# N202SR: Saab-Scania SAAB 340B, registration cancelled 2020-12-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 14, 2020
- 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-202
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 13, 1990
- Certificate issued: January 17, 2018
- Last registry action: November 13, 2020
- Mode S code: A19B11
- 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/N202SR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=202SR
- Page: https://openairdocs.org/deregistered/N202SR-2020-12-14

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 (49)

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

- [SDR NSVA2011385](https://openairdocs.org/sdr/NSVA2011385), Dec 30, 2011: TAIL CONE. MISREPAIRED. DOUBLER REPAIR TO UPPER LT TAIL CONE SKIN AT STA 793 IS NOT IN DAMAGE LOG OR ON FILE. THE RIVET PATTERN AROUND THE CUTOUT IS IRREGULAR AND DOES NOT HAVE A DOUBL
- [SDR NSVA2011382](https://openairdocs.org/sdr/NSVA2011382), Dec 29, 2011: TAIL CONE. MISREPAIRED. DOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD.
- [SDR NSVA2011378](https://openairdocs.org/sdr/NSVA2011378), Dec 29, 2011: TAIL CONE. MISREPAIRED. DOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD.
- [SDR NSVA2011375](https://openairdocs.org/sdr/NSVA2011375), Dec 29, 2011: CARGO TRACK. MISREPAIRED. PREVIOUS CARGO SEAT RAIL SPLICE LBL 18 FUSE STA 621 TO 687 NOT IN DAMAGE LOG, U-BEAM SPLICE DOES NOT HAVE SUFFICIENT NAS 1580 BOLT COUNT AND INCORRECT FASTENERS
- [SDR NSVA2011384](https://openairdocs.org/sdr/NSVA2011384), Dec 28, 2011: STRUCTURE. DAMAGED. FWD RT FWD O/B ATTACH HOLE ELONGATED. CONTROL# 202-67 REFERENCE TD. 340-54-11-37 DATED 12/13/.
- [SDR NSVA2011366](https://openairdocs.org/sdr/NSVA2011366), Dec 28, 2011: RIVET. DAMAGED. PREVIOUS DOUBLER/TRIPLER REPAIR TO RT FUSELAGE AT STA 339 TO 363, SL1615 TO 1617 HAS ONE RIVET THAT IS MISSING THE SHOP HEAD. REFER TO SAAB STATEMENT SDS 023471
- [SDR NSVA2011367](https://openairdocs.org/sdr/NSVA2011367), Dec 27, 2011: FRAME. CORRODED. THE AFT UPPER FLANGE ON THE BOTTOM FRAME AT ATA 258 HAS PREVIOUS REPAIR NOT IN DAMAGE LOG OR ON FILE. BOTH FORWARD AND AFT UPPER FLANGES HAVE SEVERE CORROSION F
- [SDR NSVA2011363](https://openairdocs.org/sdr/NSVA2011363), Dec 26, 2011: SKIN. CORRODED. CORROSION ON RT FUSELAGE SKIN JUST ABOVE WINDOW DOUBLER EDGE AT SL1607 FROM STA 583 TO 595.5 REFER TO SAAB STATEMENT 340SDS023472 PARA 1, DATED 12-16-2011, TD 3
- [SDR NSVA2011362](https://openairdocs.org/sdr/NSVA2011362), Dec 26, 2011: SKIN. CORRODED. CORROSION ON RT FUSELAGE SKIN JUST ABOVE WINDOW DOUBLER EDGE AT SL1607 FROM STA 565.5 TO 621.5 REFER TO SAAB STATEMENT 340SDS023472 PARA 1 DATED 12-16-2011, TD 
