Thrush Aircraft Inc Model S2R-T34 SECTION I
Albany, GA
AIRPLANE FLIGHT MANUAL
LIMITATIONS
FAA APPROVED: Oct. 24, 2006 Revision 2, SECTION I-1
SECTION I
LIMITATIONS
TABLE OF CONTENTS
Subject page | Subject page
POWER PLANT ................................................... I-1 | WEIGHT AND CENTER OF GRAVITY ...........I-5
INSTRUMENT MARKINGS............................... I-3 | MANEUVERS.....................................................I-6
AIRSPEED LIMITATIONS ................................. I-4 | TYPES OF OPERATION ....................................I-6
ALTITUDE LIMITATIONS................................. I-4 | GROUND OPERATION .....................................I-6
FLIGHT LOAD FACTORS.................................. I-4 | PLACARDS.........................................................I-6
NOISE ABATEMENT.......................................... I-4
POWERPLANT:
ENGINE:
STANDARD: Pratt & Whitney Canada PT6A-34AG
OPTIONAL: Pratt & Whitney Canada PT6A-34
Pratt & Whitney Canada PT6A-36 (Dry Configuration Only)
Pratt & Whitney Canada PT6A-41, -41AG
Pratt & Whitney Canada PT6A-42
FUEL:
JET A, JET B, JP-4, JP-5. (If jet fuel is not available, aviation gasoline, MIL-G-5572, all grades,
may be used for a maximum of 150 hours between overhauls).
ENGINE LIMITS: PT6A-34AG, -34, -36 (PT6A-34AG shown)
POWER
SETTING
SHP
TORQUE
(PSI)
ITT
(ºC)
N
G
(%)
N
P
(RPM)
OIL
PRESS.
(PSIG)
OIL
TEMP.
(ºC)
Takeoff & Max
continuous
750
64.5***
58.7****
790 101.6 2200 85 to 105 10 to 99
Max Climb 700
60.2***
54.7****
765 101.6 2200 85 to 105 0 to 99
Max Cruise 700
60.2***
54.7****
740 2200 85 to 105 0 to 99
Idle 685 50 40 Min. -40 to 99
Starting 1090* -40 Min.
Acceleration 68.4** 850* 102.6* 2420 0 to 99
Max. Reverse 750
64.5***
GENERAL NOTE: The operating parameters in this Table are individual limits for each engine
parameter and do not necessarily apply simultaneously.
61.4****
790 101.6 2100 85 to 105 0 to 99
*These values are time limited to two (2) seconds.
**These values are time limited to twenty (20) seconds.
***Torque limit for Max N
P
= 2000 RPM
****Torque limit for N
P
= 2200 RPM