Chapter 5 - Limitations Flashcards
NP Limitations
12 - Second Transient 105-107%
Transient (3) 101-105%
Continuous (2) 95-101%
Transient (1) 91-95%
NR (Rotor) Limitations
(Power On)
Power On
TRANSIENT 101 - 107%
TRANSIENT 95 - 101%
CONTINUOUS 91 - 95%
NR (Rotor) Limitations
Power OFF (Autorotation)
Power Off (Autorotation)
MAXIMUM 105 - 110%
TRANSIENT 90 - 105%
NORMAL 110%
UPPER RED RANGE BEGINS AT 110% TO CORRESPOND WITH THE POWER OFF LIMIT
NG (Gas Generator) Limitations
- NOTE:*
- NG DIGITAL READOUT WILL APPEAR WHEN NG INCREASES ABOVE 100%.*
12 SECOND TRANSIENT (2) 105 - 106%
CONTINUOUS (1) 0 - 105%
Torque (Q) Limitations
(10 Second Transient)
DUAL - ENGINE:
ABOVE 80 KIAS (4) 100 - 144%
80 KIAS OR BELOW 120 - 144%
SINGLE - ENGINE SINGLE 135 - 144%
Torque (Q) Limitations
(CONTINUOUS)
SINGLE - ENGINE 0 - 135%
DUAL - ENGINE:
ABOVE 80 KIAS 0 - 100%
AT OR BELOW 80 KIAS 0 - 120%
TGT Limitations
12 SECOND TRANSIENT 903 - 949 C
2.5 MINUTE TRANSIENT (CONTINGENCY POWER) (4) 879 - 903 C
START ABORT LIMIT 851 C
10 MINUTE LIMIT (3) 846 - 879 C
30 MINUTE LIMIT (2) 793 - 846 C
NORMAL (1) 0 - 793 C
NOTE: ON THE POWER POD TGT IS NOT DISPLAYED UNLESS ABOVE 793 C
ENGINE OIL TEMPERATURE Limits
ENGINE TEMP
30 MINUTE LIMIT (2) 135 - 150 C
CONTINUOUS (1) -20 - 135 C
ENGINE OIL PRESSURE Limits
ENGINE Pressure
5 MINUTE LIMIT (3) 100 - 120 PSI
NORMAL (2) 26 - 100 PSI
IDLE (1) 22 - 26 PSI
TRANSMISSION OIL TEMPERATURE Limits
TRANSMISSION Temp
PRECAUTIONARY (2) 105 - 140 C
CONTINUOUS (1) -20 - 105 C
TRANSMISSION OIL PRESSURE Limits
TRANSMISSION Pressure
PRECAUTIONARY (3) 65-130 PSI
CONTINUOUS (2) 30-65 PSI
IDLE AND TRANSIENT (1) 20-30 PSI
FUEL Indication markings
NORMAL (1) > 200 (EACH TANK)
PRECAUTIONARY (2) 0 - 200 (EACH TANK)
Engine NP Limitations
NOTE:
Avoid operations in __ - __% and __% - __% NP range except during start and shutdown.
20% - 40% and 60% - 90% NP
Engine Starter Limits (below 15°C)
At ambient temperatures of __°C and below, __ consecutive start cycles may be made, followed by a __ minute rest period, followed by two additional consecutive start cycles. A __ minute rest period is then required before any additional starts.
At ambient temperatures of 15°C (59°F) and below, two consecutive start cycles may be made, followed by a 3 minute rest period, followed by two additional consecutive start cycles. A 30 minute rest period is then required before any additional starts.
Engine Starter Limits above 15° C:
At ambient temperatures above ___ up to ___, ___ consecutive start cycles may be made. A ___ minute rest period is then required before any additional start cycles.
At ambient temperatures above 15° up to 52°C (59° up to 126°F), two consecutive start cycles may be made. A 30 minute rest period is then required before any additional start cycles.
Fuel boost pumps shall be on when operating with JP-4 or equivalent (as specificed in Operator’s Manual):
(1) At _______ feet pressure altitude and above.
(2) When operating in _____ with JP-4 at ____ altitude.
Fuel boost pumps shall be on when operating with JP-4 or
equivalent (as specified in Operator’s Manual):
(1) At 5000 feet pressure altitude and above.
(2) When operating in crossfeed with JP-4 at any altitude.
PNEUMATIC SOURCE INLET LIMITS:
The minimum ground-air source (pneumatic) required
to start the helicopter engines is __ psig and __ ppm at
___°C. The maximum ground-air source to be applied
to the helicopter is __ psig at _____ °C,
measured at the external air connector on the fuselage.
The minimum ground-air source (pneumatic) required
to start the helicopter engines is 40 psig and 30 ppm at
149°C (300°F). The maximum ground-air source to be applied
to the helicopter is 50 psig at 249°C (480°F),
measured at the external air connector on the fuselage.
ENGINE START LIMITS
CAUTION
Engine start attempts at or above a pressure
altitude of ___\_ feet could result in
a ____ _____.
Engine start attempts at or above a pressure
altitude of 18,000 feet could result in
a hot start.
CAUTION
Due to fuel volatility, when converting
from JP-4 to JP-5/JP-8, ____ helicopter
refueling operations must be completed
before performing operations with fuel
boost pumps off.
Due to fuel volatility, when converting
from JP-4 to JP-5/JP-8, three helicopter
refueling operations must be completed
before performing operations with fuel
boost pumps off.
When a helicopter operating with JP-4 is restarted
within ___ hours of engine shutdown and the air temperature
is above ___ , a minimum of ___ minutes of dual
engine ground operation at 100% NR is required prior to
takeoff to purge possible hot fuel from engine nacelle area.
When a helicopter operating with JP-4 is restarted
within 2 hours of engine shutdown and the air temperature
is above 21°C (70°F), a minimum of 2 minutes of dual
engine ground operation at 100% NR is required prior to
takeoff to purge possible hot fuel from engine nacelle area.
HELICOPTER MAXIMUM WEIGHT
UH-60M _____lbs
UH-60M external lift mission _____lbs
ESSS/ERFS helicopter onferry mission _______lbs
(Airworthinessrelease required)
HELICOPTER MAXIMUM WEIGHT
UH-60M 22,000 lbs
UH-60M external lift mission 23,500 lbs
ESSS/ERFS helicopter onferry mission 23,500 lbs
(Airworthinessrelease required)
External lift missions above _____ pounds can only be flown with cargo hook loads above _____ pounds and up to _____ pounds.
External lift missions above 22,000 pounds can only be flown with cargo hook loads above 8,000 pounds and up to 9,000 pounds.
Maximum weight is further limited by cargo floor
maximum capacity of ____ pounds per square foot.
Maximum weight is further limited by cargo floor
maximum capacity of 300 pounds per square foot.
Maximum capacity for each storage compartment is _____ pounds.
Maximum capacity for each storage compartment is 125 pounds.
The four cabin ceiling tiedown fittings have a limited load capability of ______ pounds.
The four cabin ceiling tiedown fittings have a limited load capability of 4,000 pounds.
The ____ (number) tiedown fittings installed on the cargo floor can restrain a ____ pound load in any direction.
The 17 tiedown fittings installed on the cargo floor can restrain a 5,000 pound load in any direction.
The ____ (number) net restraint rings in the cargo compartment are rated at _____ pound capacity in any direction.
The eight net restraint rings in the cargo compartment are rated at 3,500 pound capacity in any direction.
The maximum weight that may be suspended from the cargo hook is _____ pounds.
The maximum weight that may be suspended from the cargo hook is 9,000 pounds.