# TCDS A-2-599: Fairchild Hiller Corporation - Type: Type certificate data sheet - Status: Current - Holder: Fairchild Hiller Corporation - Revision: 0 - Revised: December 19, 1949 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Data sheet PDF: https://openairdocs.org/files/sha256/35/84/3584fce559ffd928819eff4288cb6ed78374364f9610dd3f45869ad13391eb47 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1B541B8CE8D86E34852567350067E7CA.0001 - Page: https://openairdocs.org/tcds/A-2-599 ## Models (1) As the data sheet lists them. - M-84-C ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. - - DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION A-2-599 FAIRCHILD M-84-C December 19, 1949 AIRCRAFT SPECIFICATION NO. A-2-599 Manufacturer Fairchild Engine and Airplane Corporation Hagerstown, Maryland I - Model M-84-C, 4 PCLM, Approved September 12, 1949 Engine Continental W-670-6N Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2075 rpm (220 hp) Airspeed limits Level flight or climb 150 mph True Ind. Glide or dive 202 mph True Ind. Flaps extended 106 mph True Ind. C.G. range (+18.1) to (+25.2) at 2900 lbs. (+21.1) to (+25.2) at 3300 lbs. Straight line variation between points given. Effect of retracting landing gear 0 in, lbs. 3300 3100 2900 18 20 22 24 26 Inches Aft of Datum Gross Wt. in Lbs. Forw'd Limit Aft Limit Empty weight C.G. range None Datum Leading edge of wing at root section Leveling means Lugs on front and rear stabilizer attachment belts, left side. Maximum weight 3300 lbs. No. seats 4 (2 at +12, 2 at +62) Maximum baggage 50 lbs. (+86) Fuel capacity 48 gals. (+39) Oil capacity 4.1 gals. (-26) Control surface movements Aileron 34° up 25.5° down Flaps 55° down Elevator 26° up 25° down Elevator trim tabs 3° up 26° down Rudder 34° left 31° right Serial Nos. eligible 6200 only Required equipment Items 1, 2, 201, 202, 204, 301, 302, 303 A-2-599 Page 2 Specifications Pertinent to All Models Certification basis Airworthiness Certificate only (CAR 4a.031) Export eligibility Eligible for export to all countries except as follows, subject to the provisions of ASR No. 312 (MOP 2-4 contains same information): Canada - landplane - eligible skiplane - not eligible. Equipment: A Plus (+) or minus (-) preceding an item of equipment indicates net weight change when that item is installed. Propellers and Propeller Accessories 1. Propeller-Beech Controllable, Hub Model R201-100, Blades Model R201-211 Diameter: Not over 88 in., not under 86 in. High pitch setting 20.5°, Low pitch setting 8.0° Blade angle determined at 30 in. radius Propeller must be indexed in the zero position on the crankshaft. 56 lbs. (-62) 2. Propeller controls Electric Motor, Control and Installation 6 lbs. (-28) Landing Gear 201. Two main wheel-brake assemblies, 7.50-10, Type III. (a) Goodrich Model 752M Wheel Assembly No. G-3-73M Brake Assembly No. G-2-122 26 lbs. (+9) 202. Main wheel 4-ply-rating tires, 6.50-10, Type III with tubes 32 lbs. (+9) 204. Tail wheel assembly, 10 in. Type I (a) Variety Model VGC-10-10, full swiveling steerable, with 6-ply-rating tire and tube 6 lbs. (+216) Electrical Equipment 301. Generator-Eclipse Type 308, Model 4 16 lbs. (-34) 302. Battery-Reading Model R-24-L 25 lbs. (+85) 303. Starter-Eclipse Model E-801 8 lbs. (-33) NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in the aircraft at the time of original certification and at all times thereafter. NOTE 2. The following placards must be displayed in front of and in clear view of the pilots: "Intentional spinning prohibited." "Use 80 minimum octane aviation gasoline." - END - ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Fairchild M-84-C](https://openairdocs.org/model/fairchild-m-84-c): 0 aircraft (registry code 3371631) ## STCs approved under this data sheet (8) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.