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3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
DFM0604_005 ntofp_anti_ice_uc_ha.uni
PERFORMANCE
Obstacle Clearance
06−04−7
REV 66, Feb 01/07
Obstacle Clearance Reference Climb Gradient, Flaps 20° − Anti-Icing On (Page 1 of 2)
Figure 06−04−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
DFM0604_006 ntofp_anti_ice_c_ha.uni
PERFORMANCE
Obstacle Clearance
06−04−8
REV 66, Feb 01/07
Obstacle Clearance Reference Climb Gradient, Flaps 20° − Anti-Icing On (Page 2 of 2)
Figure 06−04−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
B. Net Take-Off Flight Path
Figure 06−04−5 and Figure 06−04−6 present the net take-off flight path for various
obstacle clearance reference climb gradients. These charts can be either used to:
• determine the reference climb gradient which provides a 35-foot margin between the net
flight path and an obstacle, or
• determine the net take-off flight path for a given reference climb gradient.
These charts are also used to determine the gross level-off height.
Figure 06−04−5 provides the net take-off flight path for a flaps-20° take-off, for obstacles at
a distance of up to 3,000 meters (9,843 feet) from reference zero.
Figure 06−04−6 provides the net take-off flight path for a flaps-20° take-off, for obstacles
starting at a distance of 3,000 meters (9,843 feet) from reference zero.
PERFORMANCE
Obstacle Clearance
06−04−9
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
DFM0604_007 close_obs.uni
PERFORMANCE
Obstacle Clearance
06−04−10
REV 66, Feb 01/07
Net Take-Off Flight Path, Flaps 20° − Close-In Obstacles
Figure 06−04−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
DFM0604_008 far_obs_ha.uni
PERFORMANCE
Obstacle Clearance
06−04−11
REV 66, Feb 01/07
Net Take-Off Flight Path, Flaps 20° − Far Obstacles
Figure 06−04−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
C. Conversion From Geometric Height To Pressure Height
Figure 06−04−7 is provided to convert geometric height above airport to pressure height
above airport at different temperature deviations from standard.
The chart is entered with the gross level-off height (geometric height above airport) and the
corresponding value of pressure height above airport is determined. The level-off pressure
altitude is obtained by adding the pressure height above the airport, derived from
Figure 06−04−7, to the airport pressure altitude.
NOTE
Specific take-off performance adjustments, obtained from Figure 06–03–12
(Take-Off Performance section in this chapter) must be applied when the
pressure height above the airport exceeds 1,500 feet at the end of the
second segment climb.
PERFORMANCE
Obstacle Clearance
06−04−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
DFM0604_009 GEOM_PRESS_HT
PERFORMANCE
Obstacle Clearance
06−04−13
REV 66, Feb 01/07
Geometric Height Above Airport to Pressure Height Above Airport Conversion
Figure 06−04−7
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. MAXIMUM TAKE-OFF WEIGHT LIMITED BY OBSTACLE CLEARANCE REQUIREMENTS
(CONT'D)
D. Net Acceleration Distance
The net acceleration distance, which is the horizontal distance of the level flight acceleration
segment from the point where the second segment climb is completed, is provided in
Figure 06−04−8.
E. Final Segment Net Climb Gradient
Figure 06–05–2 and Figure 06–05–3 (see next section) can be used to determine the final
segment net climb gradient to a gross height of 1,500 feet, when the gross level-off height is
　
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