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
08 GO-AROUND
The go-around procedure has to be initiated when the approach has to be abandoned.
Go-Around requirements:
– Quick and correct power application.
– Stopping of sink rate by proper rotation.
– Speed at least 90-85 kts during the procedure.
If go-around is initiated :
above 500 ft HAA select CLIMB power (32,5”MAP/2325 RPM)
between 200-500 ft HAA select METO power (41” MAP/2550 RPM)
below 200 ft HAA select T/O power (48” MAP/2700 RPM)
Go-around two engines:
PF PNF
• Call: 'GO-AROUND, SET
POWER’
• Rotate to nose up attitude.
• Command when positive rate:
“GEAR UP”
• Set power and
state: ‘POWER SET’
• Monitor procedure and
rotation.
• Repeat, select confirm
Continue as for Normal Take-off, refer to Part B 2.2.1
Note:- When an engine fails during a go-around maintain a speed of 87 kts IAS
Proceed as for ‘engine failure/fire during take-off after V1’
09 WAVE-OFF
The wave-off procedure (rejected landing) is similar to the go-around procedure for two
engines except that the maneuver begins with the power levers near or at flight idle and at
altitudes below 50 ft.
Pay special attention to the following aspects:
– Initially rotate only to stop the descent.
– During power application devote full attention to pitch attitude control.
– Do not rotate to a climb attitude until the speed is a minimum of 85 kts
– Touching of the main wheels on the runway must be expected as it takes
– a few seconds for the engines to deliver take-off power.
Notes: The trim change on applying take-off power is significant but the stick force can be
held with one hand.
A rapid opening of the power levers create initially a tendency for the propellers to
fine-off with the associated drag
A wave-off during single engine operation is not possible.
1. ENGINE FIRE/FAILURE BEFORE V
1
Reject the take-off.
Rev No: 00 Stichting Catalina PH-PBY
Page: 18 18 May, 2004