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ACCU-SIM V35B BONANZA

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A2A

SIMULATIONS

FOR SIMULATION USE ONLY

WEIGHT & BALANCE

Reference

Datum

An imaginary vertical plane from

which all horizontal distances are

measured for balance purposes.

Station

A location along the airplane fuselage usually given

in terms of distance from the reference datum.

Arm

The horizontal distance from the reference

datum to the center of gravity (C.G.) of an item.

Moment

The product of the weight of an item multiplied

by its arm (Moment divided by a constant

is used to simplify balance calculations

by reducing the number of digits.)

Airplane

Center of

Gravity (CG)

The point at which an airplane would balance

if suspended. Its distance from the reference

datum is found by dividing the total moment

by the total weight of the airplane.

CG Arm

The arm obtained by adding the

airplane’s individual moments and

dividing the sum by the total weight.

CG Limits

The extreme center of gravity locations

within which the airplane must be

operated at a given weight.

Usable Fuel

Fuel available for flight planning.

Unusable Fuel

Fuel remaining after a runout test

has been completed in accordance

with governmental regulations.

Standard

Empty Weight

Weight of a standard airplane including

unusable fuel, full operating fluids and full oil.

Basic Empty

Weight

Standard Empty Weight plus optional equipment.

Payload

Weight of occupants, cargo and baggage.

Useful Load

Difference between Take-off Weight (or Ramp

Weight, if applicable) and Basic Empty Weight.

Maximum

Ramp Weight

Maximum weight approved for ground

maneuvering. {It includes weight of

start, taxi, and take-off fuel).

Maximum

Take-off

Weight

Maximum weight approved for liftoff.

Maximum

Landing

Weight

Maximum weight approved for

the landing touchdown.

Maximum

Zero Fuel

Weight

Maximum weight exclusive of usable fuel.

Tare

The weight of chocks, blocks, stands, etc., used

on the scales when weighing an airplane.

Leveling

Points

Those points which are used during the

weighing process to level the airplane.

Jack Points

Points on the airplane identified by the

manufacturer as suitable for supporting the

airplane for weighing or other purposes.

POWER

Take-off and

Maximum

Continuous

Highest power rating not limited by time.

Maximum

Normal

Operating

Power (MNOP)

Highest power rating within the normal operating

range. Noise characteristics requirements of FAR

36 have been demonstrated at this power rating.

Cruise Climb

Power recommended for cruise climb.

ENGINE CONTROLS AND INSTRUMENTS

Throttle

Control

Used to control power by introducing

fuel-air mixture into the intake passages

of the engine. Settings are reflected by

readings on the manifold pressure gage.

Propeller

Control

This control requests the propeller governor to

maintain engine/propeller rpm at a selected

value by controlling propeller blade angle.

Mixture

Control

This control is used to set fuel flow in

all modes of operation and cuts off fuel

completely for engine shut down.

EGT

(Exhaust Gas

Temperature

Indicator)

This indicator is used to identify the lean

and best power fuel flow mixtures for

various power settings during cruise.

Tachometer

Indicates the rpm of the engine/propeller.

Propeller

Governor

Regulates the rpm of the engine/

propeller by increasing or decreasing the

propeller pitch through a pitch change

mechanism in the propeller hub.

AIRPLANE PERFORMANCE

AND FLIGHT PLANNING

Climb Gradient

The ratio of the change in height during a

portion of a climb, to the horizontal distance

traversed in the same time interval.

Demonstrated

Crosswind

Velocity

The demonstrated crosswind velocity is

the velocity of the crosswind component

for which adequate control of the airplane

during takeoff and landing was actually

demonstrated during certification tests.

The value shown is not limiting.

MEA

Minimum enroute IFR altitude.

Route Segment

A part of a route. Each end of that part

is identified by: (1) a geographical

location; or (2) a point at which a

definite radio fix can be established.

GPH

U.S. Gallons per hour.

Summary of Contents for BONANZA ACCU-SIM V35B

Page 1: ...A2ASIMULATIONS BONANZA ACCU SIM V35B BONANZA ...

Page 2: ...reen should be at eye level or below and the monitor should be tilted slightly back wards to prevent strains to your cervical spine Reduce your screen s brightness to lower the con trast and use a flicker free low radiation monitor Make sure the room you play in is well lit Avoid playing when tired or worn out and take a break every hour even if it s hard Epilepsy Warning Some people experience ep...

Page 3: ...A2ASIMULATIONS BONANZA ACCU SIM V35B BONANZA ...

Page 4: ...FUTURE 36 DEVELOPER S NOTES 38 FEATURES 40 FSX QUICKSTART GUIDE 42 P3D QUICKSTART GUIDE 44 ACCU SIM 48 ACCU SIM AND THE COMBUSTION ENGINE 54 PROPELLERS 59 GENERAL 64 EMERGENCY PROCEDURES 69 NORMAL PROCEDURES 74 PERFORMANCE CHARTS 86 WEIGHT AND BALANCE 90 SYSTEMS DESCRIPTION 100 AUTOPILOT 106 2D PANELS 110 CREDITS ...

Page 5: ...www a2asimulations com ACCU SIM V35B BONANZA A2ASIMULATIONS 5 FOR SIMULATION USE ONLY ...

Page 6: ...irfoil wing which Beech had also used on its Model 18 Twin Beech a circular flush riveted stressed aluminium fuselage fully enclosed electrically retractable undercarriage a retractable by Mitchell Glicksman 2018 BEECHCRAFT BONANZA boarding step gap sealed recessed flap tracks cockpit adjustable cowl flaps internally hinged control sur faces and at first an electrically pitch adjustable 2 blade wo...

