587 

Federal Aviation Administration, DOT 

Pt. 91, SFAR No. 108 

3. Warning Systems 
4. Emergency Extension 
B. Nosewheel Steering 
C. Landing Gear/Brakes/Tires 
D. Limitations 
1. Airspeed (with flaps) 
2. Emergency Extension 
3. Tire Speed 
4. Brake Energy 

XIII. Flight Controls 

A. Primary Flight Controls (Elevator/Rud-

der/Spoilers) 

1. Description 
2. Operations 
B. Trim Systems 
1. System Description 
2. Roll Trim 
a. Normal Operation 
b. Emergency Operation 
3. Rudder Trim 
4. Pitch Trim 
a. General 
b. Operations 
c. Trim-in-Motion Alert System 
C. Secondary Flight Controls 
1. System Description 
2. Flaps 
D. Limitations 
1. Instrument Markings 
2. Placards 
E. Flight Characteristics 
1. Control Systems 
2. Stability and Stall Characteristics 
3. Single Engine Operation 
5. Maneuvering and Trim 
6. Takeoff and Landing 

XIV. Avionics 

A. Pitot-Static System 
1. System Description 
2. Pilot’s System 
3. Co-Pilot’s System 
4. Alternate Static 
B. Air Data Computer 
C. Attitude Instrument Displays (EFIS and 

Standard) 

1. EADI 
2. Standard Attitude Gyro 
D. AHRS 
1. System Description 
2. Controls and Indications 
E. Navigation 
1. Nav Systems Descriptions 
2. Compass System Descriptions 
3. Display Systems 
4. Terrain Awareness System 
5. Traffic Avoidance System 
F. Communications 
1. VHF Communications Systems 
2. Audio Control 
G. Standby Flight Instruments 
1. System Description 
2. Controls and Indications 
H. Automatic Flight Control System 
1. Controls and Indications 
2. Yaw Damper 
3. Trim-in-Motion Alert System 
4. Autopilot Automatic Disconnect 

5. Aural Alert System 
I. Angle of Attack (AOA) System 
1. System Description 
2. Controls and Indications 
J. Limitations 

XV. Oxygen System 

A. System Description 
B. Crew Oxygen 
1. Oxygen Cylinder Assembly 
2. Pressure Gauge 
3. Outlet Valves 
4. Duration 
C. Passenger Oxygen 
1. System Description 
2. Duration 
D. Limitations 

XVI. Performance and Planning 

A. Takeoff Performance Charts 
1. Runway Requirements 
2. Normal and with One Engine Inoperative 
B. Climb Performance 
1. Normal and with One Engine Inoperative 
2. Obstacle Clearance 
3. Power Assurance Charts 
C. Cruise Performance 
1. Power Charts 
2. Maximum Practical Altitude 
3. Cruise Speeds/Engine Health 
4. Buffet Boundary 
D. Landing Performance 
1. Runway Requirements 
a. Dry Runway 
b. Wet Runway 
2. Go-Around 
a. One Engine Inoperative 
b. All Engines 

XVII. Weight and Balance 

A. Aircraft Loading Procedures 
B. Limitations 
1. Weight Limits 
2. C.G. Limits 
C. Plotter 
1. Description 
2. Use 
D. Calculations 
1. AFM Procedures 
2. Examples 

XVIII. General Subjects 

A. Controlled Flight into Terrain Aware-

ness 

B. CRM/SPRM 
1. Crew Resource Management 
2. Single Pilot Resource Management 
C. MU–2B Flight Standardization Board 

Report 

A

PPENDIX

C 

TO

SFAR 108—MU–2B F

INAL

 

P

HASE

C

HECK

AND

F

LIGHT

T

RAINING

R

E

-

QUIREMENTS

 

(I) MU–2B Final Phase Check Requirements 

(A) Completion of the MU–2B Training Pro-

gram in this appendix requires successful 
completion of a final phase check taken in 
the MU–2B airplane or a Level C or D simu-
lator for Initial/Transition training. The 

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