Airplane Flight Manual
CESSNA 170B · Flight Manual
Overview
This Airplane Flight Manual (AFM) is specifically designed for the Cessna 170B, providing essential information for pilots operating this aircraft. It includes detailed sections on aircraft specifications, performance data, operating procedures, and safety information. The manual serves as a comprehensive guide for both new and experienced pilots, ensuring they have the necessary knowledge to operate the Cessna 170B safely and efficiently. Key topics include weight and balance, fuel requirements, and emergency procedures, all tailored to the unique characteristics of the Cessna 170B.
- Maximum takeoff weight: 2,400 lbs
- Stall speed: 50 knots
- Cruising speed: 120 knots
- Rate of climb: 700 feet per minute
- Service ceiling: 14,000 feet
Document
Source
Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 138
- File size
- 12 MB
- Publisher
- www.aeroelectric.com
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In this document
Aircraft Specifications
The Cessna 170B features a high-wing design with a wingspan of 36 feet 0 inches and a length of 24 feet 0 inches. The maximum takeoff weight is 2,400 lbs, with a useful load of approximately 1,200 lbs. The aircraft is powered by a Continental O-300 engine, producing 145 horsepower.
Performance Data
The Cessna 170B has a stall speed of 50 knots and a maximum cruising speed of 120 knots. The rate of climb is approximately 700 feet per minute, and the aircraft has a service ceiling of 14,000 feet. The landing distance over a 50-foot obstacle is about 1,600 feet.
Operating Procedures
Pilots should perform a thorough preflight inspection, including checking fuel levels, oil quantity, and control surfaces. The recommended fuel type is 100LL avgas. The engine start procedure involves setting the throttle to 1/4 open and engaging the starter while monitoring engine gauges.
Emergency Procedures
In the event of an engine failure during takeoff, pilots should maintain control of the aircraft and attempt to land straight ahead. If an emergency landing is necessary, the best glide speed is 65 knots. Pilots should also be familiar with the use of the fire extinguisher located in the cockpit.
Weight and Balance
Proper weight and balance calculations are crucial for safe flight. The center of gravity limits for the Cessna 170B are between 34.0 inches and 39.0 inches from the datum. Pilots must ensure that the aircraft is loaded within these limits before flight.
Safety notes
- Always perform a preflight inspection before each flight.
- Ensure weight and balance calculations are within limits.
- Be familiar with emergency procedures and locations of safety equipment.
Full document text
TEMPORARY REVISION NUMBER 2 DATED 27 JANUARY 1995 RECEIVED SEP 15 1997 5 1997 R9 71253. MANUAL TITLE MODEL 170B SERIES PARTS CATALOG (1952 THRU 1956) MANUAL NUMBER - PAPER COPY P108-12 AEROFICHE P108-12AF TEMPORARY REVISION NUMBER - PAPER COPY P108TR2-12 AEROFICHE NA MANUAL DATE 1 SEPTEMBER 1956 REVISION NUMBER NA DATE NA This Temporary Revision consists of changes to the subject Parts Catalog and replaces all previously issued Revision Sheets. Pen and ink changes should be made to the paper copy of the manual and supersede the aerofiche information. NOTE The "R" located in the first column, of the revision sheet(s), indicates changes that have occurred since the issuance of the previous Revision Sheets and/or Temporary Revision text pages. PAGE 12345 FICHE/FRAME A02 A03 A04 A05 A06 REASON FOR TEMPORARY REVISION To incorporate later parts information changes to the Parts Catalog. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For paper publications: After making pen and ink changes to the Parts Catalog Pages as noted on the attached revision sheet(s) and/or Temporary Revision Text pages; file this cover sheet and the revision sheets behind the publications title page to identify the inclusion of the Temporary Revision into the manual. For aerofiche publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. This will be a visual identifier that information in the frame (page) is no longer valid and the Temporary Revision should be referenced. Temporary Revisions should be collected and maintained in a notebook near the aerofiche library for quick reference. COPYRIGHT © 1995 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA Page Fig. Index CESSNA AIRCRAFT COMPANY MODEL 170B SERIES (1952-1956) PARTS CATALOG REVISION SHEET CHANGE REMARKS No. No. No. FROM 20 R 5 10 R 6 R 00 6 R 6 R 6 R Co R 6 R 8 22233363 R 8 3 R 9 4 RRR 10 13 R 16 RR 18 19 21 R 21 R 200 20 21 RRR R 31 31 DESPOT≈≈22222222255333333333 10 6 8 00 8 10 10 10 RRR 2112212222232212225672222069665222223342 0523005 NAS383-3 ΤΟ 0523005-58 S378-3L NAS383-2 0523005 0523508-4 S378-2 0523005-58 0523508-8 0523400-14 0523400-18 0523516-5 0720608-7 0523234-2 0720005-1 Not Listed 0523004-11 "Right" 0523007-2 0523811 0523005-21 0523811-1 0523914-2 0523914-0 0523400-15 0523234-2 0523400-19 0720005-1 0523007-1 F34-14 0523811-1 0523812 0523914-2 0523606-11 KS4 AR4-1 R R 24 R 24 R 24 R 24 R 27 14 27 14 R 20 27 14 27 14 1992-2222111166112222222222 0523005-2 0523609 AN426AD10 0523613-1 AN426AD10-30 0532005-2 0332136-4 0332136-3 Not Listed 52-3-551 Not Listed 52-3-551 MS27645-4 0523005-22 S1819-3 0523811-0 0523812-3 0523914-0 0523606-10 0523606-12 0523606-13 MS24462-4 17 49390 S878-1 R RR R 34 37 37 18 0511000-24 Refer to Notes, Page 0510114-20 0791300-5 0510113-3 0510113-5 37 0510114-21 0791300-6 39 20 0513009-2 LH 0513009-2 RH 39 20 0513009-3 RH 39 20 0510114-20 0513009-3 LH 0791300-5 39 20 0510114-21 0791300-6 41 0411129- S204 41 0713495-19 0713495-63 41 0713495-51 0713495-21 Please update your parts catalog as shown above. P108-12 Temporary Revision Number 1 27 January 1995 Page 1 Page Fig. Index CESSNA AIRCRAFT COMPANY MODEL 170B SERIES (1952-1956) PARTS CATALOG REVISION SHEET CHANGE REMARKS No. No. No. FROM TO GGGGG RRR 41 21 41 21 41 21 41 21 41 21 R 41 21 R 20 41 21 20 R 43 R 45 R 20 R R RRRR ༠:༠:ག:གྲ:ག:3:5:ཆེ 45 49 52 57 57 57 61 61 63 R 20 23 63 63 ~~~~~~22222255533338 54 55 56 56 56 57 ཐག་ཐག :g| 0713495-26 0713495-18 0713495-18 0713495-26 0713495-20 0713495-64 0713495-4 0713495-8 56 0713495-58 0713495-18 0713495-5 0742115-25 0713495-52 0713495-60 11 0311001-27 S350 1 0591200-56 0512000-36 27 31 31 31 34 34 34 11221222324 18 0512000-73 0512000-79 0512154-1 No Longer Available 29 0541117-12 95-23482 0311710 0311710-6 16 Refer to Notes, Page 6 59-022-044-37S 59-022-094-375 26 0511227 0511227-4 58 0511106-105 S1005-84 0511106-91 0511227-1 0511106-142 0511227-5 46 0511106-105 S1005-84 RR 63B 34A 3 0511106-151 0511106-164 63B 34A R 63B 34A 222 65 35 65 35 65 35 333 R 67D 36A 69 37 RR 73 41 R 73 41 RR 73 41 75 42 12222424675 10 0511106-158 0511106-166 0511227-1 0511227-5 Refer to Notes, Page 6 Refer to Notes, Page 6 28 Refer to Notes, Page 6 20 0500103-40 0411090-3 0411086-10 05001003-60 0411090-1 0411086-15 0411008-2 0713068-2 0411087-23 0450017-10 13 0411090-12 0411090-8 75 42 15 0411090-9 0411090-7 R 75 42 42 75B 75B 42A 42A 75D 42B RR 77 44 77 44 79 46 83 48 66232420 16 0411090-10 0411090-22 16 0411090-8 0411090-22 13 0411090-8 10 R 37 A1181-6Z-3 0411086-10 0411008-2 0411098-6 0552002-1 0411090-22 NAS446-2 0411086-15 Please update your parts catalog as shown above. 