Page 7: ... military advances on all fronts were a clear indication to even the most hard ened cynic that victory was forth coming Whilst horrific combat would still continue for a time in Europe and even longer in the Pacific by January 1945 the general feeling was that an end to this monstrous blood bath was indeed nigh Meanwhile as 1 000 plane bomber raids were regularly reported in newspapers and shown i...

Page 8: ...lton Standard propellers Model 18 s engines were soon upped to 450 hp 336 kW Pratt Whitney R 985 radial engines turning the new Hamilton Standard three blade constant speed propellers However the construction and manufacturing methods required for building Model 18 were entirely new to Beech In fact Beech Model 18 was a quantum leap from Model 17 in every way A beautifully restored Belgian registe...

Page 9: ...ister ing top speed of 370 mph at sea level faster than most of the Japanese fighters that it was likely to encounter Although the war ended before XA 38 Grizzly could go into pro duction and prove its worth in combat it was in its day an extraordinary and unmatched achievement in design and sophisticated construction technique for what had previ ously been a light aeroplane company Beech s produc...

Page 10: ...ft manufacturers when it conceived and designed Model 35 Bonanza in 1944 Whilst Model 18 was a great success the production of which continued until 1970 with more than 9 000 ultimately produced Walter Beech and his staff had been optimisti cally looking toward the post war civilian aviation world to come The plan they developed was to produce a high performance luxury all metal four seat single e...

Page 11: ...hought What was not spoken of if it was thought of at all was that immediately after the end of the war a tremendous glut of surplus grasshoppers all of those high wing low powered mostly two seat aircraft would be offered as sur plus to the public at very low prices For instance in 1945 the Office of Price Administration OPA made surplus two seat Aeronca L 3B Champs in virtually unused condition ...

Page 12: ...r Model 17 Staggerwing is a unique and extraor dinary design particularly for a biplane and it is certainly impressive to the eye many consider Staggerwing to be the most beautiful biplane ever built Despite its inherent disabilities the extra wing along with the struts and wires required to keep it in place Staggerwing performed very well indeed However aside from its inferior overall perfor manc...

Page 13: ...o had been instrumental in the design of both the Model 17 Staggerwing and Model 18 Twin Beech together with project engineer Ralph Harman set about the task of putting together a team of creative aircraft designers Their mission was to design an entirely new single engine aeroplane not only for the post war era but for decades to come Such an aeroplane had also been Harman s dream and he was high...

Page 14: ...e out of the box firmly sit ting atop of the aviation mountain confidently and reso lutely daring all comers to topple it As history has shown despite a most valiant but ultimately failed effort by Piper to do just that with its superb PA 24 Comanche no aero plane so far has quite been able to do so WHY BONANZA 5 In Walter Beech s own words in 1946 Airplanes have been named after stars galaxies co...

Page 15: ...r and with the elevator neutral the left ruddervator is displaced 23º upward and with full up eleva tor and with right rudder simul taneously the left ruddervator is displaced 44º upward By con trast the elevator of the con ventional tail of an A36 Bonanza is limited to 23º upward and 20º downward displacement while the rudder is limited to 25º left or right displacement V TAIL DISADVANTAGES Weigh...

Page 16: ...ll from side to side whilst also yawing in the opposite direction of the roll and not remaining at or returning to level flight without engaging a yaw and or pitch damper an auto pilot and or the pilot s corrective control input Accordingly Bonanza s 30º 33º ruddervators tend to cause Dutch Roll at the rear of the aeroplane which has been reported to cause both yaw and pitch wandering and pitch se...

Page 17: ...enting with a V tail Time would soon solve that mystery A 19 would certainly be a challenging subject for a can you name this aeroplane contest USAAF archive photo circa 1944 Eclipse Aviation 400 If you re going to put a single jet engine on top of the fuselage a V tail seems like your best if not your only bet Robin ATL Beyond appearance there seems to be no real need for a V tail in this design ...

Page 18: ... s V tail turned out to have any basis in reality Whatever Walter Beech may have thought of the V tail s aerodynamic benefits he was most enthusiastic about it for aesthetic and commercial reasons He correctly understood that even if the V tail did nothing at all about improving performance it certainly made Bonanza the most distinctive light general aviation aeroplane in the world So it was and s...

Page 19: ...for the retracted undercarriage and fuel tanks while still showing an excel lent lift drag ratio and close to a neutral pitching moment coefficient providing a stable and predictable pitch axis throughout its wide Alpha range although as we shall see this stability was somewhat undone by the mildly destabi lizing characteristics of the V tail Early Bonanza s narrow weight and balance envelope make...

Page 20: ...e on general aviation aeroplanes One of the very few of those with a nosewheel was the brilliant Fred Weick s innovative and prescient ERCO Ercoupe First flown in 1937 it remained in production by one manufacturer or another until 1969 A nosewheel for Model 35 was an innovative feature for an aeroplane of its type Even rival Spartan 7W had a tailwheel However Beech surprisingly held back a bit fro...

Page 21: ...ose home was certainly not such a bucolic environment to be sure based at a seaplane base near my home where I first learned to fly at the age of 12 That C 195 was not used for instruction of course that big Jacobs radial cost a bunch to run and maintain It was used for morning and afternoon commuter flights in and out of New York City I flew their two Luscombe Silvaire 8A floatplanes one at a tim...

Page 22: ... a laminated wooden two blade electri cally manually variable pitch not constant speed pro peller Constant speed propellers were nothing new in 1945 Beech itself was quite familiar with them as they were installed on its Model 18s had been proven reliable and were in general usage on high performance aircraft since 1935 However Beech curiously installed this throw back and inefficient propeller sy...

Page 23: ...n beyond actual dual instruction this writer can report from personal experience that checking out in a Bonanza with a throw over control wheel is an awkward and unpleasant experience especially I suss for the check out pilot 10 This the pilot is solely in command system has been and remains unpopular with many prospective Bonanza owners and has precluded such Bonanzas from use as an advanced trai...

