# N415XJ: Saab-Scania SAAB 340B, registration cancelled 2021-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2021
- Exported to: Canada
- 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-415
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 1997
- Certificate issued: March 25, 2010
- Last registry action: February 14, 2020
- Mode S code: A4E8C9
- Owner when cancelled: [US Bank Na Trustee](https://openairdocs.org/faa-owner/US%20BANK%20NA%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7452° N, 75.5937° W: Placed by OpenAirDocs at the center of ZIP code 19805, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N415XJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=415XJ
- Page: https://openairdocs.org/deregistered/N415XJ-2021-02-12

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 (117, newest 50)

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

- [SDR 29GA2019111500001](https://openairdocs.org/sdr/29GA2019111500001), Nov 13, 2019: CIRCUIT BREAKER. TRIPPED. FLIGHT: 70 EYW/MCO EMERGENCY LIGHT CABIN EXIT CTL CB L8 POPPED TWICE RESET ONCE. CORRECTIVE ACTION: RESET CB PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYST
- [SDR 29GA2019081500002](https://openairdocs.org/sdr/29GA2019081500002), Aug 14, 2019: POWER SUPPLY. INOPERATIVE. L-8 CB (EMERGENCY LIGHT CONTROL) POPPED IN FLIGHT. CORRECTIVE ACTION: UNABLE TO DUPLICATE. CHECKED WIRES AT FLIGHT ATTENDANT PANEL FOR CONDITION AND SECURITY, N
- [SDR 29GA2019081500001](https://openairdocs.org/sdr/29GA2019081500001), Aug 14, 2019: WIRE. LOOSE. FLIGHT# 0140 VPS/MCO REPORT: L8 CB (EMERGENCY LIGHT CONTROL) POPPED INFLIGHT. CORRECTIVE ACTION: INSPECTED LH. EXTERIOR EMERGENCY LIGHT + FOUND LOOSE WIRE WITH 
- [SDR 29GA2019081400002](https://openairdocs.org/sdr/29GA2019081400002), Aug 13, 2019: CIRCUIT BREAKER. TRIPPED. C/B L8 (EMERGENCY LIGHT CONTROL) POP UP IN FLIGHT. CORERECTIVE ACTION: RESET C/B AND PERFORMED OPERATIONAL CHECK NO DEFECT NOTED AT THIS TIME.
- [SDR 29GA2019072600001](https://openairdocs.org/sdr/29GA2019072600001), Jul 25, 2019: POWER SUPPLY. FAILED. FLIGHT# 0065 FLL/MHH REPORT: EMERGENCY LIGHT EXTERIOR CONTROL CIRCUIT BREAKER POPS REPEATEDLY. CORRECTIVE ACTION: T/S EMERGENCY LIGHT SYSTEM. FOUND 21LN POWER S
- [SDR 29GA2019072200001](https://openairdocs.org/sdr/29GA2019072200001), Jul 21, 2019: LIGHT. INOPERATIVE. FLIGHT# 0112 EYW/FLL REPORT: EMERGENCY LIGHT LAMP WILL NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT PUSH BUTTON INDICATION BULBS FOR " ARM" AND "
- [SDR 29GA2019071500004](https://openairdocs.org/sdr/29GA2019071500004), Jul 12, 2019: CIRCUIT BREAKER. TRIPPED. FLIGHT 0105, IN FLIGHT C/B L7 EMERGENCY LIGHT POWER AND L8 EMERGENCY LIGHT CONTROL TRIPPED. RESET C/B'S L7 EMERGENCY LIGHT POWER AND L8 EMERGENCY LIGHT CONTROL 
- [SDR 29GA2019053100001](https://openairdocs.org/sdr/29GA2019053100001), May 30, 2019: POWER SUPPLY. FAILED. FLIGHT# 0091 FLL/FLL REPORT:C/B L8 (EMER LT CABIN + EXT CTC) POPPED. CORRECTIVE ACTION: R/R EXTERIOR EMERGENCY- LIGHTING POWER SUPPLY (24LN) REF AMM 33-50-10-04
- [SDR 29GA2019053000002](https://openairdocs.org/sdr/29GA2019053000002), May 30, 2019: CIRCUIT BREAKER. TRIPPED. FLIGHT# 0091 FLL/FLL REPORT: C/B L8 POPPED. CORRECTIVE ACTION: RESET C/B L8, OPS CHECK OK IAW 39-50-00 AMM.
