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 2 Part B
ENGINE FAILURE/FIRE DURING TAKE-OFF AFTER V1
FLIGHT
PHASE/EVENT
PF PNF
Engine fire/failure
•
• Apply ailerons towards live engine to
ensure wings level.
• State nature of failure.
At Vr
• Rotate smoothly to appropriate attitude
Airborne positive
climb
• Call: 'GEAR UP'
• In case of right hand
engine failure/fire, switch
on aux. Hydraulic pump
• Repeat, select, confirm
In case of engine
failure/fire
• Call: 'TAKE ACTION
• Perform memory items.
Identify engine not below
200 ft
Initial climb.
• Maintain speed, minimum V2
• Monitor speed/attitude.
•
• Call: “SET METO POWER”
Call: “MEMORY
ITEMS
COMPLETED”
• Repeat, select, confirm
When appropriate
• Call: ’EMERGENCY CHECKLIST’
• Call: ’AFTER TAKE-OFF
CHECKLIST’
• Repeat, perform, confirm
• Repeat, perform, confirm
Notes:- For, emergency/abnormal operation, crew coordination refer to AOM2.3.1./0
General
ATC shall be informed as soon as practicable by MAYDAY or PANPAN call.
Inform ATC when deviating from the published departure.
During climb limit bank angle to 15°.
Minimum turning height is 100 ft HAA, refer to AOM 2.3.3/6.
During turn below 400 ft maintain V2.
Preferably make turns towards the live engine.
When landing conditions are below minima, climb to a minimum safe altitude
andproceed to the nearest suitable airport.
Rev No: 00 Stichting Catalina PH-PBY
Page: 20 18 May, 2004