Bell 412 IFR
1983 FOR LEASE

Exterior

SPECIFICATION

Date of Manufacture: 1983
Total Airframe Hours: 9,476


Optional Equipment

Rotor Brake Wire Strike Protection System
Exhaust Deflectors SX16 Night Sun Provisions
Pop-out Cabin Windows Emergency Float Provisions
Bleed Air Heater 90 Gallon Auxiliary Fuel Tank
High Skid Gear & Flitestep External Hoist Provisions
Exterior

Avionics

GPS/Nav/Com Garmin GNS 530W
GPS/Nav/Com Garmin GNS 430W
Multi Function Display Avidyne EX 600
Transponder Garmin GTX 327
ADF King KDF 800
Rad Alt .
DME .
Weather Radar .
HF Codan 9233
ELT Kannad 406
VHF Homer .
UHF x2 Nokia Phone Kit
Rader Altimeter 3 Axis Autopilot
3 Axis Autopilot TM 8200 VHF x 2 + portable provisions
HSI x2 SFIM
CDI x2 King KY 196A
ADI x2 Garmin GNS 430
Clock EFIS 40
ASI x2 King KR 87
VSI x2 King KN 63

Exterior
White with black upper tailboom

Exterior

Interior
VIP leather upholstery.

Component Status
(as at 9,476 airframe hours)

PROVISIONAL AND PROJECTED

Item Life Hours Remaining
Main Rotor Blade OC (2,500 I) 2,485 I
Main Rotor Blade OC (2,500 I) 2,485 I
Main Rotor Blade OC (2,500 I) 2,485 I
Main Rotor Blade OC (2,500 I) 2,485 I
Main Transmission 6,000 (3,000 I) 5,985
Main Rotor Hub Assembly 2,500 2,485
Main Rotor Yoke Assembly (x2) 5,000 3,946 (x2)
Spindle & Damper Bearing (x4) 10,000 7,845/7,012/5,222/6,245
Pitch Horn ( 4) 10,000 7,570/5,038/5,181/9,985
M/R Fitting (x4) 5,000 3,946 (x4)
M/R Damper Bridge - Upper (x4) 15,000 10,446/8,951 (x3)
M/R Damper Bridge - Lower (x4) 10,000/180 M 9,985 (x 2)/3,951 (x2)
Splined Plate Assembly 10,000/80,000 RIN 8,666/53,609 RIN
Mast Cap Assembly 10,000 9,985
Arm (x8) 5,000 4,382 (x2)/4,415/2,029/4,985 (x4)
Bracket (x8) 10,000 3,951 (x7)/7,208
Swashplate & Support Assembly 2,500 2,485
Swashplate Support 5,000 2,394
Drive Link Assembley (x2) 5,000 4,985 (x2)
Swashplate Link Assembley (x2) 5,000 4,985 (x2)
Rephasing Lever (x4) 5,000 2,202 (x2)/1,915/2,681
Mast Assembly 5,000 (3,000 I) 4,985
Mast Tube 10,000 (60,000 RIN) 9,985 (60,000 RIN)
Rotor Brake Quill 2,500 2,485
Collective Lever 10,000 8,692
Hub and Sleeve Assembly 2,500 2,485
Collective Sleeve 9,000 1,371
Scissors Drive Hub 10,000 9,985
Drive Shaft Assembly 2,500 2,485
Tail Rotor Blade 5,000 2,015
Tail Rotor Blade 5,000 2,015
Tail Rotor Yoke 5,000 3,069
Tail Rotor Hub Assembly 2,500 2,485
90 Gearbox 5,000 4,985
42 Gearbox 5,000 4,985
Main Servo 2,500 2,485
Main Servo 2,500 2,160
Main Servo 2,500 2,061

Engines Life Hours Remaining
No.1 No.2
Engine 4,000 3,985 3,985
Comp 1st Stage 15,000 C 10,003 C 4,493 C
Comp 2nd Disc 22,500 C 16,414 C 9,216 C
Comp 3rd Disc 28,000 C 22,149 C 8,897 C
Centrifugal Impeller 29,000 C 23,149 C 9,893 C
Comp Turbine Disc 10,000 C 4,266 C 4,640 C
Power Turbine Disc 15,000 C 10,003 C 4,493 C
Fuel Pump 4,500 4,485 4,485
Oil to Fuel Heater 4,500 4,485 4,485
Auto FCU 6,000/6 Yr 5,985 5,985
Manual FCU 4,500 4,485 4,485
Flow Divider Valve 4,500 4,485 4,485
Governor 4,500 4,485 4,485
Combining Gearbox 4,000 3,350
Torque Control Unit 4,500 4,485

3,000 hour/5 year inspection completed at 9,461 hours.