P2 Flashcards
AR 40-8
6 hour restriction:
Centrifuge run- and no residual effects
12 hour restrictions:
A: Anesthesia- local
S: Simulator sickness- after last symptoms subside start clock (time starts after last symptom gone)
I: Immunizations
A: Alcohol- after 12 hours and no residual effects (time starts from last drink)
24 hours restrictions:
P: Plasma- not regular (> 2x/year)
H: Hypobaric chamber runs/decompression experience- >25,000 feet- no high altitude flight duties for 24 hours, or if below 10,000 may fly before 24 hours
S: Scuba- If urgent operational requirements, may fly within 24 hours of SCUBA diving
48 hour restrictions:
A: Anesthesia- general
72 hour restrictions:
B: Blood- not regular (> 2x/year)
Engine Oil Pressure
with note
Y = 50 PSI Minimum below 78%N1
G = 90 PSI Minimum from 78% - 94% N1
G = 115 PSI Minimum above 94% N1
(double wide arc=torque meter accurate)
R = 50 PSI Minimum, 130 PSI Maximum
NOTE
During cold temperature operation the oil pressure may exceed the maximum of 130 PSI. Stabilize the engine at idle speed of 60 to 64% until the engine oil temperature is above 0*C and the engine oil pressure is within normal limits.
Engine Oil Temperature
G = 0C to 107C Continuous Operation
R = 107*C Maximum
Engine Icing
A. Engine anti-ice shall not be used in ambient temperatures above 4*C.
B. Engine anti-icing shall be ON for flight in visible moisture in temperature 4*C or below.
Transmission Oil Pressure
G = 30-50 PSI Continuous Operation
R = 30 PSI Minimum, 70 PSI Maximum
Transmission Oil Temperature
G = 15C to 110C Continuous Operation
R = 110*C Maximum
Loadmeter
70% Maximum
Fuel Pressure Gauge
R = 4 PSI Minimum
G = 4-30 PSI Continuous Operation
R = 30 PSI Maximum
|> 8 PSI Minimum - Type A, A-1, JP-5, JP-8 fuel below -18C (0F) to -32C (-25F)
(With load meter)
Airspeed Indicator
w/ note
NOTE
Autorotation above 100 KIAS will result in high rates of descent and low rotor RPM.
G = 0-130 Knots Continuous Operation
R = 130 Knots Maximum
B = 100 Knots Maximum for Autorotation
Vne for internal Gross Weight above 3,200 pounds is 78 KIAS, not to exceed placarded Vne.
Turbine Outlet Temperature gauge
NOTE
The red warning light illuminates when either of the following conditions are exceeded: 810 to 927C for 10 seconds, or higher than 927C.
G = 100 - 738*C Continuous Operation
Y = 738 - 810*C Take-off Power Range (5 minute limit)
R = 810C Maximum
810 - 843C, 6 second transient (Not to be used intentionally).
R = 927*C Maximum during Starting and Shutdown (10 seconds Maximum)
Gas Producer (N1) gauge
G = 60-105% Continuous Operation
R = 105% Maximum
105-106% Transient (15 seconds Maximum)
Rotor Limitations
(On dual tachometer)
R = 90% Minimum Operation
Y = 50-60% Accelerate through this range
G = 90-107% Normal Operation
R = 107% Maximum
Power on Transient Rotor Droop Limit is 95% (5 seconds Maximum)
Power Turbine (N2) Gauge
R = 97% Minimum Operation
G = 97-100% Continuous Operation
R = 100% Maximum
N2 75%-88%, 60 seconds Maximum (time not cumulative)
N2 Transient Overspeed Chart
From 0 to 32% torque, engine RPM may be between 100 and 107%. From 32 to 100% torque, the engine rpm decreases linearly from 107 to 103%.
“N2 transient overspeed limit is 15 seconds Maximum. Shaded area represents allowable overspeed.”
Torque Meter
G = 0-85% Continuous Operation
Y = > 85-100% Take-off Power Range (5 minute limit)
R = 100% Maximum
Transient Torque Limit is 100-110% (5 second Maximum)
INTENTIONAL USE IS PROHIBITED.
Fuel Quantity Indicator
On Empty
84.1 gallons max
82.6 gallons issuable
Low fuel light illuminated at 12 gallons
Wind Limitations
with note
A. The helicopter can be started in a maximum wind velocity of 45 knots and a maximum gust spread of 15 knots.
NOTE
Gust spreads are not normally reported. To obtain spread, compare minimum and maximum velocities.
B. Maximum wind for hovering is 35 knots crosswind and 30 knots tailwind.
C. For hover operations at gross weights above 3200 lbs:
1. IGE maneuvers - refer to chapter 8. 2. OGE maneuvers - calm wind only.
Engine Anti Ice Limitations
A. Engine anti-ice shall not be used in ambient temperatures above 4*C.
B. Engine anti-icing shall be ON for flight in visible moisture in temperature 4*C or below.
Engine Starter Limits
A. If there is no rise in TOT within the first 20 seconds of energizing starter, limit starter energizing time to the following:
External Power 25 seconds- ON 30 seconds- OFF 25 seconds- ON 30 seconds- OFF 25 seconds- ON 30 minutes- OFF
Battery 40 seconds- ON 60 seconds- OFF 40 seconds- ON 60 seconds- OFF 40 seconds- ON 30 minutes- OFF
B. If there is a rise in TOT within the first 20 seconds of energizing starter, limit starter energizing time to the following:
External/Battery Power 1 minute- ON 1 minute- OFF 1 minute- ON 1 minute- OFF 1 minute- ON 30 minutes- OFF
Engine Starting Limits
During starting if N1 does not reach 58% in a total time of 45 seconds (or 60 seconds below 10C FAT), close throttle and press starter button until TOT is below 200C. If engine fails to start on third attempt, abort start and make an entry on DA Form 2408-13-1. Starter engage time limits above do not apply to engine starting limitations should abort start procedures become necessary.
Engine RPM Limitations
Use of throttle to control RPM is not authorized. (Refer to Chapter 9, Emergency Procedures and the USAAWC Flight Training Guide for exceptions.)
TOT Limits
CAUTION
Exceeding the limits of 810*C TOT or 100% torque may cause N1 topping with resultant rotor droop.
- Longitudinal Center of Gravity Limits
VMC Center of Gravity Limits are from station 106.0 to 114.2; however, the forward and aft limits are variable depending upon gross weight and aircraft configuration (Refer to Center of Gravity vs Gross Weight Chart in Chapter 6)
Lateral Center of Gravity Limits
Lateral CG Limits Cary depending on longitudinal CG location. (Refer to Later vs Longitudinal CG Limits Chart in Chapter 6.)
A. 3.0 inches left of helicopter centerline B. 4.0 inches right of helicopter centerline.