N801FD, cancelled Feb 6, 2024

Service difficulty reports · 66

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 = 'N801FD' AND deregistration_id = 'N801FD-2024-02-06'
  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 FDEA201802220470Slat System · faultedDURING APPROACH, SLATS SYSTEMS 1 & 2 FAULTED, SLATS STUCK IN THE RETRACTED POSITION, RAN THE QRH, PERFORMED A NO SLAT LANDING. NO TRIPPED INDICATIONS. COMPLIED WITH TSM 27-80-02, FIG 101, & 102, REPEAT OCCURRENCE FOR BINDING, ALL SLAT SCREWJACK'S LOCK-Feb 22, 2018 · N801FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201802140400Bushing · wornR1 DOOR HARD TO OPEN FROM THE INSIDE AND OUTSIDE. INSPECTED THE R1 DOOR, AND FOUND UPPER AND LOWER HINGE SUPPORT ARM HAT BUSHINGS MIGRATED. NO DAMAGE FOUND ON R1 DOOR IAW MM 52-10-11-06. COMPLETED VISUAL INSPECTION OF R1 DOOR LOCKING & LATCHING COMPONEFeb 14, 2018 · N801FD · Airbus A310324 · Service DoorsSDR FDEA201702080461Girt Bar · detachedR1 DOOR WILL NOT ARM. FOUND GIRT BAR DETACHED NOT ALLOWING PROPER OPERATION REINSTALLED GIRT BAR IAW MM 25-61-22-04-01.Feb 8, 2017 · N801FD · Airbus A310324 · Emergency EquipmentSDR FDEA201611194116Power Supply · malfunctionedCOULD NOT GET RT SLIDE TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BOTH BATTERIES ON ASPSU IAW AMM 52-73-18-04, BITE TEST OK. R1 DOOR SLIDE ECAM INDICATION OPS NORM. REMOVED PLACARD.Nov 19, 2016 · N801FD · Airbus A310324 · Escape SlideSDR FDEA201611123995Warning Message · intermittentBOTH ECAM SLIDE INDICATIONS ARE INTERMITTENT. RESET EMERGENCY SLIDE SYSTEM AND PERFORMED OPS CHECK SEVERAL TIMES IAW AMM 52-73-13-04. OPS CHECKED GOOD.Nov 12, 2016 · N801FD · Airbus A310324 · Escape SlideSDR FDEA201609273375Indication Sys · faultyINFORMATION ONLY, REJECTED T/O 9L, PARKING BRAKE SET INDICATION, WE NEVER SET PARKING BRAKE. ONCE WE STARTED TAXI TO RUNWAY, CHECKED HANDLE DOWN POSITION, WE HAD NORMAL CONFIGURATION ON BELOW THE LINE CHECK LIST, PERFORMED RTO, SPEED BELOW 60 KTS, CLEARED RUNSep 27, 2016 · N801FD · Airbus A310324 · Landing Gear Brake SystemSDR FDEA201602030435Sensor · failedDUAL SLATS FAULT 1 & 2 ON APPROACH, 3000' MSL 170 KTS, FLAPS STUCK AT 15'. R & R SLAT COMMAND SENSOR UNIT 51CV IAW AMM 27-51-17-04. R & R BOTH SFCC'S IAW AMM 27-51-18-04. FLAP & SLATS OPERATION TESTED GOOD IAW AMM 27-81-00-05. ALSO REF TSM 27-80-07.Feb 3, 2016 · N801FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201404200759Stringer · corrodedSTRINGER 44L AT FRAMES 41 - 42 IN A/C BAY CORRODED. BLENED IAW SRM 51-74-10, PERFORMED DVI TO VERIFY NO CORROSION FOUND IAW NTM 51-70-00, PERFORMED ROTO TEST TO OPEN HOLES TO VERIFY NO CRACKS FOUND IAW NTM 51-10-01. FABRICATED THE REPAIR PARTS IAW SRM 53-Apr 20, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201404180749Stringer · corrodedSTRINGER 44L AT FRAMES 41 - 42 CORRODED.Apr 18, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201404180750Stringer · corrodedSTRINGER 45L AT FRAMES 41 - 42 CORRODED. REPAIRED IAW SRM 51-74-10 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Apr 18, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201401280212Computer · failedDURING FLAP EXTENSION, EXPERIENCED FLAP SYS 1 & 2 FAULT ILLUMINATION, FLAPS FAILED TO EXTEND. PERFORMED QRH PROCEDURE. WHEN FLAP HANDLE MOVED TO 40 DEGREES, FLAPS EXTENDED TO 40. BITE CHECKED BOTH SFCC'S & BOTH PASSED. RESET & TESTED EACH SEGMENT OF BOTH Jan 28, 2014 · N801FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201204271661Slide · partial deployINADVERTENT OPENING OF R1 CABIN DOOR STARTED INITIATION OF SLIDE DEPLOYMENT. INSTALLED R1 ESCAPE SLIDE IAW MM 25-61-20-02, AND ADJUSTMENT AND TEST IAW MM 25-61-20-05-01. OP'S CHECKED NORMAL, INSTALLED R1 PNEUMATIC EMERGENCY DOOR ASSIST BOTTLE ARMING LEVER,Apr 27, 2012 · N801FD · Airbus A310324 · Escape SlideSDR FDEA201110154517Skin · corrodedLEFT WING TOP SKIN CORRODED AT REAR SPAR RIB 4. ACCOMPLISHED REPAIR IAW EA 6-5730-149020. