Piper Lance II User Manual

LANCE II SERVICE MANUAL
TABLE
II-III. RECOMMENDED
LUBRICATING
OILS
Aviation
Grade Oil
Average Ambient
Air Temperature
Oil Inlet Temperature
Desired Maximum
SAE 50
SAE 40
SAE 30
SAE 20
Above 60
°
F
(16
°
C)
30
°
F to 90
°
F
(-1
°
C to 32
°
C)
0
°
F to 70
°
F
(-17
°
C to 21
°
C)
Below 10
°
F
(12
°
C)
180
°
F
(82
°
C)
180
°
F
(82
°
C)
170
°
F
(77
°
C)
160
°
F
(71
°
C)
245
°
F
(118
°
C)
245
°
F
(118
°
C)
2250 F
(107
°
C)
210
°
F
(99
°
C)
Issued: 1/3/78
HANDLING
AND
SERVICING
1C15

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers