N695QS
Service difficulty reports not matched to an aircraft · 27
They name N695QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N695QS' AND registry_match IS NULL 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 n_number = 'N695QS' AND registry_match IS NULL 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 DXTA2019020191973Actuator · malfunctionedNOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GREEN NOSE GEAR LIGHT REMAINED ILLUMINATED AND ASSOCIATED AIRFLOW NOISE WAS EVIDENT. PERFORMED QRH PROCEDURE AND FLEW LEG WITH GEAR EXTENDED BELOW 250K. INSPECTED NOSE GEAR EXTENSION AND UP LOCK SWITCH ALL WITHIN LIMISDR JGVR20171114001Bracket · corrodedUPPER BRACKET OF THE CENTER RUDDER HINGE FOUND CORRODED OUT OF LIMITS. REPLACED THE BRACKET.SDR JGVR20171113001Axle · damagedFOUNDS PLATING MISSING ON THE NOSE WHEEL AXLE TUBE DURING NOSE WHEEL R&R. REPLACED AXLE TUBE WITH NEW ONE P/N 7142022-21.SDR DXTR2015020401Bracket · crackedLOWER CLIP ON VERTICAL STABILIZER HAS 2 SMOKED HI-LOCKS ON OTBD EDGES ON FWD SIDE. FOUND A CRACK PROTRUDING FROM THE LT OTBD LOWER PIVOT FITTING FLANGE TRAVELING UP & OTBD APPROX .5" FOUND 2 CRACKS TRAVELING FROM THE RT OTBD HOLE, ONE TRAVELING UP & OTBD APPRSDR DXTA2014121505945Line · chafedLOW HYD LEVEL LIGHT CAME ON SHORTLY AFTER TAKEOFF. RAISED THE GEAR & THEN THE FLAPS. THE LIGHT CAME ON IMMEDIATELY AFTER THE FLAPS WERE RAISED. THERE WERE NO OTHER INDICATIONS. WENT TO THE ABBREVIATED CHECKLIST WHICH STATED IN PART TO LAND AS SOON AS PRACTSDR DXTA2014062305805Landing Gear · malfunctionedDURING APPROACH, SELECTED GEAR DOWN. MAIN GEAR EXTENDED NORMAL BUT THE NOSE GEAR DID NOT EXTEND. WHILE RUNNING THE LANDING GEAR WILL NOT EXTEND CHECKLIST, NOTICED WHEN TEE HANDLE IS PULLED, THERE WAS NO RESISTANCE. FELT NOTHING WHEN PULLED DOUGHNUT TO BLOW SDR DXTA2014060505791Relay · failedON TAXI OUT RECEIVED FLASHING LOW BRAKE PRESSURE & ANTI SKID INOPERATIVE ANNUNCIATORS. ABOUT 20 SECONDS LATER, LOST NORMAL BRAKES, BRAKE PEDALS LOST PRESSURE & WENT TO THE FLOOR. HAD TO USE EMERGENCY BRAKE SYS TO STOP ACFT. SHUT DOWN ACFT & HAD TO BE TOWED SDR DXTA2013121805599Relay · unserviceableUPON SHUTDOWN OF THE APU WE NOTICED A STRONG ODOR WHICH SMELLED LIKE ELEC WIRES BURNING AS WE WALKED TOWARDS THE LAVATORY, OPENED THE ACCESSORY DOOR TO THE APU & NOTICED A VERY STRONG ELEC SMOKE ODOR. DISCONNECT THE BATTERY, INSPECTED AFT J BOX AREA & FOUND RSDR DXTA2013090505494Access Panel · corrodedWHILE PERFORMING MX, FOUND SURFACE CORROSION ON FUEL PANEL 510DB DOUBLER.SDR DXTA2013082005483Brake Assy · malfunctionedDURING TAXI WHILE APPLYING EVEN BRAKE PRESSURE TO SLOW ACFT, RT BRAKE SUDDENLY BROKE FREE(STOPPING PRESSURE ON THE BRAKES RELEASED) CAUSING THE ACFT TO SWERVE ABRUPTLY TO THE LEFT. LEFT PILOT WAS OPERATING CONTROLS. RIGHT PILOT DID NOT APPLY HIS BRAKES. RIGHSDR DXTA2013080505466Master Cylinder · failedRIGHT BRAKE FAILED DURING TAXI. RIGHT COCKPIT BRAKE PEDAL FAILED TO MAINTAIN BRAKE PRESSURE TO RT MAIN WHEEL BRAKE. LT PILOT TOOK CONTROL OF THE ACFT AND BRAKING ACTION APPEARED TO BE SOMEWHAT NORMAL FOR THE REMAINDER OF THE TAXI. RT BRAKE DID SEEM SOFTER TSDR DXTA201304150555Actuator · seizedON LANDING GEAR EXTENTION LT MLG DID NOT LOCK DOWN AND HAD UNLOCK LIGHT ON TESTED LIGHT AND LIGHT WORKED DID CHECK LIST AND STILL NO LT MLG ON LANDING AND AT TOUCH DOWN LT MLG LOCKED AND HAD THREE GREEN. REMOVED LT MLG ACTUATOR, REMOVED SEIZED UPPER BOLT FROMSDR DXTA2013050805387Ring Assembly · unserviceablePERFORMED BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. DISASSEMBLED CLEANED AND VISUALLY INSPECTED HT DISC ASSEMBLY. REPLACED 70 BLADES WITH NEW DUE TO IMIPACT DAMAGE. SKIM CUT TO 11.5685 BALANCE