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OPERATION & SERVICE MANUAL

Cessna 441 Conquest II · Checklist

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Overview

This document is an Operation & Service Manual for the Tronair Multi-Head Towbar Model 01-0511-0000, which is compatible with various aircraft including the Cessna 441 Conquest II. It provides essential information regarding the specifications, safety information, operation procedures, and training requirements for using the towbar. The manual emphasizes the importance of following safety precautions to prevent personal injury and equipment damage. It includes a preliminary checklist for ensuring the towbar's readiness for use, as well as detailed instructions on how to operate the towbar safely and effectively. This manual is intended for operators and maintenance personnel involved in the towing of aircraft.

  • Towbar Maximum Gross Weight: 11,080 lbs (5.03 Metric tons)
  • Towbar Weight: 18 lbs (8.16 kg)
  • Dimensions: Width = 14.4375 in (34.1 cm), Length = 20.5 in (52.1 cm), Height = 4 in (10.2 cm)
  • Ensure all welds are checked for cracks before use.
  • Operators must be trained in safe towbar operation.

Document

Source

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

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Document details

Type
Checklist
Year
2007
Pages
21
File size
659 KB
Publisher
proservaviation.com
How rare is it?
51Cessna 441 Conquest II registered worldwide · 0 active

Common. Rarer than 2% of the aircraft models we track.

Documentation completeness
4/7

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In this document

1.0 Description

The towbar head attachment is designed for use with Tronair Multi-Head Towbar Models 01-1201-0010, 01-1202-0000, and 01-1290-0100 for towing various aircraft, including the Cessna 441 Conquest II. It utilizes a sliding pin/stationary pin arrangement to interface with the aircraft tow point.

1.1 Specifications

The specifications for the towbar include: Width = 14.4375 in (34.1 cm), Length = 20.5 in (52.1 cm), Height = 4 in (10.2 cm), Weight = 18 lbs (8.16 kg), and Maximum Aircraft Gross Weight = 11,080 lbs (5.03 Metric tons).

2.0 Safety Information

The manual outlines critical safety information, including warnings about using damaged or bent towbars, which can lead to personal injury or equipment damage. It emphasizes the need for proper training and adherence to safety protocols.

3.0 Operation

Section 3 details the operational procedures for the towbar, including a preliminary checklist to ensure the towbar is in good condition before use. It covers checks for weld integrity and the functionality of the sliding pin.

4.0 Training

This section outlines the training requirements for operators, emphasizing the employer's responsibility to provide adequate training for safe towbar operation.

5.0 Provision Of Spares

Information on obtaining spare parts from the manufacturer is provided, along with a parts list for reference.

Safety notes

  • A damaged or bent towbar should not be used; it must be repaired or replaced.
  • Only use Tronair OEM replacement parts to maintain warranty.

