ATM Flashcards
Hover
Heading +/- 10 degrees
altitude +/- 3 feet
drift +/- 3 feet
flying standards
heading +/- 10 degrees
Altitude +/- 100 ft
airspeed +/- 10 knots
Maintain ground track w/minimal drift
climb/descent +/- 200fpm
trim +/- 1/2 ball
1004 plan vfr flight
-Are aircrew capable
-Can it be done VFR w/n 95-1, FAA, local regs, SOP
-Determine procedures departure, en route, destination
-Pick routes avoiding weather, limitations, adhere to VFR cruise altitudes
-Xcountry: +/- 1nm, +/- 5 knots TAS and GS, +/- 1 min ETE, +/- 5 degrees mag headings
-fuel +/- 100lbs
-Perform risk assessment
1006 plan IFR flight
-Aircrew capability
-Can it be done IFR w/n 95-1, FAA, SOP
-Determine routes, procedures
-Select routes to avoid wx, limits, adhere to IFR cruise altitudes
-Courses +/- 5 degrees
-Select approach compatitible w/WX, determine need for alternate
-Distance +/- 1nm true airspeed +/- 5 knots ground speed +/- 5 knots ETE +/- 1 min for each leg of flight fuel required +/- 100lbs
-File flight plan
-Do RCOP
1010 PPC
-Use current software
-Compute FAT +/- 5 degrees PA +/- 1000 ft Gross weight +/- 500lbs ETF +/- 0.05
-When manual calc required calculate Q +/- 2, weight +/- 500lb, fuel +/- 100lb, airspeeds +/- 5 knots
-Correlate PPC to aircraft/mission capabilities
1011 Dynamic in flight performance
When within 3000lb max GW
after an increase of 1000 PA
after an increase of 5 degrees C
Update and find;
Max torque available
max allowable gross weight oge
Go/No go IGE OGE
AC gross weight
Weight and balance
Weight and CG through duration of flight
Any limitations ID’d
365-4 within 90 days
Pre flight inspection
Perform preflight via checklist
review AC logbook for service intervals and deficiencies
Enter appropriate info on 2408-13-1
airspace surveillance
Brief sectors/procedures
announce unplanned drift or altitude changes
Clear the AC
Announce traffic and obstacles
announce inside/outside
maintain assigned sectors
hover power check
Determine if AC exceeds max gross weight
verify gross weight
determine sufficient power for misison
slopes
Select landing area
Set parking brake before landing
heading +/- 5 degrees
no drift +/- 3 until touchdown
no drift after touchdown
Standard for All tasks
(1) Do not exceed aircraft limitations.
(2) Crewmembers will comply with all evaluation considerations, warnings, cautions, and notes in the
task.
(3) Perform crew coordination actions IAW chapter 8.
Hover standards
(1) Maintain heading ±10 degrees.
(2) Maintain altitude, ±3 feet (±5 feet for OGE). *
(3) Do not allow drift to exceed 3 feet (10 feet for OGE hover). *
(4) Maintain ground track within 3 feet.
(5) Maintain a constant rate of movement appropriate for existing conditions.
In-flight standards
(1) Maintain heading ±10 degrees.
(2) Maintain altitude ±100 feet.
(3) Maintain airspeed ±10 KIAS.
(4) Maintain ground track with minimum drift.
(5) Maintain rate of climb or descent ±200 FPM.
(6) Maintain the aircraft in trim ±1⁄2 ball width.
Standards while on APU
(1) Maintain airspace surveillance (Task 1026).
(2) Apply appropriate environmental considerations.
PC standards
-The PC is responsible for conducting the mission and for operating, securing, and servicing the aircraft they command.
-The PC will ensure that a crew briefing is done and that the mission is performed according to the mission briefing, ATC instructions, regulations, and SOP requirements.
P* responsibilities
-aircraft control
-obstacle avoidance
-proper execution of emergency procedures.
-The Pwill announce any deviation, and the reason, from instructions issued.
-The P will announce changes in altitude, attitude, airspeed, or direction.
P responsibilities
-navigation
-in-flight computations
-assisting the P* (as requested)
-properly executing emergency procedures.
