N722FD

Service difficulty reports · 191

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 = 'N722FD' 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 FDEA2020071091477Slide · inoperativeR1 MAIN CABIN ENTRY DOOR SLIDE WILL NOT ARM. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." RI SLIDE ARMS NORMAL, ECAM INDICATION ONLY IS INOP. C/7233656Jul 9, 2020 · N722FD · Airbus A300B4622R · Escape SlideSDR FDEA201906111269Oil System · leakingSHORTLY AFTER LEVEL OFF AT FL320, NOTICED ENG #2 OIL QTY SHOWING 7 QTS, WHILE ENG #1 HAD 15 QTS. WITHIN 10 MINUTES, OIL QTY CONTINUED TO DECREASE TO ZERO. DURING THAT TIME OIL PRESSURE WAS NORMAL AT 195 PSI AND OIL TEMP 140 DEGREES. RETARDED THROTTLE #2 TJun 11, 2019 · N722FD · Airbus A300B4622R · Turbine Engine Oil SystemSDR FDEA201811303396Duct · unknownPASSING THROUGH FLIGHT LEVEL 340, CABIN ALTITUDE WARNING ON ECAM ACTIVATED. VERIFIED MANUAL GAGE PASSING THROUGH 10,000 FEET CABIN ALTITUDE. SWITCHED TO MANUAL CONTROL AND ALL OUTFLOW VALVES SHOWED CLOSED, BUT CABIN ALTITUDE STILL CLIMBED PASSING 12,000 FEET. Nov 30, 2018 · N722FD · Airbus A300B4622R · Air Distribution SystemSDR FDEA201806301628Frame · corrodedFUSELAGE FR39, BETWEEN STR 52L AND STR 54L, FRAME WITH INTER-GRANULAR CORROSION. REPAIRED THE CORRODED FUSELAGE TEE BEAM AT FR39 S52L-S54L. THIS REPAIR CATEGORY IS "C", REPAIR LIFE LIMITATION IS 6 MONTHS. MAJOR REPAIR IAW GMM6-2-100.Jun 30, 2018 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201806181624Floor Support · corrodedMDCC - FR11-FR12, Y730, FLOOR SUPPORT WITH EXFOLIATING CORROSION. REPLACED MDCC FLOOR SUPPORT BETWEEN FR11 AND FR13A, Y730 PER SRM51-40-21. THIS REPAIR IS CATEGORY "A". MAJOR REPAIR IAW GMM6-2-100.Jun 18, 2018 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201806181587Stiffener · corrodedLAVATORY SERVICE PANEL CUTOUT STIFFENER WITH INTER-GRANULAR CORROSION AT LOWER EDGE, BETWEEN FR12 AND FR12A. REPLACED THE CORRODED STIFFENER OF LAVATORY SERVICE PANEL CUTOUT PER SRM 51-40-21.THIS REPAIR CATEGORY IS"A" MAJOR REPAIR IAW GMM6-2-100.Jun 18, 2018 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201806181574Floor Support · corrodedMDCC FLOOR - FR11-FR13 Y953, FLOOR SUPPORT WITH CORROSION AROUND BOLTHOLES. REPLACED MDCC FLOOR SUPPORT BETWEEN FR11 AND FR15A, Y953 PER SRM 51-40-21. THIS REPAIR IS CATEGORY "A". MAJOR REPAIR IAW GMM6-2-100.Jun 18, 2018 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201804040853Connector · damagedMULTIPLE ELECTRICAL FAILURES ON GROUND AND AIRBORNE, SOME RESET SOME DID NOT. ON GROUND ELECTRICAL SURGE DESELECTED ALL PADDLE SWITCHES, ACARS, FMS, AND FCP. 2. AIRBORNE RA 1 AND 2, TCAS, GPWS, LAND INHIBITED. VOR 1 FLAG. 3. R74 CB WAS POPED ON PREFLApr 4, 2018 · N722FD · Airbus A300B4622R · Electrical Power System WiringSDR FDEA201802240481Slat System · malfunctionedDURING APPROACH, SELECTED SLATS & FLAPS 15/0. RECEIVED SLAT 1 AND SLAT 2 FAULTS. CYCLED THE SLAT/FLAP HANDLE, STILL HAD FAULTS. RAN QRH. LANDED WITH SLATS AT 0 DEGREES AND FLAPS AT 40 DEGREES. CHECKED BOTH THE NR 1 & 2 SFCCS AND FOUND JAMB CODE ON BOTH Feb 24, 2018 · N722FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201710132929Wire · misinstalledNR 4 MAIN TIRE BLEW ON LANDING. ANTI-SKID DID NOT RELEASE. CONNECTOR AT 18GG RECEPTICALS A & C AT CONNECTION ON NR 4 BRAKE SERVO VALVE INSTALLED IN WRONG POSITIONS. INSERTED WIRE (A)-4063 INTO A, AND INSERTED WIRE (C) -4062 INTO C IAW WDM 32-42-05, AND SCOct 13, 2017 · N722FD · Airbus A300B4622R · Landing Gear System WiringSDR FDEA201702060446Battery · failedRIGHT ENTRY DOOR SLIDE WILL NOT ARM. R1 DOOR CHECKED FOR CORRECT