
Zack Gets First GA Flight in Experimental


My friend Harry sold his beautiful Cessna 150. Here are the details:














3/3/17 Tach 162.6, Total Time 182.5
3/26/17 Tach 170.3, Total Time 191.1
4/12/17 Tach 172.5, Total Time 193.8
6/27/17 Tach 202.3, Total Time 227.9
7/1/17 Tach 203.9, Total Time 229.7
7/8/17 – 7/9/17 Tach 203.9, Total Time 229.7
3/3/17
Replaced and re-glued the screens over both left and right fuel vent intakes.
There was a small weep of oil at the oil cooler / oil hose connections. I used steel fitting in the oil cooler (instead of aluminum) and did not get the oil lines tightened enough. I tried tightening them just a bit more while holding the steel fittings with another wrench. This seems to have stopped the slow weep.
I re-installed the engine air filter which had popped up from a small engine backfire during a previous start.
The alternator wire was chafing a bit. Fixed.
4/1/17
Changed oil. Took oil sample (was from end instead of middle of draining by accident). Changed oil filter. Did not change or check suction screen during this oil change.
4/12/17
Removed all 8 spark plugs. Determined 3 of 4 bottom spark plugs had lead build ups and decided to replace them (200 hours). Gapped the 4 upper plugs to < 0.020 and > 0.015 quickly but not very precisely.
Installed lower cowl heat shield material from Vans on the inside of the lower cowl to protect the fiberglass from the exhaust areas where it was starting to discolor.
Aileron travel limits: section 15, page 15-2
Max Up/Down= 32/17
Minimum Up/Down= 25/15
Elevator travel limits:
Max Up/Down= 30/25
Minimum Up/Down= 25/20
Measured 2016-12-10:
Ailerons: LU: 30, LD: 17, RU 32, RD 17
Elevator travel: 29 Up, 23 Down
max end of the range. i.e. 30* up and 25* down
Changed Oil
SB 14-02-05 Elevator Spar Cracks – Inspected – None found
SB 14-01-31 HS Front Spar Bend Cracks – Inspected – None found
http://www.precisionairmotive.com/servpubs.htm
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Found wet B-Nut on rear side of fuel pump |
| Found loose spare AN365 nut under passenger seat pan |
| Found rivet junk in footwell area |
| Found plastic cap in footwell area |
| Removed passenger stick, cut zip ties |
| Removed left and right gear tower carpet covers |
| Found cracked engine baffle near oil cooler mount on #4 cylinder, added reinforcement |
| Each aileron trailing edge droops 3/16 when opposite aileron/flap/tip are in alignment |
| Routed GDL cable to dash top through hole |
| Added pin #15 on roll servo via spare white wire (CWS Disc) and spliced it into green CWS Disc wires for sticks under right passenger seat pan |
| Added prop leading edge tape |
COMPRESSION TEST/80 HOT_______COLD__Y__1._76__2._78__3.__78__4.__78__
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| SERVICE OR REPLACE SPARK PLUGS, GAP 0.016 TO 0.021
1B: 0.018 (Original) 1T: 0.018 (Newer Tempest) 2B: 0.018 (Original) 2T: 0.018 (Newer Tempest) 3B: 0.019 (Original) 3T: 0.018 (Newer Tempest) 4B: 0.018 (Original) 4T: 0.018 (Newer Tempest) Install bottom plugs to 360-420 inch lbs torque (30-35 foot lbs) |
The connector for my plane power alternator had a wire crimp failure due to vibration. I found information on replacement connectors on VAF. Here are the links: