N378QS, cancelled Jul 2, 2026
Service difficulty reports · 43
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 = 'N378QS' AND deregistration_id = 'N378QS-2026-07-02' 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 = 'N378QS' AND deregistration_id = 'N378QS-2026-07-02' 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 DXTA2026022707024Bearing · defectiveAFTER TAKEOFF, GEAR RETRACTED NORMALLY. DURING CLIMB OUT (APPROXIMATELY 10000-12000 FEET) THE RED GEAR UNLOCK LIGHT ILLUMINATED. RAN QRH. DURING THE GVI OF THE NLG ASSEMBLY FOUND THE UPLOCK BEARING WAS COMPLETLY MISSING FROM THE NOSE GEAR CAUSING THE UPLOCK SSDR JGVR20251117005Doubler · corrodedBLENDED AREAS OF CORROSION ON RT WING FUEL FILLER ASSEMBLY DOUBLER PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20251117004Skin · corrodedBLENDED 4 AREAS OF CORROSION LOCATED ON OUTER SKIN OF E-EXIT ALONG CONTOUR RING INNER EDGE, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20251117003Hinge Bracket · corrodedBLENDED CORRODED AREA ON THE VERTICAL STABILIZER MIDDLE RUDDER HINGE UPPER BRACKET, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DXTA2025042903233Strut · contaminatedGEAR POSITION & WARNING: AFTER NORMAL TAKEOFF TRIED TO RETRACT THE GEAR, HEARD AND FELT A THUD. GEAR DID NOT RETRACT. RAN QRH AND UNEXPECTED THREAT FLOW CHART. RETURNED AND LANDED AT KIAD. DID NOT DECLARE AN EMERGENCY. JACKED ACFT & PERFORMED OPS CHECK OF THE SDR DXTA2024082800343Switch · defectiveWHEN PLACED IN THE "ON" POSITION, THE EMER LTS SWITCH IS INOP. WHEN PLACED IN THE "OFF" OR "ARMED" POSITION THE SWITCH AND LIGHTS FUNCTION NORMALLY. CORRECTIVE ACTION: INSTALLED NEW TOGGLE SWITCH. P/N A3-201-01A. PERFORMED EMERGENCY LIGHTING OPERATIONAL CHECKSSDR DXTA2024070312250Duct · blownAT 39,000 FEET WHILE IN CRUISE WE HEARD A LOUD BANG. AT THAT TIME, CABIN ALTITUDE BEGAN RISING 750' PER MINUTE. WE WERE AT AROUND 9.0 PSI DIFFERENTIAL AROUND 6000 FEET CABIN ALT. WITHIN MINUTES WE KEPT CLIMBING TO 14000' CABIN ALTITUDE. EMERGENCY DESCENT ANDSDR DXTA2024061812087Target · detachedCABIN DOOR OPEN CAS ILLUMINATED WHEN PREPARING FOR FLT. CYCLED DOOR IAW QRC. LIGHT REMAINED. PERFORMED OPS CHKS & CLOSED MED. TURNED OFF BLEED AIR & FOUND CAS MESSAGE. WENT INTO CMC & FOUND LOWER LOCK VENT DOOR SHOWING OPEN. FOUND DOOR BRUSH SEAL DAMAGED SDR DXTA2024060711976Proximity Switch · out of adjustMAIN DOOR: CABIN DOOR OPEN CAS MESSAGE DOES NOT EXTINGUISH WHEN DOOR CLOSED. ALL DOOR LOCKED PEEPHOLE INDICATORS INDICATE LOCKED. //SIGNOFF// ADJUSTED MED VENT DOOR PROXIMITY SWITCH IAW CE-680 MM 52-10-40. OPS CHECK GOODSDR DXTA2024041011456Precatch · malfunctionedMAIN DOOR PRECATCH NOT WORKING PROPERLY. DOOR DOES NOT SET