Pilot's Operating Handbook and FAA Approved Airplane Flight Manual

CESSNA 182S SKYLANE · Pilot's Operating Handbook

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Overview

The Cessna 182S Pilot's Operating Handbook (POH) is an FAA Approved Airplane Flight Manual that provides essential information for operating the Cessna 182S aircraft. It includes details on performance specifications, operating procedures, and maintenance guidelines, ensuring pilots can utilize the aircraft effectively and safely.

This manual must be carried in the airplane at all times.
The Cessna 182S is designed for performance, value, and comfort.
It includes information on equipment, operating procedures, and suggested service.
The handbook is applicable to airplane serial number 18280001 and on.
Revisions must be incorporated as they are issued to maintain current information.
Cessna Service Stations provide warranty coverage and expert service.
The manual contains nine sections covering all operational aspects.
Temporary revisions may be issued and must be incorporated into the POH.

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Source

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

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Document details

Type: Pilot's Operating Handbook
Year: 1997
File size: 58 MB
Publisher: ln-edb.com
Language: en

Specifications & performance

Extracted from this document.

Specifications

Empty weight (lb): 1925
Oil capacity qts: 9
Fuel capacity (gal): 92
Max landing weight (lb): 2950
Max takeoff weight (lb): 3100

Performance

Max range (nm): 968
Max speed (kt): 145
Cruise speed (kt): 140
Rate of climb (fpm): 924
Service ceiling (ft): 18100

V-speeds

VS_KCAS: 54
VSO_KCAS: 49

Weight & balance

Max ramp weight (lb): 3110
Max useful load (lb): 1185
Baggage allowance (lb): 200

About this document

What is the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual?

The Pilot's Operating Handbook and FAA Approved Airplane Flight Manual is a pilot's operating handbook for the CESSNA 182S SKYLANE, dated 1997.

Where does the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual come from?

This copy of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual was originally published by ln-edb.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual published?

The Pilot's Operating Handbook and FAA Approved Airplane Flight Manual — the CESSNA 182S SKYLANE pilot's operating handbook on file — is dated 1997.

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the CESSNA 182S SKYLANE.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More CESSNA 182S SKYLANEmanuals & documents

In this document

Performance Specifications

The performance specifications section outlines the aircraft's speed, climb rate, service ceiling, takeoff and landing performance, and weight limits.

Coverage/Revisions

This section details the applicability of the handbook, the importance of maintaining current revisions, and instructions for filing revisions.

Warnings, Cautions, and Notes

This section explains the use of warnings, cautions, and notes throughout the manual to highlight important operational procedures.

Congratulations

A welcome message to new owners, emphasizing the design and construction of the Cessna 182S for optimal performance.

Temporary Revisions

Details on how to incorporate temporary revisions into the POH and the importance of tracking their status.

FAA Approval

Confirms that the manual is FAA approved under FAR Part 23 Subpart J.

Safety notes

Warnings must be followed precisely to avoid injury or death.
Cautions must be adhered to in order to prevent damage to equipment.
Notes provide additional information that is important for operations.

Full document text

This is the Flight Manual whICh ~ a(t of "- Cert ificate of Airworth iness for -rer __~x1G_~ _ ~ "" ~CeSSna ~ V ' -.'j A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual TH IS DOCUMENT MUST BE CARRIED IN THE AIRPLANE AT ALL TIM ES. o The Cessna Aircraft Company Model 182S Se rial No . 18280529 Registration No. N7 2 69A This publication includes Ihe material required to be furnished to the pilot by FAR Part 23 and constitutes the FAA Approved Ai rplane Flight Manual. FAA APP ROVAL ~AA APPROVED UNDER FAR 2' SUBPART J The Ce"na Aircraft Co _~a~ Option Manufacturer CE.1 7~t'~~En8' ...r Dale : February 21. 1997 f) Member of GAMA COPYRIGHT C> 1997 The Cessna Aircraft Company Wichita, Kansas USA Origina l Issue - 3 February 1997 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON IPd;z/t; /29'9 SUBSEQUENT REVISIONS SUPPLIED BY THE CESSNA AIRCRAFT COMPANY MUST BE PROPERLY INSERTED. The Cessna Aircraft Company, Aircraft Division CESSNA MODEL 182S PUBLICATION PART NUMBER Pilot's Operat in g Handbook and FAA Approved Airplane Flight Manual Serial Numbers 18280001 and On Original Issue - 3 February 1997 Revision 4 - 1 NOVEMBER 2001 PART NUMBER: 182SPHUS04 I Nov 1/0 1 i/(ii blank) CESSNA MO DEL 182S CONGRAT ULATI ONS CONGRATULATIONS . ... Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most In performance. value and comfort. This Pilot's Operating Handbook has been prepared as a guide to help yo u get the most utility from your ai rplan e. It contains information about your airplane's equipment, operating procedures, performance and suggested service and ca re. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Service Station: THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Ca re Program Handbook supplied with your airplane. The Customer Care Ca rd assigned to you at delivery will establish your eligibility under warranty and should be presented 10 your local Cessna Service Station at Ihe time of warranty service. FACTORY TRAINED PERSONNEL to provide you with courteous, expert service. FACTORY APPROVED SERVICE EQUIPMENT to provide you efficienl and accurate workmanship. A STOCK OF GENUINE CESSNA SERVICE PARTS are available when you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNA AIRPLANES. Cessna Service Stations have all of the currenl Maintenance Manuals, Illustrated Parts Catalogs and various other support publications produced by Cessna Aircraft Company. A current Cessna Service Station Directory accompanies your new ai rplane. The Di rectory is revised annually, and a current copy can be obtained from your. nearest Cessna Service Station. We urge all Cessna owners/operators to utilize the benefits available within the Cessna Organization. Nov 15100 i ii PERFORMANCE- SPECIFICATIONS CESSNA MODEL 182S I PERFORMANCE - SPECIFICATIONS • SPEED Maximum at Sea Level ......... . ..... . .. . ... 145 KTS Cruise, 80% Power at 6000 Ft (Best Power Mixture) 140 KTS CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, c li mb and 45 minutes reserve. 75% Power at 6000 Ft . .. ........ . . Range 88 Gallons Usable Fue l Time Max Range at 10,000 Ft, 55% Power Range 88 Gallons Usable Fuel Time RATE OF CLIMB AT SEA LEVEL: .....•........... SERVICE CE ILING: ..... . ..... . ..• • ... . • ...•.. TAKEOFF PERFORMANCE: Ground Roll . .................... .. .•. . .. . . Total Distance Over 50 Ft. Obstacle ..• • .... • . .. LANDING PERFORMANCE: Ground Roll ............. . . . ... • .... Total Distance Over 50 Ft. Obstacle . . • • . ...•... STALL SPEED (KCAS): Flaps Up, Power Off .......•. . .. •. ......... Flaps Down, Power Off ... . .....•....•....•. MAXIMUM WE IG HT: Ramp Takeoff Landing 820NM 6.05 HRS 968 NM 8.05 HRS 924 FPM 18,100 FT 795 FT 1514 FT 590 FT 1350 FT 54 KCAS 49 KCAS 3110LBS 3100 LBS 2950 LBS 'Speed periormance and range are shown fo r an airpl ane equipped with optional speed fairings which increase the speeds by approximately 3 knots. All other periormance figures are unchanged when speed fairings are removed. Periormance above is based on a 2-bladed propeller. Periormance with the 3-blade propeller is essentially the same as shown above. iv Dec 1/97 CESSNA MO DEL 182S PERFORMANCE- SPECI FI CATIONS PERFORMANCE-SPECIFICATIONS (Continued) STANDARD EMPTY WEIGHT: ....•• . . . .• . ....•. . MAXIMUM USEFUL LOAD: ........ • •. . . . _•. . ... BAGGAG E A LL OWANCE: 1925 LBS I1185 LBS 200 LBS WING LOADING: Lbs/Sq Ft . ....... • . ... . • . . .. .•. . . . 17.8 POWER LOADING: Lbs/HP . . . . . . . . . . • .. . . • • . . . . 13.5 FUEL CA PAC ITY: ................. . .. . •. . ...... 92 GAL OI L CAPAC IT Y: ............. • ... . •.. . .. . ....... . 9 QTS ENG INE: Textron Lycoming . . . . . .•.. . . .. . .. . IO-540-AB1A5 230 BHP at 2400 RPM PROPE LL ER: Diameter - 3-Blade Diameter - 2-Blade NOTE 791N. 82 1N. The above peliormance figures are based on the indicated we ights, standard atmospheric conditions, level, hard-suliaced dry runways and no wind. They are calculated values derived from flight tests conducted by The Cessna Aircraft Company under carefully documented condi tions and will vary with individu al airplan es and numerous factors affecting flight performance. Nov 15/00 v COVERAGE/ REVISIONS CESSNA MODEL 182S COVERAGE The Pilot's Operating Handbook in the airplane at the time of delivery from The Cessna Ai rcraft Company contains information applicable to the Model 182S airplane by seri al number and

