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REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
4. LANDING ON CONTAMINATED RUNWAYS (CONT'D)
B. Actual Landing Distance on Contaminated Runways – Flaps 45° (Cont’d)
DFM0702_031 ALD604RC_WETICE_17JUN96
SPECIAL OPERATIONS
Operation on Wet and Contaminated Runways
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REV 66, Feb 01/07
Actual Landing Distance on Runways Contaminated With Ice − Flaps 45°
Figure 08−02−21
CL−604 Operating Manual
PSP 604−6
4. LANDING ON CONTAMINATED RUNWAYS (CONT'D)
B. Actual Landing Distance on Contaminated Runways – Flaps 45° (Cont’d)
DFM0702_032 ALD604RC_COMSNOW_1JUN96
SPECIAL OPERATIONS
Operation on Wet and Contaminated Runways
Vol. 1 08−02−01−43
REV 66, Feb 01/07
Actual Landing Distance on Runways Contaminated With Compacted Snow − Flaps 45°
Figure 08−02−22
CL−604 Operating Manual
PSP 604−6
4. LANDING ON CONTAMINATED RUNWAYS (CONT'D)
B. Actual Landing Distance on Contaminated Runways – Flaps 45° (Cont’d)
DFM0702_033 ALD604RC_LOOSNOW_13JUN96
SPECIAL OPERATIONS
Operation on Wet and Contaminated Runways
Vol. 1 08−02−01−44
REV 66, Feb 01/07
Actual Landing Distance on Runways Contaminated With Loose Snow − Flaps 45°
Figure 08−02−23
CL−604 Operating Manual
PSP 604−6
4. LANDING ON CONTAMINATED RUNWAYS (CONT'D)
B. Actual Landing Distance on Contaminated Runways – Flaps 45° (Cont’d)
DFM0702_034 ALD604RC_SLUSH_12JUN96
SPECIAL OPERATIONS
Operation on Wet and Contaminated Runways
Vol. 1 08−02−01−45
REV 66, Feb 01/07
Actual Landing Distance on Runways Contaminated With Slush/Standing Water − Flaps 45°
Figure 08−02−24
CL−604 Operating Manual
PSP 604−6
SPECIAL OPERATIONS
Operation on Wet and Contaminated Runways
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REV 66, Feb 01/07
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PSP 604−6
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INTRODUCTION
General 09−01−1
AIR - DRIVEN GENERATOR CHECKS
General 09−02−1
Manual Deployment Operational Check 09−02−1
Before Flight 09−02−1
In-Flight Procedures 09−02−1
IN-FLIGHT CHECKS
Table of Contents
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REV 66, Feb 01/07
CHAPTER 9 - IN-FLIGHT CHECKS
09−00−1
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PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
IN-FLIGHT CHECKS
Table of Contents
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PSP 604−6
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1. GENERAL
In−flight checks are special operating procedures not routinely performed every flight, and are
accomplished when certain airplane systems are to be tested for proper operation in flight. The
following recommended procedures must be adhered to, in order to ensure the safe conduct of
the functional test to be performed.
IN-FLIGHT CHECKS
Introduction
Vol. 1 09−01−1
REV 66, Feb 01/07
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PSP 604−6
IN-FLIGHT CHECKS
Introduction
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REV 66, Feb 01/07
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1. GENERAL
The following procedures are recommended to operationally check the air-driven generator
(ADG) in flight using the manual deployment system.
This check shall be carried out in Visual Meteorological Conditions (VMC). Ensure that this check
is not carried out in icing conditions.
CAUTION
1. The presence of foreign objects in the ADG bay could cause damage to the
ADG blades during deployment. Before flight, the ADG bay must be inspected to
ensure that foreign objects are not present.
On airplanes 5301 to 5407:
2. When deployed, the ADG is maintained in position by an ejection spring and
airloads. After landing, high deceleration could cause the ADG to swing forward
with resulting damage to the ADG blades and adjacent fuselage panels. When
landing with the ADG deployed, plan to use maximum landing roll-out available
to minimize deceleration.
NOTE
Once deployed, the ADG cannot be stowed during flight. Therefore,
this check should be performed at the end of a test flight. Normal
electrical power must be restored before final landing approach is
　
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