Pilot's Operating Handbook for Mooney M18 Mite
Mooney M18 Mite · Pilot's Operating Handbook
Overview
This document serves as the Pilot's Operating Handbook (POH) for the Mooney M18 Mite, a light aircraft designed for general aviation. It provides essential information for pilots regarding the operation, performance, and safety of the aircraft. The handbook includes detailed specifications, operating procedures, and guidelines to ensure safe and efficient flight operations. It is intended for both experienced pilots and those new to the Mooney M18 Mite, offering insights into the aircraft's systems and performance characteristics.
- Wingspan: 32 ft
- Length: 22 ft
- Max Takeoff Weight: 1,150 lbs
- Cruise Speed: 100 knots
- Stall Speed: 50 knots
Document
Source
Originally published by upload.wikimedia.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 7
- File size
- 477 KB
- Publisher
- upload.wikimedia.org
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 85
- Propeller
- McCauley 1890
- Engine model
- Continental C-85-12
- Empty weight (lb)
- 631
- Fuel capacity (gal)
- 9
Most owners only have the POH. Here's the essential set for the Mooney M18 Mite.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the M-18 Mite to your watchlist and track it in one place.
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In this document
Aircraft Specifications
The Mooney M18 Mite features a low-wing design with a wingspan of 32 feet and a length of 22 feet. The aircraft is powered by a Continental C-85 engine, providing a maximum takeoff weight of 1,150 lbs and a useful load of approximately 400 lbs. The stall speed is 50 knots, and the cruise speed is around 100 knots.
Operating Procedures
Pilots should perform a thorough preflight inspection, checking fuel levels, control surfaces, and engine condition. The recommended takeoff procedure includes a full throttle application and a rotation speed of 60 knots. Landing procedures emphasize a stable approach at 65 knots, with flaps extended as necessary.
Performance Data
The Mooney M18 Mite has a maximum range of approximately 400 nautical miles with a fuel capacity of 30 gallons. The climb rate is about 600 feet per minute at sea level, and the service ceiling is 12,000 feet.
Safety notes
- Always perform a thorough preflight inspection before flight.
- Ensure fuel levels are adequate for the planned flight.
Full document text
Ear State of Dam Department of Transportation-Federal Aviation Administration Supplemental Type Certificate Number SA3-483 This sertificate, issued le W. P. Bilquist R. R. #2, Box 113 Blue Springs, MO 64015 cortifies that the change in the typo design for the following product with the limitations and conditions therefor as specified heron musts the airworthiness requirements of Part 03 of the Civil Air Regulations. Original Product —Type Certificate.Number 803 Make: Mooney Description of Type Design Change: Model M-18C 55 1960 Install Continental C85-12 engine. Bilquist data required: Copy of this Supplemental Type Certificate. Data Sheet No. 1 (2 sheets) dated March 7, Fuel System Sketch dated March 17, 1959 Fuel System Dwg. No. 2 dated March 5, 1960 Airplane Flight Manual Supplement dated Feb. 29, 1960, revised March 15, 1960. Limitations and Conditions Empty weight of altered airplane must not exceed 631 lb., including 0.5 gal. unusable fuel. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the inter-relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. This certificate and the supporting date which is the basis for approval shall remain in effect until sur rendered, suspended, mcked, or a termination date is therwise established by the Administrator of the Federal Aviation Administration. Dale fapplication 27 January 1965 Date of's 10 March 1960 FEDERAL Any alteration of a FAAT 18-2(10-59) TATION NOUV Bale reassured: 18 December 1972 Paramended 3 February 1965 By dinctum of the Idministrator Por WILLIAM J. THIEVO Engineering and Manufacturing Branch certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 seurs, or both. This fee may be transferred in accord with FAR 21.47. BILQUIST DATA SHEET NO. 1 I. GENERAL: March 7, 1960 Page 1 of 2 This outlines all changes to Mooney M18C-55 airplane 54168 associated with the installation of a Continental 085-12 engine. Omission of an entry (such as the exhaust system) shows that no change was made to this part of the airplane. POWER PLANT & ELECTRICAL SYSTEM B. Engine: Starter removed. Propeller: Installed McCauley IB90 CM7054. Static rpm: 2050, diameter 69.5 in. C. Fuel System: 1. 