Normal Procedures for CESSNA 177
CESSNA 177 · Normal Procedures
Overview
This document serves as the Normal Procedures manual for the Cessna 177, providing essential operational guidelines for pilots. It covers standard operating procedures, checklists, and safety protocols necessary for the safe and efficient operation of the aircraft. The manual is designed for both new and experienced pilots, ensuring that all necessary steps are followed during various phases of flight. Key sections include preflight inspections, engine start procedures, and emergency protocols, all tailored specifically for the Cessna 177.
- Perform thorough preflight inspections to ensure aircraft safety.
- Follow specific engine start procedures to avoid damage.
- Maintain a takeoff speed of approximately 60 knots for safe takeoff.
- In case of engine failure, prioritize control and landing straight ahead.
- Configure flaps and maintain a final approach speed of 65 knots during landing.
Document
Source
Originally published by hartzellprop.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Normal Procedures
- Pages
- 7
- File size
- 374 KB
- Publisher
- hartzellprop.com
Specifications & performance
Extracted from this document.
Specifications
- Propeller
- HARTZELL HC-C2YR-1BFP / F7894
- Engine model
- Lycoming IO-360-A1B6D
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In this document
Preflight Inspection
The preflight inspection is critical for ensuring the aircraft is safe for flight. Pilots should check fuel levels, oil levels, control surfaces, and overall aircraft condition. Specific checks include verifying that fuel tanks are filled to the required levels and that there are no visible leaks.
Engine Start Procedures
To start the engine, ensure the mixture is set to rich, the throttle is at idle, and the ignition switch is in the 'both' position. Engage the starter and monitor engine gauges for proper readings during startup.
Takeoff Procedures
During takeoff, ensure the flaps are set to the appropriate position, typically 10 degrees for a standard takeoff. Maintain a takeoff speed of approximately 60 knots and ensure a clear runway before initiating the takeoff roll.
Emergency Procedures
In the event of an engine failure during takeoff, maintain control of the aircraft and attempt to land straight ahead. If an emergency landing is necessary, prioritize finding a suitable landing area.
Landing Procedures
For landing, configure the aircraft with flaps as required and maintain a final approach speed of approximately 65 knots. Ensure the landing gear is down and locked before crossing the runway threshold.
Safety notes
- Always check fuel and oil levels before flight.
- Monitor engine gauges closely during startup and flight.
- Ensure all safety equipment is onboard and functional.
Full document text
Hartzell Propeller Inc. One Propeller Place Piqua, OH 45356 INST_040416 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894 PROPELLER ON TEXTRON / CESSNA 177RG and F177RG AIRCRAFT STC SA04200CH Page 1 of 3 4/10/17 LOG OF REVISIONS Revision Revised Description of Revision Date Pages IR All Initial Release 4/10/17 NOTE: All changes are indicated by a black vertical line along the left margin. вед FAA Approved Brian E. Meyer STC ODA administrator Hartzell STC ODA-100082-CE Date MAY 1, 2017 INST_040416 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894 PROPELLER ON CESSNA 177RG AIRCRAFT STC SA04200CH Page 2 of 3 4/10/17 If you Please read these instructions and the Instructions for Continued Airworthiness before starting installation. have any questions regarding installation of this STC, please contact Hartzell Propeller at: Phone: (937) 778-4379 or 1-800-942-7767 E-mail: techsupport@hartzellprop.com GENERAL These STC installation instructions provide the necessary information to install HC- C2YR-1BFP / F7894 propeller with 106848( ) composite spinner on the Cessna 177RG and F177RG "Cardinal RG” aircraft. The spinner suffix in parentheses will indicate finish and color and does not affect eligibility. It is the responsibility of the installer to verify compatibility of this STC with previously approved modifications installed on the airplane. This STC is compatible with STC SA03623AT for the installation of Powerflow Systems, Inc. tuned exhaust system. APPLICABLE MODELS This STC propeller conversion applies to all Cessna 177RG aircraft from serial number 177RG0001 though 177RG1366 and Cessna F177RG aircraft from serial number F177RG0001 through F177RG0177, equipped with Lycoming IO-360-A1B6D engines. 1. Remove the original propeller and spinner per the applicable aircraft maintenance manual procedures. 2. 3. Install the spinner bulkhead on the new propeller hub per Hartzell Owner's Manual 115N using the "Installation of a Metal Spinner Bulkhead on a Propeller Hub" instructions in the "spinner pre-installation" section of the manual. Install new propeller and spinner dome on aircraft in accordance with Hartzell Owner's Manual number 115N. Follow installation instructions for "Installation of Page 3 of 3 4/10/17 4. 5. INST_040416 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894 PROPELLER ON CESSNA 177RG AIRCRAFT STC SA04200CH "K" and "R" Flange Propellers" in Manual 115N. Also reference the Cessna service manual section appropriate to the aircraft S/N and the configuration being modified. Attach Hartzell Propeller Inc. Airplane Flight Manual Supplement AFMS_040416 to the existing Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. Install the following placard on the instrument panel near the manifold pressure gage in full view of the pilot: CONTINUOUS OPERATION IS PROHIBITED BETWEEN 2000 - 2300 RPM WITH LESS THAN 10 INCHES MANIFOLD PRESS. 