Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 341 / 625

4-14 Before Landing
Approach Check 4-14-01
1. Altimeter...................................... SET
2. Ice Protection system.................. AS REQUIRED
3. Inertial Separator........................ OPEN, if operating on unprepared
surface or for birdstrike protection
4. Fuel Quantity............................... CHECK
5. Landing Gear.............................. DOWN (below 180 KIAS)
6. Taxi and Landing Lights.............. (AS REQUIRED)
7. Flaps........................................... AS REQUIRED
With residual airframe ice........... SET maximum 15°
Boot failure.................................. Maintain at 0°
Note
For flap settings for crosswind operation, icing conditions and associated landing
performance refer to
Airspeeds for Normal Operations
and Section 5 -
Performance.
Note
If the optional TAWS Class A or RAAS are installed, activate FLAP OVRD for
approaches and landing where flap settings are intentionally at less than 40° to
avoid an aural flaps annunciation during final approach.
8. Speed.......................................... As indicated by Dynamic Speed Bug (1.3
V
S
)
9. FMS Auto speed (if selected)...... Verify and confirm correct
---------- END -----------
Final Check 4-14-02
1. Landing Gear.............................. 3 Green Lights
2. Flaps........................................... 40° or AS REQUIRED
With residual airframe ice........... SET maximum 15°
Boot failure.................................. Maintain at 0°
Continued on next page
Section 4 - Normal Procedures (EASA Approved)
Before Landing
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 4-14-1
12-C-A15-30-0414-00A-131A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY