JASC 1400

Service difficulty reports · 42

Reports filed under 1400 · Miscellaneous Hardware, 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 jasc_code = '1400'
  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 SCNA20250508171Cotter Pin · missingMISSING COTTER PIN ON ANCHOR FITTING OF BOTH EMERGENCY ESCAPE ROPE AT COCKPIT. COTTER PIN WAS INSTALLED ON BOTH EMERGENCY ESCAPE ROPE AT COCKPIT PER B737-800 AMM 25-61-10.May 5, 2025 · N804SY · Boeing 7378Q8SDR 2023FA0000343Bearing · crackedRBC BEARING IDENTIFIED BELOW IS CRACKING AND BREAKING AT INSTALLATION ON AILERON SECTOR AND AILERON HINGE. STOP USE OF BEARING IMMEDIATELY NONE MADE IT TO PRODUCTION AIRCRAFT.Jun 27, 2023SDR 2022FA0000326None · noneAIRCRAFT REGISTRATION N28ZD SN 9191 WAS IN MAINTENANCE AND A JACKING PAD WAS FITTED TO LH WING IN ORDER TO DEFUEL THE RH WING. THE JACKING PAD WAS NOT REMOVED BEFORE THE AIRCRAFT WAS RELEASED TO SERVICE. WHEN ENGINEER FITTED THE JACKING PAD THE ENGINEER HAD NOJul 1, 2022 · N28ZD · Bombdr BD7001A10SDR GTIA2021110836106None · none"IN FLIGHT ECAM MESSAGE HYD Y RSVR LO LVL-SERVICED Y HYD SYS PER AMM 12-12-29. NO FAULTS AT THIS TIME. PERFORMED FUCTIONAL CHECK OF RESEVOIR LOW LEVEL WARNNG PER AMM 29-31-00-710-001. OPS CK. NO FAULT NOTED"Nov 8, 2021 · N533NK · Airbus A319132SDR QR9R20210617001Screw · mismanufacturedTHE ACTUATOR SCREWS (PN: NAS6204-9D) ARE MANUFACTURED OUT OF LIMITS (OVERSIZED). THIS PREVENTS SCREWS FROM PROPERLY FITTING THROUGH BUSHING OF ACTUATOR ARM.Jun 17, 2021 · Bolkms BK117C2SDR 2020FA0000145Turnbuckle · damagedTHE TURNBUCKLE IS LOCATED UNDER THE FLOORBOARD JUST IN FRONT OF THE REAR SPAR CARRY THROUGH ON THE RIGHT SIDE UNDER A HEAT DUCT THAT GOES THROUGH THE REAR SPAR AND SERVICES THE AREA BEHIND THE SECOND TWO SEATS IN THE ACFT. THIS AREA MAY HAVE A FIFTH AND SIXTFeb 12, 2020 · Beech S35SDR SWIA2020021848744Bolt · misinstalled* R/H ENGINE "SLAVE" V.G. ACTUATOR, UPPER ATTACHING HARDWARE, AT COMPRESSOR ACTUATOR BELLCRANK, IS INSTALLED INCORRECTLY PER AMM, (FLAGGED). (C-CHECK) RO:2/14/2020INSTALLED HARDWARE CORRECTLY ON R/H ENGINE SLAVE V.G ACTUATOR ( ROD END TO COMPRESSOR ACTJan 2, 2020 · N782SK · Cndair CL6002C10SDR 2016FA0000160Screw · wrong partFOUND LT MAIN WHEEL WELL SATURATED WITH JET FUEL AND FUEL STREAKING DOWN LT SIDE OF FUSELAGE AND UP THE TAIL. NO ACTIVE LEAK NOTED. UPON INVESTIGATION, FOUND PANEL 512AB LOOSE/HANGING DOWN, ALTHOUGH NOT LEAKING STATICALLY AND INCORRECT HARDWARE INSTALLED. PApr 4, 2016 · N823PM · Cessna 550SDR CA160203025Nut · mismanufactured(CAN) NEW SELF LOCKING NUTS WHICH THE FIBER IS COMING OUT OF THE NUT. LOCKING NUTS ARE BATCH NR 47333.Feb 2, 2016SDR CA150112012Bolt · broken(CAN) PILOTS HAD BURNING ODOR IN AIRCRAFT AND LOSS OF SEVERAL INSTRUMENTS AND RADIO COMMUNICATIONS. MAINTENANCE FOUND THAT THE LOWER PIVOT BOLT THAT WAS HOLDING THE ALTERNATOR HAD BROKEN OFF. THE BOLT HAD BACKED OUT AND WAS RUBBING ON THE ALTERNATOR BELT. THE Jan 11, 2015 · Diamon DA20C1SDR CA130607005Cap · missing(CAN) DURING A 300 HR INSPECTION THE MECHANIC FOUND A PLASTIC TYPE PLUG LAYING UNDER THE ELEVATOR BELLCRANK IN THE TAIL SECTION. AFTER RESEARCH AND SPEAKING WITH THE MFG IT WAS DETERMINED THAT THE PLUG/CAP CAME FROM THE TOP OF THE ANTENNA TUBE. THE CAP WAS RJun 4, 2013 · Diamon DA20C1SDR CA130607012Cap · missing(CAN) 1 ACFT IN THE FLEET CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. THE CAP WAS FOUND MISSING FRJun 3, 2013 · Diamon DA20C1SDR CA130607011Cap · missing(CAN) 1 ACFT IN THE FLEET CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FLEET AJun 3, 2013 · Diamon DA20C1SDR CA130607010Cap · missing(CAN) 1 ACFT IN THE FLEET CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FLEET AJun 3, 2013 · Diamon DA20C1SDR CA130607009Cap · missing(CAN) 1 ACFT IN THE FLEET CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FLEET ACJun 3, 2013 · Diamon DA20C1SDR CA130607008Cap · missing(CAN) 1 ACFT CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FLEET ACFT WAS CARRIJun 3, 2013 · Diamon DA20C1SDR CA130607007Cap · missing(CAN) 1 ACFT CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FLEET ACFT WAS CARRIJun 3, 2013 · Diamon DA20C1SDR CA130607006Cap · missing(CAN) ONE AIRCRAFT IN THE FLIEET CURRENTLY UNDEROING A 300 HR INSPECTION WAS FOUND TO HAVE A PLASTIC CAP FROM AN UNKNOWN SOURCE RESTING IN THE TAIL BELOW THE ELEVATOR BELLCRANK. THE CAP WAS FOUND TO BE FROM THE ANTENNA TUBE IN THE TAIL. AN INSPECTION OF THE FJun 3, 2013 · Diamon DA20C1SDR CA101221005Rivet · mismarked(CAN) NEW RIVITS ORDERED FROM BELL WERE INCORRECTLY PART NUMBERED. RIVITS WERE IDENTIFIED AS CR7771, BUT CR7773 RIVITS WERE IN THE BAG. THIS IS THE SECOND OCCURANCE OF THIS HAPPENING. BELL NOTIFIED AND THE STOCK WAS PURGED.Dec 20, 2010SDR CA110127002Nut · deformed(CAN) THESE STRUCTURAL SPACE-SAVER NUTS SEEM VERY DEFORMED BEYOND WHAT IS NORMAL FOR THIS TYPE OF FRICTION NUT. AME WAS UNABLE TO FIT A NORMAL BOX END WRENCH ON THE NUTS FOR TIGHTENING DUE TO DEFORMITY. WE CONSIDER THE MANUFACTURE OF THE NUTS TO BE SUBSTANDARDDec 15, 2010SDR CA101124003Bolt · mismanufactured(CAN) PMA SHOULDER BOLT WOULD NOT PHYSICALLY FIT THROUGH OEM BRACKET. MANUFACTURER CONTACTED AND DRAWINGS/SPECS OBTAINED AND ALL BOLTS PULLED FROM INVENTORY - LARGE PERCENTAGE OF BOLTS FOUND TO BE OUTSIDE OF MANUFACTURERS SPECS, ALL BOLTS FROM VENDOR QUARANTNov 24, 2010SDR