- [SDR 29GA2019042200001](https://openairdocs.org/sdr/29GA2019042200001), Apr 19, 2019: GAS CYLINDER. FAILED. AIRSTAIRS WILL NOT OPEN. R&R GAS SPRING ON AIRSTRAIRS IAW CMM 52-60-01, OPS CHECK GOOD.
- [SDR 29GA2019032500001](https://openairdocs.org/sdr/29GA2019032500001), Mar 24, 2019: LIGHT. CORRODED. FLIGHT 0122 EYW/FLL REPORT: EMER LT CTL CIRCUIT BRAKERS L-8 POPPED OUT. RESET ONCE STILL POPPED OUT. CORRECTIVE ACTION: CLEANED & REMOVED CORROSION ON RT EXTERN
- [SDR 29GA2019021900001](https://openairdocs.org/sdr/29GA2019021900001), Feb 15, 2019: WIRE. SHORTED. FLIGHT 0105 TCB/FLL REPORT: CB EMERGENCY EXT CTL L8 TRIPPED IN FLIGHT. REPAIRED WIRE LN59-22 THAT WAS TOUCHING GROUND ON LT BATTERY COMPARTMENT IAW WM 33-50-00.
- [SDR 29GA2019021800002](https://openairdocs.org/sdr/29GA2019021800002), Feb 15, 2019: POWER SUPPLY. MALFUNCTIONED. FLIGHT# 56, CIRCUIT BREAKER L8 TRIPPED IN FLIGHT ( EMERGENCY LIGHTS). REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY FOR EXTERNAL LIGHTS AND LEFT EMERGENCY LIG
- [SDR 29GA2019021800001](https://openairdocs.org/sdr/29GA2019021800001), Feb 14, 2019: CIRCUIT BREAKER. TRIPPED. FLIGHT# 86. CIRCUIT BREAKER L8 TRIPPED AND WAS RESET AND TRIPPED AGAIN. CORRECTIVE ACTION: RESET CIRCUIT BREAKER L8 FOR EMERGENCY LIGHTS AND PERFORMED OPERATION
- [SDR 29GA2019021500001](https://openairdocs.org/sdr/29GA2019021500001), Feb 14, 2019: CIRCUIT BREAKER. TRIPPED. CB EMER LT CTL L8 TRIPPED. RESET CIRCUIT BREAKER L8, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM REF AMM 33-50-00. OPS TEST GOOD.
- [SDR 29GA2018110200001](https://openairdocs.org/sdr/29GA2018110200001), Nov 1, 2018: CIRCUIT BREAKER. TRIPPED. L-8 CIRCUT BREAKER TRIPPED IN FLIGHT. PERFORMED MULTIPLE FUNCTIONAL TESTS OF THE EMERGENCY LIGHTS IAW AMM 24-35-00-05. CIRCUIT BREAKER L-8 NEVER TRIPPED AND ALL
- [SDR 29GA2018102900002](https://openairdocs.org/sdr/29GA2018102900002), Oct 28, 2018: WIRE. UNSECURE. FLIGHT 0086 ELH/FLL REPORT: CIRCUIT BREAKER L-8 POPPED OUT IN FLIGHT. (EMRGENCY LIGHT CB) CORRECTIVE ACTION: SECURED WIRE AT LT AFT EMERGENCY LIGHT LAMP HOLDER 
- [SDR 29GA2018052500003](https://openairdocs.org/sdr/29GA2018052500003), May 24, 2018: BULB. INOPERATIVE. ARM LIGHT ON THE FLIGHT ATTENDANT LIGHT PANEL, THE EMERGENCY LIGHT SWITCH WAS INOPERATIVE. REPLACED THE LIGHT SWITCH BULB. OPS TESTED GOOD.
