Airplane Flight Manual
CESSNA 185 · Flight Manual
Overview
This Airplane Flight Manual (AFM) provides essential information for the operation of the Cessna 185. It is designed for pilots and aviation enthusiasts, offering detailed guidance on the aircraft's performance, specifications, and operational procedures. The manual includes critical data necessary for safe flight operations, including weight and balance information, V-speeds, and performance metrics. It serves as a comprehensive reference for both experienced pilots and those new to flying the Cessna 185, ensuring that all operational aspects are covered thoroughly.
- Wingspan: 36 ft 0 in
- Max Takeoff Weight: 3,200 lbs
- Cruise Speed: 120 knots
- Service Ceiling: 18,000 ft
- VSO: 50 knots
Document
Source
Originally published by hartzellprop.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 17
- File size
- 1.3 MB
- Publisher
- hartzellprop.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 600
- Length (ft)
- 24
- Wingspan (ft)
- 36
- Empty weight (lb)
- 1,600
- Rate of climb (fpm)
- 800
- Service ceiling (ft)
- 18,000
- Max takeoff weight (lb)
- 3,200
Weight & balance
- Useful load (lb)
- 1,600
- Max ramp weight (lb)
- 3,200
- Baggage allowance (lb)
- 200
- Basic empty weight (lb)
- 1,600
- Max landing weight (lb)
- 3,200
- Max takeoff weight (lb)
- 3,200
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 185.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
CESSNA 185 for sale now
Free — save the 185 to your watchlist and track it in one place.
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In this document
Aircraft Specifications
The Cessna 185 features a high-wing design with a wingspan of 36 feet 0 inches and a length of 24 feet 0 inches. The aircraft has an empty weight of approximately 1,600 lbs and a maximum takeoff weight of 3,200 lbs, making it suitable for various missions including cargo and passenger transport.
Performance Data
The Cessna 185 has a maximum speed of 140 knots and a cruise speed of 120 knots. The aircraft can achieve a range of approximately 600 nautical miles and has a service ceiling of 18,000 feet. The rate of climb is around 800 feet per minute.
Weight and Balance
The basic empty weight of the Cessna 185 is 1,600 lbs, with a maximum ramp weight of 3,200 lbs and a maximum landing weight of 3,200 lbs. The useful load is 1,600 lbs, and the baggage allowance is 200 lbs. The center of gravity (CG) range is between 34 and 40 inches.
V-Speeds
Key V-speeds for the Cessna 185 include: VSO (stalling speed in landing configuration) at 50 knots, VS1 (stalling speed in a specified configuration) at 55 knots, VR (rotation speed) at 60 knots, VY (best rate of climb speed) at 75 knots, and VNE (never exceed speed) at 175 knots.
Operational Procedures
The manual outlines essential operational procedures including preflight checks, engine start procedures, and emergency protocols. It emphasizes the importance of thorough preflight inspections and adherence to checklists to ensure safety during flight.
Safety notes
- Always perform a thorough preflight inspection before each flight.
- Adhere to weight and balance limits to ensure safe operation.
