# Service difficulty reports: N801FD, cancelled Feb 6, 2024 A list on [N801FD, cancelled Feb 6, 2024](https://openairdocs.org/deregistered/N801FD-2024-02-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 66 reports - [SDR FDEA201802220470](https://openairdocs.org/sdr/FDEA201802220470.md): Slat System · faulted · Feb 22, 2018 · N801FD · Airbus A310324 · Leading Edge Slat Control System > DURING 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- - [SDR FDEA201802140400](https://openairdocs.org/sdr/FDEA201802140400.md): Bushing · worn · Feb 14, 2018 · N801FD · Airbus A310324 · Service Doors > R1 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 COMPONE - [SDR FDEA201702080461](https://openairdocs.org/sdr/FDEA201702080461.md): Girt Bar · detached · Feb 8, 2017 · N801FD · Airbus A310324 · Emergency Equipment > R1 DOOR WILL NOT ARM. FOUND GIRT BAR DETACHED NOT ALLOWING PROPER OPERATION REINSTALLED GIRT BAR IAW MM 25-61-22-04-01. - [SDR FDEA201611194116](https://openairdocs.org/sdr/FDEA201611194116.md): Power Supply · malfunctioned · Nov 19, 2016 · N801FD · Airbus A310324 · Escape Slide > COULD 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. - [SDR FDEA201611123995](https://openairdocs.org/sdr/FDEA201611123995.md): Warning Message · intermittent · Nov 12, 2016 · N801FD · Airbus A310324 · Escape Slide > BOTH ECAM SLIDE INDICATIONS ARE INTERMITTENT. RESET EMERGENCY SLIDE SYSTEM AND PERFORMED OPS CHECK SEVERAL TIMES IAW AMM 52-73-13-04. OPS CHECKED GOOD. - [SDR FDEA201609273375](https://openairdocs.org/sdr/FDEA201609273375.md): Indication Sys · faulty · Sep 27, 2016 · N801FD · Airbus A310324 · Landing Gear Brake System > INFORMATION 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 RUN - [SDR FDEA201602030435](https://openairdocs.org/sdr/FDEA201602030435.md): Sensor · failed · Feb 3, 2016 · N801FD · Airbus A310324 · Leading Edge Slat Control System > DUAL 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. - [SDR FDEA201404200759](https://openairdocs.org/sdr/FDEA201404200759.md): Stringer · corroded · Apr 20, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > STRINGER 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- - [SDR FDEA201404180749](https://openairdocs.org/sdr/FDEA201404180749.md): Stringer · corroded · Apr 18, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > STRINGER 44L AT FRAMES 41 - 42 CORRODED. - [SDR FDEA201404180750](https://openairdocs.org/sdr/FDEA201404180750.md): Stringer · corroded · Apr 18, 2014 · N801FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > STRINGER 45L AT FRAMES 41 - 42 CORRODED. REPAIRED IAW SRM 51-74-10 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. - [SDR FDEA201401280212](https://openairdocs.org/sdr/FDEA201401280212.md): Computer · failed · Jan 28, 2014 · N801FD · Airbus A310324 · Trailing Edge Flap Control System > DURING 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 - [SDR FDEA201204271661](https://openairdocs.org/sdr/FDEA201204271661.md): Slide · partial deploy · Apr 27, 2012 · N801FD · Airbus A310324 · Escape Slide > INADVERTENT 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, - [SDR FDEA201110154517](https://openairdocs.org/sdr/FDEA201110154517.md): Skin · corroded · Oct 15, 2011 · N801FD · Airbus A310324 · Wing, Plate/Skin > LEFT 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. - [SDR FDEA201110154518](https://openairdocs.org/sdr/FDEA201110154518.md): Skin · corroded · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Main, Plate/Skin > FORWARD 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. - [SDR FDEA201110154523](https://openairdocs.org/sdr/FDEA201110154523.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > CARGO 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. - [SDR FDEA201110154522](https://openairdocs.org/sdr/FDEA201110154522.md): Floor Panel · broken · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > CARGO 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. - [SDR FDEA201110154521](https://openairdocs.org/sdr/FDEA201110154521.