AIRPLANE
OPERATIONS
MANUAL
LIMITATIONS
EMB-145 A1 FAA
REVISION 41
1-01-40
Page
3
Code
05
Copyright © by Embraer. Refer to cover page for details.
STARTER LIMITS
On Ground:
Starting or Dry Motoring........................................... UP TO 5
MINUTES ON,
5 MINUTES OFF
OR
First to Fourth Cycles............................................... 1 MINUTE ON,
1 MINUTE OFF
Following Cycles...................................................... 1 MINUTE ON,
5 MINUTES
OFF
In Flight:
Maximum Continuous Operation Time.................... 5 MINUTES ON
NOTE: No cool down time is required should an in-flight start be re-
attempted.
AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM
(
ATTCS)
ATTCS must be operative to select ALT T/O-1 mode.
For airplanes equipped with FADEC versions previous than B8.0:
At least once a week a Thrust Assurance Check must be
performed by selecting maximum takeoff mode during takeoff and
checking engine parameters.
The Thrust Assurance Check is not required if the owner/operator
actively participate in Engine Condition Monitoring, as described
Chapter 5 of the AE3007A Series Engine Maintenance Manual.
For airplanes equipped with FADEC versions B8.0 and on, the Thrust
Assurance Check is not required.
THRUST REVERSER
Thrust reversers are intended for use during rejected takeoff or landing
o
nly. Do not attempt a go-around procedure after deployment of the
thrust reversers following a landing.
Selection of thrust reversers in flight or their preselection before
touchdown is prohibited.
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