PROPERLY. VERIFIED THE PRECATCH IS INTERMITTENT, AND OCCASIONALLY BOUNCE OUT OF PRECATCH. GAINED ACCESS TO PRECATCH MECHANISM. PERFORMED RIGGING OF PRECATCH, IAW MM CHAP 52-10-00. OPS CHECK GOOD. CLOSESDR DXTA2022091270160None · defectiveFORWARD EMERGENCY EXIT LIGHT ABOVE RIGHT WING IS MUCH DIMMER THAN THE OTHER EMERGENCY LIGHTS. // SIGNOFF// REMOVED AND REPLACED FOWARD EMER EXIT LIGHT ABOVE RIGHT WING WITH NJA PROVIDED NEW PART. OPERATIONAL CHECKS GOOD. ALL WORK
COMPLETED IAW CE-680 AMM 33-5SDR DXTA2022051361700Light · brokenSHARK LIGHT. EMERGENCY EXIT LIGHT IN RIGHT LANDING GEAR LENS INOP. REMOVED AND REPLACED RH EMERGENCY EXIT LIGHT IN RIGHT WING LANDING GEAR LIGHT REF E680 AMM 33-50-00. OPS CHECK GOOD AT THIS TIME.SDR DXTA2022022157120Not Reported · not reportedCABIN EMERG LIGHT: REPEAT WRITEUP. EMER LIGHTS FAILED PRE BATTERY CONNECTED TEST AND POST BATTERY CONNECTING TESTING, THEY NEVER CAME ON. ALSO, AFTER CONNECTING MAIN BATTERIES, COCKPIT MAIN BATTERY SWITCHES AND APU MASTER WERE LEFT IN "ON" POSITION BY MAINTENSDR JGVR20210420003Panel · corrodedFOUND 200 AREAS OF CORROSION ON INNER THRESHOLD PANELS. REMOVED PAINT FROM SUSPECT AREAS ON INNER THRESHOLD PANELS AND FOUND 180 AREAS THAT WERE BEYOND SURFACE CORROSION. MATCH DRILLED AND TRIMMED NEW FWD(P/N: 6911084-11), CENTER(P/N: 6911084-5), AFT(P/N: 6911SDR JGVR20210420002Link · corrodedFOUND PITTING CORROSION ON TRAILING LINK UPPER LUGS. REPLACED RH MLG TRAILING LINK ASSEMBLY AND INSTALLED CUSTOMER SUPPLIED INSPECTED TRAILING LINK ASSEMBLY IN SAME LOCATION IAW CESSNA 680 MM 32-10-00.SDR JGVR20210420001Skin · corrodedMECHANICALLY BLENDED MULTIPLE SPOTS OF VERIFIED CORROSION ON LH WING UPPER SKIN WHERE FWD AND AFT DRAG ANGLES ATTACH. FOUND CORROSION BLENDS UNDERNEATH AFT AND FWD DRAG ANGLES TO TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS. COMPARED CORROSION BLEND MEASUREMENTSSDR DXTA2021033040260Pressure Switch · defectiveFUEL PRESSURE LOW R AMBER CAS: CLIMBING OUT OF 370 AMBER CAS MESSAGE CAME ON WHILE READING CHECKLIST LIGHT WENT OUT, WE LEVELED OFF AT 400 AMBER CAS MESSAGE CAME BACK ON AND STAYED ON COMPLETED THE CHECK LIST WITH NO OTHER PROBLEMS SIGN OFF. OPENED THE RT ENGSDR JGVR20180126005Skin · corrodedCORROSION ON TOP OF THE RT HORIZONTAL STAB PANEL 352AC. REMOVED MINOR CORROSION AND APPLIED PROTECTIVE TREATMENT TO BARE METAL. CORROSION DETERMINED TO BE BEYOND LIMITS. BLENDED CORROSION AND POLISHED AREA TO 20:1 RATIO AND VERIFIED SURFACE CRACK AND CORROSDR JGVR20180126004Skin · corrodedCORROSION ON TOP OF LT HORIZONTAL STAB PANEL 351AC. REMOVED MINOR CORROSION. PERFORMED AN EDDY CURRENT CHECK OF BLENDED AREA. INSPECTION REVEALED NO CRACKS OR CORROSION INDICATIONS. PERFORMED AN ULTRASONIC THICKNESS CHECK ON BLENDED AREA. READINGS WERE RESDR DXTR2017051705Cowling · delaminatedTHE LT ENGINE UPPER COWLING HAS AN AREA OF DELAMINATION ON THE INNER SURFACE. THE DAMAGE
