# N370PX: 1992 Saab-Scania SAAB 340B, registration cancelled 2017-10-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 27, 2017
- Status when cancelled: Registration expired, pending cancellation
- 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-300
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 28, 1992
- Certificate issued: June 12, 2009
- Last registry action: July 19, 2011
- Mode S code: A43526
- Owner when cancelled: [Turbo Lease LLC](https://openairdocs.org/faa-owner/TURBO%20LEASE%20LLC)
- Location: [Chestnut Hill, MA](https://openairdocs.org/faa-place/MA/Chestnut%20Hill)
- Owner type: Corporation
- Owner's area on the map: 42.3143° N, 71.1528° W: Placed by OpenAirDocs at the center of ZIP code 02467, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N370PX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=370PX
- Page: https://openairdocs.org/deregistered/N370PX-2017-10-27

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 (49)

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

- [SDR NSV2008F00005](https://openairdocs.org/sdr/NSV2008F00005), Jun 24, 2008: SMOKE DETECTOR. MALFUNCTIONED. LAV SMOKE LIGHT ILLUMINATED AFTER ENGINE START, NO SMOKE FROM LAV. AIRCRAFT RETURNED TO GATE AND MX SENT. MAINTENANCE DEFERRED LAV REF. NEF 232. (K)
- [SDR NSV2008F00002](https://openairdocs.org/sdr/NSV2008F00002), Jun 4, 2008: UNKNOWN. SMOKE. AFTER SHUTTING DOWN RT ENGINE MASTER WARNING CARGO SMOKE LIGHT ILLUMINATED, STAYED ON, DISCHARGED EXTINGUISHER IN CARGO COMPARTMENT. NO SMOKE/ FLAMES NOTED BY G
- [SDR NSVA2008021](https://openairdocs.org/sdr/NSVA2008021), Apr 27, 2008: POWER SUPPLY. INOPERATIVE. DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM ON A LINE CHECK, 3 EMERGENCY COVE LIGHTS WERE FOUND NOT ILLUMINATING. EMERGENCY LIGHT POWER SUPPLY 20LN WAS R
- [SDR NSVA2008008](https://openairdocs.org/sdr/NSVA2008008), Feb 27, 2008: BULB. INOPERATIVE. EMERGENCY DECLARED DUE TO LANDING GEAR UNSAFE INDICATION. CREW RAN ABNORMAL CHECKLIST AND LANDED WITHOUT INCIDENT. MX FOUND THE BULBS IN THE GEAR HANDLE TO BE I
- [SDR NSVA20070246](https://openairdocs.org/sdr/NSVA20070246), Dec 5, 2007: POWER SUPPLY. INOPERATIVE. FLOOR EMERGENCY LIGHTS ROW 5/6 ARE INOP, 3 CONSECUTIVE. REPLACED POWER SUPPLY.
- [SDR NSVA20070239](https://openairdocs.org/sdr/NSVA20070239), Oct 2, 2007: DOOR. MALFUNCTIONED. LT INBD MLG DOOR REMAINED OPENED IN FLIGHT. INSPECTED LT MLG DOOR, CLEANED 5-10 TIMES IAW 32-10-00-00. OPS CHECK GOOD.
- [SDR NSVA20070176](https://openairdocs.org/sdr/NSVA20070176), Jul 5, 2007: DETECTION SYS. MALFUNCTIONED. DURING FIRE SHORT TEST R FIRE DET LT DID NOT ILLUMINATE. PERFORMED OPERATIONAL CHECK, NO DEFECT NOTED IAW AMM 26-10-00.
- [SDR NSVA20070142](https://openairdocs.org/sdr/NSVA20070142), May 30, 2007: WIRE HARNESS. WORN. L/R FUEL FLOW INDICATORS ERRATIC. FOUND BRACKET HOLDING START BLEED VALVE BROKEN. BLEED VALVE WORE THROUGH RT ENGINE "WHITE HARNESS." REMOVED AND REPLACED BRACK
- [SDR MALA050614](https://openairdocs.org/sdr/MALA050614), Jul 27, 2005: SKIN. DAMAGED. WARRANTY, 4Y/2Y RT ELEVATOR UPPER SURFACE HAS COMPOSITE DAMAGE 68 INCHES FROM I/B END. REPAIRED IAW MESABA EO NR S51031. REMOVED AND REINSTALLED ELEVATOR.
