SMM Flashcards
(39 cards)
List the checks in the 24 hour checks - 7(+1 as per SMM) items
Power Lever Test light
Beta Back-up system
Auto Feather system
Propeller Governor
Electrical System Check
Ancillary Electrics
Pneumatics check
ADF test
Takeoff brief contents
_____ of takeoff
_____ and _____ speeds
_____ in the event of an airborne _____
_____ procedures
Questions
Type
Decision, Safety
Intentions, emergency
Departure
Call for takeoff power should not be done prior to _____
gaining rudder authority.
Demonstrated max crosswind
27 kts
STOL Takeoff Restrictions
Shall not be flown from _____
Are not permitted when the _____ is unserviceable
Do not use _____ to arrest wheel vibration after takeoff
Should not be performed at _____ or in _____ conditions
Ensure that _____ and _____ are adequate to permit visual obstacle avoidance in the event of an engine failure
An _____ must be selected
the right seat (except by IPs)
auto feather
brakes
night, whiteout/greyout
ceiling, visibility
abort point
Initial 90 KIAS climb attitude
8°-12° nose up
Approximate power setting calculations
2 PSI Tq (both engines) = x fpm
or x KIAS
100 fpm
2 KIAS
Cruise descent is not to exceed _____ fpm
1000
Deleting a fix in an approach procedure in the active flight plan will
delete the entire approach.
Recommended holding airspeed and fuel flow (for planning purposes)
100 KIAS
400 lbs/hr
The Pre-Landing Check should be completed ____ the inbound track.
before intercepting
Flaps should be selected to 10° and an airspeed of 90 KIAS achieved _____ final descent.
prior to commencing
When should the aircraft be configured (10° flap 90 KIAS) when conducting an approach with a procedure turn?
On descent to a procedure turn altitude
Stabilized approach corridor begins at _____ AGL in IMC and _____ AGL in VMC
1000’
300’
Stabilized approach criteria - 8 items
(3 for different nav types, 1 for circling)
Descent rate no greater than 1000 fpm unless required and briefed
Approach and pre-landing checklists complete
The aircraft is in the landing configuration unless a delay in final flap setting is required and briefed
Non-precision ± 1 dot of course or 5° NDB
ILS localizer and glideslope ± 1 dot
PAR - no “well left/right/above/below” call
Circling - wings shall be level on final at 300’ AAE
Within -5/+10 KIAS approach speed
Circuit speed and approximate power settings
100 KIAS
18-20 psi Tq
Normal point in the circuit to call for 10° flap
Abeam the button of the runway
When planning a 0° flap landing, maintain _____ until rolled out on final.
100 KIAS
Starter Limitations
Normal and
Dry Motoring (eg No Light Start)
40 seconds
25 seconds
Practice stalls must be recovered by _____ AGL
5000’
Steps taken if in GYRO converting from Magnetic to True
1) Estimate compass change (CADET)
2) Select EFIS switch M -> T
3) Select AHRS mode MAG -> DG
Steps taken if in GYRO and True arriving at the destination in NDA
1) Estimate compass change
2) DG -> MAG -> DG
Steps taken if in GYRO and NDA and entering SDA
1) Estimate compass change (reverse of CADET)
2) Select EFIS T-> M
3) Select AHRS mode DG -> MAG
The PF shall ensure at least _____ feet of runway length is remaining when conducting a stop-and-go
1500
