N338QS, cancelled Jun 21, 2023

Service difficulty reports · 42

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 = 'N338QS' AND deregistration_id = 'N338QS-2023-06-21'
  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 JGVR20210319002Structure · corrodedREMOVED THE EXISTING EMERGENCY EXIT DOOR AND FOUND CORROSION ON THE DOOR AROUND THE CONTOUR RINGS. REMOVED THE CONTOUR RINGS FROM THE DOOR AND FOUND ADDITIONAL CORROSION. REPLACED CORRODED EMERGENCY EXIT DOOR WITH A NEW DOOR TEXTRON P/N 6911251-200.Mar 19, 2021 · N338QS · Cessna 680CE · Emergency ExitsSDR JGVR20210319001Spar · damagedREPAIRED THE LH WING REAR SPAR LOWER FORWARD ANGLE, LOCATED IN THE LH MAIN LANDING GEAR WHEEL WELL, BY BLENDING CORRODED AREA PERFORMING NDT AND INSTALLING A REPAIR DOUBLER PER ENGINEERING REPAIR ORDER.Mar 19, 2021 · N338QS · Cessna 680CE · Wing SparSDR DXTA2021011804615Bolt · failedWHEN THE MAIN CABIN DOOR HANDLE IS OPENED FROM THE INSIDE, THE HANDLE HITS A METAL CYLINDER THAT PROTRUDES FROM THE GROUND. IF THE HANDLE IS FORCED ALL THE WAY TO THE GROUND THE HANDLE WILL SLIDE AFT AND BECOME TRAPPED UNDERNEATH THE LIP OF THE METAL CYLINDERJan 17, 2021 · N338QS · Cessna 680A · Passenger/Crew DoorsSDR JGVR20200916001Skin · corrodedREMOVED CORRODED RT UPPER INBOARD BONDED SKIN ASSY, P/N UNKNOWN, AND INSTALLED A NEW BONDED SKIN ASSY P/N 6922680-28 ONTO RT UPPER INBOARD WING. WORK PERFORMED IN REFERENCE TO CESSNA 680 SRM 51-40-03, 51-40-06 AND 51-40-08.Sep 16, 2020 · N338QS · Gulstm 680 · Wing, Plate/SkinSDR JGVR20200914002Skin · corrodedREMOVE AND REPLACE CORRODED RT WING TRAILING EDGE SKIN P/N 6922681-70. REMOVED AND REPLACED CORRODED RT WING TRAILING EDGE SKIN BOND ASSEMBLY WITH NEW P/N 6922681-70 S/N LOT NR 29598079.Sep 14, 2020 · N338QS · Cessna 680A · Wing, Plate/SkinSDR JGVR202009141001Skin · corrodedBLENDED MULTIPLE AREAS OF CORROSION ON LT UPPER WING SKIN AT WS 37 FROM FS 408.46 THRU 482.46. PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION ON BLENDED AREAS. REMOVED BLENDED FASTENERS AND REPLACED FASTENERS AS NECESSARY WITH HLSep 14, 2020 · N338QS · Cessna 680A · Wing, Plate/SkinSDR JGVR20200902001Spar · corrodedLT MLG WHEEL WELL LOWER AFT SPAR HAS 2 AREAS OF VERIFIED CORROSION. REMOVED 3 EACH HI-LOKS FROM LT MLG WHEEL WELL LOWER AFT SPAR FOR ACCESS. BLENDED 2 EACH AREAS OF CORROSION ON LT MLG WHEEL WELL LOWER AFT SPAR. OTBD AREA WAS FOUND TO BE MILD SURFACE CORROSSep 2, 2020 · N338QS · Cessna 680A · Wing SparSDR JGVR20200827002Drag Angle · corrodedRT WING AFT DRAG ANGLE HAS 7 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 6 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. REPAIRED DELAMINATED AREA ON RT WING UPPER MIDDLE DRAG