Full document text

OPERATION & SERVICE MANUAL Tronair, Inc. Phone: (419) 866-6301 | 800-426-6301 1 Air Cargo Pkwy East Web: www.tronair.com Swanton, OH 43558 Email: sales@tronair.com Multi-Head Model: 01-0511-0000 Cessna: 210 Centurion, 310, 320, 335, 336, 337, 340, 401, 402, 404, 411, 414, 414A, 421, 421C, Conquest 441 & 425 Gulfstream: Aero Commander & Turbo Commander Piper: Aerostar, Cheyenne I, II, III, IIA, Chieftan, Navajo, Mojave 11/2007  Rev. 04 REVISION DATE TEXT AFFECTED 03 03/2007 Added CE marking 04 11/2007 Modified aircraft applications, 1.0, 1.1 & 2.1 Modified Parts List Model: 01-0511-0000 Multi-Head 11/2007 | Rev. 04 TABLE OF CONTENTS PAGE 1.0 Description......................................................................................................................................................................... 1 1.1 Specifications.......................................................................................................................................................... 1 2.0 Safety Information ............................................................................................................................................................. 1 2.1 General ................................................................................................................................................................... 1 3.0 Operation ........................................................................................................................................................................... 2 3.1 Preliminary Checklist .............................................................................................................................................. 2 3.1.1 Head Attachment Weldment ..................................................................................................................... 2 3.1.2 Sliding Pin................................................................................................................................................. 2 3.2 Usage Procedure .................................................................................................................................................... 2 4.0 Training ............................................................................................................................................................................. 2 4.1 Training Requirements............................................................................................................................................ 2 4.2 Training Program .................................................................................................................................................... 2 4.3 Operator Training .................................................................................................................................................... 2 5.0 Provision Of Spares........................................................................................................................................................... 2 Spare Parts Can Be Obtained From The Manufacturer ..................................................................................................... 2 5.1 Parts List ................................................................................................................................................................. 2 Model: 01-0511-0000 Multi-Head 11/2007 | Rev. 04 Page | 1 Tronair towbars/heads must only be used with matching Tronair heads/towbars, and Tronair shear pins. This product can not be modified without the written approval of Tronair, Inc. Any modifications done without written approval voids all warranties and releases Tronair, Inc., it suppliers, distributors, employees, or financial institutions from any liability from consequences that may occur. Only Tronair OEM replacement parts shall be used. 1.0 DESCRIPTION The towbar head attachment is designed for use with Tronair Multi-Head Towbar Models 01-1201-0010, 01-1202-0000 and 01-1290-0100 for towing the previously stated aircraft. The towbar head attachments use a sliding pin/stationary pin arrangement to interface with the aircraft tow point. 1.1 SPECIFICATIONS  Aircraft Application(s): Cessna: 210 Centurion, 310, 320, 335, 336, 337, 340, 401, 402, 404, 411, 414, 414A, 421, 421C, Conquest 441 & 425 Gulfstream: Aero Commander & Turbo Commander Piper: Aerostar, Cheyenne I, II, III, IIA, Chieftan, Navajo, Mojave  Dimensions: Width = 14.4375 in (34.1 cm) at the widest sliding pin setting Length = 20.5 in (52.1 cm) overall Height = 4 in (10.2 cm)  Weight: 18 lbs (8.16 kg)  Finish: Blue Powder Coat  Aircraft Gross Weight (Maximum): 11,080 lbs (5.03 Metric tons) 2.0 SAFETY INFORMATION 2.1 GENERAL The Tronair Model 01-0511-0000 Multi-Head is a towbar head attachment for the Cessna 210 Centurion, 310, 320, 335, 336, 337, 340, 401, 402, 404, 411, 414, 414A, 421, 421C, Conquest 441 & 425, Gulfstream Aero Commander & Turbo Commander, and Piper Aerostar, Cheyenne I, II, III, IIA, Chieftan, Navajo, Mojave aircraft. To ensure safe operation, please read the following statements and understand their meaning. This manual contains safety precautions which are explained as follows. Please read carefully. WARNING! Warning is used to indicate the presence of a hazard that can cause severe personal injury, death, and/or substantial property damage if the warning notice is ignored. CAUTION! Caution is used to indicate the presence of a hazard which will or can cause minor personal injury or property damage if the caution notice is ignored. WARNING! A damaged or bent towbar should not be used. Towbar should be repaired or replaced. Model: 01-0511-0000 Multi-Head 11/2007 | Rev. 04 Page | 2 3.0 OPERATION 3.1 PRELIMINARY CHECKLIST 3.1.1 Head Attachment Weldment  Check weld between connector tube and head plate for cracks.  Check weld between side rails and head plate for cracks.

