Supplemental Airplane Flight Manual #1
CESSNA U206F · Flight Manual Supplement
Overview
This document is a supplemental airplane flight manual for Cessna models U206F, U206G, TU206F, and TU206G, specifically detailing the operation of the aircraft with Flint Aero wing tip transfer fuel tanks installed. It includes limitations, procedures, and performance information relevant to these modifications.
- Maximum takeoff gross weight increased to 3,800 lb.
- Wing tip transfer tanks hold 30 U.S. gal. (29.8 U.S. gal. usable).
- Transfer fuel during level flight when main tanks are not supplying engine.
- VNE reduced by 5 mph per 1,000 ft. above 18,000 ft. for turbocharged models.
- Takeoff distances increased by 10% at 3,800 lb. gross weight.
- Stall speeds remain the same as unmodified aircraft at 3,600 lb. gross weight.
- Monitor main fuel tank gauge while transferring fuel to prevent overfilling.
- Test wing tip fuel tank transfer pumps early in the flight if required.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at cdn-website.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Flight Manual Supplement
- Year ·
- 2008
- File size ·
- 4.3 MB
- Copy found at ·
- cdn-website.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Max takeoff gross weight (lb) ·
- 3800
- Usable fuel capacity us (gal) ·
- 29.8
- Wing tip tank capacity us (gal) ·
- 30
Performance
- Stall speed comparison ·
- same as unmodified at 3600 lb.
- Takeoff distance increase percent ·
- 10
What is the Supplemental Airplane Flight Manual #1?
The Supplemental Airplane Flight Manual #1 is a flight manual supplement for the CESSNA U206F, dated 2008.
What year was the Supplemental Airplane Flight Manual #1 published?
The Supplemental Airplane Flight Manual #1 — the CESSNA U206F flight manual supplement on file — is dated 2008.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA U206F.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
CESSNA U206F for sale now
Free — save the 206 to your watchlist and track it in one place.
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In this document
Limitations and Placards
Details maximum takeoff gross weight, placard requirements, and fuel transfer procedures.
Procedures
Cautions regarding testing wing tip fuel tank transfer pumps early in the flight.
Performance
Stall speeds and takeoff distances for modified aircraft compared to unmodified aircraft.
Safety notes
- Transfer fuel only when main tank is not supplying engine.
- Wing tip fuel transfer pump switch must be off during takeoff, landing, filling, and when empty.
- Reduce VNE by 5 mph per 1,000 ft. above 18,000 ft. for turbocharged models.
Full document text
FLINT AERO, INC. 1942 Joe Crosson Dr. EI Cajon, CA 92020 FAP.APPROVED SUPPLEMENTAL AI'~PLANE FLIGHT MANUAL #1 CESSNA MODELS U~~06F,U206G, TU206F, TU206G Thismanual provides information pertaining to the operation of the aircraft when Flint Aero wing tip transfer fuel tanks are installed in accordance with STC SA436EWE. For limitations, procedures, and performance information not contained in this manual, refer to the FAA-approved markings, placards and manuals. I. LIMITATIONS AND PLACARDS: Limitations: (a) Ailiandplane and floatplane versions, the TU206G amphibian, the U206F skiplane and the TU206F skiplane are cleared as follows: Maximum takeoff gross weight 3,800 lb. Forward and aft limits of CG and moment diagrams are extended with straiqnt lines to 3800 lb. Maximum landing gross weight is unchanged. Placards: Placards shall be provided as follows in the location given: (b) On instrument panel in clear view of the Pilot: "Total wing tip transfer tank fuel 30 U.S. gal. (29.8 U.S. gal. usable). Transfer fuel during level flight. Transfer fuel when each main tank is 15 to :20gallons below full and when main tank is not supplying engine. Wing tip fuel transfer pump switch must be off during takeoff, landing, filling, and when empty. Monitor main fuel tank gauge while transferring wing tip fuel to prevent over filling." (c) Adjacent to the airspeed indicator: "Reduce VNE 5 mph per 1,000 ft. above 18,000 ft." (Turbocharged models only.) (d) Adjacent to each wing tip tank filler: "'15 U.S. Gallons (14.9 U.S. Gallons usable) ** minimum grade aviation gasoline." Insert for the double asterisk ** Grade number on placards for main tanks. PROCEDURES: CAUTION: If the flight plan requires wing tip fuel to complete the flight, test both wing tip fuel tank transfer pumps early in the flight to assure fuel transfer. PERFORMANCE: Stall speeds for the airplane modified with the wing tip tanks at 3800 LBGW are the same as those of the unmodified airplane at 3600 LBGW. Takeoff distances for the modified airplane at 3800 LBGW should be increased 10% over the distances in the Cessna AFM for a 3600 LBGW airplane. Rate of climb for the modified airplane at 3HOO LBGW is the same as that of the unmodified airplane at 3600 LBGW. FAA APPROVED ~~....L4J=:~====::±'-. 4?;'~~:..·=~x:A:::c::='/:::' ===== Manager, FI~ Testl8ranch, ANM-160L Federal Avj.q.tlonAdministration Los AngelKs Aircraft Certification Office Transport Airplane Directorate II. III. Revision B Date ...•.• £~ Il, z.eiT Revision A approved July 20, 1998 gross weight inoreased to 3800 100. 3800 . J .+ 3700 3600 3500 3400 3300 (j) '"0 c: :::l 3200 ~ E 3100 0> ·m ~ ~ 3000 ~ ~ 2900 '"0 {!j (IS 0 2.800 ....J 2700 2000 2500 2400 ~~300 ~~200 2100 Center of Gravity Moment Envelope Cessna 206 land planes J: ··1 - 2000 1900 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 Loaded Aircraft Moment/lOOO - (Pound - Inches) 3/25/99 Flint Asro Inc. gross weight increased to 3800 lbs. 3BOO 3i'OO I T .+ 3HOO Center of Gravity 3!iOO Moment Envelope Cessna 206 3400 float planes 3aoo u,' -t -g " 3:,00 0 e:. :E 3'100 Ol '(jj ~ ~ 3000 t· e <i; 2900 , ~<1l 0 2:300 ...J 2700 2<600 2500 2400 2300 2200 2100 2000 50 60 '70 80 90 100 110 120 130 140 150 160 170 180 190 200 Loaded Aircraft Mornent/rooo - (Pound - Inches) 3/30199 Flint Aero Inc. gross weight increased to 3800 lbs. 3/25/9~1 Flint Aero Inc. Inches gross weight increased to 3800 lbs, 3800 =.~.::~._ ....:=~.~_-::~.--~ ~_.r-~..:-+=!= __I-' -==~:::7=-x.-~'1-~-~. ~.~.~I+=::::j. :::.=....::r:::.-::::: c-=·= _... .-- _..'::J_. -. _ .- 1-_ - - -- -' -- -.- - - 1-- -_. ._-_ - .----- .-. -.- ..- -_. . - _. .-.--. .. 1-- ..- 3700 f--- 1-_ -- -1--- == Center of Gravity I-- - 3600 E Diagram != Cessna 206 GWI --1-- -- -- == .#--1-. -- 55 3500 EI- landplanes ._- - • 1--- -- ..- - 3400 r-- _ .~_ _ .. _ _..__ .. . -- -- -- .- -~-- ==f=:i==:::...:f.::±·- --='=-=-_-- -_._.. ---I-' c-- .- - f-. --i c...=F _. -- .-1----- 3300 . .._ __ _ 1--_._ - . I----~. . ·c- --------~+=~~~--~~---- 1---- - -- --f---- ..- ._-1-- 3200 __ _/ '-- __ _ _ __ .-- __I-- ._- I ~. == -- .. -- 1--. .--. ... I--- - 1---. 1--.•- 1---_. .....-- -·-f--- .- 1-. .•-1---.. -.- ""- . -1-- -...::.::.::... _.. -1---+--+ --f-- 1-. 1--- .._-.1--. 3000 --I--- ~- ... 2900 f-- . • _. 1- .._-- -- -- .._f--- f-. f----- .. -- _. ..- ..- --... --. f---. ---- NOO +-- -- -- 1--. 1---1--- _.1-- .. -- ··---··e-· . 1---1--- zooo 35 40 50 45 3/30/99 Flint Aero me, Inches