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STANDARDIZATION MANUAL and AMPLIFIED PROCEDURES CESSNA 152

Cessna 152 · Systems Description

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Overview

This Standardization Manual serves as a comprehensive reference for the Cessna 152, specifically designed for training purposes at Lake Elmo Aero. It encompasses a wide range of topics including aircraft systems, performance data, and procedural guidelines for various flight maneuvers. The manual is not a substitute for the Pilot's Operating Handbook (POH) or FAA publications but aims to enhance understanding and proficiency in operating the Cessna 152. Key sections include V-speeds, takeoff and landing data, weight and balance information, and emergency procedures, all tailored to the Cessna 152's specifications. This document is particularly useful for both private and commercial pilot training, ensuring that pilots are well-versed in the aircraft's operational standards and safety protocols.

  • The Cessna 152 is equipped with a Lycoming O-235-L2C engine producing 110 HP.
  • Usable fuel capacity is 24.5 gallons (or 37.5 gallons for long-range models).
  • Standard V-speeds are critical for safe operation during various phases of flight.

Document

Source

Originally published by www.lakeelmoaero.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Systems Description
Year
2021
Pages
55
File size
2.7 MB
Publisher
www.lakeelmoaero.com
How rare is it?
2,927Cessna 152 registered worldwide · 2,204 active

Common. One of the most common aircraft types we track.

Documentation completeness
6/7

Most owners only have the POH. Here's the essential set for the Cessna 152.

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In this document

V-Speeds

Vso: 35 KIAS (Stall speed, full landing configuration) VS1: 40 KIAS (Stall speed, clean configuration) Vx: 55 KIAS (Best angle-of-climb speed) Vy: 67 KIAS (Best rate-of-climb speed) Vg: 60 KIAS (Best glide speed) Vfe: 85 KIAS (Maximum flap extension speed) Va: 104 KIAS (Maneuvering speed) Vno: 111 KIAS (Maximum structural cruising speed) Vne: 149 KIAS (Never-exceed speed)

Safety notes

  • Always refer to the Pilot's Operating Handbook for specific operational procedures.
  • Ensure all external lights are operational during flight to enhance visibility and compliance with regulations.

