N742FD

Service difficulty reports · 203

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 = 'N742FD' AND registry_match = 'registration'
  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 FDEA201307241648Fitting · corrodedDURING FLUORESCENT PENETRANT INSPECTION ON RT WING RIB 5 RT MLG FITTING FWD LUG FOUND CORROSION ON BORE. FOUND WITHIN LIMITS DWG R57240425, SECTION B, REV B. REPAIRED IAW EA 6-5740-T0301511, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N742FD · Airbus A300B4622R · Wing, Landing Gear Attach FittingsSDR FDEA201307241647Fitting · corrodedDURING FLUORESCENT PENETRANT INSPECTION ON LT WING, RIB 5, LT MLG FITTING FORWARD LUG, FOUND CORROSION ON BORE. FOUND EXCEEDED LIMITS IAW DWG R57240425, SECTION B, REVISION B. REPAIRED IAW EA 6-5740-T0301510, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1Jul 24, 2013 · N742FD · Airbus A300B4622R · Wing, Landing Gear Attach FittingsSDR FDEA201305271091Arming Lever · obstructedL1 DOOR WOULD NOT DISARM ON RAMP. AFTER EXTENSIVE OPERATION OF SLIDE LOCK MECHANISM MAINT WAS ABLE TO DISARM SLIDE AND OPEN DOOR. EXTENSIVE DEBRIS HAD ACCUMULATED IN MECHANISM KEEPING IT FROM FULL TRAVEL. CLEANED AND LUBED MECHANISM. SLIDE ARMING/DISARMIMay 27, 2013 · N742FD · Airbus A300B4622R · Emergency EquipmentSDR FDEA201103252040Battery · failedDURING SERVICE CHECK, FOUND COURIER EMERGENCY LIGHTING SYS NOT TESTING CORRECTLY. COURIER AREA EMERGENCY POWER SUPPLY BATTERY REPLACED IAW AMM 33-51-14-04-0. OPS CHECK CARRIED OUT SATISFACTORY.Mar 25, 2011 · N742FD · Airbus A300F4605R · Emergency LightingSDR FDEA201103191083Structure · chafedRT WING KREUGER FLAP FOLDING NOSE OTBD EDGE, SURFACE HAS 1 IN CHAFED MARK. REPAIRED RT WING KREUGER FLAP IAW EA6-5750-145582 INSTRUCTIONS.Mar 19, 2011 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201002260541Uplock Hook · dirtyOPEN U NOSE GEAR AMBER LT REMAINED ON AFTER GEAR RETRACTION ON BOTH PANELS. NO VIBRATION & GEAR EXTENDED NORMALLY WITH DOOR LT INDICATIONS EXTINGUISHED. DUPLICATED NLG DOOR INDICATIONS ON GROUND, WITH BOTH NOSE GEAR DOORS FULLY CLOSED HAD DUAL NLG DOOR NOT CFeb 26, 2010 · N742FD · Airbus A300B4622R · Nose/Tail Landing GearSDR FDEA200902250723Control Unit · failedNR 7 SPOILERS ECAM CAME ON DURING CLIMB-OUT. COMPLIED W/ECAM QRH. COULD NOT CONFIRM SPOILERS RETRACTED. OPTED TO RETURN TO IND. T/S PER TSM, EFCU 1 FAULTED C1 2, EFCU 2 FAULTED M1 2, 4,7 . PER CREW DEBRIEF SPOILER 7 PUSH BUTTON WOULD NOT RESET OR LATCH IFeb 25, 2009 · N742FD · Airbus A300B4622R · Drag Control SystemSDR 08FDEA04823Dampener · lack of lubeGEAR WOULD NOT RETRACT AFTER TAKEOFF. PERFORMED ECAM AND QRH DIRECTIVES. CHECKED THE MEMORY DISPLAY OF THE PSEU AND IT SHOWS FAULT CODE "BR". REMOVED AND REPLACED RT PITCH DAMPER. ATTEMPTED TO LUBE BOTH BOGIE BEAMS, NEITHER WOULD TAKE GREASE. THE BOGIE WNov 8, 2008 · N742FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 08FDEA03024Skin Panel · corrodedCORROSION FOUND ON SKIN PANEL C 39/40, P 27-29 RT REPAIR PERFORMED BY REPLACEMENT OF PANEL AND FASTENER HL12-VF6 IAW RAS 70507112/019/2008 ISS A, APPROVED BY EA 6-5314-120049.Jul 23, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA03018Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 4 LT UPPER FLANGE OF FWD END OF HINGE ARM. REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY RAS/DABRE/7009949/2008 ISS A AND EA 6-5772-123051.Jul 22, 2008 · N742FD · Airbus A300B4622R · SpoilersSDR 08FDEA03017Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 3 LT UPPER FLANGE OF FWD END OF HINGE ARM. REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY RAS/DABRE/7008957/2008 ISS A AND EA 6-5772-123006 ISS A.Jul 22, 2008 · N742FD · Airbus A300B4622R · SpoilersSDR 08FDEA03016Panel · corrodedFOUND CORROSION AT TRANSITION OF SHROUD BOX AND TOP SKIN PANEL RT OUTER WING REPAIR PERFORMED BY CORROSION BLEND OUT, RIB CUT AND INSTALLING AN INFILL AND EXTERNAL PLATES IAW DRAWING R572-40274, APPROVED BY RAS /BAE/1007435/2008 ISS A AND EA 6-5720-123005.Jul 22, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02993Skin · damagedFOUND OLD PATCH REPAIR ON LT AILERON LOWER SKIN TRAILING EDGE AREA RIB 13- 17 WITH BAD OLD DOCUMENTATION. THE REPAIR RENEWED IAW RAS/FOK/139/2008 ISS A, APPROVED BY EA 6-5761-120107.Jul 21, 2008 · N742FD · Airbus A300B4622R · AileronsSDR 