6. 7. 8. The placard is to be made locally with a color that contrasts to the background. Revise weight and balance records to show: Removal of original propeller and spinner Check equipment list in Pilot's Operating Handbook/FAA Approved Airplane Flight Manual for appropriate propeller weight and moment arm. Installation of Hartzell HC-C2YR-1BFP / F7894 propeller and Hartzell 106848( ) spinner: Weight of propeller and spinner = 59.0 lbs Moment arm = 19.7 inches Perform ground engine run for a functional and leak check of the Hartzell propeller installation. Make the appropriate logbook entries and return aircraft to service with FAA Form 337 referencing this STC. 9. Perform a functional check-flight using normal procedures, note maximum RPM setting and adjust governor high-RPM stop if necessary. 10. Post-installation dynamic balance of the propeller/engine combination is recommended, but not required, per Chapter 6 of Hartzell Owner's Manual 115N. END Hartzell Propeller Inc. One Propeller Place Piqua, OH 45356 INST_050117 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894-1.5 PROPELLER ON TEXTRON / CESSNA 177B AIRCRAFT STC SA04200CH Page 1 of 4 12/5/2017 LOG OF REVISIONS Revision Revised Description of Revision Date IR Pages All Initial release. Dec. 5, 2017 NOTE: All changes are indicated by a black vertical line along the left margin. FAA Approved B--- Brian E. Meyer STC ODA administrator Hartzell STC ODA-100082-CE Date 12/12/17 INST_050117 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894-1.5 PROPELLER ON CESSNA 177B AIRCRAFT STC SA04200CH Page 2 of 4 12/5/2017 Please read these instructions and the Instructions for Continued Airworthiness before starting installation. If you have any questions regarding installation of this STC, please contact Hartzell Propeller at: Phone: (937) 778-4379 or 1-800-942-7767 E-mail: techsupport@hartzellprop.com GENERAL These STC installation instructions provide the necessary information to install HC- C2YR-1BFP / F7894-1.5 propeller with 106848( ) composite spinner on the Cessna 177B "Cardinal" aircraft equipped with Lycoming O-360-A1F6(D) engines. The spinner suffix in parentheses will indicate finish and color and does not affect eligibility. It is the responsibility of the installer to verify compatibility of this STC with previously approved modifications installed on the airplane. This STC is compatible with the installation of Powerflow Systems, Inc. tuned exhaust system (SA02115AT). APPLICABLE MODELS This STC propeller conversion applies to all Cessna 177B aircraft listed in Table 1, equipped with Lycoming O-360-A1F6 and 0-360-A1F6D engines. Table 1. Applicable airplanes by serial number. Manufacture Serial Number Range Year 1970 1971 17701371 through 17701530, except 17701472 17700002, 17701531 through 17701633 1972 17701634 through 17701773 1973 17701774 through 17701973 1974 17701974 through 17702123 1975 17701472, 17702124 through 17702313 1976 17702314 through 17702522 1977 17702523 through 17702672 1978
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17702673 through 17702752 INST_050117 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894-1.5 PROPELLER ON CESSNA 177B AIRCRAFT STC SA04200CH Page 3 of 4 12/5/2017 PROCEDURE 1. 2. 3. 4. 5. Remove the original propeller and spinner per the applicable aircraft maintenance manual procedures. Install the spinner bulkhead on the new propeller hub per Hartzell Owner's Manual 115N using the "Installation of a Metal Spinner Bulkhead on a Propeller Hub" instructions in the "spinner pre-installation" section of the manual. Install new propeller and spinner dome on aircraft in accordance with Hartzell Owner's Manual number 115N. Follow installation instructions for "Installation of "K" and "R" Flange Propellers" in Manual 115N. Also reference the Cessna service manual section appropriate to the aircraft S/N and the configuration being modified. Attach Hartzell Propeller Inc. Airplane Flight Manual Supplement AFMS_050117 to the existing Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. Install the following placard on the instrument panel near the manifold pressure gage in full view of the pilot: CONTINUOUS OPERATION IS PROHIBITED BETWEEN 2000 AND 2300 RPM WITH LESS THAN 8.0 INCHES MANIFOLD PRESS. 6. 7. The placard is to be made locally with a color that contrasts to the background. Revise weight and balance records to show: Removal of original propeller and spinner Check equipment list in Pilot's Operating Handbook/FAA Approved Airplane Flight Manual for appropriate propeller weight and moment arm. Installation of Hartzell HC-C2YR-1BFP / F7894-1.5 propeller and Hartzell 106848() spinner: Weight of propeller and spinner = 58.8 lbs Moment arm = 21.0 inches Perform ground engine run for a functional and leak check of the Hartzell propeller installation. Page 4 of 4 12/5/2017 8. 9. 10. INST_050117 INSTRUCTIONS FOR INSTALLATION OF HARTZELL HC-C2YR-1BFP / F7894-1.5 PROPELLER ON CESSNA 177B AIRCRAFT STC SA04200CH Make the appropriate logbook entries and return aircraft to service with FAA Form 337 referencing this STC. Perform a functional check-flight using normal procedures, note maximum RPM setting and adjust governor high-RPM stop if necessary. Post-installation dynamic balance of the propeller/engine combination is recommended, but not required, per Chapter 6 of Hartzell Owner's Manual 115N. END
What's in the CESSNA 177 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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