Limitations Flashcards
What is the Max Takeoff Wt
23,000 lbs.
Oper in HIGH (PAC FLOW) not approved for
TO and Landing Flight above 45,000 ft. Bleed air A/I sys on
Starter limits for start
3 starts per 30 minutes with one min rest period between cycles
Speed brakes with flaps prohibited
Below 500ft AGL
Max Ldg wt
20,000 lbs
Max number seats
Crew + PAX
15
2 Crew + 13 PAX
Time Limit to test Eng A/I On gnd above +10C
10 seconds
Max load factor Ldg
+3.5G at 20,000 lbs.
Altitude Speed brakes with flaps prohibited
Below 500ft AGL
APU Restriction on landing
TRs can only be used for 30 seconds
Spoiler Extend inflight Limit
Emergency descent only and on ground
Ground Idle Limit
Must be in HIGH for touch and Go landings
Maximum usable fuel quantity
Wings - 6484
Fuselage - 900
Max Usable- 7384
Min Spoiler Ext Speed
150 kts
Max Altitude
51,000 ft.
Radar Alt inop Limit
Must depart with flaps 20 land with full flaps
Max Alt TO and Ldg
14,000 ft
Operating in HP mode (PAC HP VLV Open) prohibited
During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI
How many vortex gens can be missing for TO
One per wing
When does pressurization begin
TO roll above 75% N1
When must all A/I systems be on
Visible moisture TAT/RAT below +10c
PAC Bleed Air Switch (PAC HP VLV OPEN max Altitude
NORM or HP above 45,000ft
Excessive climbing cabin altitude indications Light Warn horn EMR PRESS Auto descent mode
Cabin Alt 8500 ft light Warning horn 10,000 EMR Press 13,500 Auto descent mode 13,500 and Above 34,275 ft. FL350
Max Ramp wt
23,200 lbs
Max landing light ext Speed
250 kts
Rudder bias Limit
Rudder bias heater must be verified operational per preflight test
When can you select alternate Vmo
ZFW Less 15,350 lbs.
Max slush/water
0.75 inch
Max Altitude to start APU
20,000 ft
Max pressure Diff
Auto mode
Manual mode
Auto mode 9.3 paid
Manual mode 9.7
Radar Alt inop Limit
Must depart with flaps 20 land with full flaps
Spoiler Extend inflight Limit
EMR Descent Only
TR limits
Operationally checked first flight of day
Prohibited Touch and Go
Good only on paved runways
Max Turbulent sir penetration speed
200 KIAS or 0.75 Mach whichever is less
Emergency Pressurization Limit
Flight above 45,000ft. Both L and R Must be operational as per preflight test
Max tire Speed
165 kts
Oper in HIGH (PAC FLOW) not approved for
TO and Landing Flight above 45,000 ft. Bleed air A/I sys on
Cross gen start is how much of battery start
1/3 of a battery start
Maximum usable fuel quantity
Wings - 6484
Fuselage - 900
Max Usable- 7384
Ground Idle Limit
Must be in HIGH for touch and Go landings
Max altitude for takeoff and landing
14,000 ft.
Min Speed Brake Ext Speed
Vref+15
Min Alt for VNAV
500 Ft AGL
Fuselage fuel tank transfer must be started prior to
Wing fuel quantity 2,500lbs. ZFW CG aft of 327 or by 19,000 lbs.
Or
2,000 lbs. ZFW CG forward of 327 or by 19,000 lbs.
Max Alt with Lo Hyd Temp
FL450
BATT O’Temp
Steady temp?
Flashing temp?
Steady temp 60C BAT’O’TEMP Master Warn
Flashes 71C BAT’O’TEMP Master Warn
Speed brakes with flaps prohibited
Below 500ft AGL
Spoiler Extend inflight Limit
Emergency descent only and on ground
Max load factor flaps 7 to full
-0.0 tp +2.0G at 22,000 lbs
Max landing light ext Speed
250 kts
Spoiler Extend inflight Limit
Emergency descent only and on ground
When does pressurization begin
TO roll above 75% N1
Vmca
103 kts.
Max slush/water
0.75 inch
Oper in HIGH (PAC FLOW) not approved for
TO and Landing Flight above 45,000 ft. Bleed air A/I sys on
Pass Oxy Mask deploy Cabin Alt
13,500ft
What is Max VMO below 8000
275 kts.