ANGLE, PER S-750-ATA51-01RD REV A, DATED 17 FEB 09, SUPPOAug 27, 2020 · N338QS · Cessna 680A · Wing Main, Frame StructureSDR JGVR20200827001Hinge Fitting · corrodedRUDDER UPPER HINGE POINT, LOWER BRACKET HAS VERIFIED CORROSION AROUND ATTACH BOLT. HAND SANDED AREA OF CORROSION LOCATED ON UPPER RUDDER HINGE, LOWER PLATE, LT SIDE. FOUND CORROSION DAMAGE TO BE LEVEL 2, PER NJA GMM 2.2.2. REMOVED AND REPLACED CORRODED LOWEAug 27, 2020 · N338QS · Cessna 680A · Rudder StructureSDR DXTA2019F00066Spar Cap · corrodedVERTICAL STAB AFT SPAR CORROSION. ACCOMPLISHED ENGINEERING LETTER DQ15722M1 DATED SEPTEMBER 13, 2018; 680-0011. VERTICAL STABILIZER AFT SPAR CAP/RIM (P/N 6961526-5) DAMAGE (CORROSION).Sep 17, 2018 · N338QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR DXTA2019F00060Spar Cap · corrodedVERTICAL STABILIZER AFT SPAR CAP/RIM DAMAGE (CORROSION). ENGINEERING REPAIR DEFINITION DQ15722M1 DATED 9/13/2017.Sep 13, 2018 · N338QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR DXTA2019F00059Spar · corrodedREPAIR OF CORROSION ON LT WING REAR SPAR LOWER CAP. REPAIR DEFINITION NR S-680-0011/05RD DATED 9/4/2018 WITH FAA FORM 8100-9 DATED 9/7/2018.Sep 12, 2018 · N338QS · Cessna 680CE · Wing SparSDR DXTA2019F00057Spar · corrodedREPAIR OF CORROSION ON LT WING REAR SPAR LOWER CAP. REPAIR DEFINITION S-680-0011/05RD DATED 9/6/2017 WITH FAA FORM 8100-9 DATED 9/7/2018.Sep 12, 2018 · N338QS · Cessna 680CE · Wing SparSDR DXTA2018FA0000361Spar Web · damagedREPAIR OF RUDDER FWD SPAR LIGHTENING HOLE DAMAGED FLANGE. ENGINEERING REPAIR LETTER DQ1562M1 DATED SEPTEMBER 6, 2018.Sep 11, 2018 · N338QS · Cessna 680CE · Rudder, Spar/RibSDR JGVR20170710002Skin · dentedDENT ON THE BOTTOM OF THE LEFT WING 44 INCHES OTBD OF THE LT LANDING LIGHT. CONTOURED SKIN IAW SRM 51-00-03, AND 51-10-01. PERFORMED EDDY CURRENT INSPECTION IAW NDT MANUAL, PART 6, 20-00-02. INSPECTION REVEALED NO CRACK INDICATIONS.Jul 7, 2017 · N338QS · Cessna 680SOV · Leading Edge DevicesSDR JGVR20170710001Skin · dentedDENT IN THE RT WING LEADING EDGE CUFF SKIN. PERFORMED PERMANENT REPAIR IAW SRM 51-40-03, 51-00-03, AND MM 57-40-00Jul 7, 2017 · N338QS · Cessna 680SOV · Wing, Plate/SkinSDR DXTR2016122704Skin · corrodedTHE LEFT AND RIGHT UPPER AND LOWER HORIZONTAL STABILIZER SKIN HAVE AREAS OF CORROSION, BLENDED AREAS OF CORROSION, AND RETURNED TO SERVICE.Dec 27, 2016 · N338QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR DXTR2016122703Skin · corrodedLEFT ELEVATOR LEADING EDGE AND AFT SKIN HVE AREAS OF CORROSION, BLENDED AREAS OF CORROSION, AND RETURNED TO SERVICE.Dec 27, 2016 · N338QS · Cessna 680CE · Elevator, Plate/SkinSDR DXTA2016033106218Skin · dentedLEFT WING HAS A DENT ON BOTTOM OF LE FWD