- [SDR 29GA2018021400002](https://openairdocs.org/sdr/29GA2018021400002), Feb 13, 2018: WINDOW. DISLODGED. PAX SEATED IN 7A SAID THAT THE HE SAW THE OVERWING EMERGENCY HANDLE FALL DOWN AS WE WERE TAKING OFF, LANDED WITHOUT INCIDENT. DECLARED EMERGENCY. AS WE WERE TAX
- [SDR 29GA2018012200002](https://openairdocs.org/sdr/29GA2018012200002), Jan 20, 2018: WINDSHIELD. FAILED. FRONT RIGHT WINDSHIELD STARTED TO DELAMINATE IN FLIGHT, WITH WINDSHIELD HEAT ON. A BURN WAS NOTICED AND WINDSHIELD WAS TURNED OFF. ABOUT ONE MINUTE LATER THE EN
- [SDR 29GA2017122200001](https://openairdocs.org/sdr/29GA2017122200001), Dec 20, 2017: LINE. DISCONNECTED. LOST HYDRAULICS DURING TAXI, WENT TO ZERO, MAIN WENT TO ZERO, OTBD WENT TO ZERO. POST WALK AROUND NOTICED RIGHT MAIN HYDRAULIC LINE DISCONNECTED. REPLACED HYDRA
- [SDR 29GA2017121800002](https://openairdocs.org/sdr/29GA2017121800002), Dec 18, 2017: ENGINE. OIL CONSUMPTION. PRECAUTIONARY SHUTDOWN OF THE LT ENGINE DUE TO LOW OIL PRESSURE WITH FLUCTUATIONS. INSPECTED LT ENGINE, FOUND B-SUMP SCAVENGE LINE LOOSE, REMOVED ALL SCAVENGE S
- [SDR 29GA2017110500001](https://openairdocs.org/sdr/29GA2017110500001), Nov 4, 2017: SIGN. UNSECURE. FLIGHT 0099, EXIT SIGN IN CEILING FELL OUT. RE-SECURED ROW 7 EXIT LOCATOR IAW AMM 33-50-45-04. OPS CHECK GOOD.
- [SDR 29GA2017100800001](https://openairdocs.org/sdr/29GA2017100800001), Oct 6, 2017: FAN. FAILED. ODOR OF A BURNING PLASTIC BELOW 10,000 FT. PERFORMED AN AIR DISTRIBUTION SYSTEM OPERATIONAL TEST, NO ODOR PRESENT, OPS CHECKED GOOD IAW MM 21-20-00. REMOVED AND
- [SDR 29GA2017091800001](https://openairdocs.org/sdr/29GA2017091800001), Sep 17, 2017: UNKNOWN. ODOR. COCKPIT HAD A BURNING ODOR, FA DID NOT NOTICE IN CABIN, SEEMS WORSE WITH HP VALVES OPEN. ODOR CONSTANT DURING FLIGHT LOWER ALTITUDE, THE WORSE THE ODOR. INSPECT
- [SDR 29GA2016061900001](https://openairdocs.org/sdr/29GA2016061900001), Jun 18, 2016: STRUT. LOW. CONFIG ILLUMINATED DURING CLIMBOUT AND THEN WAS INTERMITTENT THROUGHOUT FLIGHT. FOUND MLG STRUTS NOT FULLY EXTENDING, CAUSING WOW SWITCHES TO INTERMITENTLY ACTI
- [SDR 29GA2016032000002](https://openairdocs.org/sdr/29GA2016032000002), Mar 17, 2016: BULB. BURNED OUT. EMERGENCY ARM LIGHT BULB INOPERATIVE. FOUND EMERGENCY ARM LIGHT BULB INOPERATIVE. R & R BULB IAW AMM CH 33-50-00, OPS CHECKED GOOD.