Page 24: ...climbing out after takeoff and during approach and landing both being low altitude conditions in which stall spin recovery is unlikely A Brief Primer Regarding Longitudinal Stability The lateral pitch axis of an aeroplane is that axis around which the nose rises and descends An aeroplane s CG is that point at which aircraft longitudinally balances on the lateral axis An aeroplane s centre of lift ...

Page 25: ...m helps to desensitize Bonanza s very light pitch control and give it more feel in all situations THE BONANZA BONANZA The initial price of the Bonanza was 7 345 the equiva lent of 82 010 71 in 2018 with a cumulative inflation rate of 1 016 6 A lavishly equipped 2018 Beechcraft G36 Bonanza was recently placed on sale for 913 105 although earlier and more modestly equipped Bonanzas are regularly pur...

Page 26: ...oughout the 1950s people all over the world deeply desired and worked hard to create a new beginning A new clean peaceful and prosperous world had been promised and now for some it was in their grasp In the United States everything from buildings to automobiles to kitchen appliances to furni ture to the new retractable ballpoint pens took on a clean streamlined and modern look The stodgy old heavi...

Page 27: ...www a2asimulations com ACCU SIM V35B BONANZA A2ASIMULATIONS 27 FOR SIMULATION USE ONLY ...

Page 28: ... in the late 1940s and early 1950s were not used to aircraft as clean and demanding as Bonanza and why should they have been Nothing like Bonanza had previously been available to them Aerodynamically clean low drag aeroplanes are excellent and effi cient cruisers They get the most out of the power avail able and they go fast Unfortunately that is not the totality of the matter Clean aeroplanes lik...

Page 29: ... which may also go unnoticed by a pilot not trained to fly in IFR conditions As mentioned pilots have reported that V tail Bonanzas are very light and sensitive in pitch to the extent that flying a V tail Bonanza has been described as being sportscar like Also V tail Bonanzas are notoriously unsteady in pitch and roll tending to constantly seek pitch position and laterally wander from level flight...

Page 30: ... speculated was because of Beech s apparent reluctance to officially and publicly acknowledge that there was anything fundamentally wrong with the original V tail design to begin with In addition to the increase in the ruddervators area Bonanza C35 has a more powerful Continental E 185 11 engine upping the hp from 165 hp to 205 hp for one minute and 185 hp continuous all of which make it a very de...

Page 31: ...r and Co who in 1956 was developing Piper PA 24 Comanche which Mr Piper hoped and publicly stated would be The Bonanza Killer Whilst Comanche is a superb aeroplane in every way comparable and in some ways supe rior to Bonanza neither it nor any other aeroplane has ever been able to kill Bonanza Since Bonanza s introduction it has been the icon at the top of the hill of general aviation aircraft an...

Page 32: ...sic V35 nomencla ture however the 35B is in fact a new model V35B fea tures a completely new interior with additional headroom including redesigned and improved seats a new instrument panel and a more efficient ventilation system The exte rior remains essentially the same as V35 however V35B has a new paint scheme The price of a V35B was 41 600 in 1972 248 359 96 in 2018 with an a cumulative infla...

Page 33: ...le on right flap on left Gear driven alternator Extended aft baggage area COMMON OPTIONS AND MODIFICATIONS Long range fuel two 40 gallon tanks V35TC TSIO 520D STC Other engine upgrades Forward facing family 5th and 6th seats in aft baggage area Tip tanks Large aft baggage door Improved cabin ventilation system Dual control yoke Avionics upgrades OUR NEW BIRD We hope that you will find flying A2A s...

Page 34: ...a new and more enlightened era in aviation accident forensics and caused the immediate institution of dozens of safety regulations One of the positive changes which were made was with regard to more regular and intensive inspection of commercial aircraft As might be expected after the Rockne crash and the widely published official report of its cause wooden winged aeroplanes went distinctly out of...

Page 35: ...s more vertical increas ing lift but also reducing drag oppo site and equal reaction The altered angle of lift reduces Induced Drag which accordingly reduces the rate at which the aeroplane decelerates It is the combination of additional lift and reduced drag which causes the aero plane to float above the runway when in Ground Effect 9 4 CFR 91 109 states No person may operate a civil aircraft exc...

Page 36: ...36 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY DEVELOPER S NOTES ...

Page 37: ...lay a sport on the weekend injuries erupt The same holds true for the busy professional working all week who then decides to occasionally fly a high performance air plane like the Beechcraft Bonanza V tail The V tail Bonanza was built from World War II fighter technology which was designed for highly trained professional pilots And like most Warbirds the Bonanza want so fly fast all the time Unlik...

Page 38: ...when the computer is off n n Immersive in cockpit physics driven sound environment from A2A engineered recordings n n Complete maintenance hangar internal systems and detailed engine tests including compression checks n n Aircraft DNA technology re creates actual engine and airframe vibrations n n V tail physical modeling captures the character of this classic aircraft n n New analog gauge physics...

Page 39: ...for handy in flight navigation n n Authentic fuel delivery includes priming and proper mixture behavior Mixture can be tuned by the book using the EGT Fuel flow or by ear It s your choice n n All models include A2A specialized materials with authentic metals plastics and rubber n n Airflow density and its temperature not only affect the way your aircraft flies but how the internal systems operate ...

Page 40: ...and or multiple core processor or better recommended HARD DRIVE 250MB of hard drive space or better VIDEO CARD DirectX 9 compliant video card with at least 128 MB video ram 512 MB or more recommended OTHER DirectX 9 hardware compatibility and audio card with speakers and or headphones INSTALLATION Included in your downloaded zipped zip file which you should have been given a link to download after...

