N804FD, cancelled Mar 2, 2024

Service difficulty reports · 119

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 = 'N804FD' AND deregistration_id = 'N804FD-2024-03-02'
  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 FDEA201609153243Coalescer Bag · odorAFTER 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 ENGINESep 15, 2016 · N804FD · Airbus A310324 · Humidity Control SystemSDR FDEA201607192536Smoke Detector · faulty"AVIONICS SMOKE" DISPLAYED ON ELECTRICAL PANEL AFTER ENGINE SHUTDOWN AT GATE. NO SMOKE WAS EMITTED ON THE SNIFFER FAN. R & R SMOKE DETECTOR.Jul 19, 2016 · N804FD · Airbus A310324 · Smoke DetectionSDR FDEA201511193714Bracket · damagedON 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-Nov 19, 2015 · N804FD · Airbus A310324 · Fluid Service DoorsSDR FDEA201510313432Actuator · leakingBLUE 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 Oct 31, 2015 · N804FD · Airbus A310324 · Drag Control ActuatorSDR FDEA201510303445Computer · failedDURING 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 WARNINGOct 30, 2015 · N804FD · Airbus A310324 · Central WarningSDR FDEA201503060700Slide · unwanted deployDOOR 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 52-1Mar 6, 2015 · N804FD · Airbus A310324 · Escape SlideSDR FDEA201409112578Skin · corrodedAV 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.Sep 11, 2014 · N804FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201409012391Repair · debondedAGING 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 COMPLESep 1, 2014 · N804FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201408222288Fastener · missingAGING 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 FRAug 22, 2014 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201408202239Repair · debondedAGING 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 ENAug 20, 2014 · N804FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201408202238Repair · debondedAGING 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 TAug 20, 2014 · N804FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201408202242Repair · corrodedAGING 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 4Aug 20, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201408202241Stringer · corrodedAGING 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 Aug 20, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201408072106Stringer · corrodedAV 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 6Aug 7, 2014 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201407281996Computer · failedPASSING 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 Jul 28, 2014 · N804FD · Airbus A310324 · Fuel Quantity IndicatorSDR FDEA201406281576Pulley · defectiveON 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. AFTERJun 28, 2014 · N804FD · Airbus A310324 · Aileron Control SystemSDR FDEA201405110982Rib · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-1. MAJOR REPAIR.May 11, 2014 · N804FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201405110981Rib · corrodedRIGHT 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.May 11, 2014 · N804FD · Airbus A310324 · Wing SparSDR FDEA201402140320Tru · faultedESS 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.Feb 14, 2014 · N804FD · Airbus A310324 · DC Rectifier/ConverterSDR FDEA201202160589Spar · damagedRT PYLON SPIGOT RECEPTACLE FITTING FOUND A MISDRILLED BOLT HOLE. REPAIRED IAW AMM 54-50-00 AND AMM 20-21-12Feb 16, 2012 · N804FD · Airbus A310324 · Nacelle/Pylon, Main FrameSDR FDEA201202100542Skin · contaminatedTWO 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" (NFeb 10, 2012 · N804FD · Airbus A310324 · Rudder, Plate/SkinSDR FDEA201202100543Skin · corrodedRIGHT 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.Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201202100541Skin · corrodedLEFT 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.Feb 10, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201202040470Skin · dentedNOSE 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-Feb 4, 2012 · N804FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201201110095Skin · corrodedRIGHT 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 Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110094Skin · corrodedRIGHT 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 ANDJan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110096Floor Support · corrodedFWD 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.Jan 11, 2012 · N804FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201201110093Skin · corrodedRIGHT 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. REPAIRJan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110091Skin · corrodedRIGHT 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-Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110090Skin · corrodedRIGHT 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 5Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110089Skin · corrodedRIGHT 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 51-2Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110088Skin · corrodedRT 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 Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201110086Skin · corrodedRT 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 51-49Jan 11, 2012 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201201080046Seat Track · chafedMAIN 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.Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201080045Seat Track · chafedMAIN 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.Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110174555Engine · failedCLIMBING 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 WASOct 17, 2011 · N804FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR FDEA201010093981Damper · leakingLANDING 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. COct 9, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201010073974Selector Valve · failedLOWERED 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 TSOct 7, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201009263715Connector · dirtyCLIMBING 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 CONSep 26, 2010 · N804FD · Airbus A310324 · Electrical Power System WiringSDR FDEA201008263146Pitot Head · contaminatedF/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 OKAug 26, 2010 · N804FD · Airbus A310324 · Pitot/Static SystemSDR FDEA200912104401Skin · misrepairedPREVIOUS 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 EA6-5710-8101Dec 10, 2009 · N804FD · Airbus A310324 · Leading Edge DevicesSDR FDEA200912104400Skin · misrepairedPREVIOUS 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 LOCADec 10, 2009 · N804FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA200912074364Skin · corrodedLT 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 DUDec 7, 2009 · N804FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA200812315322Sensor · malfunctionedAFTER 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 32-00-00Dec 31, 2008 · N804FD · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 08FDEA03529Selector Valve · failedLDG 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 ATTEMPTAug 21, 2008 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR 07FDEA03926Stringer · corrodedFOUND 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 201Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03924Stringer · corrodedFOUND 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 SRSep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03923Stringer · corrodedFOUND 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.Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03922Stringer Splice · corrodedFOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 50 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10.Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03921Stringer Splice · corrodedFOUND TWO CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 48 AND 49 RT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10.Sep 18, 2007 · N804FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
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