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 Part B
3.1 GENERAL
01 EMERGENCY/ABNORMAL OPERATION
Procedure priorities are:
1) Fly Aircraft
2) Memory items
3) Emergency checklist
4) Normal checklist
5) Part B
6) Inform ATC and Passengers
02 CREW CO-ORDINATION PROCEDURE:
Either pilot announces the applicable emergency/abnormal condition.
The PF commands 'TAKE ACTION' .If the applicable procedure contains memory
items:Both pilots perform their respective memory items, and confirm completion by calling
‘MEMORY ITEMS COMPLETED’.If the applicable procedure contains no memory items:
The PNF calls ‘NO MEMORY ITEMS’.
The PF commands ‘EMERGENCY CHECKLIST, MY RT’ The PNF performs the
Emergency Checklist, and confirms completion by calling‘EMERGENCY CHECKLIST
COMPLETED’
Commands to initiate the On Ground Emergency/Evacuation procedure will be given by
the captain.
03 ENGINE FEATHERING PROCEDURE:
After an engine failure/fire or engine shutdown the engine must be feathered according the
following crew coordination procedure based on ’dead foot, dead engine’:
In case of an engine failure after T/O the engine failure Checklist will not be initiated below
400 ft AGL
04 EMERGENCY AIRSPEEDS <28000 IBS
All speeds listed are IAS
Air Minimum Control Speed (Vmca)
Single Engine Best Rate of Climb (Vy)
Single Engine Best Angle of Climb (Vx)
Single Engine En-Route Climb
Single Engine Cruise Speed
Single Engine Landing Base Leg
Single Engine Final Approach
Minimum Speed for Unfeathering
Glide Speed for Range
Emergency Descent
85 Kts
87 Kts
87 Kts
87 Kts
87 Kts
90 Kts
85 Kts
90 Kts
90 Kts
30 Kts
Rev No: 00 Stichting Catalina PH-PBY
Page: 4 18 May, 2004