# N193CJ: 1990 Saab-Scania SAAB 340B, registration cancelled 2019-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 2019
- Status when cancelled: Valid registration
- 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: 340B-193
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 6, 1990
- Certificate issued: January 19, 2018
- Last registry action: April 15, 2019
- Mode S code: A1738B
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N193CJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=193CJ
- Page: https://openairdocs.org/deregistered/N193CJ-2019-07-30

From the FAA registry file of November 5, 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 (33)

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

- [SDR NSVA20120613554](https://openairdocs.org/sdr/NSVA20120613554), Jun 13, 2012: ENGINE. VIBRATION. DURING EN ROUTE CLIMB, THE CREW FELT SEVERE VIBRATION COMING FROM THE NR 2 ENGINE. THE CREW FOLLOWED UNUSUAL ENGINE VIBRATION PROCEDURES, SHUTDOWN ENGINE, DECLA
- [SDR NSVA20120427525](https://openairdocs.org/sdr/NSVA20120427525), Apr 27, 2012: HANDLE. BROKEN. DURING TAXI FOR TAKEOFF THE CREW REPORTED THE PARKING BRAKE HANDLE BROKEN OFF. RETURNED TO GATE FOR MX. MX FERRIED A/C.
- [SDR NSVA20120208444](https://openairdocs.org/sdr/NSVA20120208444), Feb 2, 2012: UNKNOWN. MALFUNCTIONED. FLIGHT 5006 MLU-IAH ON AIRCRAFT 193CJ HAD LEFT ENGINE OIL TEMPERATURE HIGH WHEN ON DESCENT INTO IAH. FLIGHT LANDED WITHOUT INCIDENT. CREW DID DECLARE EMERGENCY 
- [SDR NSVA2011323](https://openairdocs.org/sdr/NSVA2011323), Dec 3, 2011: UNKNOWN. MALFUNCTIONED. FLIGHT 4996 CLL IAH AC 193 ABORTED TAKEOFF FOR LT OIL PRESSURE, 0 PASSENGERS ON BOARD RUNWAY 16, REJECTED TAKEOFF AT 90 KNOTS.
- [SDR NSVA2011294](https://openairdocs.org/sdr/NSVA2011294), Nov 11, 2011: WARNING SYSTEM. ACTIVATED. FLIGHT 4975 LCH IAH AC 193CJ ABORTED TAKEOFF AND RETURNED TO GATE FOR LEFT ENGINE OIL PRESSURE LIGHT. HI SPEED ABORTED TAKEOFF AT 90 KNOTS.
- [SDR NSVA2011225](https://openairdocs.org/sdr/NSVA2011225), Sep 1, 2011: SPAR. CRACKED. RT WING AFT LOWER FAIRING SPAR IS CRACKED AT WS 202. REFERENCE CONTROL # 193-12. LT HORIZONTAL STAB HAS 154 DENTS NOT ON FILE OR ENTERED INTO THE DAMAGE LOG. RE
- [SDR NSVA2011223](https://openairdocs.org/sdr/NSVA2011223), Sep 1, 2011: STRUCTURE. CORRODED. LT AND RT FLIGHT DECK FLOORS HAD NUMEROUS AREAS OF CORROSION. REPAIRED IAW TD340-51-11-21.
- [SDR NSVA2011220](https://openairdocs.org/sdr/NSVA2011220), Sep 1, 2011: FRAME. CORRODED. TOP FLANGE OF FRAME AT STATION 294.0 CORRODED. COMPLETED REPAIR IAW TD340-53-11-09. COMPLETED JC 51-00-00S.
- [SDR NSVA2011218](https://openairdocs.org/sdr/NSVA2011218), Sep 1, 2011: PANEL. CORRODED. RT CABIN SIDE PANEL ABOVE THE WINDOW DOUBLER BELT CORROSION: AREA 1 TO 3, BLENDED AND ACCEPTED. AREA 4 TO 7 DOUBLER/ TRIPLER REPAIR. LT CABIN SIDE PANEL ABOVE T
- [SDR NSVA2011217](https://openairdocs.org/sdr/NSVA2011217), Sep 1, 2011: PANEL. CORRODED. RT CABIN SIDE PANEL ABOVE THE WINDOW DOUBLER BELT CORROSION: AREA 1 TO 3, BLENDED AND ACCEPTED. AREA 4 TO 7 DOUBLE/ TRIPLER REPAIR. LT CABIN SIDE PANEL ABOVE TH
