PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL MOONEY M20S

PILOT S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL MOONEY THIS HANDBOOK IN CLUDES THE MA TE RIAL RE QUIRED TO BE FUR NISHED TO THE PI LOT BY THE FED ERAL AVIA TION REGU LA TIONS, AND CON STI TUTES THE FAA AP PROVED AIR PLANE FLIGHT MAN UAL. THIS DOCU MENT MUST BE CAR RIED IN THE AIR CRAFT AT ALL TIMES. MOO NEY AIR CRAFT COR PO RA TION LOUIS SCHREI NER FIELD KERR VILLE, TEXAS 78028 SE RIAL NUM BER REG IS TRA TION NUM BER FAA AP PROVED: Mich ele M. Oswley Man ager, Air plane Cer ti fi ca tion Office FED ERAL AVIA TION ADMINISTRATION 2601 Meacham Boulevard Fort Worth, Texas 76137-0150 FAA AP PROVED in Nor mal Cate gory based on CAR PART 3 and ap pli ca ble por tions of FAR PART 23; ap pli ca ble to Model S/N listed above only; ORIGINAL IS SUE - 2-99 RE VI SION A - 8-99 POH /AFM NUMBER - 3700

MOONEY INTRODUCTION CONGRATULATIONS WEL COME TO MOONEY S NEW EST DI MEN SION IN SPEED, QUAL ITY AND ECON OMY. YOUR DE - CI SION TO SE LECT A MOO NEY AIR CRAFT HAS PLACED YOU IN AN ELITE AND DIS TINC TIVE CLASS OF AIR CRAFT OWN ERS. WE HOPE YOU FIND YOUR MOO NEY A UNIQUE FLY ING EX PE RI - ENCE, WHETHER FOR BUSI NESS OR PLEAS URE, THE MOST PROF IT ABLE EVER. - NOTICE - This manual is pro vided as an op er at ing guide for the Moo ney Model M20R. It is im por tant th at you re gard less of your pre vi ous ex pe ri ence care fully read the hand book from cover to cover and re - view it fre quently. THIS AFM MUST BE CAR RIED IN THE AIR CRAFT AT ALL TIMES. All in for ma tion and il lus tra tions in the manual are based on the lat est product in for ma tion avail able at the time of pub li ca tion ap proval and all sec tions in clud ing at tached sup ple ments are man da tory for proper op era tion of the air craft. The right is re served to make changes at any time with out no tice. Every ef fort has been made to pres ent the ma te rial in a clear and con ven ient manner to enab le you to use the manual as a ref er ence. Your co op era tion in re port ing pres en ta tion and con tentr ec om men - da tions is so lic ited. RE VIS ING THE MANUAL The i pages of this manual con tain a List of Ef fec tive Pages con tain ing a com plete cur rent listing of all pages i.e., Origi nal or Re vised. Also, in the lower right cor ner of the outlined por tion, is a box which de notes the man ual number and is sue or re vi sion of the man ual. It will be ad vanced one let ter, al pha beti cally, per re vi sion. With each re vi sion to the man ual a new List of Ef fec tive Pa ges show ing all ap pli ca pa ble re vi sions with dates of ap proval and a Log of Re vi sions page(s), with only the lat est Re vi sion shown, will be pro vided to re place the pre vi ous ones. It is the op era tors re spon sib lilty to en - sure that this manual is cur rent through the lat est pub lished re vi sion. This hand book will be kept cur rent by Moo ney Air craft Cor po ra tion when the yel low in for ma tion card in front of this hand book has been com pleted and mailed to the Serv ice Parts De part ment, Moon ey Air craft Cor po ra tion, Louis Schrei ner Field, Kerr ville, TX. 78028. ISSUED 2-99

MOONEY INTRODUCTION LIST OF EF FEC TIVE PAGES ORIGINAL..................... 2-99 REVISION A.................... 8-99 TITLE PAGE.................. ORIGINAL INTRODUCTION................. ORIGINAL i through iv..................... A v, vi.................... ORIGINAL 1-1 through 1-10................. ORIGINAL 2-1 through 2-18................. ORIGINAL 3-1 through 3-16................. ORIGINAL 4-1 through 4-16................. ORIGINAL 5-1 through 5-24................. ORIGINAL 6-1 through 6-30................. ORIGINAL 7-1 through 4.................. ORIGINAL 7-5....................... A 7-6.................... ORIGINAL 7-7....................... A 7-8 through 7-11................. ORIGINAL 7-12....................... A 7-13 through7-26................. ORIGINAL 8-1 through 8-8................. ORIGINAL 9-1 through 9-4................. ORIGINAL (with Supplements) 10-1 through 10-12................ ORIGINAL POH /AFM NUMBER - 3700 [A] This POH /AFM ef fec tive be gin ning with S/N 30-0001 ISSUED 2-99 i

INTRODUCTION MOONEY LIST OF EF FEC TIVE PAGES (con t.) POH /AFM NUMBER - 3700 [A] This POH /AFM ef fec tive with S/N 30-0001 ii ISSUED 2-99

MOONEY INTRODUCTION LOG OF RE VI SIONS RE VI SION NUM BER RE VISED PAGES DE SCRIP TION OF RE VI SIONS FAA AP PROVED DATE A Ti tle Page, i, ii, iii, iv Re vised to re flect Re vi sion A data 7-5, 7-7 Re vised Illustrations to re flect Moritz Gauges Mark ing change. 7-12 Re vised S/N Application The re vised por tions of af fected pages are in dicted by ver ti cal black lines in the margin. POH /AFM NUM BER 3700 [A] ISSUED 2-99 iii

INTRODUCTION MOONEY LOG OF RE VI SIONS (con t.) RE VI SION NUMBER RE VISED PAGES DE SCRIP TION OF RE VI SIONS FAA AP PROVED DATE POH /AFM NUM BER 3700 [A] iv ISSUED 2-99

MOONEY INTRODUCTION TA BLE OF CON TENTS TITLE.................... SECTION INTRODUCTION.................... GENERAL...................... I LIMITATIONS..................... II EMERGENCY PROCEDURES................ III NORMAL PROCEDURES................. IV PERFORMANCE.................... V WEIGHT & BALANCE.................. VI AIRPLANE & SYSTEM DESCRIPTIONS............. VII HANDLING, SERVICE & MAINTENANCE............ VIII SUPPLEMENTAL DATA.................. IX SAFETY & OPERATIONAL TIPS............... X ISSUED 2-99 v

INTRODUCTION MOONEY BLANK vi ISSUED 2-99

MOONEY SECTION I GENERAL TA BLE OF CON TENTS TITLE................... PAGE THREE VIEW................. 1-2 INTRODUCTION................. 1-3 DESCRIPTIVE DATA................ 1-3 ENGINE................. 1-3 PROPELLER................ 1-3 FUEL.................. 1-4 OIL................... 1-4 LANDING GEAR............... 1-4 MAXIMUM CERTIFICATED WEIGHTS......... 1-4 STANDARD AIRPLANE WEIGHTS.......... 1-4 CABIN & ENTRY DIMENSIONS.......... 1-5 BAGGAGE SPACE AND ENTRY DIMENSIONS...... 1-5 SPECIFIC LOADINGS............. 1-5 IDENTIFICATION PLATE............ 1-5 SYMBOLS, ABBREVIATIONS & TERMINOLOGY........ 1-5 GENERAL AIRSPEED TERMINOLOGY & SYMBOLS..... 1-5 ENGINE POWER TERMINOLOGY.......... 1-6 AIRPLANE PERFORMANCE & FLIGHT PLANNING TERMINOLOGY. 1-6 ENGINE CONTROLS & INSTRUMENTS TERMINOLOGY.... 1-7 METEOROLOGICAL TERMINOLOGY......... 1-7 WEIGHT & BALANCE TERMINOLOGY......... 1-8 MEASUREMENT CONVERSION TABLES.......... 1-8 ISSUED 2-99 1-1

SECTION I GENERAL MOONEY FIGURE 1-1 THREE VIEW - 1-2 ISSUED 2-99

MOONEY SECTION I GENERAL IN TRO DUC TION This Op era tors Man ual con forms to GAMA Speci fi ca tion No. 1 and in cludes both Manu fac tur e rs ma - te rial and FAA AP PROVED ma te rial re quired to be fur nished to the Pi lot by the ap pli ca ble Fed eral Avia tion Regu la tions. Sec tion IX con tains sup ple men tal data sup plied by Moo ney Air craft Cor po ra - tion. Sec tion I con tains in for ma tion of gen eral in ter est to the pi lot. It also con tains defini tions of the ter mi nol - ogy used in this Op era tors Man ual. This Pilot s Operating Handbook is not designed as a substitute for adequate and competent flight instruction, knowledge of current airworthiness directives, applicable federal air regulations or advisory circulars. It is not intended to be a guide for basic flight instruction or a training manual and should not be used for operational purposes unless kept in an up to date status. All limi ta tions, pro ce dures, safety prac tices, serv ic ing and main te nance re quire ments pu b lished in this POH/AFM are con sid ered man da tory for the Con tin ued Air wor thi ness of this air plane in a con di - tion equal to that of its origi nal manu fac ture. EN GINE DE SCRIP TIVE DATA Num ber of en gines.......... 1 En gine Manu fac turer..... Tele dyne Con ti nen tal Mo tors (TCM) Model.......... IO- 550-G (6) * Rec om mended TBO......... 2000 Hours Type....... Re cip ro cat ing, air cooled, fuel in jected Num ber of cyl in ders....... 6, Hori zon tally op posed Dis place ment........ 550 Cu. In. (9014 cc) Bore.......... 5.25 In. (13.3 cm) Stroke.......... 4.25 In. (10.8 cm) Com pres sion ratio.......... 8.5 : 1 Fuel Sys tem Type........... Fuel In jec tion Make............ TCM Fuel- Aviation Gaso line....... 100 oc tane - 100LL Ac ces so ries Mag ne tos......... Ben dix - S6RN- 25 Ig ni tion Har ness........ Shielded/Braided Spark Plugs....... AC 273 (or equiva lent) (18 m/m) Oil Cooler.......... TCM Full Flow Al ter na tor......... 28 Volt DC, 100 AMPS Starter........... 24 volt DC Rat ings: Maxi mum Take off Sea Level BHP/RPM...... 244/2400 PRO PEL LER Num ber............ 1 Manu fac turer.......... McCauley Model Number........ 2A34C239/90DMC- 15 * Num ber of Blades........... 2 Di ame ter (1/2 in. cut -off al lowed)...... 75 in. (190.5 cm) Type.......... Con stant Speed Gov er nor (McCauley)..... Hy drau li cally con trolled by en gine oil Blade An gles @ 30.0 in. Sta.: Low........ 19.0 de grees +/- 0.2 degrees High........ 37.5 de grees +/- 0.5 degrees * Re fer to TCDS for en gine/pro pel ler con figu ra tion re quired. ISSUED 2-99 1-3

SECTION I GENERAL MOONEY FUEL Mini mum Fuel Grade (Color).... 100 LL (Blue) or 100 Oc tane (Green) To tal Ca pac ity....... 81.0 U.S. Gal. (306.6 Li ters) Us able........ 75.0 U.S. Gal. (283.9 Li ters) OIL Oil Speci fi ca tion.......... MHS- 24 ( ) and as Ap proved by TCM. (Ref er ence En gine Main te nance & Op era tors Man ual) All Tem pera tures........ 15W50 or 20W50 Above 30 o F (-1 o C) Am bi ent Air (S.L.)...... SAE 50 Be low 50 o F (10 o C) Am bi ent Air (S.L.)..... SAE 30, 10W30 To tal Oil Ca pac ity........ 8 Qts. (7.57 li ters) Oil Filter........... Full Flow Oil grades, speci fi ca tions and chang ing rec om men da tions are con tained in SEC TION VIII. LAND ING GEAR TYPE: Elec tri cally op er ated, fully re tract able tri cy cle gear with rub ber shock discs. The main wheels have hy drau li cally op er ated disc brakes. The nose wheel is fully steer able 11 o left to 13 o right of cen - ter. Wheel Base........ 79 9/16 in. (198.91 cm) Wheel Track......... 110 in. (279.4 cm) Tire Size: Nose.......... 5.00 x 5 (6 ply) Main.......... 6.00 x 6 (6 ply) Tire Pressure Nose........... 49 PSI Main........... 42 PSI Mini mum Turn ing Radius (No brakes ap plied) Right.......... 40 ft. (12.0 m) Left.......... 48 ft. (14.4 m) MAXI MUM CER TIFI CATED WEIGHTS Gross Weight........ 3200 Lbs. (1452 Kg) Maxi mum Land ing Weight...... 3200 Lbs. (1452 Kg) Bag gage Area......... 120 Lbs. (54.4 Kg) Rear Stor age Area........ 10 Lbs. (4.5 Kg) Cargo (Rear Seats Folded Down)..... 340 Lbs. (154.2 Kg) STAN DARD AIR PLANE WEIGHTS Ba sic Empty Weight........ See Page 1-8 Use ful Load....... Var ies with in stalled equip ment. See SEC TION VI for spe cific air plane weight (pg. 6-5). 1-4 ISSUED 2-99

MOONEY SECTION I GENERAL CABIN AND ENTRY DI MEN SIONS Cabin Width (Maxi mum)....... 43.5 In. (110.5 cm) Cabin Length (Maxi mum)....... 126 In. (315 cm) Cabin Height (Maxi mum)....... 44.5 In. (113 cm) En try Width (Mini mum)....... 29.0 In. (73.4 cm) En try Height (Mini mum)....... 35.0 In. (88.9 cm) BAG GAGE SPACE AND EN TRY DI MEN SIONS Com part ment Width........ 24 In. (60.9 cm) Com part ment Length........ 43 In. (109.2 cm) Com part ment Height........ 35 In. (88.9 cm) Com part ment Vol ume......... 20.9 cu. ft. (.592 cu. m) Cargo Area (with rear seat folded down)...... 38.6 cu. ft. (1.09 cu. m) En try Height (Mini mum)....... 20.5 In. (52.1 cm) En try Width......... 17.0 In. (43.2 cm) Ground to Bot tom of Sill....... 46.0 In. (116.8 cm) SPE CIFIC LOAD INGS Wing Load ing - @ Maxi mum Gross Weight..... 18.3 lbs./sq. ft. (89.3 kg/sq. m) Power Load ing - @ Maxi mum Gross Weight..... 12.17 lbs./hp (5.52 kg/hp) IDEN TI FI CA TION PLATE All cor re spon dence re gard ing your air plane should in clude the Se rial Num ber as de pictedo n the iden - ti fi ca tion plate. The iden ti fi ca tion plate is lo cated on the left hand side, aft end of the tail cone, be low the hori zon tal sta bi lizer lead ing edge. The air craft Se rial Num ber and type cer tifi cate a re shown. SYM BOLS, AB BRE VIA TIONS & TER MI NOL OGY GEN ERAL AIR SPEED TER MI NOL OGY & SYM BOLS GS GROUND SPEED - Speed of an air plane rela tive to the ground. KCAS KIAS KTAS V a V fe V le KNOTS CALI BRATED AIR SPEED - The in di cated speed of an air craft,cor rected for po si tion and in stru ment er ror. Cali brated air speed is equal to true air speed in stan dard at mos phere at sea level. KNOTS IN DI CATED AIR SPEED - The speed of an air craft as shown on its air speed in di ca tor. IAS val ues pub lished in this hand book as sume zero in stru ment er ror. KNOTS TRUE AIRSPEED - The airspeed of an airplane relative to un dis turbed air which is the KCAS cor rected for al ti tude and tem pera ture. MA NEU VER ING SPEED - The maxi mum speed at which ap pli ca tion of full avail able aero dy namic control will not over stress the air plane. MAXI MUM FLAP EX TENDED SPEED - The high est speed per mis si ble with wing flaps in a pre scribed ex tended po si tion. MAXI MUM LAND ING GEAR EX TENDED SPEED -The maxi mum speed at which an air craft can be safely flown with the land ing gear ex tended. ISSUED 2-99 1-5