08FDEA02992Skin · damagedFOUND TWO OLD PATCH REPAIRS ON RT AILERON LOWER SKIN TRAILING EDGE AREA RIB 10-12 AND 4-10 WITHOUT OLD DOCUMENTATION. THE TWO REPAIRS RENEWED IAW RAS/FOK/138/2008 ISS A, APPROVED BY EA 6-5761-120106 .Jul 21, 2008 · N742FD · Airbus A300B4622R · AileronsSDR 08FDEA02991Skin · delaminatedFLUID INGRESS ON RUDDER RT SIDE PANEL NEAR LOWER RIB Z-PROFILE. REPAIR PERFORMED IAW SRM 51-77-10, TD/K4/S1/24567/2008 ISS B AND RAS/DAHAM/4024567/2008 ISS A, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA02990Skin · delaminatedFLUID INGRESS ON RUDDER RT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA02989Skin · delaminatedFLUID INGRESS ON RUDDER LT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA02987Structure · corrodedFOUND CORROSION UNDER STATIC DISCHARGER RT WING TIP. REPAIR PERFORMED BY BLEND OUT THE CORROSION, CUT THE AREA AND PERFORM A PATCH REPAIR IAW RAS/FOK/008/2008 ISS A, APPROVED BY EA 6-5730-120120.Jul 21, 2008 · N742FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA02986Structure · corrodedFOUND CORROSION AT CROSS STRUT C 84 LT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 21, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02920Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN UPPER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CORROSION FREE CONDITION INSTALLING STEEL PLATES IAW RAS/BAE/1007329/2008 ISS A, APPROVED BY EA 6-2910-120038.Jul 16, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02919Skin · wornFOUND ELONGATED HOLES ON LT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS. REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038.Jul 16, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02918Skin · wornFOUND ELONGATED HOLES ON RT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038.Jul 16, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02914Skin · misrepairedEDGE DISTANCE TO SMALL AT FOUR FASTENER LOCATION C 68, P 32-33 RT. EXTERNAL DOUBLER REPAIR PERFORMED IAW RAS/EFW/9000069/2008 ISS A, APPROVED BY EA 6-5317-123002.Jul 16, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02882Fitting · corrodedFOUND CORRODED CORNER FITTING C 58 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.Jul 15, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02881Skin · damagedFOUND TOOLMARK ON CENTER TANK TOP SKIN C 46, TRACK 1-2 LT REPAIR PERFROMED BY SMOOTH BLEND OUT AND NDT FOR CRACK FREE CONDITION IAW. RAS 70507169/2008 ISS.A , APPROVED BY EA 6-5710-120053Jul 15, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02880Fitting · corrodedFOUND CORROSION ON CORNER FITTING C58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.Jul 15, 2008 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02879Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 61 SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG.205Jul 15, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02878Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 56 AND C 58 SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG. 205.Jul 15, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02877Skin · corrodedFOUND CORROSION ON LT TOP SKIN AT FRONT SPAR AREA BETWEEN RIB 24-28 REPAIR PERFORMD BY CORROSION REWORK , NDT FOR CRACK FREE CONDITION AND INSTALLING FIRST OVERSIZED FASTENER IAW. RAS/BAE/1007273/2008 ISS.A, APPROVED BY EA 6-5720-120110.Jul 15, 2008 · N742FD · Airbus A300F4622R · Wing, Plate/SkinSDR 08FDEA02860Skin · delaminatedFOUND DELAMINATION ON RT SPOILER NR 5 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-61-53 PAGE 401.Jul 14, 2008 · N742FD · Airbus A300B4622R · SpoilersSDR 08FDEA02859Skin · delaminatedFOUND DELAMINATION ON LT SPOILER NR 5 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-61-53 PAGE 401.Jul 14, 2008 · N742FD · Airbus A300B4622R · SpoilersSDR 08FDEA02858Skin · delaminatedFOUND DELAMINATION ON RT SPOILER NR 3 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-61-51 PAGE 401.Jul 14, 2008 · N742FD · Airbus A300B4622R · SpoilersSDR 08FDEA02857None · noneFOUND OLD DOUBLER REPAIR ON LT KRUEGER FLAP INNER SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP IAW AMM 278711 PAGE 401.Jul 14, 2008 · N742FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02826Skin · chafedFOUND ON LT SLAT NR 2 TRAILING EDGE BOTTOM SKIN ATTACHMENT HOLES