# N321CJ: 1992 Saab-Scania SAAB 340B, registration cancelled 2022-03-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 5, 2022
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Saab-Scania SAAB 340B](https://openairdocs.org/model/saab-scania-saab-340b) (registry code 7860101)
- Engine: [GE CT7-SER series](https://openairdocs.org/engine/ge-ct7-ser-series) (registry code 30031)
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (OpenAirDocs)
- Serial number: 340B321
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: November 16, 2018
- Last registry action: November 16, 2018
- Mode S code: A37242
- Owner when cancelled: [Worthington Aviation LLC](https://openairdocs.org/faa-owner/WORTHINGTON%20AVIATION%20LLC)
- Location: [Eagan, MN](https://openairdocs.org/faa-place/MN/Eagan)
- Owner type: LLC
- Owner's area on the map: 44.8459° N, 93.1596° W: Placed by OpenAirDocs at the center of ZIP code 55121, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N321CJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=321CJ
- Page: https://openairdocs.org/deregistered/N321CJ-2022-03-05

From the FAA registry file of October 29, 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 Saab-Scania SAAB 340B: https://openairdocs.org/model/saab-scania-saab-340b.md

## Service difficulty reports (26)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR NSVA2011146](https://openairdocs.org/sdr/NSVA2011146), Jun 22, 2011: PANEL. OPEN. ON ROTATION THE RT TOP COWLING PANEL ON THE ENGINE OPENED AND BEGAN FLAPPING/BENT. CREW REQUESTED TO RETURN TO AIRPORT / REDUCED SPEED TO 160 KTS AND RETURNED W
- [SDR NSVA2011076](https://openairdocs.org/sdr/NSVA2011076), Apr 6, 2011: CLEVIS BOLT. DEFECTIVE. REJECTED TAKEOFF IN CRW DUE TO NOSE WHEEL SHIMMY 65KTS, NORMAL BRAKING. MX REMOVED AND REPLACED CLEVIS BOLT, CREW PERFORMED HIGH SPEED TAXI, OPS CHECKED GOOD.
- [SDR NSVA2010209](https://openairdocs.org/sdr/NSVA2010209), Nov 15, 2010: PUMP. FAILED. HYDRAULIC PUMP FAILED IN FLIGHT, RETURNED TO FIELD. REPLACED HYDRAULIC PUMP, OPS CHECKED GOOD.
- [SDR NSVA2010186](https://openairdocs.org/sdr/NSVA2010186), Oct 14, 2010: SEAL. DAMAGED. LEFT MASTER CAUTION ILLUMINATED ON TAKEOFF BUT QUICKLY EXTINGUISHED. DURING EN ROUTE CLIMB THE LEFT ENGINE OIL PRESSURE STARTED TO FLUCTUATE 40-50 PSI INTO THE 
- [SDR NSVA2010175](https://openairdocs.org/sdr/NSVA2010175), Oct 4, 2010: LOOP. MALFUNCTIONED. RETURNED TO FIELD DUE TO ENGINE INTAKE LIGHT ILLUMINATED AFTER TAKEOFF. COULD NOT CONTINUE DO TO ICING CONDITIONS. REPLACED LT INTAKE LOOP AND REPLACED WHITE HA
- [SDR NSVA2010137](https://openairdocs.org/sdr/NSVA2010137), Aug 21, 2010: OIL SYSTEM. LOW. SHORTLY AFTER TAKEOFF THE LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED THEN QUICKLY EXTINGUISHED HOWEVER, THE LEFT ENGINE OIL PRESSURE GAGE BECAME ERRATIC BUT NEV
- [SDR NSVA201088](https://openairdocs.org/sdr/NSVA201088), May 31, 2010: PRESSURE GAUGE. DEFECTIVE. HIGH PITCH SOUND COMING FROM RT ENGINE DURING CLIMB. LT ENGINE OIL PRESSURE GAUGE FLUCTUATION, PROP OIL TEMP WENT TO ZERO AND HYDRAULIC QUANTITY INDICATOR READI
- [SDR NSVA201049](https://openairdocs.org/sdr/NSVA201049), Feb 20, 2010: SMOKE DETECTOR. INOPERATIVE. CARGO SMOKE LIGHT ILLUMINATED DURING RUN UPS AND WOULD NOT EXTINGUISH. CHECKED CARGO AREA VERIFIED NO FIRE OR FUMES. REMOVED AND REPLACED AFT SMOKE DETECTOR.
- [SDR NSVA2010018](https://openairdocs.org/sdr/NSVA2010018), Jan 21, 2010: SKIN. DAMAGED. ACFT REQUIRES MAJOR REPAIR FOR PERM REPAIR OF PUNCTURE DAMAGE TO RT FUSELAGE AT STA 360.25 IAW TD 340-53-09-85.
- [SDR NSVA2009040](https://openairdocs.org/sdr/NSVA2009040), Sep 9, 2009: PROPELLER. OUT OF BALANCE. LEFT AILERON WAS VIBRATING IN FLIGHT CAUSING A VIBRATION IN THE FLIGHT CONTROLS AND THE AIRFRAME. CHECKED AILERON CABLE TENSIONS IN BOTH WINGS IAW SAAB AMM 27-1