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 15, 2011 · N801FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201110154518Skin · corrodedFORWARD CARGO COMPARTMENT BILGE AREA OF S45R, SKIN CORRODED BETWEEN FR 38.2 AND FR 39. CUT OUT THE DAMAGED AREA. REPAIRED WITH DOUBLER AND FASTENERS IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW G.M.M. 6-2-100.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201110154523Floor Panel · dentedCARGO COMPARTMENT 162HF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 47 A532799620. REPAIR CLASSIFIED AS MINOR IAW G.M.M. 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154522Floor Panel · brokenCARGO COMPARTMENT 161GF FLOOR PANEL BROKEN. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 48 A532799630. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154521Floor Panel · dentedCARGO COMPARTMENT 161BF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 50 A532799650. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-30-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154520Floor Panel · damagedBULK CARGO COMPARTMENT 162AF FLOOR PANEL UPPER SKIN DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 51 A532799660. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154516Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UJ DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 27-R532B1231001. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154515Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242EK DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 85-R532B1231003. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154514Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252GF DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW PANEL IAW SRM 53-10-20, AND DRAWING 09-R532B1175009. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154513Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252PH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 21-B53270276015. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-0Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154512Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252UH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 34-R532B1177004. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201103222041Power Supply · failedDURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY UNIT 29WL IAW MM 33-51-14-04. ALSO, R & R EMERGENCY LIGHT BATTERY 29WL IAW MM 33-51-14-04. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE.Mar 22, 2011 · N801FD · Airbus A300F4605R · Emergency LightingSDR FDEA201011194431Limiter · failedSLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND R TORQUE LIMITER IAW MM 27-84-12-04. ALSO SERVICED LT WING SLATS, SCREW JACKS AND GEAR BOXES INov 19, 2010 · N801FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA200906292427Fitting · corrodedCORROSION WAS FOUND ON MANHOLE FITTING AT FR 23-24. REPAIR EVALUATED AND FOUND WITH CORROSION AT FWD MANHOLE INTEGRAL FITTING. MANHOLE REPLACEMENT PLUS REPAIR WERE ACCOMPLISHED IAW EA 6-5310-131032.Jun 29, 2009 · N801FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA200906232556Cargo Track · crackedAFT CARGO COMPT - TRACK ROLLER NR 4 BTW FR55/58 AND 63 CRACKED AND WITH CORROSION AT DRAIN AREA. THE TRACK WAS REPAIRED IAW SRM 53-10-15 FIG 202.Jun 23, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906232436Skin · dentedRIGHT WING FLAP OUTBOARD UPPER SKIN SURFACE WITH DEEP DENT AT FRICTION PLATE SEATING AREA BETWEEN RIB 2.5 AND RIB 3. REPAIRED IAW E.A. 6-5710-131025.Jun 23, 2009 · N801FD · Airbus A310324 · Wing Main, Frame StructureSDR FDEA200906222519Floorbeam · corrodedAFT CARGO COMPT- FR60 CROSSBEAM WITH CORROSION BTW Y1300 AND Y1390. BEAM REPAIRED IAW SRM 53-10-15 FIG 207.Jun 22, 2009 · N801FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200906192472Arm · corrodedVERTICAL STABILIZER RUDDER HINGE ARM NR 4 FOUND WITH CORROSION AT VERTICAL STABILIZER CONNECTION. RUDDER HINGE ARM REPAIRED AS PER EA 6-5510-131027.Jun 19, 2009 · N801FD · Airbus A310324 · Horizontal Stabilizer StructureSDR FDEA200906192468Skin · damagedRIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030Jun 19, 2009 · N801FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA200906162513Track · misrepairedPREVIOUS REPAIR FOUND LOCATED AT ROLLER TRACK LT, ON FWD CARGO COMPT BTW FR38- 38.1 AT STA Y140. