Normal Procedures for the CESSNA 172M SKYHAWK
CESSNA 172M SKYHAWK · Normal Procedures
Overview
This document serves as the Normal Procedures manual for the CESSNA 172M SKYHAWK. It is designed for pilots operating this specific model, providing essential procedures and guidelines to ensure safe and efficient flight operations. The manual covers various aspects of flight operations, including preflight checks, engine start procedures, takeoff and landing protocols, and emergency procedures. It is an important resource for both new and experienced pilots to familiarize themselves with the operational characteristics and requirements of the CESSNA 172M.
- Perform a thorough Preflight Inspection to ensure aircraft readiness.
- Follow the correct Engine Start Procedures to avoid damage.
- Adhere to specified speeds during Takeoff and Landing.
- Maintain situational awareness during approach and landing phases.
- Know the Emergency Procedures for quick response in critical situations.
Document
Source
Originally published by www.regalair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Normal Procedures
- Pages
- 12
- File size
- 749 KB
- Publisher
- www.regalair.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 640
- Engine (hp)
- 150
- Height (ft)
- 8
- Length (ft)
- 27
- Propeller
- McCauley 1A170/DM
- Wingspan (ft)
- 36
- Engine model
- Lycoming O-320
- Max speed (kt)
- 124
- Cruise speed (kt)
- 110
- Empty weight (lb)
- 1,550
- Fuel capacity (gal)
- 40
- Rate of climb (fpm)
- 730
- Service ceiling (ft)
- 14,000
- Max takeoff weight (lb)
- 2,300
Performance
- Fuel burn (gph)
- 8
- Landing over 50ft
- 1,800
- Max crosswind (kt)
- 15
- Takeoff over 50ft
- 2,100
- Landing distance (ft)
- 1,200
- Takeoff distance (ft)
- 1,500
- Best glide speed (kt)
- 65
- Stall speed clean (kt)
- 50
- Stall speed landing (kt)
- 45
V-speeds
- VA
- 105
- VR
- 55
- VX
- 62
- VY
- 74
- VFE
- 85
- VNE
- 163
- VNO
- 125
- VS1
- 48
- VSO
- 40
- VREF
- 60
Weight & balance
- Useful load (lb)
- 750
- Max ramp weight (lb)
- 2,320
- Baggage allowance (lb)
- 200
- Basic empty weight (lb)
- 1,550
- Max landing weight (lb)
- 2,300
- Max takeoff weight (lb)
- 2,300
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172M SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Preflight Inspection
The Preflight Inspection section outlines the necessary checks to be performed before flight. This includes verifying fuel levels, checking oil levels, inspecting control surfaces, and ensuring all instruments are functioning correctly. Pilots are advised to follow a systematic approach to ensure safety.
Engine Start Procedures
This section details the steps for safely starting the engine, including the proper sequence for turning on electrical systems, priming the engine, and engaging the starter. It emphasizes the importance of monitoring engine gauges during the start process.
Takeoff Procedures
The Takeoff Procedures section provides guidelines for a safe takeoff, including the recommended speeds for rotation and climb-out. It also discusses the importance of checking the runway conditions and ensuring that the aircraft is properly configured for takeoff.
Landing Procedures
Landing Procedures cover the approach and landing phases, including the recommended speeds and configurations for landing. It highlights the importance of maintaining situational awareness and adjusting for wind conditions.
Emergency Procedures
This section outlines the actions to take in various emergency situations, such as engine failure, electrical failure, and other in-flight emergencies. It provides step-by-step instructions to help pilots respond effectively.
Safety notes
- Always conduct a Preflight Inspection before every flight.
- Monitor engine gauges closely during start-up and operation.
- Be aware of weather conditions that may affect takeoff and landing.