ARMING. NR 1 BATTERY AT POWER SUPPLY UNIT AUTOMOUS STANDBY, REMOVED AND INSTALLED BATTERY. OPS CHECKED IAW 52-73-18-04. ASPSU TESTED OK. PERFORMED SLIDE RELEASE WIRING TEST IAW AMM 52-73-00-Feb 6, 2017 · N722FD · Airbus A300B4622R · Escape SlideSDR FDEA201610223682Circuit Breaker · malfunctionedR1 DOOR WILL NOT INDICATE THE SLIDE ARMED ON ECAM. CIRCUIT BREAKER RESET GOOD. DOOR SLIDE INDICATION SYSTEM TESTED GOOD IAW MM 52-73-00.Oct 22, 2016 · N722FD · Airbus A300B4622R · Escape SlideSDR FDEA201607282645Gcu · failedON INITIAL CLIMB, NR 2 GENERATOR FAILED. REMOVED AND REPLACED THE NR 2 GCU IAW AMM 24-22-12-04, TESTED OK. RAN NR ENGINE AW JRH, GENERATOR TESTED OK.Jul 28, 2016 · N722FD · Airbus A300B4622R · AC RegulatorSDR FDEA201606252139Relief Valve · faultyON CLIMBOUT, APPROXIMATELY 2500' GOT ECAM, GROUND HYD RESERVOIR LOW AIR PRESSURE, PRESSURE WAS STEADY, ECAM CLEARED ITSELF. GOT SAME ECAM ON FINAL, APPROXIMATELY 1500' EXECUTED GO AROUND. RETURNED TO DEPARTURE. REMOVED AND REPLACED PRESSURE RELIEF VALVE PERJun 25, 2016 · N722FD · Airbus A300B4622R · Hydraulic Pressure Relief Valve, MainSDR FDEA201601280330Beam · crackedUPPER CTR WING SECTION STRUCTURE, RT BEAM NR 3 JUNCTION AT FRAME 46, UPPER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0322973 P 1. DAMAGE IN HOLES OF BEAM 2 RT & BEAM 3 RT & BEAM 2 LT, MDCC FRAME 46. REPAIRED UPPER CTR WING SECTION STRUCTURE, RT BEAM Jan 28, 2016 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201601280329Beam · crackedUPPER CTR WING SECTION STRUCTURE, RT BEAM NR 2 JUNCTION AT FRAME 46, LOWER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0322973 P 1. FUSELAGE - MAINFRAME - DAMAGE IN HOLES OF BEAM 2 RT & BEAM 3 RT & BEAM 2 LT, MDCC FRAME 46. REPAIRED JUNCTION AT FRAMEJan 28, 2016 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201601280328Beam · crackedUPPER CTR WING SECTION STRUCTURE, LT BEAM NR 2 JUNCTION AT FRAME 46, LOWER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0322973 P 1. DAMAGE IN HOLES OF BEAM 2 RT & BEAM 3 RT & BEAM 2 LT, MDCC FRAME 46. REPAIRED UPPER CTR WING SECTION STRUCTURE, LT BEAM Jan 28, 2016 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201601150154Web · crackedMDCC UNDER FLOOR, ONE EACH WEB, CRACKED AT FRAME 47, Y953 ~ Y1456. REPAIRED THE WEB IAW SRM 53-15-15 FIGURE 201. THE REPAIR WAS CATEGORY B & INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 24000 FC & FH NOT RELEVANT. SUBSEQUENT INSPECTION AT INTERVAL OF 3000 FJan 15, 2016 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201601150153Web · crackedMDCC UNDER FLOOR, ONE EACH WEB, CRACKED AT FRAME 47, -Y953 ~ -Y1456. FABRICATED THE NEW WEB IAW DWG A53832103 & MARKED AS FX A5383210320600 IAW GMM 7-0-1001. REPLACED THE CRACKED WEB OF MDCC FRAME 47, -Y953 ~ -Y1456 IAW SRM51-40-21. MAJOR REPAIR IAW GMM 6-2Jan 15, 2016 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201601150152Web · crackedMDCC UNDER FLOOR, ONE EACH WEB CRACKED, AT FRAME 47, Y0~Y450. REPAIRED THE WEB IAW SRM 53-15-15 FIGURE 201. THE REPAIR WAS CATEGORY B & INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 24000 FC & FH NOT RELEVANT. SUBSEQUENT INSPECTION AT INTERVAL OF 3000 FC & FHJan 15, 2016 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201601150151Web · crackedMDCC UNDER FLOOR, ONE EACH WEB CRACKED, AT FRAME 47, Y0 -Y450. FABRICATED THE NEW WEB IAW DWG A53832100. REPLACED THE CRACKED WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Jan 15, 2016 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201601120115Stringer · corrodedAV COMPARTMENT BELOW RT FLOOR FUSELAGE INTERNAL STRUCTURE, BETWEEN FRAME 11 & 