- [SDR MALA050611](https://openairdocs.org/sdr/MALA050611), Jul 26, 2005: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FLANGE IS CORRODED ON RT SIDE BETWEEN FS 272 AND FS 288. DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53102. REF: EAMS WORK ORDER 212675, TASK 2525.
- [SDR MALA050606](https://openairdocs.org/sdr/MALA050606), Jul 25, 2005: ACCESS PANEL. DENTED. LT FLAP ACCESS PANEL 541AT IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO NR S57060. REF: EAMS WORK ORDER 212675 TASK 5504.
- [SDR MALA050608](https://openairdocs.org/sdr/MALA050608), Jul 25, 2005: SEAT TRACK. CORRODED. SEAT TRACK AT FS640 AND BL 0 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR S53079.
- [SDR MALA040868](https://openairdocs.org/sdr/MALA040868), Nov 18, 2004: BATTERY PACK. INOPERATIVE. DURING TAWS INSPECTION, FOUND EMERGENCY LIGHT ASSOCIATED WITH POWER SUPPLY 24LN INOP. BATTERY PACK IN POWER SUPPLY 24LN INOP. MAINTENANCE REMOVED AND REPLACED E
- [SDR MALA040867](https://openairdocs.org/sdr/MALA040867), Nov 18, 2004: SKIN. DENTED. DURING LC2 INSPECTION, NOTED STABILIZER L/E, FOUND DENT ON UPPER SKIN OF RT HORIZONTAL STAB. DIAMETER OF DENT IS 1.875 INCH DEPTH IS .057. DENT IS 3.875 INCH AF
- [SDR MALA040881](https://openairdocs.org/sdr/MALA040881), Nov 18, 2004: BATTERY PACK. INOPERATIVE. BATTERY PACK P/N 61-0478-9, S/N 70 WILL NOT LIGHT REQUIRED EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY CELL PACK P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETUR
- [SDR MALA040654](https://openairdocs.org/sdr/MALA040654), Oct 6, 2004: POWER SUPPLY. INOPERATIVE. EMERGENCY FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED POWER UNIT IAW MM, ALL CHECKS GOOD. P/N ON & OFF P4-01-004. REMOVED FROM DMR, MAINTENANCE NOTIFIED.
- [SDR MALA040576](https://openairdocs.org/sdr/MALA040576), Sep 14, 2004: TRANSCEIVER. FAILED. RADAR STABILIZATION APPEARS TO BE INOPERATIVE RADAR RETURNS ARE DISTORTED WHEN AIRCRAFT PITCH AND OR BANK ANGLE IS ALTERED. WX RADAR FAILED INFLIGHT. AIR RETURN
- [SDR MALA040519](https://openairdocs.org/sdr/MALA040519), Aug 11, 2004: COMPUTER. MALFUNCTIONED. ON POWER UP C/BS F12 & F11 POPPED. TRIED RESETTING & POWERING UP ON INVERTER NR 2 THEN F11 POPPED. CAPT'S SIDE AVIONICS FAILED TO INITALIZE. AFTER RESETTING ALL
- [SDR MALA040439](https://openairdocs.org/sdr/MALA040439), Jun 5, 2004: SOCKET. LOOSE. WHEN L/P BLEED IS CLOSED RIGHT BLEED CLOSED LIGHT DOES NOT ILLUMINATE, THOUGH MASTER CAUTION LIGHT AND CWP A/C LIGHT DO ILLUMINATE. LAMPS CHECK GOOD ON RIGHT BL
- [SDR MALA040421](https://openairdocs.org/sdr/MALA040421), May 28, 2004: SIGN. MISSING. EXIT SIGN ABOVE SEAT 6A IS MISSING. MAINTENANCE REPLACED MISSING COVER WITH SERVICEABLE ONE AS NEEDED. SECURITY CHECKS GOOD.
