585 

Federal Aviation Administration, DOT 

Pt. 91, SFAR No. 108 

T

ABLE

3 

TO

A

PPENDIX

A 

OF

SFAR 108 

Differences training 

2 models currently ..........

1.5 hours at Level A or 

B. 

More than 2 models cur-

rently.

3 hours at Level A or B. 

Each additional model 

added.

1.5 hours at Level A or 

B. 

(e) Definitions of Levels of Training as 

Used in This Appendix 

(1) LEVEL A Training—Training that is 

conducted through self instruction by the 
pilot. 

(2) LEVEL B Training—Training that is 

conducted in the classroom environment 
with the aid of a qualified instructor who 
meets the requirements of this SFAR. 

(3) LEVEL C Training—Training that is ac-

complished in an FAA-approved Level 5, 6, or 
7 Flight Training Device (FTD). In addition 
to the basic FTD requirements, the FTD 
must be representative of the MU–2B cockpit 
controls and be specifically approved by the 
FAA for the MU–2B airplane. 

(4) LEVEL E Training—Training that must 

be accomplished in the MU–2B airplane, 
Level C simulator, or Level D simulator. 

A

PPENDIX

B 

TO

SFAR 108—MU–2B G

ROUND

 

T

RAINING

C

URRICULUM

C

ONTENTS

 

All items in the ground training cur-

riculum must be covered. The order of pres-
entation is at the discretion of the instruc-
tor. The student must satisfactorily com-
plete a written or oral exam given by the 
training provider based on this MU–2B Train-
ing Program. 
I. Aircraft General 

A. Introduction 
B. Airplane (Structures/Aerodynamics/En-

gines) Overview 

1. Fuselage 
2. Wing 
3. Empennage 
4. Doors 
5. Windshield and Windows 
C. Airplane Systems 
1. Electrical Power 
2. Lighting 
3. Fuel System 
4. Powerplant 
5. Environmental 
6. Fire Protection 
7. Ice and Rain Protection 
8. Landing Gear and Brakes 
9. Flight Controls and Trim 
10. Pilot Static System/Flight Instruments 
11. Oxygen System 
D. Operating Limitations 
1. Weights 
2. Center of Gravity and Loading 
3. Airspeeds 
4. Maneuvering Load Factors 

5. Takeoff And Landing Operations 
6. Enroute Operations 
E. Required Placards 
F. Instrument Markings 
G. Flight Characteristics 
1. Control System 
2. Stability and Stall Characteristics 
3. Single Engine Operation 
4. Maneuvering and Trim 
5. Takeoff and Landing 

II. Electrical Power 

A. General Description 
B. DC Electrical System 
1. DC Power Generation 
2. DC Power Distribution 
3. Battery System 
4. External Power System 
C. AC Electrical System 
1. AC Power Generation 
2. Controls and Indicators 
3. AC Power Distribution 
D. Limitations 
1. General Limitations 
2. Instrument Markings 

III. Lighting 

A. Exterior Lighting System 
1. Navigation Lights 
2. Anti-Collision Lights 
3. Wing Inspection Lights 
4. Taxi Lights 
5. Landing Lights 
6. Rotating Beacon 
7. Operation 
B. Interior Lighting System 
1. Flight Compartment Lights 
2. Passenger Compartment Lights 
C. Emergency Lighting System 
1. Cockpit Emergency Lighting 
2. Aircraft Emergency Lighting 
D. Procedures 
1. Normal 
2. Abnormal 
3. Emergency 

IV. Master Caution System 

A. System Description and Operation 
1. Master Caution Light and Reset Switch 
2. Annunciator and Indicator Panels 
3. Operation Lights 
4. System Tests 
B. Procedures 

V. Fuel System 

A. Fuel Storage 
1. Refueling/Balancing 
2. De-Fueling and Draining 
3. Tank Vent System 
B. Fuel Distribution 
1. Fuel Transfer 
2. Fuel Balancing 
3. Boost Pump Operation 
C. Fuel Indicating 
1. Fuel Quantity 
2. Low Fuel Warning 
D. Fuel System Limitations 
1. Approved Fuels 
2. Fuel Anti-Icing Additives 
3. Fuel Temperature Limitations 
4. Fuel Transfer and Fuel Imbalance 

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