Attachment 2.pdf

PDF 1 MB Posted

Attached to
Recompete of UC-12 Platform Training Program Federal contract opportunity
Solicitation number
N6134024R0013
Issued by
Department of the Navy Naval Air Systems Command

About this file

This document provides details for a federal solicitation seeking simulator and training services to support the Navy's Command Aircraft Crew Training program for the UC-12 fleet. Naval Air Warfare Center Training Systems Division intends to award a commercial firm-fixed-price Indefinite Quantity contract with one base year and four option periods, totaling five years, to provide a certified Level C or higher non-ProLine UC-12 simulator and certified Level D or higher ProLine UC-12 simulators. Services required include academic and simulator training to facilitate pilot training in accordance with applicable NATOPS manuals and FAA regulations. The estimated award date is June 2024.

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Other files for this federal contract opportunity

Other files attached to Recompete of UC-12 Platform Training Program, newest first.
File Type Posted
Attachment 3.pdf PDF
Attachment 4.pdf PDF
Attachment 1.pdf PDF
Attachment__Solicitation_Question_and_Response_Form.docx DOCX document
Attachment - TPP UC-12.xlsx XLSX spreadsheet
N6134024R0013 UC12 RFP.pdf PDF

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Text version

UC-12F/M with Rockwell Collins Pro Line 21

Avionics Suite Modification Configuration

General Description: The Navy UC-12F/M is a military version of the

Beechcraft B200 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 of both the UC-12F and UC-12M have been modified with the three display Rockwell Collins Pro Line 21 avionics suite. The cockpit display should be designed to closely represent the actual setup. Depictions of cockpit layout can be found at the end of this document.

Engines: PT6A-42 has a three-stage axial, single stage reaction turbine.

The power turbine two-stage reaction turbine counter-rotating with the compressor turbine driving the output shaft.

Engine instruments: ITT, Torque,N1, Propeller Tachometers, Fuel Flow, Oil pressure/Oil Temperature indicators are all displayed by the center mounted Pro Line 21 MFD.

Electrical system: The aircraft employs 28 Vdc power supplied by a

24−volt, 42 ampere (amp) hour valve regulated sealed lead battery mounted in the right wing center section and two 250−amp starter/generators connected in parallel. The generator buses are interconnected by two current limiters. The entire electrical system operates as a single bus, with power being supplied by the battery and both generators. Four dual−fed buses distribute electrical power supplied from either generator main bus through circuit breakers with a diode.

Avionics

F

M

TYPE

MODEL

(if known) PART NUMBER (if known)

X

X Collins VHF System (Dual) VHF-4000E 822-1872-101

X X Collins Weather Radar System RTA-852 622-8439-004 X X L-3 COMM ESIS Standby Instrument System GH-3100 501-1860-0601 X X TACAN System AN/ARN-154(v) 805D0602-43 X X 406 MHz ELT System C-406N 455-5062 X X M3AR VHF/UHF Communication System MR6000L 965-0770-03 X X L-3 MADRAS Flight Data Recorder FA2200 2202-2300-00 X X NAT Audio Control Panel NAT 311-004 NAT 311-004

X X Collins Adaptive Flight Display System AFD-3010

2 each Primary Flight Display (PFD) and 1 each (center) Multifunctional Display (MFD)

AFD-3010

822-1084-352

X X Display Control Panel CDP-3030 822-1828-061 X X Display Mount IMT-3010 822-1140-004 X X Cursory Control panel CCP-3000 822-1746-001

X X Collins Flight Management System FMS-3000 X X Flight Management Computer (Dual) FMC-3000 822-0883-005 X X Control Display Unit CDU-3000 822-0884-193 X X Global Positioning System/Sensor (Dual) GPS-4000A 822-1377-001 X X Database Unit DBU-4100 822-0014-104

X X Collins Air Data System ADS-3000 X X Air Data Computer ADC-3000 822-1109-011

X X Collins Autopilot System APS-3000 X X Flight Guidance Computer FGC-3000 822-1108-031 X X Flight Guidance Panel FGP-3000 822-1107-103 X X Servo SVO-3000 822-1168-001 X X Servo SVO-3000 822-1168-002 X X Servo SVO-3000 822-1168-003 X X Collins (Distance) Measuring Equip System DME-4000 X X DME Receiver/Transmitter DME-4000 822-1466-001 X X DME Indicator IND-42a 622-6524-004 X X Antenna, L-Band ANT-42 622-6591-001

X X Collins Radar Altimeter ALT-1000 X X Receiver/Transmitter ALT-1000 822-1939-001 X X Radio Altimeter Antenna ANT-52 622-6793-001