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registration number shown on the Title Page. This handbook is applicable to airplane serial number 18280001 and On. All information is based on data available at the time of publication. I This handbook is comprised of nine sections w hi ch cover all operational aspects of a standard-equipped ai rplane. Section 9, Supplements, provides expanded operational procedures for the avionics equipment (both standard and optional), details requirements for foreign certification , and provides information on special operations . I Supplements are individual documents, and may be issued or revised without regard to revision dates which apply to the POH itself. These supplements contain their own L og of Effective Pages, wh ich should be used to determine the status of each supplement. ORIGINAL ISSUE AND REVISIONS This Pilot's Operating Handbook and FAA Approved Airplane Flight Manual is comprised of the original issue and any subsequent revisions. To ensure that information in this manual is current, the r ev isions must be incorporated as they are issued. Th is manu al was origina ll y issu ed on February 3, 1997. As revisions are issued, they will be noted in the L og of Effective Pages table. The part number of this manual has also been designed to fur- ther aid the owner/operator in determining the revision level of any POH. Refer to the example below for a breakdown: vi 182S PH US 00 TTL-_- Revision Level (Revision 0, Original Issue) Manual (Pilot's Operating Handbook, U.S.) Airplane Model (182S) Nov 15/00 CESSNA MODEL 182S COVERAGE/REVISIONS It is th e responsib il ity of the ow ner to maintain this handbook in a.cu rr ent status when it is being used for operational purposes. Owners should contact their Cessna Service Station whenever the revision status of their handbook is in question. Revisions are distributed to owners of U .S. Reg istered aircraft according to FAA records at the time of revision issuance, and to Internationa ll y Registered aircraft according to Cessna Owner Advisory records at the time of issuance. Revisions should be read care fu lly upon receipt and incorporated in this PO H. REVISION FILING INSTRUCTIONS REGULAR RE VIStO NS Pages to be removed or inserted in the Pilots' Operating Handbook and FAA Approved Airplane Flight Manual are determined by the Log of Effective Pages located in this section. This log contains the page number and date of issue for each page within the POH. At original issue, all pages will contain the same date. As revisions to the POH occur, these dates will change on eHected pages. When two pages display the same page number, the page with the latest date shall be inserted into the POH. The date on the Log Of Effective Pages shall also agree with the latest date of the page in question . TEMPORARY REVISIONS Under limited circumstances, temporary revisions to the POH may be issued. These temporary r ev isions are to be filed in the applicable section in accordance with filing instructions appearing on the first page of the temporary revision. The recess io n of a temporary revision is accomplished by incorporation into the POH at revision time or by a superseding temporary revisi on . In order to accurately track the status of temporary revisions as they pertain to a POH , a Temporary Revision List will be located previous to this section when required. This list will indicate the date the temporary revision was incorporated into the POH, thus authorizing the recession of the temporary revision. Nov 15100 vii COVERAGE/REVISIONS CESSNA MODEL 182S IDENTIFYING REVISED MATERIAL Additions or revisions to the text in an existing section will be identified by a vertical line (revision bar) adjacent to the applicable revised area on the outer margin of the page. When technical changes cause unchanged text to appear on a different page, a revision bar will be placed in the outer lower margin of the page, opposite the page number and date of the page, providing no other revision bar appears on the page. These pages will display the current revision date as found in the Original Issue and Revisions paragraph of this section. When extensive technical changes are made to text in an existing section that requires extensive revision, revision bars will appear the full length of text. New art added to an existing section will be identified by a single pointing hand indicator adjacent to the figure title and figure number. Existing art which is revised will have a pointing hand adjacent to the portion of the art which has changed. WARNINGS, CAUTIONS AND NOTES Throughout the text, warnings, cautions and notes pertaining to airplane handling and operations are uti lized. These adjuncts to the text are used to highlight or emphasize important points. viii WARNING - Calls attention to use of methods, procedures or limits which must be followed precisely to avoid injury or death to persons. CAUTION - Calls attention to methods, procedures or limits wh ich must be followed to avoid damage to equipment. NOTE - Calls attention to additional procedures or inlormation