LIMITS
Minimum Pressure for NG at Ground Idle:______
Minimum pressure for NG between 80-95%:_____
Minimum pressure for NG equal to or greater
than 95%:_____
Normal operation:_______
Maximum for contingency power:_______
Maximum for cold weather starts:_______
Minimum Pressure for NG at Ground Idle: 5 psi
Minimum pressure for NG between 80-95%: 32 psi
Minimum pressure for NG equal to or greater
than 95%: 50 psi
Normal operation: 35 to 90 psi
Maximum for contingency power: 110 psi
Maximum for cold weather starts: 150 psi
ABORT START
Indications
-Rapid and abnormal rise in PTIT
-May observe flames and black smoke coming from the engine tail cone
ENG COND lever -STOP
ENG START switch - Motor (if high PTIT is indicated)
BONUS (100 POINTS) : If a second engine start is to be attempted, wait at least ___ after NG indicates zero before attempting to start.
How much pressure is stored inside the Emergency Egress Bottle?
MK2: 3000 psi
4500: 4500 psi
What are the requirements to begin an approach?
1) Cleared for approach
2) On Course
3) Within Limits
Who is the initial mission approval authority for flights outside the Local flying area?
Battalion Commander
Maximum crosswind or sideward flight: _________
Maximum airspeed for rearward flight:________
Maximum tailwind for a hover:___________
Maximum airspeed with the lower section of the cabin entrance door open and locked________
The rescue hatch door shall not be opened or closed above:________.
The windshield wipers shall be off at airspeeds above:________.
Upper section of the cabin entrance- ensure that airspeed is less than __________ before closing the door in flight.
If a sling or hook should fail while carrying a tandem load, limit airspeed to a maximum of _____.
Maximum crosswind or sideward flight: 45 KCAS
Maximum airspeed for rearward flight:40 KCAS
Maximum tailwind for a hover: 40 KCAS
Maximum airspeed with the lower section of the cabin entrance door open and locked: 60 KCAS
The rescue hatch door shall not be opened or closed above: 90 KCAS
The windshield wipers shall be off at airspeeds above: 130 KCAS
Upper section of the cabin entrance- ensure that airspeed is less than 100 KCAS before closing the door in flight.
If a sling or hook should fail while carrying a tandem load, limit airspeed to a maximum of 60 KCAS
SMOKE AND FUME ELIMINATION
a) What are your Immediate Actions?
b) What are the associated WARNING(s) with this EP?
c) What are the associated NOTE(s) with this EP
a/s - Above 60 KCAS
Pilot's sliding window - open
Helicopter attitude - Yaw left (one half to one ball width on the inclinometer)
-Upper half of main cabin door - open
WARNING 1: If the flight engineer is unable to manually position the ramp, the pilot should attempt to check that the ramp is clear of personnel and equipment before opening and closing it.
WARNING 2: Unannounced opening and closing of the ramp may lead to injury to personnel or damage to equipment.
Note 1: Intensification of smoldering fire may occur if the pilot's sliding window, upper half of the main cabin door, and the ramp are open.
Note 2: If the source of the fire cannot be determined, close the cargo loading ramp but keep the pilot's window and the upper half of the main cabin door open.
How long does the SWET qualification remain current?
Four years
Types of Instrument Departure Pocedures
1) Obstacle depature: Provides obstacle clearance (not assigned by ATC)
2) Standard Instrument Depature: ATC requested depature route typically used in busy areas to reduce pilot/controller workload
3) Diverse Departure; 35ft at the end of the runway, climb to 400 ft AGL, 200 ft/NM
What is the lateral limits of the low level routes within FS R3005?
100M
Hydraulic limits
Temperature:
yellow/white _________.
Red/white _______ Maximum.
Pressure:
Flight Hydraulics
Utility hydraulics
Temperature: yellow/white: 95 to 120° C
Red/white 120° C Maximum.