SECTION I GENERAL MOONEY GEN ERAL AIR SPEED TER MI NOL OGY & SYM BOLS (con t.) V lo MAXI MUM LAND ING GEAR OP ER AT ING SPEED - The maxi mum speed at which the land ing gear can be safely ex tended or re tracted. V ne V no V s V so V x V y NEVER EX CEED SPEED - The speed limit that may not be ex ceeded at any time. MAXI MUM STRUC TURAL CRUIS ING SPEED - The speed that should not be ex ceeded ex cept in smooth air and then only with cau tion. STALL ING SPEED - The mini mum steady flight speed at which the air plane is con trol la ble. STALL ING SPEED - The mini mum steady flight speed at which the air plane is con trol la ble in the land ing con figu ra tion. BEST ANGLE- OF- CLIMB SPEED - The air speed which de liv ers the great est gain of al ti tude in the short est pos si ble hori zon tal dis tance. BEST RATE- OF- CLIMB SPEED - The air speed which delivers the great est gain in al ti tude in the short est pos si ble time with gear and flaps up. EN GINE POWER TER MI NOL OGY BHP CHT EGT MCP MP RPM BRAKE HORSE POWER - Power de vel oped by the en gine. CYL IN DER HEAD TEM PERA TURE - Op er at ing tem pera ture of en gine cyl in der(s) be ing moni tored by sen sor unit. Ex pressed in o F. EXHAUST GAS TEMPERATURE - The exhaust gas temperature meas ured in the ex haust pipe mani fold. Ex pressed in o F. MAXI MUM CON TINU OUS POWER - The maxi mum power for takeoff, nor mal, ab nor mal or emer gency op era tions. MANI FOLD PRES SURE - Pres sure meas ured in the en gi ne s in duc tion sys tem and ex pressed in inches of mer cury (Hg). REVO LU TIONS PER MIN UTE - En gine speed. AIR PLANE PER FORM ANCE AND FLIGHT PLAN NING TER MI NOL OGY De mon- The ve loc ity of the cross wind com po nent for which ade quate strated con trol of the air plane dur ing take off and land ing test was Cross wind ac tu ally dem on strated dur ing cer ti fi ca tion. The value shown Ve loc ity is not con sid ered to be lim it ing. g Ac cel era tion due to grav ity. Serv ice The maxi mum al ti tude at which air craft at gross weight has the Ceil ing ca pa bil ity of climb ing at the rate of 100 ft/min. 1-6 ISSUED 2-99

MOONEY SECTION I GENERAL EN GINE CON TROLS & IN STRU MENTS TER MI NOL OGY Pro pel ler Con trol Throt tle Con trol The control used to se lect en gine speed. The control used to se lect en gine power by con trol ling MP. Mixture Provides a mechanical linkage to the fuel injector mixture control Control to control the size of the fuel feed aperture, and therefore the air/fuel mix ture. It is the pri mary method to shut the en gine down. CHT Gauge Cylinder head temperature indicator used to determine that engine op er at ing tem pera ture is within manu fac tur ers speci fi ca tions. Tachometer An instrument that indicates rotational speed of the engine. The speed is shown as pro pel ler revo lu tions per minute (RPM). Pro pel ler Gov er nor The de vice that regu lates RPM of the en gine/pro pel ler by in creas ing or de creas ing the pro pel ler pitch, through a pitch change mecha nism in the pro pel ler hub. ME TE ORO LOGI CAL TER MI NOL OGY AGL Above ground level. Density Altitude as determined by pressure altitude and existing ambient Altitude temperature. In standard atmosphere (ISA) density and pressure al ti tude are equal. For a given pres sure al ti tude, the higher the the tem pera ture, the higher the den sity al ti tude. Indicated The altitude actually read from an altimeter when, and only when Al ti tude baro met ric subscale ( Kolls man win dow) has been set to Sta tion Pres sure. ISA OAT IN TER NA TIONAL STAN DARD AT MOS PHERE as sumes that (1) The air is a dry per fect gas; (2) The tem pera ture at sea level is 15 de grees Cel sius (59 o F); (3) The pres sure at sea level is 29.92 inches Hg (1013.2 mb ); (4) The tem pera ture gra di ent from sea level to the al ti tude at which the tem pera ture is -56.5 o C (-69.7 o F) is -0.00198 o C (-0.003564 o F) per foot. OUT SIDE AIR TEM PERA TURE - The free air static tem pera ture, ob tained ei ther from in flight tem pera ture in di ca tions or ground me te oro logi cal sources. It is ex pressed in o C. Pressure The indicated altitude when Kollsman window is set to 29.92 In. Hg. Altitude or 1013.2 MB. In this handbook, altimeter instrument errors are as sumed to be zero. Sta tion Pres sure Ac tual at mos pheric pres sure at field ele va tion. WEIGHT AND BAL ANCE TER MI NOL OGY Arm Ba sic Empty Weight Cen ter of Grav ity (C.G.) The hori zon tal dis tance from the ref er ence da tum to the cen ter of grav ity (C.G.) of an item. The ac tual weight of the air plane and in cludes all op er at ing equip ment (in clud ing op tional equip ment) that has a fixed lo ca tion and is ac tu ally in stalled in the air craft. It in cludes the weight of un us able fuel and full oil. The point at which an air plane would bal ance if sus pended. Its dis tance from the ref er ence datum is found by di vid ing the to tal mo ment by the to tal weight of the air plane. ISSUED 2-99 1-7

SECTION I GENERAL MOONEY WEIGHT AND BAL ANCE TER MI NOL OGY (con t.) C.G. Arm The arm ob tained by add ing the air plane s in di vid ual mo ments and di vid ing the sum by the to tal weight. C.G. in Cen ter of Gravity ex pressed in per cent of mean aero dy namic % MAC chord (MAC). C.G. Lim its MAC Maxi mum Weight Maxi mum Land ing Weight Mo ment Ref er ence Da tum Sta tion Tare Un us able Fuel Us able Fuel Use ful Load LENGTH The ex treme cen ter of gravity lo ca tions within which the air plane must be op er ated at a given weight. Mean Aero dy namic Chord. The maxi mum authorized weight of the air craft and its con tents as listed in the air craft speci fi ca tions. The maxi mum authorized weight of the air craft and its con tents when a nor mal land ing is to be made. The prod uct of the weight of an item mul ti plied by its arm. (Mo ment di vided by a con stant is used to sim plify bal ance cal culations by re duc ing the number of dig its.) An imagi nary ver ti cal plane from which all hori zon tal dis tances are are meas ured for bal ance pur poses. A lo ca tion along the air plane fu se lage usu ally given in terms of dis tance from the ref er ence da tum. The weight of chocks, blocks, stands, etc. used when weigh ing an air plane, and is in cluded in the scale read ings. Tare is de ducted from the scale read ing to ob tain the ac tual (net) air plane weight. Fuel re main ing af ter a ru nout test has been com pleted in ac cor dance with gov ern men tal regu la tions. Fuel avail able for air craft en gine com bus tion. The ba sic empty weight sub tracted from the maxi mum weight of the air craft. This load con sists of the pi lot, crew (if ap pli ca ble), us able fuel, pas sen gers, and bag gage. MEAS URE MENT CON VER SION TA BLES U. S. Cus tom ary Unit....... Met ric Equiva lents 1 inch.......... 2.54 cen ti me ters 1 foot........... 0.3048 meter 1 yard........... 0.9144 meter 1 mile (stat ute, land)........ 1, 609 me ters 1 mile (nau ti cal,......... 1, 852 me ters in ter na tional) AREA U. S. Cus tom ary Unit....... Met ric Equiva lents 1 square inch........ 6.4516 sq. cen ti me ters 1 square foot......... 929 sq. cen ti me ters 1 square yard......... 0.836 sq. Meter 1-8 ISSUED 2-99