- [SDR NSVA2011361](https://openairdocs.org/sdr/NSVA2011361), Dec 26, 2011: FRAME. CRACKED. FUSELAGE BOTTOM FRAME AT STA 294 HAS MODERATE TO SEVERE CORROSION FROM LBL 25 TO RBL 10.5 AND A CRACK AT RBL 19.5. REFER TO SAAB STATEMENT 340SDS023466 DATED 12
- [SDR NSVA2011358](https://openairdocs.org/sdr/NSVA2011358), Dec 26, 2011: SKIN. CORRODED. FUSELAGE SKIN UNDER RT ICE SHIELD NR 8 HAS 15 SMALL AREAS OF PITTING CORROSION AND 1 SMALL AREA OF PITTING CORROSION UNDER ICE SHIELD NR 7. REFER TO SAAB STATEM
- [SDR NSVA2011355](https://openairdocs.org/sdr/NSVA2011355), Dec 23, 2011: STRUCTURE. CRACKED. THE COCKPIT FLOOR IS CORRODED AND OR CRACKED UNDER THE TWO SNAPS LOCATED OB OF THE AFT OB CORNER OF THE RT CONTROL COLUMN AND JUST AFT OF STA 186. REFERENCE TD 
- [SDR NSVA2011354](https://openairdocs.org/sdr/NSVA2011354), Dec 23, 2011: ANGLE. CORRODED. FLIGHT DECK ENTRANCE RISER AND THE ATTACHED FLOORBOARD MOUNT ANGLE AT STA 225 HAVE SEVERE CORROSION. REFERENCE TD 340-53-11-95 DATED 12-22-11 AND MM409#407174 U
- [SDR NSVA2011349](https://openairdocs.org/sdr/NSVA2011349), Dec 23, 2011: STRUCTURE. CORRODED. LT COCKPIT FLOOR CORROSION AT AND UNDER PREVIOUS DOUBLER REPAIRS AND SNAP FASTENERS IB, OB AND FORWARD OF CONTROL COLUMN. (REF ITEMS 1 THROUGH 5 & 7 THROUGH 9 O
- [SDR NSVA2011347](https://openairdocs.org/sdr/NSVA2011347), Dec 23, 2011: STRUCTURE. DAMAGED. CARGO FLOOR FRAME AT STA 694 IS KINKED FROM LBL 8.75 TO LBL 17. REF TO TD 340-53-11-92 AND MM409#407231 FOR REPAIR DETAILS UNDER CONTROL #202-14.
- [SDR NSVA20111223346](https://openairdocs.org/sdr/NSVA20111223346), Dec 23, 2011: FLOORBEAM. MISREPAIRED. CARGO FLOORBEAM AT BS 694 IS KINKED FROM LBL 8.75 TO LBL 17. PREVIOUS REPAIRS NOT IN DAMAGE LOG OR ON FILE. BOTH REPAIRS ARE MISSING THE REINFORCEMENT ANGLES AN
- [SDR NSVA2011372](https://openairdocs.org/sdr/NSVA2011372), Dec 22, 2011: RIVET. CORRODED. RT COCKPIT FLOOR HAS MULTIPLE CORRODED RIVETS, 3 PREVIOUS REPAIRS FORWARD OF STA 186 ARE NOT IN DAMAGE LOG. THE O/B MOST REPAIR DOES NOT TIE INTO THE RIVET ROW 
- [SDR NSVA20111222370](https://openairdocs.org/sdr/NSVA20111222370), Dec 22, 2011: FLOOR SKIN. CORRODED. RIGHT COCKPIT FLOOR HAS MULTIPLE CORRODED RIVETS. REPAIRED.
- [SDR NSVA2011353](https://openairdocs.org/sdr/NSVA2011353), Dec 22, 2011: SEAT TRACK. CORRODED. CONTROL # 202-61: LT FWD SEAT RAIL AT LBL 18.3 FROM STA 297-352 CORRODED. COMPLETED SEAT RAIL SPLICE REPAIR IAW TD 340-53-11-59.
- [SDR NSVA2011352](https://openairdocs.org/sdr/NSVA2011352), Dec 22, 2011: FRAME. DAMAGED. CONTROL # 202-17: FRAME STATION 339 GOUGED AND KINKED. COMPLETED REPAIR IAW TD 340-53-11-09.
