14 Class B Regulations Flashcards
For a Class B AC with all engines operational, what are the Take Off Climb conditions?
- Min climb gradient
- Power setting
- Gear position
- Flap position
- Min speed
- Steady climb gradient of at least 4% with:
- T/O power on each engine
- Landing gear extended (unless it can be retracted in <= 7sec)
- Flaps in T/O configuration
- Climb speed not less than the greater of 1.2Vs1 or 1.1Vmca
For a Class B AC with one engine operational at 400ft, what are the Take Off Climb conditions?
- Climb gradient
- Power setting
- Gear
- Flap
- Speed
- Steady positive climb gradient with:
- Critical engine inoperable and prop in min drag position
- Remaining engine at T/O power
- Landing gear up
- Flaps in T/O position
- Climb speed equal to that at 50ft
For a Class B AC with one engine operational at 1500ft, what are the Take Off Climb conditions?
- Climb gradient
- Power setting
- Gear
- Flap
- Speed
- Steady climb gradient >= 0.75% with:
- Critical engine inoperable and prop in min drag position
- Remaining engine not more than max continuous power
- Landing gear and flaps retracted
- Climb speed not less than 1.2Vs1
For a Class B AC, what are the Gross to Net safety factors regarding Take Off Distance?
TOD x 1.25 <= TORA
Or if there is a stopway and/or clearway
TOD <= TORA
TOD x 1.30 <= ASDA
TOD x 1.15 <= TODA
For a Class B AC, what are the T/O surface safety factors for:
- Dry Grass (<20cm)
- Wet Grass (<20cm)
- Wet Paved
- Dry Grass: 1.20
- Wet Grass: 1.30
- Wet Paved: 1.00
For a Class B AC, what are the T/O slope safety factors?
- Up to 2% upslope: 5% increase for each 1% upslope
- Above 2% upslope requires approval of authority
- Downslope: no adjustment
For a Class B AC, what are the dimensions for a straight Semi/Half Width?
- Centre section: 60m + 0.5 x Wing Span
- Angled outer section: 0.125 x D
- Outer section max width (half width): 60+(0.5 x Wing Span) + 0.125 X D
- Where D is distance from the reference zone
For a Class B AC, what are the maximum Half Width’s if a change of track is required for:
- VMC (or good Nav Aid)
- IMC
- VMC with 0 to 15 degrees track change: 300m
- VMC with >15 degrees track change: 600m
- IMC with 0 to 15 degrees track change: 600m
- IMC with >15 degrees track change: 900m
For a Class B AC, what are the Landing slope safety factors?
- Downslope up to 2%: 5% increase per 1% downslope
- No correction for upslope of 2% or less
For a Class B AC, what is the safety factor for landing on Grass?
1.15
For a Class B AC, what are the limitations on the Net Take Off Flight Path with a cloud base above 1500 ft?
0.77 all engine gradient
For a Class B AC, what are the limitations on the Net Take Off Flight Path with a cloud base below 1500 ft?
- 0.77 all engine gradient
- Assume one engine fails at the cloud base
For a Class B multi engine AC, what are the limitations for En-Route?
- AC is capable of continuous flight at or above the minimum altitude
- Assume AC to be no higher than the altitude where ROC is 300Ft/min
- En-route gradient is degraded by 0.5%
For a Class B AC, what is the public safety factor for Landing?
LD / 0.7 = Net LD
For a Class B AC, what is the safety factor for landing on a Wet Paved surface?
1.15
For a Class B AC, on a bulked (Landing Climb) all engines, what is required regarding:
- Climb gradient
- Thrust
- Gear
- Flaps
- Climb speed
- 2.5%
- Not more thrust than is available 8 sec after thrust levers moved from idle
- Gear extended
- Flaps in landing configuration
- Climb speed = Vref
For a Class B AC, on a bulked (Landing Climb) what climb speed must be achieved?
1.2 Vs1
For a Class B AC, what set of safety factors (take off or landing) should be used for a Bulked (Landing Climb)?
Take off factors
For a Class B AC, what are the regulations for Vr?
Vr (velocity rotate) is the faster of 1.05 Vmc or 1.1 Vs1
For the MEP, what are the minimum speeds required during the climb (V2), all engines operating?
Must be faster than 1.2 Vs1 and 1.1 Vmc
For a Class B AC, on a bulked (Landing Climb) with one engine inoperable, what is required regarding:
- Climb gradient
- Thrust
- Gear
- Flaps
- Climb speed
- 0.75% at 1500 ft
- Remaining engine not more than MCT
- Gear up
- Flaps up
- Climb speed >= 1.2 Vs1
Regarding the MEP, what is the minimum climb gradient required after T/O, all engines operating?
4%
Regarding the MEP, what is the minimum speed required after T/O, all engines operating?
No less than the greater of:
- 1.1 Vmc
- 1.2 Vs1
Regarding the MEP, what are the requirements for the initial climb, one engine inoperable, <= 300ft?
Assumes no engine fail
Regarding the MEP, what are the requirements for the initial climb, one engine inoperable:
- Climb gradient above 400ft
- Climb gradient at 1500ft
- Speed
- 400ft+: measurably positive
- 1500ft: 0.75%
- Spd: >= 1.2 Vs1