OF OVERWING FUEL CAP. RT WING HAS LONG DENT RUNNING ABOUT 3 INCHES ALONG A LINE OF RIVETS ON BOTTOM OF LE FWD OF OVERWING FUEL CAP. CLEANED DAMAGED AREA. PERFORMED DETAILED VISUAL INSPECTION. MAPPED DAMAGE. PERFORMMar 31, 2016 · N338QS · Cessna 680CE · Wing, Plate/SkinSDR DXTA2015090306075Unknown · odorPASSENGERS COMPLAINED OF BOTH EXCESSIVE HEAT & EXHAUST ODOR. AIR FLOWS FROM BOTH COCKPIT & CABIN, WEMACS VERY LOW FROM ENGS ONLY, IMPROVES WITH APU ON LINE. WHEN AN INFLIGHT APU START WAS ATTEMPTED THE EXHAUST GAS ODOR WAS VERY STRONG. COMPLIED WITH APU, LSep 2, 2015 · N338QS · Cessna 680CE · Air Distribution SystemSDR DXTA2015081706060Trim System · uncontrollablePRIMARY STAB TRIM RUNAWAY INITIALLY UNCONTROLLABLE, ACFT PITCHED DOWN LOSING 2000 FEET UNTIL ACTUATING RED DISCONNECT BUTTON & TURNING ON SECONDARY TRIM, INDICATION WE HAD WAS ERRATIC FROM DASHED YELLOW LINES TO FULL UP & DOWN INDICATIONS. WE HAD CYAN AUTO PIAug 16, 2015 · N338QS · Cessna 680CE · Stabilizer Control SystemSDR DXTA2015031305994Control Handle · malfunctionedLEFT MLG WOULD NOT INDICATE DOWN & LOCKED WHEN LOWERED FOR LANDING. R & R THE LG CONTROL HANDLE ASSEMBLY IAW MM 32-30-10. OPS CHECKED GOOD. COMPLIED WITH HYD SYS BLEED IAW MM 12-12-02. OPS & LEAK CHECKED GOOD. ALL LIGHT INDICATIONS OPERATIONS CHECKED GOOMar 12, 2015 · N338QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2013120905593Actuator · malfunctionedUPON SELECTING LG DOWN RT MLG INDICATED NOT DOWN. RED UNLOCK LIGHT WAS ILLUMINATED AT THE SAME TIME. BY CHECKING A ROTARY TEST, BOTH RT LDG GEAR LIGHT BULBS WERE FUNCTIONING.Dec 6, 2013 · N338QS · Cessna 680CE · Landing Gear ActuatorSDR CWQR20131016046Door Frame · crackedDURING INSPECTION, FOUND THE OUTER DOOR FRAME CRACKED UNDER THE TELECOPING ROD ATTACH POINT ON THE FWD OUTER CABIN DOOR FRAME. VERFIED CRACK WITH EDDY CURRENT INSPECTION. REPLACED CABIN DOOR FRAME.Oct 16, 2013 · N338QS · Cessna 680CE · Fuselage Main, StructureSDR CWQR20131016045Door Frame · crackedDURING AN INSPECTION, FOUND OUTER DOOR FRAME CRACKED UNDER THE TELECOPING ROD ATTACH POINT ON THE AFT OUTER CABIN DOOR FRAME. VERFIED CRACK WITH EDDY CURRENT INSPECTION. REPLACED CABIN DOOR FRAME.Oct 16, 2013 · N338QS · Cessna 680CE · Fuselage Main, StructureSDR CWQR20130501033Firewall · crackedDURING A SCHEDULED INSPECTION, FOUND THE APU FIREWALL CRACKED 2.75" IN LENGTH. REPLACED WITH NEW FIREWALL. THIS CONDITION AND A PICTURE WAS SENT TO UNDER SCR 657019.May 1, 2013 · N338QS · Cessna 680CE · APU Cowling/ContainmentSDR DXTA2013040105343Bracket · looseFLAPS FAILED IN FLIGHT BETWEEN 15-35 DEGREES. TRIED RESET BUTTON SEVERAL TIMES. AFTER LANDING AND AFTER POWER DOWN FLAPS RETRACTED NORMALLY. FAULT CODES 