SALES ITEM:
FAIRCHILD 24 G
Serial Number 2958
NC-19173
|
|
|
 |
|
|
Click on image to view a larger photo.
|
|
|
|
|
|
|
|
Equipment List:
(As weighed, June 26, 1996)
ENGINE
1. Warner Super Scarab 185, R-550, Serial Number 6008
2. Starter, Eclipse
3. Alternator, 35 amp, Farhat
4. Oil temperature regulator, 5 inch, U.A. P.
5. Vacuum pump, Airborne, 212
6. Propeller, Wooden, Sensenich, (Weight & Balance Report dated June 26, 1996) OR
7. Propeller, Aluminum, Curtis Reed, 8668, Model 55518, Serial Number M2150
(Weight & Balance Report dated April 18, 2005) see NOTE below
AIRFRAME
1. Wheels and hydraulic brakes, Cleveland 7.50 x 10
2. Battery, Gill, G-35
3. Tailwheel, 8 inch, streamline
4. Landing light, retractable, Grimes
5. Navigation lights, Grimes
6. Flare tube ports and switches
7. Ground handles
INSTRUMENTS & EQUIPMENT
1. Airspeed Indicator, U. S Gauge
2. Turn & Bank indicator, vacuum, Bendix
3. Rate of Climb indicator, Pioneer
4. Altimeter, sensitive, Kollsman
5. Gyro Horizon, A.I.M.
6. Gyro Compass, Sperry
7. Outside Air Temperature Indicator, electric
8. Magnetic Compass, Bendix
9. Oil Pressure Indicator, U. S. Gauge
10. Oil Temperature Indicator, U. S. Gauge
11. Voltmeter/Ammeter, General Electric
12. Clock, Wakmann
13. Carburetor Temperature Indicator, A. I.D.
14. Manifold Pressure Indicator, U. M. A.
15. Hour Meter, Hobbs
16. Vacuum Gauge
17. Exhaust Gas Temperature Gauge
18. Cylinder Head Temperature Gauge
19. Strobe Light, Tri-Star
20. Seaplane lift/attach fittings
21. Fire Extinguisher
22. Auxiliary Power Receptacle, Piper
AVIONICS
1. Navcom, Bendix King, KX-125
2. Transponder, Bendix King, KT-76A
3. Audio Panel/Marker Beacon, Terra TMA 350
4. Loran, 618-C, Apollo II
5. Emergency Locater Transmitter, Ameri-King AK 450
6. Antennas; Communicaton, GPS, Marker Beacon, Transponder, VOR, Loran
OPTIONAL FACTORY EQUIPMENT
1. Bench seat, rear
2. Streamlines, wheel
3. Ventilating system
4. Flaps and Controls
5. Cabin Trim
6. Exterior Finish
7. Fuel Tank, Auxiliary, 20 gallon capacity
8. Gust lock
NOTE: Weight and Balance Reports dated June 26, 1996, and April 18, 2005, are both valid. Aircraft owner/operator/pilot is responsible for using the applicable Weight and Balance Report (based on propeller installation) in order to determine proper aircraft loading.
RECAP OF WEIGHT & BALANCE
With Curtis Reed Propeller and above listed equipment installed:
Weight Center of Gravity
Empty 1,635 17.04
Useful Load 765
Maximum 2,400 +16.6 to 25.9
Datum is wing leading edge