User manual
Table Of Contents
- PBY Catalina
- Introduction
- System requirements
- Credits
- Copyrights
- Contact support
- Models and versions
- Limitations
- Failure model and special features
- Aerosoft Sound Control
- Flight model
- Using the switches and knobs
- Interactive Checklist
- Avionics, 1940’s military cockpit
- Avionics, modern cockpit
- Engine Settings
- Mission
- Appendix A: Simplified checklist
- Appendix B: KX 165A TSO
- Appendix C: KLN-90B User Manual
- INTRODUCTION
- OVERVIEW
- DEFINITIONS:
- SYSTEM USE
- NAV: NAVIGATION PAGES
- CALC: CALCULATOR PAGES
- STAT: STATUS PAGES
- SETUP: SETUP PAGES
- OTHER: OTHER PAGES
- TRIP: TRIP PLANNING PAGES
- MOD: MODE PAGES
- FPL: FLIGHT PLAN PAGE
- NAV: NAVIGATION PAGES (right screen)
- APT: AIRPORT PAGES
- NEAREST Airport Pages
- VOR: VOR Page
- NDB: NDB Page
- INT: INTERSECTION PAGE
- SUPL: SUPPLEMENTAL PAGE (SUP)
- CTR: CENTER WAYPOINT PAGE
- REF: REFERENCE WAYPOINT PAGE
- ACTV: ACTIVE WAYPOINT PAGE (ACT)
- D/T: DISTANCE/TIME PAGES
- MESSAGE PAGE
- DIRECT-TO PAGE
Section 12.27 Part B
steady whilst taxiing to prevent such damage. This is the responsibility of the non-flying
pilot.
External locks may also be fitted if aircraft is to be left outdoors in stormy conditions. With
external locks fitted it is impossible to release the Flight Station Control Locks
08 TRIM TABS
All control surfaces have metal trim tabs, which are adjustable by the Pilots.
The elevator and rudder controls are overhead in the Flight Station while the aileron
control is located to the left of centre below the instrument panel.
Trim tab control runs must be checked for full travel as part of the Pre Start checklist.
09 CONTROL SURFACE RANGE OF MOVEMENT
1 Rudder Right
Rudder Left
17 Deg
17 Deg
2 Elevator Up
Elevator Down
30 Deg
20 Deg
3 Aileron Up
Aileron Down
21 Deg
19.75Deg
4 Rudder Trim Tab Right
Rudder Trim Tab Left
15 Deg
20 Deg
5 Elevator Trim Tab Up
Elevator Trim Tab Left
5 Deg
5 De9
6 Aileron Trim Tab Up
Aileron Trim Tab Down
16 Deg
16 Deg
Rev No: 00 Stichting Catalina PH-PBY
Page: 2 18 May, 2004