- [SDR MALA040397](https://openairdocs.org/sdr/MALA040397), Apr 30, 2004: SKIN. DENTED. DURING 4K INSPECTION IN LCQ, BS 362 LT FUSELAGE HAD DENTS. CUT OUT DENTED, FABRICATED, LOCATED, DRILLED AN EXTERNAL DOUBLER REPAIR IAW MESABA EO NR S53009. REFE
- [SDR MALA040398](https://openairdocs.org/sdr/MALA040398), Apr 30, 2004: SKIN. DENTED. DURING 4K INSPECTION IN LCQ, FS 364 RT FUSELAGE HAS DENTS. CUT OUT DENTED AREA FABRICATED, LOCATED DRILLED AND INSTALLED AN EXTERNAL DOUBLER REPAIR IAW EO NR S5
- [SDR MALA040396](https://openairdocs.org/sdr/MALA040396), Apr 30, 2004: FLOORBEAM. CRACKED. DURING 4K INSPECTION IN LCQ, FS 363.0 FLOORBEAM CRACKED. CUT OUT DAMAGED AREA OF FLOORBEAM, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW EO NR S53108. R
- [SDR MALA040395](https://openairdocs.org/sdr/MALA040395), Apr 30, 2004: SEAT TRACK. CORRODED. DURING 4K INSPECTION IN LCQ, FS 294-319 RT IB SEAT TRACK CORRODED. REMOVED AND REPLACED RT IB SEAT TRACK FROM FS 294-FS 319 IAW MESABA EO NR S53060. REFER TO LG
- [SDR MALA040409](https://openairdocs.org/sdr/MALA040409), Apr 24, 2004: BATTERY. DISCHARGED. ELT REMAINS ON PN 95210000-20, SN/0343. UNIT WAS FOUND TO HAVE NO TROUBLE . UNIT WAS FOUND TO HAVE NO THROUGH. MAINTENANCE REPLACED BATTERY DUE TO DISCHARGED ST
- [SDR MALA040220](https://openairdocs.org/sdr/MALA040220), Mar 2, 2004: SEPARATOR. DAMAGED. RIGHT INTAKE LIGHT ILLUMINATES AFTER 15 MINUTES AND STAYS ON. AIR RETURN TO MSP. REPLACED RIGHT WHITE HARNESS P/N 7292533-602, NO HELP. REMOVED AND REPLACED RT 
- [SDR MALA030363](https://openairdocs.org/sdr/MALA030363), Jul 31, 2003: TRANSDUCER. LEAKING. DURING FLIGHT CREW NOTED LT ENGINE OIL PRESSURE CONTINUALLY DROPPING INFLIGHT. RED WARNING LIGHT WAS ON. SHUTDOWN ENGINE AND DIVERTED TO SDF. MAINTENANCE FOUND 
- [SDR MALA030268](https://openairdocs.org/sdr/MALA030268), May 15, 2003: DOWNLOCK SWITCH. MALFUNCTIONED. ON FINAL APPROACH WITH GEAR SELECTEDDOWN THERE WAS NO RT MAIN GREEN LIGHT INDICATION. THERE WAS NO AMBER DIWSAGREEMENT LIGHT. A GO-AROUND WAS INITIATED. WHEN FL
- [SDR MALA020669](https://openairdocs.org/sdr/MALA020669), Nov 20, 2002: FRAME. CORRODED. DURING 6Y/4Y INSPECTION IN CWA, FOUND TOP FLANGE ON BOTTOM FRAME AT STA 294 LBL 18.3 HAS CORROSION OUT OF LIMITS. MAINTENANCE COMPLETED REPAIR IAW EO S53108. A/
- [SDR MALA020658](https://openairdocs.org/sdr/MALA020658), Nov 20, 2002: SEAT TRACK. CORRODED. DURING 6Y/4Y INSPECTION IN CWA, NOTED LT FWD SEAT TRACK LBL 18.3 HAS HEAVY CORROSION. MAINTENANCE COMPLETED REPAIR BETWEEN STA 297-329 IAW EO S53060. A/C RELEAS
- [SDR MALA020659](https://openairdocs.org/sdr/MALA020659), Nov 19, 2002: SEAT TRACK. CORRODED. DURING 6Y/4Y INSPECTION IN CWA, SEAT TRACK CORROSION IN CARGO AREA. MAINTENANCE COMPLETED SEAT TRACK SPLICE REPAIR IAW EO S53060 AT BL 0 STA 619.138 - 686.888. 
