# Service difficulty reports: N804FD, cancelled Mar 2, 2024 A list on [N804FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N804FD-2024-03-02.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 3 · 119 reports - [SDR FDEA201609153243](https://openairdocs.org/sdr/FDEA201609153243.md): Coalescer Bag · odor · Sep 15, 2016 · N804FD · Airbus A310324 · Humidity Control System > AFTER PARKING, THE AVIONICS SMOKE WARNING SOUNDED. PULLED CIRCUIT BREAKERS, TURNED ON OVERRIDE NR 1 AND 2 AND OPEN THE AVIONICS HATCH, SMELLED SMOKE. POWERED DOWN THE AIRCRAFT AND EVACUATED. R & R LT AND RT COALESCER BAGS IAW AMM 21-51-16-04. AFTER ENGINE - [SDR FDEA201607192536](https://openairdocs.org/sdr/FDEA201607192536.md): Smoke Detector · faulty · Jul 19, 2016 · N804FD · Airbus A310324 · Smoke Detection > "AVIONICS SMOKE" DISPLAYED ON ELECTRICAL PANEL AFTER ENGINE SHUTDOWN AT GATE. NO SMOKE WAS EMITTED ON THE SNIFFER FAN. R & R SMOKE DETECTOR. - [SDR FDEA201511193714](https://openairdocs.org/sdr/FDEA201511193714.md): Bracket · damaged · Nov 19, 2015 · N804FD · Airbus A310324 · Fluid Service Doors > ON POST FLIGHT FOUND FUELING DOOR 144DR MISSING WITH DAMAGE TO RT PACK INLET FAIRING. REPLACED BROKEN COOLING DUCT SUPPORT BRACKET IAW SRM 51-72-10. REMOVED AND REPLACED R/H AIR INLET FAIRINGS DUCT AND REFUELING PANEL DOOR ASSY IAW MM 53-15-73-04 AND 52-42- - [SDR FDEA201510313432](https://openairdocs.org/sdr/FDEA201510313432.md): Actuator · leaking · Oct 31, 2015 · N804FD · Airbus A310324 · Drag Control Actuator > BLUE RESERVOIR LO LEVEL ECAM WITH ASSOCIATED SPOILERS FAULTS. FOLLOWED ECAM & QRH, RETURNED FOR UNEVENTFUL LANDING. FOUND NR 3 RT SPOILER ACTUATOR, SIDE CAP BLOWN OUT, REQUIRES ACTUATOR PART. R & R NR 3 RT SPOILER ACTUATOR IAW AMM 27-64-14-04. OPERATIONAL - [SDR FDEA201510303445](https://openairdocs.org/sdr/FDEA201510303445.md): Computer · failed · Oct 30, 2015 · N804FD · Airbus A310324 · Central Warning > DURING LANDING, GEAR EXTENSIONS WITH POSITION DETECTOR, SYS NR 2 SELECTED, GOT ECAM, LG DOOR SYS INOPERATIVE UNTIL ALL GEARS WERE DOWN & LOCKED. SYS NR 1 MEL'D, INOPERATIVE. R & R NR 2 FLIGHT WARNING COMPUTER IAW AMM 31-53-34-04. PERFORMED ECAM & LG WARNING - [SDR FDEA201503060700](https://openairdocs.org/sdr/FDEA201503060700.md): Slide · unwanted deploy · Mar 6, 2015 · N804FD · Airbus A310324 · Escape Slide > DOOR R1 SLIDE DEPLOYED ACCIDENTALLY AT BLOCK. REMOVED AND REPLACED THE R1 SLIDE IAW MM 25-61-22-04-02, ARMED THE R1 SLIDE OPS TEST IAW MM 52-73-00-05. REMOVED AND REPLACED THE DIAPHRAGM AND SERVICED THE EMERGENCY OPERATION CYLINDER OF R1 DOOR IAW AMM 52-1 - [SDR FDEA201409112578](https://openairdocs.org/sdr/FDEA201409112578.md): Skin · corroded · Sep 11, 2014 · N804FD · Airbus A310324 · Fuselage Main, Plate/Skin > AV COMPARTMENT FUSELAGE SKIN FRAME 16A - 17 STRINGER 44 - 45 RT INNER SURFACE FOUND CORROSION. COMPLIED WITH EA 6-5310-T0310792 P1 EA TITLE FUSELAGE MAIN FRAME CORROSION INTERNAL DOUBLER AT FRAME 16A - 17. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201409012391](https://openairdocs.org/sdr/FDEA201409012391.md): Repair · debonded · Sep 1, 2014 · N804FD · Airbus A310324 · Trailing Edge Flaps > AGING INSPECTION - EXISTING REPAIR ON LT WING I/B FLAP TRAILING EDGE RIB8-10 UPR & LWR SURFACE. REPAIR PATCH DISBONDED. REPORTED TO ENGINEER. REMOVED THE OLD REPAIR PATCH & REPAIRED THE DAMAGE PER A310 SRM 57-52-12 FIG 204 EO 6-5100-7-5000 PART1 WAS COMPLE - [SDR FDEA201408222288](https://openairdocs.org/sdr/FDEA201408222288.md): Fastener · missing · Aug 22, 2014 · N804FD · Airbus A310324 · Fuselage Miscellaneous Structure > AGING INSPECTION EXISTING REPAIR ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59 & 64 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND THE REPAIR WAS MISSING A FASTENER, WAS FOUND COMPARED WITH EA 6-5317-81082 TITLE:FUSELAGE -DEVIATION FR - [SDR FDEA201408202239](https://openairdocs.org/sdr/FDEA201408202239.md): Repair · debonded · Aug 20, 2014 · N804FD · Airbus A310324 · Trailing Edge Flaps > AGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 5 - 7 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR PATCH DISBONDED REMOVED OLD REPAIR PATCH & DAMAGE CORE IT EXCEEDED THE REPAIRABLE LIMIT PER A310SRM57-52-12 FIG 204 REPORTED TO EN - [SDR FDEA201408202238](https://openairdocs.org/sdr/FDEA201408202238.md): Repair · debonded · Aug 20, 2014 · N804FD · Airbus A310324 · Trailing Edge Flaps > AGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 3 - 5 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED AND FOUND THE OLD REPAIR PATCH DISBONDED. REMOVED OLD REPAIR PATCH & DAMAGE CORE REPORTED TO ENGINEER. REPAIRED T - [SDR FDEA201408202242](https://openairdocs.org/sdr/FDEA201408202242.md): Repair · corroded · Aug 20, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > AGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 16 & 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS FOUND CORRODED HEVAILY. THE REPAIR ANGLE FITTING WAS REPLACED IN SNRM:N00360 AND COMPLETED TITLE: AV COMPT- STRINGER 4 - [SDR FDEA201408202241](https://openairdocs.org/sdr/FDEA201408202241.md): Stringer · corroded · Aug 20, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > AGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 15A & 16 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND THE STRINGER CORRODED HEVAILY. THE OLD REPAIR AND STRINGER WAS REMOVED AND RE-REPAIRED WITH A NEW - [SDR FDEA201408072106](https://openairdocs.org/sdr/FDEA201408072106.md): Stringer · corroded · Aug 7, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > AV COMPARTMENT STRINGER 44 RT FOUND HEAVY CORROSION AT FRAME 16 LOCATION. COMPLIED WITH EA 6-5310-T0310620 PART 1 TITLE:FUSELAGE MAINFRAME SECTION 12. CORROSION ON STRINGER S-44 RH AT FR 16. THE REPAIR WAS CATEGORY "B' AND WAS CLASSIFIED AS MAJOR PER GMM 6 - [SDR FDEA201407281996](https://openairdocs.org/sdr/FDEA201407281996.md): Computer · failed · Jul 28, 2014 · N804FD · Airbus A310324 · Fuel Quantity Indicator > PASSING 10000 FT TRIM TANK PUMPS ECAM MSG FUEL QTY SHOWED 34K TOTAL, 64.2 TAKEOFF FUEL. ECAM MSG SELF-CLEARED & FUEL SLOWLY ROSE AGAIN, FUEL WAS GOOD. AFTER TAKEOFF PLUS 45 MIN TOTAL LOSS OF FUEL QTY SYS. RTB SENSOR STATUS SHOWED FQ 3 FAIL. R & R FQIC IAW - [SDR FDEA201406281576](https://openairdocs.org/sdr/FDEA201406281576.md): Pulley · defective · Jun 28, 2014 · N804FD · Airbus A310324 · Aileron Control System > ON DEPARTURE CLIMB WITH AUTO PILOT NR 2 ON WHEN THE SLATS WERE RETRACTED THE ACFT GAVE VERY HARD TO THE RT. THE AILERONS COMPENSATED BY GOING LT 6 UNITS. AT THIS POINT WE CHECKED THE FLIGHT CONTROL POS PAGE & SPOILERS 7, 6 & 5 ON THE LT WING WERE UP. AFTER - [SDR FDEA201405110982](https://openairdocs.org/sdr/FDEA201405110982.md): Rib · corroded · May 11, 2014 · N804FD · Airbus A310324 · Wing, Rib/Bulkhead > LEFT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-1. MAJOR REPAIR. - [SDR FDEA201405110981](https://openairdocs.org/sdr/FDEA201405110981.md): Rib · corroded · May 11, 2014 · N804FD · Airbus A310324 · Wing Spar > RIGHT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-2, WING BASIC WING STRUCTURE, LT & RT RIB 5 FWD LUG CORROSION. MAJOR REPAIR. - [SDR FDEA201402140320](https://openairdocs.org/sdr/FDEA201402140320.md): Tru · faulted · Feb 14, 2014 · N804FD · Airbus A310324 · DC Rectifier/Converter > ESS TR INDICATED 4A NUMEROUS TIMES IN CRUISE. FOUND ONLY 4A ON ESS TR & I ESS TRANSFORMER RECTIFIER IAW MM 24-32-11-04. OPERATIONS CHECK SATISFACTORY RUN NR 2 ENG IAW A310JRH. GOOD DC LOAD DISTRIBUTION, ACFT OK FOR SERVICE. - [SDR FDEA201202160589](https://openairdocs.org/sdr/FDEA201202160589.md): Spar · damaged · Feb 16, 2012 · N804FD · Airbus A310324 · Nacelle/Pylon, Main Frame > RT PYLON SPIGOT RECEPTACLE FITTING FOUND A MISDRILLED BOLT HOLE. REPAIRED IAW AMM 54-50-00 AND AMM 20-21-12 - [SDR FDEA201202100542](https://openairdocs.org/sdr/FDEA201202100542.md): Skin · contaminated · Feb 10, 2012 · N804FD · Airbus A310324 · Rudder, Plate/Skin > TWO WATER TRAPPED AREAS WERE FOUND AT RT RUDDER NR 27 SCREW (5.5" X 5") AND NR 38 SCREW (3" X 1.5") (EO 6-5530-7-5004, PART 2) NDT INSPECT L/E AND T/E. THE OUTER SKIN AND EVLUATED THE DIMENSION OF THE DAMAGED AREA ARE 5.5"X5" (NR 27 SCREW) AND 3"X1.5" (N - [SDR FDEA201202100543](https://openairdocs.org/sdr/FDEA201202100543.md): Skin · corroded · Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 4 AND RIB 6. PERFORMED THE REPAIR IAW EA 6-5730-1490. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR. - [SDR FDEA201202100541](https://openairdocs.org/sdr/FDEA201202100541.md): Skin · corroded · Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > LEFT WING BOTTOM SKIN UPPER SURFACE CORRODED AT RIB 5 REINFORCING BEHIND REAR SPAR AREA. REMOVED CORROSION IAW EA 6-5730-149035. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. - [SDR FDEA201202040470](https://openairdocs.org/sdr/FDEA201202040470.md): Skin · dented · Feb 4, 2012 · N804FD · Airbus A310324 · Fuselage Main, Plate/Skin > NOSE SECTION RT LOWER HALT SKIN PLATE EXTERNAL HAS A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR2 AND FR3 POSITION 1. PAIN REMOVED IAW SRM 51-75-20. CUT OUT THE DAMAGED AREA. REPAIRED THE REWORK AREA WITH FASTENERS AND DOUBLER REFER TO SRM 53- - [SDR FDEA201201110095](https://openairdocs.org/sdr/FDEA201201110095.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND WITHIN THE ALLOWABLE DAMAGE LIMIT IAW SRM 57-20-12. RESTORED SURFACE PROTECTION IAW SRM 51-49-00 AND - [SDR FDEA201201110094](https://openairdocs.org/sdr/FDEA201201110094.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR MIDDLE SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND - [SDR FDEA201201110096](https://openairdocs.org/sdr/FDEA201201110096.md): Floor Support · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Fuselage Miscellaneous Structure > FWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORRODED FROM FR 12 TO FR 14 BETWEEN Y 383 AND Y 953. REPLACED WITH NEW SUPPORT IAW SRM 51-40-21 AND 51-72-10. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. - [SDR FDEA201201110093](https://openairdocs.org/sdr/FDEA201201110093.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION AT RIB 7. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51-21-10. REPAIR - [SDR FDEA201201110091](https://openairdocs.org/sdr/FDEA201201110091.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPERSKIN NEAR FRONT SPAR FOUND CORRODED, POSITION BETWEEN RIBS 16 AND 17. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51- - [SDR FDEA201201110090](https://openairdocs.org/sdr/FDEA201201110090.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 20 AND RIB 21. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED SURFACE PROTECTION IAW SRM 51-49-00 AND 5 - [SDR FDEA201201110089](https://openairdocs.org/sdr/FDEA201201110089.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 25 AND RIB 26. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND 51-2 - [SDR FDEA201201110088](https://openairdocs.org/sdr/FDEA201201110088.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RT WING UPPER SKIN FOUND CORROSION POSITION ABOUT RIB 27 BESIDE THE OTBD JET FUEL PANEL. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49-00 AND - [SDR FDEA201201110086](https://openairdocs.org/sdr/FDEA201201110086.md): Skin · corroded · Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/Skin > RT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 28 AND RIB 29. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FOUND WITHIN THE ALLOWABLE DAMAGE LIMITS IAW SRM 57-20-12. RESTORED THE SURFACE PROTECTION IAW SRM 51-49 - [SDR FDEA201201080046](https://openairdocs.org/sdr/FDEA201201080046.md): Seat Track · chafed · Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y0. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16 A53274256. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. - [SDR FDEA201201080045](https://openairdocs.org/sdr/FDEA201201080045.md): Seat Track · chafed · Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y1456. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16, A53274256. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. - [SDR FDEA201110174555](https://openairdocs.org/sdr/FDEA201110174555.md): Engine · failed · Oct 17, 2011 · N804FD · Airbus A310324 · Engine (Turbine/Turboprop) > CLIMBING THRU FL300 F/O FELT SLIGHT VIBRATION, BUT NO INDICATIOINS OR ECAM AT FL 355, THERE WAS A YAW AND LOUD BANGING, EPR HAD DROPPED TO BELOW 1, OTHER ENGINE INSTRUMENTS LOOKED NORMAL, BUT THE LOUD BANGING CONTINUED WITH THROTTLE AT IDLE. OIL PRESSURE WAS - [SDR FDEA201010093981](https://openairdocs.org/sdr/FDEA201010093981.md): Damper · leaking · Oct 9, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension System > LANDING GEAR WOULD NOT RETRACT ON DEPARTURE, RETURNED TO RPVM, HAD LANDING GEAR RETRACTION FAULT PROX. DETECTION BOX FAULTED TO "BR" - BOGIE RIGHT FAIL. ON INSPECTION RT MAIN GEAR, FOUND PITCH DAMPER BUTTON POPPED OUT. FAILED RETRACTION ON BOTH SYSTEMS. C - [SDR FDEA201010073974](https://openairdocs.org/sdr/FDEA201010073974.md): Selector Valve · failed · Oct 7, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension System > LOWERED MLG HANDLE (WITH SYS 2, POSITION DET SELECTED) GOT UNLOCK LIGHTS BUT NO MLG DOWN, SELECTED SYS 1, NO CHANGE, RAISED MLG HANDLE, LIGHTS WENT OUT, LOWERED MLG AGAIN IN SYS 2, AND MLG CAME DOWN NORMALLY. BITE ON PROX BOX, NO FAULT REGISTERED, FOLLOWED TS - [SDR FDEA201009263715](https://openairdocs.org/sdr/FDEA201009263715.md): Connector · dirty · Sep 26, 2010 · N804FD · Airbus A310324 · Electrical Power System Wiring > CLIMBING THROUGH FL330 GOT RT R1 DOOR NOT CLOSED COMPLIED WITH QRH AND DESCENTED BELOW 10,000. GOING THROUGH FL200 THE WARNING WENT AWAY. ATC WOULD NOT LET US CONTINUE AT 10,000 SO RETURNED TO DEPARTURE. CABIN PRESSURE WAS GOOD. ALL NORMAL, CLEANED THE CON - [SDR FDEA201008263146](https://openairdocs.org/sdr/FDEA201008263146.md): Pitot Head · contaminated · Aug 26, 2010 · N804FD · Airbus A310324 · Pitot/Static System > F/O A/S INOP DURING T/O ROLL ABORTED T/O. PVG U CHECKED F/O PITOT TUBE FOUND A BUG INSIDE, CLEARED PITOT TUBE AND PERFORMED THE PITOT TUBE INSP ALL OK IAW AMM 34-11-15-6, PERFORMED AUTO LAND SYS TEST PASSED IAW AMM 22-00-00, ACFT REMAINED CAT 3III, ACFT OK - [SDR FDEA200912104401](https://openairdocs.org/sdr/FDEA200912104401.md): Skin · misrepaired · Dec 10, 2009 · N804FD · Airbus A310324 · Leading Edge Devices > PREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT