# TCDS TC 788: Fleet Aircraft Ltd. - Type: Type certificate data sheet - Status: Current - Holder: Fleet Aircraft Ltd. - Revision: 0 - Revised: January 29, 1947 - Product: Aircraft, Small Airplane - Data sheet PDF: https://openairdocs.org/files/sha256/91/27/9127493d3e3d1dfc6b9aef1ad09c3a6922ec2ee3b8b6f264d086ac4e27163b72 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4193A81005EF170285256737004CFDD9.0001 - Page: https://openairdocs.org/tcds/TC%20788 ## Models (1) As the data sheet lists them. - Fleet 80 ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: Fleet 80, 2 PCIM-SM SPEC. NUMBER: 788 (Approved 1/29/47) Engine Continental C-55-12J Fuel 73 minimum octane aviation Jasoline Engine limits 2575 cpm (85 hp) Airspeed limits Level flight or climb - 112 mph Glide or dive - 150 mph C.G. range (+66.6) (14.85 percent MAC) to (+71.55) (*67.4) (16.11 percent MAC) to (+75) (28.17 percent Datun firewall (58.25 in. forward of b axle main I.G.) MAC 63 in. L.E. MAC 57.25 in. Leveling means Firewall perpendicular Maximum weight No. of seats 2 (adjustable fron +76 to +80) Baggage 105 lbs. maximum (+116) Fuel capacity Oil capacity Control surface movements 30 degrees up, 20 degrees down, + 2 degrees 23 degrees up, 14 degrees down, +2 degrees Rudd degrees left, 30 degrees right, +2 degrees Elevator trin tab: 20 degrees up, 20 degrees down, 45 degrees Cert. basis Canadian Certificate of Airworthiness for Export Serial Nos. eligible 002 and up in accordance with the provisions of NOTE A (See also NOTE 1) Required equipment: Landplane: 1(a), 101, 201, 202, 203, 204, 205 and 601 seaplan 101, 204, 206, 301, 302, 303, 304 and 601 (Items included under "Required equipment" may not be removed unless replaced by approred equivalent items. The effect upon balance of all eyuip- ment changes must be computed and the aircraft operation record revised accordingly.) Propeller and Propeller Accessories Propeller - fixed pitch wooc Sensenich 74PC-48 for - 12J engine, or 74PK-48 for - 12JF engine, including weight of propeller bub (Landplane only) . Propeller throttle - not more than 2150, not less than 2000. 14 Ibs. (0) 76RC-40 for - 12J engine, Or 76RK-40 fOI - 12JF Propeller limits: at full throttle - not more than 2280, not less than 2180. 14 1bs. (0) 2. Propeller - plastic ground adjustable Hartzell MA-1200 with blade Static rpm at full throttle; less than 2000,3 degrees; (Seaplane) - Not more than 2400, minimum blade angle pitch setting Wot more than 2400, not less than 2300; approved blade setting 3. Propeller spinner Neglect weight Engine and Engine Accessories 101. Air Maze- Air Filter 102. Engine (a) Continental C-75-12J (landplane only) Engine limits - all opera- tions 2275 rpm (75 hp) Continental C-85-12FJ (0) Engine limits - all operations 2575 rpm (85 hp) 103. Long range fuel tank installation (25 gallons) (See NOTE 4) (LT. +) Landing Gear and Floats 201. 6.00-6 single disk wheels and brakes (Goodyear Drawing OD127 #1) with tires 202. Scott tail wheel - Type No. 3-245 203. Scott 5/8" diameter brake master cylinder 204. Brake pedals Fleet Drawing No. 80-2121-130 205. Parking brake installation, Fleet Drawing No. 80-2124-000 206. Float installation to Fleet Drawin] 80-7000 +117.5 (+60) OI 80-7001 (+60) Fleet floats to Fleet Drawing No. 80-7110 0I 207. Ski installation to F.M.A.I. Drawing No. 80-6300 Rev. Northwest main ski to Nw. 17-03001 Issue E and Northwest Drawing No. 17-03002 Issue D. Ski installation to F.M.A.L. Drawing No. 90-6400 using F.M.A. L. main ski to Drawing No. 80-6410 and F.M.A. L. tail ski to Drawing NO. 80-5420. Electrical Equipment 301. Battery installation - Reading Type 241 *26 1bs. (+31) 302. Starter installation - Continental Drawing No. 50309 +17 Ibs. (+23.5) 303. External starting plug installation F.M.A.L. Drawing No. 80-2052-000 +0.5 1bs. (+31.5) 304. Generator instailation, voltage regulator and ammeter (Continental Drawing No. 40435 and 40483) +12 1hs. (+39) Miscell entor ted above Elevator trim tab control NOTE A. The Canadian Certificate of Airworthiness for Export must be submitted for each individual aircraft for which application for certification is made and each aircraft shall be inspected by a CAA inspector. NOTE 1. (a) All aircraft serial numbers 142 and up as well as a number of aircraft prior to serial number 142 are factory equipped with attachments for skis (Item 207 (b)). Other aircraft may be made eligible for Item 207(a) or 207 (b) by welding on suitable serial numbers 016, 025 and up are factory equipped with Aircraft serial numbers 142 and up are factory fitted with seaplane cowling and baffles. All aircraft are eligible when suitable fittings are welded on and when seaplane baffles are installed according to Fleet Modification No. 80-27. NOTE 2. The following placard must be appropriately displayed: "Intentional Spins Prohibited if Baggage Carried." Aircraft should be checked for conformity with the followl adjacent The words "fuel 19 gals." and "73 octane" should be marked to the fuel tank filler opening. The words "oil 4.5 quarts" should be marked adjacent to the oi. filler opening. Cockpit instruments should be marked to indicate the proper airspeed and engine limitations. ``` ## ADs None name its models. ## STCs approved under this data sheet (3) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. 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