Schweizer S300C 269C - Section II - LIMITATIONS (FAA APPROVED)

Limitations
Model 269C Helicopter Pilot's Flight Manual
Reissued:
2-i
Sec tion II
LIM I TA TIONS
IN DEX
Paragraph
Title Page
2-1
2-2
2-3
2-4
2-5
2-6
2-7
2-8
2-9
2-10
2-11
2-12
Ro tor craft Cer tif i ca tion ..............
Flight Lim i ta tions .................
Flight Lim i ta tions Plac ards ............
Mul ti pur pose Util ity Op er a tions .........
Air speed Lim i ta tions ...............
Ro tor Speed Lim i ta tions .............
Fig ure 2-1 Vari a tion of V
NE
with Al ti tude . .
snoit at i miL GC dna thgieW ............
)epol ev nE GC( yti varG fo ret neC ........
Fig ure 2-2. Cen ter-of-Grav ity En ve lope....
Power Plant Lim i ta tions
(Lycoming HIO-360-D1A) ..........
Ta ble 2-1. SAE Oil Grades ..........
met syS leuF ...................
Ta ble 2-2. Fuel Ca pac ity............
Aux il iary Fuel Tank Cal i bra tion .........
Ta ble 2-3. Aux il iary Fuel Quan tity ......
In stru ment Mark
ings ...............
Fig ure 2-3. Air craft In stru ments ........
2-1
2-1
2-2
2-4
2-4
2-4
2-5
2-6
2-6
2-7
2-8
2-8
2-9
2-9
2-9
2-9
2-10
2-10
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
FAA Approved
CSP Book 1 CSP-C-1.indd 49 8/4/19 12:45 PM