Specifications

SECTION I
DESCRIPTION AND SPECIFICATIONS
MODEL 560
APPROACH AND LANDING IN ICING CONDITIONS
When any residual ice is present or can be expected during approach and landing, V
REF
and V
APP
must
be increased. V
REF
and V
APP
, the landing distance, and the maximum landing weight permitted by brake
energy limits must be corrected per the appropriate tables in the Airplane Flight Manual Section IV,
Performance - Approach and Landing.
NOTES
1. Oil Pressure
a. Normal Oil pressure is 45 to 140 PSI at N
2
speeds above 60%. Oil pressure
below 45 PSI is undesirable and should be tolerated only for the completion
of the flight, preferably at reduced power setting.
b. For starting, oil pressure may exceed 140 PSI (not to exceed 270 PSI) for up
to 400 seconds. N
1
should not be increased above idle until oil pressure is
below 140 PSI.
2. Takeoff ratings that are nominally limited to 5 minutes duration may be used for
up to 10 minutes for One Engine Inoperative operations without adverse effects
on engine airworthiness.
3. High idle corresponds to flight idle.
4. N
1
% Fan RPM is limited to either 100% N
1
or the appropriate thrust setting chart
in Section IV (Standard Charts) of the basic FAA Approved Airplane Flight
Manual, whichever is less.
Figure 1-4 Engine Operating Limits
* Refer to Figure 1-6.
** Refer to Figure 1-7.
OPERATING CONDITION
THRUST
SETTING
(Configuration
Code)
TIME LIMIT
(MINUTES)
OPERATING LIMITS
MAX
OBSERVED
ITT
°C
N
2
%
N
1
%
OIL
PRESSURE
(NOTE 1)
PSI
OIL TEMP
°C
TAKEOFF
5 (NOTE 2)
700 100 100
(NOTE 4)
45 TO 140
10 TO 132.2
MAXIMUM
CONTINUOUS
CONTINUOUS 700 100 100
(NOTE 4)
45 TO 140
10 TO 132.2
GROUND IDLE CONTINUOUS
>> 49.1 MIN >> 25 TO 140 -40 TO 132.2
FLIGHT IDLE
(NOTE 3)
CONTINUOUS
>> 52.9 MIN >> 25 TO 140 -40 TO 132.2
STARTING
>> 740** >> >> >> -40 MIN
TRANSIENT 20 SECONDS 740
** 102* 102* 0 MIN >>
TRANSIENT
(AH,AI)
200 SECONDS
(NOTE 1b)
>> >> >> 20 TO 270 140.5 MAX
TRANSIENT
(AB,AR)
400 SECONDS
(NOTE 1b)
>> >> >> 20 TO 270 140.5 MAX
I 1-10 Configuration AA 56OMB-01