Checkride Additional GK Flashcards
(48 cards)
AOA Comp Fail Effect on TP Stalls
AOA circuit breaker (batt buss front cockpit)
Land as soon as practical
Stick shaker and aural tones/warnings for CWS and LDG GR will be inop
Fly known pitch and power settings
Oil tank and system capacities
Oil tank: 10 quarts
Oil systems: 18.5 quarts
Oil specification
MIL -PRF-23699
Battery voltage limits
23.5 minimum
do not connect external power if below 22.0
Prop limits
62-80%
Overspeed limit is 110%
VMO (max operating speed)
316
MMO (max operating mach)
0.67
VG (turbulent air penetration speed)
195 max
180 recommended
Prohibited maneuvers
inverted spins
inverted stalls
aggravated spins past 2 turns
spins with pcl above idle
spins above/below 22000/10000ft PA
abrupt cross-controlled (snap) maneuvers
tail slides
aerobatics with greater than 50lbs fuel imbalance
Weight limits
max ramp weight: 6550
max TO weight: 6500
max LDG wight: 6500
max zero fuel weight: 5500
max weight in baggage compartment: 80lbs
max weight on glareshield: 8.5lbs
Barrier limits
taxi over arresting cables as slowly as possible, avoid contact with support donuts
TO/land beyond arresting cables
taxiing over lowered net barries should be avoided, idle and discontinue braking before crossing
raised web barrier should never be used, steer around or eject
Icing limits
climb or descend out of icing layer
aerobatics prohibited when icing is present
30 degree AOB and 2Gs
approach speed increased by 10 knots
fuel limits
aerobatics prohibited below 150lbs each side
799PPH all phases of flight
engine driven high pressure pump is limited to 10 hours without back up of boost pump/engine driven low pressure pump
max fuel imbalance
50 pounds
runway surface limits
tarmac, concrete or similar
Eejction seat nude BW limits
103lbs - 231lbs
How does RCR affect TOLD
Max abort speed increases as RCR increases
Maximum braking speed
if max abort speed is > (VB-20knots), then VB-20 is the new abort speed
Max Range
level flight speed that produces most miles (white triangle, 4.9 units)
Max Endurance
speed for minimum fuel flow in level flight time (white diamond 8.8 units)
Landing distance assumptions
a 3 degree approach to the 50ft obstacle height
idle power and threshold speed as determined by chart at 50ft
2 second delay from touchdown to initiation of braking
max braking once a/c is firmly on the ground
braking friction coefficient for dry asphalt or concrete rwy corresponds to an RCR of 23
FOD prevention
do not approach an operating engine
no excessive power
avoid prop/jet blast from other a/c
loose items stowed/secured before opening canopy
do not place anything on the canopy
GPS approach minimums used
LNAV and circling lines of minima listed
When not to request high key from initial
a/c between 5 & 2 NM on straight in
a/c between report high key and lowkey
when a/c reports OH field direct to VFR entry
orbiting high key
high pattern