1 AND 9 ON CONTROL BOX. INSPECTED FLAP FLEX DRIVES AND FOUND RT FLAP POSITION SENSOR RETAINING BRACKET LMar 30, 2013 · N338QS · Cessna 680CE · Fuselage Miscellaneous StructureSDR CWQR20121221053Line · chafedDURING A SCHEDULED INSPECTION, THE SHROUDING SCAT DUCT (PN S1053E24T) WAS FOUND TORN IN SEVERAL PLACES. WHEN REPLACING THE SCAT DUCT WE FOUND THE DUCT HAD CHAFED THE HYD LINE MORE THAN 50 PERCENT OF WALL THICKNESS. THIS HYD LINE DAMAGE IS NOT VISABLE DURING IDec 21, 2012 · N338QS · Cessna 680CE · Hydraulic System, MainSDR DXTA2012101505144Strut · dischargedON GEAR RETRACTION, A VIOLENT, RHYTHMIC, CONTINUOUS THUMPING WAS FELT AND HEARD COMING FROM THE NOSE GEAR. THE RED GEAR UNLOCK LIGHT REMAINED ON ALSO, UNTIL GEAR EXTENSION. AFTER EXTENSION, ALL OPS, INCLUDING NOSE GEAR STEERING, WERE NORMAL. FOUND NOSE GEAOct 12, 2012 · N338QS · Cessna 680CE · Main Landing Gear Strut/Axle/TruckSDR DXTA2011011804415Switch · intermittentNLG TOOK 45 SECONDS TO EXTEND AFTER GEAR HANDLE WAS LOWERED. RED UNLOCK LIGHT WAS ILLUMINATED DURING THAT TIME FRAME. CHECKED SWITCH ADJUSTMENT & FOUND NOSE UPLOCK SWITCH PLUNGER SWITCH ADJUSTMENT & FOUND NOSE UPLOCK SWITCH PLUNGER BOTTOM OUT. CHECKED RESISJan 15, 2011 · N338QS · Cessna 680CE · Nose/Tail Landing GearSDR DXTA2010071204147Connector · damagedDURING CRUISE & DESCENT, MLG UNLOCK ANNUNCIATOR ILLUMINATED ON & OFF IN TURBULENCE. CYCLED MLG APPLYING FREEZE SPRAY TO UPLOCK SWITCH. NO DEFECTS NOTED. CHECKED RIGGING. RIG CHECK GOOD. OHM CHECKED NOSE UPLOCK SWITCH. RESISTANCE .002 ACROSS ALL CONTACTS. CHJul 11, 2010 · N338QS · Cessna 680CE · Landing Gear System WiringSDR DXTA2010051704096Uplock Switch · out of adjustDURING CRUISE FLIGHT, IN MODERATE TURBULENCE, THE RED GEAR UNSAFE LIGHT FLASHED ON AND OFF FOR AS LONG AS THE TURBULENCE LASTED. IT STOPPED IN SMOOTH AIR. NO PROBLEMS NOTED DURING EXTENSION FOR LANDING. FOUND THE LT AND RT MAIN GEAR UPLOCK SWITCHES OUT OF ADJMay 13, 2010 · N338QS · Cessna 680CE · Landing Gear Position and WarningSDR DXTA2008121503402Actuator · inoperativeUPON LOWERING GEAR HANDLE, NOSE GEAR DID NOT LOCK DOWN. RECYCLED GEAR WITH SAME RESULTS. ON GO AROUND, NOSE GEAR LOCKED DOWN ON ITS OWN. DID NOT RUN CHECKLIST OR BLOW GEAR DOWN. REMOVED NOSE GEAR ACTUATOR AND INSTALLED, INSPECTED ACTUATOR IAW MM 32-30-30, OPSDec 15, 2008 · N338QS · Cessna 680CE · Landing Gear ActuatorSDR DXTA2008121603402Landing Gear · malfunctionedUPON LOWERING GEAR HANDLE, NOSE GEAR DID NOT LOCK DOWN. RECYCLED GEAR WITH SAME RESULTS. ON GO-AROUND, NOSE GEAR LOCKED DOWN ON ITS OWN.Dec 15, 2008 · N338QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA200802749Actuator · malfunctionedRUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPONENTS. C/W