171
Federal Aviation Administration, DOT
Pt. 60, App. B
T
ABLE
B2D—A
LTERNATIVE
D
ATA
S
OURCE FOR
FTD L
EVEL
5 S
MALL
, S
INGLE
E
NGINE
(T
URBO
-
P
ROPELLER
) A
IRPLANE
—Continued
QPS requirement
The performance parameters in this table must be used to program the FTD if flight test data is not used to program the FTD.
Applicable Test
Authorized performance range
Entry No.
Title and procedure
2.c.8.b. .......
Phugoid dynamics ...........................................................
Must have a phugoid with a period of 30–60 seconds.
May not reach
1
⁄
2
or double amplitude in less than 2
cycles.
2.d. .............
Lateral Directional Tests
2.d.2. ..........
Roll response ..................................................................
Roll rate must be measured through at least 30
°
of roll.
Aileron control must be deflected
1
⁄
3
(33.3 percent) of
maximum travel.
Must have a roll rate of 4
°
–25
°
/second.
2.d.4.b. .......
Spiral stability ..................................................................
Cruise configuration and normal cruise airspeed. Estab-
lish a 20
°
–30
°
bank. When stabilized, neutralize the
aileron control and release. Must be completed in
both directions of turn.
Initial bank angle (
±
5
°
) after 20 seconds.
2.d.6.b. .......
Rudder response .............................................................
Use 25 percent of maximum rudder deflection. (Appli-
cable to approach or landing configuration.).
3
°
–6
°
/second yaw rate.
2.d.7. ..........
Dutch roll, yaw damper off ..............................................
(Applicable to cruise and approach configurations.)
A period of 2–5 seconds; and
1
⁄
2
–3 cycles.
2.d.8. ..........
Steady state sideslip .......................................................
Use 50 percent rudder deflection.
(Applicable to approach and landing configurations.)
2
°
–10
°
of bank; 4
°
–10
°
of sideslip; and 2
°
–10
°
of aile-
ron.
6. FTD System Response Time
6.a. .............
Flight deck instrument systems response to an abrupt
pilot controller input. One test is required in each axis
(pitch, roll, yaw).
300 milliseconds or less.
T
ABLE
B2E—A
LTERNATIVE
D
ATA
S
OURCE FOR
FTD L
EVEL
5 M
ULTI
-E
NGINE
(T
URBO
-P
ROPELLER
)
A
IRPLANE
QPS Requirement
The performance parameters in this table must be used to program the FTD if flight test data is not used to program the FTD.
Applicable test
Authorized performance range
Entry No.
Title and procedure
1. Performance
1.c ..............
Climb.
1.b.1. ..........
Normal climb with nominal gross weight, at best rate-of-
climb airspeed.
Climb airspeed = 120–140 knots.
Climb rate = 1000–3000 fpm (5–15 m/sec).
1.f. ..............
Engines
1.f.1. ...........
Acceleration; idle to takeoff power ..................................
2–6 Seconds.
1.f.2. ...........
Deceleration; takeoff power to idle .................................
1–5 Seconds.
2. Handling Qualities
2.c. .............
Longitudinal Tests
2.c.1. ..........
Power change force
VerDate Mar<15>2010
20:48 Jan 30, 2014
Jkt 232047
PO 00000
Frm 00181
Fmt 8010
Sfmt 8002
Q:\14\14V2.TXT
ofr150
PsN: PC150