Kodiak 100 Series User Manual

Pilot’s Operating Handbook
3A-3
DO NOT USE FOR FLIGHT OPERATIONS
Section 3A
ABNORMAL PROCEDURES
100 SERIES
Abnormal
3A-1 GENERAL
This section of the Pilot’s Operating Handbook describes the recommended
procedures for managing various types of abnormal procedures or
malfunctions that may occur. Performing proper preight inspections and
maintenance procedures will help prevent abnormal airplane or powerplant
malfunctions. However, if an abnormal malfunction should take place, the
basic procedures outlined in this section should be considered and applied,
as required, to remedy the problem.
3A-2 ABNORMAL PROCEDURES CHECKLIST
The following checklist is provided for abnormal procedures with the airplane
or powerplant system. The list provides a challenge or item of issue on the
left hand and the proper response or condition for each item on the right.
ABNORMAL ENGINE PROCEDURES
ITT
(ITT annunciation shown on PFD)
1. Power Lever: REDUCE POWER to within limits and carefully monitor
engine gages for abnormal oil pressure, oil temperature or power
indications.
2. If engine gages are normal, proceed to destination and determine if an
engine inspection is required prior to next ight.
3. If engine gages suggest imminent engine failure, proceed in accordance
with Engine Failures checklists or at the discretion of the pilot and
consistent with safety; continue engine operation in preparation for an
emergency landing as soon as possible.
NG Overspeed
1. Power Lever: REDUCE POWER to within limits and carefully monitor
engine gages for abnormal oil pressure, oil temperature or power
indications.
2. Proceed to destination and determine if an engine inspection is required
prior to next ight.
NP Overspeed
1. Propeller Lever .................................................. REDUCE
Np
to within limits
(If propeller RPM continues to overspeed, reduce power to minimum
possible.)
2. Airspeed..............................................................Reduce to 100 KIAS or less
3. Aircraft
......................................................... Land at nearest suitable aireld
If possible, always retain glide capability to the selected landing aireld
in case of total propeller failure. In the event of heavy vibration or
uncontrolled propeller speed runaway, be prepared to shut down engine.
Uncontrolled if printed

Kodiak 100 Series Specifications

General

Manufacturer	Daher
Engine	Pratt & Whitney Canada PT6A-34
Service Ceiling	25, 000 feet
Seating Capacity	10
Crew	1-2
Range	1, 132 nautical miles
Type	Utility aircraft
Length	34 feet 2 inches
Wingspan	45 feet
Max takeoff weight	7, 255 pounds
Power Output	750 shp
Cabin Width	4 feet 6 inches