MEASURES APPROXIMATELY 18.0 INCHES BY 12.0 INCHES. AQRD ERO-895901 PROVIDED ENGINEERING FOR A ONE-TIME FLIGHT TO MOVE THE AIRCRAFT TO KADS WHERE A PERMANENT REPAIR WILL BSDR DXTR2017051703Skin · corrodedESCAPE HATCH ASSY HAS THREE (3) AREAS OF MINOR LEVEL 1 CORROSION ON EXTERIOR SKIN. AQRD ERO-895800 PROVIDES ENGINEERING FOR A PERMANENT MAJOR REPAIR IN ZONE 284 AT WL 154, WL 126, & WL 120.5.SDR DXTR2017051702Stinger · corrodedTAIL STINGER ASSY HAS SEVERAL AREAS OF MINOR LEVEL 1 CORROSION ON THE LH SIDE AT FS 718-725 ZONE 331. AQRD ERO-895673 PROVIDED ENGINEERING FOR A PERMANENT REPAIR.SDR DXTR2017051701Skin · corrodedSURFACE CORROSION FOUND ON LEFT HAND & RIGHT HAND NOSE SKINS ADJACENT TO THE FORWARD & AFT DOOR LATCHES FOR THE AVIONICS DOORS & ON THE AFT BAGGAGE DOOR SKIN DESCRIBED AS ZONES 213, 214, & 831. MEMO DQ8188 DATED 5/16/17 ADDRESSED MINOR CORROSION TO BE TREATEDSDR 2017F00073Fitting · corrodedCORROSION AT LOWER FITTING IN LEFT WING CENTER SPAR.SDR DXTA221701230660Circuit Board · failedDURING CLIMBOUT THRU 8000 FEET, WOW MISCOMPARE AMBER CAS MESSAGE ILLUMINATED. PERFORMED QRH CHECKLIST. ON GEAR EXTENSION, MESSAGE EXTINGUISHED, THEN CAME BACK ON SHORT FINAL. HAD NO NOSEWHEEL TILLER STEERING, ALL OTHER SYSTEMS NORMAL. DURING TAXI IN MESSAGE SDR DXTR2015030301Riser · bentUPPER FOLDING ENTRY DOOR STEP RISER BENT. R & R FOLDING ENTRY DOOR STEP IAW 52-10-02 MM.SDR DXTA2015021205976Unknown · odorWITH THE APU RUNNING & BLEED AIR TURNED ON, SMOKE WITH A BURNING ODOR IMMEDIATELY FILLED THE COCKPIT & CABIN. RAN LT & RT ENGS TO ISOLATE DISCREPANCY, NOTED NO ODOR OR SMOKE. RAN APU & TURNED BLEED AIR ON, NOTED SLIGHT ODOR BUT NO SMOKE. REMOVED APU ACCESS SDR CWQR20140625003Skin · damagedAIRCRAFT WAS IN MX TO TROUBLESHOOT A PITCH TRIM DISCREPANCY. THE TECHNICIAN WORKING THE PROBLEM NOTICED A DENT ON THE BOTTOM OTBD END OF RT ELEVATOR & TOUCHUP PAINT. REMOVED PAINT WITH PAINT STRIPPER FROM THE DENT AREA. FOUND A RUBBER SUBSTANCE UNDER PAINT SDR CWQR20130311020Heat Exchanger · crackedDURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 2 CRACKS ABOUT .30" LONG. A NEW HEAT EXCHANGER WAS INSTALLED. WE PREFORMED A LEAK CHECK ON THE DEFECSDR CWQR20130311019Heat Exchanger · crackedDURING A SCHEDULED INSPECTION, WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 4 CRACKS ABOUT .30" LONG. A NEW HEAT EXCHANGER WAS INSTALLED. WE PREFORMED A LEAK CHECK ON THE DEFSDR CWQR20130204007Heat Exchanger · crackedDURING A SCHEDULED INSPECTION, REPLACED