N2251Z
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
18 reports on file, 1995-07-06 – 1999-02-22.
Part: FLOAT — DAMAGED (MLG)
FLOAT BAG ASSEMBLY HAS HOLE IN RIGHT HAND CHAMBER.
Earlier reports · 1995–1998 · 17 reports
1998
Part: INDICATOR — STUCK (TOT)
INDICATOR INTERMITTENTLY STICKS AT ZERO.
Part: INDICATOR — FAILED (COCKPIT T&B)
T&B INDICATOR IS NOT WORKING.
Part: AIRSPEED IND — DEFECTIVE (COCKPIT)
AIRSPEED INDICATOR RANGE MARKINGS ARE FADED.
Part: TACH GENERATOR — FAILED (ROTOR)
TACH GEN HAS NO ROTOR NEEDLE INDICATION.
Part: COMPASS — DEFECTIVE (COCKPIT)
COMPASS [24 VOLT] IS OUT OF LIMITS.
1997
Part: INDICATOR — FAILED (ENG OIL)
INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DID NOT WORK. SCRAPPED INDICATOR AND REPLACED WITH SERVICEABLE PART.
Part: ACTUATOR — FAILED (DROOP COMP)
ACTUATOR DOES NOT MOVE IN OR OUT.
Part: INDICATOR — INOPERATIVE (COCKPIT TOT)
TOT INDICATOR INOPERATIVE.
Part: TACH GEN — WORN (M/R)
TACH GEN WORN SHAFT COUPLING SPLINES.
Part: RESTRAINT — WORN BEARING (TRANSMISSION)
TRANSMISSION RESTRAINT WORN BEARINGS.
Part: SKID TUBE — CRACKED (RT SKID)
SIX LONGITUDINAL CRACKS IN SKID TUBE ITSELF. SKID TUBE WAS MANUFACTURED 8-95.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)
TRANSCEIVER DEFECTIVE. SOME NUMBERS WERE NOT READABLE.
1996
Part: HANGAR BRACKET — MIS MFG (FUSELAGE)
BRACKET IS TOO WIDE. DOES NOT FIT INTO BELL APPROVED FIXTURE S/N 0116 AFTER MODIFICATION OF SUPPORTS AS PER PRODUCT SUPPORT CANADA.
Part: LINK ASSY — WORN EXCESS (XMSN MOUNT)
WORN BEARING.
Part: NOZZLE — CRACKED (1ST STAGE)
ENGINE REMOVED DUE TO CRACKED FIRST STAGE NOZZLE AND LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: EXCESSIVE RUN OUT (.007) BEYOND SERVICEABLE LIMITS ON #2 NOZZLE TIP PATHS. REPLACED DISCREPANT PART.
Part: FRAME — CRACKED (TAILBOOM)
PART IS CRACKED. L/H UPPER T/B FITTING CRACKED P/N 206-031-329-003. TAILBOOM MOUNT FRAME P/N 206-032-308-103S CRACKED AT UPPER L/H MOUNT HOLE. REPLACED FITTING UPPER L/H SIDE WITH 206-031-329-103S AND REPLACED T/B FRAME WITH P/N 206-032-308-103S.
1995
Part: TRANSCEIVER — INOPERATIVE (COCKPIT)
INOPERATIVE. WONT IDENT. REPLACED TRANSISTOR Q415. REPAIRED. REPLACED DETERIORATED RESISTOR R477. INSTALLED HEATSINK BEHIND TRANSISTOR Q415. ADJUSTED FREQUENCY AND POWER OUT TO SPECS. BENCH CHECK GOOD.