedFOUND A CRACK 6MM IN LENGTH AT RT SIDE FRAME 40 LOWER OTBD RADIUS AREA. COMPLIED WITH EA 6-5710-163147.Oct 24, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201210243731Frame · crackedFOUND A CRACK 8MM IN LENGTH AT LT SIDE FRAME 40 LOWER OTBD RADIUS AREA. REPAIRED PER EA 6-5710-163147Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing SparSDR FDEA201210243730Rib · crackedONE CRACK ABOUT 10MM IN LENGTH WAS FOUND IN THE AREA OF HOLE 47 OF MLG RIB 5, RT SIDE. COMPLIED WITH EA 6-5710-163-146Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Rib/BulkheadSDR FDEA201210053559Limiter · failedFAULT ON INITIAL SLAT EXTENSION SLATS STUCK AT 00 FOLLOWED QRH ECAM. TRIED FLAP/SLAT LEVER EXTEND TWO TIMES SAME AS SLAT ONLY STUCK 0. PERFORMED SFCC BITE, CHECKED NR 1 SFCC FAULT CODE 00110 & NR 2 SFCC SLAT JAM LATCHED. PERFORMED FLAP/SLAT OPS CHECKED NORMAOct 5, 2012 · N720FD · Airbus A300F4622R · Leading Edge Slat Control SystemSDR FDEA201208102939Computer · faultedFLAPS STUCK AT 20 DEG ON TAKEOFF. WOULD NOT MOVE AND RECYCLE WAS NO HELP. LEFT FLAPS DOWN AFTER LANDING AT 20 DEG. NR 1 SFCC FAULTED HIGH SPEED P SWITCH AND NR 2 SFCC FAULTED FLAP JAM. R & R SCREWJACK IAW AMM 27-54-21-04, 27-54-22-04, & 27-54-24-04. CAAug 10, 2012 · N720FD · Airbus A300B4622 · Trailing Edge Flap Control SystemSDR FDEA201208102937Flap System · malfunctionedFLAPS WOULD NOT RETRACT AFTER TAKE OFF. FLAPS STUCK AT 20 DEGREES. RECYCLE, NO HELP. RETRACTED NORMAL AFTER LANDING. AFTER BLOCK IN, NOTED FLAPS WERE FULLY RETRACTED. INTERROGATED MTP, NO FAULTS. INSPECTED BOTH NR 1 & NR 2 SFCC'S. BOTH SFCC'S REGISTERED AAug 10, 2012 · N720FD · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR FDEA201203170993Flap System · malfunctionedAFTER TAKE OFF, FLAPS WOULD NOT RETRACT FROM 20 DEG COMPLIED QRH. RETURNED TO LAND IAW INSTRUCTION CARRIED OUT LUBRICATION ON LT FLAP TRACK AND JACKSCREW DRIVE UNITS. SERVICED LT FLAP TRACK TORQUE LIMITER, TEE GEAR BOX, DOWN DRIVE GEAR BOX, BEVEL GEAR AND Mar 17, 2012 · N720FD · Airbus A300B4622 · Trailing Edge Flap Control SystemSDR FDEA201201220300Rib · crackedA CRACK WAS FOUND IN THE AREA OF HOLE 47 OF LT SIDE MLG RIB NR 5 AT THE SPOT FACE, THE CRACK LENGTH WAS 33 MM. REPAIRED THE HOLE 47 OF LH MLG RIB 5 IAW EA 6-5750-149032 PART1.Jan 22, 2012 · N720FD · Airbus A300F4622R · Wing, Landing Gear Attach FittingsSDR FDEA201107082618Unknown · smokeON TAKEOFF, TOWER REPORTED "EXCESSIVE SMOKE TRAILING FROM LT WING." DID AN ATB, NO INDICATION OF SMOKE ON ACFT AND NO ECAM WARNINGS. MX NOTED NO LEAKS FROM LT WING OR ENGINE. CREW STATED NO ABNORMAL HYD QTY OR OIL QTY DECREASE DURING TAKEOFF. NO ABNORMAJul 8, 2011 · N720FD · Airbus A300B4622 · Wing StructureSDR FDEA201103040852Lug · corrodedLT MLG RIB 5 AFT PINTLE FWD LUG BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN. REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 LT MLG RIB 5 AFT PINTLE FWD LUG.Mar 4, 2011 · N720FD · Airbus A300B4622 · Wing, Landing Gear Attach FittingsSDR FDEA201103040850Bushing · failedRT MLG FIB 5 AFT PINTLE FWD BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 RT MLG AFT PINTLE FWD LUG.Mar 4, 2011 · N720FD · Airbus A300B4622 · Wing, Landing Gear Attach FittingsSDR FDEA201010053949Smoke Detector · malfunctionedLOWER FWD CARGO COMPT SMOKE ALERT. BOTH BOTTLES HAVE BEEN DISCHARGED. R&R'D BOTH FORWARD LOWER CARGO BAY SMOKE DETECTORS. AS PER A300-600 AMM 26-16-11-04, PERFORMED OPS TEST NORMALLY. OK FOR SERVICE. RAN UP ENGINES FOR 15 MINS, PACKS ON , AND COULD NOT FINOct 5, 2010 · N720FD · Airbus