# N416XJ: 1997 Saab SAAB 340B, registration cancelled 2015-11-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 18, 2015
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Saab SAAB 340B](https://openairdocs.org/model/saab-saab-340b) (registry code 7860105)
- Engine: [GE CT7-9B](https://openairdocs.org/engine/ge-ct7-9b) (registry code 30148)
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU), [TCDS E8NE](https://openairdocs.org/tcds/E8NE) (OpenAirDocs)
- Serial number: 340B416
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 20, 2015
- Certificate issued: August 18, 2015
- Last registry action: August 18, 2015
- Mode S code: A4EC80
- 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/N416XJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=416XJ
- Page: https://openairdocs.org/deregistered/N416XJ-2015-11-18

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 Saab SAAB 340B: https://openairdocs.org/model/saab-saab-340b.md

## Service difficulty reports (68, newest 50)

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

- [SDR MALA090095](https://openairdocs.org/sdr/MALA090095), Jul 8, 2009: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY PACK 23LN LOW. REMOVED AND REPLACED 23LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003.
- [SDR MALA090094](https://openairdocs.org/sdr/MALA090094), Jul 8, 2009: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY PACK 21LN LOW. REMOVED AND REPLACED 21LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003, PN ON/OFF 3301-51 SN OFF 1405, SN ON 
- [SDR MALA090080](https://openairdocs.org/sdr/MALA090080), Jun 6, 2009: WARNING SYSTEM. FALSE ACTIVATION. ON TAKEOFF RT TAILPIPE HOT LIGHT CAME ON. RAN QRH ALL ENGINE PARAMETERS WERE NORMAL. PERFORMED VISUAL INSPECTION OF RT TAIL PIPE HOT DETECTION CONNECTORS, HARNE
- [SDR MAL2008F00018](https://openairdocs.org/sdr/MAL2008F00018), Jul 25, 2008: MOTOR. MALFUNCTIONED. F/A REPORTS STRONG ODOR IN CABIN AGAIN. SMELLS LIKE AN ELECTRICAL SMELL. NOTED STRONG ELECTRICAL SMELL COMING FROM BURNT UP SUPP AIR MOTOR. SYSTEM ON MEL (INOP)
- [SDR MALA070182](https://openairdocs.org/sdr/MALA070182), Oct 16, 2007: SKIN. DENTED. SEVERAL DENTS WERE FOUND IN THE RT FUSELAGE SKIN, IN THE ICE GUARD AREA LOCATED FROM STA 313 AND STA 321, BETWEEN STRINGERS SL1615 AND SL 1622. DOUBLER/TRIPLER 
- [SDR MALA070016](https://openairdocs.org/sdr/MALA070016), Jan 22, 2007: POWER SUPPLY. INOPERATIVE. DURING LC2 NOTED EMERGENCY LIGHTS FROM BATTERY PACK 24LN INOP. REMOVED AND REPLACED POWER SUPPLY 24LN PN 3301-51, SN ON 2205, SN OFF 2129.
- [SDR MALA060632](https://openairdocs.org/sdr/MALA060632), Dec 22, 2006: BATTERY PACK. NO TEST. FAILED CAP CHECK PER BF GOODRICH C.M.M.W.O. 417138. REPLACED BATTERY PACK.
- [SDR MALA060503](https://openairdocs.org/sdr/MALA060503), Aug 4, 2006: WIRE. CHAFED. EMERGENCY CALL LIGHT ON PILOTS OVERHEAD PANEL WAS INOP WHEN EMERGENCY CALL BUTTON WAS PUSHED. LAMP TEST OK. FOUND WIRE RY63-24 CHAFED ALMOST THROUGH. REPLACED W
- [SDR MALA060479](https://openairdocs.org/sdr/MALA060479), Jul 18, 2006: ENGINE. MAKING METAL. RT CHIP DETECT LIGHT ILLUMINATED INTERMITTENT. AIR RETURNED. CHANGED ENGINE.