AND B25 TRIM ADDEDSDR DXTA2012061805003Unknown · odorDURING DESCENT, ENCOUNTERED VERY STRONG INTERMITTENT ODOR ON THE FLIGHT DECK. DURING POSTFLIGHT CHECK WITH THE BATTERY MASTER ON, ODOR REAPPEARED. COULD NOT DUPLICATE OF INSPECTION.SDR DXTA2012061805002Actuator · inoperativeDURING CLIMB WITH THE GEAR UP, THE GREEN NOSE GEAR DOWN LIGHT CAME ON WITH NO RED GEAR UNSAFE LIGHT. PUT THE GEAR HANDLE DOWN WITH THE ABNORMAL CHECKLIST, THE NOSE GEAR LIGHT WENT OUT FOR A SECOND AND CAME BACK ON. BLEW THE GEAR DOWN WITH THE BOTTLE AS PART SDR DXTA2011111004780Oil System · overservicedWITH APU ON AND BLEED AIR ON, COCKPIT AND CABIN FILLED WITH THICK, PUNGENT AND ACRID SMOKE. TROUBLESHOT TO OIL LEVEL TO HIGH, ADJUSTED OIL LEVEL TO CORRECT LEVEL IAW MM 12-11-03. CLEANED WATER SEPERATOR CONDENSER IAW MM 12-19-02. OPS AND LEAK CHECKED GOOD.SDR DXTA2011010304388Brake Assy · weakAFTER TOUCHDOWN BRAKES FELT SPONGY AND THEN BECAME EXCESSIVELY GRABBY WHEN SLOWING. CONDUCTED BRAKE BLEED PROCEDURE AND TAXI CHECK. BRAKES FUNCTION NORMAL AT THIS TIME IAW MM 32-42-00.SDR DXTA2010012503955Hinge · lack of lubePASSING THROUGH 18,000' AND AN AIRSPEED OF APPOX 260KTS, FELT A SUDDEN JOLT FOLLOWED BY MEDIUM TO HIGH FREQUENCY VIBRATIONS IN THE FUSELAGE AND FLIGHT CONTROLS. AIRPLANE ALSO SEEMED TO WANT TO PITCH NOSE DOWN. LEVELED OFF AND DISENGAGED THE AUTOPILOT AND THESDR DXTA2009070103711Bulb · burnedSMOKE FROM CABIN LIGHTS IN BETWEEN SEATS 4 AND 6 AFTER ABOUT 40 MINUTES OF USE. SMOKE AND ELECTRICAL ODOR DISSIPATED WHEN CABIN LIGHT SWITCH TURNED OFF. R & R BURNED BULB & BULB CLIP WITH NEW BULB & CLIP. LIGHT OPERATES NORMAL AT THIS TIME IAW MM 33-20-01.SDR DXTA2009031603547Pcb · inoperativeON TAKEOFF ROLL JUST PRIOR TO 70 KTS, NO TAKEOFF ANNUNCIATOR, WARNING HORN, AND MASTER CAUTION. EVERYTHING AS FAR AS FLAPS, SPEED BRAKES & TRIM WAS IN CORRECT POSITION FOR TAKEOFF. AFTER SHUTTING DOOR, RESTARTED ACFT & CHECKED TO MAKE SURE ANNUNCIATOR LIGHT, SDR DXTA200702698Water Separator · odorNOXIOUS FUMES ENTER COCKPIT WHEN COCKPIT TEMPERATURE CONTROL IS RAISED TO HEAT COCKPIT. REMOVED & CLEANED WATER SEPARATOR. REINSTALLED WATER SEPARATOR IAW CESSNA 560XL MM CH 12-19-02. OPS & LEAK CHECK GOODSDR DXTA200701832Connector · dirtyDURING TAKEOFF THERE WAS A LARGE THROTTLE SPLIT AND TOOL, A LOT OF RT RUDDER TO MAINTAIN DIRECTIONAL CONTROL. RESET FAULT, DISCONNECTED, CLEANED AND INSPECTED, RECONNECTED WIRING HARNESS IAW MM 73-20-02. PERFORMED ENGINE GROUND RUN. NO DEFECTS NOTED.SDR DXTA200601408Control Unit · failedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. WITH LDG GEAR HANDLE UP STILL HAD (3) GREEN INDICATION. CYCLED GEAR HANDLE DOWN AND BACK UP WITH SAME INDICATION. SELECTED LANDING GEAR HANDLE DOWN AND PERFORMED (MANUAL GEAR EXTENSION) IAW CHECKLIST. REMOVED ANDSDR DXTA200500958A/C Pack · odor15 MIN PRIOR WITH APU RUNNING AT HPN (NJA FACILITY) OUR A/C WAS TAIL TO TAIL WITH A COMPANY ULTRA. THE ULTRA STARTED IT'S ENGINES AND RAN FOR 10 TO 15 MINS BLOWING ITS FUMES INTO OUR TAIL. AT FL 380, SELECTED A WARMER TEMP AND IMMEDIATELY HAD JET EXHAUST FUMSDR DXTA200500809Control Cable · shearedLT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PEDAL AND FIREWALL. FOUND RUDDER CONTROL CABLE ASSY (UPPER) BROKEN AT 9 O' CLOCK POSITION. REPLACED RSDR DXTA200400386Arm · unsecureDURING CLIMB OUT, THE GEAR UNLOCK LIGHT CAME ON, RECYCLED GEAR AND PROBLEM DID NOT GO AWAY. ACCOMPLISHED AIR TURN BACK TO MRY. FOUND THE EMERGENCY GEAR BOTTLE ARM NOT SAFETIED AND THE ARM PARTIALLY ACTUATED SUPPLYING NITROGEN TO THE GEAR EXTEND SYSTEM. RESESDR DXTA200300186Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.
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