Page 41: ...NOT set as the default aircraft flight in FSX SUPPORT AND QUESTIONS Please visit us and post directly to the A2A support and com munity forums https a2asimulations com forum index php QUICK FLYING TIPS To Change Views Press A or SHIFT A Keep the engine at or above 800 RPM Failure to do so may cause spark plug fouling If your plugs do foul the engine will sound rough try running the engine at a hig...

Page 42: ... exe file which when accessed contains the automatic installer for the software To install double click on the executable and follow the steps provided in the installer software Once complete you will be prompted that installation is finished Important If you have Microsoft Security Essentials installed be sure to make an exception for Lockheed Martin Prepar3D as shown on the right REALISM SETTING...

Page 43: ... at or above 800 RPM Failure to do so may cause spark plug fouling If your plugs do foul the engine will sound rough try running the engine at a higher RPM You have a good chance of blowing them clear within a few seconds by doing so If that doesn t work you may have to shut down and visit the maintenance hangar On landing once the airplane settles slowly pull back on the yoke for additional eleva...

Page 44: ...44 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY ACCU SIM ...

Page 45: ...ns they behave differently For example the tempera ture of the air that enters your carbure tor has a direct impact on the power your engine can produce Pushing an engine too hard may produce just slight damage that you as a pilot may see as it just not running quite as good as it was on a pre vious flight You may run an engine so hot that it catches fire However it may not catch fire it may just ...

Page 46: ...f fuel you left off when you quit your last flight You will learn the easy or the hard way to make at the very least some basic checks on your systems before jumping in and taking off just like a real aircraft owner Additionally in each flight things will sometimes be dif ferent The gauges and systems will never be exactly the same There are just too many moving parts variables changes etc that co...

Page 47: ... or the gyro gauge may fluc tuate when starting the motor or the gauge needles may vibrate with the motor or jolt on a hard landing or tur bulent buffet The gauges are the windows into your aircraft s systems and therefore Accu Sim requires these to behave authentically LANDINGS Bumps squeaks rattles and stress all happens in an air craft just when it is taxiing around the ground Now take that hug...

Page 48: ... ONLY The piston pulls in the fuel air mixture then compresses the mixture on its way back up The spark plug ignites the compressed air fuel mixture driving the piston down power then on its way back up the burned mixture is forced out the exhaust ACCU SIM AND THE COMBUSTION ENGINE ...

Page 49: ...e needs air We need air Engines need air Engines are just like us as they need oxygen to work Why Because fire needs oxygen to burn If you cover a fire it goes out because you starved it of oxygen If you have ever used a wood stove or fireplace you know when you open the vent to allow more air to come in the fire will burn more The same principle applies to an engine Think of an engine like a fire...

Page 50: ...in an emergency situation that requires it For the most part you will be throt tling your motor meaning you will be setting the limit MANIFOLD PRESSURE AIR PRESSURE You have probably watched the weather on television and seen a large letter L showing where big storms are located L stands for LOW BAROMETRIC PRESSURE low air pressure You ve seen the H as well which stands for HIGH BAROMETRIC PRESSUR...

Page 51: ... standard day at sea level your manifold pressure with the engine off will be 30 IGNITION The ignition system provides timed sparks to trigger timed explosions For safety aircraft are usually equipped with two completely independent ignition systems In the event one fails the other will continue to provide sparks and the engine will continue to run This means each cylinder will have two spark plug...

Page 52: ...oil pressure does not rise within seconds then the engine must be shut down immediately Above is a simple illustration of a crankshaft that is located between two metal caps bolted together This is the very crankshaft where all of the engine s power ends up Vital oil is pressure injected in between these surfaces when the engine is running The only time the crankshaft ever physically touches these...

Page 53: ...s creating torque and using that torque to twist the crankshaft With a more pow erful explosion comes more torque The more fuel and air that can be exploded the more torque You can increase an engine s power by either making bigger cylinders adding more cylinders or both Horsepower on the other hand is the total power that engine is creat ing Horsepower is calculated by com bining torque with spee...

Page 54: ...54 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY PROPELLERS ...

Page 55: ...eyond the scope of this manual Unfortunately over time the Bernoulli theory specifi cally has been misrepresented in many textbooks causing some confusion in the pilot and flight training community Misrepresentations of Bernoulli such as the equal tran sit theory and other incorrect variations on Bernoulli have caused this confusion Rather than get into a highly tech nical review of all this we at...

Page 56: ...g creating moderate lift Air vortices lines stay close to the wing Stall A wing that is stalled will be unable to create significant lift Climb Wing creating significant lift force Air vortices still close to the wing LEADING EDGE CAMBERED SIDE OR FRONT FLAT LOWER SIDE TRAILING EDGE CROSS SECTION OF A PROPELLER BLADE ...

Page 57: ...ing which stalled more gradually across the wing The Hershey bar wing has an abrupt stall whereas the tapered wing has a gentle stall A propeller is basically a wing except that instead of relying on incoming air for lift it is spinning around to create lift it is perpendicular to the ground creating a backwards push of air or thrust Just remember whether a propeller is a fixed pitch variable pitc...

Page 58: ......

Page 59: ... Gallons Total Usable 114 Gallons GENERAL GROUND TURNING CLEARANCE A Radius for Wing Tip 26 feet 4 inches B Radius for Nose Wheel 12 feet 2 inches C Radius for Inside Gear 5 feet 1 inch D Radius for Outside Gear 14 feet 8 inches Turning radii are calculated using full steering one brake and partial power OIL Oil Capacity 12 Quarts MAXIMUM CERTIFICATED WEIGHTS Max Ramp Weight 3412 lbs Max Take off ...