Full document text
Air Plains Services Corp. P. O. Box 541 Wellington Airport Wellington, KS 67152 Section 9 Supplements FAA Approved Supplemental Airplane Flight Manual For Cessna 172M & N Serial No. 17265685 to 17271034 Serial No. 17269856 N 73884 The information contained in this Manual is FAA Approved Material, which, along with the FAA Approved placards and instrument markings, is applicable to the operation of the airplane when modified in accordance with STC SA2196CE, which increases the maximum certificated takeoff weight to 2550 lbs. and limits the flap travel to 30 degrees. The airplane must previously have been modified in accordance with STC SA4428SW which installs a 180hp. Lyc. 0-360 series engine and a fixed pitch propeller. FAA Approved SEPT. 25, 1986 Rev. 2 date JUL 06 1988 1. GENERAL 2. LIMITATIONS 3. EMERGENCY PROCEDURES 4. NORMAL PROCEDURES 5. PERFORMANCE 6. WEIGHT AND BALANCE FAA Approved Утвали Manager, Wichita Aircraft Certification Office FAA Central Region, Wichita, KS Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Kansas 67152 Rev. Pages Affected 1 1 10 2 1 - 10 Section 9 Supplements Cessna Model 172M & N FAA Approved Date Log of Revisions Description Changed Page Numbers Revised Cover Sheet Added Engine Models Added M Models Changed name to Air Plains Services Corp. G. M. Baker 10/02/87 G. M. Baker 07/06/88 3 3 & 4 Added 0360A4N B.L. Sensen 3/21/90 FAA Approved Sept. 25, 1986 Page 2 of 10 Rev. 3. date 3/21/90 Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Ks. 67152 SECTION 1. General DESCRIPTIVE DATA PAGE 1-3 ENGINE Cessna Model 172M & N Section 9 Supplements Engine Model Number: 0-360-A2F, A3A, A4A, A4M & A4N Engine Type: Normally aspirated, direct drive, air cooled, horizontally opposed, carburetor equipped, four cylinder engine with 360 cu. in. displacement. Horsepower Rating and Engine Speed: 180 rated BHP at 2700RPM Maximum Continuous RPM: 2540 RPM PAGE 1-5 MAXIMUM CERTIFICATED WEIGHTS Takeoff, Normal 2550lbs. Utility 2000lbs. Landing, Normal 2550lbs. Utility 2000lbs. SECTION 2. Limitations FLAP TRAVEL Limited to 30 degrees. PAGE 2-5 AIRSPEED INDICATOR MARKINGS Airspeed indicator must be replaced with Cessna P/N C661064- 0112, Air Plains Services P/N172861-2 or remarked as follows: FAA Approved Sept. 25, 1986 Page 3 of 10 Rev.3 date 3/21/90 Air Plains Services Corp. P.O. Box 541. Wellington Airport Wellington, Ks. 67152 Cessna Model 172M & N PAGE 2-5 AIRSPEED INDICATOR MARKINGS, (cont.) MARKING KIAS VALUE OR RANGE White Arc 40-85 Green Arc 50-127 Yellow Arc 127-158 Red Line 158 PAGE 2-4 AIRSPEED LIMITATIONS VA Maneuvering Speed: 2550 Pounds 105 KIAS 2150 Pounds 95. KIAS 1750 Pounds 85 KIAS Section 9 Supplements PAGE 2-5 POWER PLANT LIMITATIONS Engine Model Number: 0-360-A2F, A3A, A4A, A4M and A4N Maximum Power: 180 BHP rating Maximum Continuous RPM: 2540 RPM PAGE 2-6 WEIGHT LIMITS Maximum Takeoff Weight, Normal 2550lbs. Utility 2000lbs. Maximum Landing Weight, Normal