Oh yeah and as to do I understand what 'beta' means. You bet I do. Been beta testing for a good while. Fact is I have a form that I use to beta test aircraft. (it probably won;t format correctly since it is is in word 97 but here ya go. (BTW I am a commercial pilot with nearly 5000 hours)
BETA TEST LOG (Aircraft)
Aircraft tested_________________Date__
________________
FUNCTIO YES NO Mouse
Controllable?
Y / N
N/A Rating / Outstanding / Excellent / Good / Fair / Poor
O E G F P
# of test
Comments
Does This Simulation Have?
Throttle Levers
Mixture Levers
Prop Levers
Fuel Flow Levers (Usually Turboprop AC only)
Landing Gear Lever
Flap Lever
Cowel Flap Control
Turbo Charger Control
Waste Gate Control
Carbeurator Heat Control
Anit Ice Equipment
De Icing Equipment (Ususally Military Aircrafrt Only)
Internal Light Controls
External Light Controls
External Power
Internal Power
Voltage Meters
Charge Meters
Generators
Inverters
Magnetos
Magneto Controls for Each Mag
Mag controls for each engine
MAP Guage
CHT Guage
N1 Guage
N2 Guage
ITT Guage
Prop RPM Guage
Prop Torque Guage (Usually Turboprops Only)
Eng RPM Guage
Fuel Quantity Guage
Fuel Flow Guage
Fuel Tank Selector Control
Fuel CROSS FEED Selector
Fuel Pump Controls
Fuel BOOST pump Controls
Fuel Primer Controls
Engine Temp Guage
Exhaust gas Temp Guage
Oil Pressure Guage
Oil Temperature Guage
Vaccume Guage
Bleed Air Bands (Turbine Aircraft Only)
Magnetic Compass
Clock
Turn Timer
Turn Coordinator
Slip Skid Indicator
'Ball Turn and Bank' Indicator
Gyro Compass
RMI Indicator
Attitude Indicator
HIS Indicator
Altimeter
Kolosman Window in altimeter
VSI Guage
Airspeed Indicator
ILS
VOR
DME Indicator
NDB
Autopilot
Tacan
GPS
Weather Radar
Storm Scope
Wheel Brakes
Differential Wheel Brakes
Elevator Trim Tab
Aileron Trim Tab
Rudder Trim Tab
STARTUP and RUNUP Procedures
Does the enginestart procedure follow the POH?
Can engines be started seperately?
If improper start sequence is used will engines still start?
Will Damage result?
Do engine instruments respond properly to start sequence?
EGT?
Oil Press?
Oil Temp?
MAP?
RPM?
Prop RPM?
Prop Torque?
N1?
N2?
ITT?
EGT?
When Carb Heat is applied does engine resppond properly?
Does Exercising Turbos cause a rise in MAP?
Does Exercising Props cause a change in RPMs?
Do Rapid Pitch Changes Seem to cause damage to systems during Runup?
Do Pitch Changes cause a change in Prop Torque?
(Ususally Turboprop Only)
Can Props be feathered at full throttle?
If yes does damage result?
When props are feathered with brakes off will aircraft move along the ground?
When Beta Pitch is applied will aircraft Move backward along the ground? (Turbo Prop Only)
Is Beta Pitch Operating range set according to the POH?
What happens if Beta pitch is applied 'out of range'?
When Thrust Reversers are deployed will aircraft move backward along the ground? (Turbine Only)
Are differential brakes effective during taxi operations?
If Engine Oil Temperature exceeds recommended ranges does engine damage result?
If Engine Oil pressure drops below recommended ranges does engine damage result?
Can maximum recommended power settings be exceeded?
Do guages properly reflect the result of a power setting that is too high?
Oil Temp rise
Oil Press Rise/Fall if oil seals fail
EGT rise
N1rise
N2 rise
ITT rise
MAP rise
CHT rise
Fuel Flow rise
Will wheel Brakes hold the aircraft stationary during engine runups?
Does the generator accurately indicate the turning on and off of systems?
Momentary drop in voltage on system on?
Momentary Rise in voltage on system off?
Can control surfaces be viewed from the cockpit when checking proper operation?
Do control surfaces appear, visually, to deflect the proper amount?