Page 60: ...ed at which the airplane is controllable VSO Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configuration VX Best Angle of Climb Speed is the airspeed which delivers the greatest gain of altitude in the shortest possible horizontal distance VY Best Rate of Climb Speed is the airspeed which delivers the greatest gain in altitude in the shortes...

Page 61: ...g an airplane Leveling Points Those points which are used during the weighing process to level the airplane Jack Points Points on the airplane identified by the manufacturer as suitable for supporting the airplane for weighing or other purposes POWER Take off and Maximum Continuous Highest power rating not limited by time Maximum Normal Operating Power MNOP Highest power rating within the normal o...

Page 62: ...ve This Speed Maximum Flap Extension Extended VFE Approach 15 Full Down 30 152 122 154 123 Do Not Extend Flaps or Operate With Flaps Exended Above This Speed Maximum Landing Gear Operating Extended VLO VLE 152 154 Do Not Extend Retract or Operate With Gear Extended Above This Speed Except in Emergency AIRSPEED INDICATOR MARKINGS MARKING KCAS VALUE OR RANGE KIAS VALUE OR RANGE SIGNIFICANCE White Ar...

Page 63: ...hes forward of center line through for ward jack points MAC leading edge is 66 7 inches aft of datum MAC length is 65 3 inches MANEUVER LIMITS This is a utility category airplane Spins are prohibited No acrobatic maneuvers are approved except those listed below Maximum slip duration is 30 seconds APPROVED MANEUVERS 3400 POUNDS MANEUVER ENTRY SPEED KCAS KIAS Chandelle 132 134 Steep Turn 132 134 Laz...

Page 64: ...64 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY EMERGENCY PROCEDURES ...

Page 65: ...e followmg 1 Fuel Selector Valve SELECT OTHER TANK feel for detent 2 Auxiliary Fuel Pump ON 3 Mixture FULL RICH then LEAN AS REQUIRED 4 Magnetos CHECK RIGHT LEFT then BOTH ON NOTE The most probable cause of engine failure would be loss of fuel flow or improper functioning of the ignition system If No Restart 1 Select most favorable landing site 2 The use of landing gear is dependent on the terrain...

Page 66: ...f reaching the landing site selected and on final approach 1 Airspeed ESTABLISH 78 to 83 KTS 2 Fuel Selector Valve OFF 3 Mixture IDLE CUT OFF 4 Magneto Start Switch OFF 5 Flaps AS REQUIRED 6 Landing Gear DOWN or UP depending on terrain 7 Battery and Alternator Switches OFF LANDING GEAR RETRACTED WITH POWER If possible choose firm sod or foamed runway Make a normal approach using flaps as necessary...

Page 67: ...only DO NOT ATTEMPT TO RETRACT THE GEAR MANUALLY 5 If electrical system is operative check landing gear position lights and warning horn check LOG GR RELAY circuit breaker engaged 6 Handcrank DISENGAGE Always keep it stowed when not in use WARNING Do not operate the landing gear electrically with the handcrank engaged as damage to the mechanism could occur After emergency landing gear extension do...

Page 68: ...68 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY ...

Page 69: ...gle of Climb Vx 77 KTS Best Rate of Climb Vy 96 KTS Cruise climb 107 KTS Turbulent Air Penetration 134 KTS Landing Approach 70 KTS Balked Landing Climb 70 KTS PRE FLIGHT INSPECTION The Pre Flight Inspection is another advancement in bring ing real life standard operating procedures into FSX and P3D The inspection system is done in such a way as to emu late making your walkaround inspection prior t...

Page 70: ...heck Gear Lights GREEN 6 AUX Pump ON until ff goes into the green then OFF 7 Throttle Cracked Clear prop 8 Mag Start Switch START 9 Oil Pressure CHECK 10 Ammeter CHECK 11 Mixture LEAN 12 Avionics ON 13 Cowl Flaps OPEN TAXI 1 Radios ON 2 Transponder ALT 3 Altimeter SET 4 Heading Indicator SET 5 Landing Gear Indicator GREEN 6 Radio ATIS 7 Parking Brake RELEASE 8 Breaks Test on Inital Roll 9 Lights A...

Page 71: ...m 25 MP 4 SPEED Best angle 77 kts Best rate 96 kts Best en route 107 kts 5 CHT CHECK 6 Mixture SET FUEL FLOW CRUISE 1 Cowl Flaps CLOSED 2 Power SET 3 RPM AS DESIRED 2 100 2 500 4 Mixture SET FUEL FLOW LANDING APPROACH LANDING 1 Autopilot OFF 2 Fuel Pump ON 3 Fuel Selectors Desired Tank 4 Fuel Levels CHECK 5 Mixture RICH 6 Altimeter SET 7 Cowl Flaps CLOSED 8 If airport elevation is over 4 000 ft LE...

Page 72: ...PERFORMANCE CHARTS ISA CONVERSION PRESSURE ALTITUDE vs OUTSIDE AIR TEMPERATURE TEMPERATURE C PRESSURE ALTITUDE FEET I S A 3 0 C I S A 2 0 C I S A 1 0 C I S A 1 0 C I S A 2 0 C I S A 3 0 C I S A 4 0 C I S A 25 000 20 000 15 000 10 000 5 000 80 70 60 50 40 30 20 10 0 10 20 30 40 50 60 70 80 ...

Page 73: ...STANCE FEET OBSTACLE HEIGHT FEET WIND COMPONENT KNOTS WEIGHT POUNDS OUTSIDE AIR TEMPERATURE ºC OUTSIDE AIR TEMPERATURE ºF Weight lbs Take Off Speed Lift Off 50 FT KTS MPH KTS MPH 3400 71 82 77 89 3200 69 79 75 86 3000 66 76 73 84 2800 64 74 70 81 2600 61 70 67 77 2400 59 68 64 74 Associated Conditions Power Full Throttle at 2700 RPM Mixture Lean to Appropriate Fuelflow Flaps UP Landing Gear Retrac...

