# N384AE: Saab-Scania SAAB 340B, registration cancelled 2010-05-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 13, 2010 - Exported to: Australia - Status when cancelled: Triennial form not returned - 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-384 - Year built: 0 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: April 10, 1996 - Certificate issued: October 29, 1996 - Last registry action: November 18, 2008 - Mode S code: A46A2B - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N384AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=384AE - Page: https://openairdocs.org/deregistered/N384AE-2010-05-13 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 (13) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA200828201](https://openairdocs.org/sdr/SIMA200828201), Oct 8, 2008: SEAT TRACK. CORRODED. DURING A HMBV INSPECTION THE SEAT TRACK AT 18.3L WAS FOUND TO BE CORRODED FROM FS 296 TO FS 310. REMOVED A 31 INCH SECTION OF SEAT TRACK. CUT NEW SECTION OF SEA - [SDR SIM2008F00029](https://openairdocs.org/sdr/SIM2008F00029), Oct 3, 2008: REPAIR. CORRODED. DURING A HMBV INSP, AN OLDER REPAIR ON THE GALLEY FRAME AT FS 258 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR FILLER. FABRICATED A NEW FILLER. DRILLED - [SDR SIMA200734401](https://openairdocs.org/sdr/SIMA200734401), Dec 6, 2007: SENSOR. FAILED. RIGHT PROP PSI INDICATIONS PEGGED IN RED. FLUCTUATES WHEN IN FEATHER. OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT PROP OIL PRESSURE SENSOR ON TH - [SDR SIMA200719701](https://openairdocs.org/sdr/SIMA200719701), Jul 13, 2007: OIL COOLER. FAILED. RIGHT ENGINE OIL TEMPERATURE INDICATION IN RED, DURING TAXI OIL PRESSURE INDICATION ERRATIC WITH ENGINE SHUTDOWN. RETURNED TO LFT. REMOVED AND REPLACED OIL SAVA - [SDR SIMA200701502](https://openairdocs.org/sdr/SIMA200701502), Jan 12, 2007: OVERHEAT SENSOR. FAILED. RIGHT TAIL PIPE HOT LIGHT CAME ON CLIMB-OUT, LIGHT WENT OUT WITHOUT ANY CREW ACTION. MGM EGT 874 DEGREES, OAT 8 DEGREES WITH ANTI-ICE ON. REMOVED AND REPLACED T - [SDR SIMA200418814](https://openairdocs.org/sdr/SIMA200418814), Jun 4, 2004: FRAME. CORRODED. DURING AN MBV INSPECTION A PREVIOUS REPAIR TO FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORRODED PREVIOUS REPAIR AND EXTENDED THE EXISTING CUT - [SDR SIMA200416001](https://openairdocs.org/sdr/SIMA200416001), Jun 2, 2004: SEAT TRACK. CORRODED. ABI - DURING AN MBV INSPECTION, THE CABIN SEAT TRACK AT BL 0.0 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT THE WING BOX. REMOVED CORRODED SEAT TRACK AND INSTA - [SDR SIMA200416204](https://openairdocs.org/sdr/SIMA200416204), May 29, 2004: FRAME. DENTED. ABI - DURING AN MBV INSPECTOIN, CARGO FRAME AT STATION 677 WAS FOUND DENTED 5.5 INCH ABOVE FLOOR. PERFORMED A CUTOUT OF FRAME 677 FLANGE WITH A MIN RADIUS OF .0 - [SDR SIMA200416205](https://openairdocs.org/sdr/SIMA200416205), May 29, 2004: FRAME. CORRODED. ABI - DURING AN MBV INSPECTION, THE BOTTOM FRAME UPPER FLANGE AT STATION 258, 17 INCHES FROM OUTBOARD HAS SINGLE ISOLATED CORROSION PIT. REMOVED CORROSION BY DR - [SDR SIMA200219132](https://openairdocs.org/sdr/SIMA200219132), Jul 8, 2002: POWER SUPPLY. INOPERATIVE. CREW REPORTED EMERGENCY LIGHT CONTROL CIRCUIT BREAKER POPED DURING FLIGHT. C/A: REMOVED AND REPLACED BATTERY SUPPLY 21LN AND 23LN IAW MM. OPS CHECK GOOD. - [SDR SIMA1553](https://openairdocs.org/sdr/SIMA1553), Jun 3, 2000: LIGHT. INOPERATIVE. DFW - FLT 3605 - EMERGENCY LIGHT STRIP BETWEEN 8A AND 9A DOES NOT WORK. PUT ON MEL. C/A - INSTALLED ENTRY LIGHT AT 8A-9A IAW SAAB AMM 33-50-02. OPS CHECKED GOOD - [SDR SIMA980152](https://openairdocs.org/sdr/SIMA980152), Jan 15, 1998: END CAP. CORRODED. ABI - DURING MBV, FOUND RT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 297 FROM BL ZERO TO BLR 32.8. REMOVED AND REPLACED RT TRACK END CA IAW SAAB 340 SRM 5 - [SDR SIMA980151](https://openairdocs.org/sdr/SIMA980151), Jan 15, 1998: END CAP. CORRODED. ABI - DURING MBV, FOUND LT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 297 FROM BLL 18.3 TO BLL 32.8. REMOVED AND REPLACED LT TRACK END CAP IAW SAAB 340 SRM ## Other aircraft with N384AE - [Registered now](https://openairdocs.org/aircraft/N384AE): DJI AGRAS T25, S/N 63NBLBD0030094 - [Cancelled 2014-02-28](https://openairdocs.org/deregistered/N384AE-2014-02-28): American Eurocopter MBB-BK 117 C-2, S/N 9634. Owner: [American Eurocopter Corp](https://openairdocs.org/faa-owner/AMERICAN%20EUROCOPTER%20CORP), [Grand Prairie, TX](https://openairdocs.org/faa-place/TX/Grand%20Prairie) --- 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.