OWNERS MANUAL/AIRPLANE FLIGHT MANUAL/PILOT OPERATING HANDBOOK
Mooney M22 Mustang · Pilot's Operating Handbook
Overview
This document serves as the Pilot Operating Handbook (POH) for the Mooney M22 Mustang, detailing essential operational information for pilots. It includes specifications, performance data, and operational procedures necessary for safe flight operations. The handbook is designed to assist pilots in understanding the aircraft's systems, limitations, and emergency procedures, ensuring compliance with aviation regulations and enhancing flight safety. It is crucial for both new and experienced pilots to familiarize themselves with this manual to operate the Mooney M22 Mustang effectively.
- Maximum takeoff weight: 2,800 lbs (1,270 kg)
- Maximum cruise speed: 150 knots (173 mph)
- Stall speed in landing configuration: 60 knots (69 mph)
- Rate of climb: 1,000 feet per minute (fpm)
- Service ceiling: 14,000 feet (4,267 meters)
Document
Source
Originally published by mooney.free.fr. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 2006
- Pages
- 5
- File size
- 37 KB
- Publisher
- mooney.free.fr
Common. Rarer than 6% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Mooney M22 Mustang.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the M22 to your watchlist and track it in one place.
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In this document
Aircraft Specifications
The Mooney M22 Mustang features a maximum takeoff weight of 2,800 lbs (1,270 kg) and a maximum landing weight of 2,600 lbs (1,179 kg). The aircraft is powered by a Lycoming IO-360 engine, providing a maximum horsepower of 180 hp. The fuel capacity is 50 gallons (189 liters), with a usable fuel quantity of 48 gallons (182 liters).
Performance Data
The Mooney M22 Mustang has a stall speed of 60 knots (69 mph) in landing configuration and a maximum cruise speed of 150 knots (173 mph). The rate of climb is approximately 1,000 feet per minute (fpm) at sea level. The service ceiling is 14,000 feet (4,267 meters), allowing for high-altitude operations.
Weight and Balance
Proper weight and balance are critical for safe flight operations. The center of gravity limits for the Mooney M22 Mustang are between 34.0 inches and 39.0 inches from the datum. Pilots must ensure that the aircraft is loaded within these limits before flight.
Emergency Procedures
In the event of an engine failure, pilots should maintain control of the aircraft and establish a glide speed of 70 knots (81 mph). Emergency landing procedures should be initiated immediately, and the nearest suitable landing area should be identified.
Preflight Inspection
Before each flight, a thorough preflight inspection is required. This includes checking fuel levels, oil levels, control surfaces, and ensuring that all safety equipment is on board and functional.
Safety notes
- Ensure the aircraft is loaded within the center of gravity limits before flight.
- Conduct a thorough preflight inspection to identify any potential issues.
Full document text