MOONEY SECTION I GENERAL VOL UME OR CA PAC ITY U. S. Cus tom ary Unit....... Met ric Equiva lents 1 cu bic inch........ 16.39 cu bic cen ti me ters 1 cu bic foot......... 0.028 cubic meter 1 cu bic yard......... 0.765 cubic meter U.S. Cus tom ary........ Met ric Equiva lents Liq uid Meas ure 1 fluid ounce......... 29.573 mil li li ters 1 pint........... 0.473 liter 1 quart........... 0.946 liter 1 gal lon........... 3.785 li ters U.S. Cus tom ary........ Met ric Equiva lents Dry Measure 1 pint........... 0.551 liter 1 quart........... 1.101 li ters Brit ish Im pe rial.... U. S........ Met ric Liq uid and Dry Measure.. Equiva lents.... Equiva lents 1 fluid ounce..... 0.961 U.S..... 28.412 mil li li ters fluid ounce, 1.734 cu bic inches 1 pint...... 1.032 U.S..... 568.26 mil li li ters dry pints, 1.201 U.S. liq uid pts., 34.678 cubic inches 1 quart...... 1.032 U.S...... 1.136 li ters dry quarts 1.201 U.S. liq uid qts., 69.354 cubic inches 1 gal lon...... 1.201 U.S...... 4.546 li ters 277.420 cu bic inches WEIGHT U. S. Cus tom ary Unit....... Met ric Equiva lents (Avoir du pois) 1 grain......... 64.79891 mil li grams 1 dram........... 1.772 grams 1 ounce.......... 28.350 grams 1 pound.......... 453.6 grams PRES SURE U.S. Cus tom ary Unit....... Met ric Equiva lents 1 PSIG........... 6.895 KPA 1 Inch Hg.......... 3.388 KPA 1 Inch Hg.......... 25.40 mm Hg ISSUED 2-99 1-9

SECTION I GENERAL MOONEY COM MON CON VER SIONS 1 pound/square foot....... 0.488 kg/ me ter square 1 pound /sq. inch......... 2.036 inch Hg. 1 Pound/HP.......... 0.4538 kg/hp 1-10 ISSUED 2-99

MOONEY SECTION II LIMITATIONS TA BLE OF CON TENTS TITLE................... PAGE INTRODUCTION................. 2-2 NOISE LIMITS................. 2-2 AIRSPEED LIMITATIONS.............. 2-3 AIRSPEED INDICATOR MARKINGS........... 2-4 POWER PLANT LIMITATIONS............. 2-5 POWER PLANT INSTRUMENT MARKINGS......... 2-6 FUEL LIMITATIONS................ 2-7 WEIGHT LIMITS................. 2-7 CENTER OF GRAVITY (GEAR DOWN)........... 2-7 MANEUVER LIMITS................ 2-8 FLIGHT LOAD FACTOR LIMITS............. 2-8 FLIGHT CREW................. 2-8 OPERATING LIMITATIONS.............. 2-8 OXYGEN SYSTEM LIMITATIONS............ 2-8 KINDS OF OPERATION LIMITS............. 2-8 KINDS OF OPERATION EQUIPMENT LIST......... 2-8 DECALS & PLACARDS............... 2-11 CABIN INTERIOR............... 2-11 FUSELAGE INTERIOR............. 2-15 EXTERIOR................. 2-16 FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-1

SECTION II LIMITATIONS MOONEY IN TRO DUC TION SEC TION II in cludes the man da tory op er at ing limi ta tions, in stru ment mark ings, and ba sic plac ards nec es sary for the safe op era tion of the air plane, its en gine, stan dard sys tems and stan dar d equip - ment. The limi ta tions in cluded in this section have been ap proved by the Fed eral Aviation Ad min - istra tion. When ap pli ca ble, limi ta tions as so ci ated with op tional sys tems or equip ment such as autop i lots are in cluded in SEC TION IX. NOTE The airspeeds listed in the Airspeed Limitations chart (Figure 2-1) and the Airspeed Indicator Markings chart Figure 2-2) are based on Airspeed Calibration data shown in SECTION V with the normal static source. If the alternate static source is being used, ample margins should be observed to allow for the airspeed calibration variations between the normal and alternate static sources as shown in SECTION V. Your Moo ney is cer tifi cated un der FAA Type Cer tifi cate No. 2A3 as a Moo ney. NOISE LIM ITS The cer tifi cated noise level for the Moo ney at 3200 lbs. (1452 Kg.) maxi mum weight is 75.8 db(a) in ac cor dance with FAR 36, Ap pen dix G. No de ter mi na tion has been made by the Fed eral Avia tion Ad min istra tion that the noise levels of this air plane are or should be ac cept able or un ac cept - able for op era tion at, into, or out of, any air port. AIRPLANE FLIGHT MANUAL FAA APPROVED 2-2 ISSUED 2-99

MOONEY SECTION II LIMITATIONS AIR SPEED LIMI TA TIONS Air speed limi ta tions and their op era tional sig nifi cance are shown in Fig ure 2-1. This cali bra tion as - sumes zero in stru ment er ror. V / SPEED KCAS/KIAS RE MARKS V NE V NO Never Exceed Speed Maxi mum Struc tural Cruis ing Speed 195/195 Do not ex ceed this speed in any op era tion. 175/174 Do not ex ceed this speed ex cept in smooth air, and then only with cau tion. V A Ma neu ver ing Speed at: lbs. /Kg. 2232/1012 2430/1102 2900/1315 3200/1452 104/103 109/108 118/117 124/123 Do not make full or abrupt con trol move ment above this speed. V FE V LE V LO (EXT) V LO (RET) Maxi mum Flap Ex tended Speed Maxi mum Land ing Gear Ex tended Speed Max. Speed for Gear Ex ten sion Max. Speed for Gear Re trac tion Maxi mum Pi lot Win dow Open Speed 111/110 Do not ex ceed this speed with flaps in full down po - si tion. 166/165 Maxi mum speed at which the air craft can be safely flown with the land ing gear ex tended. 141/140 Max. speed at which the land ing gear can be safely ex tended. 107/106 Maxi mum speed at which the landing gear can be safely re tracted. 133/132 Do not ex ceed this speed with pi lot win dow open. ================================================= FIGURE 2-1 AIRSPEED LIMITATIONS FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-3

SECTION II LIMITATIONS MOONEY AIR SPEED IN DI CA TOR MARK INGS Air speed in di ca tor mark ings, their color code and op era tional sig nifi cance are shown in Fig ure 2-2. MARK ING IAS VALUE or RANGE (KIAS) SIG NIFI CANCE ================================================= White Arc (Flap Op er at ing Range) 58-110 KIAS Lower limit is maxi mum weight V so in landing con figu ra tion. Up - per limit is maxi mum speed per - missable with flaps ex tended. Green Arc (Nor mal Op er at ing Range) 65-174 KIAS Lower limit is maxi mum weight V s with flaps re tracted. Up per limit is maxi mum struc - tural cruis ing speed. Yel low Arc (Cau tion Range) 174-195 KIAS Op era tions must be con ducted with cau tion and only in smooth air. Ra dial Red Line 195 KIAS Maxi mum speed for all op era - tions. ================================================ FIGURE 2-2 AIRSPEED INDICATOR MARKINGS AIRPLANE FLIGHT MANUAL FAA APPROVED 2-4 ISSUED 2-99