pertaining to the text. Feb 3/97 Temporary Revisions MODEL 182 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Cessna Model 182S, 182T, and T182T The following list of Temporary Revisions must be incorporated into the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual until the removal instructions have been complied with. Insert this page opposite the Log of Effecti ve Pages in the front of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. TEMPORARY PAGE REVISION NUMBER NUMBER 182PHTR01 4-12 ISSUE DATE 02/16/04 ~ I A j IlW Ci:..sSIol Pl g& \!!lr - Z ... ,O I ~ t'Io~ /k ..... pi.., 16 February 2004 182PHTR CESSNA MODEL 182S LOG OF EFFECTIVE PAGES LOG OF EFFECTIVE PAGES Th e following L og of Effective P ages provides the date of issue fo r original and revised pages , as wel l as a listing of all pages in the POH. Pages which are affected by the current revision wi ll carry the date of that revision. Revi sio n Level Oate of Issue Revi s ion Level Date of Issue o (O ri ginal Issue) Feb . 3, 1997 3 Nov . IS, 2000 1 June 13, 1997 4 Nov. 1. 2001 2 Dec. 1. 1997 PAGE DATE PAGE DATE Tille .. . . . . .. .. .. . Feb 3/97 1-16 . .. . . . . . . . Nov 15/00 Assignment Record Feb 3197 - 1-17 Nov 15/00 i Nov 1101 1-18 · . . . . . . . . - Nov 15/ 00 ii (Blank) . ........ Feb 3197 1·19 · . . . . . . . . . . June 13/97 · iii .. . Nov 15/ 00 1·20 . . . . . . .... . No v 15/ 00 iv .. . De c 1197 1-21 . .. .. . .... . No v 15/ 00 v . . . . Nov 15/00 1-22 .... . . . . . . Nov 15/00 vi Nov 15/00 1-23 ... ....... Nov 15/ 00 vii Nov 15/00 1-24 · . . . . . . . . . June 13/97 viii . . . . . , .. . . . . . . Feb 3197 1-25 Nov 15/00 ix Nov 15/ 00 1-26 . ......... Nov 15/ 00 x ... , ... Nov 15/ 00 2-1 . . ....... . ... Feb 3/97 xi . . . . . . Nov 15/ 00 2·2 (Blank) Feb 3/97. xi i ... . . .. . . .. , Nov 15/ 00 2·3 · . . . . . . . . . . . Nov 15/ 00 xiii Feb 3197 2·4 ..... .. . , . .. Feb 3/97 xiv (Blank) Feb 3/97 2·5 June 13/97 . 1· I Nov 15/00 2-6 Nov 15/ 00 1-2 Feb 3/97 2·7 · ... . ... . .... Feb 3/97 1-3 ... . . . ... . . . . Feb 3/97 2·8 Feb 319 7 1-4 .. . - .. ... .. , . Dec 1/ 97 - 2·9 · .... . ...... . Feb 3197- 1·5 Nov 15/ 00 2·10 . .......... . Feb 3197 1·6 ., .. .. .... .. No v 15/ 00 2 -11 . . . . ... . . . .. Feb 3/97 1·7 Nov 15/00 2- 12 Fe b 3/97 1·8 . . . . . . . . . . . Feb 3/97 2· 13 "', ... . .. .. Feb 3/97 1·9 . ... . . . . . Feb 3/97 2·14 (Blank) ....... Feb 3/ 97- 1-10 ... . . . . . .. , Feb 3197 3·1 .. ..... . , .. . Feb 3/97 1· 11 Feb 3197 3·2 .... . ... Feb 3/ 97 1·12 . . . . . . . . . . . Feb 319 7- 3-3 . .. .. ... . ... Nov 15/ 00 1-13 . . . . . . . . . . . Nov 15100 3·4 Feb 3/97 1-14 . ... . . .. .. Nov 15/00 3·5 Nov 15/ 00 1· 15 . . . . . .. . . . June 13/97 3·6 . . . . . . . . . . . Feb 3/ 97 Nov 15/00 ix LOG OF EFFECTIVE PAGES CESSNA MODEL 182S x LOG OF EFFECTIVE PAGES (Continued) PAGE DATE PAGE DATE 3-7 ...... . .. . . . Nov 15/00-· 4-16 Nov 15/00 3-8 Nov 15/00 - 4-17 Nov 15/ 00 3-9 ......... ' .. Feb 3/97 4-18 Nov 15/00 3-10 ....... . . .. . Feb 3/97 4-19 Feb 3/97 3- 11 . . . . .. . . .. . Nov 15/00 4-20 .... .... ... Feb 3/97 3-12 ...... ... , . Nov 15/00 4-21 .... , . . ... . Nov 15/00 3 -1 3 · . . . . . . . . . . . Feb 3/97 4 -2 2 · . . . . , , . . Feb 3/97 3-14 Feb 3/97 4-23 "' . .... Nov 1/01 3 -1 5 Nov 15/00 · 4-24 Feb 3197 3-16 ........... . Dec 1/97 4-25 ....... . . Feb 3197 3 -1 7 ... . . . . .•. . . Dec 1/97 4-26 .. . .. . . . ... . Feb 3/97 3-18 · . . . . . . . . . . . Feb 3/97 4-27 ... . . - ... .. Nov 15/00 3 -1 9 ..... . . .. .. . Feb 3/97 4-28 ..... . .. . . . Nov 15/00 3-20 · .. . ... . . . .. Feb 3/97 4-29 ...... ..... Nov 15/00 3-21 Feb 3/97 4-30 ... . ..... Nov 15/00 3-22 ... .. .. .. . . Nov 15/00 4-31 . ...... ... Nov 15/00 4 -1 · . . . . . . . . . . . Feb 3/97 - 4-32 Nov 15/00 4-2 · . . . . . . . . . . . Nov 15/00 4-33 · . . . . . , . . Nov 15/00 4-3 Nov 15/00 4-34 Nov 15/00 4-4 (Blank) Feb 3/97 5-1 ....... . De c 1/97 - 4-5 ........ Nov 1/01 5-2 (Blank) Feb 3/97- 4-6 .. .. . Nov 15/00 5-3 ............ Nov 15/ 00 4-7 .. . . . .. . Dec 1/97_ 5-4 .. .... .... . . . Feb 3197- 4-8 · . . . . . . . . . . . Nov 15/00 5-5 .......... Nov 15/00 4-9 ...... . Nov 15/00 5-6 .... . . . . . .... Feb 3/97 4-10 · ... . .. .. .. Nov 15/00 5-7 ......... . .. Nov 15/00 4-11 Nov 15/00 5-8 ., .... . ... . . Nov 15/00 4-12 ... . .. ... . Nov 15/00 5-9 ............. Feb 3/97- 4-13 ..... - . ... . Nov 15/00- 5-10 .. . - .. . .. ... Dec 1/97 4-14 ... . . . . . , . , , Nov 1/01 5- 11 · . . . . . .... . . Feb 3/97 4-15 .... . .. -.- .. Feb 3/97 5-12 .. .. . .. .... . Feb 3/97· Nov 1/ 01 --~ I '--- CESSNA MODEL 182S LOG OF EFFECTIVE PAGES LOG OF EFFECTIVE PAGES (Conti nued) PAGE DATE PAGE DATE 5-13 Feb 3197/ 6·15 Feb 3197/ 5·14 Nov 15 100 6 -1 6 . . . . " .. Feb 319 7"'-- 5·15 Nov 15100 6 -1 7 Dec 1197' 5·16 ..... , . .. .. Nov 15100 6-18 Nov 15100 5· 17 Nov 15100 6 -1 9 Nov 15100 5- 18 · .... . ~ . Nov 15100 6·20 Nov 15100 5-19 Nov 1 5100 6·21 Nov 15100 5-20 Nov 15100 6·22 Nov 15100 5·21 .... . . • . Nov 15100 6-23 Nov 1 5100 5-22 Nov 15100 6-24 (Blank) Feb 3197"--- 5·23 .. . . . .. . Nov 15100 7-1 , . , Nov 15100 5-24 · . . . . . . . - . Nov 15100 7-2 Nov 15 100 5-25 ... .. .... Nov 15100 7·3 Nov 15100 5-26 Nov 15100 7- 4 (Blank) Feb 3197 5-27 .... . ... Nov 15100 7·5 Nov 1 5100 ' 5·28 Nov 15100 7·6 .. . . ... .. ... Nov 15100 5·29 .... . ... Nov 15100 7-7 . . . . . . . . . . . F eb 3197 5-30 Nov 15100 ..... 