Quest KODIAK 100
Service difficulty reports · 30
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 = 'KODIAK100' 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 aircraft_model_key = 'KODIAK100' 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 2026FA0000786Control Cable · failedDURING PREFLIGHT, ONE OF OUR PILOTS FOUND A BROKEN ELEVATOR TRIM CABLE. IT BROKE UP FRONT NEAR THE FIREWALL RIGHT AROUND WHERE THE CABLE GOES THROUGH THE PULLEYS AND THEN ENTERS / EXITS THE CABLE SHEATHING. IT APPEARS THE SHEATHING WAS PULLED DUE TO AN ADEL CLSDR EVGR20260325001Actuator · jammedPITCH TRIM WHEEL COULD ONLY BE MOVED WITHIN A VERY SMALL RANGE. MAINTENANCE INVESTIGATED AND FOUND THAT THE LH PITCH TRIM ACTUATOR WAS BOUND UP AND WOULD NOT ROTATE. THE ACTUATOR WAS REMOVED AND DISASSEMBLED IAW THE KODIAK 100 AMM CH. 2731.5.10 AND DAHER FIELSDR 2025FA0000768Torque Tube · debondedTHE ELEVATOR TORQUE TUBES HAD UNBONDED CREATING MOVEMENT BETWEEN ELEVATOR TORQUE TUBE & COLLAR. WE HAVE NOTED THIS CONDITION ON AT LEAST 10 DIFFERENT SERIAL NUMBERS OF ACFT. NOTE, THE RUDDER HAS SAME METHOD OF ATTACHMENT & FAILURES HAVE BEEN NOTED AT THAT LOSDR 2025FA0000747Crosstube · brokenDURING A ROUTINE ANNUAL INSPECTION, IT WAS DISCOVERED THAT THE FORWARD MAIN LANDING GEAR CROSS TUBE HAD BROKEN IN HALF AND HAD PUNCTURED THE FUSELAGE SKIN.SDR 2025F00092Rivet · looseTHERE ARE FOUR RIVETS AROUND THE MLG FRAMES (INSIDE THE FUSELAGE, ALONG THE SEAT TRACKS) THAT ARE SMOKING (TWO ON THE RIGHT SIDE OF THE FUSELAGE, TWO ON THE LEFT SIDE). ON ANOTHER KODIAK 100 OUR ORGANIZATION OPERATES IN KALIMANTAN, INDONESIA, ONE OF THESE RIVSDR 2020FA0000309Hydraulic Line · failed6650 FLOATS HYDRAULIC LINES PART NUMBER 66-47014 AND 66-47017 FAILED. THESE ARE ALUMINUM LINE USED ON 6650 AMPHIBIOUS FLOAT. LOSS OF HYDRAULIC FLUID CAUSED MAIN LANDING GEAR TO EXTEND WITH NOSE GEAR LEFT IN THE UP POSITION. BECAUSE OF THE FLUID LOOSE THERE WASSDR CA190730026Control Cable · corroded(CAN) DURING A SCHEDULED INSPECTION, THE LH FWD RUDDER CABLE P/N 100-617-4413-D01, AND RH FWD RUDDER CABLE P/N 100-4415-D01 WERE REPLACED DUE TO EXCESSIVE CORROSION. BOTH CABLES REPLACED WITH NEW TO RECTIFY. ALL WORK PERFORMED IAW THE APPLICABLE MAINTENANCE PUSDR CA180822003Line · leaking(CAN) THE PILOT REPORTED WHILE RETRACTING THE LANDING GEAR AFTER TAKEOFF, THE LANDING GEAR CIRCUIT BREAKER TRIPPED WITH THE LANDING GEAR AT MID RETRACTION. THE LANDING GEAR WAS PUMPED DOWN MANUALLY, AND A PRECAUTIONARY LANDING WAS MADE TO A REMOTE MAINTENANCESDR 4P1A2017042400001Igniter · brokenWHEN PERFORMING A PROGRESSIVE ROUTINE 300 HOUR INSPECTION ON THE ENGINE, FOUND PART OF THE RIGHT IGNITER MISSING. PERFORMED A BORESCOPE INSPECTION AND FOUND MELTED PIECES ON THE POWER TURBINE BLADES AND IN THE RIGHT EXHAUST DUCT. THERE WAS ALSO DENTS IN A COSDR 4P1A2017021500001Battery Cable · chafedPILOT REPORTED THAT THE ALTERNATOR FAIL LIGHT CAME ON BUT THE ALTERNATOR CONTINUED TO WORK. WHEN THE AIRCRAFT RETURNED TO HOME BASE, REPLACED THE ALTERNATOR CONTROL UNIT. ON THE RETURN TO SERVICE FLIGHT THE ALTERNATOR FAIL LIGHT CAME ON AGAIN. DECIDED TO REPLASDR CA150923007Lock · bent(CAN) AIRCRAFT WAS INSPECTED FOLLOWING RECEIPT OF MFG SAFETY COMMUNIQUE QSC-008. CO-PILOT SEAT FOUND WITH DAMAGE EXACTLY AS DESCRIBED IN THE COMMUNIQUE. NO SEAT LOCKING DIFFICULTY WAS NOTED BY CREW PRIOR TO NOTICING DEFECT.SDR OW6A20151002001Fitting · bentBENT FOOT CAPS ON CREW SEATS, WHICH MAY CAUSE BINDING & FAILURE OF THE SEAT LOCKS TO ENGAGE INTO THE SEAT RAIL.SDR CA150713005Engine · malfunctioned(CAN) THE PILOT REPORTED THAT DURING DESCEND AT APPROX 1000 FT ITT STARTED TO CLIMB, ALL OTHER PARAMETERS REMAINED NORMAL. AFTER LANDING THE PILOT DECIDED TO SHUT DOWN THE ENG & REQUIRED ASSISTANCE TO TAXI THE