1991 BELL 212

1991

BELL

212

35046

Used

VFR

MDJB

17891.8

Yes

The Helicopter Registration, Airworthiness Certificates, Pilots Operating Handbook (POH), Weight and Balance, and Equipment List are all located in the helicopter. This Helicopter has been maintained according to Bell Helicopter Maintenance Manual Service Bulletin Status: According to maintenance tracking reports and Alert Service Bulletin List all service bulletins are current. AD's Complied With: Records report all AD’s are in compliance 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 #1; 1623.1 hrs remaining Main rotor blade #2; 3988.5 hrs remaining Main rotor hub; 1200.3 hrs remaining Swashplate & Support; 598.1 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 Power Section Assy S/N: CP-PS-TB0344 was Repaired in accordance with current Manufacturer Specifications & F.A.R. regulations of the F.A.A. 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 Power Section Assy was repaired in accordance with current manufacturer Specifications

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 SX16 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

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

2018

Hinged and Sliding

TBO upon requirement

Yes