Flight Hydraulics
Low: 2500 Normal: 2500-3200 psi High: 3200 psi
Utility Hydraulics
Low: 2500 psi Normal: 2500-3500 psi High: 3500 psi
Diagnose this EP.
-Excessive TQ splits
-NG, fuel flow, NR, and PTIT indications with a set thrust position
a) What are the associated WARNING(s) with this EP?
b) What are the associated CAUTION(s) with this EP?
WARNING 1: When selecting REV on either engine, the engine in PRI will no longer be in automatic load matching (i.e., TQ, PTIT, or NG)
WARNING 2: The engine in PRI will attempt to maintain the FADEC panel selected NR
CAUTION 1: Abrupt NR changes may occur when operating the FADEC in single or dual engine REV mode (S)
All personnel aboard an Army aircraft flown _____ or a _______ will wear a life preserver.
All personnel aboard an Army aircraft flown beyond glide distance of shore in a single-engine aircraft or a multi-engine aircraft without single-engine capability will wear a life preserve
How does an area forecast differ from a terminal forecast?
Area WX is reported in MSL and Terminal is represented in AGL
What gridline delineates a difference in R3005 Inadvertent IMC recovery procedures?
What are the associated Headings?
Gridline 43
West: 230
East: 090
Maximum continuous _______
Maximum for not more than 30 minutes ______
Maximum for not more than 10 minutes ______
Maximum for not more than 2.5 minutes
(contingency power) _______
Maximum for not more than 12 seconds (never
exceed) ______
Maximum transient for not more than 4 seconds
(never exceed) _______
Maximum continuous 816° C
Maximum for not more than 30 minutes 854° C
Maximum for not more than 10 minutes 899° C
Maximum for not more than 2.5 minutes
(contingency power) 932° C
Maximum for not more than 12 seconds (never
exceed) 943° C
Maximum transient for not more than 4 seconds
(never exceed) > 943° C
Indications:
-#1 GEN FAIL or #2 GEN FAIL + audible "CHECK CAUTION"
-Secondary indications without a bus tie (on the failed side) -RECT FAIL / ENG1 FUEL PRESS LO / AFCS 1 FAIL
a) Diagnose EP
b) What are the associated NOTE(s) with this EP?
c) What other EP may you consider executing as a result of this EP?
SINGLE GENERATOR FAILURE CAUTION
Note 1: THe defective generator must be left OFF, if the fault is cleared and power is restored and a generator switch is left ON, unanticipated transients in the helicopter may occur.
Note 2: Load shedding should be considered by the crew and chosen with respect to current aircraft operating conditions and mission compatibility.
Note 3: If no bus tie exists, the hydraulic oil cooler fans will not function
Consider: AFT XMSN HOT
Life rafts sufficient for all POB are required on all Army aircraft during flights made more than _____ minutes flying time or ____ NM from the nearest shoreline.
Life rafts sufficient for all POB are required on all Army aircraft during flights made more than 30 minutes flying time or 100 NM from the nearest shoreline.
1) VFR training
2) Time limit
3) VFR mission
4) Excessie IFR delays
5) Hazardous weather
6) Single pilot
When you are flying multiship on R3005, and the flight goes IIMC, when do you turn to the assigned headings per the APG?
After all aircraft report reaching assigned altitudes
This can occur when rearward flight or a tailwind exceeds 40 KCAS
A dual FADEC Primary channel failure may occur. These conditions should be avoided
These are the maximum range and maximum glide distance airspeeds during autorotation.
80 KCAS and 105 KCAS
How much buoyancy is provided by the LPU-40 when inflated by both CO2 cylinders?
65 lbs.
This is the standard circling approach area radius/distance on a category A approach
1.3 miles
At what minimum forecasted ceiling and/or visibility are you required to carry IFR approach charts, IFR enroute charts and IFR area charts?
Less than 3’000’ and/or less than 5 SM