- [SDR NSVA2011350](https://openairdocs.org/sdr/NSVA2011350), Dec 22, 2011: STRUCTURE. CORRODED. LT COCKPIT FLOOR CORROSION UNDER SNAP FASTENERS AFT AND OB OF CONTROL COLUMN. (REF ITEM 10 OF CA-M268 FOR CONTROL #202-11) REFERENCE TD 340-53-11-27 AND MM409#4
- [SDR NSVA2011348](https://openairdocs.org/sdr/NSVA2011348), Dec 22, 2011: ANGLE. CORRODED. FLIGHT DECK ENTRANCE RISER AND THE ATTACHED FORWARD FLOORBOARD MOUNT ANGLE AT STA 225 HAVE SEVERE CORROSION REFERENCE TD 340-53-11-95 409#407174 CONTROL #202-29
- [SDR NSVA2011343](https://openairdocs.org/sdr/NSVA2011343), Dec 22, 2011: RIB. CRACKED. UPPER AND LOWER ENDS OF I/B AND O/B CLOSING RIBS ON RT WING I/B LEADING EDGE 611AR ARE CRACKED. REF TD 400-57-11-17 AND MM409# 100232 FOR REPAIR DETAILS. CONTRO
- [SDR NSVA2011340](https://openairdocs.org/sdr/NSVA2011340), Dec 21, 2011: CARGO TRACK. DAMAGED. CARGO SEAT TRACK AT BL 0 WAS REPLACED FROM STA 631.5 TO 686.888. THIS REPAIR APPEARS TO CONFORM TO THE PRINCIPLES OF TD 340-53-11-59. REF TD 340-53-11-59 DATED 
- [SDR NSVA2011335](https://openairdocs.org/sdr/NSVA2011335), Dec 19, 2011: STRUCTURE. CHAFED. CONTROL # 202-50: RT ENGINE INLET COMPARTMENT CHAFED IN CENTER DECK AREA. COMPLETED REPAIR IAW TD 340-54-11-02.
- [SDR NSVA2011331](https://openairdocs.org/sdr/NSVA2011331), Dec 14, 2011: RIVET. MISSING. WATER SERVICE RELOCATION MOD DOUBLER NOT ENTERED INTO DAMAGE LOG. DOUBLER IS LOCATED FROM STA 248 TO 262, BETWEEN SL1622 AND SL1636. 1.5" ABOVE SKIN SPLICE AT S
- [SDR NSVA2011106](https://openairdocs.org/sdr/NSVA2011106), May 10, 2011: OIL SYSTEM. LOW. CREW RECEIVED RT ENG OIL PRESSURE MASTER WARNING DURING INITIAL CLIMB. ALL RT ENG INDICATIONS WERE NORMAL EXCEPT ENG OIL PRESSURE WHICH WAS FLUCTUATING FROM 50 
- [SDR NSVA2011072](https://openairdocs.org/sdr/NSVA2011072), Apr 4, 2011: STRUT. LOW PRESSURE. AFTER TAKEOFF, CREW COULD NOT RAISE THE LANDING GEAR. THE AIRCRAFT RETURNED TO BGM AND LANDED SAFELY WITHOUT FURTHER INCIDENT. CREW CONFIRMED THAT GEAR PIN WAS 
- [SDR NSVA2011016](https://openairdocs.org/sdr/NSVA2011016), Feb 1, 2011: AUTOPILOT SYS. MALFUNCTIONED. RETURNED TO GATE DUE TO PRE TAKEOFF FLIGHT CHECKS CREW FELT A BINDING IN THE YOKE. FOUND TO BE AUTO PILOT, MEL'D AUTO PILOT.