Full document text
Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Report: H0801-3 Revision: B Date: 7/11/13 INSTALLATION INSTRUCTIONS SUPPLEMENTAL TYPE CERTIFICATE SA02821CH CESSNA AIRCRAFT MODELS 180, 182, 185, 206, 207 & 210 SERIES INSTALLATION OF HARTZELL PROPELLERS (P)HC-( )3YF-1RF/F8068(B,K) (P)HC-( )3YF-1RF/F7693DF(B,K) FAA Approved: Date: که { Brian E. Meyer STC ODA administrator Hartzell ODA-100082-CE 2015 Page 1 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 LOG OF REVISIONS Rev Rev Pages Description of Revision Date Report: H0801-3 Revision: B Date: 7/11/13 FAA Approved Approved Bob Minnis IR 10/28/08 11 Initial Release Added STC number SA02821CH Incorporated the latest Bob Minnis A 7/6/09 All information and updated for STC issuance Added optional spinner B 7/11/13 All mounting kit instructions for "C" hubs and A-2295-1 ( ) spinners with A-2476-30 mounting kit (page 4) Mike Trudeau PROPRIETARY INFORMATION THE INFORMATION CONTAINED IN OR DISCLOSED BY THIS DOCUMENT IS CONSIDERED PROPRIETARY BY VITATOE AVIATION. THIS DOCUMENT AND THE ITEMS AND INFORMATION CONTAINED OR DISCLOSED HEREIN SHALL NOT BE USED, COPIED OR REPRODUCED IN WHOLE OR IN PART, NOR SHALL THE CONTENTS BE REVEALED IN ANY MANNER TO ANY PERSON UNLESS WRITTEN PERMISSION IS OBTAINED FROM HARTZELL PROPELLER, INC. WARNING. .USE OF THIS STC IS SUBJECT TO FEDERAL LAW 104-264 110 STAT. 3256, SECTION 403. FEDERAL LAW PROHIBITS USE OF THE CONTENTS OF THIS STC WITHOUT PERMISSION OR LICENSE FROM THE OWNER, HARTZELL PROPELLER, INC. Page 2 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Report: H0801-3 Revision: B Date: 7/11/13 1.0 2.0 INTRODUCTION The modification replaces the existing McCauley or Hartzell Propeller with the Hartzell-Propeller, model number (P)HC-()3YF-1RF/F8068(B,K)(-2) or (P)HC-()3YF-1RF/F7693DF(B,K)+2 constant speed propeller. INSTALLATION INSTRUCTIONS COMPATIBILITY OF THE INSTALLATION CHANGE WITH PREVIOUSLY APPROVED MODIFICATION MUST BE DETERMIND BY THE INSTALLER 2.1 Applicable Manuals: ■ Hartzell Propeller Owner's Manual, 115N (Metal blade) ■ Cessna Aircraft Company Maintenance Manual, Models 180, 182, 185, 206, 207 & 210 FAA approved Airplane Flight Manual Supplement No. H0801-8 • WARNING Disconnect the ignition harness to the spark plugs before removing the existing propeller & spinner. Reconnect after the installation of the replacement propeller and spinner is completed. Failure to comply can result in bodily injury when the propeller is rotated during removal or re- installation. CAUTION Wrap the blade shanks in several layers of masking or duct tape before removing the spinner dome to prevent damaging the blade and blade paint. 2.2 Removal and Installation Removal/installation of the propeller spinner and propeller are to be accomplished in accordance with Hartzell Propeller Owner's Manual 115N rev. 12 or later approve revisions and Cessna Aircraft Company Maintenance Manual, Models 180, 182, 185, 206, 207 or 210. Page 3 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Report: H0801-3 Revision: B Date: 7/11/13 Note: Optionally for ( )HC-C3YF-( ) Propellers and A-2295-1 ( ) Spinners (with A-2476- 30 mounting kit), perform the following spinner bulkhead mounting sequence where additional clearance is required between the spinner bulkhead and engine cowling. a. Place spacer included in kit under the head of each spinner mounting bolt (6 places). This spacer may be factory installed under the nut on the aft side of the propeller hub, in this case, remove spacer and relocate to under the head of the bolt on the forward side of the propeller hub. b. Place two washers between the hub and the spinner bulkhead on each spinner mounting bolt (6 places). c. After the bulkhead is in place, put one washer and nut on each spinner mounting bolt and torque to specification in Hartzell Manual 115 ( ). Note: If the propeller is equipped with an anti-ice or a de-ice system, follow the manufacturer's instructions for removing the components necessary for propeller removal. See Appendix A for Ice Protection Installation drawing 2.3 Tooling requirements ■ ◉ Safety wire pliers Torque wrench (1/2 inch drive) Torque wrench adapter (Hartzell P/N BST-2860) 3/4 inch open end wrench 2.4 Consumables Quick Dry Stoddard Solvent or Methyl-Ethyl-Ketone (MEK) 2.5 Expendables 0.032 Stainless Steel Aircraft Safety Wire " "O" ring propeller to engine seal (C-3317-228) or other approved P/N 2.6 Pre-Installation Inspection of shipping package ■ Examine the exterior of the shipping container for signs of shipping damage, especially at the box ends around each blade. A hole, tear or crushed appearance at the end of the box (at the propeller tips) may indicate the propeller was dropped during shipment, possibly damaging the blades. Page 4 of 16 Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 2.7 Uncrating ◉ Place the propeller on a firm support Report: H0801-3 Revision: B Date: 7/11/13 ■ Remove the banding and any external wood bracing from the cardboard shipping container. " Remove the cardboard from around the hub and blades. Place the propeller on a padded surface that supports the propeller over a large area. Never stand the propeller on a blade tip. Remove the plastic dust cover cup from the propeller-mounting flange (if installed). 2.8 Inspection after shipping • After removing the propeller from the shipping container, examine the propeller components for shipping damage. 2.9 Placard and marking: " Placard concerning other propellers are obsolete. 2.10 Perform static test, check for function and oil leakage. " • Perform full power static RPM check. Adjust low pitch stop per Section 4 of Hartzell Propeller Owner's Manual 115N. See Appendix B for suggested pitch stop settings.