UPPER NOSE SKIN BETWEEN RIBS 14 TO 17 MEASURES 11.7 INCHES X 9.8 INCHES. PREVIOUSLY INSTALLED REPAIR LOCATED AT LT WING NR 2 SLAT UPPER NOSE SKIN BETWEEN RIBS 14 TO 17 WAS DETERMINE NOT TO BE IAW EA6-5710-8101 - [SDR FDEA200912104400](https://openairdocs.org/sdr/FDEA200912104400.md): Skin · misrepaired · Dec 10, 2009 · N804FD · Airbus A310324 · Fuselage Main, Plate/Skin > PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RT SIDE FUSELAGE SKIN AT FRAME 74 AND BETWEEN STRINGERS 39 TO 41 RT MEASURES 9 INCHES X 7.2 INCHES, WITH A SKIN CUTOUT BETWEEN STRINGERS 39 AND 40 RT MEASURES 2.7 INCHES X 1.7 INCHES. PREVIOUSLY INSTALLED REPAIR LOCA - [SDR FDEA200912074364](https://openairdocs.org/sdr/FDEA200912074364.md): Skin · corroded · Dec 7, 2009 · N804FD · Airbus A310324 · Wing, Plate/Skin > LT WING UPPER SURFACE GRAVITY FUEL PORT INBD HAS LEVEL 1 CORROSION AROUND CUT-OUT EXTENDING UNDER SKIN APROX 1" TO 1.5" REPAIRED UPPER WING SKIN AROUND LT UPPER FUEL PORT IAW EA NR 6-5730-135142 AND A/B DWG R57349265 AND RAS NR RAS/BAE/1011485/2009 ISSUE 'A DU - [SDR FDEA200812315322](https://openairdocs.org/sdr/FDEA200812315322.md): Sensor · malfunctioned · Dec 31, 2008 · N804FD · Airbus A310 · Landing Gear Retraction/Extension System > AFTER T/O LANDING GEAR FAILED TO RETRACT. ECAM DISPLAYED L/G RETRACTION INOP. ACFT LOST AUTO-THROTTLES. FOUND TARGET SENSORS 9GA AND 11GA LOS SE AND OUT OF "C" DIMENSIONS OUT OF LIMITS; REMOVED AND REPLACED SENSORS 9GA AND 11GA ON LT BOGIE REF. MM 32-00-00 - [SDR 08FDEA03529](https://openairdocs.org/sdr/08FDEA03529.md): Selector Valve · failed · Aug 21, 2008 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension System > LDG GEAR DID NOT EXTEND WITH GEAR HANDLE, GRAVITY EXTENSION OK PER CREW DEBRIEF, WHEN GEAR HANDLE CYCLED THERE WAS NO ASSOCIATED AUDIABLE SOUND NORMALLY HEARD DURING GEAR EXTENSION. CREW DID NOT TRY SELECTING LDG GEAR POSITON DET SYSTEM TO "2" DURING ATTEMPT - [SDR 07FDEA03926](https://openairdocs.org/sdr/07FDEA03926.md): Stringer · corroded · Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND PITTING CORROSION ON FOLLOWING MILLED STRINGER: 52, 53 AND 54 RT AND STRG 52, 53, 54 AND 56 LT, BETWEEN FRAME 54.1-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTIONS AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 - [SDR 07FDEA03924](https://openairdocs.org/sdr/07FDEA03924.md): Stringer · corroded · Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND PITTING CORROSION ON FOLLOWING STRINGER: 48 AND 50 RT AND STRG 46, 47, 48, 50 AND 51 LT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 AND IAW SR - [SDR 07FDEA03923](https://openairdocs.org/sdr/07FDEA03923.md): Stringer · corroded · Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND PITTING CORROSION ON STRINGER 44 RT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 AND IAW SRM 51-72-10. - [SDR 07FDEA03922](https://openairdocs.org/sdr/07FDEA03922.md): Stringer Splice · corroded · Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 50 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. - [SDR 07FDEA03921](https://openairdocs.org/sdr/07FDEA03921.md): Stringer Splice · corroded · Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND TWO CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 48 AND 49 RT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10. Next page: https://openairdocs.org/deregistered/N804FD-2024-03-02/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 = 'N804FD' AND deregistration_id = 'N804FD-2024-03-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N804FD-2024-03-02/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.