MOONEY SECTION II LIMITATIONS POWER PLANT LIMI TA TIONS Num ber of En gines........... 1 En gine Manu fac turer..... Tele dyne Con ti nen tal Motors (TCM) En gine Model Num ber........ IO- 550-G (6) * En gine Op er at ing Limits for Take off and Con tinu ous Op era tions: Maxi mum Con tinu ous Power...... 244 BHP Maxi mum Con tinu ous RPM...... 2400 RPM Tran sient RPM Limit....... 2600 RPM Maxi mum Cyl in der Head Tem pera ture... 460 o F (237.7 o C) Maxi mum Oil Tem pera ture..... 240 o F (115 o C) Mini mum Oil Temperature- Takeoff..... 75 o F (24 o C) Recm ded Cruis ing Tem pera ture... 170 o F- 220 o F (76 o C-104 o C) Oil Pres sure Normal Op er at ing....... 30-100 PSI Mini mum ( IDLE ONLY )....... 10 PSI Oil Speci fi ca tion...... MHS- 24 ( ) and TCM Ap proved oils Fuel Grade (Color)..... 100LL (Blue) ** or 100 oc tane (Green) ** Num ber of Pro pel lers.......... 1 Pro pel ler Manu fac turer......... McCauley Pro pel ler/blade Model Num ber..... 2A34C239/90DMC- 15 * Num ber of Blades........... 2 Pro pel ler Di ame ter: McCauley Min......... 74.5 In. (189.2 cm) Max......... 75 In. (190.5 cm) McCauley - Pro pel ler Blade An gles @ 30.0 In. sta.: Low....... 19.0 De grees +/- 0.2 De grees High...... 37.5 De grees +/- 0.5 De grees Pro pel ler Op er at ing Lim its ( McCauley )...... 2400 RPM * Re fer to TCDS for en gine and pro pel ler con figu ra tion re quired. ** 100LL fuel is cali brated at 5.82 lb/gal(.69 Kg/li ter) 100 oc tane fuel is cali brated at 6.0 lb.gal. (.72 Kg/liter) FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-5

SECTION II LIMITATIONS MOONEY POWER PLANT IN STRU MENT MARK INGS IN STRU MENT RED LINE * MINI MUM LIMIT GREEN ARC * NOR MAL OP ER AT ING YEL LOW ARC * RED LINE * MAXI MUM LIMIT ================================================= Tachometer 600 RPM No Red line 2200-2400 RPM 2400 RPM Cyl in der Head Tem pera ture 250-460 o F (121-215.5 o C) --------- 460 o F (237.7 o C) Oil Tem pera ture No Red line 170-240 o F (76.6-104 o C) 100-170 o F (37.7-76.6 o C) 240 o F (115.5 o C) Oil Pressure 10.0 PSI (IDLE ONLY) 30-100 PSI 10-30 PSI 100 PSI Ex haust Gas Tem pera ture 1400-1450 o F (760-788 o C) (BLUE ARC= --------- rec om mended climb) 1650 o F (899 o C) * SEE SECTION VII, INSTRUMENT PANEL, FLIGHT PANEL & INSTRUMENTS, and ENGINE, ENGINE INSTRUMENTS, FOR DESCRIPTION OF OPERATIONAL PARAMETERS WITHIN COLORED ARCS or LINES. ================================================= -------- NOTE -------- Refer to TCM Engine Maintenance and Operators Manual Section on Engine Specifications and Operating Limits for recommended cruise power and temperature limitations. FIGURE 2-3 POWER PLANT INSTRUMENT MARKINGS AIRPLANE FLIGHT MANUAL FAA APPROVED 2-6 ISSUED 2-99

MOONEY SECTION II LIMITATIONS FUEL LIMI TA TIONS ////////////// // WARNING // ////////////// Turning takeoffs with less than 12 gallons useable fuel in the selected tank are prohibited. NOTE Each fuel quantity gauge is calibrated to read zero (RED LINE) only in coordinated level flight when remaining quantity of fuel can no longer be safely used. NOTE An optional visual fuel quantity gauge is installed on top of each tank and is to be used as a reference for refueling tanks only. Stan dard Tanks (2)...... 40.5 U.S. Gal. (153 li ters) each To tal Fuel......... 81 U.S. Gal. (307 li ters) Us able Fuel:........ 75 U.S. Gal. (284 li ters) Un us able Fuel:........ 6 U.S. Gal. (22.7 li ters) Fuel Grade (and color): 100LL (low lead) (blue) or 100 oc tane (green) is ap proved. ~~~~~~~ ~ CAUTION ~ ~~~~~~~ To reduce possibility of ice formation within the aircraft or engine fuel system it is permissible to add ISO-PROPYL alcohol to the fuel supply in quantities NOT TO EXCEED 3% of total fuel volume per tank. DO NOT add other additives to fuel system due to potential deteriorating effects within the fuel system. WEIGHT LIM ITS Maxi mum Weight - Takeoff....... 3200 lb. (1452 Kg) Maxi mum Weight - Land ing....... 3200 lb. (1452 Kg) Maxi mum Weight in Bag gage Com part ment.... 120 lb. (54.4 Kg) @ Fus. Sta. 101.5 (253.7 cm) Maxi mum Weight in Rear Stor age Area..... 10 lb. (4.54 Kg) @ Fus. Sta. 131.0 (297.5 cm) Maxi mum Weight in Cargo Area (Rear seats folded down)... 340 lbs. (154.2 Kg) @ Fus. Sta. 70.7 (176.8 cm) CEN TER OF GRAV ITY LIM ITS (GEAR DOWN) Most For ward.... Fus. Sta. 41.0 IN. (104.1 cm) @ 2430 lb. (1102 Kg)............ 16.79% MAC In ter me di ate Forward... Fus. Sta. 43.0 IN. (109.2 cm) @ 3000 lb. (1361 Kg)............ 20.07% MAC For ward Gross.... Fus. Sta. 45.0 IN. (114.3 cm) @ 3200 lb. (1452 Kg)............ 20.89% MAC Aft Gross.... Fus. Sta. 51.0 IN. (129.5 cm) @ 3200 lb. (1452 Kg)............ 33.18% MAC MAC (at Wing Sta. 94.85) (241 cm)....... 61.00 In. Da tum (sta tion zero) is 13 inches (32.5 cm) aft of the cen ter line of the nose gear trun ion at tach/pivot bolts. MA NEU VER LIM ITS This air plane must be op er ated as a Nor mal Cate gory air plane. Aero batic ma neu vers, includ ing spins, are pro hib ited. FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-7

SECTION II LIMITATIONS MOONEY NOTE Up to 500 foot altitude loss may occur during stalls at maximum weight. FLIGHT LOAD FAC TOR LIM ITS Maxi mum Posi tive Load Fac tor Flaps Up.......... +3.8 g. Flaps Down (33 De grees)........ +2.0 g. Maxi mum Nega tive Load Fac tor Flaps Up........... -1.5 g. Flaps Down...........0.0 g. FLIGHT CREW Pi lot............ One Maxi mum pas sen ger seating con figu ra tion...... Three OP ER AT ING LIMI TA TIONS For flight op era tion above 12,000 f t., a sup ple men tal oxy gen sys tem is re quired. Dual Bat ter ies weigh ing 29.5 lbs. each, at fu se lage sta tion 146.0, must be in stalled for all op era tions. AL TER NA TOR OP ER AT ING LIMI TA TIONS IS 99 AMPS. PRO PEL LER LIMI TA TIONS - Pro pel ler is re stricted from static ground op era tion in rear quar ter ing winds of 15 knots or higher at RPM set tings above 1350 RPM. KINDS OF OP ERA TION LIM ITS This is a Nor mal Cate gory air plane cer ti fied for VFR/ IFR day or night op era tions when the re quired equip ment is in stalled and op era tional as speci fied in the KINDS OF OP ERA TION EQUIP MENT LIS T and the ap pli ca ble op er at ing rules. Op tional equip ment in stal la tions may not be re quired to be op era tional. The pi lot must de ter mine that the ap pli ca ble op er at ing rules re quire ments for each kind of op era tion are met. OPERATIONS IN KNOWN ICING CONDITIONS ARE PROHIBITED. KINDS OF OP ERA TION EQUIP MENT LIST The fol low ing equip ment was ap proved dur ing Type Cer ti fi ca tion and must be in stalled and op er able for each kind of op era tion as speci fied. NOTE The KINDS OF OPERATION EQUIPMENT list may not include all the equipment as required by applicable operating rules. SEE NEXT PAGE FOR LISTINGS. AIRPLANE FLIGHT MANUAL FAA APPROVED 2-8 ISSUED 2-99