Max Ramp wt
23,200 lbs
Cross gen start is how much of battery start
1/3 of a battery start
What is Vlo
What is Vle
Vlo and Vle 210 kts
Vfe full flaps
Full flaps 170
Max Turbulent air penetration speed
200 KIAS or 0.75 Mach whichever is less
Reverse thrust to idle by
65 kts.
Which wing feeds APU
Right Wing
Max Altitude operation of stab anti-ice prohibited
FL410
Max Altitude operation of stab anti-ice prohibited
FL410
Max zero fuel wt
16,500 lbs
Restrictions Ail Boost INOP
Basic Autopilot (Pitch & Roll
Max asymmetric fuel imbalance
Normal 200 lbs.
Emergency 800 lbs.
APU Restriction on landing
TRs can only be used for 30 seconds
GPU Min amps for starting
1,000 Amps
Max Speed Brake Ext Speed
No limit
Time limit on gnd with EFIS FAN light illuminated
10 min and must maintain VFR
Operating in HP mode (PAC HP VLV Open) prohibited
During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI
Vfe Full Flaps
170 kts
Max pressure Diff
Auto mode
Manual mode
Auto mode 9.3 paid
Manual mode 9.7
No Takeoff Warning Items
6 Items
- Cabin door light
- Trim out of Takeoff Range
- flaps up or full
- Gust lock
- Speed Brakes not down
- Spoiler hold on
Battery Limit for Eng/APU
3 Eng/APU per hour
Gen Amp Limit Takeoff Gnd ops Up to FL 410 Up to FL 470 Above FL 470 Single gen
Gen Amp Limit Takeoff 365 amps Gnd ops 300 amps Up to FL 410 300 amps 410 to FL 470 200 amps Above FL 470 200 amps Single gen 365 amps up to FL 250
When can you select alternate Vmo
ZFW Less 15,350 lbs.
Radio Alt limits for takeoff and Ldg
Must be on, operative and Tested to TO flaps 7 or land flaps 20
Radar Alt inop Limit
Must depart with flaps 20 land with full flaps
Authorized operations
5 Items
Day Night VFR IFR Known icing conditions
Operating in HP mode (PAC HP VLV Open) prohibited
During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI
Max Loaf Factor Flaps Up
-1 to +3 Gs at 23,000 lbs.
Time Limit to test Eng A/I On gnd above +10C
10 seconds
Vmcg 23,000 lbs
116 kts
Max Alt to operate both PACs on one bleed source (Isolation valve open) in HI flow
Above 25,000 ft.
When must all A/I systems be on
Visible moisture TAT/RAT below +10c
Anti skid required for TO
Must be on unless using supplement 11
Min alt autopilot use
200ft AGL
autopilot and Yaw damper must be off for TO and Ldg
Reverse thrust to idle by
65 kts.
Approved Hydraulic fluid
Color
Braco
Red
Rudder bias Limit
Rudder bias heater must be verified operational per preflight test
Max Reverse Limit
90% TO thrust
Max Ldg wt
20,000 lbs
Max altitude to operate APU
30,000 ft.
Crosswind limitations?
Without T/R deploy
With T/R deploy
Ailerons or roll Spoilers inop
Without T/R deploy 25 kts.
With T/R deploy limiting 25 kts.
Ailerons or roll Spoilers inop 10 kts
Max Tailwind component
10 kts.
Max Air Temp TO and LDG
ISA +37C
Max VMo below 8,000 ft.
275 kts.
What type engine and max thrust
Garrett TFE.731-4R/2S
4080 lbs.
What Items are on The hydraulic system
6 items
Aux system
3 items
1 Landing gear 2 NW steering 3 Spoilers 4 Speed brakes 5 Aileron boost 6 Thrust Reversers 7 Spoiler Holddown - Aux system 8 Brakes - Aux system 9 Roll spoilers - Aux System
Max altitude with Hyd Press Low or Fluid Loss
45,000 ft.
Charge batteries from GPU 4
No battery less than 23VDC
Batteries must be charged together
No longer than 4 hours
Ambient air temperature less than 100°F
Autopilot limitation
One pilot must remain in his seat with seatbelt and shoulder harness fastened during all autopilot operations.
Manual engagement of altitude hold mode is prohibited when the airplane descent rate is greater than _______ ft. per minute.
5,500
Maximum dual generator loads?
Up to 41,000 ft. 300 amps
Above 41,000 ft. 250 amps
Above 47,009 ft. 200 amps
Flap extension or landing gear is prohibited above ______ altitude.
20,000 ft.