- [SDR MALA020657](https://openairdocs.org/sdr/MALA020657), Nov 18, 2002: SKIN. CHAFED. DURING 6Y/4Y INSPECTION IN CWA, CHAFING DAMAGE TO LT INBOARD NACELLE SKIN CAUSED BY WING LEADING EDGE FAIRING SEAL. MAINTENANCE COMPLETED REPAIR IAW EO S54053. 
- [SDR MALA020670](https://openairdocs.org/sdr/MALA020670), Nov 13, 2002: WEB. CORRODED. DURING 6Y/4Y INSPECTION IN CWA, WEBBING AT STA 288 HAD 294 HAS CORROSION. MAINTENANCE INSTALLED WEBBING AT STA 288 AND 294 IAW SF340 AMM SRM 51-40-21 AND MAL EO
- [SDR MALA020656](https://openairdocs.org/sdr/MALA020656), Nov 12, 2002: SEAT TRACK. CORRODED. DURING 6Y/4Y INSPECTION, SEAT TRACK BL 0, STA 297-348 HAS CORROSION. MAINTENANCE COMPLETED SEAT TRACK REPAIR SPLICE IAW EO 53060. A/C RELEASE DATE 11/20/02.
- [SDR MALA020638](https://openairdocs.org/sdr/MALA020638), Nov 5, 2002: DOWNLOCK SWITCH. DURING APPROACH OF FLIGHT #3189 TO BRD, THE RIGHT MAIN GEAR DIDN'T ILLUMINATED. WE PUSHED THE TEST SWITCH AND THE LIGHTS ALL TESTED OKAY ON GO-AROUND THE RIGHT 
- [SDR MALA020602](https://openairdocs.org/sdr/MALA020602), Oct 6, 2002: AIRSTAIR. MALFUNCTIONED. ON FLIGHT NR 3260, AIR STAIR WOULD NOT COME DOWN, LOCKED IN THE UP POSITION. MAINTENANCE CHECKED DOOR OPERATION SEVERAL TIMES, COULD NOT DUPLICATE. RETURNED TO 
- [SDR MALA020587](https://openairdocs.org/sdr/MALA020587), Sep 27, 2002: SWITCH. MALFUNCTIONED. DURING FLIGHT 2768, RT OIL PRESSURE LIGHT ILLUMINATED ON CWP. ENGINE PRESSURE AT 75 PSI PROP OIL AT 80 PSI, BOTH CONSISTENTLY AT THOSE PRESSURES. AIR RETURN TO 
- [SDR MALA020302](https://openairdocs.org/sdr/MALA020302), May 23, 2002: COMPUTER. FAILED. DURING CRUISE CREW RECEIVED AN AVIONICS CAUTION ROLL COMPARITOR FLAG. FOLLOWED QRH AND ISOLATED RIGHT EADI AS BAD COMPONENT. IN LEVEL FLIGHT EADI SHOWED CLIMBIN
- [SDR REXA01009](https://openairdocs.org/sdr/REXA01009), Jun 12, 2001: ECU. FAULTY. ON SEVEN MILE FINAL INTO MEMPHIS, THE LEFT ENGINE WENT INTO AUTOCOURSEN. TORQUE INDICATION WENT TO ZERO, BUT ALL OTHER INDICATIONS WERE NORMAL. THE FLIGHT CREW 
- [SDR REXA98051](https://openairdocs.org/sdr/REXA98051), Feb 12, 1998: CIRCUIT BREAKER. TRIPPED. OUTSIDE AIR TEMP INOP. LIGHT CAME ON IN FLIGHT. RESET CIRCUIT BREAKER, NO FIX. PERFORMED GROUND RUNS AT HIGH POWER SETTINGS FOR 15 MIN. COULD NOT DUPLICATE. (M)