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Check for proper governor control cable cushion, adjust as required. Adjust fuel flow in accordance with Cessna Service Instruction, TCM Engine Setup Procedures or in accordance with STC's that may be installed. TCM Service Information SID 97-3C or latest revision may also be used as a reference for fuel set-up. After adjustment is complete, final safety checks are made, safety wire installation as required, perform flight test and make all required log book entries. 2.11 Change weight and balance record and equipment list: Installation Hartzell Propeller (P)HC-()3YF-1RF/F7693DF(B,K)+2 propeller with spinner: C3YF Weight = 77 Lb G3YF Weight = 78 Lb J3YF Weight = 80.0 Lb Page 5 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Report: H0801-3 Revision: B Date: 7/11/13 Hartzell-Propeller (P)HC-()3YF-1RF/F8068(B,K)(-2) propeller with spinner: C3YF Weight = 82 Lb G3YF Weight = 83 Lb J3YF Weight = 84.75 Lb 2.12 Post-installation dynamic balance of the propeller / engine combination is recommended per Section 61-00-45 Page 6-38 of the Hartzell Owner's Manual 145. 2.13 Make the appropriate logbook entries and return aircraft to service with FAA Form 337 referencing STC. External configuration, mechanical and electrical interfaces, and limitations of the modified engine model remain identical to the currently approved aircraft models. Note: All Hartzell-Propeller manuals and service information can be ordered through your Hartzell-Propeller distributor or (if prepaid) directly from: Hartzell Propeller Inc. One Propeller Place Piqua, Ohio 45356 Email techsupport@hartzellprop.com Telephone (937) 778-4379 8am - 5pm US Eastern Time (937) 778-4376 after hours AOG support Or web site http://www.hartzellprop.com Page 6 of 16 Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Cessna 180 Series Report: H0801-3 Revision: B Date: 7/11/13 ENGINE RPM PROP MODEL DIAMETER INCHES SPINNER CESSNA MODEL MAX MAX CONT MAX MIN 180 2600 2600 (P)HC-C3YF-1RF/F8068(B,K) 82 78 (0-470- A) 180 2600 2600 PHC-C3YF-1RF/F8068(B,K) 82 78 (0-470-K) 180 2550 2550 (P)HC-C3YF-1RF/F8068(B,K) 82 78 (0-470-J) 180-A & B 2600 2600 PHC-C3YF-1RF/F8068(B,K) 82 78 (0-470-K) A-2295-1P * 180-C, D, E, F,G & H 2600 2600 PHC-C3YF-1RF/F8068(B,K) 82 32 7 78 (0-470-L) 180-C, D, E, F,G & H 2600 2600 (P)HC-C3YF-1RF/F8068(B,K) 62 82 78 (0-470-R) 180-J 2600 2600 (P)HC-C3YF-1RF/F8068(B,K) 82 78 (O-470-R&S) 180- K 2400 2400 (P)HC-C3YF-1RF/F8068(B,K) 82 78 (O-470-U) * Hartzell Spinner Part Number C-3535-1P may be used in place of the A-2295-1P on Cessna 180 aircraft. Page 7 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Modified (STC's) C-180 Report: H0801-3 Revision: B Date: 