7-8 Feb 3197 ...... .. .. 5-31 · ..... .. .. Feb 3197 7·9 . . . . . . . . . . . . Nov 15100 5·32 . ~ . . . ..... Feb 3197 7· 10 . . .... .. Feb 3197 5-33 . . . . . . . . . F eb 3197 7-11 Nov 15100 5·34 Feb 3197 7 -1 2 Feb 3197 5-35 Feb 3197 7-13 Nov 15100 5·36 (B lank) , , Feb 3197/ 7-14 Nov 15100 6-1 Dec 1/9"H - 7-15 Nov 15100 6-2 (Blank) Feb 319 ?- 7-16 Nov 1 5100 6·3 Nov 1 5100 7-17 . . . . . . . . . Nov 1 5100 6-4 .... . .... . . . Nov 15100 7-18 Nov 15100 6-5 Nov 15100....... 7·19 Nov 15100 6-6 Feb 319 7' 7-20 Nov 15100 6-7 Nov 1 5100 - 7- 21 Nov 15100 6-8 Feb 3197- 7-22 Nov 1510 0/ 6-9 Feb 3197 7-23 Feb 3197. 6-10 Nov 15100 7·24 Nov 15100 - 6 ·1 1 Feb 3197 - 7-25 Feb 3/97 ," 6 -1 2 . . . . . . ... Nov 15100- 7-26 Dec 1197 6-13 Feb 319 7- 7 -2 7 Nov 15100 6-14 Feb 3197 · 7-28 June 13/97- Nov 15100 xi LOG OF EFFECTIVE PAGES CESSNA MODEL 182S LOG OF EFFECTIVE PAGES (Continued) PAGE DATE PAGE DATE 7-29 June 13/97 8-2 · . . . . . . . . . . . Nov 15 /00 7-30 Nov 15/00 8-3 · . . . . . . . . , . . Nov 15/00 7· 31 Nov 15 /00 8·4 . . . . . . .. ... . Nov 15/00 7·32 Nov 15/00 8-5 Nov 15/00 7·33 ... ... .. .. . Nov 15/00 8·6 Nov 15/00 7·34 .... .. , .. Nov 15/00 8·7 Nov 15 /00 7·35 Dec 1/97 8·8 Nov 15/00 7·36 Dec 1/97 8·9 · . , . . , , , .' . . Nov 15/00 7·37 . . . . . . . . . . , Nov 15/00 · 8· 10 ... .... .. .. Nov 15 /00 7·38 . . . .. . . . . Feb 3/97 8·11 . .. . .. ... . . Nov 15 /00 7-39 . . . , _ .. . Nov 15 /00 - 8· 12 . ... ... . . . . Nov 15 /00 7·40 Nov 15 /00 8·13 . .... . ..... Nov 15 /00 7-41 Feb 3/97 8-14 ,., ........ Nov 15 /00 7·42 Feb 3/97/ 8· 15 .. ... . ... Nov 15/00 7·43 . . . . . . . . . . . . Feb 3/97. 8·16 Nov 15 /00 7-44 Nov 15/ 00 8·17 . . ... . .. Nov 15 /00 7·45 . . . . . .. . . . Feb 3/97 8·18 . " . . ... . . . Nov 15/00 7·46 . ... .. . . ... Nov 15/00 . 8·19 . ....... . .. Nov 15 /00 7-47 .... .... .. Nov 15/00 8·20 . .. . . . . , . Nov 15/00 7·48 .. , . . .... Nov 15 /00 8-21 . . . ... . . Nov 15/00 7·49 Nov 15 /00 8·22 . . . . . . . . . . Nov 15/00 7·50 ... ..... . Nov 15 /0 CY 8·23 Nov 15/00 7-51 Feb 3/97- 8-24 . . . . . . . . . . . Nov 15/0 7·52 (Blan k) Feb 3/97 9·1 . . ... " .. ... Nov 15/00- 8·1 Nov 15/00- 9-2 (Blank) Feb 3/97_ xii Nov 15/00 -~ CESSNA MODEL 182S TABLE OF CONTENTS CONTENTS SECTION GENERAL .......... . ... . ............. . 1 LIMITATIONS ... . ............ . ......... 2 EMERGENCY PROCEDURES ............ .. 3 NORMAL PROCEDURES .. ....... . ....... 4 PERFORMANCE .. . . .. ................ . . 5 WEIGHT & BALANCE/EQUIPMENT LIST . ..... 6 ,~ AIRPLANE & SYSTEMS DESCRIPTION . ...... 7 HANDLING, SERVICE & MAINTENANCE . . . . .. 8 SUPPLEMENTS .. . . . ................ . .. 9 ";::/{,,;,,h l ........ I. \ CESSNA MODEL 182S SECTION 1 GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Three View - Normal Ground Attitude . .. . .... _. ... . . . ..• Introduction Descriptive Data ....... ... . . . • . . . . ... . .... .. . . •. . . Engine .............. . • •..... . . . . . • • . ... . . .. .. Propeller (2-Bladed) ... .. . . . . . . • •..... • ........ Propeller (3 -Bladed) .. . .. . ..•.. Fuel .. . .. . ..... . ... • . .... . .. .. • . .. Oil ......... . . . • .... .. . . . . . . ... . Maximum Certificated Weights .. .. ... . . . . . .. .• . . .. Standard Airplane Weights ... . ........ • ....•... Cabin And Entry Dimensions ....... . ... . . . . . . .. • . Baggage Space and Entry Dimensions .... . ....• . ... • Specific Loadings ............ . . Symbols, Abbreviations and Terminology ...... .. . . . . .•.. General Airspeed Terminology And Symbols .. . . . •• ... . Me teorological Terminology .... . .. .. .. . ...... . ... . Engine Power Terminology ............. . ......... . Airplane Performance And Flight Planni ng Terminology Weight And Balance Terminology .. ........ . . Metric ! Imperial ! U.S. Conversion Charts ...• . .... . .. . . Weight Conversions .......... .... •• . . .. . Length Conversions . . . .. . . . . . ... . . . . . ... ... . . Distance Conversions . . . ... . . .• . . . .. . .. . . . .•.... Volume Conversions . . ......... .. . . Temperature Conversions Volume to Weight Conversions Quick Conversions Nov 15100 Page 1-2 1-4 1-4 1-4 1-4 1-4 1-5 1-6 1-7 1-7 1-71 1-7 1-7 1-8 1-8 1-9 1-9 1-10 1-11 1-13 1-14 1-16 1- 20 1- 21 1-24 1- 25 1-26 1-1 SECTION 1 GENERAL .J • PIVOT POIN T - :::rI Ir-- ~ ~ r=11'-8"=-1 rr-> I . . 