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N457GH 

 

 

Rev 4  12/29/19 
 
 
 
 
 
 
 
 
 
 
 
 

22 

SYSTEMS INFORMATION 

 
HDX database updates 
 
Download current data using Seattle Avionics Chart Data Manager (PC only). Download 
aviation obstacle data from Dynon: 

http://www.dynonavionics.com/us-aviation-obstacle-

data.php

. Plug USB drive with current data into cable hanging from HDX under panel, 

then update software in HDX Settings. 
 
12V switch powers USB and 12V charging outlets, magnetic compass light. 
 
D-2 turns on when Master switch is turned on; it will power off automatically if it is not 
set to attitude display showing. 
 
Primer switch is momentary-on type; release and primer valve closes. Priming for 2-3 
seconds should be sufficient for a cold start. 
 
Landing light wig-wag 
 
Landing lights must be on. Wig-wag will automatically activate at 85 kias (VP-X 
setting). 
 
Flap operation 
 
Flap switch will lower flaps to approximately 10, 20, and 30 degrees; depress switch once 
to lower to next setting. Pressing switch up commands flaps to retract full up; if retraction 
to less-than-full up is desired, momentarily press switch down at desired position. Flaps 
may be lowered to approximately 40 degrees using VP-X screen. 
 
Elevator trim 
 
Elevator trim motor operation is limited to 5 seconds. Release and press hat switch again 
to continue trimming. 
 
 
 

Содержание RV-7A

Страница 1: ...Van s Aircraft RV 7A Pilot s Operating Handbook N457GH NOTE Yellow highlighted text indicates items that need to be verified...

Страница 2: ...LING 19 500 FT TAKEOFF PERFORMANCE 575 Ft LANDING PERFORMANCE 500 Ft STALL SPEED CAS Flaps Up Power Off 54 kias Flaps Down Power Off 44 kias MAXIMUM WEIGHT Normal Category 1800 Lbs EMPTY WEIGHT 1034 L...

Страница 3: ...ed 20 95 kias Full 87 kias Do not exceed this speed with flaps down Vy Best Rate of Climb 90 kias Vx Best Angle of Climb 76 kias Vs Stall Speed Clean 54 kias Vso Stall Speed Landing Configuration 44 k...

Страница 4: ...N457GH Rev 4 12 29 19 4 Views...

Страница 5: ...fly the aircraft during normal operations may be on board This aircraft shall be operated under visual flight rules VFR only This aircraft may not be used for compensation or hire except as allowed b...

Страница 6: ...HECK freedom of movement and security 4 Static Sources CHECK open and clear 5 Nav Strobe Light CHECK condition 6 Elevator Trim Linkage SECURE 7 Rudder Cables SECURE RIGHT WING 1 Flap CHECK security 2...

Страница 7: ...ft Landing Light CHECK condition 9 Nav Strobe Light CHECK Condition 10 Aileron CHECK freedom of movement and security 11 Flap CHECK security BEFORE STARTING ENGINE 1 Towbar REMOVED 2 Shoulder Harnesse...

Страница 8: ...agnetos CHECK max 125 drop 50 diff c Carb Heat CHECK RPM drop d Engine Instruments CHECK e Throttle IDLE CHECK then 800 1000 RPM 7 Friction Lock ADJUST 8 Radios SET 9 Transponder SET 10 D 2 ON as need...

Страница 9: ...E 1 Throttle 2100 2700 RPM 2 Mixture LEAN 3 Terrain Alert Layer ON for night flight DESCENT BEFORE LANDING 1 Shoulder Harnesses SECURE 2 Fuel Selector to fullest tank 3 Mixture ADJUST for altitude 4 T...

Страница 10: ...T OFF 6 Ignition Switch OFF REMOVE key 7 Fuel Remaining Hobbs and Tach RECORD 8 Master Switch OFF 9 Fuel Selector OFF 10 12V outlets OFF 11 D 2 OFF SECURING AIRCRAFT 1 Wheel Chocks INSERT 2 Wing Tail...

Страница 11: ...rmance at 10 000 Density Altitude KTAS RPM MAP Fuel Flow Power 130 2200 16 1 6 5 GPH 36 136 2300 17 7 7 6 GPH 46 140 2400 19 4 8 4 GPH 56 Cruise Performance at 12 000 Density Altitude KTAS RPM MAP Fue...

Страница 12: ...datum Main wheel right 93 75 aft of datum Main wheel left 94 00 aft of datum Nose wheel 39 13 aft of datum Fuel 80 aft of datum Pilot and Passenger 97 48 aft of datum Baggage 126 78 aft of datum Airc...

Страница 13: ...N457GH Rev 4 12 29 19 13 Empty CG 81 00 Empty Weight 1033 lbs Sample Weight and Balance Chart...

Страница 14: ...20160 Fuel 6 lbs gal 252 80 20 160 Pilot 170 97 48 16571 60 Pilot 170 97 48 16571 60 Passenger 170 97 48 16571 60 Passenger 0 97 48 0 Baggage 60 126 78 7606 80 Baggage 0 126 78 0 Total 1725 144578 34...

Страница 15: ...F SAE 20 SAE 30 or 20W30 Oil Sump Capacity 8 U S Quarts Minimum Safe Quantity 4 U S Quarts Operating Conditions Oil Temp 75 220 deg F 245 deg F maximum Oil Pressure 115 psi max 55 psi min 25 psi idle...

Страница 16: ...GH Rev 4 12 29 19 16 EMERGENCY PROCEDURES AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure After Takeoff Wing Flaps Up 78 KIAS Wing Flaps Down 70 KIAS Maneuvering Speed Va 76 87 KIAS Maximum Glide 85...

Страница 17: ...ch OFF 5 Wing Flaps AS REQUIRED 6 Master Switch OFF ENGINE FAILURE DURING FLIGHT 1 Airspeed 85 kias 2 Fuel Pump ON 3 Fuel Selector SWITCH TANKS 4 Mixture RICH 5 Carb Heat ON 6 Primer verify OFF 7 Igni...

Страница 18: ...d temp warning red is set to 450 F 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Master Switch OFF 4 Cabin Heat and Vents CLOSE 5 Airspeed 100 KIAS to attempt to extinguish fire 6 Forced Landing...

Страница 19: ...cuit interrupted Vertical Power 4 LAND as soon as conditions permit Note Standby battery will power EFIS for 1 hour COM radio ADS B receiver transponder and autopilot servos will not function ALTERNAT...

Страница 20: ...FAILURE 1 Vertical Power OPERATE FLAPS from touch screen CO DETECTOR ALARM 1 Cabin Heat OFF 2 Air Vents OPEN full 3 If alarm continues LAND as soon as conditions permit WARNING AND CAUTION MESSAGES GP...

Страница 21: ...G FILE MISMATCH Engine monitor indications may be incorrect STANDBY NETWORK ERROR SkyView network has lost its secondary network redundancy ATTITUDE RECOVERING Roll rate has exceeded 150 degrees secon...

Страница 22: ...e display showing Primer switch is momentary on type release and primer valve closes Priming for 2 3 seconds should be sufficient for a cold start Landing light wig wag Landing lights must be on Wig w...

Страница 23: ...AAS GPS System programming and operation is described in the Skyview Installation Guide and HDX Pilot s Guide The installed ADS B OUT system has been shown to meet the equipment requirements of 14 CFR...

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