MOONEY SECTION II LIMITATIONS KINDS OF OPERATION EQUIPMENT LIST......... VFR DAY *......... VFR NIGHT......... IFR DAY......... IFR NIGHT SYS TEM or COM PO NENT AIR SPEED IN DI CA TOR...... 1 1 1 1 AL TIME TER, SEN SI TIVE...... 1 1 1 1 MAG NETIC DI REC TION IN DI CA TOR.... 1 1 1 1 MANI FOLD PRES SURE GAUGE.... -- -- -- -- TA CHOME TER....... 1 1 1 1 FUEL QUANTITY IN DI CA TOR..... 2 2 2 2 FUEL PRES SURE IN DI CA TOR..... -- -- -- -- OIL PRES SURE IN DI CA TOR..... 1 1 1 1 OIL TEM PERA TURE IN DI CA TOR.... 1 1 1 1 CYL IN DER HEAD TEM PERA TURE IN DI CA TOR.. 1 1 1 1 EX HAUST GAS TEM PERA TURE IN DI CA TOR.. 1 1 1 1 AM ME TER/ LOADMETER..... 1 1 1 1 AL TER NA TOR....... 1 1 1 1 LAND ING GEAR PO SI TION IN DI CA TOR... 2 2 2 2 SEAT BELT & SHOUL DER HAR NESS FOR EACH OC CU PANT **..... 1 1 1 1 OXY GEN MASK FOR EACH OC CU PANT ***.. 1 1 1 1 PO SI TION LIGHTS...... -- 3 -- 3 STROBE LIGHTS (ANTI- COLLISION).... -- 3 -- 3 * Equip ment must be in stalled and op er able for all op era tions. ** If in op era tive for un oc cu pied seat(s), seat(s) must be plac arded: DO NOT OC CUPY *** Only re quired when the op er at ing rules re quire use of oxy gen. FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-9

SECTION II LIMITATIONS MOONEY KINDS OF OPERATION EQUIPMENT LIST......... VFR DAY *......... VFR NIGHT......... IFR DAY......... IFR NIGHT SYS TEM or COM PO NENT (con t.) GYRO HORIZON....... -- -- 1 1 DI REC TIONAL GYRO...... -- -- 1 1 TURN CO OR DI NA TOR or TURN & BANK IN DI CA TOR. -- -- 1 1 LAND ING LIGHT ****...... -- 1 -- 1 IN STRU MENT LIGHTS (IN TER NAL or GLARE SHIELD). -- 1 -- 1 CLOCK (WITH SWEEP SECOND HAND or DIGI TAL). -- -- 1 1 COM MU NI CA TION SYS TEM..... -- -- 1 1 NAVI GA TION SYS TEM...... -- -- 1 1 (AP PRO PRI ATE TO FA CILI TIES BE ING USED) BAT TERIES........ 2 2 2 2 VAC UUM SYS TEM/IN DI CA TOR.... -- -- 1 1 FUEL BOOST PUMP...... 1 1 1 1 PI TOT, HEATED ****...... -- -- 1 1 OAT GAUGE ****....... -- -- 1 1 VSI ****........ -- -- 1 1 AL TER NATE STATIC SOURCE ****.... -- -- 1 1 STAND- BY VAC UUM SYS TEM ****.... -- -- 1 1 PI LOT S OP ER AT ING HAND BOOK & AIR PLANE FLIGHT MAN UAL..... 1 1 1 1 * Equip ment must be in stalled and op er able for all op era tions. **** When re quired by the ap pro pri ate regu la tions. AIRPLANE FLIGHT MANUAL FAA APPROVED 2-10 ISSUED 2-99

MOONEY SECTION II LIMITATIONS CABIN IN TE RIOR DE CALS AND PLAC ARDS The fol low ing plac ards are relev ent to proper op era tion of the air plane and must be in stalled in side the cabin at the lo ca tions speci fied. OPERATING LIMITATIONS THE MARKINGS AND PLACARDS INSTALLED IN THIS AIRPLANE CONTAIN OP - ERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE IN THE NORMAL CATEGORY. THIS AIRPLANE IS CERTIFIED FOR DAY AND NIGHT VFR/IFR OPERATION WHEN THE REQUIRED EQUIPMENT IS INSTALLED AND OPERATIONAL. FLIGHT INTO KNOWN ICING CONDITIONS IS PROHIBITED. NO AEROBATIC MANEUVERS, IN- CLUDING SPINS ARE APPROVED. OTHER OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE IN THIS CATE - GORY ARE CONTAINED IN THE AIRPLANE FLIGHT MANUAL. MANEUVERING SPEED (3200 LBS) 124 KIAS; (2600 LBS.) 111KIAS. EMERGENCY MANUAL GEAR EXTENSION 1. PULL LANDING GEAR ACTUATOR CIRCUIT BREAKER. 2. PUT GEAR SWITCH IN GEAR DOWN POSITION. 3. PUSH RELEASE TAB FORWARD AND LIFT UP RED HANDLE. 4. PULL T-HANDLE STRAIGHT UP (12 TO 20 INCHES). 5. ALLOW T-HANDLE TO RETURN TO ORIGI NAL POSITION. 6. REPEAT UNTIL GEAR DOWN LIGHT COMES ON (12 TO 20 PULLS). IF TOTAL ELECTRICAL FAIL URE -- SEE MECHANICAL INDICATOR. ON LEFT SIDE PANEL IN PI LOT S VI SION 150056-1033 ON LEFT LOWER SIDE PANEL CAUTION 1. TURN OFF STROBE LIGHTS WHEN TAXIING NEAR OTHER ACFT OR WHEN FLYING IN FOG OR IN CLOUDS. STD POSITION LIGHTS MUST BE USED FOR ALL NIGHT OPERATIONS. 2. IN CASE OF FIRE, TURN OFF CABIN HEAT. 3. DO NOT SCREW VERNIER CONTROLS CLOSER THAN 1/8 FROM NUT FACE. ON CON SOLE (OP TIONAL) GREEN ARC TAILWIND GROUND OPERATION GREEN ARC BLUE ARC 2200-2400 RPM ABOVE 1350RPM PROHIBITED 250 o -460 o 1400 o -1450 o ABOVE EN GINE IN STRU MENT CLUS TER ON BEZEL GREEN ARC YELLOW ARC GREEN ARC YELLOW ARC 30-100 PSI 10-30 PSI 170 o -240 o 100 o -170 o FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-11

SECTION II LIMITATIONS MOONEY CON SOLE ABOVE & BE LOW SWITCH (OP TIONAL- IF IN STALLED ON) PI LOT S L/H PANEL, FWD OF ARM REST FWD END OF REAR SEAT BOT TOM STRUCTURE FLOOR BOARD BE TWEEN SEATS ON RA DIO PANEL, AD JA CENT TO ELT SWITCH.(OP TIONAL) BE LOW INSTR. PANEL MIC PHONE AD JA CENT TO DIGI TAL AMMETER ALTERNATOR + LOAD E-W CCW CW N S FREE SLAVE (TYPI CAL - PLACARDS WILL VARY WITH AIR CRAFT CON FIGU RA TION) ON RA DIO PANEL BATTERY + AMPS AIRPLANE FLIGHT MANUAL FAA APPROVED 2-12 ISSUED 2-99

MOONEY SECTION II LIMITATIONS UP PER CTR INSTR. PANEL ABOVE IN SIDE BAG GAGE DOOR HAN DLE LWR INSTR PNL, BE LOW CON TROL WHEEL SHAFT DO NOT OPEN ABOVE 132 KIAS BE LOW PILOT S STORM WINDOW ON MAG NETIC COM PASS (OP TIONAL- IF OXY GEN IN STALLED) AROUND EACH OXY GEN OUTLET-O/H PANEL ABOVE EACH 14 VOLTS 3 AMPS MAX. 5 A IN TER MIT TENT AD JA CENT TO AUX. PWR. SUP PLY PLUG (OP TIONAL) CONTROL ON LWR INSTR. PANEL CON SOLE ON CON TROL KNOB FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-13

SECTION II LIMITATIONS MOONEY BAG GAGE COM PART MENT ON HAT RACK SHELF TOP OF BAG GAGE DOOR JAMB IN STRU MENT PANEL VACUUM 37.5 GAL 37.5 GAL OPERATING RANGE USE ABLE USE ABLE 4.2-5.2 IN. HG ABOVE FUEL QTY. GAUGE ON BEZEL NXXXXX UP PER IN STRU MENT PANEL FLOOR BOARD BE TWEEN SEATS BE TWEEN SEATS - ON EMER GENCY GEAR RE LEASE EX TEN SION HANDLE BAG GAGE DOOR FRAME FLOOR BOARD - FWD OF CO- PILOT SEAT AIRPLANE FLIGHT MANUAL FAA APPROVED 2-14 ISSUED 2-99