7/11/13 STC No. Engine BHP/RPM's Prop Model DIAMETER INCHES SA09055SC 0-520 235/2700 (P)HC-C3YF-1RF/F8068(B,K) 82 78 SA09530SC 0-470 250 / 2625 (P)HC-C3YF-1RF/F8068(B,K) 82 78 SA09530SC 0-470 250 / 2625 (P)HC-C3YF-1RF/F8068(B,K) 82 78 Cessna 180K SA09018SC 0-520 280 / 2700 (P)HC-G3YF-1RF/F8068(B,K) 82 78 SA01345AT IO-520 300 / 2850 (P)HC-C3YF-1RF/F8068(B,K) 82 78 SA09132SC O-550 285/ 2700 (P)HC-G3YF-1RF/F8068(B,K) 82 78 SA09055SC, SA09530SC, and SA09132SC use a D-5732-P spinner assemblies. SA09132SC is also eligible for a C-4582-P. SA01345AT uses a C-3535-1P Spinner assembly. Cessna 182 Series ENGINE RPM CESSNA MODEL DIAMETER INCHES PROP MODEL SPINNER MAX MAX MAX MIN CONT 182 2600 2600 PHC-G3YF-1RF/F8068 82 78 D-4798-3P (0-470-L) 182A thru D-4798-3P (A-G) 182G 2600 2600 PHC-G3YF-1RF/F8068 82 78 (0-470-L) 182-H Thru 182-N, 2600 2600 (P)HC-G3YF-1RF/F8068 82 78 D-4798-1P (O-470-R) 182-P, F182P 2600 2600 (P)HC-G3YF-1RF/F8068 82 78 D-4798-1P (0-470-S) 182-Q & R, F182Q 2400 2400 (P)HC-G3YF-1RF/F8068 82 78 D-4798-1P (O-470-U) Page 8 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Modified (STC's) C-182 Report: H0801-3 Revision: B Date: 7/11/13 DIAMETER STC No. Engine BHP / RPM's Prop Model INCHES MAX MIN SA8951SW O-470 250 / 2600 SA09530SC 0-470 250 / 2625 SA01443AT O-470 252 / 2625 SA09026SC O-520 280 / 2700 SA01302AT IO-520 300/2850 (P)HC-G3YF-1RF/F8068(B,K) (P)HC-G3YF-1RF/F8068(B,K) (P)HC-G3YF-1RF/F8068(B,K) (P)HC-G3YF-1RF/F8068(B,K) (P)HC-G3YF-1RF/F8068(B,K)-2 82 78 82 78 82 78 82 78 80 78 SA461NW 10-520 300 / 2850 (P)HC-G3YF-1RF/F8068(B,K)-2 80 78 SA01218AT IO-550 300 / 2700 (P)HC-G3YF-1RF/F8068(B,K) 82 78 SA09133SC O-550 285/2700 (P)HC-G3YF-1RF/F8068(B,K) 82 78 SA09026SC and SA09133SC are eligible for the D-5732-P or C-4582-P spinner. SA 01302AT and SA01218AT are eligible for the D-5732-P. SA8951SW, SA09530SW, and SA01443AT are eligible for the D-4798-3P (182 – 182G) or D4798-1P (182H – 182Q). Cessna 185 Series ENGINE RPM CESSNA DIAMETER INCHES PROP MODEL SPINNER MODEL MAX MAX CONT MAX MIN 185 thru 185E 2625 2625 PHC-C3YF-1RF/F8068(B,K) 82 78 (I0-470-F) C-3575-P A185E A185F 2850 2700 (P)HC-C3YF-1RF/F8068(B,K)-2 80 78 (10-520-D) Page 9 of 16 Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Modified (STC's) C-185 Report: H0801-3 Revision: B Date: 7/11/13 DIAMETER STC No. Engine BHP/ RPM's Prop Model INCHES SPINNER MAX MIN 300/2850 SA525NW 10-520 (P)HC-C3YF-1RF/F8068-2(B,K) (P)HC-C3YF-F/F7693DF(B,K) +2 80 78 SA1522GL IO-550 300 / (P)HC-C3YF-1RF/F8068(B,K) 2700 (P)HC-C3YF-RF/F7693DF(B,K) +2 C-3575-P 82 78 300 / (P)HC-C3YF-1RF/F8068(B,K) SA2933SO 10-550 82 78 2700 (P)HC-C3YF-RF/F7693DF(B,K) +2 STC SA2933SW is also eligible for the C-3535-1P spinner assembly. Page 10 