THRUSH S2R-T34 Technische Daten
Thrush Aircraft Inc Model S2R-T34 MANUAL
Albany, GA AIRPLANE FLIGHT MANUAL ORGANIZATION
FAA APPROVED: Oct. 24, 2006 Revision 2, page i
SECTION I-----------------------------------------------------LIMITATIONS
SECTION II-------------------------------------- NORMAL PROCEDURES
SECTION III--------------------------------EMERGENCY PROCEDURES
SECTION IV-------------------------------------------------PERFORMANCE
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) NG
(%) NP
(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 NP= 2000 RPM
****Torque limit for NP= 2200 RPM
Thrush Aircraft Inc Model S2R-T34 SECTION I
Albany, GA AIRPLANE FLIGHT MANUAL LIMITATIONS
FAA APPROVED: Jan. 27, 2009 Revision 4, SECTION I-2
ENGINE LIMITS: PT6A-41AG, -41, -42 (PT6A-41AG shown)
***
TORQUE
POWER
SETTING SHP
GENERAL NOTE: The operating parameters in this Table are individual limits for each engine
parameters and do not necessarily apply simultaneously.
(PSI)
ITT
(ºC) NG
(%) NP
(RPM)
OIL
PRESS.
(PSIG)
OIL
TEMP.
(ºC)
Takeoff & Max
continuous 750 64.5 750†101.5 2000 105 to
135††† 0 to 99
Max Climb 700 60.2 725†† 101.5 2000 105 to
135††† 0 to 99
Max Cruise 700 60.2 725†2000 105 to
135††† 0 to 99
Idle 50 60 Min. -40 to 99
Starting 1000* -40 Min.
Acceleration 68.4* 850 102.6 2205 99 to 104**
Max. Reverse 750 64.5 750 101.5 2000 105 to
135††† 0 to 99
*These values are time limited to five (5) seconds.
**Time limited to ten (10) minutes at any operating condition.
***Torque limit shown for NP= 1600-2000 RPM.
†For PT6A-42 790ºC.
††For PT6A-42 765ºC.
†††For PT6A-42 100 to 135
STARTER: Maximum starter engagement duration is 30 Seconds followed by a 60 Seconds
cool down period. Total of 3 cycles to be followed by 30 minutes starter cool
down.
AIR STARTS: Normal air starts are approved from sea level to 12,000 feet altitude and from 80
MPH to 126 MPH air speed. See the Emergency Procedures in Section III.
PROPELLER: Hartzell Hub Model HC-B3TN-3C (or HC-B3TN-3D) with Blade Model T-10282,
Diameter 102.5 inches maximum, 92.5 inches minimum or optional Blade Model
T-10282 (N) +4, Diameter 106.5 inches maximum, 98.0 inches minimum.
REVERSE POWER: Do not use in flight
P-3 HEATER: Regardless of fuel type used, the P-3 heater switch must be turned on (if installed)
for flight and ground operations when the free air temperature is below 40 Degrees
F.
Thrush Aircraft Inc Model S2R-T34 SECTION I
Albany, GA AIRPLANE FLIGHT MANUAL LIMITATIONS
FAA APPROVED: OCT 24, 2006 Revision 2, SECTION I-3
INSTRUMENT MARKINGS:
Limits Features Meaning
OIL TEMP ( °C)
-40
-40 to10
10 to 99
99
Red Radial
Yellow Arc
Green Arc
Red Radial
MINIMUM
CAUTION
NORMAL
MAXIMUM
OIL PRESSURE (PSI) PT6A-34AG, -34, -36
40
40 to 85
85 to 105
105
Red Radial
Yellow Arc
Green Arc
Red Radial
MINIMUM
CAUTION
NORMAL
MAXIMUM
OIL PRESSURE (PSI) PT6A-41AG,-41
60
60 to 105**
105 to 135
135
Red Radial
Yellow Arc
Green Arc
Red Radial
MINIMUM
CAUTION
NORMAL
MAXIMUM
OIL PRESSURE (PSI) PT6A-42
60
60 to 100***
100 to 135
135
Red Radial
Yellow Arc
Green Arc
Red Radial
MINIMUM
CAUTION
NORMAL
MAXIMUM
FUEL PRESSURE (PSI) 5
5 to 50
50
Red Radial
Green Arc
Red Radial
MINIMUM
NORMAL
MAXIMUM
ITT (°C) PT6A-34AG, -34, -36 400 to 790