Full document text

STANDARDIZATION MANUAL and AMPLIFIED PROCEDURES LAKE ELMO AERO CESSNA 152 Revised July 2021 Table of Contents GENERAL INFORMATION. Revision History. QUICK REFERENCE GUIDE. V-Speeds...... Takeoff Data Cruise Data Landing Data........ Weight and Balance Information SYSTEMS INFORMATION Engine..... Fuel System....... Electrical System......... External Lights Audio Control Panel... COMMON TASKS Traffic Pattern Arrival Traffic Pattern Departure. Traffic Pattern Quick Reference. Clearing Turns........... Configuring the Aircraft for Maneuvers. TAKEOFFS AND LANDINGS Normal Takeoff and Climb.. Crosswind Takeoff and Climb. Short Field Takeoff Soft Field Takeoff....... Normal Approach and Landing ...... Crosswind Approach and Landing. Short Field Approach and Landing. Soft Field Approach and Landing.. Go-Around/Balked Landing. PERFORMANCE MANEUVERS. Steep Turns... Lake Elmo Aero, LLC - July 2021 ..3 .4 4 4 4 4 4 .5 ..5 .5 6 ..7 .8 ..9 10 11 12 13 14 14 15 16 17 18 19 20 21 22 23 23 1 Slow Flight Power-On Stall. Power-Off Stall Secondary Stall Elevator Trim Stall Cross-Controlled Stall. Accelerated Stall......... Forward Slips Chandelles Lazy Eights GROUND REFERENCE MANEUVERS.. Rectangular Course Turns Around a Point.... S-Turns Across a Road Eights on Pylons............. Steep Spirals INSTRUMENT FLIGHT.. Recovery From Unusual Attitudes.... Instrument Approach Holding EMERGENCIES.. Engine Failure in Flight Engine Failure on Takeoff.. Power-Off Landing.. Engine Fire in Flight. Engine Fire on Start Electrical Fire Emergency Descent. Engine Roughness......... Loss of Oil Pressure.. High Oil Temperature.. Alternator Failure Electrical System Failure....... Spin Recovery 2 Lake Elmo Aero, LLC - July 2021 24 25 26 27 28 29 30 31 32 33 34 34 35 36 37 38 39 39 40 41 42 42 43 44 45 46 47 48 49 50 51 52 53 54 Lake Elmo Aero, LLC - July 2021 GENERAL INFORMATION This standardization manual is published to serve as a master reference document for expanded aircraft procedures during training. It does not replace the Pilot's Operating Handbook or any other document published by the manufacturer, nor does it replace the Airplane Flying Handbook or any other document published by the FAA. This manual is intended as a reference for training at all levels. As such, some maneuvers differentiate between requirements for Private and Commercial training. Ensure that you are studying, training and performing maneuvers to the applicable standards and procedures. References to "POH” indicate the aircraft Pilot's Operating Handbook for the 1978 C152 Pilot's Operating Handbook References to "AFH" indicate the Airplane Flying Handbook, FAA-H-8083-3B. References to "IPH" indicate the Instrument Procedures Handbook, FAA-H-8083-16B. With regards to emergencies, "Land as Soon as Practical" means that a return to the home base airport (21D) is recommended. "Land as Soon as Possible" means a landing at the nearest suitable airport or landing site is recommended, and return to the base airport should not be prioritized. This manual's reference airspeeds are in NAUTICAL MILES PER HOUR (KTS/KIAS). Revision History • 7/6/2021 Initial version published. 3 Lake Elmo Aero, LLC - July 2021 QUICK REFERENCE GUIDE V-Speeds 35 KIAS 40 KIAS Vso VS1 Vx 55 KIAS VY 67 KIAS VG 60 KIAS VFE 85 KIAS VA VNO VNE 104 KIAS 111 KIAS 149 KIAS Stall speed Full landing configuration Stall speed - Full clean configuration Best angle-of-climb speed Best rate-of-climb speed Best glide speed Maximum flap extension speed Maneuvering speed Maximum structural cruising speed Never-exceed speed Takeoff Data (Assumes no wind/ISA/max weight) Sea Level 2000' MSL 4000' MSL Ground Roll 725 feet 845 feet 1010 feet Total to Clear 50' Obstacle 1340 feet 1460 feet 1730 feet Cruise Data (Assumes ISA/leaned mixture) RPM %PWR KTAS GPH 2000' MSL 2400 75 101 6.1 2300 66 96 5.4 2200 59 91 4.8 4000' MSL 2400 71 101 5.7 2300 63 95 5.1 2200 56 90 4.6 6000' MSL 2500 69 116 6.1 2400 63 109 5.4 2300 57 103 4.9 Landing Data (Assumes no wind/ISA/max weight) Sea Level 2000' MSL Ground Roll 475 feet 495 feet Total to Clear 50' Obstacle 1200 feet 1245 feet 4000' MSL 535 feet 1300 feet Weight and Balance Information N68736 N69066 Basic Empty Weight 1185 lb 1182 lb Maximum Takeoff Weight 1670 lb 1670 lb Baggage Area Load Limit 120 lb Usable Fuel Capacity 37.5 gal Useful Load 485 lb 120 lb 24.5 gal 488 lb 4 Lake Elmo Aero, LLC - July 2021 SYSTEMS INFORMATION Engine Ref: POH 7-15 The Cessna 152 engine is a Lycoming O-235-L2C. It produces 110HP at full power, under sea level standard conditions (ISA). It burns 100LL Avgas and is serviced with Phillips XC 20W-50 oil. The O-235-L2C is a reciprocating (non-turbine), carbureted (not fuel injected), four-stroke, normally-aspirated (no forced induction system, such as a turbocharger), four-cylinder engine, with 235 cubic inches of displacement. The engine's ignition is supplied by a dual-redundant magneto system, which is fully independent and does not require electrical power to operate. Fuel System Ref: POH 7-19 The Cessna 152 has two fuel tanks, one in each wing. Each tank normally holds 13 gallons of 100LL fuel, for a total of 26 gallons. 1.5 gallons of fuel are unusable, for a total of 24.5 gallons of usable fuel. N68736 is equipped with a long-range fuel system, which holds a total fuel volume of 39 gallons. 37.5 gallons are usable. Fuel from each wing tank flows by gravity to a shutoff valve, then through the fuel strainer and into the carburetor. There are no auxiliary or electric fuel pumps installed in this system. FILLER CAP VENT LEFT FUEL TANK FUEL FUEL SHUTOFF VALVE 24.5 GALS ON TO CYLINDER INTAKE PORTS ENGINE PRIMER CODE FUEL SUPPLY VENT MECHANICAL LINKAGE OFF FUEL STRAINER CARBURETOR TO ENGINE CYLINDERS 5 VENTED FILLER CAP RIGHT FUEL TANK THROTTLE MIXTURE CONTROL KNOB Due to crossfeeding between fuel tanks, the tanks should be re- topped after each refueling to assure maximum capacity. Lake Elmo Aero, LLC - July 2021 Electrical System

