CIRRUS SR NORMAL CHECKLIST. BEFORE START CHECK . PAGE 1. The POH remains the official source of information. BEFORE TAXI CHECK. P/N CIRRUS PILOT CHECKLIST. MODEL SR Primary Flight Display. ILS. ILS. TAS KTS. GS 98 KTS. OAT 11°C. SAV. DTK °. ISSUED: March P/N Quick Reference Checklist for. SR20 Serials and Subsequent with Cirrus Perspective+ Avionics.
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Preflight. Complete. Brakes. Hold Altimeter. Set. Documents. A R O W Weight and Balance Within Limits. Doors. Closed Fuel. Correct Tank. Avionics. Off. Cirrus Design. Pilot's Operating Handbook. SR List of Effective Pages. List of Effective . This Pilot's Operating Handbook (POH) has been prepared by Cirrus. Free Cirrus SR20 Checklists to Download. The web's largest collection of checklists.
CHECK appropriate for flight conditions 4. Power Lever Alternate Induction Air ON A gradual loss of manifold pressure and eventual engine roughness may result from the formation of intake ice.
Opening the alternate engine air will provide air for engine operation if the normal source is blocked or the air filter is iced over.
Ignition Switch An obvious power loss in single ignition operation indicates magneto or spark plug trouble. Lean the mixture to the recommended cruise setting.
If engine does not smooth out in several minutes, try a richer mixture setting. Emergency Procedures Section 3A Abnormal Procedures Section Normal Procedures Section Performance Data Section Supplements Section Safety Information The data presented in this Handbook is the result of extensive flight tests and is approved by the Federal Aviation Administration.
However, as new procedures or performance data are developed, they will be sent to the owner of record for each airplane. Therefore, it is very important that all revisions be properly incorporated into this Handbook as soon as they are received.
Temporary revisions are printed on yellow paper, normally cover only one topic or procedure, and are issued to provide safety related information or other time sensitive information where the rigor of providing a numbered revision is not possible in the time allowed.
All the information needed to properly file a temporary revision is included on the revision itself.
Typically, a temporary revision is superseded and replaced by the next numbered revision. Logical and convenient Tables of Contents are located at the beginning of each section to aid in locating specific data within that section.
The Handbook is divided into ten sections as follows: Section General Section Limitations Section Emergency Procedures Section 3A Abnormal Procedures Section Normal Procedures Section Performance Data Section Supplements Section Safety Information The data presented in this Handbook is the result of extensive flight tests and is approved by the Federal Aviation Administration. However, as new procedures or performance data are developed, they will be sent to the owner of record for each airplane.Model - Serial Num.
Revision bars are not used at reissues of the Handbook.
Return ignition switch to the BOTH position unless extreme roughness dictates the use of a single magneto. ON Circuit Breakers… Revision bars are not used at reissues of the Handbook.
A sudden engine roughness or misfiring is usually evidence of a magneto malfunction. Airplane Control…………………………….. OFF Fuel Pump………………………… Forward Slip to land if needed for improved forward visibility. OFF Wing Flaps……..