1981 AGUSTA BELL 412

AIRCRAFT CHARACTERISTICS AND STATUS

REGISTRATION I-GONI SERIAL NUMBER 25506 YEAR OF CONSTRUCTION 1981 ENGINE Type XXX1 Pratt & Whitney PT6T-3B ENGINE #1 s/n CP-PS TB0387 ENGINE #2 s/n CP-PS TB0386 AIRFRAME TOTAL TIME 10214 ENGINE 1 TOTAL TIME 1399 ENGINE 2 TOTAL TIME 1647 P&W GEARBOX TSO 378 AVAILABLE IMMEDIATELY

AVIONICS

The Helicopter is certified for IFR flights with 3 axis autopilot and the avionics installed includes:

• VHF/COM 1 KTR 905 • VHF/COM 2 KTR 905 • AUDIO SYSTEM NAT • PUBBLIC ADDRESS PROVISION • 2 CABIN AUDIO SELECTOR • FM TACTICAL RADIO NAT • NAV 1 KNR 634 • NAV 2 KNR 634 • WHEATHER RADAR RT 1401 • RADIO ALTIMETER KRA405 • TRANSPONDER KXP 755 • AIR DATA SYSTEM – ANALOGUE • GYRO COMPASS SYSTEM • HF PROVISION • ADF KDF806 • DME KDM-706A • ELT KANNAD 406AF

OPTIONALS

• AP/AFCS SPZ-412 • WINDSHIELDS • AUX FUEL TANK PROVISIONS • CARGO HOOK • UTILITY CONFIGURATION + VIP INTERIORS (5 PLACE) • POP OUT WINDOWS • EMERGENCY FLOAT • WSPS • HOIST PROVISIONS • EXT LOUD SPEAKER PROVISIONS • UMS – ALTAIR • SMARTCYCLE

MAIN COMPONENTS TIME

Airframe P/N Consumed

HRS Remaining

HRS TBO HRS

Remaining

Tail Rotor Blade #1 212-010-750-113 3136 1864 5000

37% %

Tail Rotor Blade #2 212-010-750-113 968 4032 5000

81% %

M/r Blade 412-015-300-109 374 2126 2500 85% %

M/r Blade 412-015-300-109 1429 1071 2500 43% %

M/r Blade 412-015-300-104 1221 1279 2500 51% %

M/r Blade 412-015-300-104 1221 1279 2500 51% %

M/r Yokes 412-010-101-129 4418 582 5000 12% %

M/r Spindles 412-010-190-103 8110 1890 10000 19% %

M/r Spindles 412-010-190-103 1331 8669 10000 87% %

M/r Spindles 412-010-190-103 7617 2383 10000 24% %

M/r Spindles 412-010-190-103 6751 3249 10000 32% %

M/r pitch horn 412-010-149-111 258 9742 10000 97% %

M/r pitch horn 412-010-149-111 258 9742 10000 97% %

M/r pitch horn 412-010-149-111 1364 8636 10000 86% %

M/r pitch horn 412-010-149-111 8458 1542 10000 15% %

M/r Mast assy 412-040-366-105 1708 3292 5000 66% %

Main Rotor Head 412-010-100-193 377 2123 2500 85% %

Hub and sleeve assy 412-010-401-105 1945 555 2500 22% %

Swashplate & Support

assembly 412-010-402-101 1221 1279 2500 51% %

Main Transmission 412-040-002-103 1708 4292 6000 72% %

Intermediate Gearbox 212-040-003-23 557 4443 5000 89% %

Tail Rotor gear box 212-040-004-9 2020 2980 5000 60% %

Tail Rotor hub 212-010-701-125 583 1917 2500 77% %

Main Servo #1 212-076-005-x 2500 0 2500 toll %

Main Servo #2 212-076-005-x 378 2122 2500 85% %

Main Servo #3 212-076-005-x 2500 0 2500 toll %

Twin-Pack Gearbox 3024780 378 3622 4000 91% %

Engine #1 PT6T-3B 1399 2601 4000 65% %

Engine #2 PT6T-3B 1647 2353 4000 59% %

Starter Generator #1 209-060-221-001 494 506 1000 51% %

Starter Generator #2 209-060-221-001 44 956 1000 96% %