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Ref: POH 7-23 The Cessna 152 is powered by a one-battery, one-alternator electrical system. The 24-volt battery is located on the firewall, on the instructor's side of the aircraft. The 28-volt alternator is located on the front of the engine, and is belt-driven by the crankshaft just aft of the spinner. This alternator is voltage-protected, and should automatically trip off in the event of excessive voltage. The electrical system is protected by circuit breakers, eliminating the need for spare fuses to be carried on board at night in accordance with FAR 91.205(c)(6). REGULATOR OVER- VOLTAGE SENSOR G CLOCK OIL PRESSURE SWITCH MASTER SWITCH OVER-VOLTAGE WARNING LIGHT TO FUEL QUANTITY INDICATORS ALTERNATOR FUEL IND ALTERNATOR FIELD CIRCUIT BREAKER TO FLASHING BEACON TO PITOT HEAT BCN PITOT STROBE LTS. ALT AMMETER STARTER FLIGHT HOUR RECORDER STARTER CONTACTOR H BATTERY BATTERY CONTACTOR B SC BAR LDG LTS. TO STROBE LIGHTS TO CIGAR LIGHTER (WITH FUSE AND CIRCUIT BREAKER) TO LANDING AND TAXI LIGHTS FLAP TO IGNITION SWITCH TO WING FLAP SYSTEM TO INSTRUMENT, RADIO, AND COMPASS LIGHTS TO OIL TEMPERATURE GAGE INST LTS TO TURN COORDINATOR NAV DOME TO AUDIO MUTING RELAY TO CONTROL WHEEL MAP LIGHT TO NAVIGATION LIGHTS TO DOME LIGHT ΤΟ WING TO RADIO FLAP CIRCUIT BREAKER RADIO L GROUND SERVICE TO RADIO RADIO 2 PLUG RECEPTACLE CODE CIRCUIT BREAKER (AUTO-RESET) CIRCUIT BREAKER (PUSH-TO-RESET) FUSE DIODE RESISTOR CAPACITOR (NOISE FILTER RADIO 3 IGNITION SWITCH MAGNETOS 6 TO RADIO OR TRANSPONDER AND ENCODING ALTIMETER TO RADIO RADIO 4 External Lights Lake Elmo Aero, LLC - July 2021 Navigation (Position) Lights Navigation Lights consist of one rear-facing white light on the rudder, one red light on the left wingtip, and one green light on the right wingtip. These should always be on any time the aircraft is electrically powered. Lake Elmo Aero checklists dictate that this switch should be left in the On position. Multiple aircraft in the Lake Elmo Aero fleet are equipped with a uAvionix SkyBeacon, which is a 1090MHZ ADS-B transmitter attached to one of the navigation lights. For this reason, navigation lights must remain powered on whenever the aircraft is in operation; failure could result in noncompliance with FAR 91.225(b) regarding ADS-B in required airspace. Beacon Light The Beacon Light is a red flashing light located on top of the vertical stabilizer. It should be turned on prior to engine start, and remain on until the engine is shut down. It is a commonly accepted practice in aviation that a flashing beacon indicates an aircraft with intent to start an engine, if it has not already. When operating or walking around a ramp or parking area, use appropriate vigilance and judgement. Landing Light The Landing Light is a forward-facing white light, angled to provide optimal visibility during a takeoff or an approach to landing. It should be turned on before to takeoff and landing, but can be turned off in flight at the pilot's discretion. In the absence of a taxi light being installed, the landing light can be turned on before taxi. Use caution when taxiing parallel to an active runway, and consider turning the landing light off if it could cause a hazard to arriving aircraft. NOTE: When operating in Lake Elmo Aero practice areas, leaving all external lights on during flight is recommended. 7 Lake Elmo Aero, LLC - July 2021 Audio Control Panel Not installed on all aircraft The aircraft's intercom and ATC audio are controlled through a Garmin GMA340 audio panel. Understanding this panel's functionality is crucial to situational awareness and safety. The double knobs on each side of the audio panel, titled PILOT and COPILOT, control the intercom volume and squelch. The inner (smaller) knob controls the intercom volume for the respective occupant; turn clockwise to increase intercom volume. Pulling the COPILOT volume knob out (away from the panel) will allow control of the rear seat intercom volume. The outer (larger) knob control controls the intercom squelch (microphone sensitivity) for the respective occupant. Turn this knob clockwise to increase the threshold of volume required to speak over the intercom; turn it counterclockwise to make the microphone more sensitive. If one pilot cannot be heard over the intercom, twist the respective squelch knob all the way counterclockwise to completely open the squelch (known as a "hot mic"). The