CHAFING MARKS AND UNDETERMINED HOLES. REPAIR PERFORMED BY REMOVING THE DAMAGED SKIN PANEL AND INSTALLING A REPLACEMENT SKIN PANEL IAW RAS/FOK/089/2008ISS A, APPROVED BY EA 6-5743-120041.Jul 11, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02825Skin · corrodedFOUND CHAFING MARKS ON LOWER SKIN AT RIB 21, LT SLAT NR 1 REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/FOK/098/2008 ISS A, APPROVED BY EA 6-5742-120040.Jul 11, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02824Skin · chafedFOUND ON RT SLAT NR 1 TRAILING EDGE LOWER SKIN WEAR DAMAGE AT FOLDING NOSE CUTOUT. REPAIR PERFORMED BY BLENDOUT THE DAMAGE TO SMOOTH CONTOUR IAW. RAS/FOK/097/2008 ISS A, APPROVED BY EA 6-5742-120057.Jul 11, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02823Pan · damagedFOUND OLD DOUBLER REPAIR ON RT SLATNR 1 FOLDING NOSE INNER PAN. REPAIR PERFORMED IAW SB A300-57-6067 (REPLACEMENT OF INNER PAN), APPROVED BY EA 6-5742-120037.Jul 11, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02822Pan · damagedFOUND OLD DOUBLER REPAIR ON LT SLAT NR 1 FOLDING NOSE INNER PAN REPAIR PERFORMED IAW SB A300-57-6067 (REPLACEMENT OF INNER PAN), APPROVED BY EA 6-5742-120037.Jul 11, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02783Support · corrodedFOUND CORRODED SUPPORT ON RT KRUEGER FLAP STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 9, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02782Fitting · corrodedFOUND CORRODED FITTING ON RT KRUEGER FLAP STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 9, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02781Fitting · corrodedFOUND CORRODED FITTING ON RT KRUEGER FLAP STRUCTURE REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 9, 2008 · N742FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02742Skin · damagedFOUND OLD DOUBLER REPAIR ON LT INNER FLAP UPPER SKIN NEAR RIB 27, STRG 2.1 AND 2.2 WITHOUT AI APPROVAL. DOUBLER REPAIR RENEWED IAW RAS/FOK/198/2008 ISS A, APPROVED EA 6-5752-123008.Jul 8, 2008 · N742FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02741Frame · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT, C 57.2, P14-15A, RT ON INNER FRAME FLANGE. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000054/2008 ISS A, APPROVED BY EA 6-5316-123024.Jul 8, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA02740Frame · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT, C 55, P14-15A, LT ON INNER FRAME FLANGE. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000052/2008 ISS A, APPROVED BY EA 6-5316-123023.Jul 8, 2008 · N742FD · Airbus A300B4622R · Emergency ExitsSDR 08FDEA02738Cover · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT, C 56-57.1, P14-15A, LT ON COVER SHEET. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000052/2008 ISS A, APPROVED BY EA 6-5316-123022.Jul 8, 2008 · N742FD · Airbus A300B4622R · Emergency ExitsSDR 08FDEA02737Stringer · corrodedFOUND CORROSION ON STRINGER P 51 LT, C 54.2-57.1 REPAIR PERFORMED BY CUT THE FRAME 54.3 TO INSTALL NEW STRINGER PROFILE, PERFORM SPLICE REPAIR AT STRINGER AND FRAME IAW RAS/EFW/9000058/2008 ISS C, APPROVED BY EA 6-5316-123001.Jul 8, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02736Skin · corrodedFOUND CORROSION ON UPPER SURFACE OF BOTTOM SKIN RIB 6A-7A, AFT OF REAR SPAR, LT WING. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECT THE AREA IAW RAS/BAE/1007293/2008 ISS A, APPROVED BY EA 6-5751-120113.Jul 8, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02733Window Frame · corrodedFOUND CORROSION IN 7 FASTENER HOLES OF WINDSHIELD FRAME LT/RT. REPAIR PERFORMED BY OVERSIZING OF HOLES, NDT FOR CRACK FREE CONDITION AND INSTALLING NEW FASTENER IAW RAS 70507106/2008 ISS A, APPROVED BY EA 6-5311-120048.Jul 8, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02732Skin · damagedFOUND OLD DOUBLER REPAIR ON LT WING TOP SKIN, TRAILING EDGE, RIB 18-19 WITHOUT ANY OLD DOCUMENTATION. DOUBLER REPAIR RENEWED IAW RAS/BAE/1007270/2008 ISS A, APPROVED BY EA 6-5751-120109 .Jul 8, 2008 · N742FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02731Crossbeam · corrodedFOUND CORROSION ON AFT FACE OF CROSS STRUT C87 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2008 · N742FD · Airbus A300B4622R · Fuselage Main, Structure
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