- [SDR NSVA2008002](https://openairdocs.org/sdr/NSVA2008002), Jan 29, 2008: WARNING LIGHT. FALSE ACTIVATION. RT MAIN BUSS LIGHT CAME ON DURING DESCENT, RIGHT ESS BUSS LIGHT ON DURING DESCENT. RESET CB (5-I), RAN ENGINES OPS CHECK GOOD PER MM 24-52-00 AND 24-50-00 VERIF
- [SDR NSVA20070248](https://openairdocs.org/sdr/NSVA20070248), Dec 6, 2007: BRAKE ASSY. MALFUNCTIONED. AFTER LANDING ON RW31 LGA, WHILE TAXIING ON ALPHA TO RAMP WAS TOLD TO HOLD SHORT, WHEN PUSHED ON BRAKES THERE WAS NO RESPONSE. HYDRO PRESSURE CHECKED OK, PUT PO
- [SDR NSVA20070243](https://openairdocs.org/sdr/NSVA20070243), Nov 19, 2007: BRAKE. INOPERATIVE. BRAKES INOP DURING TAXI. REMOVED AND REPLACED NR 4 BRAKE ASSY.
- [SDR NSVA20070186](https://openairdocs.org/sdr/NSVA20070186), Jul 15, 2007: POWER SUPPLY. MALFUNCTIONED. DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK 3 COVE EMERGENCY LIGHTS WERE FOUND NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY LIGHT
- [SDR NSVA20070147](https://openairdocs.org/sdr/NSVA20070147), Jun 1, 2007: INDICATOR. MALFUNCTIONED. LEFT ENGINE ITT RED LINED ON TAKE OFF AND DIGITAL PORTION OF GAUGE WENT BLANK. REMOVED AND REPLACED LT ENG ITT GAUGE IAW AMM 77-20-05. OPS GOOD P/N ON/OFF 10227
- [SDR NSVA20070117](https://openairdocs.org/sdr/NSVA20070117), Apr 26, 2007: POWER SUPPLY. READS LOW. DC EMERGENCY BUSS POWER SUPPLY VOLTAGES APPEAR LOW. TESTED EMERGENCY BATTERY VOLTAGE IAW SAAB AMM 24-35-00, OPS CHECK GOOD EMERGENCY PWR LIGHTS. 
- [SDR NSVA20070105](https://openairdocs.org/sdr/NSVA20070105), Apr 17, 2007: INDICATOR. DAMAGED. RT ENG ITT DIGITAL APPEARED TO READ 947 DURING TAKEOFF. CREW COLD NOT VERIFY IF ANALOG READING SAME. AFTER ABORT FOUND DIGITAL SEGMENT TO BE MISSING. REMOVED AN
- [SDR NSVA20070056](https://openairdocs.org/sdr/NSVA20070056), Mar 8, 2007: CONTROL PANEL. MALFUNCTIONED. LT ENG CAME OFF CTOT/APR ON TAKEOFF, TORQUE FELL FROM 85 PERCENT TO 40 PERCENT. REMOVED AND REPLACED CTOT CONTROL PANEL IAW SAAB AMM 76-10-50-04. OPS CHECK GOOD
- [SDR NSVA20070045](https://openairdocs.org/sdr/NSVA20070045), Feb 23, 2007: SMOKE DETECTOR. DIRTY. AVIONICS SMOKE ANNUNCIATOR BRIEFLY ILLUMINATED. CK CONNECTOR ON BACK OF SMOKE DETECTOR, FOUND TO BE TIGHT CLEAN . REINSTALLED PLUG LAMP CK OK AT THIS IME PER 26
- [SDR NSVA20070015](https://openairdocs.org/sdr/NSVA20070015), Jan 20, 2007: AUTOCOARSEN SYS. MALFUNCTIONED. AUTOCOARSEN LIGHT DID NOT ILLUMINATE WHEN TURNED ON. RESET ALL C/B'S IN SYS ROW ENG'S CHECKED SYS IAW 61-22-00, OP CHECKED NORMAL ON GROUND.
- [SDR 01252006C](https://openairdocs.org/sdr/01252006C), Jan 19, 2006: PANEL. INOPERATIVE. RT APR DID NOT ENGAGE ON T/O ROLL. REMOVED AND REPLACED CTOT PANEL IAW 76-10-50. PN ON/OFF 7239060-503, SN ON 0296, SN OFF 0393. PERFORMED OPERATIONAL CHECK OF 
- [SDR 11182005A](https://openairdocs.org/sdr/11182005A), Nov 17, 2005: B-NUT. LOOSE. ON TAKEOFF ROLL, AUTOCOARSEN HIGH LIGHT DID NOT ILLUMINATE WITH TORQUE SET TO 80%. REPLACED AUTOCOARSEN COMPUTER FOR TROUBLESHOOTING AND DID NOT CORRECT THE PRO
- [SDR 09212005F](https://openairdocs.org/sdr/09212005F), Sep 20, 2005: HMU. MALFUNCTIONED. LEFT ENGINE WILL NOT SHUT DOWN, HAD TO PULL T-HANDLE TO SHUT DOWN. RIGGED CONDITION LEVER INPUT TO HMU GEAR BOX AND THE PCU.
- [SDR 09192005C](https://openairdocs.org/sdr/09192005C), Sep 18, 2005: PROPELLER. MALFUNCTIONED. LT PROP WILL NOT COME OUT OF FEATHER, MEL'ED.
- [SDR 09092005B](https://openairdocs.org/sdr/09092005B), Sep 7, 2005: INDICATOR. MALFUNCTIONED. LT TORQUE GAUGE INDICATED AN ADDITIONAL 7 PERCENT ON T/O WITH APR ENGAGED. MEL'ED SYSTEM.
- [SDR 08302005B](https://openairdocs.org/sdr/08302005B), Aug 25, 2005: CONTROL UNIT. MALFUNCTIONED. RT ENGINE TORQUE FLUX. REMOVED AND REPLACED DECU. OPS CHECK GOOD.

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