MOONEY SECTION II LIMITATIONS FU SE LAGE IN TE RIOR The fol low ing plac ards must be in stalled in side the fu se lage at the lo ca tions speci fied. HY DRAU LIC OIL RESERVOIR (AUX. PWR. SYS TEM IS OP TIONAL; IF IN STALLED ON) BACK SIDE OF AUX. PWR. RE CEP TA CLE DOOR ON BATTERY ACCESS PANELS L/H & R/H (OXY GEN SYS TEM IS OP TIONAL; IF IN STALLED ON) IN SIDE OXY GEN FILLER DOOR IN SIDE EN GINE OIL FILLER DOOR FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-15

SECTION II LIMITATIONS MOONEY EX TE RIOR The fol low ing plac ards must be in stalled on the ex te rior of the air craft at the lo ca tions speci fied. ON IN BOARD END OF FLAP, WING LEAD ING EDGES & WING, AHEAD OF FLAPS UN DER SIDE OF WING (2 PLCS ) & AFT OF L/H COWL FLAP (1 PLC) HO RIZ. STAB. L/E; RUD DER T/E (BOTH SIDES) UN DER TAILCONE AFT OF WING T/E UN DER LEFT WING L/E NEAR FUSELAGE UN DER WING NEAR SUMP DRAINS UN DER FU SE LAGE RT. SIDE AFT OF NOSE WHEEL WELL AIRPLANE FLIGHT MANUAL FAA APPROVED 2-16 ISSUED 2-99

MOONEY SECTION II LIMITATIONS MAIN LAND ING GEAR DOOR NOSE LANDING GEAR DOOR NOSE LANDING GEAR LEG ASSY NOSE LAND ING GEAR SPIN DLE ASSY. LWR L/H WING PANEL O/B OF HOIST POINT BOTH FUEL FILLER CAPS FUEL -- 100 (GREEN) OR 100LL (BLUE) MIN OCT 37.5 U.S. GAL USABLE 142.0 LI TERS USABLE OIL FILLER DOOR WIN TERI ZA TION KIT FILLER DOOR FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 2-17

SECTION II LIMITATIONS MOONEY BLANK AIRPLANE FLIGHT MANUAL FAA APPROVED 2-18 ISSUED 2-99

MOONEY SECTION III EMERGENCY PROCEDURES TA BLE OF CON TENTS TITLE................... PAGE INTRODUCTION................. 3-3 AIRSPEEDS FOR EMERGENCY OPERATIONS......... 3-4 ANNUNCIATOR PANEL WARNING LIGHTS.......... 3-5 ENGINE................... 3-6 POWER LOSS - DURING TAKEOFF ROLL......... 3-6 POWER LOSS - AFTER LIFTOFF........... 3-6 POWER LOSS - IN FLIGHT (RE-START PROCEDURES)..... 3-6 POWER LOSS - PRIMARY ENGINE INDUCTION AIR SYSTEM BLOCKAGE............ 3-7 ENGINE ROUGHNESS.............. 3-8 HIGH CYLINDER HEAD TEMPERATURE......... 3-8 HIGH OIL TEMPERATURE............. 3-8 LOW OIL PRESSURE.............. 3-8 LOW FUEL PRESSURE.............. 3-8 ENGINE DRIVEN FUEL PUMP FAILURE......... 3-8 FUEL VAPOR SUPPRESSION (FLUCTUATING FUEL PRESSURE)... 3-9 FIRES................... 3-9 ENGINE FIRE - DURING START ON GROUND........ 3-9 ENGINE FIRE - IN FLIGHT............. 3-9 ELECTRICAL FIRE - IN FLIGHT (SMOKE IN CABIN)...... 3-9 EMERGENCY DESCENT PROCEDURE........... 3-10 GLIDE................. 3-10 FORCED LANDING EMERGENCY............ 3-11 GEAR RETRACTED OR EXTENDED.......... 3-11 OVERWEIGHT LANDING PROCEDURES.......... 3-11 SYSTEMS EMERGENCIES.............. 3-11 PROPELLER................ 3-11 FUEL.................. 3-11 ELECTRICAL................ 3-11 LANDING GEAR............... 3-12 VACUUM................. 3-13 OXYGEN................. 3-13 ALTERNATE STATIC SOURCE........... 3-13 FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 3-1

SECTION III EMERGENCY PROCEDURES MOONEY TA BLE OF CON TENTS (con t) TITLE................... PAGE UNLATCHED DOORS IN FLIGHT............ 3-14 ICING................... 3-14 EMERGENCY EXIT OF AIRCRAFT............ 3-15 SPINS................... 3-16 OTHER EMERGENCIES............... 3-16 AIRPLANE FLIGHT MANUAL FAA APPROVED 3-2 ISSUED 2-99

MOONEY SECTION III EMERGENCY PROCEDURES IN TRO DUC TION This sec tion pro vides the rec om mended pro ce dures to fol low dur ing ad verse flight con di tions. The in for ma tion is pre sented to enable you to form, in ad vance, a defi nite plan of ac tion f or cop ing with the most probable emer gency situa tions which could oc cur in the op era tion of your air plane. As it is not pos si ble to have a pro ce dure for all types of emer gen cies that may oc cur, it is the pi - lot s re spon si bil ity to use sound judge ment based on ex pe ri ence and knowl edge of the airc raft to de ter mine the best course of ac tion. There fore, it is con sid ered man da tory that the pi lot read the en tire man ual, es pe cially this sec tion be fore flight. When ap pli ca ble, emer gency pro ce dures as so ci ated with op tional equip ment such as Autopi - lots are in cluded in SEC TION IX. NOTE All airspeeds in this section are indicated (IAS) and assume zero instrument error unless stated otherwise. FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 3-3

SECTION III EMERGENCY PROCEDURES MOONEY AIR SPEEDS FOR EMER GENCY OP ERA TIONS CON DI TION....... REC OM MENDED SPEED ================================================= EN GINE FAIL URE AF TER TAKEOFF Wing Flaps UP........... 85 KIAS Wing Flaps DOWN.......... 80 KIAS BEST GLIDE SPEED 3200 lb/1452 kg.......... 89.0 KIAS 2900 lb/1315 kg.......... 84.5 KIAS 2600 lb/1179 kg.......... 80.0 KIAS MA NEU VER ING SPEED 3200 lb/1452 kg.......... 123 KIAS 2900 lb/1315 kg.......... 117 KIAS 2430 lb/1102 kg.......... 108 KIAS 2232 lb/1012 kg.......... 103 KIAS PRE CAU TION ARY LAND ING WITH EN GINE POWER Flaps DOWN........... 75 KIAS EMER GENCY DE SCENT (GEAR UP) Smooth Air............ 195 KIAS Tur bu lent Air 3200 lb/1452 kg.......... 123 KIAS 2430 lb/1102 kg.......... 108 KIAS 2232 lb/1012 kg.......... 103 KIAS EMER GENCY DE SCENT (GEAR DOWN) Smooth Air............ 165 KIAS Tur bu lent Air 3200 lb/1452 kg.......... 123 KIAS 2430 lb/1102 kg.......... 108 KIAS 2232 lb/1012 kg.......... 103 KIAS ================================================= AIRPLANE FLIGHT MANUAL FAA APPROVED 3-4 ISSUED 2-99