SATISFACTORY OPERATIONAL CHECKS IAW MM 27-20-00 & FT-680-0022.Jan 5, 2008 · N338QS · Cessna 680CE · Rudder ActuatorSDR DXTA200702465Servo · out of adjustAIRCRAFT WILL NOT FLY STRAIGHT WITH A/P AT FL360. AILERON TRIM FULL R. RUDDER TRIM .1250 L, SLIGHT LT TURN, FUEL BALANCED, .79M / FL240 A TRIM FULL R - RUD TRIM .1250 L, NO TURNS, FUEL BALANCED, 290 KTS / 10,000 FT A TRIM .5 R - RUD TRIM .1250 L, NO TURNSep 10, 2007 · N338QS · Cessna 680CE · Aileron Control SystemSDR DXTA200702466Starter Gen · trippedDURING TAKEOFF POWER APPLICATION THE LT GENERATOR HAS TRIPPED OFF LINE. ALL PRE-FLIGHT TESTS AND STARTS SHOW NORMAL OPERATION. REPLACED LT ENGINE STARTER/GEN WITH OVH STARTER/GEN. PERFORMED GROUND OPS TEST OF BOTH GENERATORS, TEST GOOD. RAN LT ENG TO POWER WSep 10, 2007 · N338QS · Cessna 680CE · Starter-GeneratorSDR DXTA200702376Position Sensor · malfunctionedAMBER CAS (FLAPS FAIL) MESSAGE PUSHED EVENT MARKER, AT FL410, FOLLOWED CHECKLIST FLAP ON NR 2 DISPLAYED MOVED TO 7 DEGREES, WHEN IND = 0 DEGREES. R & R BOTH NR 1 & 2 FLAP POSITION SENSOR'S , OPS CHECKS GOOD, I/A/W 860 MM 27-50-00.Aug 1, 2007 · N338QS · Cessna 680CE · Trailing Flap Position Indicating SystemSDR DXTA200601807Uplock Switch · out of rigAT FL410 RED GEAR UNSAFE LIGHT ILLUMINATED AND EXTHINGUISHED APPROX 5-6 TIMES. NO GEAR HORN OR CAS MESSAGE. PERFORMED CONTINUITY CHECKS OF L, R + NOSE UPLOCK SWITCHES. NO DEFECTS NOTED. DURING GEAR FUNC. CHK, MONITORED LDG SYS PCB'S IN CMS. NO DEFECTS NOTEDec 19, 2006 · N338QS · Cessna 680CE · Landing Gear Position and WarningSDR DXTA200601735Connector · arcedNOTED ODOR IN COCKPIT FOUND CABIN PRESS CB POPPED. APPROX 30 SEC LATER THE RT ELEC PWR FEED, 3 CB POPPED NOTICED PRESSURE MODE SWITCH LIGHTS INOP. HAD TO USE MANUAL CHERRY PICKER TO DESEND CABIN ON DESCENT. OPENED RT C/B PANEL. NOTICED STRONG BURNING ODOR DINov 18, 2006 · N338QS · Cessna 680CE · Electrical Power System WiringSDR DXTA200601278Tire · failedON TOUCH DOWN LEFT MAIN TIRES LOCKED UP AND BLEW OUT ON LANDING ROLL. NO ANTISKID CAS MESSAGE WAS DISPLAYED. - REMOVED & REPLACED LEFT INBOARD & OUTBOARD WHEELS TIRES & BRAKES WITH NEW IAW 680 MM 32-41-20 & 32-42-10. OPS CHECKED ANTI SKID SYSTEM IAW 680 MM 32-Mar 3, 2006 · N338QS · Cessna 680CE · TireSDR DXTA200501023Air Data Module · failedAIR SPEED RT PFD FAILED, NO AIRSPEED INDICATION ON TAKEOFF ROLL. LEAK CHECKED COPILOT PITOT STATIC SYSTEM WITH NO DEFECTS NOTED. SYSTEM OPERATED NORMALLY. SWAPPED NR 1 AND NR 2 AIR DATA MODULES FOR FURTHER TROUBLESHOOTING IAW CE680 M/M CH 34-12-00, 34-11-00Oct 14, 2005 · N338QS · Cessna 680CE · Airspeed/Mach Indicator
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