Page 74: ...ROPELLER INSTALLED AND D 10313 AND AFTER WITH McCAULEY 3 BLADE PROPELLER INSTALLED EXAMPLE OAT PRESSURE ALTITUDE WEIGHT 5ºC 23ºF 11 500 FT 3380 LBS RATE OF CLIMB CLIMB GRADIENT CLIMBSPEED 470 FT MIN 3 8 96 KTS 110 MPH 60 40 20 0 20 40 60 80 100 120 80 50 60 40 30 20 10 OUTSIDE AIR TEMPERATURE ºC WEIGHT POUNDS RATE OF CLIMB FT MIN CLIMB GRADIENT OUTSIDE AIR TEMPERATURE ºF 0 10 20 30 40 50 60 3400 3...

Page 75: ...S A 1 4 7 1 5 6 1 6 5 1 7 6 1 8 7 1 9 4 1 9 2 18 8 1 4 0 0 0 1 2 0 0 0 1 0 0 0 0 8 0 0 0 6 0 0 0 4 0 0 0 2 0 0 0 SL F U E L F L O W G A L H R W E I G H T S L B S 2 4 0 0 2 8 0 0 3 1 0 0 3 4 0 0 TIME FUEL AND DISTANCE TO CLIMB CLIMB SPEED 107 KNOTS 123 MPH ASSOCIATED CONDITIONS POWER FUEL DENSITY MIXTURE COWL FLAPS 25 IN HG OR FULL THROTTLE 2500 RPM 6 0 LBS GAL LEAN TO APPROPRIATE FUEL FLOW CLOSED ...

Page 76: ...500 15 4 65 9 11 0 158 124 42 6 2500 15 4 63 7 10 6 156 118 Full throttle manifold pressure settings are approximate Red shaded area represents operation with full throttle CRUISE POWER SETTINGS 65 MAXIMUM CONTINUOUS POWER OR FULL THROTTLE 2300 RPM 3200 POUNDS PRESS ALT FEET ISA 36 F 20 C STANDARD DAY ISA ISA 36 F 20 C IOAT ENGINE SPEED RPM MAN PRESS IN HG FUEL FLOW TAS KTS CAS KTS IOAT ENGINE SPE...

Page 77: ...3 2100 16 2 57 6 9 6 138 114 16000 31 35 2100 15 6 55 6 9 3 135 110 Full throttle manifold pressure settings are approximate Red shaded area represents operation with full throttle CRUISE POWER SETTINGS 45 MAXIMUM CONTINUOUS POWER OR FULL THROTTLE 2100 RPM 3200 POUNDS PRESS ALT FEET ISA 36 F 20 C STANDARD DAY ISA ISA 36 F 20 C IOAT ENGINE SPEED RPM MAN PRESS IN HG FUEL FLOW TAS KTS CAS KTS IOAT EN...

Page 78: ...TITUDE FEET F U L L T H R O T T L E 2 1 0 0 R P M F U L L T H R O T T L E 2 3 0 0 R P M F U L L T H R O T T L E 2 5 0 0 R P M 1 5 6 8 B H P 2 1 0 0 R P M 5 5 M C P 1 2 8 3 B H P 2 1 0 0 R P M 4 5 M C P 1 8 5 3 B H P 2 3 0 0 R P M 6 5 M C P 2 1 3 8 B H P 2 5 0 0 R P M 7 5 M C P CRUISE SPEEDS EXAMPLE ASSOCIATED CONDITIONS AVERAGE CRUISE WT TEMPERATURE 3200 LBS STANDARD DAY ISA PRESSURE ALTITUDE POWE...

Page 79: ...800 1900 2000 2100 2200 ENGINE SPEED RPM 2300 2400 2500 2600 2700 2800 MANIFOLD PRESSURE IN HG NOT RECOMMEDED FOR CRUISE POWER SETTINGS RECOMMENDED VALUES OF MANIFOLD PRESSURE AND RPM FOR CRUISE SETTING MANIFOLD PRESSURE VS RPM EXAMPLE ENGINE SPEED MANIFOLD PRESSURE 2450 RPM 24 5 IN HG WITHIN RECOMMENDED LIMITS ...

Page 80: ...25 26 27 28 29 30 140 160 180 200 BRAKE HORSEPOWER 220 240 260 280 SL 3000 5000 7000 75 65 55 45 PERCENT MAXIMUM CONTINUOUS POW ER PRESSURE ALTITUDE FEET TAKE OFF AND CLIMB CRUISE 1 2 1 2 FUEL FLOW VS BRAKE HORSEPOWER EXAMPLE BRAKE HORSEPOWER 213 75 75 MCP BRAKE HORSEPOWER FUEL FLOW CONDITION LEVEL FLIGHT CRUISE 15 25 GAL HR 14 6 GAL HR LEVEL FLIGHT CRUISE 204 CONDITION FUEL FLOW ...

Page 81: ... P M F U L L T H R O T T L E 2 1 0 0 R P M 7 5 M C P 6 5 M C P 5 5 M C P 4 5 M C P 169 159 147 133 136 138 CRUISE TRUE AIRSPEED KTS NOTE RANGE INCLUDES START TAXI AND CLIMB WITH 45 MINUTES RESERVED FUEL AT 45 MCP 145 157 165 150 163 170 RANGE PROFILE 74 GALLONS STANDARD DAY ISA ASSOCIATED CONDITIONS WEIGHT FUEL FUEL DENSITY INITIAL FUEL LOADING 3412 LBS BEFORE ENGINE START AVIATION GASOLINE 6 0 LB...

