2-8. POWER PLANT LIM I TA TIONS
Lycoming: HO-360-C1A
Car bu re tor: Model HA-6 10-6030-1 on Air craft S/N 73 thru 0138
Model HA-6 10-6030 on Air craft S/N 1-72 un less
retro fit ted with Model HA-6 10-6030-1
Lycoming: HIO-360-G1A, Fuel in jected.
Max i mum con tin u ous power is 180 horse power at 2700 rev o lu tions
per min ute. (No mo men tary overspeed is al lowed, ref er ence
Lycoming Ser vice Bul le tin No. 369J).
The min i mum rpm is 2530.
The range for en gine idle speed is 1200 to 1600 rpm.
With ro tor dis en gaged, avoid en gine idle speed in ex cess of 1600
rpm.
CAU TION
If engine RPM ex ceeds 2000 RPM with rotor dis en -
gaged in spec tion of drive shaft in ac cor dance with
HMI Ap pen dix B is re quired be fore any fu ture op -
er a tion.
The ini tial clutch en gage ment speeds are 1500 to 1600 rpm.
Min i mum grade fuel = 100/130 or 100LL.
Lu bri cating oil rec om men da tions (see Ta ble 2-1, See Lycoming Ser -
vice In struc tion No. 1014K or later re vi sion for ad di tional oil rec om -
men da tions).
Limitations
Pilot's Flight Manual
2-6 Reissued: 16 Jan 2019
SCHWEIZER
Model 269C-1 Helicopter
FAA Approved
CSP book 2..indd 52 8/4/19 12:53 PM
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