曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

ROTATION SPEED VR
Refer to applicable figure entitled TAKEOFF SPEEDS, Section V.
TAKEOFF SAFETY SPEED V2
Refer to applicable figure entitled TAKEOFF SPEEDS, Section V.
Limitations
FM-126 1-7
FAA Approved 5-19-2004
Change 1
OPERATIONAL LIMITS/REQUIREMENTS
TAKEOFF
Maximum Pressure Altitude.......................................................14,000 feet
Ambient Temperature ........................ Refer to Figure 1-3 and Section V
Tailwind Component
- Aircraft not modified by SB 45-72-1 .................................... 10 knots
- Aircraft modified by SB 45-72-1:
- 12,000 feet and below........................................................ 10 knots
- Above 12,000 feet................................................................. 0 knots
Runway Conditions:
Takeoff is limited to paved runways.
Runway water............................................................3/4 inch (19 mm)
HI FLOW ..................................................................................................OFF
Fuel Load ..............................Wings balanced within 200 pounds (91 kg)
EICAS.........................................................................SUMRY or FLT PAGE
Rudder Boost..............................................................................................On
EN ROUTE
Maximum Pressure Altitude ..................................................... 51,000 feet
Ambient Temperature .................................................. Refer to Figure 1-3
Fuel Load
- Aircraft 45-002 thru 45-258, and 45-260
not modified by SB 45-28-8 ..................................... Wings balanced
within 500 pounds (227 kg)
- Aircraft 45-259, 45-261 thru 45-2000
and prior aircraft modified by SB 45-28-8................ Wings balanced
within 200 pounds (91 kg)
LANDING
Maximum Pressure Altitude.......................................................14,000 feet
Ambient Temperature ........................ Refer to Figure 1-3 and Section V
Tailwind Component ...................................................................... 10 knots
Runway Conditions:
Landing is limited to paved runways.
Runway water............................................................3/4 inch (19 mm)
Pressurization ......................................................... Cabin not pressurized
Fuel Load ..............................Wings balanced within 200 pounds (91 kg)
EICAS........................................................................ SUMRY or FLT PAGE
Limitations
1-8 FM-126
FAA Approved 5-19-2004
OPERATIONAL LIMITS/REQUIREMENTS (Cont)
LIMIT MANEUVERING LOAD FACTORS
- Flaps Up.................................................................... +2.9 g to -1.0 g
- Flaps Down ............................................................... +2.0 g to 0.0 g
These acceleration values limit the bank angle in a
level coordinated turn to 70° (flaps up) and 60° (flaps
down).
EICAS or MFD
SUMRY or FLT page must be selected for takeoff and landing.
FLAPS
Do not extend flaps above 18,000 feet.
GEAR
Do not extend gear above 18,000 feet.
MANEUVERS
No aerobatic maneuvers, including spins, are approved.
Intentional stalls are prohibited above 18,000 feet.
SEAT BELTS AND SHOULDER HARNESSES
Seat belts must be worn by all occupants during takeoff and landing.
When a seat is equipped with a shoulder harness, it must be worn by
the occupant during takeoff and landing.
The lavatory seat is certified for takeoff and landing
using the seat belt only. This seat is not equipped
with a shoulder harness.
NOTE
NOTE
Limitations
FM-126 1-9
FAA Approved 5-19-2004
Change 1
OPERATIONAL LIMITS/REQUIREMENTS (Cont)
AMBIENT TEMPERATURE LIMITS
Figure 1-3
GROUND OPERATING TEMPERATURE
If the aircraft is cold soaked on the ground for an extended period of
time at an ambient temperature colder than -23°C (-9°F), the aircraft
and its components must be warmed to -23°C (-9°F) or above prior to
start.
The cabin temperature must be -15°C (+5°F) or warmer prior to takeoff.
-100
0
10000
20000
30000
40000
50000
-75 -50 -25 0 25 50 75
STATIC AIR TEMPERATURE (SAT) — °C
PRESSURE ALTITUDE — FEET
45-180
Aircraft 45-006 thru 45-017 not
modified by SB 45-26-1.
TAKEOFF
AND
LANDING
Limitations
1-10 FM-126
FAA Approved 5-19-2004
SYSTEM LIMITS
AUTOMATIC DIRECTION FINDER (ADF)
(Aircraft 45-006 thru 45-011 not modified by SB 45-34-2)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Bombardier_Learjet-Limitations(5)