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200906162473Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR76-77 AT ATGR 23LH-25LH, NEXT TO AFT DOOR LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA200906162459Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR25-26/32 AT STGR 41LH. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA200906162439Floorbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON FLOORBEAM RT BTW FR11A-12A AT STA Y-953. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REJun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200906092412Floor Support · corrodedCABIN - FLOOR TRACK WITH CORROSION BTW FRAMES 12A AND 13 AT Y730. TRACK WAS REPLACED AS PER SRM 51-72-10.Jun 9, 2009 · N801FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA200906082413Seat Track · corrodedFWD CABIN SEAT TRACK Y-953 CORRODED BTW FRAMES 15B AND 19. THE TRACK WAS REPLACED AS PER SRM 51-72-10.Jun 8, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906082411Seat Track · corrodedFWD CABIN SEAT TRACK AT Y-450 WITH CORROSION BTW FR14B AND FR19. TRACK WAS REPLACED AS PER SRM 51-72-10.Jun 8, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200809063752Tire · failedON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER TAKEOFF. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD.Sep 6, 2008 · N801FD · Airbus A310324 · TireSDR 08FDEA03752Tire · failedON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER T/O. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD.Sep 6, 2008 · N801FD · Airbus A310324 · TireSDR 07FDEA02560Proximity Sensor · failedON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FUTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00 -4. WHILE REPLACING 8GA PROX DETECTOR FOUND 12GA PROJul 19, 2007 · N801FD · Airbus A310324 · Landing Gear Position and WarningSDR 07FDEA02559Proximity Sensor · failedON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FURTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00-4. WHILE REPLACING 8GA PROX DETECTOR FOUND 12GA PROXJul 19, 2007 · N801FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR 07FDEA01523Attach Fitting · corrodedRT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG RT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS REF: RAS/BAC/1004683/2007 ISSUE A.Apr 18, 2007 · N801FD · Airbus A310324 · Fuselage, Landing Gear Attach FittingsSDR 07FDEA01522Attach Fitting · corrodedLT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG LT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS/BAC/1004683/2007 ISSUE A.Apr 18, 2007 · N801FD · Airbus A310324 · Fuselage, Landing Gear Attach FittingsSDR 07FDEA01507Skin · dentedTHS - FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".Apr 16, 2007 · N801FD · Airbus A310324 · Horizontal Stabilizer, Plate/SkinSDR 07FDEA01506Skin · dentedTHS-FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".Apr 16, 2007 · N801FD · Airbus A310324 · Leading Edge DevicesSDR 07FDEA01444Strut · damagedRT MLG DOOR STRUT W/SKIN SURFACE DAMAGED REPAIRED PER FEDEX EA NR 6-5280-106709 AND SRM 51-77-12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.Apr 11, 2007 · N801FD · Airbus A310324 · Landing Gear DoorsSDR 07FDEA01441Skin · corrodedCORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10-08, 51-10-01 AND 51-10-04. REPAIRED PER SRM 57-10-12 PG. 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.Apr 11, 2007 · N801FD · Airbus A310 · Wing, Plate/SkinSDR 07FDEA01440Skin · corrodedLT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.Apr 11, 2007 · N801FD · Airbus A310 · Wing, Plate/SkinSDR 07FDEA01439Door Frame · wornFWD CARGO COMPARTMENT DOOR AFT FRAME FOUND WORN AT FRAME 25 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.Apr 11, 2007 · N801FD · Airbus A310 · Fuselage Main, Structure
Back to N801FD, cancelled Feb 6, 2024