-When duties permit, the P assists the P* with obstacle
clearance.
A degraded visual environment (DVE) is a circumstance where weather, obscurations or obstacle hinder the ability of the crew to determine where they are in relation to the surrounding terrain.
Utilization of the ______________ prior to encountering DVE may aid and assist in the prevention of spatial disorientation, reduce crew workload, fatigue and prevent accidents.
coupled flight director
______ reduces available ground references and may increase the possibility of spatial disorientation. Consideration should be given to reducing pilot workload with the aid of the coupled
flight director.
When conditions exist where radar altitude fluctuations are made due to terrain, obstacles, or wind, “RAD ALT” should be placed in the active standby mode by pressing and holding the collective trim button to manually control altitude with collective.
Hovering OGE
TASK 1000
Participate in a Crew Mission Briefing
- The pilot in command (PC) will acknowledge an understanding of DA Form 5484 and will actively
participate in a crew mission briefing. - The PC will ensure a mission briefing is conducted using table 4-1, or a more detailed unit-approved crew
briefing CL. - Crewmembers will acknowledge a complete understanding of the aircrew mission briefing.
TASK 1004
Plan a Visual Flight Rules Flight
- Determine whether the aircrew and aircraft are capable of completing the assigned mission.
- Determine whether the flight can be performed under VFR IAW AR 95-1, applicable Federal Aviation
Regulations FARs)/host-nation regulations, local regulations, and SOPs. - Determine the departure, en route, and destination procedures.
- Select route(s) and altitudes that avoid hazardous weather conditions; do not exceed aircraft or equipment
limitations, and conform to VFR cruising altitudes IAW DOD FLIP. - For cross-country flights, determine the distance ±1 nautical mile, true airspeed ±5 knots, ground speed ±5
knots, and estimated time en route (ETE) ±1 minute for each leg of the flight. Compute magnetic heading(s) ±5
degrees. - Determine the fuel required IAW AR 95-1, ±100 pounds.
- Complete and file the flight plan IAW AR 95-1 and DOD FLIP.
- Perform mission risk assessment IAW unit SOP.
TASK 1006
Plan an Instrument Flight Rules Flight
- Determine whether the aircrew and aircraft are capable of completing the assigned mission.
- Determine whether the flight can be performed under IFR IAW AR 95-1 and applicable Federal
Aviation Regulations (FARs)/host-nation regulations, local regulations, and SOPs. - Determine the departure, enroute, and destination procedures.
- Select route(s) and altitudes that avoid hazardous weather conditions, do not exceed aircraft or equipment
limitations, and conform to IFR cruising altitudes IAW DOD FLIP. - If off airway, determine the course(s) ±5 degrees.
- Select an approach that is compatible with the weather, approach facilities, and aircraft equipment; determine
if an alternate airfield is required. - Determine distance ±1 nautical mile, true airspeed ±5 knots, ground speed ±5 knots, and ETE ±1 minutes for
each leg of the flight. - Determine the fuel required IAW AR 95-1 and TC 3-04.5, ±100 pounds.
- Complete and file the flight plan IAW AR 95-1 and the DOD FLIP.
- Perform mission risk assessment IAW unit SOP.
TASK 1010
Prepare a Performance Planning Card
- Compute all applicable items of the PPC using the most current software.
- Input the appropriate information into the software.
- Compute PPC values using accurate conditions for the time of takeoff within the following parameters:
a. Free air temperature (FAT) ±5 degrees Celsius.
b. Pressure altitude (PA) ±1,000 feet.
c. Gross weight ±500 pounds.
d. Engine torque factor (ETF) ± 0.05. - When manual calculations are required, calculate PPC values IAW the current operator’s manual and
IAW the instructions in appendix D (now known as TSP 011-60Z-IMCA and located at: FTB website.)
Compute values within following parameters:
a. Torque values ±2 percent.
b. Weight values ±500 pounds.
c. Fuel flow ±100 pounds per hour.
d. Airspeeds ±5 knots. - Correlate planning information to determine aircraft and mission capabilities.