SCHWEIZER 269C-1 STARTUP/SHUTDOWN
SCHWEIZER 269C · Checklist
Overview
This document is a checklist for the Schweizer 269C helicopter, detailing the startup and shutdown procedures. It includes safety checks, operational steps, and post-flight requirements to ensure safe operation of the aircraft.
- Ensure all controls are free and secure before startup.
- Check fuel quantity and caution lights before engine start.
- Do not exceed 1600 RPM with rotor disengaged.
- Monitor oil pressure and temperature during engine operation.
- Perform a thorough cockpit check before starting the engine.
- Shutdown procedures include securing the aircraft and notifying maintenance of any issues.
- Always have a clear area before engaging the starter.
- Follow post-flight requirements for safety.
Document
Source
Originally published by etlaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 55 KB
- Publisher ·
- etlaviation.com
- Language ·
- en
What is the SCHWEIZER 269C-1 STARTUP/SHUTDOWN?
The SCHWEIZER 269C-1 STARTUP/SHUTDOWN is a checklist for the SCHWEIZER 269C.
Where does the SCHWEIZER 269C-1 STARTUP/SHUTDOWN come from?
This copy of the SCHWEIZER 269C-1 STARTUP/SHUTDOWN was originally published by etlaviation.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the SCHWEIZER 269C.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More SCHWEIZER 269Cmanuals & documents
In this document
Startup Procedures
Includes checks for tail rotor pedals, seat belts, control frictions, and various switches before starting the engine.
Starting Engine
Details the steps to engage the rotor and monitor engine RPM and oil pressure during startup.
Engine Ground Run
Outlines the procedure for running the engine at 2000 RPM for a minimum of 2 minutes and checking various parameters.
Engine Shutdown
Describes the steps to safely shut down the engine and secure the aircraft.
Post Flight Requirements
Emphasizes the importance of briefing passengers on exit safety and servicing the aircraft as needed.
Safety notes
- Do not exceed 1600 RPM with rotor disengaged.
- Do not add throttle during rotor engagement.
- Ensure area is clear before engaging starter.
- Monitor oil pressure minimum of 25 PSI within 30 seconds after startup.
- Confirm throttle needle split before closing throttle.
Full document text
SCHWEIZER 269C-1 STARTUP/SHUTDOWN Tail Rotor Pedals: ADJUST/SECURE Seat Belts and Shoulder Harness: CHECK Collective Area: NO OBSTRUCTIONS Control Frictions: RELEASE Controls: FREE Control Frictions: ON Altimeter: SET All Switches: OFF (beacon may remain on) Circuit Breakers: IN Throttle: CLOSED Mixture: IDLE CUTOFF (pull/out) Battery Switch: ON Fuel Quantity: CHECK Low Voltage Caution Light: ON Low Fuel Caution Light: OFF (press-to-test) Transmission Warning Light: ON Tail Rotor Chip Detector Light: OFF (press-to-test) Clutch Control Switch: RELEASE (down) Clutch Light: ON (disengaged) COCKPIT CHECK Fuel Valve: OPEN (push/in) Throttle Friction: ADJUST Carb Heat: OFF Prime: AS NEEDED Primer: DOWN and LOCKED Magneto Switch: BOTH Mixture: FULL RICH (push/in) Beacon: ON Position Lights: AS NEEDED Throttle: CLOSED Area: CLEAR Starter: ENGAGE (disengage when engine starts) CAUTION: Do not exceed 1600 RPM with rotor disengaged. RPM: 1400 RPM Oil Pressure: MINIMUM 25 PSI (within 30 secs or shut down) Alternator: ON Avionics Master: ON Instrument Master: ON STARTING ENGINE Collective: DOWN and FRICTION ON Pedals: NEUTRAL Cyclic: CENTERED and FRICTION ON Area: CLEAR Engine RPM: 1500 Rotor: ENGAGE (1500-1600 RPM) Clutch Control Switch: ENGAGE CAUTION: Do not add throttle during rotor engagement. Clutch Light: OFF (engaged) Clutch Guard: CLOSED ROTOR ENGAGEMENT Engine Speed: 2000 RPM Engine Oil Pressure: CHECK Engine Oil Temperature: CHECK All Warning/Caution Lights: OFF Ammeter: CHECK Radio: SET Transponder: 1200 (sby/alt/grd) Collective Friction: RELEASE Collective: 15 inches MP and 2000 RPM Magneto: CHECK (125 max drop allowable within 5 seconds Carb Heat: CHECK Collective: FULL DOWN/2000 RPM Throttle: CLOSE (confirm needle split) Throttle Override: CHECK (do not raise collective) RPM: 2000 Cyclic Friction: RELEASE Cyclic Trim: SET Tip Path Plane: CHECK VNE: NOTE ENGINE GROUND RUN Collective: DOWN and FRICTION ON Cyclic: NEUTRAL and FRICTION ON Engine RPM: 2000 for 2 Minutes MIN and CHT < 300 Throttle: CLOSE Clutch: RELEASE (down) Mixture: IDLE CUTOFF (pull/out) Magnetos: OFF (after engine stops) Alternator: OFF Switches: OFF (except battery and beacon) Battery: OFF (after clutch is fully disengaged) ENGINE SHUTDOWN • Brief PAX on exit safety. • Shutdown in accordance with procedures • Service aircraft as required. • Notify maintenance of discrepancies. • Secure aircraft as required. POST FLIGHT REQUIREMENTS Have a Safe Flight!