ATT 41 T6B MEL.pdf

1 1 2 2 3 4 4 5 5

WUC D N D N D D N D N

11000 X X X X X X X X X

11000 X X X X X X X X X 1

12000 X X X X X X X X X 2

13000 X X X X X X X X X

13000 X X X X X X X X X

14000 X X X X X X X X X 9

22000 X X X X X X X X X

41000 X X X X X X X X X 3

42000 X X X X X X X X X

44000 X X X X X X X X X

44000 X X X X X X X X X 4

44000 X X X X X X X X X

44000 X X X X X X X X X 2

44000 X X X X 2

44000 X X X X X X X X X

45000 X X X X X X X X X

46000 X X X X X X X X X 6

47000 X X X X X X X X X 2

49000 X X X X X X X X X

57000 X X X X X X X X X 11

57000 X X X X X X X X X

51000 X X X X X X X X X 2

51000 X X X X X X X X X 14

51000 X X X X X X X X X 2

51000 X X X X X 2, 7

51000 X X X X X X 2, 8

51000 X X X X X X X X X 2

51000 X X X X X X X X X 2

57000 X X X X X X X X X 2

63000 X X X X X X X X X 2, 10

62000 X X X X X X X X X 2, 10

64000 X X X X X X X X X

65000 X X X X X X X X X

71000 X X X X X X X X X 5

71000 X X X X X X 12, 13

71000 X X X X 12

71000 X X X X X X X X X 12, 13

91000 X X X X X X X X X

72000 X X X X X X X X X

91000 X X X X X X X X X

VHF Omni-directional Range (VOR)

Emergency Locator Transmitter (ELT)

Traffic Collision Avoidance System (TCAS)

Emergency Equipment

Interphone/Intercommunications System

(ICS)

Transponder (Including Mode S)

Distance Measuring Equipment (DME)

Global Posiutioning System (GPS)

Instrument Landing System (ILS)

Fire and Overheat Detection System

Air Conditioning and Pressurization

Electrical Power Supply

Position Lights

Landing/Taxi Lights

Strobe Lights

Interior Lights

Active Matrix Liquid Crystal Display (AMLCD)

Display Lighting Controls

Hydraulic

Fuel

Oxygen

UHF Communication

VHF Communication

Integrated Avionics Computer (IAC)

Inertial Reference System (IRS)

Multifunction Display (MFD)

Flight Instruments

Accelerometer

Angle of Attack (AOA)

Clock

Utility Instrumentation

Fuel Quantity

Up Front Control Panel (UFCP)

Warning Lights

Brakes

NOTES

Flight Controls

Powerplant

Landing Gear

Mission Profiles:

T-6B MINIMUM EQUIPMENT LIST (MEL)

SYSTEM

Airframe

Windshield and Canopy

Cockpit

ATTACHMENT 41

T-6B MEL N61340-18-FOSR-0001

1 1 2 2 3 4 4 5 5

WUC D N D N D D N D N

97000 X X X X X X X X X

71000 X X X X X X X X X

12. Mission profile dependent, aircraft commander/instructor pilot discretion.

13. At least 1 operational NAV device required.

14. Flight Instruments must be operational, No warning flags/indications associated with Airspeed, ADI, Baro

Altitude, VSI, Turn Rate, Slip-Skid, HSI, BFI, Pitot Heat, Torque, ITT, N1, NP, Oil Temp, Oil Press, HYD Press.

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

7. Restricted to flight by Rated pilot.

8. Clock required in each cockpit (forward and aft).

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

10. VHF/UHF are redundant except when mission profile designates system specific usage. (UHF required at USN training bases).

11. IAC1 and IAC2 both required. No IAC related "Caution" messages (IAC1 FAIL, IAC2 FAIL, UFCP1 FAIL, IAC1 OVHT, IAC2 OVHT, IAC1CONFIG, IAC2CONFIG).

5. Restricted to dual day local or solo only with a Rated pilot.

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. 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 18,000 feet (with supplemental oxygen). Rated pilot decision.

4. 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.

NOTESSYSTEM

Legend:

WUC = Work Unit Code

D = Day

N = Night

Egress System

Radar Altimeter (RAD ALT)

Mission Profiles:

ATTACHMENT 41

T-6B MEL N61340-18-FOSR-0001