Utility 2550lbs. 2000lbs. PAGE 2-7 CENTER OF GRAVITY LIMITS NORMAL CATEGORY Center of Gravity Range: Forward: 35.0 inches aft of datum at 1950 lbs. or less, with straight line variation to 41.0 inches aft of datum at 2550 lbs. FAA Approved Sept. 25, 1986 Page 4 of 10 Rev. 3 date 3/21/90 Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Ks. 67152 Cessna Model 172M & N PAGE 2-7 CENTER OF GRAVITY LIMITS, (cont.) UTILITY CATEGORY Section 9 Supplements Center of Gravity Range: Forward: 35.0 inches aft of datum at 1950lbs. or less, with straight line variation to 35.5 inches aft of datum at 2000lbs. Aft: 40.5 inches aft of datum at all weights. PAGE 2-8 FLIGHT LOAD FACTORS NORMAL CATEGORY - Flight Load Factors (Maximum Takeoff Weight 2550lbs): Flaps Up. Flaps Down. PAGE 2-12 PLACARDS 10. +3.8g, -1.52g .+3.0g Near airspeed indicator: MANEUVER SPEED SECTION 3. Emergency Procedures PAGE 3-3 AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure after Takeoff: Wing Flaps Up.... Wing Flaps Down. Maneuvering Speed: 2550 lbs... 2150 lbs. 1750 lbs.!. Maximum Glide: 2550 lbs. 105 KIAS 70 KIAS ..65 KIAS 105 KIAS .95 KIAS ,85 KIAS 68 KIAS 2150 lbs. 1750 lbs. Precautionary Landing With Engine Power. Landing Without Engine Power: 1 Wing Flaps Up..... Wing Flaps Down. FAA Approved Sept. 25, 1986 Page 5 of 10 Rev.2 date JUL 06 1988 62 KIAS ..56 KIAS .65 KIAS . 70 KIAS .65 KIAS Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Ks. 67152 Cessna Model 172M & N PAGE 3-4 ENGINE FAILURES ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. -- Airspeed 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) PAGE 3-4 ENGINE FAILURE DURING FLIGHT 1. Airspeed 75 KIAS Section 9 Supplements PAGE 3-4 FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1. Airspeed 5. Wing Flaps 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) AS REQUIRED (30 deg recommended PRECAUTIONARY LANDING WITH ENGINE POWER Airspeed 65 KIAS Wing Flaps 30 deg (on final approach). Airspeed -- 65 KIAS 2. 5. 6. PAGE 3-5 DITCHING 4. Wing Flaps -- 20-30 deg. NOTE approach at 70 KIAS with flaps up If no power is available, or at 65 KIAS with 10 deg flaps. PAGE 3-7 ICING INADVERTENT ICING ENCOUNTER 11. Approach at 80 to 90 KIAS depending upon the amount of the accumulation. FAA Approved Sept. 25, 1986 Page 6 of 10 Rev. 2 date JUL 06 1988 Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Ks. 67152 Cessna Model 172M & N SECTION 4. Normal Procedures PAGE 4-3 NORMAL PROCEDURES Section 9 Supplements SPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a maximum weight of 2550 pounds and may be used for any lesser weight. Page 4-3 Takeoff Normal Climb Out. ...75-85 KIAS Short Field Takeoff, Flaps 10 deg, Speed at 50 Feet..57 KIAS Enroute Climb, Flaps Up: Normal, Sea Level... Normal, 10,000 Feet.. Best Rate of Climb, Sea Level. .75-85 KIAS 70-80 KIAS 73 KIAS .72 KIAS 62 KIAS 67 KIAS 65-75 KIAS Best Rate of Climb, 10,000 Feet. Best Angle of Climb, Sea Level..