- [SDR 29GA2015111800001](https://openairdocs.org/sdr/29GA2015111800001), Nov 16, 2015: ACCUMULATOR. LEAKING. WHILE PARKING BRAKE FELT SOFT, AND PARKED AT THE GATE ENGINES RUNNING BRAKES BOTTOM DOWN NOTICED MAIN ACCUMULATOR RUNNING LOW AND FREQUENTLY. R & R HYDRAULIC PR
- [SDR 29GA2015061900001](https://openairdocs.org/sdr/29GA2015061900001), Jun 10, 2015: SKIN. DENTED. DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED FUSELAGE SKIN DENTED IN 2 PLACES, BETWEEN FS 658.5 AND FS 677, S-1520 AND S-1524. REMOVED DAMAGE AND INSTALLED 
- [SDR 29GA2015042200001](https://openairdocs.org/sdr/29GA2015042200001), Apr 20, 2015: SLIDE. DIRTY. AIRSTAIR DOOR DIFFICULT TO SLIDE CLOSE. CLEANED SLIDE OPS CHECK GOOD.
- [SDR 29GA2015021600001](https://openairdocs.org/sdr/29GA2015021600001), Feb 11, 2015: WINDSHIELD. ODOR. STRONG ODOR FROM RT FRONT WINDSHIELD. R & R COPILOT'S WINDSHIELD, OPS CK GOOD.
- [SDR 29GA35932121713](https://openairdocs.org/sdr/29GA35932121713), Dec 17, 2013: HANDLE. MALFUNCTIONED. ON DEPARTURE, WITH FLAPS 15 DEGREES AND GEAR HANDLE UP GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH HYDRAULIC PUMP RUNNING UNTIL FLAPS BROUGHT TO 0 DEGREES. ON P
- [SDR 29GA35932092213](https://openairdocs.org/sdr/29GA35932092213), Sep 22, 2013: BRAKE SYS. INOPERATIVE. LOSS OF BRAKING ON TAXI. REPLACED NR 1 AND 4 ANTI-SKID TRANSDUCERS, POWER BRAKE VALVE, LT ANTI-SKID CONTROL VALVE AND RELAY 13JA-K1. OPS CHECKED GOOD.
- [SDR 2013FA0000551](https://openairdocs.org/sdr/2013FA0000551), Sep 20, 2013: VALVE. BYPASSING. MAIN HYD ACCUMULATOR SEEMS TO BE DROPPING PRESSURE MORE QUICKLY THAN NORMAL. AS PRESSURE DROPS WE LOST BRAKE EFFECTIVENESS UNTIL PUTTING PUMP IN OVERRIDE. DURIN
- [SDR 2013FA0000550](https://openairdocs.org/sdr/2013FA0000550), Sep 20, 2013: HYDRAULIC SYSTEM. MALFUNCTIONED. MAIN HYD ACCUMULATOR SEEMS TO BE DROPPING PRESSURE MORE QUICKLY THAN NORMAL. AS PRESSURE DROPS WE LOSS BRAKE EFFECTIVENESS UNTIL PUTTING PUMP IN OVERRIDE. DURIN
- [SDR 29GA201306140013](https://openairdocs.org/sdr/29GA201306140013), Jun 12, 2013: WIRE HARNESS. DAMAGED. AFTER SELECTING THE GEAR HANDLE UP, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED, RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING UPLOCK SWI
- [SDR 29GA35921060713](https://openairdocs.org/sdr/29GA35921060713), Jun 7, 2013: UNKNOWN. FUMES. FLIGHT: 3946 FLL/EYW ON DESCENT THROUGH 9000 FEET STRONG FUMES EMITTED THROUGH VENT IN THE COCKPIT. PERFORMED RIGHT ENGINE RUNS WITH LEFT AND RIGHT PACKS SEPARA
- [SDR MALA090129](https://openairdocs.org/sdr/MALA090129), Oct 22, 2009: SEAT TRACK. CORRODED. DURING 2 YEAR INSPECT IN CWA, NOTED CORROSION AT LT AISLE SEAT TRACK, IB SIDE, STA 622 REPAIRED IAW EO S53077
- [SDR MALA090043](https://openairdocs.org/sdr/MALA090043), Mar 17, 2009: SKIN. DENTED. DURING 30K AND 6Y INSPECTIONS, DENT IN LOWER SKIN OF LT HORIZONTAL STAB 6 INCH FROM FUSELAGE, 5 INCH FROM FWD EDGE OF SKIN. REPAIRED.