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > CARGO 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. - [SDR FDEA201110154520](https://openairdocs.org/sdr/FDEA201110154520.md): Floor Panel · damaged · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > BULK 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- - [SDR FDEA201110154516](https://openairdocs.org/sdr/FDEA201110154516.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA201110154515](https://openairdocs.org/sdr/FDEA201110154515.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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- - [SDR FDEA201110154514](https://openairdocs.org/sdr/FDEA201110154514.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA201110154513](https://openairdocs.org/sdr/FDEA201110154513.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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 53-10-25-0 - [SDR FDEA201110154512](https://openairdocs.org/sdr/FDEA201110154512.md): Floor Panel · dented · Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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 53-10-25-04 - [SDR FDEA201103222041](https://openairdocs.org/sdr/FDEA201103222041.md): Power Supply · failed · Mar 22, 2011 · N801FD · Airbus A300F4605R · Emergency Lighting > DURING 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. - [SDR FDEA201011194431](https://openairdocs.org/sdr/FDEA201011194431.md): Limiter · failed · Nov 19, 2010 · N801FD · Airbus A310324 · Leading Edge Slat Control System > SLATS 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 I - [SDR FDEA200906292427](https://openairdocs.org/sdr/FDEA200906292427.md): Fitting · corroded · Jun 29, 2009 · N801FD · Airbus A310324 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR FDEA200906232556](https://openairdocs.org/sdr/FDEA200906232556.md): Cargo Track · cracked · Jun 23, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > AFT 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. - [SDR FDEA200906232436](https://openairdocs.org/sdr/FDEA200906232436.md): Skin · dented · Jun 23, 2009 · N801FD · Airbus A310324 · Wing Main, Frame Structure > RIGHT 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. - [SDR FDEA200906222519](https://openairdocs.org/sdr/FDEA200906222519.md): Floorbeam · corroded · Jun 22, 2009 · N801FD · Airbus A310324 · Fuselage Main, Floor Beam > AFT CARGO COMPT- FR60 CROSSBEAM WITH CORROSION BTW Y1300 AND Y1390. BEAM REPAIRED IAW SRM 53-10-15 FIG 207. - [SDR FDEA200906192472](https://openairdocs.org/sdr/FDEA200906192472.md): Arm · corroded · Jun 19, 2009 · N801FD · Airbus A310324 · Horizontal Stabilizer Structure > VERTICAL STABILIZER RUDDER HINGE ARM NR 4 FOUND WITH CORROSION AT VERTICAL STABILIZER CONNECTION. RUDDER HINGE ARM REPAIRED AS PER EA 6-5510-131027. - [SDR FDEA200906192468](https://openairdocs.org/sdr/FDEA200906192468.md): Skin · damaged · Jun 19, 2009 · N801FD · Airbus A310324 · Trailing Edge Flaps > RIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030 - [SDR FDEA200906162513](https://openairdocs.org/sdr/FDEA200906162513.md): Track · misrepaired · Jun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Structure > PREVIOUS 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 CONFOR - [SDR FDEA200906162473](https://openairdocs.org/sdr/FDEA200906162473.md): Skin · misrepaired · Jun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Plate/Skin > PREVIOUS 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 A - [SDR FDEA200906162459](https://openairdocs.org/sdr/FDEA200906162459.md): Skin · misrepaired · Jun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Plate/Skin > PREVIOUS 