receive select buttons, labeled COM1, COM2, and COM3, control which Com radios are able to be heard through the headsets. Multiple radios can be selected to receive simultaneously. The transmit select buttons, labeled COM1 MIC, COM2 MIC AND COM3 MIC, control which Com radio is being used to transmit. Only one of these can be selected to transmit at any given time. The Com Split button on the lower right, labeled COM 1/2, will allow the left seat pilot to transmit and receive on Com 1 only and the right seat pilot to transmit and receive on Com 2 only. Neither pilot will be able to hear the opposite radio until this button is deselected. This can be useful, for example, when an instructor wants to call flight service and provide a PIREP but not interrupt a student's communications on the main radio. The Speaker button on the lower right, labeled SPKR, sends all received audio from Com and Nav radios through the airplane's speaker. Not commonly used. The Intercom Isolation buttons on the lower right, labeled PILOT and CREW, allow ATC and intercom audio to be isolated to certain seats of the aircraft. In this mode, passengers are on their own intercom channel and can communicate with each other, but cannot hear ATC radios or communicate with the selected occupants (PILOT = left seat pilot, CREW = both front seats). Useful when flying with passengers in busy airspace and/or critical phases. GARMIN GMA 340 AOM MKR COM1 COM2 COM3 NAV1 NAV2 DME ADF TEST MUTE PILOT HI -- OFF LO COM1 COM2 COM3 MIC MIC MIC COM SPKR CABIN AUDIO 1/2 VOL SENS PA 8 PILOT ICS ISOLATION VOL PULL CREW PASS ΟΙ VOL COPILOT Lake Elmo Aero, LLC - July 2021 COMMON TASKS Traffic Pattern Arrival Ref: AFH Ch. 7, AC 90-66B Objective: To safely and efficiently arrive at an airport and perform traffic pattern operations. 1. Complete the Descent Checklist. 2. At least 10nm from the airport, attempt to determine the runway in use*. 3. At least 2nm from the runway, enter the traffic pattern at the published Traffic Pattern Altitude on a 45- degree entry to the downwind leg, maintaining a ½-mile distance from the runway once established. a. If approaching from the opposite side of the airport, overfly the airport at least 500' above Traffic Pattern Altitude. 4. Complete the Before Landing Checklist. The above procedure assumes an ideal traffic pattern situation. Other traffic, ATC, local traffic pattern restrictions, obstacles, etc may require a modification of these procedures. In all cases, the pilot shall exercise good judgement and maintain positive airplane control. * If the runway in use cannot be determined, overfly the airport at least 500' above Traffic Pattern Altitude to observe traffic and/or wind direction indicators to determine a runway for use. Standards Maintain proper spacing from other aircraft. Maintain orientation with landing runway. Maintain traffic pattern altitude +/- 100' (Private) or 50' (Commercial) and +/- 10 KIAS. 9 Lake Elmo Aero, LLC - July 2021 Traffic Pattern Departure Ref: AFH Ch. 7, AC 90-66B Objective: To safely depart an airport after takeoff or integrate into the flow of traffic when remaining in the traffic pattern. If departing the traffic pattern... 1. Climb straight out on runway heading until above traffic pattern altitude, or... 2. Exit with a 45-degree turn to the left (assuming left-hand traffic) beyond the departure end of the runway, OR exit on the downwind leg once above traffic pattern altitude. 3. Pitch to an appropriate speed that balances climb performance with engine cooling. 4. Complete the Climb Checklist. If remaining in the traffic pattern... 1. Begin a turn to the crosswind leg when beyond the departure end of the runway and within 300 feet of Traffic Pattern Altitude. The above procedure assumes an ideal traffic pattern situation. Other traffic, ATC, local traffic pattern restrictions, obstacles, etc may require a modification of these procedures. In all cases, the pilot shall exercise good judgement and maintain positive airplane control. Standards Maintain proper spacing from other aircraft. Maintain orientation with runway. Maintain traffic pattern altitude +/- 100' (Private) or 50' (Commercial) and +/- 10 KIAS. 10 10 Traffic Pattern Quick Reference Pattern Departure Upwind Downwind Base Final 70-80 KIAS 67 KIAS [VY] 80 KIAS 70 KIAS 60 KIAS Lake Elmo Aero, LLC - July 2021 BASE 70 KIAS FLAPS 20 FINAL 60 KIAS FLAPS 30 DOWNWIND 80 KIAS FLAPS 10 45 ENTRY RUNWAY 11 CROSSWIND DEPARTURE 70-80 KIAS UPWIND 67 KIAS FULL POWER Lake Elmo Aero, LLC - July 2021 Clearing Turns Ref: AIM Sec. 4 Objective: To observe any local threats or hazards, including obstacles or other traffic, prior to commencing any training maneuver. 