C-414 NORMAL CHECKLIST
CESSNA 414 · Pilot's Operating Handbook
Overview
This document is a checklist for the Cessna 414, providing pilots with a structured sequence of tasks to perform during various phases of flight operations. It includes preflight checks, engine start procedures, takeoff preparations, and post-flight actions. The checklist is designed to ensure safety and compliance with operational standards, making it an essential tool for pilots operating this aircraft. The document emphasizes critical parameters such as fuel management, engine performance, and weight and balance considerations, which are vital for safe flight operations.
- Oil pressure should reach 25 PSI within 30 seconds after engine start.
- Minimum takeoff oil temperature must be 75°F.
- Vx (best angle of climb) is 88 KTS; Vy (best rate of climb) is 112 KTS.
- Maximum takeoff weight is 7087 lbs; maximum zero fuel weight is 6515 lbs.
- Ensure all flight controls are checked and secured before takeoff.
Document
Source
Originally published by www.tomgorski.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 2016
- Pages
- 2
- File size
- 19 KB
- Publisher
- www.tomgorski.com
Specifications & performance
Extracted from this document.
Specifications
- Engine model
- Continental TSIO 520-NB
- Fuel capacity (gal)
- 206
- Max takeoff weight (lb)
- 7,087
V-speeds
- VA
- 151
- VR
- 88
- VX
- 88
- VY
- 112
- VFE
- 140
- VS1
- 98
Weight & balance
- Cg range (in)
- 155.5
- Max landing weight (lb)
- 6,750
- Max takeoff weight (lb)
- 7,087
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In this document
Preflight Inspection
The preflight inspection section includes checks for fuel and oil quantity, maintenance status, and passenger briefing completion. It emphasizes the importance of ensuring that all surfaces are clear and that the aircraft is properly chocked.
Engine Start Procedures
This section outlines the steps for starting the engines, including checking oil pressure and engine indicators. It specifies that oil pressure should reach 25 PSI within 30 seconds of starting the engines.
Before Takeoff
Before takeoff, pilots must complete a series of checks including setting the parking brake, verifying fuel selectors, and ensuring that all flight controls are operational. The checklist also includes a takeoff briefing and confirms that the minimum takeoff oil temperature is 75°F.
Takeoff Procedures
During takeoff, the checklist instructs pilots to set the power, check fuel flow and engine instruments, and ensure that the gear is up. It also specifies airspeeds for safe operation, including Vx at 88 KTS and Vy at 112 KTS.
Weight and Balance
The weight and balance section provides critical data for safe operations, including maximum takeoff weight of 7087 lbs and maximum zero fuel weight of 6515 lbs. It also lists various weight limits for different compartments and seating arrangements.
Safety notes
- Always perform a thorough preflight inspection to ensure aircraft readiness.
- Monitor engine instruments closely during startup and takeoff phases.
- Confirm that all doors and windows are locked before flight.
Full document text
C:\Data\Hwyc01c\asr\Checklist_C414.doc 4/28/2016 C-414 NORMAL CHECKLIST 1. Fuel and Oil Quantity...........…..…...CHECKED 2. Surfaces and Chocks..……….….…CHECKED 3. Maintenance Status....…….…...….CHECKED 4. Passenger Briefing....………..…COMPLETED 5. Weight and Balance……….…...COMPLETED 1. Parking Brake………………………………SET 2. Prefllight…..……………………...COMPLETED 3. Cabin Door………...LATCHED AND SECURE 4. Seat, Belts and Harnesses….….…SECURED 5. Emergency Crossfeed Shutoff...………OPEN 6. Fuel Selectors ….…….…..........MAIN TANKS 7. Cowl Flaps……………….……..……….OPEN 8. Yaw Damper…………….…………………OFF 9. Mixtures………………….…..……FULL RICH 10. Props………………………….……HIGH RPM 11. Throttles1/2" …………………….………OPEN 12. Synchrophaser………………….…………OFF 13. Flight Controls…………………..…….CHECK 14. Switches & Circuit Breakers…….……….SET 15. Magneto Switches………………….…..….ON 16. Battery and Alternator Switches….………ON 17. Fuel Quantity Gauges ………..…….…CHECK 18. Gear Switch and Position Lights …..CHECK 19. Prop and Blast Areas…………………CLEAR 20. Exterior Lights……………..…AS REQUIRED ----------CLEARED FOR START---------- 1. Engines……………………..………..….START 2. Oil Pressure…….…25 PSI within 30 Seconds 3. Engine Indicators….……………………CHECK 4. Vacuum Gage………….……………….CHECK 1. Aux. Fuel Pumps….…….…………………OFF 2. Warm Up……………………… 900-1000 RPM 3. Avionics………….…….…………………….ON 4. Exterior Lights………...……….AS REQUIRED 5. Air Circulator/Heater.….