Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
74 Cards in this Set
- Front
- Back
|
Max. Ramp Wt. |
85,870 lb |
|
|
Max. T/O Wt. |
85,517 |
|
|
Max. Lnd. Wt. |
74,957 lb |
|
|
Max. Zero Fuel Wt. |
69,886 lb |
|
|
Min. Runway Width |
100 ft (SW) |
|
|
Wing Span |
93 ft 11 in. |
|
|
Aircraft Length |
103 ft 11 in. |
|
|
Tail Height |
32 ft 4 in. |
|
|
Max. Ops. Alt. |
41,000 ft |
|
|
Max. T/O & Lnd Altitude |
8,000 ft |
|
|
Max. Temp. T/O & Lnd |
ISA + 35 C (52 C) |
|
|
Min. Temp. T/O & Lnd |
-40 C |
|
|
Max. RWY Slope T/O & Land |
+/- 2% |
|
|
Max. Tailwind |
15 kt |
|
|
Max. Single Pack Operations |
31,000 ft |
|
|
VMO SL - 8,000' |
300 |
|
|
VMO 10,000 - Mach Transition |
320 |
|
|
MMO |
0.82 |
|
|
VA |
240 |
|
|
VLO EXT |
250 |
|
|
VLE RET |
250 |
|
|
VLE |
250 |
|
|
V Tire |
195 |
|
|
V RAT DEPLOY MAX |
VMO/MMO |
|
|
V Min (to provide electr. pwr.) |
130 |
|
|
VB (below 10,000) |
250 |
|
|
VB (10,000 ft and above) |
270/.76M (whichever is lower) |
|
|
V wiper ops max |
250 (SW) |
|
|
V window |
160 |
|
|
VFE1 |
230 |
|
|
VFE 2 |
215 |
|
|
VFE 3 |
200 |
|
|
VFE 4 |
180 |
|
|
VFE 5 |
180 |
|
|
VFE FULL |
165 |
|
|
Max. Rcmnd. Xwnd. Dry |
38 kt |
|
|
Max. Rcmnd. Xwnd. Wet |
31 kt |
|
|
Max. Rcmnd. Xwnd. Compacted Snow |
20 kt |
|
|
Max. Rcmnd. Xwnd. Stnd. Wtr./Slush/Wet/Dry Snow |
18 kt |
|
|
Max. Rcmnd. Xwnd. With ice |
12 kt |
|
|
Max. Alt. Flaps/Slats Extended |
20,000 ft |
|
|
Flaps/Slats Enroute Ops |
Prohibited |
|
|
Min. Spoiler Speed |
180 kt |
|
|
Flaps/Slats Cat II Approach |
Flaps 5 (Mandatory) |
|
|
Landing Flaps Full Go around |
Flaps 4 |
|
|
Landing Flaps 5 Go Around |
Flaps 2 |
|
|
Min. Batt. Voltage |
22.5 V |
|
|
Eng. Start Max. ITT |
815 C |
|
|
Min. Eng. Start Oil Temp. |
- 40 C |
|
|
Min. Eng. Start Oil Press. |
25 PSI |
|
|
Engine Starter Run Time Limit (Ground) |
Start 1&2 (90 Sec. 10 Sec. Off) Start 3 - 5 (90 Sec. 5 Min. Off) |
|
|
Engine Starter Run Time Limit ( In FLight) |
Start 1&2 (120 Sec. 10 Sec. Off) Start 3 - 5 (120 Sec. 5 Min. Off) |
|
|
Engine Starter Run Time Limit Dry Motoring |
Dry Motor 1 (90 Sec. 5 Min. Off) 2 - 5 (30 Sec. 5 Min. Off) |
|
|
Eng. Start with tailwind Limitation |
N1 must indicate positive increase before starter cut out @ 50% N2 |
|
|
Takeoff with Automatic Takeoff Thrust Control System (ATTCS) OFF |
Is not Authorized |
|
|
Max. Fuel Capacity |
20,935 lb |
|
|
Max. Altitude For APU Operation & Generator usage |
33,000 ft |
|
|
Max. Altitude for APU BLEED Use |
15,000 ft |
|
|
Max. Altitude for APU assisted Engine Start |
21,000 ft |
|
|
Max. Differential Pressurization Up to 37,000 ft |
7.8 PSI |
|
|
Max. Differential Pressurization Above 37,000 ft |
8.34 PSI |
|
|
Max. Differential Pressure |
8.77 PSI |
|
|
Max. Differential Neg. Pressure |
- 0.5 PSI |
|
|
Max. Differential Pressure Takeoff and Landing |
0.2 PSI |
|
|
Min. Hydraulic Reservoir Temp. For Engine Start |
- 18 C |
|
|
Max. Fuel Imbalane |
794 lb |
|
|
Min. Fuel Tank Temp. |
- 40 C |
|
|
Fuel Crossfeed must be selected OFF for |
Takeoff and Landing |
|
|
After the EICAS is energized how many seconds do you need to wait before starting the APU |
30 Seconds |
|
|
How long can you leave the aircraft unattended with the APU running |
5 minutes (SW) |
|
|
Simultaneous use of the APU bleed and HP cart is |
Prohibited |
|
|
APU Starter Run Time Limit |
Start 1&2 (60 Sec. Off) Start 3 (5 Min. Off) |
|
|
Temp. Limit for APU Start & continuous operation |
- 54 C to ISA + 35 C |
|
|
Max. Altitude to Start APU |
30,000 ft |
