N848EX

Cancelled 2006

Deregistered aircraft · 1992 Dehavilland DHC-8-106 · Pratt & Whitney Canada PW121

Cancelled
November 3, 2006
Exported to
Canada
Status when cancelled
Triennial form not returned
Serial number
331
Year built
1992
Type
Fixed wing multi engine
Engine
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
Owner type
Non-citizen corporation

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.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N848EX and the event date: up to this one’s cancellation.

Service difficulty reports · 10

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

SDR HNAA0500040Actuator · misriggedNOSE 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.Apr 19, 2005 · N848EX · Dhav DHC8102 · Landing Gear ActuatorSDR PCAA0403176Tire · failedFLIGHT 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 FLIGHT. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED FOR EMERGENCY. AIRCRAFT WILL BE INTERIMar 1, 2004 · N848EX · Dhav DHC8102 · TireSDR PCAA0311137Structure · crackedFLIGHT 3555, INTO NEWBURG NEW YORK EXPERIENCED GEAR UNSAFE LIGHT ILLUMINATION WHEN GEAR SELECTED DOWN. THE GEAR WAS CYCLED, STILL NO CHANGE. CREW THEN COMPLIED WITH ALTERNATE EXTENSION PROCEDURES. AIRCRAFT FERRIED INTO MIDDLETOWN WHERE UPON FURTHER INVESTIGNov 7, 2003 · N848EX · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR PCAA0310128Eec · faultyAIRCRAFT 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 DID NOT ASSUME THE BRACE POSITION. MAINTENANCE GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE. MAINTENOct 26, 2003 · N848EX · Dhav DHC8102 · Fuel Controlling SystemSDR PCAA0209111Engine · false indicationSYR-BOS FLIGHT#3848. CREW REPORTED #1 ENGINE OIL PRESSURE INDICATION WENT TO ZERO, ENGINE SHUT DOWN AS A PRECAUTION. EMERGENCY DECLARED, AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND CIRCUIT BREAKER K5 POPSep 23, 2002 · N848EX · Dhav DHC8102 · Engine Oil PressureSDR PCAA0111132Window · crackedALB- FLIGHT#3512. CREW REPORTED TWO ONE INCH CRACKS NEAR LOWER EDGE MOUNTING BOLT ON FIRST OFFICERS SIDEWINDOW. MAINTENANCE REPLACED FIRST OFFICERS SIDE WINDOW IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETURNED TO SERVICE.Nov 2, 2001 · N848EX · Dhav DHC8102 · Flight Compartment WindowsSDR PCAA0111152Link · wornDURING 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 PINS IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. SERVICED STRUT AS REQUIRED IN ACCORDOct 26, 2001 · N848EX · Dhav DHC8102 · Nose/Tail Landing Gear Strut/AxleSDR PCAA0108104Rivet · missingDURING 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 RIVETS ON INSPECTION PANEL REPLACED IN ACCORDANCE WITH DER CALLAHAN REPAIR SERVICES 8110 FORM CASAAAug 31, 2001 · N848EX · Dhav DHC8102 · Nacelle/Pylon, Main FrameSDR PCAA0009064Engine · fluctuatesFLIGHT 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 PLANE RETURNED TO FIELD. NO EMERGENCY WAS DECLARED, PAX DEPLANED. NR 2 ENGINE OIL SERVICED WITH 4Sep 22, 2000 · N848EX · Dhav DHC8102 · Turbine Engine Oil SystemSDR PCAA0001004Skin · crackedBGM - 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. AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2000 · N848EX · Dhav DHC8102 · Rudder, Plate/Skin