A DUCT ASSY OFF OF THE HEAT EXCHANGER WITH AN IMPROVED DUCT ASSY. AT DISASSEMBLY, DISCOVERED THAT LT HEAT EXCHANGER HAD CRACKS FROM THE BOLT ATTACH POINTS. THE CRACKS WERE FROM .25 TO .75 IN LENGTH. IT APPEARS THE CRSDR DXTA2012070305026Control Valve · inoperativeAMBER CABIN ALTITUDE CAS MESSAGE ILLUMINATED AT APPROX 36,000 FT, FOLLOWED SHORTLY AFTER BY THE RED CABIN ALTITUDE CAS MESSAGE. PERFORMED PRESSURIZATION CONTROLLER BUILT-IN-TEST. NO DEFECTS NOTED. PERFORMED MANUAL PRESSURIZATION OF ACFT WITH APU. NO EXTERNSDR DXTA2012062505009Warning Message · illuminatedAMBER CABIN ALTITUDE CAS MESSAGE ILLUMINATED AT APPROX 36,000 FEET FOLLOWED SHORTLY THEREAFTER BY THE RED CABIN ALTITUDE CAS MESSAGE.SDR 2010F00128Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCSDR 2010F00127Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCSDR 2010F00126Diffuser · cracked((JGVR)) FOUND THESE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DSDR 2010F00125Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCSDR DXTA2010040804063Uplock · stickingLANDING GEAR INDICATED UNSAFE (RED LIGHT) DURING RETRACTION. ADDITIONALLY, A LOUD THUMPING NOISE WAS HEARD COMING FROM THE NOSE GEAR AREA. CHECKED NOSE STRUT SERVICING, FOUND WITHIN LIMITS. CHECKED UPLOCK SWITCHES FOR PROPER GROUNDS AT PCB'S, FOUND NORMAL. CHSDR DXTA2010011203943Packing · failedWHEN GEAR WAS SELECTED UP, ONLY THE NOSE GEAR CAME UP. TROUBLESHOT SYS AND FOUND NOSE STRUT NO FULLY EXTENDED W/ACFT ON JACKS. CK'D STRUT SERVICING AND FOUND NO PRESSURE IN LOWER CHAMBER. DISASSEMBLED LOWER PISTON FORK ASSY AND REPACKED IAW CMM 32-20-01. REASSDR DXTA2009112003865Line · leakingLOSS OF HYD CONTENT ON APPROACH TO LAND. AFTER LANDING GEAR WAS SELECTED DOWN. COMPLETED APPROIATE CHECKLIST AND LANDED ACFT USING EMERGENCY BRAKE TO STOP ON RUNWAY. HYD LEAK IN NOSE GEAR WELL. FOUND NOSE WHEEL STEERING UNIT CENTERING LINE RUPTURED AT UPPESDR DXTA2009102903831Actuator · inoperativeON DEPARTURE NOSE GEAR FAILED TO RETRACT. THE MAINS CAME UP FINE. FOUND NOSE WHEEL STEERING ACTUATOR TO BE FAULTY, REMOVED ACUATOR, AND REPLACED WITH A SERVICABLE NOSE GEAR STEERING ACUATOR. WORK DONE IAW THE MM 32-50-00. OPERATIONAL CHECKS, AND LEAK CHECKS SDR DXTA200802783Actuator · activatedON GEAR EXTENTION THE RT GEAR INDICATED NOT DOWN AND LOCKED. REMOVED AND INSTALLED A RENTAL ACTUATOR PER MM 32-30-40 AND OPERATIONAL CHECKED PER MM 32-00-00 GROUND OPERATIONAL CHECKED GOOD.SDR DXTA200702522Landing Gear · inoperativeAFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT LANDING GEAR. 10-29-07 ADJUSTED NOSE LANDING GEAR SQUAT SWITCH. OPS CHECKED GOOD. WORK DONE IAW 680 M.M. CHAPTER 32-60-00.
Back to N378QS, cancelled Jul 2, 2026