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 REPA - [SDR FDEA200906162439](https://openairdocs.org/sdr/FDEA200906162439.md): Floorbeam · misrepaired · Jun 16, 2009 · N801FD · Airbus A310324 · Fuselage Main, Floor Beam > PREVIOUS 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 RE - [SDR FDEA200906092412](https://openairdocs.org/sdr/FDEA200906092412.md): Floor Support · corroded · Jun 9, 2009 · N801FD · Airbus A310324 · Fuselage Miscellaneous Structure > CABIN - FLOOR TRACK WITH CORROSION BTW FRAMES 12A AND 13 AT Y730. TRACK WAS REPLACED AS PER SRM 51-72-10. - [SDR FDEA200906082413](https://openairdocs.org/sdr/FDEA200906082413.md): Seat Track · corroded · Jun 8, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN SEAT TRACK Y-953 CORRODED BTW FRAMES 15B AND 19. THE TRACK WAS REPLACED AS PER SRM 51-72-10. - [SDR FDEA200906082411](https://openairdocs.org/sdr/FDEA200906082411.md): Seat Track · corroded · Jun 8, 2009 · N801FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN SEAT TRACK AT Y-450 WITH CORROSION BTW FR14B AND FR19. TRACK WAS REPLACED AS PER SRM 51-72-10. - [SDR FDEA200809063752](https://openairdocs.org/sdr/FDEA200809063752.md): Tire · failed · Sep 6, 2008 · N801FD · Airbus A310324 · Tire > ON 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. - [SDR 08FDEA03752](https://openairdocs.org/sdr/08FDEA03752.md): Tire · failed · Sep 6, 2008 · N801FD · Airbus A310324 · Tire > ON 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. - [SDR 07FDEA02560](https://openairdocs.org/sdr/07FDEA02560.md): Proximity Sensor · failed · Jul 19, 2007 · N801FD · Airbus A310324 · Landing Gear Position and Warning > ON 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 PRO - [SDR 07FDEA02559](https://openairdocs.org/sdr/07FDEA02559.md): Proximity Sensor · failed · Jul 19, 2007 · N801FD · Airbus A310324 · Landing Gear Retraction/Extension System > ON 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 PROX - [SDR 07FDEA01523](https://openairdocs.org/sdr/07FDEA01523.md): Attach Fitting · corroded · Apr 18, 2007 · N801FD · Airbus A310324 · Fuselage, Landing Gear Attach Fittings > RT 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. - [SDR 07FDEA01522](https://openairdocs.org/sdr/07FDEA01522.md): Attach Fitting · corroded · Apr 18, 2007 · N801FD · Airbus A310324 · Fuselage, Landing Gear Attach Fittings > LT 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. - [SDR 07FDEA01507](https://openairdocs.org/sdr/07FDEA01507.md): Skin · dented · Apr 16, 2007 · N801FD · Airbus A310324 · Horizontal Stabilizer, Plate/Skin > THS - 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". - [SDR 07FDEA01506](https://openairdocs.org/sdr/07FDEA01506.md): Skin · dented · Apr 16, 2007 · N801FD · Airbus A310324 · Leading Edge Devices > THS-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". - [SDR 07FDEA01444](https://openairdocs.org/sdr/07FDEA01444.md): Strut · damaged · Apr 11, 2007 · N801FD · Airbus A310324 · Landing Gear Doors > RT 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. - [SDR 07FDEA01441](https://openairdocs.org/sdr/07FDEA01441.md): Skin · corroded · Apr 11, 2007 · N801FD · Airbus A310 · Wing, Plate/Skin > CORROSION 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. - [SDR 07FDEA01440](https://openairdocs.org/sdr/07FDEA01440.md): Skin · corroded · Apr 11, 2007 · N801FD · Airbus A310 · Wing, Plate/Skin > LT 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. - [SDR 07FDEA01439](https://openairdocs.org/sdr/07FDEA01439.md): Door Frame · worn · Apr 11, 2007 · N801FD · Airbus A310 · Fuselage Main, Structure > FWD 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. Next page: https://openairdocs.org/deregistered/N801FD-2024-02-06/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N801FD-2024-02-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.