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Cessna P206A-E User Manual

Cessna P206A-E
38 pages
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ISSUE DATE:
PO Box 2119
265 Shannon Lane
Priest River ID 83856
Page
1 of 38
8/23/10
INCORPORATED
FILE NO.
REVISION
DATE
TITLE: Supplemental Airplane Flight Manual
A-10060
03/04/15
SUBTITLE:
Cessna 206 on Model 3400 Floats
REVISION: D
FAA APPROVED
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
FOR
CESSNA 206 SERIES FLOATPLANES
MODELS: 206, P206, P206A-E, U206, U206A-G,
TU206A-G, TP206A-E, T206H
Equipped With AEROCET 3400 Amphibious Seaplane Floats
Registration No.__________________
Serial No._________________
The information contained in this document is FAA approved material
which must be applied together with the basic FAA approved airplane
placards and markings and/or FAA approved Airplane Flight Manual. This
supplemental manual must be carried in the airplane when it is modified by
the installation of the Aerocet Model 3400 amphibious seaplane floats in
accordance with Supplemental Type Certificate (STC) No. SA01257SE.
The information contained in this document supersedes the basic airplane
markings and placards and/or Flight Manual covered in the items contained
herein. For Limitations, Procedures, and Performance information not
contained in this supplement, consult the basic airplane markings and
placards, and/or Flight Manual.
FAA Approved: ________________________
Manager, Seattle Aircraft Certification Office
Date: ______________
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Cessna P206A-E Specifications

General IconGeneral
ManufacturerCessna
ModelP206A-E
Maximum Takeoff Weight3, 600 lb (1, 633 kg)
Seating Capacity6
Fuel Capacity84 US gallons (318 L)

Summary

SECTION 2. LIMITATIONS

CENTER OF GRAVITY LIMITS

Defines the acceptable range for aircraft weight distribution, essential for stability.

WEIGHT LIMITS

Specifies maximum allowable weights for various configurations, ensuring structural integrity.

AIRSPEED LIMITS

Outlines maximum and recommended airspeeds for different flight phases and configurations.

SECTION 3. EMERGENCY PROCEDURES

EMERGENCY OPERATIONAL CHECKLISTS

Step-by-step procedures for critical engine failure scenarios during takeoff.

FORCED LANDINGS

Detailed instructions for emergency landings on water and land without engine power.

LANDING GEAR MALFUNCTION PROCEDURES

Steps to follow if the landing gear fails to retract or extend properly.

GEAR UP LANDING ON LAND

Procedure for conducting a landing on land with the landing gear in the 'up' position.

MECHANICAL FAILURE

Guidance for landing gear failure when position cannot be confirmed or corrected.

SECTION 4. NORMAL PROCEDURES

TAKEOFF ON WATER

Step-by-step guide for executing a takeoff from water.

SECTION 5. PERFORMANCE

SECTION 6. WEIGHT AND BALANCE

SECTION 7. AIRPLANE AND SYSTEMS DESCRIPTIONS

EMERGENCY HAND PUMP SYSTEM

Description of the emergency hand pump system for landing gear actuation.

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