CA090826004Nut · missingCLEVIS BOLT NOT SECURED. RETAINING NUT IS MISSING (AND COULD NOT BE LOCATED IN ACFT) CLEVIS BOLT DID NOT COMPLETLEY SEPARATE FROM THE CLEVIS HSG (ITEM NR 32).Jul 16, 2009 · Cessna 425SDR CA080714005Bolt · mismanufactured(CAN) TBAL HAD A CUSTOMER REPORT OF THE LOCK WIRE TEARING THROUGH THE LOCK WIRE HOLE DURING INSTALLATION ON 2 OF THE 4 PURCHASED DRAIN VALVE BOLTS. ALL BOLTS IN STOCK WERE PULLED FROM THE SHELF AND EXAMINED. THE BOLTS CONFORMED TO THE TBAL DRAWING. THE BOLTS Jul 8, 2008 · Dhav DHC6SDR WSA12262007Bolt · mismanufacturedHAVE ORDERED FROM MFG THE LANDING GEAR DRAG LEG BOLTS TWICE AND HAVE RECEIVED (2) DEFECTIVE BOLTS EACH TIME. THE COTTER PIN HOLE WAS MISDRILLED AND WOULD COULD NOT GET THE HOLES TO LINE UP WITH THE NUT CASTELLATION. (2) OF THE BAD BOLTS WERE DATE TAGGED 12/2/2Dec 26, 2007 · N1558 · Beech 200BEECHSDR 2007FA0001113Bolt · brokenNEW BOLT BROKEN DURING TORQUE. TORQUE VALUE NEVER OBTAINED BEFORE THE BOLT BROKE. THIS BOLT HOLDS THE BEARING CAP IN PLACE THAT HOLDS THE MAIN LANDING GEAR ON THE AIRCRAFT. (K)Dec 14, 2007 · N673AE · Emb EMB145LRSDR 2007FA0000310Nut · mismanufacturedWHILE INSTALLING KIT MK172-25-10C TO COMPLY WITH SB 04-25-01 R4 AND AD 2007-05-10, ONE OF THE PARTS IN THE KIT WAS MACHINED IMPROPERLY. THE HEIGHT ADJUSTING NUT HAD THE THRU HOLE FOR THE ULTRALOC WITH MALFORMED THREADS. THE MINOR DIAMETER OF THE THREAD WAS GREApr 6, 2007 · N949SP · Cessna 172SSDR 2007FA0000301Nut · mismanufacturedWHILE INSTALLING KIT MK172-25-10C TO COMPLY WITH SB 04-25-01 R4 AND AD 2007-05-10, ONE OF THE PARTS IN THE KIT WAS MACHINED IMPROPERLY. THE HEIGHT ADJUSTING NUT HAD THE THRU HOLE FOR THE ULTRALOC WITH MIS FORMED THREADS. THE MINOR DIAMETER OF THE THREAD WAS GRApr 6, 2007 · N949SP · Cessna 172SSDR CA041213003Tube · wrong part(CAN) DURING ENGINE VISUAL INSPECTION AT MFG, HAVE IDENTIFIED THAT 2 ITEMS FROM THE FUEL PRESSURE TUBING WERE NOT GENUINE AND WERE MANUFACTURED BY AN UNKNOWN SOURCE. THOSE 2 ITEMS HAVE NO IDENTIFICATION NUMBERS BUT WERE INSTALLED IN REPLACEMENT OF: FUEL CONNECDec 13, 2004SDR HNAA0400056Pin · looseNOISE NOTED AT AIRSTAIR DOOR EXTERIOR AFTER T/O AIR TURNBACK, FOUND PROP TIE STREAMER HANGING FROM AIRSTAIR DOOR PROP TIE STORAGE AREA. INSPECTION OF ACFT FOUND NO DAMAGE.May 19, 2004 · N942HA · Dhav DHC8102SDR CA020913005Washer · mismanufactured(CAN) SPECIAL 7/8 INCH DIAMETER PRELOAD INDICATING WASHER ASSY USED ON LOWER FORWARD WING ATTACH BOLTS INDICATED PROPER TORQUE PREMATURELY. ESTIMATE NORMAL TORQUE TO BE AT LEAST 300 FT LBS AND SUSPECT WASHER ASSEMBLY INIDCATED TORQUE AT APPROX 100 FT LBS.Sep 6, 2002 · Beech E90SDR CA020426002Pin · cut(CAN) WHILE TRYING TO ADJUST