790 Green Arc
Red Radial NORMAL
MAXIMUM
ITT (°C) PT6A-41AG, -41 400 to 750
750 Green Arc
Red Radial NORMAL
MAXIMUM
ITT (°C) PT6A-42 400 to 800
800 Green Arc
Red Radial NORMAL
MAXIMUM
TORQUE (PSI) PT6A-34AG, -34, -36
0 to 58.7
58.7*
64.5
Green Arc
Red Radial
Red Diamond
NORMAL
MAXIMUM
Max @
2000RPM
TORQUE (PSI)
PT6A-41AG, -41, -42 0 to 64.5
64.5 Green Arc
Red Radial NORMAL
MAXIMUM
PROPELLER RPM (NP)
PT6A-34AG, -34, -36 0 to 2200
2200 Green Arc
Red Radial NORMAL
MAXIMUM
Thrush Aircraft Inc Model S2R-T34 SECTION I
Albany, GA AIRPLANE FLIGHT MANUAL LIMITATIONS
FAA APPROVED: OCT 24, 2006 Revision 2, SECTION I-4
INSTRUMENT MARKINGS (Continued)
Limits Features Meaning
PROPELLER RPM (NP)
PT6A-41AG, -41, -42 0 to 2000
2000 Green Arc
Red Radial NORMAL
MAXIMUM
GAS GENERATOR SPEED (% NG) 50 to 101.6
101.6 Green Arc
Red Radial NORMAL
MAXIMUM
AIRSPEED
66 to 123 MPH CAS
70 to 126 MPH CAS
126 to 159 MPH CAS
159 MPH CAS
White Arc
Green Arc
Yellow Arc
Red Radial
Flaps Operating Range
Normal Operating Range
Caution Range
Never Exceed
* In addition to a red radial limit marker at 58.7 PSI, the torque meter is marked with a red diamond at 64.5
PSI. (58.7 PSI is the torque limit for 2200 RPM, the normal takeoff RPM. 64.5 PSI is the torque limit for
2000 RPM, an optional RPM setting for in-flight use.)
** The 60-105 oil pressure caution range is for idling and for emergency completion of a flight using 36 PSI
torque or below.
*** The 60-100 oil pressure caution range is for idling and for emergency completion of a flight using 36 PSI
torque or below.
AIRSPEED LIMITATIONS:
Never Exceed Speed VNE – 159 MPH
Maximum Structural Cruising - VNO – 126 MPH
Maneuvering Speed – VA– 126 MPH
Flap Extended Speed – VFE – 123 MPH
Maximum Dump Speed – 120 MPH
Maximum Crosswind Velocity – 15 MPH
All airspeeds are given in Calibrated Air Speeds.
ALTITUDE LIMITATIONS:
Maximum approved altitude is 12,000 feet.
FLIGHT LOAD FACTORS:
Design Load Factors - Flap Up; 3.8 Positive, 1.9 Negative
Design Load Factors - Flap Down; 2.4 Positive, 0.0 Negative
NOISE ABATEMENT:
This airplane has not been shown to comply with the noise limits in FAR 36 and must be
operated in accordance with the noise operating limitation prescribed under FAR §91.815.
Thrush Aircraft Inc Model S2R-T34 SECTION I
Albany, GA AIRPLANE FLIGHT MANUAL LIMITATIONS
FAA APPROVED: Jan. 27, 2009 Revision 4, SECTION I-5
WEIGHT AND CENTER OF GRAVITY:
NOTE
Datum is the leading edge of the wing.
Maximum Weight – 6000 pounds
C.G. Range for SINGLE & DUAL COCKPIT
* Forward Limit at 6000 pounds is 26.5 inches AFT of Datum.
* Forward Limit at 4000 pounds is 24.0 inches AFT of Datum.
* AFT Limit is 29.0 inches AFT of Datum (Normal Category).
Straight Line variation in the Forward Limit between 4000 pounds and 6000 pounds.
7,000
6,500
6,000
5,500
5,000
4,500
4,000
3,500
3,000
23.0 23.5 24.0 24.5 25.0 25.5 26.0 26.5 27.0 27.5 28.0 28.5 29.0 29.5 30.0
4,000 lbs
@ 24.0 in
6,000 lbs
@ 26.5 in
4,000 lbs
6,000 lbs
@ 29.0 in
Center of Gravity - in. aft of datum
Airplane Weight - lbs
Thrush S2R-T34 Single & Dual Cockpit
Weight & Center-of-Gravity Envelope
Normal Catagory
Inhaltsverzeichnis
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