- [SDR NSVA201085](https://openairdocs.org/sdr/NSVA201085), May 27, 2010: BATTERY PACK. DISCHARGED. FLOOR PROXIMITY ESCAPE PATH LIGHTS ARE DIM AT SEATS 5D AND 6D AND OVERHEAD EMERGENCY LIGHT IS DIM AT SEAT 6A. REMOVED AND REPLACED NR 3 EMERGENCY POWER SUPPLY B
- [SDR NSV2008F00022](https://openairdocs.org/sdr/NSV2008F00022), Aug 27, 2008: SMOKE DETECTOR. FALSE INDICATION. AVIONICS SMOKE LIGHT ILLUMINATED. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR (PN 72-111211-000) SN A4091, SN ON A5414, DONE IAW 26-13-06-04, OPS CHECK GOOD. (
- [SDR NSV2008F00018](https://openairdocs.org/sdr/NSV2008F00018), Aug 10, 2008: CONNECTOR. UNKNOWN. AVIONICS SMOKE LIGHT CAME ON INFLIGHT FOR A FEW SECONDS. RESET CONNECTOR TO SMOKE DETECTOR IAW SAAB AMM 28-13-00. OPS CHECKED GOOD. (S)
- [SDR NSV2008F00017](https://openairdocs.org/sdr/NSV2008F00017), Aug 7, 2008: POWER SUPPLY. DISCHARGED. MAIN EMERGENCY LIGHTS IN CABIN OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT SEAT 5A CWC 33-50-026. OPS CHECK GOOD. P/N ON/OFF 60-1321-1, S/N: OFF 17486, 
- [SDR NSV2008F00015](https://openairdocs.org/sdr/NSV2008F00015), Aug 5, 2008: CONNECTOR. CONTAMINATED. TAIL PIPE HOT LIGHT (RT) CAME ON AFTER TAKEOFF THEN WENT OUT AND STAYED OUT. CLEANED CONNECTORS AT DISCONNECTS WITH CONTACT CLEANER TO REMOVE MOISTURE, PERFORME
- [SDR NSV2008F00012](https://openairdocs.org/sdr/NSV2008F00012), Jul 24, 2008: COWLING. DAMAGED. LT ENGINE INBOARD COWLING DAMAGED. REMOVED AND REPLACED LT INBOARD COWLING IAW SAAB MM 71-10-05-08. (A)
- [SDR NSVA20070230](https://openairdocs.org/sdr/NSVA20070230), Sep 18, 2007: SMOKE DETECTOR. LOOSE. CARGO COMPARTMENT SMOKE DETECTION SYSTEM DOES NOT TEST. FOUND SMOKE DETECTOR LOOSE RESECURED, OPS CHECK GOOD.
- [SDR NSVA20070219](https://openairdocs.org/sdr/NSVA20070219), Aug 27, 2007: COOLING FAN. FAILED. AVIONICS VENT FAN LIGHT ILLUMINATED AND CB G-11 POPPED ACCOMPANIED BY HOT ELECTRICAL ODOR. AVIONICS VENT FAN MEL'D, WILL BE REPLACED AT NEXT MAINTENANCE BASE VI
- [SDR NSVA20070110](https://openairdocs.org/sdr/NSVA20070110), Apr 23, 2007: SWITCH. MALFUNCTIONED. GUST LOCK LIGHT ON DURING FLIGHT CONTROL CHECK. REINSTALLED RUDDER GUST LOCK ACTUATOR IAW SAAB 340 AMM 27-72-10-04, OPS CHECK GOOD TS IAW AMM 72-27-00-00. FOUND
- [SDR NSVA20070088](https://openairdocs.org/sdr/NSVA20070088), Apr 6, 2007: SWITCH. MALFUNCTIONED. GUST LOCK LIGHT ILLUMINATED WHEN GUST LOCK IS RELEASED. TS TO QUADRANT GUST LOCK SWITCH QUADRANT REMOVED AND REPLACED IAW 76-10-05-09 OPS AND RIGGING KS STILL N
- [SDR NSVA20070039](https://openairdocs.org/sdr/NSVA20070039), Feb 14, 2007: CONTROL QUADRANT. UNKNOWN. CONFIG WARNING ON TAKEOFF ROLL. VERIFIED POWER TO RELAY 8 GA W PINX1. VERIFIED GROUND TO RELAY AT 8GA PIN X2.5. VERIFIED GROUNDS FROM RELAY 8GA PINS D1 AND A2. 