0713068-2 DM 7653 0552002-68 Page 2 P108-12 Temporary Revision 1 27 January 1995 CESSNA AIRCRAFT COMPANY MODEL 170B SERIES (1952-1956) PARTS CATALOG REVISION SHEET Page Fig. Index CHANGE REMARKS No. No. No. FROM 83 48 11 0552002-2 TO 0552002-71 RRR 83 83B 85 87 R 87 87 87 91 R 91 93 94 R 97 100 R 105 R 106 107 R 107 107 107 R 107A 107B 107B R 109 R 109 RR 109 109 109 R 109 R 109 R 111 R 111 R 113 R 113 R 113 R 113 R 113A R 113A 117 8:ཅྀ::⌘༠;༠:ཝཿཝ ཝཝཿ::8: 2222222222222222222222223677222222222 48 26 0552002-51 0595000-6 48A 11 0552002-71 0552002-68 49 14 0550158 50 11 S-51-10-12 50 13 0550159 50 35 0450320-29 50 36 0450320-28 No Change S1104-3 S51-10 0550179-1 No Change Add: Order AD79-9-2 (Bulk) Add: Order 9AX11-2 (Bulk) 52 Not Listed SK170-1 52 11 0450171 0550117 53 Not Listed SK170-2 54 57 59 WANN 22 0450320 0450320-16 Order AD79-9-2D (Bulk) 22 035112-8 035112-5 4 AN515-10R8 1024X1/2 37 0511191 0511191-1 64 7 AF934-5 M829513-10 65 5 A114 S378-4 65 12 BB-208 S378-3L 65 17 BB-208 S378-3L 65 27 65 65A 65A 66 66 66 66 66 66 66 22342225345 #6 #6 S338-10 S338-10 Deleted 0311323-4 Chain Deleted 0742200-6 Clip 15 NAS383-4 S378-4 19 AN210-4B S378-4 26 AN210-4B S378-4 31 AN210-4B S378-4 AN210-4B S378-4 F-140 S394 51 NAS383-3 S378-3L 11 NAS383-3 S378-3L 68 78 17 NAS383-3 S378-3L 30 AN163-16L AN165-16RL 68 35 NAS383-2 S378-2
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68 47 AN210-2B S378-2 68 53 AN383-2 S378-2 68 69 NAS43HT-5-36 NAS42HT-5-36 68 70 70 223 NAS42DD-4-16 NAS42-4-16 28 0411021-1 0712603-1 R 117A 70A 3 124E 72B 22 0411062-2 0500027-1 0411062-4 0500027-4 Cessna R Please update your parts catalog as shown above. P108-12 Temporary Revision Number 1 27 January 1995 Page 3 Page Fig. Index CESSNA AIRCRAFT COMPANY MODEL 170B SERIES (1952-1956) PARTS CATALOG REVISION SHEET CHANGE REMARKS No. No. No. FROM 124E 72B 22 Not Listed TO 0500027-5 |(170) 133 76 R RR 135 77 135 139 77 79 140 80 143 82 143 82 143 82 150 89 RR RR RR 153 91 153 93 153 93 155 94 155 94 R 155 94 R 157 95 157 95 157 95 157 95 157 95 157 95 157 95 R 157 95 157 95 157 95 158 95 158 95 RRRRR 158 95 159 97 159 97 g:༠:༠:8:8;8:ཞ:ཞ:8:8;::8:ū:8;8:➢;:;:: 8:8;dཔས 2212-22213- 24 Refer To Notes, Page 6 30 0513004-26 0513004-10 Not Listed 05130004-26 9 0513004-26 0552001-60 0513004-10 0513004-10 0513004-10 No Change Add:3rd Col, above Card-Com. 24 AN515-8R5 No Change 25 AN365-832 53-3-832 No Change 52-3-832 Add, in Desc: Not Part of Kit Add, in Desc: Not Part of Kit Add, in Desc: Not Part of Kit 0511231-19 AN2552-2 0511231-140 AN2552-3A 19 20 69 2722512222226DORF 0513034-1 0513034-2 0442010-2 0442010-36 24 0442006-21 0442006-11 0442006-22 0442006-11 MS28741-4-010 S1167-4-0100 14 0441150-8 No Change Delete: "Tire" Description 19 0441150-9 0541116-37 0541116-38 No Change Delete: "Tire" in Description No Longer Available No Longer Available 6:00 X 6 0441016-24 (1st Column) 6:00 X 6 0441016-13 (1st Column) 30 C2311-27 0341005-66 0541116-41 0541116-42 0541117-7 95-30593 95-5383 0541116-36 70 #10-24NCX7/8 95-5163 AN936C10 95-5163 AK70B52-1 AK70B53-4 AK7054-1 AK8053-13 161 100 1 0441143-12 0441143-50 161 100 8 0441143-13 0441143-51 Please update your parts catalog as shown above. Page 4 P108-12 Temporary Revision 1 27 January 1995 PG Figure 34 18 CESSNA AIRCRAFT COMPANY MODEL 170B SERIES (1952-1956) PARTS CATALOG REVISION SHEET NOTES Index No. P/N 6 P/N 0511000-24 57 31 16 65 35 26 65 89 35 27 65 35 28 133 76 24 0500101-45 0500102-45 Remarks: Cap only. Refer to Page 104, Figure 63, Item #1, for vent system. Change Serial 26039 thru 26054 to read 26039 thru 26300. Change Serial 26505 thru 26995 to read 26301 thru 26995. Change Serial 25372 to 20524, and "& on " to "thru 25372". Change Serial 25372 to 20524, and " & on to "thru 25372. " Change Serial 25372 to 20524, and " " & on to "thru 25372. Use 2each AN844-6D elbow 1 each S51-6-13 hose 2 each NAS 397-12 clamp Please update your parts catalog as shown above. Page 5 P108-12 Temporary Revision Number 1 27 January 1995 TEMPORARY REVISION NUMBER 1 RECEIVE DATED 5/01/92 SEP 1997 R 9 7 125 3 MANUAL TITLE MODEL 170B SERIES PARTS CATALOG (1952 THRU 