11A, FOUND CORROSION ON BOTTOM STRINGER. COMPLIED WITH EA 6-5310-T0323047 P 1. REPLACED NLG BULKHEAD, RT SIDE LATERAL KEEL BEAM AT FRAME 11 - 11A. MAJOR REPAIR IAW GMM 6-2-100.Jan 12, 2016 · N722FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201512244081Hinge Bracket · damagedDURING WALK AROUND, FOUND RT FOLDING NOSE DROP A LITTLE BIT, FURTHER TROUBLESHOOTING FOUND HINGE BRACKET ASSEMBLY BROKEN APART. THE HINGE BRACKET REF TO IPC 27-81-33-01 ITEM 310.FOLDING NOSE BENT & CRACKED, NEED TO REPLACE. FURTHER INSPECTION FOUND THE LEADIDec 24, 2015 · N722FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201512164016Hook And Loop · looseFIRST OFFICER ESCAPE ROPE COVER KEEPS FALLING DOWN. THE VELCRO BACKING NEEDS TO BE REPLACED. R & R VELCRO BACKING FROM FIRST OFFICERS ESCAPE ROPE COVER PANEL IAW SMP, SECURED SAID PANEL. CONDITION NOW SATISFACTORY. ACFT OK FOR SERVICE.Dec 16, 2015 · N722FD · Airbus A300B4622R · Emergency EquipmentSDR FDEA201410113112Frame · crackedNOSE WW LT AFT CUT OUT LOWER FRAME 17 HAS ONE CRACK. REPAIRED IAW EA 6-5330-T0312514 PT1. REPAIR MINOR IAW GMM 6-2-100.Oct 11, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201410032942Fitting · crackedRT SIDE CONNECTION FITTING IN NLG BAY BETWEEN FRAMES 13A & 14 FOUND A CRACK MORE THAN 2.5 MM. REPAIRED IAW EA T6-5310-73832 P1. MAJOR REPAIR IAW GMM 6-2-100Oct 3, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201410032939Stringer · corrodedAFT CARGO BAY STRINGER 54L FOUND CORRODED AT FRAME 63. REPAIRED THE STRINGER IAW SRM 53-10-14 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201410022910Floor Support · delaminatedMAIN DECK, FRAMES 11 - 14 Y730 FLOOR SUPPORT DELAMINATED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21, MAJOR REPAIR IAW GMM 6-2-100.Oct 2, 2014 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201410022911Frame Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26L FOUND CRACKED. REPAIRED IAW EO 6-5310-7-5017 C PT5. MAJOR REPAIR IAW GMM 6-2-100.Oct 2, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201409302861Stringer · corrodedAFT CARGO BAY STRINGER 55L, FOUND CORRODED BETWEEN FRAMES 58 & 60. REPAIRED THE STRINGER IAW SRM 53-10-14 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201409302862Floor Support · corrodedBULK CARGO BAY FRAME 65 - Y805 FLOOR SUPPORT DELAMINATED. REPLACED THED FLOOR SUPPORT IAW SRM 51-40-21 MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201409302864Floorbeam · corrodedBULK CARGO BAY, FRAME 66 - Y494 FLOORBEAM DELAMINATED. REPLACED THE FLOORBEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201409302863Floorbeam · corrodedBULK CARGO BAY FRAME 65 - Y805 FLOORBEAM DELAMINATED. REPLACED THE FLOORBEAM IAW SRM 51-40-21 MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201409292849Frame Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 & 26 LT HOLE C FOUND CRACK SIGNAL. REPAIRED IAW EO 6-5310-7-5017 C PT5. MAJOR REPAIR IAW GMM 6-2-100.Sep 29, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201409262803Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE G FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312477 P1. MAJOR REPAIR IAW GMM 6-2-100.Sep 26, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201409262802Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE G FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312477 P1. MAJOR REPAIR IAW GMM 6-2-100Sep 26, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201409262801Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312477 P1.Sep 26, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201409262800Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE A FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312477 P1. MAJOR REPAIR IAW GMM 6-2-100Sep 26, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201409252765Stringer · corrodedAFT CARGO STRINGER 54L FOUND CORRODED AT FRAME 62. REPAIRED IAW SRM53-10-14 FIG 201, SHEET 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 25, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201409252764Stringer · corrodedAFT CARGO STRINGER 54L FOUND CORRODED BETWEEN FRAMES 59 & 60. REPAIRED IAW SRM 53- 10-14 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Sep 25, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201409252763Frame · crackedLOWER HOLE OF CTR WING JOINT AT FRAME 40L HAS A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312351 PT1. MAJOR REPAIR IAW GMM 6-2-100Sep 25, 2014 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201405110983Jackscrew · contaminatedAFTER DEPARTURE, WITH FLAPS 15/20, DURING RETRACTION, FLAP SYS 1 & SYS 2 FAULTED. FLAP HANDLE CYCLED, FLAP STUCK AT 15/20, IAW ECAM GPWS SWITCH TO OVERIDE. IAW QRH FLAP HANDLE SELECTED TO 30/40 FLAP WENT TO 30/40 FAULT LIGHTS EXTINGUISHED. AFTER LANDING FLMay 11, 2014 · N722FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA201401220178Switch · failedEMERGENCY LIGHT TEST SWITCH AT DOOR 1L NOT WORKING. COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS TEST FUNCTION INOPERATIVE. CHECK FOUND THE TEST PBSW 25WL INTERMITTENT. R & R THE SWITCH IAW ESPM. PERFORMED EMERGENCY LIGHT TEST IAW AMM 33-51-00-05-09,TEST Jan 22, 2014 · N722FD · Airbus A300B4622R · Emergency LightingSDR FDEA201306121283Fmc · failedAFTER LEVEL OFF AT 9800 M, LOST NR 2 FMC COMPLETELY. FMC UNAVAILABLE MESSAGE SHOWED ON NR 2 FMC CDU. TROUBLESHOT IAW TSM34-60-00/P107, R & R NR 2 FMC IAW AMM34-68-34-04, CROSSLOADED FMC DATABASE IAW AMM 34-60-00-03-09. PERFORMED FMS OPS TEST SATIS IAW AMMJun 12, 2013 · N722FD · Airbus A300B4622R · Flight Management Computing Hardware SystemSDR FDEA201304170796Skin · dentedLEFT WING NR 1 SLAT LIP SKIN FOUND WITH TWO DENTS NEAR FASTENER. REPAIRED IAW SRM 51-73-10, PAR 3B.Apr 17, 2013 · N722FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201304100761Cascade · damagedRT ENGINE OUTBOARD THRUST REVERSER COWL CASCADE BROKEN & MISSING AT 1 O`CLOCK. REPLACED COWL CASCADE PER AMM78-32-12-04. PERFORMED AN OPS TEST OF RT THRUST REVERSER PER AMM78-32-11-05, TEST PASSED.Apr 10, 2013 · N722FD · Airbus A300B4622R · Engine Thrust ReverserSDR FDEA201104291674Spar · crackedULTRASONIC INSP CARRIED OUT ON LT WING, FOUND ULTRASONIC INDICATION MORE THAN 30 PERCENT ON THE HOLE 'B' AT REAR SPAR UPPER CHORD OTBD OF RIB 9. REPAIRED AS PER E.A. 6-5730-150317 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 29, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281669Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CENTER WING BOX CENTER SPAR, AT RIGHT CUT-OUT DOUBLER RUNOUT RIGHT SIDE UPPER HOLE SECOND LAYER AT 6 O' CLOCK POSITION LOOKING FORWARD. CRACKED AT CENTER WING BOX CENTER SPApr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281668Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CENTER WING BOX CENTER SPAR, AT RIGHT HAND CUT-OUT DOUBLER RUNOUT LEFT SIDE LOWER HOLE FIRST LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. CRACKED AT CENTER WING BOX CENApr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281667Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT LOWER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSApr 28, 2011 · N722FD · Airbus A300B4622R · Wing Spar
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