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

Figure 06−24−6 N1 Corrections − Packs OFF, Cowl and Wing Anti-Icing On 06−24−11
Figure 06−24−7 Take-Off Weight Limited by Climb Requirements 06−24−13
Figure 06−24−8 VR Adjustment 06−24−15
Figure 06−24−9 V2 Adjustment 06−24−15
Figure 06−24−10 Obstacle Clearance Reference Climb Gradient Corrections 06−24−16
Figure 06−24−11 Net Take-Off Flight Path 06−24−17
Figure 06−24−12 Approach Climb Gradient Corrections 06−24−19
Figure 06−24−13 Landing Climb Gradient Corrections 06−24−20
Figure 06−24−14 Landing Weight Limited by Climb Requirements 06−24−22
APPROACHES BELOW 4.5 DEGREES
Figure 06−25−1 Approach Glidepath Angle Operating Limit 06−25−2
Figure 06−25−2 Precision (ILS/PAR) Approaches below 4.5 Degrees 06−25−5
SUPPLEMENTARY PROCEDURES
Table of Contents
Vol. 1 06−00−15
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
Page
STEEP APPROACHES UP TO 5.5 DEGREES
Figure 06−26−1 Precision (ILS/PAR) Approaches up to 5.5 Degrees 06−26−6
Figure 06−26−2 Landing Field Length and Landing Speed, Flaps 45 06−26−11
Figure 06−26−3 Distance from Glideslope System Position on Runway to
Full Stop 06−26−13
SUPPLEMENTARY PROCEDURES
Table of Contents
Vol. 1 06−00−16
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
Page
1. INTRODUCTION
Supplementary procedures are normal procedures not related to a specific phase of flight, and
are accomplished “as required”, and not routinely performed on each flight. That may include
procedures to conform with Air Traffic Control (ATC) instructions and other considerations, and
for the operation of airplane systems which are used either as an option or as the situation
warrants (e.g. Cat II operations, etc).
The supplementary procedures contained in this chapter are organized by system, sequenced
similar to the Operating Manual (FCOM) Vol. 2, Systems Description. These recommended
procedures are usually accomplished by recall (memory). However, certain procedures which are
not performed frequently should preferably be performed with reference to the FCOM.
SUPPLEMENTARY PROCEDURES
Preface
Vol. 1 06−01−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
SUPPLEMENTARY PROCEDURES
Preface
Vol. 1 06−01−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. AIR-CONDITIONING ON THE GROUND USING THE APU
The APU is used to provide air-conditioning on the ground, as follows:
(1) APU................................................................ Operating PLT
• Check that APU AVAIL light is on.
(2) 10TH STAGE, L and R BLEED
valves ..................................................................Closed PLT
• Switch/light is pressed out and check that L and R CLOSED lights are on.
(3) APU LCV ............................................................... Open PLT
• Press in switch/light and check that APU LCV OPEN light comes on.
(4) 10TH STAGE ISOL valve.....................................OPEN PLT
• Press in switch/light and check that 10TH ISOL OPEN light comes on.
(5) AIR-CONDITIONING, L and R
PACKS ......................................................................On PLT
• Press in switch/lights and check that L and R PACK OFF lights go out.
(6) Cabin and cockpit mode and
temperature .............................................Set as desired CPLT
NOTE
Flight compartment and duct temperatures should not exceed 71°C (160°F)
or be less than 3°C (37°F) during manual mode operations.
2. AIR-CONDITIONING FROM ENGINE BLEEDS DURING TAKE-OFF
If the engine bleed is desired to provide air-conditioning during take-off, transfer bleeds as
follows:
(1) 10TH STAGE, R BLEED AIR ................................ Open PLT
(2) 10TH STAGE ISOL valve....................................Closed PLT
(3) 10TH STAGE, L BLEED AIR................................. Open PLT
(4) APU LCV .................................................. Check closed PLT
• Press out LCV switch/light to match APU LCV position, i.e. closed.
3. UNPRESSURIZED TAKE-OFF AND LANDING PROCEDURE
The procedures outlined below are recommended when performing a no-engine bleed (for
whatever reason) take-off and landing, with the APU inoperative.
　
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