A300F4622R · Smoke DetectionSDR FDEA201007242656Stiffener · corrodedAVIONICS COMPARTMENT FUSELAGE STRUCTURE BELOW WASTE WATER CONNECTION BOX AT FRAME 12 STR 44L HAS CORROSION ON INTERNAL DOUBLE REMOVED LEVEL 1 CORROSION. REPLACED INTERNAL DOUBLE/STIFFENER AT WASTE WATER CONNECTION BOX IAW EA NR 6-5310-135232, DATED 7/23/10Jul 24, 2010 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201007102472Web · crackedAFT CARGO DOOR INNER SURFACE WEB, FWD OF HINGE FITTING HAS A 2" CRACK. FABRICATED WEB PLATE REPAIR IAW SRM 51-71-30 PG 201-204 INSTALLED WEB PLATE REPAIR IAW SRM 51-71-30, PG 201-204.Jul 10, 2010 · N720FD · Airbus A300F4622R · Cargo/Baggage DoorsSDR FDEA201007102471Skin · damagedRT FWD FUSELAGE EXTERNAL SKIN AT FRAME 20 COMMON TO FWD EDGE OF DOOR CUT-OUT 2 EA AREAS OF IMPACT DAMAGE. AREA 1=.500" X .250" X .316" AREA 2= 8.500" X .250" X .365" BETWEEN RT STR 36 AND 40 REMOVED DAMAGED FRAME SECTION IAW REPAIR DWG SR 30-53-001. INSTALJul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR FDEA201007102470Seat Track · crackedMAIN CARGO DECK FRAME 50, SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FR 50, SEAT TRACK 4 LT IAW SRM 51-40-21.Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007102469Seat Track · crackedMAIN CARGO DECK FRAME 48, SEAT TRACK 4 RT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 RT IAW SRM 51-40-21.Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007102468Seat Track · crackedMAIN CARGO DECK FRAME 48 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 LT IAW SRM 51-40-21.Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007102467Seat Track · crackedMAIN CARGO DECK FRAME 49 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART AT FR 49, SEAT TRACK 4 LT IAW SRM 51-40-21.Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200809053733Smoke Detector · failed"AVIONICS SMOKE" WARNING ILLUMINATED AT 9000 FT ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT LSep 5, 2008 · N720FD · Airbus A300B4622 · Smoke DetectionSDR 08FDEA03733Smoke Detector · failed"AVIONICS SMOKE" WARNING ILLUMINATED AT 9000' ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT LISep 5, 2008 · N720FD · Airbus A300B4622 · Smoke DetectionSDR 08FDEA01753Skin · damagedUPON SLAT/ K-FLAP EXTENSION, THE RT/K-FLAP PANEL CONTACTED THE UPPER CLOSE-OUT PANEL RESULTING IN DEFORMATION OF PANEL EDGES AND ATTACH LINK. REPLACED K-FLAP SKIN IAW SRM 51-40-21, REPLACED K-FLAP VANE ASSY IAW AMM 27-87-12-4. REPLACED WING WEB/FORMER IAW SRMay 5, 2008 · N720FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01148Floor Support · corrodedBULK CARGO COMPT FR 69 FLOOR SUPPORT CORRODED LBL20 AND TIE DOWN FITTING MISSING. REMOVED DAMAGED FLOOR CROSS BEAM IAW SRM 51-40-21. RECEIVED NEW FLOOR CROSS BEAM P/N NR A59374322230 BATCH NR 0001436243. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED AND Mar 26, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 08FDEA01147Shear Plate · crackedMCD FR79-80 STRING 26L ATTACH WEB CRACKED REMOVED SHEAR PLATE IAW SRM 51-40-21. FABBED SHEAR PLATE IAW MAE TRAVLER T8/731840. LOCATED AND DRILLED IAW SRM 51-40-44, ALODINED IAW SRM 51-20-10. PRIMED IAW SRM 51-20-10. INSTALLED SHEAR PLATE IAW SRM 51-40-21.Mar 26, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 08FDEA01130Floorbeam · corrodedAFT CARGO FR 67 FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION LBL 60 TO RBL 60, CROSS BEAM. REMOVED CROSS BEAM IAW SRM 51-73-10 LOCATED AND DRILLED NEW CROSS BEAM IAW SRM 51-40-44. INSTALLED CROSS BEAM IAW SRM 51-40-21.Mar 24, 2008 · N720FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 08FDEA01129Floor Support · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FR 14 AND FR 16 RBL 40 HAS CORROSION IN SEVERAL PLACES ON LOWER SURFACE AROUND FASTENER HOLES REMOVED FLOOR SUPPORT BEAM IAW SRM 51-40-21. FABRICATED NEW FLOOR SUPPORT BEAM IAW SRM 53-12-15 AND SPLICES, LOCATED ANDMar 24, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 08FDEA01016Seat Track · corrodedMAIN DECK ZONE 221, FORWARD CABIN SEAT TRACK 37.5 LBL HAS STRUCTURAL DAMAGE (HEAVY CORROSION EXFOLIATED) BETWEEN FR 15A THRU FR 19. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 5Mar 18, 2008 · N720FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00902Seat Track · corrodedMAIN DECK ZONE 221.FORWARD CABIN SEAT TRACK LBL 18 (Y450) BETWEEN FR 14 THRU FR19 HAS STRUCTURAL DAMAGES (HEAVY CORROSION, EXFOLIATION). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 5Mar 12, 2008 · N720FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00345Rib · crackedRIB NR 25 FOUND TO BE CRACKED. REPLACE DAMAGED RIB.Feb 3, 2008 · N720FD · Airbus A300B4622 · Wing, Rib/BulkheadSDR 06FDEA03634Module · malfunctionedF/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. FACT 13OCT06 06:02 ORD R REPLACED F/O ADC AND CHECK PER MM 34-11-34-4 Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static SystemSDR 06FDEA03633Indicator · malfunctionedON T/O ROLL F/O'S AIRSPEED INDICATION ON THE PFD DID NOT BREAK UNTIL THE THE CAPTAINS AIRSPEED REACHED 70KTS. (30 KT DIFFERENCE) IN WORK.Oct 13, 2006 · N720FD · Airbus A300B4622 · Airspeed/Mach IndicatorSDR 06FDEA03631Module · malfunctionedPDIS 720 34-11 0002739 13OCT06 ORD CLOSE R 1ST RTO OF 2 F/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT. PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. OFF MFG 404Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static SystemSDR 06FDEA2593Tee Fitting · leakingGREEN SYSTEM OIL QUANTITY (LOST AUTOPILOT NR 1 SPOILERS ETC) CHECKED ECAM, HYDRO SYSTEM ALMOST ZERO, PRESSURE GONE, AFTER MANUALLY LOWERING GEAR, QUANITTY CAME UP SOME. FOUND T-FITTING LEAKING ON STAB JUST O/B OFF PITCH ACT, ON LT SIDE. REMOVED T-FITTING ANJul 16, 2006 · N720FD · Airbus A300B4622 · Hydraulic System, MainSDR 05FDEA04314Frame · crackedEXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS. COMPLIED WITH EA 6-7830-923658 EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS PART 1.Dec 14, 2005 · N720FD · Airbus A300B4622R · Engine Thrust ReverserSDR 05FDEA03933Repair · unknownTHRUST REVERSER-UPPER TORQUE BOX CAP GOUGE REPAIR. COMPLIED WITH EA 6-7830-92361 THRUST REVERSER UPPER TORQUE BOX GOUGE REPAIR.Nov 21, 2005 · N720FD · Airbus A300B4622R · Engine Thrust ReverserSDR 05FDEA03902Access Door · gougedCOMPLY WITH EA 6-7830-92360, THRUST REVERSER NR 1 INBD T/R ACCESS DOOR GOUGE REPAIR. COMPLIED WITH EA 6-7830-92360.Nov 19, 2005 · N720FD · Airbus A300B4622R · Engine Thrust ReverserSDR 05FDEA03899Fitting · damagedCOMPLY WITH EA 6-5310-92351, FUSELAGE SB 53-6111, DISCREPANT BASE FITTING HOLES AT FS 45 RT. COMPLIED WITH EA 6-5310-92351B.Nov 18, 2005 · N720FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 05FDEA03847Frame · misdrilledCOMPLY WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT. COMLIED WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT.Nov 16, 2005 · N720FD · Airbus A300B4622R · Fuselage Main, FrameSDR 05FDEA03590Panel · crackedRT WING BOTTOM PNL 675 DB CUT-OUT HAS CRACK.Oct 30, 2005 · N720FD · Airbus A300B4622R · Wing, Plate/Skin
Back to N720FD, cancelled Jun 28, 2024