1'-- ./ ~ L I CESSNA MODEL 182S • PIVOT POINT 1-+-1'---36'-O" ---~'1 1-2 82" MAX - --1-d"'-n-1 078ST1001 0785T1oo1 Figure 1-1. Thr ee View - Normal Ground Attitude (Sh eet 1 of 2) Feb 3/97 CESSNA MODEL 182S SECTION 1 GENERAL ~-- ------ ,29 '- O"--------+i,! r9'_ 4" o /::1 NOTE 1: WING SPAN SHOWN WITH STANDARD STROBE LIGHTS IN STALLED. NOTE 2: NORMAL GROUND ATIITUDE IS SHOWN WITH NOSE STRUT SHOWING APPROXIMATELY 2" OF STRUT, AND WINGS LEVEL. NOTE 3: WHEEL BASE LENGTH IS 66 y,". NOTE 4: PROPELLER GROUND CLEARANCE IS 10 %" . NOTE 5: WING AREA IS 174 SQUARE FEET. NOTE 6: MINIMUM TURNING RADIUS ('PIVOT POINT TO OUTBOARD WING TIP) IS 27' - 0". j 0785T100 1 Figure 1-1. Thr ee View - Normal Ground Attitude (Sheet 2 of 2) SECTION 1 GENERAL INTRODUCTION CESSNA MODEL 182S This handbook contains 9 sections, and includes the material required to be furni shed to the pilot by FAR Part 23. It also contains supplemental data supp li ed by The Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology common ly us ed . DESCRIPTIVE DATA ENG INE Number of Eng ines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-540-AB1A5. Engine Type: Norma ll y aspirated, direct dri ve, air-cooled , horizontally opposed, fuel injected, six cylinder eng ine with 541 cu. in. displacement. Horsepower Rating a nd Engine Speed: 230 rated BHP at 2400 RPM . IPROPELLER (2-Bladed) Prope ll er Manufacturer: McCauley Propeller Systems. Propeller Model Number: B2D34C235/90DKB· 8. Number of Blades: 2. Propeller Diameter: 82 inches. Pro pe ll er Type: Constant speed and hydraulically actuated , with a low pitch setting of 17.0° and a high pitch setti ng of 31.8 ° (30 inch station). IPROPELLER (3-Bladed) Propeller Manufacturer: McCauley Propeller Systems. Propeller Model Number: B3D36C431 /80VSA-1 . Number of Blades: 3. Propeller Diamet er: 79.0 inch es. Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 14.9 ° and a high pitch setting of 31.7 ° (30 inch station). CESSNA MODEL 182S SECTION 1 GENERAL FUEL A WARNING USE OF UNAPPROVED FUELS MAY RESULT IN DAMAGE TO THE ENGINE AND FUEL SYSTEM COMPONENTS, RESULTING IN POSSIBLE ENGINE FAILURE. Approved Fuel Grades (and Colors): 1OOLL Grade Aviation Fuel (B lu e) . 100 Grade Aviation Fuel (Green). NOTE Isopropyl alcohol or diethylene g ly col monomethyl ether (DiEGME) may be add ed to the fuel supply. Additive concentra ti ons shall not exceed 1% for isopropyl alcohol or 0.10% to 0.15% for DiEGME. Refer to Section 8 f or additional information. Fuel Capacity: Total Capacity: Total Usabl e: Total Capacity Each Tank: Total Usable Each Tank: 92.0 U .S. gallons. 88.0 U.S. gallons. 46.0 U.S. ga llons. 44.0 U.S. gallons. NOTE To ensure maxim um fuel capacity and minimize cross- feeding when refueling, always park the airplane in a wings- level, normal ground attitude and place the fu el se lector in the Left or Right position. Refer to Figure 1-1 for normal ground attit ude dimensions. Nov 15/00 I I '-5 SECTION 1 GENERAL CESSNA MODEL 182S I OIL Oil Specification: MIL·L·6082 Aviation Grade Straight Mineral Oil: Used when the airplane was delivered from the factory and should be used to repleni sh the supply during the first 25 hours. This oil should be drained and the filter changed after the first 25 hours of operation. Refill the engine with MIL·L·6082 Aviation Grade Straight Mineral Oil and continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. MI L·L·22851 Aviation Grade Ashless Dispersant Oil: Oil conforming to Textron Lycoming Service Instruction No 1014, and all revisions and supplements thereto, must be used after first 50 hours or once oi l consumption has stabilized. Recommended Viscosity for Temperature Range: Temperature MIL·L·6082 MIL·L·22851 SAE Grade Ashless Dispersant SAE Grade Above 27 ' C (SO ' F) 60 60 Above 16' C (60' F) 50 40 or 50 · 1'C (30'F) to 32'C (90' F) 40 40 ·lS ' C (O ' F) to 21 ' C (70'F) 30 30,40 or 20W·40 Below ·12 ' C (10' F) 20 30 or 20W·30 · lS 'C (O ' F) . 32 ' C (90' F) 20W·50 20W·50 or 15W·50 All Temp eratures ._-- 15W·50 or 20W·50 NOTE When operating temperatures overlap, use the lighter grade of oil. Oil Capacity: Sump: 8 U .S. Quarts Total: 9 U .S. Quarts 1·6 Nov 15100 SECTION 1 GENERAL CESSNA MODEL 182S SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS KIAS KTAS Vs Vso 1-8 Knots Calibrated Airspeed is indicated airspeed corrected for position and instrument error and expressed in knots. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level. Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots. Knots True Airspeed is the airspeed expressed in knots re lative to undisturbed air which is KCAS corrected for altitude and temperature. Maneuvering Speed is the maximum speed at wh ich full or abrupt control movements may be used. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position . Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution. Never Exceed Speed is the speed limit that may not be exceeded at any time. Stalling Speed or the minimum steady fl i ght speed is the minimum speed at which the airplane is controllable. Stal ling Speed or the minimum steady f l ight speed is the minimum speed at which the airpl ane is controllable in the landing configuration at the most forward center of gravity. Feb 3/97 ~- CESSNA MODEL 182S Vx Vy SECTION 1 GE NERAL Best Angle-of-Climb Speed is the speed which re- sults in the greatest gam of altitude in a given hori- zontal distance. Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. METEOROLOGtCAL TERMINOLOGY OAT Outside Air Temperature is the fr ee air sta ti c temperature. It may be expressed in either degrees Celsius or degrees Fahrenheit. Standard Temperature Pressure Altitude Standard Temperature is 15'C at sea level press ur e al titude and decreases by 2 ' C for each 1000 feet of altitude. Pressure Altitude is the altitude read from an altim ete r when the altimeter's barometric scale has been set to 29 .9 2 inches of mercury (1013 mb). ENGINE POWER TERMINOLOGY BHP Brake Horsepower is the power developed by th e eng in e. RPM Rev olutions Per Minute is engine speed. Static Static RPM is engine speed atta in ed during a full RPM throttle engine runup when the airplane is on th e ground and stationary. MP Manifold Pressure is a pressure measured in th e engine's induct io n sys tem and is expressed in in ches of mercury (in Hg). SECTION 1 GENERAL CESSNA MODEL 182S AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demon- strated Crosswind Velocity Usable Fue l Unusable Fuel GPH NMPG g Course Datum Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing was actually demonstrated during certification tests. The value shown is not considered to be limiting. Usable Fuel is the fuel avai lable for flight planning. Unusable Fuel is the quantity of fuel that can not be safely used in flight. Gallons Per Hour is the amount of fuel consumed per hour. Nautical Miles Per Gallon is the distance which can be expected per ga ll on of fuel consumed at a specific engine power setting and/or flight configuration . g is acceleration due to gravity. Course Datum is the compass reference used by the autopilot, along with course deviation, to provide lateral control when tracking a navigation signal. C ...... h ') / 07 CESSNA MODEL 1828 SECTION 1 GENERAL WEIGHT AND BALANCE TERMINOLOGY Reference Datum Station Arm Moment Center of Gravity (C .G.) C.G. Arm C.G. Limits Standard Empty Weight Reference Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Station is a location along the airplane fuselage given in terms of the distance from the reference datum. Arm is the horizontal distance from the reference datum to the center of gravity (C .G.) of an item. Moment is the product of the weight of an item multiplied by its arm. (Moment divided by the constant 1000 is us ed in this handbook to simplify balance calculations by reducing the number of digits .) Center of Gravity is the point at which an airplane, or equipment, would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. Center of Gravity Arm is the arm obtained by adding the airplane's individual moments and dividing the sum by the total weight. Center of Gravity Limits are the extreme center of gravity locations within which the airplane must be operated at a given weight. Standard Empty Weight is the weight of a standard airplane, including unusable fuel, full operating fluids and full engine oil. Basic Empty Basic Empty Weight is the standard empty weight Weight plus the weight of optional equipment. Useful Load Useful Load is the difference between ramp weight and the basic empty weight. MAC MAC (Mean Aerodynamic Chord) is a chord of an imaginary re ctangu lar airfoil having the same pitching moments throughout the flight range as that of the actual wing. SECTION 1 GENERAL Maximum Ramp Weight Maximum Takeoff Weight Maximum Landing Weight Tare CESSNA MODEL 182S Maximum Ramp Weight is the maximum weight approved for ground maneuver, and includes the weight of fuel used for start, taxi and runup. Maximum Takeoff Weight is the maximum weight approved for the start of the takeoff ro ll. Maximum Landing Weight is the maximum weight approved for the landing touchdown. Tare is the weight of chocks, blocks, stands, etc. used when weighing an airplane, and is included in the scale readings. Tare is deducted from the scale reading to obtain the actual (net) airplane weight. CESSNA MODEL 182S SECTION 1 GENERAL METRIC {IMPERIAL { U.S. CONVERSION CHARTS The following charts have been provided to help international operators convert U.S. measurement supplied with the Pilot's Operating Handbook into metric and imperial measurements. The standard followed for measurement units shown, is th National Institute of Standards Technology (NIST), Publication 811, "Guide for the Use of the International System of Units (SI) ." Please refer to the following pages for these charts. Nov 15/00 1-13 SECTI ON 1 GENERAL CESSNA MODEL 182S (Kilograms x 2.205 =Pounds) (Pounds x .454 =K il ograms) KILOGRAM S IN TO POUNDS kg 0 1 2 3 4 5 6 7 8 9 lb. lb. lb. lb. lb. lb. lb. lb. l b. lb. 0 2.205 4.409 6.614 B.819 11.023 13.228 15.432 17.637 19.842 10 22.046 24,251 26.456 28.660 30 . 865 33 .069 35.274 37.479 39.683 41.888 20 44.093 46,297 48.502 50.706 52.9 1 1 55.116 57.320 59.525 61.729 63.934 30 66 .139 68.343 70.548 72.753 74 .957 77.162 79.366 81.571 83.776 85.980 40 88.185 90.390 92.594 94 .799 97 .003 99.208 101.41 103.62 105.82 108.03 50 110.23 112.44 114.64 116.85 119.05 121 .25 123.46 125.66 127.87 130.07 60 132.28 134.48 136.69 138.89 141.10 143.30 145.51 147.71 149.91 152,12 70 154.32 156.53 158.73 160.94 163.14 165.35 167. 