1. Visually scan the area to the left and right of the aircraft. 2. Select a visual landmark off the wingtip in the direction of the turn to be executed as a 90-degree reference point. 3. Enter a 30-degree bank in the direction of the visual landmark. 4. Continuously scan the area above, below, and ahead of the flight path. Use the aircraft's wing position to your advantage; in a Cessna, the best visibility will be on the side from which you are turning away. 5. After completing a 90-degree turn, roll wings level on the selected landmark. 6. Select another visual landmark off the opposite wingtip in the direction of the next 90-degree turn. 7. Enter a 30-degree bank in the direction of the visual landmark. 8. Continuously scan the area above, below, and ahead of the flight path. 9. After completing the second 90-degree turn, roll wings level on the selected landmark. The aircraft should now be on its original heading. Note: Clearing turns do not absolve a pilot of his/her responsibility to see and avoid traffic while performing training maneuvers. 12 12 Lake Elmo Aero, LLC - July 2021 Configuring the Aircraft for Maneuvers Prior to commencing any maneuvers, the following configuration settings should be considered. Recommendations are offered below for individual maneuvers. BOOST/FUEL PUMP No auxiliary fuel pumps are installed on the Cessna 152; this step can be disregarded for this aircraft. CARBURETOR HEAT Carburetor heat should be used any time the engine will experience continuous RPM settings below 2000 RPM. GAS/FUEL TANKS The Fuel Shutoff Valve should always be in the "on" position. UNDERCARRIAGE/LANDING GEAR Brakes should never be set in flight. Brake pressure can be checked before ground reference or landing maneuvers by briefly pressing on both toe pedals and feeling for feedback/pressure. If operating an aircraft equipped with retractable landing gear, the down-and-locked position should be ensured if required by the maneuver. The Cessna 152 is not equipped as such. MIXTURE Mixture should always be set to full rich for maneuvers. POWER/PROPELLER Engine power and/or propeller RPM should be set as needed for the maneuver to be performed. SEAT BELTS All occupants' seat belts should be fastened at all times, and any baggage that may shift during maneuvers should be secured with seat belts if possible. SWITCHES All aircraft lights should be on for maneuvers. Additionally, pitot heat should be used if entering instrument conditions or in any form of visible moisture. The preceding configuration can be accomplished by following the acronym: BCGUMPSS Boost Pump Carburetor Heat Gas Undercarriage Mixture Power Seat belts Switches الله 13 Lake Elmo Aero, LLC - July 2021 TAKEOFFS AND LANDINGS Normal Takeoff and Climb Ref: POH 4-7 and 4-14, AFH 5-3 Objective: To safely execute a takeoff under normal conditions. 1. Complete the Before Takeoff Checklist. 2. Center the aircraft on the runway centerline with the nose wheel straight ahead. 3. Advance the throttle to full power. 4. Check engine instruments as power increases. 5. When airspeed indicator begins moving, call out "Airspeed Alive". 6. Accelerate aircraft to 50 KIAS. 7. Increase back pressure on the control yoke to pitch up until the glare shield meets the horizon (approximately 10 degrees nose-up). 8. When practical, accelerate to 67 KIAS [VY] and climb on centerline. Trim as necessary. If departing the pattern... 9. Execute a Traffic Pattern Departure procedure as applicable. 10. Above 1000' AGL, complete the Climb Checklist. If remaining in the pattern... 11. Begin a turn to the crosswind leg when beyond the departure end of the runway and within 300 feet of Traffic Pattern Altitude. Takeoff power Best climb speed Vy, Vx or POH/AFM cruise climb speed Takeoff pitch altitude Takeoff roll (1) Lift-off (2) Safe maneuvering altitude climb power Climb (3) Standards Maintain airspeed +10/-5 KIAS (Private) or +5/-5 KIAS (Commercial) from VY. 14 WIND En route climb

Type certificate, explained

What's in the Cessna 152 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.

TCDS 3A19Rev 40· Issued 1997
Read the full TCDS

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