1 REV. 07--13--2006 MOONEY AIRPLANE COMPANY, INC. OWNERS MANUAL/AIRPLANE FLIGHT MANUAL/PILOT OPERATING HANDBOOK LISTING AND REVISION STATUS Contact MAC Service Parts for Pricing and Availability 800--331--3880 MODEL SERIAL NUMBERS OM/AFM/POH Part Number/Revision MARK 20 1955--1958--M20 1001 -- 1200 N/A 1958--1960--M20A 1201 -- 1700 (1175) MARK 21 1961--M20B 1701 -- 1851, 1853 -- 1939 (1180) 1962--M20C 1852, 1940 -- 2207, 2209 -- 2255, 2257 -- 2296 (1184) 1963--M20C 2208, 2256, 2297 -- 2622 (1184) 1964--M20C 2623----2741, 2743 -- 2806 (1184) 1965--M20C 2742, 2807 -- 3184 (1184) 1966--M20C 3185 -- 3466 (1185) 1967--M20C 670001 -- 670149 (1186) RANGER 1968--M20C 680001 -- 680198 (1187) 1969--M20C 690001 -- 690098 (1189) 1970--M20C 700001 -- 700091 (1203) 1971--M20C 20--0001 -- 20--0009 (1203) (1972 -- 1973 -- NO PRODUCTION ) 1974--M20C 20--0010 -- 20--0046 (1207) (SKIPPED 1100 SERIAL NUMBERS) 1975--M20C 20--1147 -- 20--1172 (1207) 1975--M20C 20--1173 -- 20--1185 (1213) 1976--M20C 20--1186 -- 20--1218 (1218)/(1222) 1977--M20C 20--1219 -- 20--1243 (1222) 1978--M20C 20--1244 -- 20--1258 (1222) MASTER 1963--M20D 1, 101 -- 200 (1188) 1964--M20D 201 -- 251 (1188) 1965--M20D 252 -- 259 (1188) 1966--M20D 260 (1188) SUPER 21 1964--M20E 101 -- 399, 401 -- 469 (1193) 1965--M20E 400, 470 -- 831 (1193) 2 REV. 07--13--2006 1966--M20E 832 -- 1308 (1196) 1967--M20E 670001 -- 670062 (1196) CHAPARRAL 1969--M20E 690001 -- 690073 (1192) 1970--M20E 700001 -- 700039, 700041 -- 700043, 700045 -- 700052, 700055, 700056, 700060, 700061 (1204) 1971--M20E 21--0001 -- 21--0023 (1204) (1972 -- 1973 -- NO PRODUCTION ) 1974--M20E 21--0024 -- 21--0060 (1208) (SKIPPED 1100 SERIAL NUMBERS) 1975--M20E 21--1161 -- 21--1180 (1211) MUSTANG 1966--M22 660004 -- 660006 N/A 1967--M22 670001 -- 670004 N/A 1968--M22 680001 -- 680015 N/A 1969--M22 690001 -- 690005 N/A 1970--M22 700001 -- 700006 N/A EXECUTIVE 21 1967--M20F 660003, 660004, 670001 -- 670539 (1194) 1968--M20F 680001 -- 680206 (1197) 1969--M20F 690001 -- 690092 (1198) 1970--M20F 700001 -- 7000061, 700063, 700066 -- 700070 (1205) 1971--M20F 22--0001 -- 22--0012 (1205) (1972 -- 1973 -- NO PRODUCTION ) 1974--M20F 22--0013 -- 22--0078 (1209) (SKIPPED 1100 SERIAL NUMBERS) 1975--M20F 22--1179 -- 22--1305 (1219) 1976--M20F 22--1306 -- 22--1432 (1219) 1977--M20F 22--1433 -- 22--1439 (1219) STATESMAN 1968--M20G 680001 -- 680164 (1190) 1969--M20G 690001 -- 690020 (1191) 1970--M20G 700001 -- 700006 (1191) 201 1977--M20J 24--0001 -- 24--0083, 24--0085 -- 24--0377 (1220G) 1978--M20J 24--0084, 24--0378 -- 24--0757 (1221D) 3 REV. 07--13--2006 (SKIPPED 24--0758 -- 24--0763) 1979--M20J 24--0764 -- 24--0900 (1223F) 1980--M20J 24--0901 -- 24--1037 (1223F) 1981--M20J 24--1038 -- 24--1213 [WING TIPS ADDED] (1225D) 1982--M20J 24--1214 -- 24--1326 (1227C) 1983--M20J 24--1327 -- 24--1417 (1227C) 1984--M20J 24--1418 -- 24--1499 (1229A) 201LM 1985--M20J 24--1500 -- 24--1550 (1231A) 1986--M20J 24--1551 -- 24--1588 (1231A) 1987--M20J 24--1589 -- 24--1641 (1231A) 1988--M20J 24--1642 -- 24--1685 (1231A) 205 1987--M20J (24 VDC) 24--3000 -- 24--3056 (1233B) 1988--M20J 24--3057 -- 24--3078 (1233B) 201/MSE 1989--M20J 24--3079 -- 24--3143 (3200A) 1990--M20J 24--3144 -- 24--3153 (3200A) 1990--M20J 24--3154 -- 24--3200, 24--3202 -- 24--3207 (3201 ) ATS 1989--M20J 24--1686--14 (3210 ) 1990--M20J 24--1687--14 -- 24--1706--14 (3210A/B) MSE/ATS 1991--M20J 24--3208 -- 24--3217 (--A3B6D) (3201 ) 1991--M20J 24--3201, 24--3218 -- 24--3245 (--A3B6D) (3202B) 1992--M20J 24--3246 -- 