Piper Comanche PA-24 Service Manual page 57

TABLE II-I. LEADING PARTICULARS AND PRINCIPLE DIMENSIONS (CONT.)
MODEL
ENGINE
Manufacturer
Model
FAA type certificate
Rated horsepower, RPM:
Full throttle
Oil, SAE number
Oil sump capacity
Fuel aviation grade:
Minimum octane
Fuel injector, Bendix
Magnetos (2), Scintilla:
Left
Right
Magneto timing
Magneto point clearance
Spark plugs (shielded):
Spark plug gap setting
Firing Order
Tachometer drive, ratio to crankshaft
Starter:
Prestolite, 12 volt
Alternator, Prestolite 12 volt (70 amp)
Alternator voltage regulator, Prestolite
Alternator overvoltage relay, Prestolite
Fuel pump drive
6. Refer to latest revision of Lycoming Service Instruction No. 1042.
04/01/09
PIPER COMANCHE SERVICE MANUAL
PA-24-260 Turbo
Lycoming
I0-540-R1A5
1E4
260 HP @ 2700 RPM
See Figure 2-30
12 qts
100/130
RSA-5AD1
S6LN-1209
S6LN-1208
25 degrees BTC
0.016 ± 006 in.
6
6
1-4-5-2-3-6
0.5:1
MZ-4206
ALX8421
VSF 7203
X17621
Lear Seigler RG-17980
II - HANDLING AND SERVICING
1B13