- [SDR MALA060332](https://openairdocs.org/sdr/MALA060332), May 19, 2006: SKIN. DAMAGED. HAIL CONTACT DAMAGE ON LT AILERON 33 1/4" OB ON LEADING EDGE 2" AFT OF LEADING EDGE AND ALSO AT STA 390.82, 2" FROM AILERON TRAILING EDGE. DAMAGE REPAIRED IAW E
- [SDR MALA060313](https://openairdocs.org/sdr/MALA060313), May 9, 2006: SKIN. DENTED. HAIL CONTACT DAMAGE ON LEFT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS113, .025 INCH DEEP AND .703 INCH DIAMETER. LOCATED 6.5 INCHES AFT OF 
- [SDR MALA060288](https://openairdocs.org/sdr/MALA060288), Apr 28, 2006: SKIN. DENTED. HAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS 38.58, .022 INCH DEEP AND 1.0 INCH DIAMETER. LOCATED 6.5 INCHES FORW
- [SDR MALA060287](https://openairdocs.org/sdr/MALA060287), Apr 28, 2006: SKIN. DENTED. HAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS99.92, .025 INCH DEEP AND 0.640 INCH DIAMETER. LOCATED 11.5 INCHES FR
- [SDR MALA060080](https://openairdocs.org/sdr/MALA060080), Feb 16, 2006: SKIN. LIGHTNING STRIKE. ON CLIMBOUT FROM DTW A/C STRUCK BY LIGHTNING. THE STRIKE APPEARED TO HIT NEAR CAPTAIN'S SIDE AROUND PITOT TUBE AREA. ALL INSTRUMENTS FINE. AIR RETURNED TO DTW. 
- [SDR MALA050483](https://openairdocs.org/sdr/MALA050483), Jun 19, 2005: WARNING LIGHT. ILLUMINATED. CREW RETURNED TO MSP FOLLOWING INDICATION OF DUCT OVER TEMPERATURE INDICATION. NO EMERGENCY DECLARED AND FLIGHT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NO FU
- [SDR MALA050384](https://openairdocs.org/sdr/MALA050384), Apr 26, 2005: FLOOR SUPPORT. CORRODED. AIRSTAIR FLOOR RAIL, P/N 7253710-871 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21/22.
- [SDR MALA050388](https://openairdocs.org/sdr/MALA050388), Apr 25, 2005: SKIN. DENTED. FUSELAGE SKIN IS DENTED BETWEEN FS 339 AND FS 363 AND BETWEEN STRINGER'S SL1504 AND SL1506. THE DENTS ARE OUT OF LIMITS AND HAVE BEEN REPAIRED IAW MESABA EO S53
- [SDR MALA050386](https://openairdocs.org/sdr/MALA050386), Apr 25, 2005: STRUCTURE. CORRODED. LEFT WRAP AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21.
- [SDR MALA050385](https://openairdocs.org/sdr/MALA050385), Apr 25, 2005: STRUCTURE. CORRODED. RIGHT WRAP AROUND P/N 7253710243 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 51-40-21.
- [SDR MALA050387](https://openairdocs.org/sdr/MALA050387), Apr 23, 2005: SEAT TRACK. CORRODED. GALLEY SEAT TRACK HAD PROFILE P/N'S 7253721-459 AND 7253721-495 ARE CORRODED AND HAVE BEEN REPLACED IAW SRM 51-40-21 AND 51-40-22.
- [SDR MALA050311](https://openairdocs.org/sdr/MALA050311), Apr 2, 2005: ENGINE. MALFUNCTIONED. LT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND GAUGE WAS READING LOW (ABOUT 25-30 PSI) ON TAKEOFF. CREW FOLLOWED QRH BUT DID NOT SHUT DOWN ENGINE. AIR RETURNED. R
- [SDR MALA050107](https://openairdocs.org/sdr/MALA050107), Jan 5, 2005: WARNING LIGHT. ILLUMINATED. LT MAIN AND ESS BUSS BREAKER POPPED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE RAN BOTH ENGINES, APPLIED HEAVY LOAD ON PDU. NO FAULTS NOTED. REFER TO LOG PG NR 12
- [SDR MALA040571](https://openairdocs.org/sdr/MALA040571), Sep 13, 2004: CONTROL UNIT. MALFUNCTIONED. LOST PRESSURIZATION AT 25,000 FT DESCENDED TO 10,000 FT NOTE CABIN ALTITUDE FOLLOWED TO -1. FOUND C/B G7 POPPED. RESET, SWITCHED TO MANUAL MODE, FOUND IT CONTRO
- [SDR MALA040568](https://openairdocs.org/sdr/MALA040568), Sep 7, 2004: CHARGER. INOPERATIVE. CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED HOLDER.