- [SDR REXA98045](https://openairdocs.org/sdr/REXA98045), Feb 4, 1998: CONDITION LEVER. OUT OF ADJUST. LEFT PROP RPM BELOW 1000, AND TORQUE VERY SLOW TO RISE ON TAKEOFF ROLL. RERIGGED LEFT CONDITION LEVER AT SECTOR PULLEY. GROUND RUN AND CTOT CHECKS GOOD. (M)
- [SDR REXA98036](https://openairdocs.org/sdr/REXA98036), Jan 24, 1998: CTOT. MALFUNCTIONED. LEFT CTOT WOULD NOT HOLD. CREW DID ANOTHER P-3 TST. OPS CHECK GOOD. TRIED ANOTHER T/O OPS CHECK GOOD. (M)
- [SDR REXA98022](https://openairdocs.org/sdr/REXA98022), Jan 20, 1998: SMOKE DETECTOR. FAILED. AVIONICS SMOKE ILLUMINATED ON CWP DURING CLIMB-OUT, RETURNED TO PFN. REMOVED AND REPLAED AVIONICS SMOKE DETECTOR. OPS CHECK GOOD. (M)
- [SDR REXA97029](https://openairdocs.org/sdr/REXA97029), Feb 14, 1997: BATTERY. DISCHARGED. ALL EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL 5 EMERGENCY LIGHT BATTERIES. CHECK OK, GOOD FOR SERVICE. (M)
- [SDR REXA97022](https://openairdocs.org/sdr/REXA97022), Feb 8, 1997: CONNECTOR. LOOSE. AVIONICS SMOKE LIGHT ON GROUND. DEFERRED PER MEL 26-13-03. CLEARED DEFERRAL BY RE-RACKING CANNON PLUG ON SMOKE DETECTOR. (M)
- [SDR REXA96067](https://openairdocs.org/sdr/REXA96067), Oct 31, 1996: PDU. FAILED. LEFT MAIN AND ESS BUS BREAKER POPS INTERMITTENTLY. REMOVED AND REPLACED LEFT PDU. OPS CHECK GOOD. AC OK FOR SERVICE. (M)
- [SDR REXA96053](https://openairdocs.org/sdr/REXA96053), Oct 18, 1996: TEMP BULB. SHORTED. LT PGB OIL TEMPERATURE ENTERED RED ARC. FERRIED TO MEMPHIS. REMOVED AND REPLACED TEMP BULB. (M)
- [SDR REXA96037](https://openairdocs.org/sdr/REXA96037), Aug 28, 1996: BATTERY. DISCHARGED. EMERGENCY LIGHTS 58 LN, 59 LN, 60 LN, 41 LN, AND 39 LN ARE OUT. REMOVED AND REPLACED LIGHT BATTERIES AT LOCATIONS, 23LN, AND 24LN, S/N ELB071, ELB092. OPERATION
- [SDR REXA96029](https://openairdocs.org/sdr/REXA96029), Jun 16, 1996: FIRE BOTTLE. DEPLETED. CARGO SMOKE INDICATION AIRBORNE, NO INDICATION OF COMBUSTION WHEN INSPECTED ON GROUND. CARGO FIRE BOTTLE DEPLETED, DEFERRED DM14773. CLEANED CANNON PLUG AND INS

## FAA accident and incident reports (1)

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 19960616021649I](https://openairdocs.org/incident/19960616021649I), Jun 16, 1996: Saab SF340A (N370PX), Columbus, GA. Narrative: the cargo smoke indication was noted during cruise flight shortly after takeoff. As a result of the fire, extinguisher was fired, and the crew…

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