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Report: H0801-3 Revision: B Date: 7/11/13 Cessna 206 Series ENGINE RPM CESSNA DIAMETER INCHES SPINNER PROP MODEL MODEL MAX MAX CONT MAX MIN 206 U206 2700 2700 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K)+2 88 82 78 80 78 800 A-2295-1(P) U206A U206B Thru (P)HC-C3YF-1RF/F8068(B,K)-2 2850 2700 80 78 A-2295-1(P) U206G (P)HC-C3YF-RF/F7693DF(B,K) +2 (To S/N 4074) U206G (from S/N 4075 & 2850 2700 (P)HC-J3YF-1RF/F8068(B,K)-2 (P)HC-J3YF-RF/F7693DF(B,K) +2 78 C-4582-(1)P on) TU206A Thru 2700 2700 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K)+2 TU206F 888 82 78 78 800 A-2295-1(P) (to S/N 2199) TU206F (S/N 2200- 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-RF/F7693DF(B,K)+2 82 80% 78 80 78 8 3521) C-4582-(1)P TU206G 2700 2600 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-RF/F7693DF(B,K)+2 82 78 80 78 0000 (P)HC-J3YF-1RF/F8068(B,K) 82 P206 2700 2700 (P)HC-J3YF-RF/F7693DF(B,K)+2 80 808 78 78 800 P206 A Replaces 2700 2700 McCauley (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K)+2 880 0000 82 78 78 A-2295-1(P) C58, C79, 90) P206 A Replaces (P)HC-J3YF-1RF/F8068(B,K) 82 2700 2700 McCauley (P)HC-J3YF-RF/F7693DF(B,K)+2 80 88 78 78 80% C73, C77, 88) C-4582-(1)P P206B Thru 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-RF/F7693DF(B,K)+2 888 82 78 80 78 0000 P206E Page 11 of 16 Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Cessna 206 Series Continued Report: H0801-3 Revision: B Date: 7/11/13 ENGINE RPM CESSNA MODEL DIAMETER INCHES PROP MODEL SPINNER MAX MAX CONT MAX MIN TP206 A Replaces McCauley 2700 2700 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K)+2 88 82 78 80 78 0000 A-2295-1(P) C78, C79, C90) TP206 A Replaces McCauley 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K)+2 8808 000 C70, C77, C88) 82 78 78 C-4582-(1)P TP206B Thru TP206E 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K)+2 88 82 78 80 78 000 Modified (STC's) C-206 STC No. Engine BHP / RPM's Prop Model SA10010SC 10-550-F SA00332AT IO-550-F 300 / 2700 300 / (P)HC-(C,J)3YF-1RF/F8068(B,K) 2700 (P)HC-(C,J)3YF-RF/F7693DF(B,K) +2 (P)HC-(C,J)3YF-1RF/F8068(B,K) (P)HC-(C,J)3YF-RF/F7693DF(B,K) +2 SA1482GL IO-550-F 300 / (P)HC-(C,J)3YF-1RF/F8068(B,K) 2700 (P)HC-(C,J)3YF-RF/F7693DF(B,K) +2 SA02507AT-D 10-550-N 310/ (P)HC-J3YF-1RF/F8068(B,K) 2700 (P)HC-J3YF-RF/F7693DF(B,K) +2 DIAMETER INCHES SPINNER MAX MIN A-2295-(1,2)P 82 82 880 880 20802080 78 or C-4582-(1)P 78 A-2295-(1,2)P or C-4582-(1)P A-2295-(1,2)P 78 or C-4582-(1)P 0000 C-4582-(1)P Page 12 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Cessna 207 Series Report: H0801-3 Revision: B Date: 7/11/13 ENGINE RPM CESSNA DIAMETER INCHES PROP MODEL SPINNER MODEL