- [SDR MALA040385](https://openairdocs.org/sdr/MALA040385), May 7, 2004: GENERATOR. FAILED. DURING TAXI OUT, LT AC GEN FAILED TO COME ON LINE. PAX REPORTED SMOKE AND FLAMES EXIT A/C OF EXHAUST HOLE. A/C RETURNED TO GATE. MAINTENANCE REPLACED LT AC GEN.
- [SDR MALA040343](https://openairdocs.org/sdr/MALA040343), Apr 24, 2004: ENGINE. OVERTEMP. LEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE WAS LESS THAN 10 PERCENT ITT WAS 1200-1300C
- [SDR MALA020546](https://openairdocs.org/sdr/MALA020546), Sep 3, 2002: STRUCTURE. CORRODED. DURING 4K-INSPECTION IN CWA, LT FWD SEAT TRACK WRAP AROUND HAS HEAVY CORROSION AT STA 294. MAINTENANCE INSTALLED NEW WRAP AROUND.
- [SDR MALA020539](https://openairdocs.org/sdr/MALA020539), Sep 2, 2002: ANGLE. DURING 4K-INSPECTION IN CWA, CARGO FLOOR ANGLE BETWEEN AFT CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED NEW ANGLE IAW SRM CHAP 51. RE
- [SDR MALA020547](https://openairdocs.org/sdr/MALA020547), Sep 1, 2002: SEAT TRACK. CORRODED. DURING 4K-INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK FWD PORTION AND CLIP HAS CORROSION AT APPROXIMATELY STA 294. MAINTENANCE REMOVED CORROSION IAW SRM 51-70
- [SDR MALA020545](https://openairdocs.org/sdr/MALA020545), Sep 1, 2002: FLOORBOARD. CORRODED. DURING 4K-INSPECTION IN CWA, RT O/B FLOORBOARD FLANGE HAS CORROSION AFT OF STA 288. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020544](https://openairdocs.org/sdr/MALA020544), Sep 1, 2002: SEAT TRACK. CORRODED. DURING 4K-INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK TOP AND PROFILE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GALLEY SEAT TRACK IAW SRM 51.
- [SDR MALA020541](https://openairdocs.org/sdr/MALA020541), Sep 1, 2002: ANGLE. CORRODED. DURING 4K-INSPECTION IN CWA, ANGLE AT FRAME STA 225 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020540](https://openairdocs.org/sdr/MALA020540), Sep 1, 2002: STRUCTURE. CORRODED. DURING 4K-INSPECTION IN CWA, RT SEAT TRACK FWD WRAP AROUND AT STA 294 HAS HEAVY CORROSION. MAINTENANCE INSTALLED NEW WRAP AROUND.
- [SDR MALA020538](https://openairdocs.org/sdr/MALA020538), Sep 1, 2002: CHANNEL. CORRODED. DURING 4K-INSPECTION IN CWA, AIRSTAIR SLIDE UNIT CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020537](https://openairdocs.org/sdr/MALA020537), Sep 1, 2002: SEAT TRACK. CORRODED. DURING 4K-INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK FWD PORTION STA 297 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020543](https://openairdocs.org/sdr/MALA020543), Aug 30, 2002: FRAME. CORRODED. DURING 4K-INSPECTION IN CWA, FRAME AND ANGLE TOPS AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020542](https://openairdocs.org/sdr/MALA020542), Aug 30, 2002: BEAM. CORRODED. DURING 4K-INSPECTION IN CWA, LT BEAM AND ANGLE LBL 10.5 BETWEEN FRAME STA 258 & 236.5 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020352](https://openairdocs.org/sdr/MALA020352), Jun 15, 2002: SPEAKER. SHORTED. ON FLIGHT 3349, F/A NOTED SMOKE FROM ANC SPEAKER, ROW 3 / 4A. FOLLOWED BY AN ELECTRICAL ODOR, F/A SHUT OFF ANC AND ODOR WENT AWAY. MAINTENANCE PERFORMED OPS CHE
- [SDR MALA020141](https://openairdocs.org/sdr/MALA020141), Jan 29, 2002: MODULE. FAILED. DURING FLIGHT 3317, RT INTAKE HEAT FAILED, INTAKE HEAT WAS CYCLING ON AND OFF AT ABOUT 14 SECOND INTERVALS. AC DIVERTED TO CWA, BECAUSE OF WEATHER CONDITIONS IN