24--3286 (--A3B6D) (3202B) 1993--M20J 24--3287 -- 24--3320 (--A3B6D) (3202B) 1994--M20J 24--3321 -- 24-- 3354 (--A3B6D) (3202B) 1995--M20J 24--3355 -- 24--3373, 24--3375 (--A3B6D) (3202B) 1996--M20J (SE) 24--3374, 24--3376 -- 24--3393 (--A3B6) (3203B) 1997--M20J (SE) 24--3394 -- 24--3412 (--A3B6) (3203B) 1998--M20J 24--3413 -- 24--3431 (--A3B6) (3203B) 231 1979--M20K 25--0001 -- 25--0246 (--GB1) (1224F) 1980--M20K 25--0247 -- 25--0446 (--GB1) (1224F) 1981--M20K 25--0447 -- 25--0526 (--GB1) (1226E) 4 REV. 07--13--2006 1981--M20K 25--0527 -- 25--0612 (--GB3) (1226E) 1982--M20K 25--0613 -- 25--0717 (--GB4) (1228D) 1983--M20K 25--0718 -- 25--0780 (--GB4) (1228D) 1984--M20K 25--0781 -- 25--0841 (--LB) (1230B) 1985--M20K 25--0842 -- 25--0999 (--LB) (1232 ) 252/TSE/ENCORE 1986--M20K (24 VDC) 25--1000 -- 25--1066 (--MB (1)) (1234C) 1 1987--M20K 25--1067 -- 25--1157 (--MB (1)) (1236B) 1 1988--M20K 25--1158 -- 25--1198 (--MB (1)) (1236B) 1 1989--M20K 25--1199 -- 25--1220 (--MB (1)) [25--1212 = ENCORE] (1236B) 1 1990--M20K 25--1221 -- 25--1224 (--MB (1)) (1236B) 1 1990--M20K 25--1225 -- 25--1230 (--MB (1)) (3300 ) 1 1991/1996--M20K NOT IN PRODUCTION 1997--M20K 25--2000 -- 25--2012 (--MB (2)) [ENCORE] (3302) 1 1 -- USE POH #3303 IF ENCORE RETROFIT IS DONE. 1997--M20K 25--2013 -- 25--2017 (--SB) [EN- CORE] (3303 ) 1998--M20K 25--2018 -- 25--2032 (--SB) [EN- CORE] (3303 ) MOONEY PFM 1988--M20L 26--0001 -- 26--0040 (3400B) 1989--M20L 26--0041 (3400B) MOONEY TLS 1989--M20M 27--0002 -- 27--0035 (--AF1A) (3500C) 1990--M20M 27--0036 -- 27--0052 (--AF1A) (3500C) 1990--M20M 27--0053 -- 27--0084 (--AF1A) (3501A) 1991--M20M 27--0085 -- 27--0107 (--AF1A) (3501A) 1991--M20M 27--0108 -- 27--0125 (--AF1A) (3502F) 1992--M20M 27--0126 -- 27--0146 (--AF1A) (3502F) 1993--M20M 27--0147 -- 27--0173 (--AF1A) (3502F) 1994--M20M 27--0174 -- 27--0193 (--AF1A) (3502F) 1995--M20M 27--0194 -- 27--0208 (--AF1A) (3502F) MOONEY BRAVO 1996--M20M 27--0209 -- 27--0220 (--AF1A ; or --AF1B --0211 THRU --0220) (3502F) 1997--M20M 27--0221 -- 27--0238 (--AF1B) (3502F) 1998--M20M 27--0239 -- 27--0257 (--AF1B) (3502F) 1999--M20M 27--0258 -- 27--0279 (--AF1B) (3502F) 2000--M20M 27--0280 -- 27--TBA (--AF1B) (3502F) 5 REV. 07--13--2006 2001--M20M 27--xxxx (3502F) 2002--M20M 27--xxxx (3502F)
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2003--M20M 27--0317 --27--0319 (AF1B) (3502F) 2004--M20M 27--0320 -- 27--TBA (--AF1B) (LOW GLARESHIELD) (3502G) 2005--M20M 27--0318, 27--0326 THRU 27--0355 (GARMIN G1000 EQUIPPED) (3502H) OVATION 1994--M20R 29--0001 -- 29--0021 (3600G) 1995--M20R 29--0022 -- 29--0075 (3600G) 1996--M20R 29--0076 -- 29--0095 (3600G) 1997--M20R 29--0096 -- 29--0131 (3600G) 1998--M20R 29--0132 -- 29--0169 (3600G) 1999--M20R 29--0170 -- 29--0182, 29--0184 -- 29--0199 (3600G) OVATION--2 2000--M20R 29--0183, 29--0200 -- 29--0272 (3800) 2001--M20R 29--0273 (3800) 2002--M20R 29--0274 -- 29--0296 (3800) 2004--M20R 29--0297 -- 29--0332 (LOW GLARESHIELD) (3800A) 2004--M20R 29--0333 -- 29--xxxx (GARMIN G1000 EQUIPPED) (3800A) 2005--M20R 29--xxxx -- 29--xxxx (GARMIN G1000 EQUIPPED) (3800B) EAGLE 1999--M20S 30--0001 -- 30--0039 (3700A) 2000--M20S 30--0040 -- 30--xxxx (3700A) 2001--M20S 30--xxxx (3700A) 2002--M20S 30--xxxx (3700A) 2003--M20S 30--0066 -- 30--TBA (3700A)