- [SDR MALA090040](https://openairdocs.org/sdr/MALA090040), Mar 17, 2009: SKIN. DENTED. DURING 30K AND 6Y INSPECTIONS, DENT IN AILERON UPPER SKIN LOCATED AT WS 367.4 AND 7 INCH FWD OF TRAILING EDGE. REPAIRED.
- [SDR MALA090039](https://openairdocs.org/sdr/MALA090039), Mar 17, 2009: INLET. CHAFED. DURING 30K AND 6Y INSPECTIONS, LT NACELLE LOWER DECK BELOW INLET ASSY IS CHAFED THRU. REPAIRED
- [SDR MALA090038](https://openairdocs.org/sdr/MALA090038), Mar 17, 2009: SKIN. DENTED. DURING 30K AND 6Y INSPECTIONS, DENT IN LOWER SKIN OF RT HORIZONTAL STAB 4.5 INCH FROM AFT EDGE AND HS131.67. REPAIRED.
- [SDR MALA090018](https://openairdocs.org/sdr/MALA090018), Feb 10, 2009: BATTERY PACK. FAILED. WHILE PERFORMING JC335003, FUNCTIONAL TEST OF EMERGENCY BATTERY PACK CAPACITY, POWER PACK 21LN FAILED CHECK. REMOVED AND REPLACED POWER SUPPLY 21LN, P/N 3301-51
- [SDR MALA090005](https://openairdocs.org/sdr/MALA090005), Jan 15, 2009: ENGINE. MALFUNCTIONED. AFTER TAKEOFF, THE RT ENGINE WAS MAKING A LOUD POPPING SOUND AND THEN STARTED SHUTTING ITSELF DOWN. CREW SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY.
- [SDR MAL2008F00024](https://openairdocs.org/sdr/MAL2008F00024), Aug 13, 2008: POWER SUPPLY. INOPERATIVE. EMERGENCY POWER SUPPLY AT 23LN INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT LOCATION 23LN P/N 3301-51 OFF/ON S/N 2108 OFF S/N 2057 ON IAW SAAB AM
- [SDR MALA080022](https://openairdocs.org/sdr/MALA080022), Feb 7, 2008: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHT P/N 6636-2 INOP. REMOVED AND REPLACED LIGHT IAW SAAB AMM 33-50-20-04.
- [SDR MALA070204](https://openairdocs.org/sdr/MALA070204), Dec 28, 2007: ANTENNA. MALFUNCTIONED. ON ILS APPROACH TO DTW, APPROACH MODE ARMED AT 4000 FT, SHOWING HIGH ON SLOPE. AUTO PILOT ON. UNCOMMANDED DESCENT TO 4000 FPM NOTED. AP OFF. AP REMAINED OFF FOR
- [SDR MALA070162](https://openairdocs.org/sdr/MALA070162), Sep 12, 2007: STRUCTURE. PUNCTURED. RUDDER LEADING EDGE PUNCTURE. REPAIRED PER EOS55127.
- [SDR MALA070160](https://openairdocs.org/sdr/MALA070160), Sep 12, 2007: SKIN. DENTED. LT ELEVATOR 2ND UPPER SKIN DENT 11.5" FROM THE INBD END 9.0" FWD OF THE T/E REPAIRED PER EOS51031.
- [SDR MALA070159](https://openairdocs.org/sdr/MALA070159), Sep 12, 2007: SKIN. DENTED. DENTS IN THE RT FUSELAGE SKIN BENEATH THE NR 7 AND NR 8 ICE GUARDS. REPAIRED PER EOS53472.

All 117: https://openairdocs.org/deregistered/N415XJ-2021-02-12/reports.md

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