MOONEY SECTION III EMERGENCY PROCEDURES ANNUNCIATOR PANEL WARN ING LIGHTS WARN ING LIGHT FAULT & REM EDY GEAR UN SAFE RED light in di cates landing gear is not in fully ex - tended/or re tracted po si tion. Re fer to FAIL URE OF LAND ING GEAR TO EX TEND ELEC TRI CALLY pro - ce dure or FAIL URE OF LAND ING GEAR TO RE - TRACT pro ce dure. LEFT or RIGHT FUEL SPEED BRAKE ALT AIR PROP DE- ICE PI TOT HEAT HI/LO VAC (Flash ing) RED light indicates 6 to 8 gallons (23 to 30.3 liters) of usable fuel remain in the respective tanks. Switch to fuller tank. AM BER light in di cates Speed Brakes are ac ti vated. AM BER light in di cates al ter nate in duc tion air door is open. BLUE light in di cates power ap plied to De- Ice boots BLUE light indicates power is applied to heater. (Some Foreign A/C - AMBER light indicates power is NOT ap - plied to heater.) Suc tion is be low 4.25 in. Hg. (RED) Turn Stand- by Vac uum pump - ON HI/LO VAC (Steady) Suc tion is above 5.5 in. Hg. (RED) Turn Stand- by Vac uum pump - ON NOTE Attitude and Directional Gyros are unreliable when VAC light is illuminated (steady or flashing). Vacuum system should be checked and/or adjusted as soon as practicable. ALT VOLTS (Flash ing) ALT VOLTS (Steady) START POWER STBY VAC RE MOTE RNAV BOOST PUMP RED light indicates alternator output low. Refer to AL - TERNATOR OUTPUT LOW. RED light in di cates over volt age and Alt. field. C/B tripped. Re fer to AL TER NA TOR OVER VOLT AGE. RED light in di cates switch or re lay is en gaged and starter is en er gized. Flight should be ter mi nated as soon as prac ti ca ble. En gine dam age may re sult. This is nor mal in di ca tion during en gine start. AM BER light in di cates stand- by vac uum pump is ON. NOT USED AT THIS TIME BLUE light in di cates power is being supplied to the aux il iary fuel boost pump. FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 3-5

SECTION III EMERGENCY PROCEDURES MOONEY POWER LOSS - DUR ING TAKE OFF ROLL EN GINE Throt tle........... CLOSED Brakes....... AS RE QUIRED TO STOP AIR CRAFT Fuel Se lec tor........... OFF Mag neto/starter Switch......... OFF Mas ter Switch........... OFF POWER LOSS - AF TER LIFT OFF Air speed......... 90 KIAS (Flaps UP)......... 83 KIAS (Flaps TAKE OFF/DOWN) KEEP THE AIR CRAFT UN DER CON TROL - then: Fuel Se lec tor........ SE LECT OTHER TANK Throt tle.......... FULL FOR WARD Mag neto switch......... Ver ify on BOTH Mix ture.......... FULL FOR WARD Pro pel ler.......... FULL FOR WARD LOW Boost Pump Switch...... ON - to at tempt re- start If En gine Quits - then: HIGH BOOST Pump (guarded switch).... ON - to at tempt re- start LAND AS SOON AS PRACTICABLE; CORRECT MALFUNCTION PRIOR TO NEXT FLIGHT. If en gine does not re- start, pro ceed to FORCED LAND ING EMER GENCY. ///////////// // WARNING // ///////////// Engine may run rough due to overrich mixture. Lean mixture until engine operates smoothly. - NOTE If high power is required, mixture may require enrichening. POWER LOSS - IN FLIGHT (RE- START PRO CE DURES) Air speed.......... 85 KIAS minimum Fuel Se lec tor..... SE LECT OTHER TANK (Ver ify full est tank) LOW Boost Pump Switch...... ON - to at tempt re- start Throt tle.......... FULL FOR WARD Pro pel ler.......... FULL FOR WARD Mix ture........ AS RE QUIRED to re store power Mag neto/starter Switch....... VER IFY on BOTH LOW Boost Pump Switch... OFF if en gine does not start im me di ately HIGH BOOST Pump (guarded switch).... ON - to at tempt re- start Al ter nate Air Door......... Manu ally Open If en gine does not start af ter ini tial at tempts: Mix ture......... IDLE CUT- OFF (Ini tially)...... then ad vance slowly to ward RICH un til en gine starts. If en gine does not re- start af ter sev eral at tempts es tab lish best glide speed (Re fer to Max i mum Glide Dis tance Chart) and pro ceed to FORCED LAND ING EMER GENCY. Af ter en gine re- start: Throt tle......... AD JUST as re quired Pro pel ler......... AD JUST as re quired Mix ture....... RE- LEAN as re quired for power set ting HIGH BOOST Pump Switch......... OFF NOTE If engine fails when HIGH BOOST pump is turned OFF, suspect engine driven fuel pump failure. Proceed to ENGINE DRIVEN FUEL PUMP FAILURE. AIRPLANE FLIGHT MANUAL FAA APPROVED 3-6 ISSUED 2-99

MOONEY SECTION III EMERGENCY PROCEDURES LAND AS SOON AS PRACTICABLE; CORRECT MALFUNCTION PRIOR TO NEXT FLIGHT. ~~~~~~ ~ CAUTION ~ ~~~~~~ Should engine excessively cool during engine out, care should be exercised during re-start to avoid excessive oil pressure. Allow engine to warm up. OP ER AT ING THE EN GINE AT TOO HIGH AN RPM BE FORE REACH ING MINI MUM OIL TEM PERA TURES MAY CAUSE LOSS OF OIL PRES SURE. POWER LOSS - PRI MARY EN GINE IN DUC TION AIR SYS TEM BLOCK AGE Block age of the pri mary en gine in duc tion air sys tem may be ex pe ri enced as a re sult of fly ing in cloud or heavy snow with cold out side air tem pera tures (0 o C or below). At these tem pera tures, very small wa ter drop lets or solid ice crys tals in the air may enter the pri mary en gine in duc tion in let in cowl open ing and travel in side in let duct to the in duc tion air fil ter. Ice par ti cles or water d rop lets may col - lect and freeze on the air filter caus ing par tial or to tal block age of the pri mary en gine in duc tion sys - tem. If pri mary in duc tion air sys tem block age oc curs, the al ter nate en gine in duc tion air sys tem will auto - mati cally open, sup ply ing en gine with an al ter nate air source drawn from in side the cowl ing rather than through the air fil ter. The al ter nate air sys tem can also be manu ally opened at any time by pull - ing the con trol la beled AL TER NATE AIR. Auto matic or man ual ac ti va tion of the al ter nate in duc tion sys tem is dis played in the cockpit by the il lu mi na tion of the ALT AIR light in the main ann un cia tor panel. When op er at ing on the al ter nate air sys tem, avail able en gine power will be less for a given pro - pel ler RPM com pared to the pri mary in duc tion air sys tem. This is due to loss of ram ef fecta nd in duc - tion of warmer in let air. The fol low ing check list should be used if a par tial power loss due to pri mary in duc tion air sys tem block age is ex pe ri enced: Al ter nate Air...... Ver ify OPEN (an nun cia tor light ON) Mani fold Pres sure.. 1-2 inches less than nor mal, due to warm in duc tion air NOTE The alternate air door should open automatically when primary induction system is restricted. If alternate air door has not opened (Annunciator light-off) it can be opened manually by pulling alternate air control. Throt tle......... IN CREASE as de sired Pro pel ler......... IN CREASE as re quired..... to main tain de sired cruise power set ting (Ref.SEC TION V) Mix ture......... RE LEAN to de sired EGT Flight..... CON TINUE - re quest al ti tude with warmer air, if able. In the un likely event that a to tal power loss, due to pri mary en gine in duc tion air block age, is ex pe ri - enced, the fol low ing check list should be used: Air speed......... BEST GLIDE SPEED Al ter nate Air......... Manu ally OPEN LOW Boost Pump Switch......... ON Throt tle.......... Full FOR WARD Pro pel ler.......... FULL FOR WARD Mix ture........ AS RE QUIRED to re store power Mag neto/starter Switch........ Ver ify on BOTH Af ter en gine re- start : Throt tle......... AD JUST as re quired Pro pel ler......... AD JUST as re quired Mix ture....... RE LEAN as re quired for power set ting........ (Re fer to power charts - SEC TION V) LOW Boost Pump Switch......... OFF FAA APPROVED AIRPLANE FLIGHT MANUAL ISSUED 2-99 3-7