55 169.76 171 .96 174.17 80 176.37 178 .57 180.78 182.98 185.19 187.39 189.60 191.80 194 .01 196.21 90 198.42 200.62 202 .83 205.03 207.24 209.44 211.64 213.85 216 .05 218.26 100 220.46 222.67 224.87 227.08 229.28 231.49 233.69 235.90 238.10 240.30 POUNDS INTO KILOGRA MS lb. 0 1 2 3 4 5 6 7 8 9 kg kg kg kg kg kg kg kg kg kg 0 0.454 0.907 1.361 1.814 2.268 2.722 3.175 3.629 4.082 10 4 .536 4.990 5.4 43 5.897 6. 350 6.804 7.257 7.711 8.165 8.618 20 9.072 9.525 9.979 10.433 10.886 11.340 11.793 12.247 12.701 13. 154 30 13 .608 14.06 1 14.515 14.969 15.422 15.876 16.329 16.783 17.237 17.690 40 18.144 18. 597 19.051 19.504 19.958 20.412 20.865 21.319 21 .772 22.226 50 22 .680 23.133 23.587 24 .0 40 24.494 24.948 25.401 25.855 26.303 26.762 60 27 .2 16 27.669 28. 123 28.576 29.030 29.484 29.937 30.391 30.844 31 .298 70 31 .752 32 .205 32.659 33 . 112 33.566 34.019 34.473 34.927 35.380 35 .834 80 36.287 36.741 37 .195 37.648 38.102 38.555 39.009 39.463 39.916 40 .370 90 40.823 41 .277 41.731 42 .184 42 .6 38 43 .091 43 . 545 43.999 44.452 44.906 100 45.359 45.813 46.266 46.720 47.1 74 47.627 48.081 48 . 534 48.988 49.442 Figure 1·2. Weight Conve rsions (Sheet 1 of 2) 1· 14 Nov 15/00 ~ CESS NA MODE L 182S SECTION 1 GENERAL (Kilograms x 2.205 = Pounds) - (Pounds x .454 = Kilograms) POUNDS KILOGRAMS 220 100 210 95 200 90 190 85 180 80 170 75 160 150 70 140 65 130 60 120 55 1 10 50 100 45 90 40 80 35 70 30 60 25 50 40 20 30 15 20 10 10 5 0 0 Units x 10, 100, etc . 0585T 10 27 -- Figure 1-2 . Weight Conversions (Sheet 2 of 2) June 13/97 1-15 SECTION 1 GENERAL CESSNA MODEL 182S (Meters x 3.281 = Feet) (Feet x .305 = Meter s) m a feet 0 .. . 10 32.808 20 65.617 30 98.425 40 131.23 50 164.04 60 195.85 70 229.66 80 262.47 90 295 .27 100 328.08 It a m 0 ... 10 3. 048 20 6. 096 30 9.144 40 12.192 50 15.240 60 18.288 70 21 . 336 80 24.384 90 27.432 100 30.480 1· 16 1 feet 3.281 36.089 68.897 10 1.71 134.51 167.32 200.13 232. 94 265.75 298 .56 33 1.36 1 m 0.305 3.353 6.401 9.449 12.497 15. 545 18.593 21 .641 24.689 27.737 30 .785 __ METERS INTO FEET METRES EN PIEDS 2 3 4 5 feet feel l eel feet 6.562 9.8 42 13.123 16.404 39.370 42.651 45 .932 49 .212 72.178 7 5.4 59 78.740 82.0 21 104.99 108.27 111 .55 114. 83 137.79 141.08 144.36 147.64 170.60 173.86 177.16 180.45 203.41 206.69 209 .97 213.25 236.22 2 39 .50 242 .78 246.06 269 .03 272.31 275.59 278.87 301.84 305.12 308.40 311 .68 334.64 337.93 341 . 21 344.49 __ FEET INTO METERS PIEDS EN METRES 2 3 4 5 m m m m 0.610 0.914 1.219 1.524 3.658 3.962 4.267 4.572 6.706 7.010 7. 315 7.620 9.754 10.058 10.363 10.668 12.802 13.106 13.411 13.716 15.850 16.154 16.459 16.754 18.898 19.202 19.50 7 19.812 21.946 22.250 22.555 22. 860 24.994 25.298 25.603 25.908 28.042 28 . 346 28.651 28.956 31 .090 31.394 31.699 32 .004 6 7 8 9 feet feet feet feet 19 .685 22.9 56 26 .247 29 .528 52.493 55.774 59.055 62.336 85.302 88 ,582 91.863 95.144 118 . 11 121.39 124 .67 127 .95 150.92 154 .20 157.48 160.76 183.73 187.01 190.29 193.57 216.53 2 19.82 223.10 226.38 249 . 34 252 .62 255.90 259.19 282 .15 285.43 288. 7 1 291.58 314 .96 318 .24 321 .52 324.80 347 .77 351.05 354.33 357.61 6 7 8 9 m m m m 1.829 2.134 2.4 38 2.743 4.877 5.182 5.486 5.791 7.925 8 .2 30 8.534 8.839 10.973 11. 278 11.582 11 .887 14.021 14 . 326 14.630 14.9 35 17.069 17. 374 17.678 17.983 20.117 20 .422 20.726 21.031 23.165 23. 470 23.774 24.079 26. 213 26.518 26.822 27 .127 29.261 29.5 66 29. 870 30 .175 32 . 309 3 2.6 14 32 .918 33 .223 Figure 1- 3. Length Conversions (S heet 1 of 2) Nov 15100 CESSNA SECTION 1 MODEL 182S GENERAL (Meters x 3. 281 = Feet) (Feet x .305 = Meters) FEET METERS 100 ,320 95 300 90 280 85 260 80 240 75 70 220 65 200 60 180 55 160 50 45 140 40 120 35 100 30 80 25 20 60 15 40 10 20 5 0 0 Units x 10, 100, etc. Figure 1- 3. Length Conversions (Sheet 2 of 2) Nov 15100 1- 17 SEC TI ON 1 GENERAL CESSNA MODEL 182S (Centimeters x .394 = Inches) (Inches x 2.54 = Centimeters) .... CENTIMETERS INTO IN CHES em a 1 2 3 4 5 6 7 8 9 in. in. in. i n. in. in. in. in. in. in. 0 --- 0.394 0.787 1.181 1.575 1.969 2.362 2.756 3.150 3.543 10 3. 937 4 .331 4 . 724 5.118 5.512 5.906 6.299 6.693 7.087 7.480 20 7.874 8.268 8.661 9.055 9.449 9.843 10.236 10.630 11 . 024 11 .417 30 11.811 12.205 12.598 12.992 13.386 13.780 14.173 14.567 14.961 15.354 40 15.748 16. 142 16.535 16.929 17.323 17.717 18.110 18.504 18.898 19.291 50 19 .685 20,079 20.472 20.866 21.260 21.654 22.047 22.441 22.835 23 .228 60 23.622 24.016 24.409 24.803 25.197 25.591 25.984 26.378 26.772 27 . 164 70 27.559 27 .953 28.346 28.740 29.134 29.528 29.921 30.315 30.709 31.102 80 31.496 31 .890 32.283 32.677 33.071 33.465 33.858 34.252 34.646 35 .039 90 35.433 35.827 36.220 36 .614 37.008 37.402 37 .795 38.189 38 . 583 38 .976 100 39 .370 39 .764 40 .1 57 40.551 40.945 41.339 41.732 42.126 42 . 520 42.913 .... INCHES INTO CENTIMETERS in. a 1 2 3 4 5 6 7 8 9 em em em em em em em em em em 0 2.54 5.08 7.62 10. 16 12.70 15.24 17.78 20.32 22. 96 10 25.40 27.94 30.48 33.02 35 .56 38 .10 40 .64 43 .18 45.72 48 .26 20 50.80 53.34 55.88 58.42 60.96 63.50 66.04 68.58 71. 12 73 .66 30 76.20 78.74 81 .28 83.82 86.36 88.90 91.44 93.98 96.52 99.06 40 101 .60 104. 14 106.68 109.22 111 .76 114. 