ACFT. NO INJURIES WERE REPORTED MFG WILL INVESTISDR CA130923005Cable · corroded(CAN) DURING A SCHEDULED INSPECTION, BOTH ACFT ELEVATOR CONTROL CABLES WERE FOUND BADLY CORRODED. BOTH ELEVATOR CONTROL CABLES WERE REPLACED WITH NEW CABLES, PN 100-618-4412-D01, AND PN 100-618-4413-D01. CABLES WERE INSTALLED IAW QUEST MM. THE CORRODED CABLESDR CA130513022Bulkhead · cracked(CAN) DURING A SCHEDULED INSPECTION, THE VERTICAL BULKHEAD FLANGES IN THE RT AND LT FLOATS, COMPARTMENT 13 WERE FOUND BUCKLED/CRACKED. THE DAMAGE WAS LIMITED TO THE CENTER FLANGE, WITH THE BULKHEAD SKIN DISTORTED IN A 1.5" DIAMETER. BOTH FLANGES WERE REPAIRESDR CA130513021Door · damaged(CAN) DURING A SCHEDULED INSPECTION, SMOKING RIVETS WERE FOUND IN THE LAP JOINT OF THE INTAKE DIVERSION DOOR AND DEFLECTOR. THE INTAKE PLENUM WAS REMOVED, ALL ATTACHMENT RIVETS REPLACED AND DIVERSION DOOR AND INTAKE PLENUM RE-INSTALLED.SDR CA130510001Arm · cracked(CAN) DURING A SCHEDULED INSPECTION, THE CENTER FORWARD FLAP BRACKET ON THE RT FLAP ASSY WAS FOUND CRACKED IN THE ARM RADIUS ON THE INBD SIDE. THE FLAP ROLLER ARM ASSY PN 100-330-5003-02 WAS REPLACED WITH A NEW FLAP ROLLER ARM ASSY SUPPLIED BY QUEST ACFT COMPSDR EVGR201304260001Tube · rupturedON ROLL OUT AFTER LANDING THE RT MAIN TIRE WENT FLAT. PILOT WAS ABLE TO KEEP THE AIRCRAFT ON THE AIRSTRIP AND NO DAMAGE RESULTED TO THE AIRCRAFT. FOLLOWING INSPECTION OF THE FLAT TIRE ASSEMBLY, IT WAS FOUND THAT THERE WAS DAMAGE TO THE TUBE WHICH APPEARED TO BSDR 2013FA0000251Duct · crackedDISCOVERED EXHAUST CASE FLANGE CRACKED (APPROX 2" LONG) AT THE RADIUS OF THE FLANGE TO THE EXHAUST CASE PROPER. THIS CRACK WAS NOTED DURING MX FOLLOWING AN EXHAUST STACK/DUCT PIPE FRACTURE.SDR CA121221005Landing Gear · slow(CAN) PILOT REPORTS ON NUMEROUS OCCASIONS THAT THE NLG WILL NOT FULLY RETRACT WITH THE LANDING GEAR PUMP ASSY. ON CLIMB OUT ONCE THE GEAR UP IS SELECTED, THE MAINS RETRACT NORMALLY, BUT THE SYS PUMP WILL CUT OUT BEFORE THE NOSE GEAR IS FULLY RETRACTED. STANDSDR CA121219014Spring · corroded(CAN) DURING ROUTINE INSPECTION, THE WATER RUDDER TENSION STEERING SPRINGS WERE FOUND BADLY CORRODED, WITH CABLE ATTACHMENT POINT EXCESSIVELY WORN. NEW SPRINGS ON ORDER, AND WILL BE REPLACED BEFORE ACFT LEAVES MAINTENANCE BASE.SDR EVGR20101006Fcu · leakingBRG GREASE WAS WASHED OUT DUE TO FUEL PUMP SEAL FAILURE. BLUE DYE WAS FOUND IN THE DRAIN BETWEEN THE FUEL PUMP AND FUEL CONTROL UNIT.SDR EVGR20101005Pump · leaking(EGVR) FUEL PUMP SEAL FAILED, WASHING OUT BLUE DYE FROM THE BEARING. DYE WAS FOUND COMING OUT THE FUEL PUMP /FCU DRAIN LINE.SDR 2010FA0001079Fcu · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BRG GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.SDR 2010FA0001074Pump · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BEARING GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.SDR 2010FA0000635Strut · leakingAFTER APPROX 65 HOURS SINCE THE NOSE STRUT WAS LAST RESEALED, IT WAS LEAKING BADLY AND NEEDED TO BE RESEALED AGAIN. HYD FLUID WAS COMING FROM THE LOWER GLAND OF THE TRUNNION SUGGESTING THAT THE BOTTOM POLY PACK SEAL WAS LEAKING. AFTER IT WAS DISASSEMBLED, THSDR 2010FA0001075Pump · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BRG GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.SDR 2010FA0001078Fcu · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BRG GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.SDR 2010FA0001077Seal · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BEARING GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.SDR 2010FA0001076Pump · leakingFUEL PUMP SEAL LEAKAGE THAT LED TO FCU BRG GREASE WASHOUT. DISCOVERED BY OBSERVING BLUE DYE COMING FROM WITNESS HOLE IN BOTTOM OF FCU.
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