X X Collins Altitude Heading Reference System AHS-3000 X X Altitude Heading Computer AHC-3000S 822-1800-001 X X Flux Detector Unit FDU-3000 822-1193-001 X X External Compensation Unit ECU-3000 822-1200-002

X Collins Navigation Receivers

NAV-

4000/4500/VIR-

4000/ADF-

X X VOR, ILS, Marker Beacon, ADF Receiver (2) NAV-4000 822-1465-001 X X Radio Turning Unit (2) RTU-4200 822-0668-261 X X Dual ADF Antenna (1) ANT-462B 622-7384-001

1. NO. 1 COMPASS DG FREE/NORM SWITCH

2. NO. 1 GYRO COMPASS SLEW SWITCH

3. PILOT PFD COMPOSITE/NORM SWITCH

13. WARNING ANNUNCIATOR PANEL

14. ANNUNCIATOR TEST SWITCH

15. REVERSION SWITCH PANEL

16. CAUTION ADVISORY PANEL

17. CABIN ALTIMETER AND DIFFERENTIAL PRESSURE GAUGE

18. CABIN CLIMB RATE INDICATOR

19. FLAP POSITION INDICATOR

20. HYDRAULIC FLUID SENSOR TEST BUTTON

21. EMERGENCY LIGHTS OVERRIDE SWITCH

22. LANDING GEAR POSITION INDICATOR LIGHTS

23. LANDING GEAR HANDLE LIGHTS TEST SWITCH

24. LANDING GEAR CONTROL HANDLE

4. AIR INLET

5. PILOT PRIMARY FLIGHT DISPLAY

6. MASTER WARNING ANNUNCIATOR

7. MASTER CAUTION ANNUNCIATOR

8. DISPLAY CONTROL PANEL

9. EGPWS ANNUNCIATORS

10. MULTIFUNCTION DISPLAY

11. ENGINE FIRE DETECTOR/EXTINGUISHER

SWITCHES/ANNUNCIATORS

12. FLIGHT GUIDANCE PANEL

31. ELECTRONIC STANDBY INSTRUMENT SYSTEM (ESIS)

32. RADIO TUNING UNIT (RTU)

33. DISPLAY CONTROL PANEL

34. MASTER CAUTION ANNUNCIATOR

45. GYRO SUCTION GAUGE

46. COPILOT AIR CONTROL

47. CABIN AIR CONTROL

48. FIRE DETECTORS AND EXTINGUISHERS TEST

SWITCH

49. CABIN TEMPERATURE MODE CONTROL SWITCH

50. CABIN TEMPERATURE CONTROL KNOB

51. FORWARD VENT BLOWER SWITCH

52. AFT BLOWER SWITCH

53. STALL WARNING AND LANDING GEAR TEST

SWITCH

54. BLEED AIR VALVE CONTROL SWITCHES

55. PROP ANTI−ICE AMMETER

36 4

UC-12F Instrument Panel

35. MASTER WARNING ANNUNCIATOR

36. COPILOT PRIMARY FLIGHT DISPLAY

37. AIR INLET

38. COPILOT PFD COMPOSITE/NORM SWITCH

39. NO. 2 GYRO COMPASS SLEW SWITCH

40. DG FREE/NORM SWITCH

41. PNEUMATIC PRESSURE GAUGE

42. OXYGEN PRESSURE GAUGE

43. FLIGHT HOUR METER

44. CABIN AIR TEMPERATURE GAUGE

UC-12F Instrument Panel

1. CONTROL DISPLAY UNIT

2. PEDESTAL SWITCH PANEL

3. AUDIO CONTROL PANEL

4. TCAS/IFF CONTROL PANEL

5. HF CONTROL PANEL

6. PRESSURIZATION CONTROL

PANEL

7. IFF KEY FILL PANEL/FMS PC DATA

LOAD

8. DATABASE UNIT

9. COCKPIT VOICE RECORDER

CONTROL PANEL

10. CURSOR CONTROL PANEL

11. VHF/UHF COMM RECEIVER

12. ENGINE START PANEL

UC-12F Center Pedestal

UC-12M Instrument Panel

UC-12M Overhead Control Panel

UC-12M Pedestal (Note: Second FMS not shown)

Radio Tuning Unit

ESIS

Pilot Flight Display

Multi Function Display

1. Windshield Wiper Control

2. Overhead Flood

3. Instrument Indirect

4. Annunciator Push/Bright

5. Overspeed Test Switch

6. Copilot Instrument Panel

7. Copilot Displays

8. Side Panel

9. Overhead Pedestal and Subpanel

10. Standby Magnetic Compass

11. Right DC Loadmeter

12. Left DC Loadmeter

13. Pilot Displays

14. Pilot Instrument Panel

15. Master Panel Lights On/Off

UC-12F Overhead Panel

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