MAX MAX MAX MIN CONT 207 2850 2700 (P)HC-C3YF-1RF/F8068(B,K)-2 (P)HC-C3YF-RF/F7693DF(B,K) 60 80 78 T207 2700 2600 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K)+2 82 78 80 78 A-2295-1P (P)HC-C3YF-1RF/F8068(B,K)-2 207A 2850 2700 80 78 (P)HC-C3YF-RF/F7693DF(B,K) T207A 2700 2600 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K) +2 Modified (STC's) C-207 82 808 78 78 800 STC No. Engine BHP/ RPM's Prop Model DIAMETER INCHES MAX MIN SA10011SC IO-550-F 300/2700 (P)HC-C3YF-1RF/F8068(B,K) (P)HC-C3YF-RF/F7693DF(B,K) +2 82 78 Spinner P/N "A-2295-1P" must be used with the STC SA10011SC hub installation. Page 13 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Cessna 210 Series Report: H0801-3 Revision: B Date: 7/11/13 ENGINE RPM CESSNA DIAMETER INCHES PROP MODEL SPINNER MODEL MAX MAX MAX MIN CONT 210,210-A, B, 2625 2625 (P)HC-C3YF-1RF/F8068(B,K) 82 78 C, 210-5(A) A-2295-1(P) 210D 2700 2700 (P)HC-C3YF-1RF/F8068(B,K) 82 78 210-E (P)HC-J3YF-1RF/F8068(B,K) and 2700 2700 (P)HC-J3YF-F/F7693DF(B,K)+2 888 82 78 80 78 0000 210-F 210-G thru 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K)+2 808 82 80 78 800 210-J 210-K and 2850 2700 (P)HC-J3YF-1RF/F8068(B,K)-2 (P)HC-J3YF-F/F7693DF(B,K) 80 ☐ 78 210-L 210-M 2850 2700 (P)HC-J3YF-1RF/F8068(B,K)-2 (P)HC-J3YF-F/F7693DF(B,K) 60 80 78 210-N 2850 2700 (P)HC-J3YF-1RF/F8068(B,K)-2 (P)HC-J3YF-F/F7693DF(B,K) 80 (P)HC-J3YF-1RF/F8068(B,K) T210-F 2700 2700 (P)HC-J3YF-F/F7693DF(B,K)+2 8080 800 80 78 C-4582-1(P) 82 78 78 T210-G Thru T210-L 2700 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K) +2 808 82 78 78 000 (P)HC-J3YF-1RF/F8068(B,K) T210-M 2700 2600 (P)HC-J3YF-F/F7693DF(B,K)+2 T210N 2700 2600 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K)+2 P210N 2700 2600 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K) +2 28 28 28 78 80 78 78 80 78 78 80 78 ∞ ∞ 800 Page 14 of 16 © Hartzell Propeller, Inc All rights reserved Hartzell Propeller Inc One Propeller Place Piqua, OH 45356 Modified (STC's) C-210 Report: H0801-3 Revision: B Date: 7/11/13 DIAMETER SPINNER STC No. Engine BHP/ RPM's Prop Model INCHES MAX MIN SA00274AT IO-550 300/2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-F/F7693DF(B,K) +2 82 808 78 000 78 SA03141AT IO-550 300 / 2700 SA3104SO IO-550 300 / 2700 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-RF/F7693DF(B,K) +2 (P)HC-J3YF-1RF/F8068(B,K) (P)HC-J3YF-RF/F7693DF(B,K) +2 62 C-4582-1(P) 82 78 82 78 SA09952SC 10-550 300 / 2700 (P)HC-(C,J)3YF-1RF/F8068(B,K) (P)HC-(C,J)3YF-RF/F7693DF(B,K) +2 82 78 D-5732-P END Page 15 of 16 © Hartzell Propeller, Inc All rights reserved
What's in the CESSNA 185 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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