曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

In-Flight Procedures..................................................................... 3A-6
Inadvertent Icing Encounter ...................................................... 3A-6
Inadvertent IMC Encounter....................................................... 3A-6
Door Open In Flight .................................................................. 3A-6
Landing Procedures..................................................................... 3A-7
Landing With Failed Brakes...................................................... 3A-7
Landing With Flat Tire............................................................... 3A-7
System Malfunctions.................................................................... 3A-9
Alternator Failure ...................................................................... 3A-9
Engine Indicating System Failure ........................................... 3A-11
LOW VOLTS Warning Light Illuminated ................................. 3A-11
Communications Failure ......................................................... 3A-12
Pitot Static Malfunction ........................................................... 3A-13
Electric Trim/Autopilot Failure................................................. 3A-14
Revision A5
3A-2 P/N 13772-001
Section 3A Cirrus Design
Abnormal Procedures SR22
Revision A5
Intentionally Left Blank
P/N 13772-001 3A-3
Cirrus Design Section 3A
SR22 Abnormal Procedures
Introduction
This section provides procedures for handling abnormal system and/or
flight conditions which, if followed, will maintain an acceptable level of
airworthiness or reduce operational risk. The guidelines described in
this section are to be used when an abnormal condition exists and
should be considered and applied as necessary.
Revision A5
3A-4 P/N 13772-001
Section 3A Cirrus Design
Abnormal Procedures SR22
Abnormal Procedures Guidance
Although this section provides procedures for handling most abnormal
system and/or flight conditions that could arise in the SR22, it is not a
substitute for thorough knowledge of the airplane and general aviation
techniques. A thorough study of the information in this handbook while
on the ground will help you prepare for time-critical situations in the air.
Sound judgement as well as thorough knowledge of the aircraft, its
characteristics, and the flight manual procedures are essential in the
handling of any abnormal system and/or flight condition. In addition to
the outlined items in the Abnormal Procedures, the following steps are
considered part of all abnormal situations:
• Maintain Aircraft Control
• Analyze the Situation
• Take Appropriate Action
Revision A5
P/N 13772-001 3A-5
Cirrus Design Section 3A
SR22 Abnormal Procedures
Ground Procedures
Brake Failure During Taxi
Ground steering is accomplished by differential braking. However,
increasing power may allow some rudder control due to increased
groundspeed and airflow over the rudder.
1. Engine Power......................................................... AS REQUIRED
• To stop airplane - REDUCE
• If necessary for steering - INCREASE
2. Directional Control ...............................MAINTAIN WITH RUDDER
3. Brake Pedal(s) ......................................................................PUMP
If directional control can not be maintained:
4. Mixture ..............................................................................CUTOFF
Aborted Takeoff
Use as much of the remaining runway as needed to safely bring the
airplane to a stop or to slow the airplane sufficiently to turn off the
runway.
1. Power Lever ............................................................................ IDLE
2. Brakes.................................................................... AS REQUIRED
• Caution •
For maximum brake effectiveness, retract flaps, hold control
yoke full back, and bring the airplane to a stop by smooth,
even application of the brakes to avoid loss of control and/or a
blown tire.
After a high-speed aborted takeoff, brake temperatures will be
elevated; subsequent aborted takeoffs or other high-energy
use of the brakes may cause brake overheat, failure and
possibly even fire. A 25-minute cooling time is recommended
following high-energy use of the brake system before
attempting to conduct operations that may require further
high-energy braking. Brake temperature indicator should be
inspected prior to flight following a high-energy brake event
(refer to Preflight Walk-Around Checklist for detail).
Revision A9
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CIRRUS DESIGN SR22西銳22飛行員操作手冊和飛機飛行手冊(25)