Attachment 1 - TC12B Configuration.doc
DOC document 1 MB Posted
- Solicitation number
- N61339-09-R-0002
About this file
Attachment 1
View the file
Other files
| File | Type | Posted |
|---|---|---|
| N6133909R0002 Amend 0002.zip | ZIP file | |
| N6133909R0002 Amend 0001.zip | ZIP file | |
| Attchment 3 - CNATRA Inst1542.153B.pdf | ||
| N6133909R0002.doc | DOC document | |
| Attachment 6 - Visual Database.doc | DOC document | |
| Attchment 5 - MESM with changes.doc | DOC document | |
| Attachment 4 - Floor Plan.doc | DOC document | |
| Attachment 2 - CNATRA Inst1542.147C.pdf | ||
| Attachment 7 - PP Questionnaire.rtf | RTF text file | |
| Attachment 2 - CNATRA Inst1542.147C.pdf | ||
| Attachment 7 - PP Questionnaire.rtf | RTF text file | |
| Attachment 4 - Floor Plan.doc | DOC document | |
| Attachment 6 - Visual Database.doc | DOC document | |
| Attchment 5 - MESM with changes.doc | DOC document | |
| DRAFT N61339-09-R-0002.doc | DOC document | |
| Attachment 1 - TC12B Configuration.doc | DOC document | |
| Attchment 3 - CNATRA Inst1542.153B.pdf |
Show all 17
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
TC-12B “Huron” Configuration
General Description: The Navy TC-12B 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 CNATRA PRELIMINARY NATOPS MANUAL TC-12B Change 2 figs. 2-3, 2-4, 2-6, 2-8, 2-11 and 2-13 are excellent depictions and should be used as references.
Engines: PT6A-41 have a three-stage axial, single stage centrifugal compressor driven by a single-stage reaction turbine . The power turbine, a two-stage reaction turbine counter rotating 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 / 42 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. (Collins VIR-30B)
· 1 TACAN indicator (Sierra Corporation DME-42)
· 1 TACAN receiver (Sierra Corporation SANS-706)
· 2 Altimeters
· 2 Instantaneous Vertical Speed Indicators (IVSI)
· 1 RAD ALT (Sperry AA-200)
· 1 Flight Director / Autopilot (Sperry SPZ-200A)
· 1 FMS-GPS receiver (L3)
· 2 ADF receiver (Collins ADF-60)
· 1 Radar (RCA Primus 30)
· 1 Transponder (Collins TDR-90)
· 1 GPWS (Sunstrand)
Communications:
· 2 VHF receiver/transmitters (Collins VHF-20B)
· 1 UHF receiver/transmitter (American Radio Corporation ARC-164)
· Voice Recorder (Fairchaild CDR Voice)
· 1 PRC-90 handheld radio
Upgrades
The delivery dates of upgrades are not certain, however a digital cockpit upgrade is planned in FY07 and should be given due consideration in a simulator contract for future TC-12 B. Some of these upgrades include the following:
· Enhanced GPWS
· Digital Weather Radar
· Electronic Flight Instrumentation
· TCAS / TCAS II Traffic Collision and Avoidance system
Attachment (1)
File details come from the government source that posted it. Updated .