# N326QS: 1999 Cessna 560, registration cancelled 2013-09-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 18, 2013 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Cessna 560](https://openairdocs.org/model/cessna-560) (registry code 2076750) - Engine: [Pratt & Whitney Canada JT15D 5 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5-series) (registry code 52113) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (OpenAirDocs) - Serial number: 560-0526 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 19, 1999 - Certificate issued: September 5, 2012 - Last registry action: September 5, 2012 - Mode S code: A38609 - Owner when cancelled: [Ultra Holdings Corp](https://openairdocs.org/faa-owner/ULTRA%20HOLDINGS%20CORP) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N326QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=326QS - Page: https://openairdocs.org/deregistered/N326QS-2013-09-18 From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Cessna 560: https://openairdocs.org/model/cessna-560.md ## Service difficulty reports (16) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2012030904911](https://openairdocs.org/sdr/DXTA2012030904911), Mar 8, 2012: SQUAT SWITCH. OUT OF ADJUST. AFTER TAKEOFF, GEAR WOULD NOT RETRACT. UNABLE TO MOVE GEAR HANDLE. FOUND LT MAIN SQUAT SWITCH ON OUTER LIMITS OF ADJUSTMENT AND OUT OF RIG. ADJUSTED SQUAT SWITC - [SDR DXTA2011050204569](https://openairdocs.org/sdr/DXTA2011050204569), Apr 30, 2011: PITOT TUBE. OBSTRUCTED. ON TAKEOFF ROLL, ABORTED TAKEOFF FOR NO AIRSPEED INDICATION ON PILOTS PFD. REMOVED PILOT'S PITOT TUBE. REMOVED SAND FROM PITOT TUBE PURGED PITOT LINE FROM PILOT - [SDR DXTA2009022003516](https://openairdocs.org/sdr/DXTA2009022003516), Feb 19, 2009: BRAKE SYS. FAILED. POWER BRAKE FAILED WHILE TAXIING FOR TAKEOFF. - [SDR DXTA2009021903516](https://openairdocs.org/sdr/DXTA2009021903516), Feb 18, 2009: PRESSURE SWITCH. STICKING. FOUND THE 900-1300 PSI SWITCH STICKING. REMOVED SWITCH PN 1206P27, SN 3568 AND INSTALLED SWITCH PN 1206P27, SN 3751. PERFORMED COMPLETE BRAKE SYS BLEED. PERFORM - [SDR DXTA200808113223](https://openairdocs.org/sdr/DXTA200808113223), Aug 11, 2008: BRAKE ASSY. MALFUNCTIONED. AFTER LANDING, AT ABOUT 20 KNOTS THE BRAKES LOST ABOUT HALF THEIR CONTROL PRESSURE AND BRAKING EFFECTIVENESS IS QUESTIONABLE. LAST FOR ABOUT 1 SECOND AND BRAKES - [SDR DXTA20080811](https://openairdocs.org/sdr/DXTA20080811), Aug 11, 2008: BRAKE SYS. CONTAMINATED. AFTER LANDING, AT ABOUT 20 KNOTS THE BRAKES LOOSE ABOUT HALF THEIR CONTROL PRESSURE AND BRAKING EFFECTIVENESS IS QUESTIONABLE. LAST FOR ABOUT 1 SECOND AND BRAKE - [SDR DXTA200803223](https://openairdocs.org/sdr/DXTA200803223), Aug 11, 2008: BRAKE. WEAK. AFTER LANDING, AT ABOUT 20 KNOTS, THE BRAKES LOST ABOUT HALF THE CONTROL PRESSURE AND BRAKING EFFECTIVENESS. (S) - [SDR DXTA200803206](https://openairdocs.org/sdr/DXTA200803206), Jul 29, 2008: BRAKE ASSY. MALFUNCTIONED. EXCESSIVE AMOUNT OF BRAKE PEDAL APPLICATION IS NEEDED TO STOP AIRPLANE. INSP BRAKE SYSTEM FOR LEAKS. NO LEAK DETECTED AT THIS TIME. PERFORMED BRAKE BLEEDING PRO - [SDR DXTA200702460](https://openairdocs.org/sdr/DXTA200702460), Sep 9, 2007: STARTER GEN. TRIPPED. DURING TAKEOFF POWER APPLICATION, LT GENERATOR TRIPPED OFF LINE (LOW SPEED ABORT). VISUALLY INSPECTED LH GENERATOR WIRING. ALL CONNECTIONS TIGHT. RAN BOTH ENGIN - [SDR DXTA200601743](https://openairdocs.org/sdr/DXTA200601743), Nov 19, 2006: BRAKE ASSY. WEAK. SOFT BRAKE PEDALS ON BOTH SIDES. BLEED THE BRAKE SYSTEM AND INSTALLED NEW PACKINGS ON BLEED FITTING NAS1612-4. OPS OK. WORK DONE IAW CH 32-42-00 OF MM. LEAK CHE - [SDR DXTA200601587](https://openairdocs.org/sdr/DXTA200601587), Aug 29, 2006: WHEEL. DAMAGED. RT MAIN TIRE BLEW ON LANDING ROLLOUT. EVIDENCE OF WHEEL LOCK FROM TIRE DAMAGE. REMOVED WHEEL ASSY P/N 3-1490-1, S/N 3844 AND INSTALLED WHEEL ASSY P/N 3-1490-1, - [SDR DXTA200601296](https://openairdocs.org/sdr/DXTA200601296), Mar 14, 2006: BRAKE. MALFUNCTIONED. UPON LANDING APPLIED BRAKES AT APPROX, 90-100 KTS, BOTH BRAKE PEDALS ON CAPTAIN SIDE FELT HARD AND NO EFFECTIVE BRAKE ACTION FOR 3 SEC, THEN BRAKES FELT NORMAL - [SDR DXTA200500929](https://openairdocs.org/sdr/DXTA200500929), Aug 26, 2005: ENGINE. INOPERATIVE. DURING ENGINE START, THE RIGHT ENGINE HAD NORMAL START, LEFT ENGINE STARTED, ENGINE ACCELERATED THRU 52 PERCENT AND WOULD NOT SHUT OFF WITH THRUST LEVER IN CUT - [SDR DXTA200500563](https://openairdocs.org/sdr/DXTA200500563), Jan 26, 2005: BRAKE. MALFUNCTIONED. BRAKES WORKED NORMALLY AFTER LANDING, AS AIRCRAFT DECELERATED THROUGH APPROXIMATELY 20 KTS, THE BRAKES FAILED. BRAKE PRESSURE RECOVERED WHEN BRAKE PEDALS WERE P - [SDR DXTA200300162](https://openairdocs.org/sdr/DXTA200300162), Nov 16, 2003: CONTROL LEVER. LOOSE. RIGHT HAND THRUST REVERSER LEVER VERY LOOSE, DEPLOYED BY ITSELF DURING TAXI. INSPECTED ENGINE CONTROL AND THRUST REVERSER LEVER SPRING PLUNGER LOOSE, TIGHTEN RT - [SDR 99ZZZX4489](https://openairdocs.org/sdr/99ZZZX4489), Nov 17, 1999: WHEEL. MISMANUFACTURED. WHEEL WAS DISASSEMBLED FOR TIRE REPLACEMENT. DURING INSPECTION, FOUND THAT NO HOLES HAD BEEN DRILLED INTO WHEEL HALF INSIDE DIAMETER FOR THERMAL RELIEF. THERMAL ## Other aircraft with N326QS - [Registered now](https://openairdocs.org/aircraft/N326QS): Embraer Executive EMB-505, S/N 50500385, built 2016 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.