Taxi and Takeoff procedures
Will the aircraft make a 360 deg turn on the ground in accordance with the POH?
Does the rudder turn the aircraft as it should during taxi operations?
Do the wheel brakes apply and release as they should?
If taxied too fast will the aircraft exhibit adverse handling characteristics?
Does the aircraft STOP in the stated distance at the stated speed during ground operations?
On takeoff does the aircraft accelerate to takeoff speed in the stated distance?
For Single Engine Aircraft is right rudder pressure required to maintain proper runway alignment?
Does the aircraft require flap application for normal takeoff?
Is this consistent with the POH?
Does the aircraft rotate at the proper speed?
Does the aircraft establish proper climb and airspeed at the recommended power settings?
If equipped with retractable gear does the airspeed rise as the gear is retracted?
If flaps were required toes the airspeed rise as the flaps are retracted?
Is this a gradual rise?
Is this a sudden rise?
Does the nose of the aircraft pitch down as flaps are retracted requiring the pilot to re-trim?
Is this pitch change gradual?
Is this pitch change sudden?
Are trim settings easily maintained?
Are they too coarse?
Are they Too Fine?
Does the trim indicator, if equipped, properly reflect the direction of the trim deflection?
Climb / Cruise Observations
Does Climb performance deteriorate as the aircraft gains altitude?
Is this change in performance consistent with the POH?
Do the instruments properly reflect this difference?
MAP
CHT
EGT
RPM
Prop Torque
Prop RPM
Outside Air Temp?
Are adjustments to the engine, prop, and mixture settings required to maintain proper instrument readings? (Engine power and Fuel flow only for Turbines, Additionally Prop Torque for Turboprops)
Does the settings required accurately reflect data in the POH?
Can the simulated aircraft exceed it's service ceiling?
What effects are noted on the following when this happens?
MAP
RPM
Prop RPM
EGT
CHT
Fuel Flow
Oil Temp
Oil Press
Will the aircraft level at desired cruise altitude ?
If yes does the aircraft hold it's speed or does speed gradually increase?
When entering cruise by the proper method. Does the aircraft settle into the desired altitude at the desired speed?
Do the power, prop and mixture settings accurately reflect data in the POH?
Can the aircraft be trimmed to fly virtually hands off in calm air at cruise altitude?
If equipped with an autopilot will the AP maintain altitude?
Will the Ap maintain heading?
Is the Ap course adjustable?
If yes does the AP turn the aircraft in the proper manner?
If Altitude is Ap adjustable does the AP bring the AC to the proper altitude and hold it?
If the Ap is speed adjustable does it hold the speed properly?
If a 'fully coupled' system can the aircraft be flown properly using only the AP for normal cruise , climb and descent operations?
Will the Ap properly track a VOR signal?
Will the ap properly intercept a localizer signal?
Will the AP hold the runway center line?
Will the Ap hold the glideslope?
Descent and Landing
Does the aircraft accelerate when the nose is lowered?
Is this acceleration rate appropriate for this aircraft?
With proper power settings will the aircraft descend as stated in the POH?
Does airframe damage result from overacceleration of the aircraft?
Is this damage proper?
Will the flaps deploy at speds above that recommended in the POH?
If yes does damage result from such a deployment?
Is the damage consistent with what would be expected at that speed?
Can the landing gear be deployed above the recommended ranges?
If yes, does damage to systems occurr when this is done?
Is the damage consistent with what one could expect by deploying the gear at that speed?
Do the flaps deploy as stated in the POH?
Correct number of settings?
Correct angle and % for each setting?
Does flap deployment cause the nose to picth up?
Is the change gradual?
Is the change sudden?
Dxoes flap deployment cause the aircraft to decelerate?
Is this change in speed consistent with what would be normally expected?
Does the deployment of the landing gear cause the aircraft to nose down slightly?
Is this change gradual?
Is this change sudden?
Does Gear deployment cause a loss of airspeed?
Is this loss consistent with what would normally be expected?
Does the aircraft respond properly to power setting changes when gear and flaps are deployed?
Is the pilot required to re-trim the aircraft after deployment of flaps and / or gear?
Will the aircraft maintain the stated rate of descent at the power settings stated in the POH?
Can the aircraft, with proper power management, be 'flown' onto the runway?
Can a full stall landing be made in this aircraft?
