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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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 NOSDR 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"SDR QR9R20210617001Screw · mismanufacturedTHE ACTUATOR SCREWS (PN: NAS6204-9D) ARE MANUFACTURED OUT OF LIMITS (OVERSIZED). THIS PREVENTS SCREWS FROM PROPERLY FITTING THROUGH BUSHING OF ACTUATOR ARM.SDR 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 SIXTSDR 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 ACTSDR 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. PSDR CA160203025Nut · mismanufactured(CAN) NEW SELF LOCKING NUTS WHICH THE FIBER IS COMING OUT OF THE NUT. LOCKING NUTS ARE BATCH NR 47333.SDR 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 SDR 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 RSDR 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 FRSDR 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 ASDR 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 ASDR 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 ACSDR 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 CARRISDR 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 CARRISDR 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 FSDR 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.SDR 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 SUBSTANDARDSDR 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 QUARANTSDR 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).SDR 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 SDR 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 12/2/2SDR 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)SDR 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 GRESDR 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 GRSDR 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 CONNECSDR 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.SDR 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.SDR 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 STRIPPEDSDR AUS20020205Static Wick · faulty(AUS) ALL STATIC WICKS (10OFF) UNSERVICEABLE.SDR 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 BASESDR 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 DOWNSDR AUS20011461Nut · corroded(AUS) VERTICAL STIFFENER ANCHOR NUT ATTACHMENT POINT CORRODED BEYOND LIMITS.SDR AC2A076112Strap · crackedCRACKED IN BENT RADIUS. REMOVED AND REPLACEDSDR AC2A076111Receptacle · wornPREMATURE WEAR R&R RECEPTICLESDR 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, SDR 2002FA0000237Fastener · looseRIGHT WING: 16 LOOSE NAILS, 3 VERY LOOSE, 1 MISSING LEFT WING: 9 LOOSE NAILS, 0 VERY LOOSE, 0 MISSING.SDR 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.SDR 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.SDR 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
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