- [SDR MALA010284](https://openairdocs.org/sdr/MALA010284), Mar 21, 2001: SELECTOR VALVE. DEFECTIVE. ON FLIGHT 2861, WHILE ON APPROACH IN MSP THE GEAR DISCREPANCY LIGHT ILLUMINATED. AFTER GOING MISS APPROACH AND PERFORMING THE ORH, DISCOVERED THE F7 C/B WAS POP
- [SDR MALA010153](https://openairdocs.org/sdr/MALA010153), Feb 1, 2001: POWER LEVER. UNDERTORQUED. LT AND RT ENGINE WILL ONLY MAKE 72 PERCENT TORQUE WITH POWER LEVERS FIREWALLED. AT FL210 WHILE SETTING POWER FOR TREND TRIED TO SET TORQUE TO 74 PERCENT, PL''S 
- [SDR MALA000684](https://openairdocs.org/sdr/MALA000684), Nov 18, 2000: MODULE. FAILED. RH ENGINE INTAKE LIGHT ON IN FLIGHT. QRH RESET THEN LIGHT CAME ON AGAIN. AIR TURN BACK TO DTW. MAINTENANCE REPLACED RH DEICE CONTROL MODULEPN 44730-501, SN/ON A
- [SDR MALA000624](https://openairdocs.org/sdr/MALA000624), Sep 26, 2000: DUCT. CRACKED. FOUND DURING C-CHECK, RT ENGINE INBOARD NACA DUCT CRACKED AT PANEL 463AL. REFER TO CELSIUS TASK CARD 4535, W/O 18843 AND SAAB STATEMENT 340 SDS000144. MAINTENAN
- [SDR MALA000623](https://openairdocs.org/sdr/MALA000623), Sep 26, 2000: SKIN. DENTED. FOUND DURING C-CHECK, RT HORIZONTAL STABILIZER UPPER SURFACE AT HS STA 439.2 HAS SEVERAL DENTS. REFER TO CELSIUS TASK CARD 3510, W/O 18843 AND SAAB STATEMENT 34
- [SDR MALA000622](https://openairdocs.org/sdr/MALA000622), Sep 23, 2000: SKIN. DENTED. FOUND DURING C-CHECK, GROUP OF DENTS IN LT FUSELAGE BENEATH ICE SHIELD STA 331, WL 107. REFER TO CELSIUS TASK CARD 2548, W/O 18843, AND SAAB STATEMENT 340SDS000
- [SDR MALA000625](https://openairdocs.org/sdr/MALA000625), Sep 20, 2000: RIB. CRACKED. FOUND DURING C-CHECK, 3 RIBS CRACKED ON LEADING EDGE PANEL 611BR. REFER TO CELSIUS TASK CARD 6506, W/O18843. MAINTENANCE REMOVED CRACKED SECTION OF 3 CRACKED RI
- [SDR MALA000620](https://openairdocs.org/sdr/MALA000620), Sep 20, 2000: SKIN. DENTED. LT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX
- [SDR MALA000619](https://openairdocs.org/sdr/MALA000619), Sep 20, 2000: SKIN. DENTED. FOUND DURING C-CHECK, LT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF 
- [SDR MALA000618](https://openairdocs.org/sdr/MALA000618), Sep 20, 2000: SKIN. DENTED. FOUND DURING C-CHECK, SEVERAL DENTS IN RT FUSELAGE ABOVE AND BELOW PREVIOUS REPAIR AT STA 339.0. REFER TO CELSIUS TASK CARD 2528, W/O 18843. MAINTENANCE FOUND D
- [SDR MALA000617](https://openairdocs.org/sdr/MALA000617), Sep 19, 2000: FLOOR SUPPORT. CORRODED. FOUND DURING C-CHECK, CORROSION ON RT FLOORBOARD BL 0 FROM STA 294 TO STA 350. REFER TO CELSIUS TASK CARD 1524, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINT

All 68: https://openairdocs.org/deregistered/N416XJ-2015-11-18/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20080725847019I](https://openairdocs.org/incident/20080725847019I), Jul 25, 2008: Saab 340B (N416XJ), Peoria, IL, No damage. (-23) Incident # igl 1920080033. While the aircraft was sitting on the gate, the pilot advised Peoria ground control that after engine start thaey had smoke on…
- [Incident 20020225012049I](https://openairdocs.org/incident/20020225012049I), Feb 25, 2002: Saab 340B (N416XJ), Detroit, MI, Substantial damage. (-23) During docking operations on February 25, 2002, mesaba airlines, inc., hit the jet way shroud at gate C2 at dtw airport. The aircraft had been marshaled…

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