Page 82: ... T H R O T T L E 2 3 0 0 R P M F U L L T H R O T T L E 2 1 0 0 R P M CRUISE TRUE AIRSPEEDS KNOTS NOTE ENDURANCE INCLUDES START TAXI AND CLIMB WITH 45 MINUTES RESERVE FUEL AT 45 MCP 133 147 159 169 136 150 163 170 138 145 157 165 ENDURANCE PROFILE 74 GALLONS STANDARD DAY ISA ASSOCIATED CONDITIONS WEIGHT FUEL FUEL DENSITY INITIAL FUEL LOADING 3412 LBS BEFORE ENGINE START AVIATION GASOLINE 6 0 LBS GA...

Page 83: ...E LINE REFERENCE LINE T A I L W I N D H E A D W I N D G U I D E L I N E S N O T A P P L I C A B L E F O R I N T E R M E D I A T E O B S T A C L E H E I G H T S ASSOCIATED CONDITIONS POWER FLAPS LANDING GEAR RUNWAY APPROACH SPEED BRAKING RETARDED TO MAINTAIN 900 FT MIN ON FINAL APPROACH DOWN DOWN PAVED LEVEL DRY SURFACE IAS AS TABULATED MAXIMUM EXAMPLE WEIGHT LBS 3400 3200 3000 2800 2600 2400 70 68...

Page 84: ...dings All subsequent changes in airplane weight and balance are the responsibility of the airplane owner and or operator The basic empty weight and moment of the airplane at the time of delivery are shown on the airplane Basic Empty Weight and Balance form Useful load items which may be loaded into the airplane are shown on the Useful Load Weight and Moment tables The minimum and maximum moments a...

Page 85: ... 100 2800 2900 3000 3600 3500 3400 3300 3200 3100 3000 2900 2800 2700 2600 2500 2400 2300 2200 2100 2000 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 74 MOMENT 100 76 78 80 82 84 86 88 WEIGHT POUNDS CENTER OF GRAVITY INCHES AFT OF DATUM MOMENT LIMITS VS WEIGHT Envelope Based on the following Weight and Center of Gravity Limit Data Landing Gear Down Weight Condition Forward C G ...

Page 86: ...TAL Take off Condition 6 Subtract the weight and moment of the fuel in the incremental sequence in which it is to be used from the take off weight and moment The Zero Fuel Condition the Take off Condition and the Landing Condition moments must be within the minimum and maximum moments shown on the Moment Limit vs Weight graph for that weight If the total moment is less than the minimum moment allo...

Page 87: ...4 Occupant Center 1 190 2658 123 0 82 4 234 2190 5 Occupant Center 1 190 2848 123 0 85 1 234 2424 6 Baggage 120 2968 150 0 87 7 180 2604 Use the C G MOM 100 for the occupants as they are positioned in your airplane Consult the POH Weight and Balance Section for the latest occupant positions If the seats are adjustable fore and aft use the position in which that seat is located during flight The Ba...

Page 88: ...f each pedal and move the pedal to its forward or aft position The adjustment lever can also be used to place the right set of rudder pedals against the floor when the copilot brakes are not installed when not in use TRIM CONTROLS Elevator trim is controlled by a handwheel located to the left of the throttle An elevator tab position indicator dial is located above and to the left of the trim contr...

Page 89: ...on of the indicator senses fuel pressure at the fuel distributor and is calibrated to indicate fuel flow in gallons per hour The green arc indicates the normal fuel flow operating range while the red radials indicate the min imum and maximum allowable fuel pressures The higher end of the green arc includes a sawtooth seg ment to indicate the approximate fuel flow required for takeoff and climb at ...

Page 90: ... by engagement of a roller with a track as the nose wheel is retracted The steering link attaches to the steering mechanism on the nose gear with a swivel connection which permits the mechanism to disengage when the nose gear is retracted and operation of the rudder pedals will have no tendency to turn the nose wheel with the gear retracted The minimum wing tip turning radius using full steer ing ...

Page 91: ...r 7 Turn and Slip 8 Compass System 9 Vertical Speed Indicator 10 Warning Light Test Switch 11 Outside Air Temperature 12 Autopilot Altitude Selector 13 Autopilot Mode Controller 14 VOR Indicator 15 Altimeter 16 Slave and Align 17 Ignition 18 Battery and Altenator 19 Propeller De Ice and Pitot Heat 20 Exterior Lights 21 Interior Lights 22 Elevator Trim Wheel 23 Cowl Flap 24 Firewall Air 25 Wing Shi...

Page 92: ...r retracted if the throttle is retarded below approximately 12 in Hg manifold pressure a warning horn will sound intermittently BAGGAGE COMPARTMENT The baggage compartment is accessible through the baggage door on the right side of the fuselage This area extends aft of the pilot and copilot seats to the rear bulkhead Because of structural limitations this area is divided into two sec tions each ha...

Page 93: ...purature 5 Oil Temperature 6 Ammeter 7 Oil Pressure 8 Right Fuel Tank 9 DME Mode 10 Exhaust Gas Temperature 11 Flaps Lever 12 Throttle 13 Mixture 14 Fuel Pump 15 Engine RPM 16 Alternator Air 17 Landing Gear Level 18 Avionics Master 19 NAV GPS Mode 20 Audio Control Panel 21 Nav Com Radio 1 22 Nav Com Radio 2 23 ADF Receiver 24 Transponder 25 Fuel Tip Tank 26 Suction 27 Tip Tank Selector 28 Left Rig...

Page 94: ... excess fuel per hour which bypasses the fuel control and returns to the tank being used Three fuel drains are provided one in each fuel sump on the underside of each wing and one in the fuel selector valve inboard of the left wing root These points should be drained daily before the first flight An additional 40 gallons of fuel and 200lbs of gross weight capacity can be added when tip tanks are i...

