285 

Federal Aviation Administration, DOT 

Pt. 60, App. B 

navigation systems (including inertial navi-
gation systems, global positioning systems, 
or other long-range systems) and the associ-
ated electronic display systems will be eval-
uated if installed. The NSP pilot will include 
in his report to the TPAA, the effect of the 
system operation and any system limitation. 

c. At the request of the TPAA, the NSP 

Pilot may assess the FTD for a special as-
pect of a sponsor’s training program during 
the functions and subjective portion of an 

evaluation. Such an assessment may include 
a portion of a specific operation (e.g., a Line 
Oriented Flight Training (LOFT) scenario) 
or special emphasis items in the sponsor’s 
training program. Unless directly related to 
a requirement for the qualification level, the 
results of such an evaluation would not af-
fect the qualification of the FTD. 

E

ND

I

NFORMATION

 

lllllllllllllllllllllll

T

ABLE

B3A—T

ABLE OF

F

UNCTIONS AND

S

UBJECTIVE

T

ESTS

L

EVEL

6 FTD 

QPS requirements 

Entry No. 

Operations tasks 

Tasks in this table are subject to evaluation if appropriate for the airplane system or systems simulated as indicated in the SOQ 

Configuration List as defined in Appendix B, Attachment 2 of this part. 

1. Preflight 

Accomplish a functions check of all installed switches, indicators, systems, and equipment at all crewmembers’ 

and instructors’ stations, and determine that the flight deck (or flight deck area) design and functions replicate 
the appropriate airplane. 

2. Surface Operations (pre-takeoff) 

2.a. ............

Engine start: 

2.a.1. .........

Normal start. 

2.a.2. .........

Alternative procedures start. 

2.a.3. .........

Abnormal procedures start/shut down. 

2.b. ............

Pushback/Powerback (powerback requires visual system). 

3. Takeoff (requires appropriate visual system as set out in Table B1A, item 6; Appendix B, Attachment 1.) 

3.a. ............

Instrument takeoff: 

3.a.1. .........

Engine checks (e.g., engine parameter relationships, propeller/mixture controls). 

3.a.2. .........

Acceleration characteristics. 

3.a.3. .........

Nosewheel/rudder steering. 

3.a.4. .........

Landing gear, wing flap, leading edge device operation. 

3.b. ............

Rejected takeoff: 

3.b.1. .........

Deceleration characteristics. 

3.b.2. .........

Brakes/engine reverser/ground spoiler operation. 

3.b.3. .........

Nosewheel/rudder steering. 

4. In-Flight Operations 

4.a. ............

Normal climb. 

4.b. ............

Cruise: 

4.b.1. .........

Demonstration of performance characteristics (speed vs. power). 

4.b.2. .........

Normal turns. 

4.b.3. .........

Demonstration of high altitude handling. 

4.b.4. .........

Demonstration of high airspeed handling/overspeed warning. 

4.b.5. .........

Demonstration of Mach effects on control and trim. 

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