# N848EX: 1992 Dehavilland DHC-8-106, registration cancelled 2006-11-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 3, 2006
- Exported to: Canada
- Status when cancelled: Triennial form not returned
- Airframe: [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106) (registry code 2809020)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 331
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 27, 2006
- Certificate issued: January 28, 1999
- Last registry action: October 31, 2006
- Mode S code: AB9E0B
- Owner when cancelled: [Bombardier Capital Inc](https://openairdocs.org/faa-owner/BOMBARDIER%20CAPITAL%20INC)
- Location: [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester)
- Owner type: Non-citizen corporation
- Owner's area on the map: 44.5541° N, 73.2255° W: Placed by OpenAirDocs at the center of ZIP code 05446, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N848EX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=848EX
- Page: https://openairdocs.org/deregistered/N848EX-2006-11-03

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 Dehavilland DHC-8-106: https://openairdocs.org/model/dehavilland-dhc-8-106.md

## Service difficulty reports (10)

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

- [SDR HNAA0500040](https://openairdocs.org/sdr/HNAA0500040), Apr 19, 2005: ACTUATOR. MISRIGGED. NOSE GEAR DOOR WILL NOT CLOSE AFTER TAKEOFF, CYCLED GEAR OPS NORMAL. ADJUSTED NOSE GEAR DOOR ACTUATOR ROD END AND ADJUSTED SENSOR GAP. OPS CHECK GOOD.
- [SDR PCAA0403176](https://openairdocs.org/sdr/PCAA0403176), Mar 1, 2004: TIRE. FAILED. FLIGHT 3940 REPORTED EXTENSIVE DAMAGE TO REAR OF NR 2 NACELLE AND LOSS OF NR 2 HYDRAULIC CONTENTS DUE TO THE OUTBOARD RIGHT MAIN TIRE ASSEMBLY EXPLODING DURING 
- [SDR PCAA0311137](https://openairdocs.org/sdr/PCAA0311137), Nov 7, 2003: STRUCTURE. CRACKED. FLIGHT 3555, INTO NEWBURG NEW YORK EXPERIENCED GEAR UNSAFE LIGHT ILLUMINATION WHEN GEAR SELECTED DOWN. THE GEAR WAS CYCLED, STILL NO CHANGE. CREW THEN COMPLIED 
- [SDR PCAA0310128](https://openairdocs.org/sdr/PCAA0310128), Oct 26, 2003: EEC. FAULTY. AIRCRAFT HAD NR 1 ENGINE SHUTDOWN AS A PRECAUTIONARY MEASURE DUE TO NR 1 ENGINE TORQUE FLUXING BETWEEN 50 AND 90 PERCENT. CABIN WAS ADVISED OF EMERGENCY, BUT DI
- [SDR PCAA0209111](https://openairdocs.org/sdr/PCAA0209111), Sep 23, 2002: ENGINE. FALSE INDICATION. SYR-BOS FLIGHT#3848. CREW REPORTED #1 ENGINE OIL PRESSURE INDICATION WENT TO ZERO, ENGINE SHUT DOWN AS A PRECAUTION. EMERGENCY DECLARED, AIRCRAFT RETURNED TO TH
- [SDR PCAA0111132](https://openairdocs.org/sdr/PCAA0111132), Nov 2, 2001: WINDOW. CRACKED. ALB- FLIGHT#3512. CREW REPORTED TWO ONE INCH CRACKS NEAR LOWER EDGE MOUNTING BOLT ON FIRST OFFICERS SIDEWINDOW. MAINTENANCE REPLACED FIRST OFFICERS SIDE WINDOW 
- [SDR PCAA0111152](https://openairdocs.org/sdr/PCAA0111152), Oct 26, 2001: LINK. WORN. DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LOWER LINK BUSHING AND PIN FOUND WORN. REPLACED LINK AND LOWER & UPPER
- [SDR PCAA0108104](https://openairdocs.org/sdr/PCAA0108104), Aug 31, 2001: RIVET. MISSING. DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET WAS FOUND MISSING ON INSPECTION PANEL ON REAR OF RIGHT NACELLE. LOOSE AND MISSING 
- [SDR PCAA0009064](https://openairdocs.org/sdr/PCAA0009064), Sep 22, 2000: ENGINE. FLUCTUATES. FLIGHT 3899 ABE TO BOS. DURING TAKEOFF NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH OIL PRESSURE FLUCTUATING BETWEEN 35 AND 60 PSI. ENGINE WAS SHUTDOWN AND P
- [SDR PCAA0001004](https://openairdocs.org/sdr/PCAA0001004), Jan 13, 2000: SKIN. CRACKED. BGM - DURING A ROUTINE WALK AROUND, THE FORWARD RUDDER WAS FOUND CRACKED AT THE UPPER RIGHT SIDE. MAINTENANCE REPAIRED THE CRACK IAW REPAIR DRAWING 8-55-130. AI

## 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 20031026032209I](https://openairdocs.org/incident/20031026032209I), Oct 26, 2003: Dhav DHC8102 (N848EX), Ithaca, NY. (-23) On October 26, 2003 at 06:48EST a DHC-8-102 operated by allegheny airlines inc, (pcaa), shutdown the #1 engine while climbing out of ith due to the…
- [Incident 20020923029819I](https://openairdocs.org/incident/20020923029819I), Sep 23, 2002: Dhav DHC8102 (N848EX), Syracuse, NY. (-23) On September 23, 2002, allegheny flight 3848 departed Syracuse-Hancock international airport (syr) when the crew reported #1 engine oil pressure…

---
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.