HI924 - 1991 BELL 212

1991

BELL

212

35046

HI924

Used

17891.8

Yes

The Helicopter Registration, Airworthiness Certificates, Pilots Operating Handbook (POH), Weight and Balance, and Equipment List are all located in the helicopter. Exterior Paint Condition: Paint is in excellent condition with a wet look and high shine. Skids are in very good condition

3988.5

1200.3

576.2

Tail Rotor

4169.1

3544.5

Main Rotor Blade - 3,988.5 Hrs Remaining Main Rotor Blade - 1623.1 Hrs Remaining Tail Rotor Blade - 4,169.1 Hrs Remaining Tail Rotor Blade - 3,778.7 Hrs Remaining

PRATT & WHITNEY

PT6T-3B

CP-PS-TB0344

2000

3170.9

SNEW

4000

• Time Since Repaired: 579.3 Hrs • Compressor Serial No: 4T470 • 2ND Stage Compressor Disk Cycles Remaining: 22,614 Cycles • 3RD Stage Compressor Disk Cycles Remaining: 22,614 Cycles • Impeller (Centrifugal) Cycles: 22,614 Cycles • Power Turbine Disk Cycles/Hours Remaining: 9,320.4 Hrs / 44,826 Cycles • Compressor Turbine Disk Remaining: 1780.7 Hrs • Manual Fuel Control Time Remaining: 1331.5 Hrs • Solenoid Valve Time Remaining: 1331.5 Hrs • Fuel Pump Time Remaining: 1331.5 Hrs • Oil to Fuel Heater Time Remaining: 1331.5 Hrs • Bleed Valve Time Remaining: 1331.5 Hrs • Flow Divider Time Remaining: 1331.5 Hrs Performed Hot Section Inspection at TTSN: 2591.6 TCSN: 5762

PRATT & WHITNEY

PT6T-3B

CP-PS-TB0388

2000

1616.1

SNEW

4000

• Time Since Repaired: 735.6 • Compressor Serial No: YUAA004A761 • 2ND Stage Compressor Disk Cycles Remaining: 26,602 Cycles • 3RD Stage Compressor Disk Cycles Remaining: 26,602 Cycles • Impeller (Centrifugal) Cycles: 26,602 Cycles • Power Turbine Disk Cycles/Hours Remaining: 13,383.9 Hrs / 54, 602 Cycles • Compressor Turbine Disk Remaining: 8383.9 Hrs • Manual Fuel Control Time Remaining: 2883.9 Hrs • Solenoid Valve Time Remaining: 2883.9 Hrs • Fuel Pump Time Remaining: 2883.9 Hrs • Oil to Fuel Heater Time Remaining: 2883.9 Hrs • Bleed Valve Time Remaining: On Condition • Flow Divider Time Remaining: 2883.9 Hrs Power Section Assy S/N: CP-PS-TB0388 Hot Section Inspection performed at TTSN: 880.5 Hrs TCSN 1546

Yes

Yes

Yes

Yes

Yes

-Northern Airborne Technology AA38-301 ICS Expansion Panel, -Audio from the Pilot Side Garmin Aera 796 and the Co-Pilot side Garmin Aera 796, -Panel is protected by a 5 amp circuit breaker located in the Airborne Technology Installation and Operation Manual, -Garmin GNS-530W GPS/NAV/COM -Garmin GNS-430W GPS/NAV/COM -Honeywell KR-21 Marker Beacon -Mid-Continent Instrument NAV/GPS Annunciators -Garmin GTX-330 Mode S Transponder -Airborne Technology AMS43 Audio Control Panel -Garmin GMX-200 MFD.

Yes

Yes

Yes

I. STC SR01634SE Supplemental Lightning System. II. STC SR02289LA Wire Strike Protection System, P/N: 647.3704. III. STC SR00646AT Aeronautical Accessories High Skid Gear Forward Crosstube. IV. STC SR00713SE Onboard System Cargo Hook Suspension System, P/N: 200-089-22. V. STC SH3189SO Aeronautical Accessories Goodrich Hoist Provisions, P/N 412-140-100. VI. STC SR02297LA Nose Utility Mount, P/N AF412NM-006, For the Spectrolab SX-16 Nightsun Searchlight System. VII. STC SR01446NY Dart Aerospace Door Roller Kit, Right Hand Kit, P/N: D412-698-012 and Left Hand Kit, P/N: D412-698-011 VIII. Installed wiring Provisions for the Installation of a Spectrum Aeromed Interior P/N SP-KT-41

2018

Hinged and Sliding

Paint is in excellent condition with a wet look and high shine

Passenger / Utility