………AS REQUIRED 6. Interior Lights………….………AS REQUIRED 7. Accessory Switches……..…...…………….ON 8. Mixtures………………………..……………SET 9. Radios…………………….…..…………….SET 10. Brakes…………………….……………..CHECK 11. Instruments……………………………..CHECK 12. Altimeters/ASA……………………………..SET 1. Parking Brake……………..……………….SET 2. Autopilot…………….….……………….CHECK 3. Electric Trim………….….….………….CHECK 4. Fuel Quantity…………….….…..……..CHECK 5. Fuel Selectors…………….…….MAIN TANKS 6. Cowl Flaps……………………………….OPEN 7. Flaps………………………………………….UP 8. Trim………………………SET FOR TAKEOFF 9. Avionics and Radios………………………SET 10. Flight Instruments…………………………SET 11. Alternate Air and Ram Dump……………… IN 12. Pressurization Controls……..….…………SET 13. Mixture………………………RICH or as Req'd 14. Throttles……………………………..1700 RPM 15. L&R Hyd Flow Lights…………………..…OFF 16. Vacuum System………………….……CHECK 17. Annunciator Panel……….…….………CHECK 18. Alternators and Battery Meter…..……CHECK 19. Props……….…………FEATHERING CHECK 20. Magnetos…….….……………………..CHECK 21. Engine Instruments……………………CHECK 22. Throttles……….….………….IDLE 1000 RPM 23. Doors and Windows…………………LOCKED 24. Spoilers (if installed)…………...RETRACTED 25. Takeoff Briefing……….…….……REVIEWED 26. Parking Brake…………..…………………OFF 27. Minimum Takeoff Oil Temp.………………75F ----------CLEARED FOR TAKEOFF---------- 1. Wing Flaps……………..……………………UP 2. Transponder……………………………ON ALT 3. Air Conditioner……….RECIRCULATE or OFF 4. Boost Pumps………..….…..……………..LOW 5. Lights………………….....…… AS REQUIRED 6. Anti-Ice…….…………....……..AS REQUIRED 7. Takeoff Time…………….….……DOCUMENT 8. Power……………………………………….SET 9. Fuel Flow & Engine Instruments....CHECKED Vx……….88 Vy………….112 1. Gear…………………………………………UP 2. Yaw Damper………………..……………….ON 3. Taxi Lights……………….………………….OFF 4. Heater or Air Conditioner……..AS REQUIRED 5. Climb Power…………………………………SET 6. Mixtures……………………….…………CHECK 7. Engine Instruments………….……….…CHECK 8. Pressurization……………….…………..CHECK SAFETY AND INSPECTION BEFORE STARTING ENGINES AFTER START / TAXI BEFORE TAKEOFF AFTER TAKEOFF / CLIMB C:\Data\Hwyc01c\asr\Checklist_C414.doc 4/28/2016 1. Cruise Power…………….…….……….SET 2. Cowl Flaps……..……..……AS REQUIRED 3. Props…………………………….……….SET 4. Mixture……………….….………..……..SET 5. Cabin Altitude and Differential……CHECK 6. Recognition Lights (if installed)…...….OFF 1. Approach Briefing…………….COMPLETE 2. Fuel Selectors…………………….…..MAIN 3. Pressurization…………….….…………SET 4. Altimeters…………………….……….…SET 5. Power………………….……….….…….SET 6. Anti-Ice…………………….AS REQUIRED 7. Mixtures……………………………ADJUST 8. Seat Belts and Shoulder Harnesses….ON 9. Seat Backs……………..…….….UPRIGHT 10. Tables…..………………..……….STOWED 11. Lights…….………………….AS REQUIRED 12. Cowl Flaps…………………..……..CLOSED 1. Heater………………..…COMBUSTION OFF 2. Lights …………….….……….AS REQUIRED 3. Boost Pumps……………….……..……..LOW 4. Prop Sync…………………………..……..OFF 5. Gear…………………………..….……..DOWN 6. Mixtures………………..…………….ADJUST 7. Auto-Pilot ..…….………………………….OFF 8. Flaps………………..……..…AS REQUIRED 9. Yaw Damper …….………....……………OFF 10. Props……….……..………………………SET 1. Cowl Flaps…………….……………….OPEN 2. Flaps…………………..……………………UP 3. Trim Tab……………....………SET TO ZERO 4. Transponder………...……….…….STANDBY 5. Air Circulation….…………….AS REQUIRED 6. Boost Pumps……….….…………………OFF 7. Lights………………….……..AS REQUIRED 1. Flight Time……..……………....DOCUMENT 2. Accessory Switches/Air Circulators…...OFF 3. Mixtures…………..….………IDLE CUT OFF 4. Magneto Switches.………………….……OFF 5. Battery and Alternators….…..…………..OFF 6. Emergency Crossfeed Shutoff……CLOSED 7. Wheel Chocks……………..……INSTALLED AIRSPEEDS FOR SAFE OPERATION Vmca………………………………………72 KTS VX………………………………………….88 KTS VssE……………………………………....98 KTS VxSE……………………………………..100 KTS VySE……………………………………..112 KTS Vy…………………………………………110 KTS Va……………………………………..….151 KTS Vlo & vle..……………………………..…178 KTS Vfe…………….…15 = 171…...….45 = 140 KTS ENGINES Continental TSIO 520-NB Oil Capacity 12 Quarts Useable Fuel 206 Gallons Battery 24V Mains 70 psi Nose 35 psi Max Diff 5.3 psi WEIGHT & BALANCE ARM DATA Avionics Bay 200 MAX…………..……….32 Nose Bags 325 MAX……………..……….71 Front Seats…………………….….……...137 Aft Facing Seats……………...…...…..…178 Wing Lockers 400 MAX……….….……..186 Back Row Seats…………..….…...…..…218 Lav Seat………………………….……….250 Rear Bags A 400 MAX……….….………266 Rear Bags B 100 MAX……….….………282 Fuel 1236 Max..…………………..…….165.2 CG Limits 155.5 to 160.04 at Full Weight See AFM for Lighter Weight Operations TAKEOFF WT 7087 MAX ZERO FUEL WT 6515 MAX LANDING WT 6750 CRUISE DESCENT / APPROACH BEFORE LANDING AFTER LANDING SHUTDOWN
What's in the CESSNA 414 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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