Weight & Balance for Mooney M20TN Acclaim Type S

Full document text

F.A.A. APPROVED AIRPLANE FLIGHT MANUAL MOONEY MARK 200 MOONEY AIRCRAFT, INC. Louis Schreiner Field Serial No.. Registration No.. Kerrville, Texas APPROVED /s/ H. H. Slaughter Chief, Engineering & Mfg. Branch Federal Aviation Agency Southwest Region DATE OF APPROVAL 20 October '61 FOREWORD This Manual has been prepared for the guidance of flight personnel who operate the Mooney Mark 20C.. It is hoped that all pilots will read the Manual thoroughly and use it as a ready reference. It should be pointed out that the limitations in the Manual are mandatory and that the Manual must be kept in the airplane at all times. TABLE OF CONTENTS OPERATING LIMITATIONS OPERATING PROCEDURE Page 1 4 WEIGHT & BALANCE DATA (Loading Schedule) Insert MOONEY M200 FLIGHT MANUAL Mooney Aircraft, Inc. Revision Page Α 4 B 1 નં C 6 20 LOG OF REVISIONS Date FAA Approval 8-10-62 11-9-62 /s/ J.D. Ludwig. 4/17/63 JA Ludwig FAA APPROVED Power Plant Limitations OPERATING LIMITATIONS PAGE 1 Engine Lycoming Model 0-360-AID Lycoming Model 0-360-AIA Limit for all Operations - 2700 RPM, 180 HP No continuous operation in the range of 2000 RPM to 2250 RPM Maximum Allowable Cylinder Head Temperature 500 Degrees F. Fuel 91/96 Octane Aviation Gasoline, 48 Gal. Usable Capacity; 24 gal. each tank. Full Rich Mixture required for prolonged M/C power operation at S/L in climb. Auxiliary Electric Fuel Pump Provided (Use for take-off and landing) Oil - 8 Quart Capacity Maximum Allowable Oil Temperature Propeller Hub Hartzell Blades Diameter HC-C2YK-1 7666-2 74 inches 245 Degrees F. Propeller McCauley Hub Blades 2D34C53-A 74E-0 Diameter 74 inches Stall warning indicator is inoperative with master switch off. Revised 11-9-62 FAA APPROVED Airspeed Limitations Never Exceed Speed 189 MPH C.A.S. Maximum Structural Cruising Speed 150 MPH C.A.S. Maximum Maneuvering Speed 132 MPH C.A.S. Maximum Gear Operating Speed 120 MPH C.A.S. Maximum Gear Extended Speed 120 MPH C.A.S. 100 MPH C.A.S. PAGE 2 Maximun Flap Operating Speed Instrument Dial Markings Airspeed Serial No. 1852, 1940 and on Radial Red Line דין 189 MPH (Never Exceed Speed Which is the Maximum Safe Airspeed) Yellow Arc 150 to 189 MPH (Denotes Range of Speeds in Which Operations Should Be Conducted with Caution and Only in Smooth Air) Green Arc 70 to 150 MPH (Denotes Normal Operating Speed Range) White Arc 63 to 100 MPH (Denotes Speed Range in Which Flaps May be Safely Lowered) Tachometer Serial No. 1852, 1940 and on Radial Red Line (Rated) Green Arc Narrow (Rated Operating Range) Green Arc Wide (Recommended Operating Range) 2700 RPM 2300 to 2700 RPM 2300 to 2500 RPM Red Arc Narrow (No Continuous Operation in this Range) 2000 to 2250 RPM Cylinder Head Temperature Serial No. 1852, 1940 and on Radial Red Line (Maximum) Green Arc (Operating Range) 500 Degrees F. 350 to 500 Degrees F. Oil Pressure Serial No. 1852, 1940 and on Radial Red Line (Minimum) Radial Red Line (Maximum) Green Arc (Operating Range) 60 PSI 85 PSI 60 to 85 PSI FAA APPROVED PAGE 3 Turn & Bank Voltmeter Serial No. 1852, 1940 & on Red radial line (minimum) Green arc (operating range) Vacuum Warning Lights in Artificial Horizion "High" light "Low" light 10 volts 10 to 14 volts 5.0 inches of Hg. 3.5 inches of Hg.. FAA APPROVED Fuel Pressure Radial Red Line (Minimum) Radial Red Line (Maximum) Green Arc-Wide (Desired Range) Green Arc-Narrow (Normal Operating Range) Oil Temperature Radial Red Line (Maximum) Green Arc (Operating Range) Flight Load Factors Maximum Positive Load Factors Maximum Negative Load Factory 3.8 No inverted maneuvers approved PAGE 4 0.5 PSI 6.0 PSI 2.5 to 3.5 PSI .5 to 6.0 PSI 245 Degrees F. 100 to 245 Degrees F. Gross Weight and Center of Gravity Limitations M 2575 pounds Maximum Weight Center of Gravity Datum Most Forward 42 Inches (15% MAC) Gear Down, 2100 Pounds Forward Gross 46.5 Inches (22.6% MAC) Gear Down, 2575 Pounds Rear Gross 49.0 Inches (26.8% MAC) Gear Down, 2575 Pounds Center Line of Nose Gear Attachment Bolts. (Airplane Sta. 0) 33 Inches Forward of Wing Leading Edge at Wing Sta. 59.25. (Inboard Edge of Stall Strip) Note: Warning: See Weight and Balance Section for Loading Schedule The front seat positions can adversely effect C.G. limitations at most rearward loading. Allowable baggage weight dictated by seat positions. Placards (1) This Airplane Must Be Operated As A Normal Category Airplane In Compliance With The Approved Airplane Flight Manual. Acrobatics, Maneuvers, Including Spins, Are Prohibited. (2) Maximum Speed, Landing Gear Extended 120 MPH Maximum Speed for Operation Of Landing Gear (3) (On Storm Window) Do Not Open Above 150 MPH (4) Load In Accordance With Loading Schedule Maximum Baggage Limit 120 Pounds DOTAD 120 MPH (5) Cowl Flap-Pull To Open-Do Not Open Above 150 MPH In Case of Engine Fire Turn Cabin Heater OFF All (7) Pull To Retract Flaps (8) Retract Flaps After Landing (9) WARNING: Do Not Exceed 10 Pounds in This Compartment. See Aircraft Loading Schedule Data for Baggage Compartment Allowable. General Landings when 90° crosswind component is more than 17 MPH not recommended. Rev. (A) dated August 10, 1962 FAA APPROVED Pre-Flight PAGE 5 OPERATING PROCEDURES Check Oil (6 Qts. Minimum) Check Fuel & Secure Filler Caps Drain Gascolator and 3 Quick Drains Inspect Airplane for Defects Starting Check to Assure Gear is LOCKED Fasten Seat Belts Fuel Valve ON (Right or Left Main) Master Switch ON Mixture Rich Auxiliary Fuel Pump ON for Pressure Build Up, Then OFF Brakes Set Clear Prop Visually & Verbally Pump Throttle to Prime Engage Starter-Return Magneto Switch to Both After Start Check Oil Pressure After Engine Starts Open Cowl Flaps Take-Off Check Controls for Freedom and Proper Operation Check Fuel Quantity & Pressure Gauges Check Instruments. Set Trim to Take-off Position Check Cowl Flaps Set Wing Flaps to 15° Turn ON Auxiliary Fuel Pump Check Mags at 1500 RPM Check Carb. Heat-Return to OFF Check Governor & Prop Operation at 2200 RPM Governor Control Full Forward