30 116.84 119.38 121.92 124.46 50 127.00 129.54 132.08 134.62 137.16 139.70 142.24 144.78 147.32 149.86 60 152.40 154.94 157.48 160.02 162.56 165.10 167.64 170.18 172.72 175. 26 70 177.80 180.34 182.88 185.42 187.96 190.50 193.04 195_58 198.12 200 .66 80 203.20 205.74 208. 28 210.82 213.36 215.90 218 .44 220.98 223.52 226 . 06 90 228.60 231.14 233.68 236.22 238.76 241.30 243.84 246.38 248.92 251.46 100 254.00 256.54 259.08 261 .62 264.16 266.70 269 .24 271.78 274.32 276.86 Fi gure 1-4_ Length Conversions (Sheet 1 of 2) 1-18 Nov 1 5/00 '~ CESSNA MODEL 182S SECTION 1 GENERAL (Centimeters x .394 = Inches) - (Inches x 2.54 = Centimeters) INCHES CENTIMETERS 10 25 24 9 23 22 21 8 20 19 7 18 17 16 6 15 14 5 13 12 11 4 10 9 3 8 7 6 2 5 4 Units x 10, 100, etc. 3 2 0585 T1 028 0 0 __ Figure 1-4. Length Conversions (Sheet 2 of 2) June 13/ 97 1-19 SEC TI ON 1 CESSNA GENERAL MO DEL 182S (Statute Mile s x l .609=KHometers) (Kilo meters x.622=S tatute Miles) (S tatute Miles x.869 =Nautica l Miles) (Nautical Miles x 1.1 5=Stat ute Mil es) (Nautical Mi les xl .852=K il ometers) (K ilo meters x. 54 =Nautical Mil es ) STATUTE NAUTICAL MILES MILES KILOMETERS 115 100 100 110 95 180 95 105 90 90 170 100 85 85 160 95 150 90 80 80 85 75 75 140 80 70 70 130 75 65 65 120 70 60 60 110 65 55 55 100 60 50 50 90 55 50 45 45 80 45 40 40 70 40 35 35 60 35 30 30 30 25 25 50 25 20 20 40 20 30 15 15 15 10 10 20 10 Un its x 10, 100, etc. 5 5 5 10 0 0 0 0 ; 0585T1029 Figure 1-5. Distance Conversions 1- 20 Nov 15/ 00 CESSNA MODEL 182S SECTION 1 GENERAL (Imperial Gallons x 4 .546 = Liters) (Li te rs x .22 = Imperial Gallons) LITERS INTO IMPERtAL GALLONS __ Lt 0 1 2 3 4 5 6 7 8 9 IG IG IG IG IG IG IG IG IG IG 0 ... 0. 220 0.440 0. 660 0. 880 ' .100 1 .320 1. 540 1.760 1. 980 10 2.200 2.420 2. 640 2. 860 3. 080 3.300 3. 520 3.740 3 .960 4.180 20 4.400 4. 620 4 . 840 5.059 5.279 5.499 5.719 5.939 6.159 6.379 30 6.599 6.819 7.039 7. 259 7.479 7.699 7.919 8 .139 8.359 8.579 40 8.799 9.019 9.239 9.459 9.679 9.899 10 . 119 10.339 10. 559 10. 779 50 10.999 11.219 11.439 11 .659 11 .879 12.099 12.319 12.539 12.759 12.979 60 13. 199 13.419 13.639 13. 859 14.078 14.298 14.518 14 . 738 14.958 15.178 70 15. 398 15. 618 15 . 838 16.058 16.278 16.498 16.7 18 16.938 17.158 17.378 80 17 . 598 17.818 18. 036 18.258 18.478 18.698 18.918 19. 138 19.358 19.578 90 19.798 20.018 20.238 20.458 20.678 20. 898 21. 118 21 .338 21.558 21.778 100 21.998 22.218 22.438 22.658 22 .878 23 .098 23 .318 23.537 23.757 23.977 IMPERIAL GALLONS INTO LITERS __ IG 0 1 2 3 4 5 6 7 8 9 Lt Lt Lt Lt Lt Lt Lt Lt Lt LI 0 -- . 4. 546 9.092 13.638 18.184 22.730 27.276 31.822 36 . 368 40 .914 10 45.460 50. 006 54.552 59. 097 63.643 68 .189 72 .735 77.281 81.827 86 . 373 20 90.919 95.465 100.01 104 .56 109 .10 113.65 118.20 122 .7 4 127. 29 131.83 30 136.38 140.93 145.47 150.02 154.56 159. 11 163.66 168.20 172. 75 177.29 40 181.84 18G . 38 190.93 195.48 200 .02 20 4.57 209 . 11 213.66 218.21 222.75 50 227 . 30 231.84 236.39 240.94 245.48 250.03 254.57 259. 12 263 .67 268.21 60 272.76 277 . 30 28 1.85 286.40 290 .94 295.49 300 .03 304.58 309 .13 313 .67 70 318.22 322.76 327.31 331 . 86 3364 0 340 .9 5 345.49 350 .04 354 .59 359 .13 80 363.68 368 .22 372. 77 377 . 32 381.86 386.41 390.95 395.50 400 .04 404.59 90 409 .14 413.68 418.23 422.77 427 . 32 43 1. 87 436.41 440.96 445.50 450. 05 100 454 .60 459 .14 463.69 468 .23 472. 78 477 . 33 481.87 486.42 490.96 495.51 Figure 1-6. Volume C on versions (Sheet 1 of 3) Nov 15/00 1-21 SECTION 1 GENERAL -- (Imperial Gallons x 4.4546 = Liters) ( Li ters x .22 = Imperial Gallons) 100 IMPERIAL 440 LITER SGALLONS 95 420 90 400 85 380 80 360 75 340 70 320 65 300 60 280 260 55 240 50 220 45 200 40 180 35 160 30 140 25 120 20 100 80 15 60 10 40 5 20 0 0 Un i ts x 10, 100, etc. CESSNA MODEL 182S .... 0585 T10 32 Figure 1-6. Volume Conversions (Sheet 2 of 3) 1-22 Nov 15/00 CESSNA MODEL 182S (Imperial Gallons x 1.2 = U .S. Gallons) (U.S. Gallons x .833 = Imperial Gallons) (U. S. Gallons x 3.785 = Liters) ~ (Liters x .264 = U.S. Ga llons) SECTION 1 GENERAL IMPERIAL U. S. LI TERS 120 GALLONS 100 GALLONS 100 ~ 95 1 15 95 360 90 11 0 90 340 105 85 100 85 320 80 95 80 300 75 90 75 280 70 85 70 260 65 80 65 75 240 60 70 60 220 55 65 55 200 50 60 50 180 45 55 45 50 160 40 40 45 140 35 40 35 30 30 120 35 25 30 25 100 20 25 20 80 15 20 15 60 15 10 40 10 10 5 5 5 20 0 0 0 0 Units x 10, 100, etc. 0585T1 033 Figure 1-6. Volume Conversions (Sheet 3 of 3) Nov 15100 1-23 SECTION 1 GENERAL --1-24 TEMPERATURE CONVERSIONS CESSNA MODEL 182S (' F-32) x 5/9 ='C ' C x 9/5 + 32 =' F ' F ·c ' F · C -40 -40 320 160 -30 340 -20 -30 360 180 - 10 380 O. -20 4 00 20 0 10 -1 0 4 20 22 0 20 440 30 0 460-. 240 40 480 50 10 5 00 2 60 60 520 70 : 20 280 80 : 30 300 90 -, 100 - 40 320 110 62 120 50 640 340 130 660 140 60 680 360 150 . 700 160-: 70 720 . 380 170 . 74 180 : 80 7 60 400 1 90- 90 780 . 420 200 . 800 210 : 100 820 440 220- 840 230 110 860 . 460 240 - 880 250 120 900 480 260 920 270 130 940 500 280 140 960 520 290 980 300 150 1000 540 310 1020 320 160 1040 560 OSBS T 1034 Figure 1-7. Temperature Conversions June 13/ 97

All CESSNA 182S SKYLANE pilot's operating handbook