Attachment 1.pdf

C-12B/F “Huron” Configuration

General Description: The Navy C-12B/F is a military version of the Beechcraft BE200

KingAir. It is an all–metal, low-wing, twin turbo prop, T-tail monoplane with an axial flow engine mounted on each wing. Fully pressurized, FAA certified aircraft capable of carrying up to 10 people (crew included) and/or cargo up to the maximum airframe weight of 13,500 lbs. (restricted).

Cockpit Instrumentation: The cockpit should be designed to closely represent the actual setup. Depictions can be found in the NATOPS Manual (*see note below) NAVAIR 01-

C12AAA-1 Change 2 figs. 2-2, 2-3,2-4 are excellent depictions and should be used as references.

• * REF (1) Note the C-12 Bravo NATOPS NAVAIR 01-C12AAA-1 and C-12F

NATOPS NAVAIR 01C12FFF-1 manuals will be combined as soon as the NATOPS

CNO office can have them printed.

Engines: PT6A-41 (B) / PT6A-42 (F) have a three-stage axial, single stage reaction turbine. The power turbine two-stage reaction turbine counterrotating with the compressor turbine drives the output shaft.

Engine instruments: ITT, Torque and Propeller Tachometers, Fuel Flow, Oil pressure/Oil Temperature indicators are vital and should be matched closely to ref (1).

Electrical system: 28 VDC. 115 / 26 VAC. Starter/Generators: (2) 250amp 27.5 - 29

VDC. Inverters: (2) 110 - 120 VAC 390-410 Hz. 11 buses (B), 12 (F). Battery is 24V /

34 Amps. Ground Power receptacle right wing requires 30 VDC Max, 300 amps cont.

Avionics

Navigation:

• 2 VOR/LOC/GS receivers receive and interpret VOR and LOC signals in the freq.

range 108.00-117.95MHZ 160 VOR channels, 40 localizer channels and 40 glideslope channels. VIR-30 (B), VIR-32 (F)

• DME indicator: DME-42 (F)

• 1 TACAN receiver: SANS-706 (B/F)

• Altimeter: VG-14A (B/F)

• RAD ALT: AA-200 (B), AA-300 (F)

CACT UC-12 RFP N6134024R0013 ATTACHMENT 1 UC-12 BFM AC DESCRIPTION

• Flight Director / Autopilot: SPZ-200A (B), SPZ-4000 (F)

• 1GNS/FMS receiver: 9002M

• 1 ADF receiver: ADF-60 (B/F)

• Radar: Primus 30 (B), Primus 300SL w/ Data Nav (F)

• Transponder: TDR-90 (B), APX-100 (F)

• GPWS

Communications:

• 2 VHF receiver/transmitters: VHF-20B (B), VHF-22B (F)

• 1 UHF receiver/transmitter: ARC-164

• 1HF receiver/transmitter: HF-718U (B), KHF-950 (F)

• Voice Recorder: CDR Voice

• 2 PRC-90 handheld radios.

Upgrades

The delivery dates on the following upgrades are not certain, however they should be given due consideration in a simulator contract for the future C-12 B/F developments.

• Enhanced GPWS Allied Signal Model Number

• Digital Weather Radar RDR 2000 Allied Signal Bendix/King

• Electronic Flight Instrumentation EFS 40/50 allied Signal Bendix/King

• TCAS / TCAS II Traffic Collision and

Avoidance system TCAS 2000

C-12M “Huron” Configuration

General Description: The Navy C-12M is a military version of the Beechcraft BE200

Kingair. It is an all –metal, low-wing, twin turbo prop, T-tail monoplane with an axial flow engine mounted on each wing. Fully pressurized, FAA certified aircraft capable of carrying up to 10 people (crew included) and /or cargo up to the maximum airframe weight of 13,500 lbs. (restricted).

Cockpit Instrumentation: The cockpit should be designed to closely represent the actual setup. Depictions can be found in the NATOPS Manual NAVAIR 01-C12MMM-1

Change 1 figs. 2-2, 2-3,2-4 are excellent depictions and should be used as references.

Engines: PT6A-42 have a three-stage axial, single stage reaction turbine. The power turbine two-stage reaction turbine counterrotating with the compressor turbine drives the output shaft.

Engine instruments: TGT, torque, propeller RPM (N2), engine RPM (N1), fuel flow, oil pressure/temperature indicators are vital and should be matched closely to above cockpit figures.

Electrical system: 28 VDC, 115/26 VAC. Starter/Generators (2) 250amp 27.5-29 VDC.

Inverters (2) 110-120 VAC, 390-410 Hz. 13 buses. Battery is 24V, 34 Amps. Ground power receptacle located in underside of the right wing requires 30 VDC Max, 300 amps cont, 1000 amps for 0.1 seconds.

Avionics

Navigation:

• 2 VOR/LOC/GS receivers: receive and interpret VOR and LOC signals in the frequency range 108.00-117.95 MHZ; 160 VOR channels, 40 localizer channels and

40 glideslope channels. KNR-634

• 1 DME: KDA-689

• 1 TACAN receiver: KTU-709

• 2 Attitude Gyros: VG-14A

• 2 Radar Altimeters: AA-300

• 2 Flight Directors/Autopilot: SPZ-400

• 1 GPS/FMS receiver: IEC 9002M

• 2 ADF receivers: KDF-806

• 1 Radar: Primus 650

• 1 Transponder: APX-100

Communications:

• 2 VHF receiver/transmitters: KTR-908

• 1 UHF receiver/transmitter: ARC-164

• 1 HF receiver/transmitter: KTR-953

• 1 Cockpit Voice Recorder

• 1 PRC-90 handheld radios.

Upgrades

Note: By the summer of 2001, the UC-12 community will be going through a flight safety upgrade to improve its avionics capabilities. Improvements include: TCAS II, Enhanced GPWS, new radar, moving map presentation on new MFD, aircrew ICS, and rudder position to empty channel in Flight Data Recorder. More information on these new systems is available on request.

• Enhanced GPWS/TAWS: AlliedSignal MK VII E

• Digital Weather Radar: RDR 2000 AlliedSignal Bendix/King

• Electronic Flight Instrumentation: EFS 40/50 AlliedSignal Bendix/King

• TCAS II Traffic Collision and Avoidance system: TCAS 2000