Airbus A310-324

Service difficulty reports · 1,439

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'A310324'
  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 07FDEA04485Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 65, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04483Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P48, C 68-69 AND C 70-71. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04451Skin · dentedFOUND DENT AT SLAT NR 2 LT OUT OF LIMIT. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11 FIG 202.Oct 2, 2007 · N805FD · Airbus A310324 · Leading Edge DevicesSDR 07FDEA04446Lug · corrodedFOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RAS/BAE/1000347/2005 ISS A.Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Attach FittingsSDR 07FDEA04467Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 56, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04466Stringer · corrodedFOUND CORROSION AT STRINGER P 48 LT, C 69-70 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04465Fitting · corrodedFOUND CORROSION AT CORNER FITTING P 44 LT, C64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04464Frame · damagedFOUND ENLARGED HOLES AT C 26/32 BETWEEN P 13-22 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, FrameSDR 07FDEA04463Fitting · corrodedFOUND CORROSION AT CORNER FITTING C 33 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04462Channel · dentedLT AFT CREW DOOR LOWER CHANNEL HAS A NOTCH OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Passenger/Crew DoorsSDR 07FDEA04461Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 56 LT, C 80 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04460Skin · misrepairedFOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 57-2055.Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04459Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 72, P 48 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04458Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C 72, 45 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04457Flange · corrodedFOUND FLANGE C61-62, AD CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR 07FDEA04456Fitting · corrodedFOUND CORROSION AT RUN OUT FITTING P44 LT/RT, C17 REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04455Fitting · corrodedFOUND FITTING AT C13-13A, P26 LT CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04454Seat Track · corrodedFOUND SEAT TRACK C 15A-19, Y-953 CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04453Skin Panel · corrodedFOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING OF TWO DOUBLERS IAW DRAWING R573-10011 AT BEAM 4 AND 6, C 44-2 AND C 44 LT/RT IAW EA 6-5710-81129 AND RAS/AS/0036/2005 ISS A.Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04452Rib · damagedFOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055.Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04450Skin · wornFOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04449Skin · wornFOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA04448Skin · damagedRT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND RELEASED IAW FAA FORM 8130-3 NR 05/1145.Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04447Skin · delaminatedDELAMINATION FOUND AT RUDDER SIDE PANEL IN THE AREA OF ATTACH FITTINGS REPAIR PERFORMED IAW SRM 55-41-12 FIG 216.Oct 2, 2007 · N805FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04445Skin Panel · dentedFOUND OLD FLUSH REPAIR AT C20-21, P 35-37 LT NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR RENEWED IAW RAS/DABRE/7004645/2004 ISS A.Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04432Skin Panel · dentedFOUND DENT DAMAGE AT SERVICE BOX PANEL C10-13 BUSH REPAIR PERFORMED IAW SRM 53-10-12 FIG 221.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04431Skin Panel · dentedFOUND DENT AT C77-78, P 27-28 LT FLUSH DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 227 AND STRINGER REPAIR PERFORMED IAW SRM 53-10-14.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04428Stringer · corrodedFOUND CORROSION AT STRINGER P 56LH, BETWEEN C 76-77. REPAIR PERFORMED BY BLEND OUT CORROSION AND FLAP PEENING IAW EA 6-5318-81118 AND RAS/DATLS/0002357/2005 ISS A.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04427Stringer · corrodedFOUND CORROSION AT STRINGER P 54 AND P56, LT, BETWEEN C 70-72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04426Floorbeam · corrodedFOUND CORROSION AT UPPER FLANGE OF TOP CAP BEAM C33 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 07FDEA04424Stringer · corrodedFOUND CORROSION AT STRINGER P47LT, C72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04422Stringer · corrodedFOUND CORROSION AT STRINGER P56LH BETWEEN C55/58-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04421Stringer · corrodedFOUND CORROSION AT STRINGER P54LH BETWEEN C55/58-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04418Stringer · corrodedFOUND CORROSION AT STRINGER P55LH BETWEEN C 55/58-61 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04416Stringer · corrodedFOUND CORROSION AT STRINGER P56 RT BETWEEN C 55/58-59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04414Stringer · corrodedFOUND CORROSION AT STRINGER P57 C 66. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04412Stringer · corrodedFOUND CORROSION AT STRINGER P56 C 68-70 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04411Panel · dentedFOUND OLD DENT AT C 8 IN 9 O'CLOCK POSITION. DOUBLER REPAIR PERFORMED IAW SRM 53-11-12 FIG 201.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04410Skin Panel · dentedFOUND DENT AT SKIN C63-65, P41-42 LT (AREA 1) AND P45-46 LT (AREA 2) DOUBLER REPAIR PERFORMED IN AREA 1 IAW SRM 53-10-12 FIG 228 AND LET THE DENT IN AREA 2 AS IT IS IAW EA 6-5317-81131 AND RAS/DATLS/0002418/2005 ISS A.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04409Bulkhead · damagedFOUND OLD REPAIR (MISDRILLED HOLE) AT FRAME 54 BULKHEAD LT WEB, WAS ACCEPTED FOR ONLY ONE FERRY FLIGHT. REPAIR RENEWED BY REMOVING THE EXISTING DOUBLER, CUT OUT ON WEB FOOT AND INSTALLING DOUBLER AND REPAIR ANGLE IAW EA 6-5315-81126 AND RAS/AS/0248/2004 ISS BOct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, BulkheadSDR 07FDEA04408Skin Panel · dentedFOUND SKIN DENT AT C72, P26-27 RT ON SKIN PANEL NR 1 REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A EXTERNAL DOUBLER AND FILLER IAW DRAWING R539-70630, APPROVED BY EA 6-5318-81127 AND RAS/DAHAM/4019001/2005 ISS A.Oct 1, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04407Skin Panel · damagedFOUND DURING P TO F CONVERSION A CUT (10MM) AT SKIN PANEL C 35, P 35 LT REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A FLUSH REPAIR WITH NEW STRAP AND COUPLING IAW EA 6-5314-82877 AND RAS/DABRE/7005190/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04406Fitting · chafedFOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Attach FittingsSDR 07FDEA04405Skin Panel · dentedFOUND NICK ON SKIN PANEL NR 3 C 18-19, P 33 RT REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5313-82859 AND RAS/DABRE/7005143/2005 ISS A.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04404Skin · delaminatedFOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A.Oct 1, 2007 · N806FD · Airbus A310324 · Rudder, Plate/SkinSDR 07FDEA04403Fitting · damagedFOUND MISDRILLED HOLES IN CORNER FITTING C59, P 44 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04402Doubler · corrodedFOUND CORROSION AT DOUBLER C71-72, P 47-48 LT REPAIR PERFORMED BYREWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-82856 AND RAS/DATLS/0002522/2005 ISS B.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA04401Stringer · corrodedFOUND CORROSION AT STRINGER P52 LT, C70-71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA04400Fitting · crackedFITTING AT P 48, C78 LT CRACKED (ABOUT 8MM). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR 07FDEA04399Fitting · corrodedFOUND CORROSION AT FITTING C 63, P44-46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach Fittings
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