Page 95: ...s fully charged and that alternator output has been adjusted by the voltage regu late to balance the load of the electrical equipment in use The alternator out warning light located on the instrument panel can be tested with the TEST WARN LIGHTS switch adjacent to the warning lights INTERIOR LIGHTING Lighting for the instrument panel is controlled by thumb rotated disc type rheostats located on th...

Page 96: ...lets pull the AFT CABIN HEAT control For maximum heat the control is pulled fully out To obtain heated air for defrost ing the windshield pull the DEFROST control out It may be necessary to vary or close the AFT CABIN HEAT control to obtain maximum air flow for defrosting To close off all air from the heater system pull the red FIREWALL AIR control located to the extreme left of the pilot s lower ...

Page 97: ...s from the system The closure bulkhead is held in place with Velcro and may be removed by pulling forward The drain plug should be removed and the moisture drained from the clear plastic line every 100 hours and after exposure to visible moisture either in the air or on the ground EMERGENCY STATIC AIR SYSTEM An emergency static air source may be installed to provide air for instrument operation sh...

Page 98: ...100 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY AUTOPILOT ...

Page 99: ...n his selected mode has been received and accepted by the system and if an armed mode is selected when capture has been initiated It also has integral marker beacon lights and trim failure warning 2 The KI 256 Flight Command Indicator FCI displays the following information Pitch and roll attitude Flight Director pitch and roll commands DH decision height annunciation when used with a radar altimet...

Page 100: ...Autopilot will not engage when the Flight Director is not operating To confirm proper operation of all servos synchronize the Flight Director for wings level Command nose up with FD Vertical Trim control After 3 seconds you should observe the elevator trim wheel turning in the direction com manded Re synchronize the FD for wings level by using the CWS button then command nose down with FD Vertical...

Page 101: ...The NAV mode provides visual bank commands on the Flight Command Indicator and deviation guidance on the PNI to intercept and track a VOR course or an RNAV course Operation of the NAV mode requires the pilot to 1 Tune to the frequency of the selected VOR or VORTAC station For RNAV operation set in waypoint distance and bearing from the VORTAC station 2 Set the PNI course pointer on the desired cou...

Page 102: ...l when the aircraft is on course Automatic crosswind compensation will provide precise tracking VOR LOC deviation is shown on the PNI and actual crab angle will be shown by offset of the course arrow from the lubber line Throughout APPR mode operation LOC and Glideslope deviation or VOR RNAV deviation are displayed on the PNI If the Autopilot is engaged during operation in the APPR mode automatic ...

Page 103: ...puted visual pitch command on the FCI command bars to hold the aircraft at the pressure altitude existing at the time it was activated The mode is activated either automatically by the ALT ARM function or manually by depressing the ALT button on the Mode Controller If the autopilot is engaged it will automatically hold the aircraft at that altitude The Vertical Trim switch may be used to adjust th...

Page 104: ...in miles hour and knots Endurance this figure tells you approximately how long you could remain in powered flight before running out of fuel This figure will update throughout your flight and as such you should take into account that during a climb phase the endurance will be less than once the aircraft is settled in a cruise configuration Range given in statute sm and nautical miles nm this figur...

Page 105: ...ir craft balance when you remove the pilot Control electrical systems such as the generator or magnetos Toggle aircraft lighting both internal and external Change the GPS system installed in your air craft from a bracket mounted handheld unit to panel mounted units or no GPS installed at all Set whether you want the aircraft to already be in a Cold and Dark state when you first enter it Have your ...

Page 106: ...D APT 2 Airport name APT 3 Airport elevation APT 4 Airport radio frequencies Quick Radios Shift 6 This small popup panel provides input for your virtual cockpit radios but in a simplified and easy to use manner This popup features all the amenities of the actual radios but in a singular unit which allows you to control your com munication navigation ADF and tran sponder radios from a single source...

Page 107: ...s components Any component with a yellow highlight is worn but not unserviceable so do not have to be replaced Compression Test At the lower right hand corner is a COMPRESSION TEST button which will tell your mechanic to run a high pressure differential compression test on the engine cylinders This is done by compressed air being applied through a regulator gauge to the tester in the cylinder The ...

Page 108: ... where subsequent checks will be carried out The check list starts with actions to be carried out in the cockpit prior to your walkaround Ensure that the checklist is carried out cor rectly as checks and actions missed here will prevent you from carrying out the proper checks during your walkaround The first of the external checks covers the right wing The checklist now has an addi tional bottom s...

Page 109: ... reset your flight for the changes to take effect you can adjust shortcuts on the fly Aircraft Configurator The Aircraft Configurator for the Accu Sim V35B Bonanza enables the user to customize various aspects of the aircraft 1 GPS If you own third party GPS products including the Flight1 and RealityXP v2 GTN and GNS units you can use this option to add them to the Bonanza s virtual cockpit Defaul...

Page 110: ...110 A2ASIMULATIONS ACCU SIM V35B BONANZA www a2asimulations com FOR SIMULATION USE ONLY CREDITS ...

Page 111: ... PROOFREADING The Beta Team QUALITY CONTROL BETA TEAM The world s most effective and knowledgeable flight simulation beta team including Cody CodyValkyrie Bergland Lewis Bloomfield Forest FAC257 Crooke Glenn GlennC Cummings Ryan HogDriver Gann Captain Jake Gentile Mitchell Glicksman Darryl Killratio Hackett Dudley Henriques Dave Slingers Kingshott Tom Tol3458 LeCompte Alexander Metzgergva Metzger ...

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A2A Simulations BONANZA ACCU-SIM V35B, Manual

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