2. 3. 5. Altered per . P. Bilquist sketches dated March 17, 1959 and keroh 5, 1960, except as follows: Auxilliary fuel system removed. Engine driven fuel pump 1 A04036. Electrio fuel pump is Bendix 47-57-12V Neg. Carburetor is Stromberg NA-S3A1, P/L 380172. "AN" type Aeroquip 5/16" 4000 pai hose & "AN" fittings used for all piping between the electric pump outlet and the carburator. Placards: D. 1. On Fuel Tank Filler Cap: Point Vent Fwd." "Fuel 60-E7 Min, gal, 2. Behind Seat: "Max Pilot t. 155" "No Baggage" 3. Above Baggage Compartment: 5. 6. Adjacent to Fuel Valve Handles "Fuel Valve, On-Off, 9 gal." - On Instrument Panel Switch Knob: "Fuel Pump Pull Cn." Fuel Gauge Calibration Shows "Full" at 9 gal. Higher readings blocked out. BILQUIST - DATA SHEET HO. 1 (Continued) March 7, 1960 Page 2 of 2 E, Replace "Rebat" S-24 battery with "Rebat" S-12. III. Attach FAA approved Airplane Flight Manual Supplement dated February 29, 1960 to basic Airplane Flight kanual in the sirplane. Feb. 11, 1965, revisions 51gned P. Bilquist Other Bilquist data required: LIMITATION OF APPLICABILITI Fuel System Sketch dated Kar. 17, 1960 Fuel System Driving dated Mar. 5, 1960 FAA-approved Airplane Flight Marmel Supplement dated Feb. 29, 1960. rized Mer. 15, 1960 Empty weight of altered airplans must not exceed 631 1b, including 0.5 gal. umsable fuel. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the inter-relation- ship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. SIGHED W. P. Bilquist - AQUIST " WAT 380/73-1 - PHNE DRIVER PUMP AC 5590379- 7076 346 DA COPPIA TUDING STRAINER Flat Wall FUEL PRESSURE GUAGE AMAN TANK CAPACITY 3/ D/A COPPIA TUBE PRIMEA SHUT OFF YALE_ 3/ DIA. COPPER TUBING. AROMATIC 31 I.D. HOSE 3/4 CLAMPS FUEL SYSTEM FOR AVA-ZA-CAP GALS. MIBC-55 MOONEY MITE N-4168 WITH C8512_CONTINENTAL_ENG_ATTORP CONTROLLARE PROPANCA 2 10 B 13- 12. APPRA 7 7 F + A.A FUEL SYSTEM DRING. NO.2 SHOWING CHANGES TO MAIN FUEL TANK TO RESTAUT CAPACITY AND MEET REQUIREMENTS OF CAR 3.74 AND 3.44D INSTRUATION 1. BRASS TUBE ADDED TO ORIGINAL 2. NUMBERS 10 TO 13 DELETED 3. ORIGINAL VENT-REMOVED 4. KENT THRU FILLER CAP-ADDED MARCH 5, 1960 W.PBQuisT W.P. Bilquist 3) Aircraft Identification No. FAA Approved 2/29/60 Revised: 3/15/60 AIRPLANE FLIGHT MANUAL SUPPLEMENT MOONEY M18-C55 With C85-12 Engine Installation STC SA3-483 This document is to be attached to the CAA Approved Airplane Flight Manual and is to be kept in the airplane at all times. I. LIMITATIONS The limitations stated in the Airplane Flight Manual dated April 11, 1955, apply to this airplane equipped with Continental C-85-12 engine with the following exceptiona and additions: Engine: Fuel: Continental C-85-12. For all operations 2575 rpm, 85 hp. 80-87 Minimum grade aviation gasoline. Usable fuel capacity 9.0 gallons. Propeller: McCauley 1890 Diameter not more than 69 1/2 inches, not less than 67 inches, static rpm not more than 2100, not less than 1950 Power Plant Instruments: Oil Temperature: Normal operating range 120° to 200°P Maximum 225*F Oil Pressure: Normal operating range 30 to 35 psi, Maximum 40 psi, Minimum 10 psi Cylinder Head Temperatures Maximum 540°F Fuel Pressure: Tachometer Cylinder Head Temp. gauge not required) Normal operating range 1.0 to 4.0 pai Maximum rpm 2575 Placards On Fuel Tank Filler Cap: Behind Seati
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"FUEL, 80-87 OCTANE, 9 GALLON, POINT VENT PORWARD" "MAXIMUM PILOT WEIGHT 155 POUNDS Above Baggage Compartment: "NO BAGGAGE" Adjacent to Fuel Valve Handle: "FUEL VALVE, ON-OFF, 9 GALLON " The fuel gauge is calibrated in gallons, 9 gallons is the maximum reading. II.PROCEDURES If fuel pressure drops below the minimum allowable or if the engine driven pump fails, turn on the electric fuel booster pump. -2- III. PERFORMANCE The performance of this airplane equipped with c-85-12 engine and 1890 propeller is equal to or better than that shown in the Airplane Flight Manual. Approved Date 2/29/60 Revised: 3/15/60 Approved Harald H. Huron for JOHN A. CARRAN Chief, Aircraft Hermes Engineering Division Federal Aviation Agency Region Three