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Best Angle of Climb, 10,000 Feet. Landing Approach: Normal Approach, Flaps Up..... Normal Approach, Flaps 30 deg.. Short Field Approach, Flaps 30 deg. Balked Landing: Maximum Power, Flaps 20 deg.... Maximum Recommended Turbulent Air Penetration Speed: 2550 Lbs... 2150 Lbs. 1750 Lbs. . .60-70 KIAS 62 KIAS ..60 KIAS 105 KIAS .95 KIAS 85 KIAS PAGE 4-8 SHORT FIELD TAKEOFF Climb Speed -- 57 KIAS (until all obstacles are cleared). PAGE 4-8 ENROUTE CLIMB Airspeed FAA Approved Sept. 25, 1986 Page 7 of 10 ―― 75-85 Rev. 2 date JUL 06 1988 Air Plains Services Corp. P.O. Box 541 Wellington Airport Wellington, Ks. 67152 PAGE 4-9 LANDING NORMAL LANDING Cessna Model 172 M & N Section 9 Supplements 65-75 KIAS (flaps up) -- AS DESIRED(0-10 deg. below 110 KIAS, 10-30 deg. below 85 KIAS). 1. Airspeed 2. Wing Flaps 3. Airspeed -- SHORT FIELD LANDING 1. -- 60-70 KIAS (flaps down) Airspeed 2. Wing Flaps Airspeed 3. BALKED LANDING -- Wing Flaps -- 65-75 KIAS (flaps up) FULL DOWN (30deg.) 62 KIAS (until flare) 10 deg. (until obstacles are cleared) RETRACT SLOWLY after reaching a safe altitude and 65 KIAS. 5. Section 5 PAGE 5-21 LANDING DISTANCE SHORT FIELD CONDITIONS: Flaps 30 deg. NOTES: 4. If a landing with flaps up is 'necessary, increase approach speed by 9 kias and allow for 35% longer distance. WEIGHT LBS SPEED AT 50 FT 0°C 10°C 20°C 30°C 40°C PRESS ALT FT KIAS 50 FT OBS GRND TOTAL FT GRND TOTAL FT GRND TOTAL FT GRND TOTAL FT GRND TOTAL FT ROLL TO CLEAR ROLL TO CLEAR ROLL TO CLEAR ROLL TO CLEAR ROLL TO CLEAR FT 50 FT OBS FT FT 50 FT OBS FT 50 FT OBS FT 50 FT OBS 2550 62 62 S.L. 545 1290 565 1320 585 1350 605 1380 625 1415 1000 555 1320 585 1350 605 1385 625 1420 650 1450 2000 585 1355 610 1385 630 1420 650 1455 670 1490 3000 610 1385 630 1425 655 1460 675 1495 695 1530 4000 6:30 1425 655 1460 675 1495 700 1535 725 1570 5000 655 1460 680 1500 705 1535 725 1575 750 1615 6000 680 1500 705 1540 730 1580 755 1620 780 1660 7000 705 1545 730 1585 760 1625 785 1665 810 1705 8000 735 1585 760 1630 790 1670 815 1715 840 1755 FAA Approved Sept. 25, 1986 Page 8 of 10 Rev. 2 date JUL 06 1988 2500 2500 WEIGHT AND BALANCE FOR CESSNA 172M & N 2400 2300 CENTER OF GRAVITY LIMITS 2200 2100 |LOADED AIRPLANE WEIGHT (POUNDS) 2000 1900 UTILITY CATEGORY HORMAL CATEGORY 1800 17001 1600 1500 34 35 36 37 38 39 AIRPLANE C.G. 40 41 LOCATION - 42 43 44 45 46 47 INCHES AFT OF DATUM (STA 0.0 ) 43 FAA Approved Page 9 of 10 Sept. 25, 1986 Rev. 2, date JUL. 06 1988 LOADED AIRPLANE WEIGHT (POUNDS) 2600 2500 2400 2300 2200 2100 2000 1900 1300 1700 1600 Weight and Balance for Cessna 172M & N CENTER OF GRAVITY MOMENT ENVELOPE 1500 50 55 60 05 UTILITY CATEGORY 70 75 80 85 90 NORMAL CATEGORY LOADED AIRPLANE MOMENT/1000 (POUND 95 100 เจร 110 115 120 - INCHES) FAA Approved Page 10 of 10 260 250 Pressure Altitude Ft. 180HP CESSNA 172 SKYHAWK CRUISE PERFORMANCE Standard Temperature % RPM BHP GPH 2000 2550 76 10.2 2500 72 9.6 2400 64 8.7 2300 58 7.9 2200 52 7.2 2100 46 6.6 4000 2600 .76 10.2 2500 68 9.2 2400 52 8.3 2300 55 7.6 2200 49 6.9 2100 44 6.3 6000 2650 76 10.1 2500 69 9.2 2400 62 8.4 2300 56 7.7 2200 53 7.3 8000 2700 76 10.1 2600 69 9.2 2500 62 8.4 2400 56 7.7 2300 53 7.3 2200 47 6.7 10000 2700 72 9.6 2600 65 8.8 2500 59 8.1 2400 53 7.4 2300 48 6.8 12000 2650 65 8.8 2600 62 8.4 2500 56 7.7 2400 51 7.1
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