- [SDR NSVA20070004](https://openairdocs.org/sdr/NSVA20070004), Jan 7, 2007: SMOKE DETECTOR. NO TEST. FOUND CARGO SMOKE TEST FAILED. REMOVED AND REPLACED CARGO AFT SMOKE DETECTOR, OM CARGO OM REF WITH SMM 26-13-15-4. OPS CHECK GOOD, PN ON/OFF CGAB1201-01, SN ON 
- [SDR NSVA200600228](https://openairdocs.org/sdr/NSVA200600228), Dec 11, 2006: CONNECTOR. LOOSE. FOUND FIRE TEST RIGHT SIDE FAILED. FOUND RT FIRE LOOP CONNECTOR LOOSE TIGHTENED AND SATISFIED IAW SAAB AMM CHP 26-11-05, NO DISCREPANCY.
- [SDR NSVA200600087](https://openairdocs.org/sdr/NSVA200600087), Jun 21, 2006: WIRE. MALFUNCTIONED. AFTER TAKEOFF, NG FLUCTUATED ERRATICALLY BETWEEN 0-97% THEN DROPPED TO 0%. AUTO COARSEN HIGH LIGHT FLUCTUATED ON AND OFF ALSO. DURING LOW POWER SETTING NG NORMA
- [SDR NSVA200600076](https://openairdocs.org/sdr/NSVA200600076), Jun 15, 2006: UNKNOWN. UNKNOWN. LT ENGINE ITT REACHED 942 DEGREES FOR ABOUT 5 SECONDS. PERFORMED CAPPED AND UNCAPPED RUNS. DELTA FOUND TO BE 4.92, OPS CHECK OK.
- [SDR 06052006A](https://openairdocs.org/sdr/06052006A), Jun 4, 2006: TURBINE BLADES. DAMAGED. ON TAKEOFF 200 FEET OFF THE GROUND LT ENGINE SHUTDOWN. FOUND EXTENSIVE BLADE DAMAGE ON THE FIRST STAGE TURBINE IN THE HOT SECTION GOING AFT. FOUND DURING BORESC
- [SDR 05262006B](https://openairdocs.org/sdr/05262006B), May 24, 2006: PRESSURE SWITCH. FAULTY. LT ENGINE OIL PRESSURE LIGHT ON. R&R NR 1 ENGINE OIL PSI SWITCH PN 8346-501 OPS CHECK GOOD.
- [SDR 03012006C](https://openairdocs.org/sdr/03012006C), Feb 25, 2006: WARNING SYSTEM. MALFUNCTIONED. NR 2 ENGINE CHIP DETECTOR LIGHT ON INTERMITTENTLY. PERFORMED INSPECTION IAW GE MM 72-00-00 PAGE 128-144 INSPECTION OF OIL SCREENS. PERFORMED OIL CHANGE ON NR 2 
- [SDR 01252006B](https://openairdocs.org/sdr/01252006B), Jan 22, 2006: INDICATOR. INOPERATIVE. LOST ITT NEEDLE AND DIGITAL INDICATION ON TAKEOFF ROLL. REMOVED AND REPLACED ITT GAUGE IAW 77-20-05 PN ON/OFF 10227N01TOO SN ON 157A, SN OFF 124A, OPS CHECK GOO
- [SDR 11172005A](https://openairdocs.org/sdr/11172005A), Nov 14, 2005: WARNING SYSTEM. FALSE ACTIVATION. ABORTED TAKEOFF DUE TO CONFIG WARNING DURING TAKEOFF. PERFORMED OPERATIONAL TEST OF TAKEOFF CONFIG WARNING. NO DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD.

## Other aircraft with N202SR

- [Registered now](https://openairdocs.org/aircraft/N202SR): Cirrus Design SR22T, S/N 11394, built 2026

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