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Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
DIMENSIONS AND GENERAL DATA (CONT'D) Landing gear (Cont’d)
Tire size 38 in. 21 in.
Max loaded tire pressure Main gear track Nose gear track Wheel base (max.) 172 psi. 13 ft. 8 in. (4.18 m) 13.14 in. (33.4 cm) 40 ft. 2 in. (12.25 m) 154 psi
Areas
Equivalent wing area (including ailerons, flaps spoilers and area within the fuselage) Horizontal tail area (Gross) Vertical tail area (Gross) 1022 sq. ft. 245 sq. ft. 186 sq. ft. (94.95 sq. m) (22.76 sq. m) (17.28 sq. m)
Doors
Passenger door (LH. fwd)
Height to sill (one step below the floor line) Width Height to sill (at floor line) 6 ft. 2 in. 3 ft. 5 ft. 4 in. (188 m) (0.91 m) (163 m)
Baggage compartment door (LH, aft)
Height Width Height to sill (floor line) 2 ft. 9 in. 3 ft. 7 in. 6 ft. 7 in. (0.84 m) (1.09 m) (2.01 m)
Volume 2 Flight Crew Operating Manual Rev 12, Aug 14, 2006
ANTENNA LOCATION SCHEMATIC
SATCOM
(If installed)
VHF COMM #1 VHF COMM #3 VOR/LOC
FGF0110_003
Personnel should not stand nearby and in front of the radar antenna when it is transmitting. When the antenna is not scanning, the danger increases.
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
VISUAL EYE REFERENCES FOR GROUND OPERATION
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
STEERING RADII
Steering radii are shown below.
STEERING RADII SCHEMATIC
NOTE
Maximum steering Symmetrical and idle thrust No differential braking 75° steering angle 3° slip Dry runway Slow continuous turn Max A/C weight AFT CG.
FGF0110_005
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
TURNING RADII
Minimum paving width for 180° turn . 65 ft. (19.92 m)
TURNING RADII SCHEMATIC
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
JET EXHAUST SINGLE ENGINE GROUND IDLE THRUST
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
JET EXHAUST SINGLE ENGINE TAKE-OFF THRUST
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
JET EXHAUST TWO ENGINE GROUND IDLE THRUST
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
JET EXHAUST TWO ENGINE TAKE-OFF THRUST
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
AIRPLANE JACKING
Three jacking points are provided, one on the forward fuselage and one on each wing rear spar for jacking the complete airplane.
JACKING POINTS SCHEMATIC
SUPPORT BEAM
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