Attachment 16 19 Oct 10 T-6A MESM.pdf

FA8617-11-R-6208

Section J, Attachment 16

22 Dec 09

MINIMUM ESSENTIAL SUBSYSTEM MATRIX

NFO MISSION (T-6A)

System WUC

1 1 2 2 3 3 4 4 5 5

NOTES D N D N D N D N D N

Airframe 11000 X X X X X X X X X X

Windshield and Canopy 11100 X X X X X X X X X X 1 Cockpit 12000 X X X X X X X X X X 2

Landing Gear 13000 X X X X X X X X X X

Brakes 13000 X X X X X X X X X X 3 Flight Controls 14000 X X X X X X X X X X 14 Powerplant 23000 X X X X X X X X X X 4

Air Conditioning and Pressurization 41100 X X X X X X X X X X 5

Electrical Power Supply 42000 X X X X X X X X X X

Position Lights 44100 X X X X X X X X X X

Landing/Taxi Lights 44100 X X X X X X X X X X 6 Strobe Lights 44100 X X X X X X X X X X

Warning Lights 44000 X X X X X X X X X X 2 Interior Lighting 44000 X X X X X 2

AMLCD or CRT Display Lighting Cntrls 44000 X X X X X X X X X X 2 Hydraulic 45100 X X X X X X X X X X

Fuel 46000 X X X X X X X X X X 10 Oxygen 47000 X X X X X X X X X X 2

Fire and Overheat Detection System 49100 X X X X X X X X X X

Flight Instrumentation 51100 X X X X X X X X X X 2

EADI 51100 X X X X X X X X X X 2

EHSI 51100 X X X X X X X X X X 2

Accelerometer 51100 X X 2 Angie of Attack 51100 X X X X X X X X X X 2,11 Navigation Instrumentation 51200 X X X X X X X X X X 2,7 Clock 51212 X X X X 12 Utility Instrumentation 51600 X X X X X X X X X X 2 Fuel Quantity 51700 X X X X X X X X X X 2

UHF Communication 63300 X X X X X X X X X X 15 VHF Communication 63300 X X X X X X X X X X 15 Interphone System 64100 X X X X X X X X X X 2

UHF Communication 63300 X X X X X X X X X X 15 VHF Communication 63300 X X X X X X X X X X 15

FA8617-11-R-6208

Section J, Attachment 16

22 Dec 09

UHF Communication 63300 X X X X X X X X X X 15 VHF Communication 63300 X X X X X X X X X X 15 Interphone System 64100 X X X X X X X X X X 2 Transponder (Including Mode S) 65000 X X X X X X X X X X 8

DME 71200 X X X X X X X X X X 9

GPS 71XXX X X X X X X X X X X 13

ILS 71300 X X X X X

VOR 71300 X X X X X X X X X X

ELT 91000 X X X X X X X X X X

TAS 72000 X X X X X X X X X X

Emergency Equipment 91000 X X X X X X X X X X

Egress System 97A00 X X X X X X X X X X

MISSION LEGENDS:

WUC = Work Unit Code D = Day N = Night

MISSION PROFILES:

1 = Contact Familiarization 2 = Instrument 3 = Formation 4 = Low Altitude Navigation 5 = High Altitude Navigation

NOTES:

1. Aircraft with canopy or windscreen distorted/crazed within TO limits are restricted to day dual local visual meteorological conditions (VMC) and no formation flights (Rated pilot decision).

2. Aircraft may be flown solo with discrepancies in rear cockpit which do not affect safety of flight.

3. Restricted to dual day local, dual local instrument meteorological conditions (IMC), or solo with a rated pilot for first flight when brake system has been bled due to component removal, replacement, or installation (JPPT only).

4. Restricted to local with a rated pilot for first flight when an engine is replaced with a non-Functional Check Flight (FCF) engine (JPPT only). Aircraft with engine requiring special oil analysis surveillance and or sampling are restricted to local missions. Restricted to ferry flight, in manual mode, by rated pilot.

5. Manual mode required for all missions. Vapor cycle air conditioning not required during cool weather (rated pilot decision). Inoperative pressurization system has no flight restrictions below 25,000 feet (with supplemental oxygen).

Rated pilot decision.

6. Both Landing/Taxi lights inoperative, restricted to day local VMC (dual or solo) if no instrument or straight-in approaches are planned. Continued flight with one bulb inoperative allowable. Both strobes must operate for day and night flying.

7. For a standby magnetic compass swing required by maintenance, the aircraft is restricted to dual day local VMC or solo with a rated pilot.

8. Restricted to day local VMC for home field pattern only missions with local air traffic control approval.

9. Restricted to dual day local or solo only with a rated pilot.

10. Restricted to rated pilot if fuel auto balance system is inoperative. Single point refueling not required.

11. Restricted to flight by rated pilot.

12. Clock required in student position.

13. Restricted to day local VMC.

14. Trim Aid Device not a required subsystem. Failure does not impact flight safety.

15. VHF/UHF are redundant except when mission profile designates system specific usage.