THE CABLE TENSION DURING AN OPS IT WAS NOTED THAT THE TURN BARREL WAS VERY STIFF TO TURN AND THE LOCK PIN SLOT WAS FULL OF CUTTINGS. AT DISASSEMBLY TO INVESTIGATE THE TURN BARREL IT WAS FOUND THAT THE TURN BARREL HAD BEEN STRIPPEDApr 25, 2002 · Beech A100SDR AUS20020205Static Wick · faulty(AUS) ALL STATIC WICKS (10OFF) UNSERVICEABLE.Feb 23, 2002 · Cessna TR182SDR 2002FA0000331Nut · looseTHE ELT ANTENNA WAS FOUND TO BE LOOSE ON VISUAL INSPECTION. REMOVED ELT ANTENNA ASSEMBLY, FOR PROGRESSIVE INSPECTION. FOUND SHIELD LOCKING NUT SECURING METAL RADIATING ROD TO ANTENNA BASE ASSEMBLY WAS LOOSE. WHEN RADIATING ROD WAS REMOVED FROM ANTENNA BASEFeb 7, 2002 · N375HW · Cessna 210DSDR CA020124009Bolt · worn(CAN) DURING APPROACH FOR LDG, CREW SELECTED GEAR DOWN&GOT 2 MAIN GEAR RED IND.S, THEN 2 MAIN GEAR GREEN IND.S WITH NO NOSEGEAR IND.. CREW BROKE OFF APPROACH & CYCLED GEAR COUPLE OF TIMES WITH NO IMPROVEMENT.AS SOON AS EMERG EXTENSION PERFORMED, GEAR CAME DOWNJan 23, 2002 · Swrngn SA226TCSDR AUS20011461Nut · corroded(AUS) VERTICAL STIFFENER ANCHOR NUT ATTACHMENT POINT CORRODED BEYOND LIMITS.Dec 23, 2001 · Boeing 727277SDR AC2A076112Strap · crackedCRACKED IN BENT RADIUS. REMOVED AND REPLACEDSep 18, 2001 · N430CV · Bell 430SDR AC2A076111Receptacle · wornPREMATURE WEAR R&R RECEPTICLESep 17, 2001 · N430CV · Bell 430SDR 2001FA0000366Tape · loosePILOT COMPLAINED OF ROUGH RUNNING ENGINE LOW STATIC RPM ONLY OBTAINABLE BY LEANING MIXTURE, FOUND APPROX 1 SQUARE INCH OF TIN FOIL LODGED IN CARB VENTURI, EXAMINATION OF HEAT SHROUD ON EXHAUST PIPE RUB AREA WAS WRAPPED WITH ALUMINUM FOIL TAPE TO TAKE UP PLAY, Aug 20, 2001 · N9831W · Piper PA28140SDR 2002FA0000237Fastener · looseRIGHT WING: 16 LOOSE NAILS, 3 VERY LOOSE, 1 MISSING LEFT WING: 9 LOOSE NAILS, 0 VERY LOOSE, 0 MISSING.Aug 13, 2001 · N38WK · Bbavia 7GCBCSDR 2002FA0000255Fastener · missingNUMEROUS RIB NAILS MISSING OR BACKED OUT FARTHER THAN .1250 ON FORWARD AND AFT WING SPARS, LEFT AND RIGHT WINGS. INSPECTED SPARS AND REPLACED SUCH NAILS.Aug 1, 2001 · N86983 · Bbavia 7ECASDR 2002FA0000244Fastener · missingAPPROXIMATELY 10 RIB NAILS WERE MISSING ON EACH WING. NAIL HOLES WERE NOT ELONGATED. NO OTHER DAMAGE WAS FOUND. THE GENERAL LOCATION OF MISSING NAILS WERE AT STRUT ATTACH AREAS.May 17, 2001 · N2561Z · Bbavia 8KCABSDR 2002FA0000243Fastener · missingAPPROXIMATELY 8 RIB ATTACH NAILS WERE FOUND MISSING ON EACH WING. (BOTH SPARS) SCRATCHES AND GOUGES WERE FOUND ON LEFT REAR SPAR MID AREA. THESE WERE APPARENTLY MADE BY REPAIRMAN SLIDING RIBS DOWN SPAR, DURING THE LAST REPAIR OF WING. BOTH WINGS WILL HAVE May 17, 2001 · N9510S · Bbavia 7ECA
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