- [SDR NSVA2011213](https://openairdocs.org/sdr/NSVA2011213), Sep 1, 2011: SKIN. DAMAGED. COMPLETED TD 340-51-11-24 AND JC 51-00-00S. RT AILERON HAS THREE DENTS IN LOWER SKIN.
- [SDR NSVA2011211](https://openairdocs.org/sdr/NSVA2011211), Sep 1, 2011: ATTACH FITTING. CRACKED. OUTBOARD HINGE ATTACH FITTING ON RT FLAP IN FLAP FAIRING AT WS 123 IS CRACKED AT TRAILING EDGE. REQUIRES INSTALLATION OF MOD KIT P/N: 340-57-038-02. REFERENCE C
- [SDR NSVA2011210](https://openairdocs.org/sdr/NSVA2011210), Sep 1, 2011: FRAME. DAMAGED. COMPLIED WITH COLGAN TD 340-51-11-21. RT NACELLE FRAME AT STA 197 HAS MISSING MATERIAL ON O/B SIDE MIDDLE SECTION FROM CHAFING ON INLET.
- [SDR NSVA2011209](https://openairdocs.org/sdr/NSVA2011209), Sep 1, 2011: STRUCTURE. DAMAGED. COMPLIED WITH COLGAN TD 340-54-11-10. REPAIR MISC RIVET DEVIATION ON RT I/B NACELLE.
- [SDR NSVA2011092](https://openairdocs.org/sdr/NSVA2011092), Apr 19, 2011: SMOKE DETECTOR. FALSE ACTIVATION. WHILE TAXIING FOR TAKEOFF, PILOT REPORTED THAT AVIONICS SMOKE LIGHT ILLUMINATED FOR 2 SECONDS. SPOKE TO 9L MX AND RETURNED BACK TO GATE. PLACED ON MEL. THEN REP
- [SDR NSVA2011070](https://openairdocs.org/sdr/NSVA2011070), Apr 3, 2011: ENGINE. DEFECTIVE. ON CLIMBOUT (ABOUT 400 FT) RIGHT ENGINE OVERTEMP LIGHT CAME ON AND ITT EXCEEDED 980 DEG C WHILE THE TORQUE DROPPED OFF TO ABOUT 60 PERCENT CTOT WAS DIALED BACK 
- [SDR NSVA2011068](https://openairdocs.org/sdr/NSVA2011068), Mar 24, 2011: UNKNOWN. ODOR. WRITE UP STATES "WITH RIGHT AC PACKS ON, FLIGHT CREW COULD SMELL A BURNING ODOR IN FLIGHT DECK. PERFORMED OPS CHECK OF FLIGHT DECK AC PACK, NO ODOR OR FAULT FOU
- [SDR NSVA2011024](https://openairdocs.org/sdr/NSVA2011024), Feb 10, 2011: SMOKE DETECTOR. FAULTY. AVIONICS SMOKE LIGHT ILLUMINATED ON APPROACH, CREW DECLARED AN EMERGENCY AND DID NORMAL LANDING. CREW DEPLANED AIRCRAFT AND CONTACTED MX. NO VISIBLE SMOKE, OR S
- [SDR NSVA2010154](https://openairdocs.org/sdr/NSVA2010154), Sep 3, 2010: WINDSHIELD WIPER. OUT OF ADJUST. BIRD STRIKE AT ROTATION SPEED. BIRD HIT F/O WINDSCREEN AND WINDSHIELD WIPER. WIPER MALFUNCTION. INSPECTED NO DAMAGE FOUND. FOUND WINDSHIELD WIPER OUT OF ADJUSTM
- [SDR NSVA2010115](https://openairdocs.org/sdr/NSVA2010115), Jul 7, 2010: OIL SYSTEM. LOW. ABORTED TAKEOFF FOR RIGHT ENGINE OIL PRESSURE WARNING LIGHT. SERVICED ENGINE OIL, OIL LIGHT DID NOT RETURN.
- [SDR NSVA201079](https://openairdocs.org/sdr/NSVA201079), Apr 20, 2010: SKIN. DAMAGED. MAJOR REPAIR OF LT NACELLE INBOARD SKIN REPAIR DOUBLER AT STA 203 IAW TD 340-54-10-05.
- [SDR NSV2008F00023](https://openairdocs.org/sdr/NSV2008F00023), Sep 3, 2008: STRUCTURE. VIBRATION. AIRPLANE SHAKES DURING CLIMBOUT AT SLOW SPEED AND DURING APPROACH. CAPTAINS CONTROL COLUMN SHAKES. MOVES APPROXIMATELY 3 INCHES. VIBRATION DIMINISHES SOME IN CR