1955) MANUAL NUMBER - PAPER COPY P108-12 AEROFICHE P108-12AF AEROFICHE N/A DATE TEMPORAARY REVISION NUMBER - PAPER COPY P108TR1-12 MANUAL DATE OCTOBER 1954 REVISION NUMBER This Temporary Revision consists of the following pages, which effect and replace existing pages in the paper copy manual and supersede aerofiche information. PAGE 21 FICHE/FRAME 1 C8 REASON FOR TEMPORARY REVISION To correct part number of Aileron Push Pull Rod End FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For paper publications: File this cover sheet behind the publication's title page to identify the inclusion of the Temporary Revision into the manual. Insert the new pages into the publication at the appropiate location(s) and remove and discard the superseded pages. For aerofiche publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. This will be a visual identifier that the information in the frame (page) is no longer valid and the Temporary Revision should be referenced. Temporary Revisions should be collected and maintained in a notebook near the aerofiche library for quick reference. COPYRIGHT CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1992 ફ્ T P108-12 Temporary Revision 1 1 May 1992 Cessna ILLUSTRATED PARTS CATALOG 21 FIGURE AND UNITS DESCRIPTION PARTS NUMBER INDEX ASSY NO. 10- No Number -2 74945459 0523223-1 Allaros Installation - Right wing (see figure 7 for NHA) Bellcrank Assembly - Aileron (0523800 Ref). Ref 1 0422280 Bushing B610x 0522629 AN4-42A AN365-428 0523221 0523222 0523218 -9 0523218-2 -10 S1819-3 -11 AN316-4R -13 AN3-7A -13 AN365-1032 -14 NAS229-8 -15 AN365-1032 -16 0523800-1 -17 0523806-1 -18 0523808-2 -19 0523809-1 -20 0523810 -21 0523811-1 -23 0523812 -23 -24 0523814 0721109 0523800-7 NAS-445-163C-48 0523814-2 0523800-0 0523800-11 Bearing - Torrington Washer . Bolt - (Attach bellcrank) Nut - (Attach.bellcrank) Bushing (Attach bellcrank) Bushing-Bellcrank stop Rod Assembly - Allaron push-pull Rod - Alleron push-pull Ead - Rod Net - Check Bolt - (Attach aileron push-pull rod) Not - (Attach aileros push-pull rod) Screw - (Attach aileron hinge to wing) Not - (Attach allaron hinge to wing) Alleroa Assembly - Right wing Spar - Right aileron Rib #1-Aileron. Rib 2-Right ailaron (not available for spares) Rib #3 - Alleros (not available for spares) Rib #4 - Aileron. Brackst-Control Rivet - (Attach bracket) Bracket - (Attach aileron weight) Bracket - (Attach aileron weight) Weight-Allaron balance Skin - Upper right inboard (not available for spares) Upper right outboard min-Lower right inboard (not available for spares) Skin - Lower right outboard 2. R 2 2 12 12 • • • 0523800-18 -31 0523813-1 cer -33 0529813-8 Spacer -33 0523813-6 Spacer • • • • -34 0523813-7 Spacer -35 0523807 Hinge Assembly - Alleros ORDER BY PART NUMBER AND NAME SERIAL NUMBER AND COLOR IF APPLICABLE 22 Cessna ILLUSTRATED PARTS CATALOG 15 17 0000 31 FIGURE 11. RIGHT FLAP INSTALLATION (10) 24 30 (17) 15 MK8958- CessnaⓇ RECEIVED OFF TO 1997 КУ 7 1 25 3 PARTS CATALOG REVISIONS P108-12 REFERENCE CATALOG NUMBER: CATALOG TITLE: 170B TO: All Distributors and Dealers FROM: CAT. PAGE FIG. INDEX 170B 107 65 55 Service Parts Center TO ELIMINATE SHIPMENTS OF INCORRECT PARTS, PLEASE CORRECT YOUR CATALOG IMMEDIATELY AS SHOWN BELOW. CHANGE FROM ΤΟ 27 NO6 S338-10 Fairlead Feb. 26, 1971 DATE: REMARKS Form 924 The Cessna Aircraft Company Wichita, Kansas Model 170 (P108-12) Feb 16, 1965 Catalog Revisions PLEASE CORRECT CATALOG AS SHOWN BELOW CHANGE REMARKS Cat. Page Fig. Index FROM TO 170 39 39 2 20 20 26 0513009-2 26 0513009-3 Change from Left to Right Change from Right to Left TO ELIMINATE SHIPMENTS OF INCORRECT PARTS PLEASE CORRECT CATALOGS IMMEDIATELY.
What's in the CESSNA 170B 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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