Limitations Flashcards
Maximum zero fuel weight:
49,000 lbs
Maximum ramp weight:
75,000 lbs
Maximum takeoff weight:
74,600 lbs
Maximum landing weight:
66,000 lbs
ASC 007 lowers it to 58,500 lbs for Cat C approaches
Maximum permissible fuel imbalance in-flight:
- Up to weight 55,000 = 2000lbs
- Greater than 55,000 less than 60,500 = consult chart
- 60,500 to 75,000 = 400 lbs
Maximum cabin differentials:
9.94 psi
0. 3 psi for taxi, takeoff or landing
Single engine autopilot coupled go-around:
Not Approved
Minimum autopilot engagement height:
200 ft
Minimum autopilot disengage height:
- 60 ft from an ILS Approach
- 50 ft below MDA/DA from an LNAV/VNAV Approach
Use of auto-throttles on single-engine approach:
Not permitted
Use of speed brakes with the HMG in operation:
Slow Operation (approx 3 seconds for full range of movement)
IDG electrical load limit:
45% (18kVa) when ambient temperature is greater than 43°c (110°f)
Speed brakes not approved for extension in-flight when:
Flaps are at 39°, or landing gear extended
Take off permitted with automatic ground spoilers inoperative provided:
- Antiskid is operative
- 20° flaps are used
- Cowl and wing anti-ice systems are not used
Usable fuel capacity:
29,500 lbs
Wing anti-icing must be turned on:
If icing conditions are imminent, or immediately upon detection of ice formation on wings, winglets or windshield edges
Cowl anti-icing is required on the ground:
When SAT is +10°c or below and visible moisture, precipitation or wet runways are present
Cowl anti-icing is required in flight:
As indicated in the cowl anti-icing table, when visible moisture or precipitation is present or when signs of icing are observed
Procedure to shed engine ice in flight is:
Quickly retard one engine at a time to idle, hold for 5 seconds and then accelerate engine to 85% LP RPM for 2 seconds
Take off is permitted with anti-skid inoperative, provided:
- Runway is dry
- Ground spoilers are operative
- 20° flaps are used
- Cowl and wing anti-ice systems are not used
Do not operate weather radar on the ground:
- During refueling of the airplane
- Within 300 ft of fueling operations
- Within 49 ft of ground personnel
A current FMS database is required for:
GPS Approaches
Localizer based approaches must be flown using the following displayed / coupled navigation source:
NAV (green data)
The following approaches may be flown using FMS as the displayed / coupled source:
RNAV (GPS)
VOR, VOR/DME, VOR/DME RNAV
NDB
GPS
TCAS operation with one engine inoperative:
TA only as operating mode
Maximum speed for RVSM operations:
0.85 M
Crew and passenger oxygen masks are not approved for use above:
40,000 ft cabin altitude
Newer Scott EROS crew masks is approved for use to a cabin altitude of 45,000 ft
General EICAS range marking colors:
Green or White = Normal Range Values
Amber = Caution Range Values
Red = Warning Range Values
APU starting limits (battery power):
Three consecutive start attempts, followed by 1 hour cooldown
APU starting limits (external DC power):
3 start attempts, 15 minute cool down in between each attempt
Maximum APU operating altitude:
37,000 ft
APU generator electrical load limit:
- 100% (40kVa) Sea Level to 37,000 ft
- 85% between 30,000 and 37,000 at speeds faster than 0.85 M
Maximum engine TGT prior to ground start:
200 °c
Maximum takeoff TGT:
800°c
5 minutes both engines
10 minutes on one engine
Maximum continuous TGT:
715°c
Maximum crosswind component for engine start:
25 knots
Maximum tailwind component for engine start:
25 knots
Stabilized engine operation on the ground (static) is prohibited between:
60% and 72% LP RPM
Maximum runway slope for takeoff and landing operations:
+/- 2%
Maximum tailwind component approved for takeoff and landing:
10 knots
Maximum approved airport pressure altitude for takeoff or landing:
15,000 ft
Maximum operating altitude:
45,000 ft
Maximum operating altitude with the yaw damper inoperative, coupled with failure of the mach trim compensation:
41,000 ft
Maximum landing gear extension altitude:
20,000 ft
Maximum altitude for extending flaps 39°:
20,000 ft
Maximum altitude for extending flaps 10 or 20 degrees:
25,000 ft
Minimum control speed, air:
106 kcas
Minimum control speed, landing:
99 kcas
Minimum control speed, ground:
109 kcas
Maneuvering speed (Va):
206 kcas
Flaps extended speeds (Vfe / Mfe):
Takeoff (10°): 250 kcas / 0.60 m
T/O APP (20°): 220 kcas / 0.60 m
Down (39°): 180 kcas / 0.60 m
Landing gear extended speed (Vle / Mle):
250 kcas / 0.70 M
Landing gear operation speeds (Vlo / Mlo):
225 kcas / 0.70 M (normal operation) 175 kcas (alternate operation)
Minimum speeds with yaw damper inoperative:
210 knots above 20,000 ft
Use reference table below 20,000 ft
Maximum speed with Mach trim or electric elevator trim inoperative:
0.75 M
Turbulence penetration speeds:
270 kcas / 0.75 M above 10,000 ft
240 kcas below 10,000 ft
Maximum tire speed:
195 knots
Maximum speed with emergency stabilizer trim armed, autopilot engaged and a jammed elevator:
270 kcas / 0.75 M
Max demonstrated crosswind for takeoff and landing
24 knots