Is touchdown speed appropriate for this aircraft per the POH?
Does the aircraft, when properly landed, exhibit a tendancy to bounce more than it should?
Does the aircraft decelerate as stated in the POH?
Does full back pressure on the controls accelerate this slowing of the aircraft?
Do thrust reversers work properly?
(Turbine ONLY)
Does Beta Pitch work properly?
(Turbo props ONLY)
Do the wheel brakes slow the aircraft smoothly?
Are there any adverse effects noted if wheel brakes are applied above the recommended speed?
Can differential brakes be applied above taxi speed?
Does the aircraft ground loop or crash if one differential brake is applied on landing?
Will the aircraft ground loop or crash if the rudder is deflected at high speed during landing?
Radical In flight manuvers
Does damage result from full or abrupt control movements at speeds in excess of those recopmmended in the POH?
Can the aircraft be rolled?
Can the real world counterpart perform this manuver?
Can the aircraft be looped?
Can the real world counterpart perform this manuver?
Are power settings proper?
If placed in a high banked very tight turn will the aircraft decelerate rapidly to stall speed?
Will it loose significant altitude if opposite rudder is not applied during this manuver and prior to the stall?
Does the Aircraft stall toward the low wing?
Just prior to entering this stall do the tail surfaces lose all control authority?
Will proper stall recovery, neutral controls and gradual back pressure as speed rises, bring the aircraft out of the stall?
Does damage result from this manuver?
Is this consistent with the POH? (Non aerobatic aircraft should sustain at least minimal damage as a result of this)
Are power on stalls entered properly as outlined in the POH?
Are power off stalls entered properly as outlined in the POH?
If placed in a high speed descent and rapidly recovered will the aircraft sustain significant damage?
Can the aircraft be places in a sideslip?
Can the pilot cause a significant altitude loss with proper cross control in a sideslip?
Does the aircraft recover from this configuration properly?
If landed in a 'slip' configuration does the aircraft crash?
If landed HARD will the landing gear fail?
If landed gear up will the aircraft crash?
If landed at a significantly banked attitude will the aircraft crash?
Can the aircraft make a proper two minute turn?
Can the aircraft be manuvered and landed using an instrument approach plate and following the procedure turns?
Will the aircraft make 'S' turns in the appropriate distance and time?
Will the aircraft perform procedure turns and hit the proper headings?
If the rudder is deflected in flight will the aircraft skid?
Does the aircraft 'cross control' appropriately?
Other observations
Does the magnetic compass turn in the proper direction when turning the aircraft?
Does the magnetic compass accurately reflect magnetic deviation?
Is there a compass card for this instrument and if so is it correct?
Does the Gyro Compass turn in the proper direction when turning the aircraft?
Does the gyro compass accurately reflect gyro drift?
Is the Gyro compass adjustable?
Does the attitude indicator properly reflect the aircraft's attitude?
Do the VSI and altimeter readings match properly?
Do engines stop if magnetos are turned off?
Can the ignitors on a turbine aircraft be turned off without causing the engine to stop?
Does the VOR guage accurately track VOR signals?
Does the NDB guage accurately track radio signals?
Does the localizer accurately reflect runway center line?
Does the glideslope accurately reflect the proper glide slope?
Is the ILS signal line of sight only?
Does changing the Kolosman reading on the altimeter properly reflect changes in the aircrafts current altitude?
Does the turn coordinator accurately reflect a standard turn?
Does the turn coordinator / turn and bank indicator accurately reflect a skid or slip?
Does the ball deflect properly and to the correct side of the guage?
Is slip roll coupling properly modled?
Is adverse yaw properly modled?
Is torque properly modled?
Is helical propwash properly modled?
Is 'P' factor properly modled?
Is weather adjustable in this sim?
If yes does the aircraft react properly to cross winds?
Is course drift and deviation correct?
Will the aircraft fly a proper true heading and end up where it should?
If turbulence is modled does the aircraft respond appropriately to air turbulence?
If density altitude is modled does the aircraft perform according to the POH at the various DA's?
Will the aircraft take off at DA above those specified in the POH?
Does the aircraft respond properly to changes in wind direction and speed?
Does the aircraft respond properly to wind gusts?

[This message has been edited by Shacker (edited 11-18-1999).]