- [SDR NSVA20070255](https://openairdocs.org/sdr/NSVA20070255), Jan 15, 2008: UNKNOWN. ODOR. DCP FLAGS ON CA SIDE EFIS TUBES WITH ELECTRICAL ODOR IN FLIGHT DECK DURING LANDING. INSPECTED CAPS SIDE EFIS AND SURROUNDING EQUIPMENT COULD NOT GET EFIS TO FAU
- [SDR NSVA20070096](https://openairdocs.org/sdr/NSVA20070096), Apr 11, 2007: STOP. INTERMITTENT. FI IDLE STOP LT INTERMITTENT. PERFORMED ADJUSTMENT TEST OF THE FLIGHT IDLE STEP SYSTEM IAW SAAB 340 AMM 76-10-60. OPERATIONAL TEST PASSED.
- [SDR NSVA20070041](https://openairdocs.org/sdr/NSVA20070041), Feb 18, 2007: PUMP. INTERMITTENT. HYDRAULIC LIGHT CAME ON ON TAXI INOP IN AUTO AND MANUAL MODE THEN WORKED LATER. HYD PUMP WAS FOUND TO WORK INTERMITTENTLY AND OPERATION WAS WEAK. REMOVED AND RE
- [SDR NSVA20070040](https://openairdocs.org/sdr/NSVA20070040), Feb 15, 2007: ACTUATOR. MALFUNCTIONED. FOUND FLAPS FAILED TO RETRACT UNLESS HYD PUMP IS IN OVERRIDE. REMOVED AND REPLACED RT FINE ACTUATOR BLEED HYDS SYSTEM AND OPS CHECK GOOD IAW 27-51-25-04 PN TP10
- [SDR NSVA20070038](https://openairdocs.org/sdr/NSVA20070038), Feb 14, 2007: CONTROL VALVE. MALFUNCTIONED. FLAPS WOULD NOT EXTEND ON APPROACH. NO WARNINGS AURAL OR VISUAL. FLAPS TAKE 10 SECONDS TO EXTEND WHEN ACTUATED WITH HANDLE. TESTED IAW AMM 27-51-00-05 AND OPERA
- [SDR NSVA200600227](https://openairdocs.org/sdr/NSVA200600227), Dec 11, 2006: GENERATOR. LEAKING. PAX NOTICED SMOKE FROM LT ENG I/B SIDE. FOUND OIL COMING FROM DC GENERATOR EXHAUST WAS GOING INTO COWLING SCOOP OF PRECOOLER CLEANED OFF RESIDUAL FROM COWLING A
- [SDR NSVA200600224](https://openairdocs.org/sdr/NSVA200600224), Dec 7, 2006: LAMP. INOPERATIVE. FOUND EMERGENCY LIGHT ARM LIGHT ON FLIGHT ATT PANEL INOP. RELAMPED F/A EMERG ARMED LIGHT.
- [SDR NSVA200600100](https://openairdocs.org/sdr/NSVA200600100), Jul 10, 2006: SMOKE DETECTOR. INOPERATIVE. WHILE STARTING NR 2 ENGINE, CARGO SMOKE LIGHT COMES ON. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR PN ON/OFF CGAB1201-01, SN OFF 537, SN ON 630 OPS CHECK GOO
- [SDR 03152006D](https://openairdocs.org/sdr/03152006D), Mar 13, 2006: OIL SYSTEM. LOW. DURING TAKEOFF ROLL AT 110 KIAS, MASTER WARNING ON RT ENGINE OIL PRESSURE (CWP) CENTRAL WARNING PANEL LIGHT ILLUMINATED. SERVICED RT ENGINE WITH 3 QUARTS OF OIL
- [SDR 03082006A](https://openairdocs.org/sdr/03082006A), Mar 3, 2006: OIL SYSTEM. LOW. RT ENGINE OIL PRESSURE LIGHT ILLUMINATED ON T/O ROLL. ADDED 3 QUARTS OF OIL AND C/W CLEARING PROCEDURE, PER GE MM 72-00-00 OPS CHECK C/W.
- [SDR 01242006D](https://openairdocs.org/sdr/01242006D), Jan 21, 2006: PUMP. INOPERATIVE. ON SHORT FINAL TO LAND HYDRAULIC LIGHT ILLUMINATED WHEN LANDING GEAR WAS SELECTED DOWN. PERFORMED HYDR LIGHT ON ABNORMAL CHECK LIST. 3 GREEN LANDING GEAR WAS AC

## Other aircraft with N193CJ

- [Cancelled 1998-01-27](https://openairdocs.org/deregistered/N193CJ-1998-01-27): Cessna 525, S/N 5250193. Exported to Germany. Owner: [Joda Partnership](https://openairdocs.org/faa-owner/JODA%20PARTNERSHIP), [Chesterfield, MO](https://openairdocs.org/faa-place/MO/Chesterfield)

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