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 Check weld between side rail and stationary pin for cracks.  Check weld between side rail and sliding pin sleeve for cracks. 3.1.2 Sliding Pin  Check sliding pin for bending or excessive wear. Ensure sliding pin slides freely.  Check sliding pin ball lok-T pin. ensure ball lok-T pin is securely attached to the head attachment weldment via its lanyard.  Ensure ball lok-T pin is not loose or missing. 3.2 USAGE PROCEDURE Secure the towbar head attachment using the ball lok-T pin (supplied with the multi-head towbar) onto one of the following Tronair Multi-Head Towbar Models:  01-1201-0010  01-1215-0000  01-1290-0100  01-1202-0000  01-1216-0000 Set the sliding pin to the correct location on the multi-head towbar using its ball lok-T pin. Reference Figures 1  3. 4.0 TRAINING 4.1 TRAINING REQUIREMENTS The employer of the operator is responsible for providing a training program sufficient for the safe operation of the towbar. 4.2 TRAINING PROGRAM The employer-provided operator training program should cover safety procedures concerning use of the towbar in and around the aircraft at the servicing location. 4.3 OPERATOR TRAINING The operator training should provide the required training for safe operation of towbar. NOTE: Maintenance and Trouble Shooting are to be performed by the skilled and trained technician. 5.0 PROVISION OF SPARES Spare Parts can be Obtained from the Manufacturer TRONAIR, Inc. Telephone: (419) 866-6301 or 800-426-6301 1740 Eber Road Fax: (419) 867-0634 Holland, Ohio 43528-9794 USA E-mail: sales@tronair.com Website: www.tronair.com 5.1 PARTS LIST Reference Parts List and Illustration on following page. Model: 01-0511-0000 Multi-Head 11/2007 | Rev. 04 Page | 3 Parts List When ordering replacement parts/kits, please specify model, serial number and color of your unit. ITEM PART NUMBER DESCRIPTION QTY 1 ..................... Z-1344-01 ............................................... Head Weldment (Not Sold Separately) .................................... 1 2 ..................... G-1310-0415 .......................................... Ball Lok-T Pin, ¼" diameter x 1 ½" long ................................... 1 3 ..................... H-1026*07.0 ........................................... Lanyard Assembly .................................................................... 1 4 ..................... B-115 ...................................................... Sliding Pin ................................................................................ 1 5 ..................... G-1300-19040 ........................................ Roll Pin, 3/16" diameter x ½" long ............................................ 1 K-1283 Kit, Replacement Sliding Pin; consists of: 4 ..................... B-115 ...................................................... Sliding Pin ................................................................................ 1 5 ..................... G-1300-19040 ........................................ Roll Pin, 3/16" diameter x ½" long ............................................ 1 K-1308 Kit, Replacement Ball Lok-T Pin; consists of: 2 ..................... G-1310-0415 .......................................... Ball Lok-T Pin, ¼" diameter x 1 ½" long ................................... 1 3 ..................... H-1026*07.0 ........................................... Lanyard Assembly .................................................................... 1 6 ..................... G-1351-04 .............................................. Rivet, 1/8 Open-End Steel........................................................ 1 APPENDIX I INS-1582 Towbar Usage Instructions Tronair, Inc. Phone: (419) 866-6301 | 800-426-6301 1 Air Cargo Pkwy East Web: www.tronair.com Swanton, OH 43558 Email: sales@tronair.com APPENDIX I INS-1582 Towbar Usage Instructions 11/2003 – Rev. 03 REVISION DATE TEXT AFFECTED 03 11/25/03 pg 1 Warning added INS-1582 Towbar Usage Instructions 11/2003 | Rev. 03 Page | 1 Your Tronair towbar is engineered and built to the highest standards of quality and workmanship. Under normal usage and with minimal maintenance this towbar will provide exceptional service. WARNING! A damaged or bent towbar should not be used, but should be repaired or replaced. USING A DAMAGED OR BENT TOWBAR CAN RESULT IN AIRCRAFT OR EQUIPMENT DAMAGE AND POSSIBLE PERSONAL INJURY. WARNING! Towbars With Hydraulic Lifting Mechanism: The hydraulic lift mechanism (on those towbars so equipped) should only be used to raise the towbar to facilitate connection to the aircraft or tug. Release any hydraulic pressure when towing aircraft or moving towbar. WARNING! Towbars Should be Used with Category 1 Tugs: Tronair recommends the use of a towbar with a category 1 or category 2 tug and aircraft not exceeding 75,000 lbs gross weight. Using the towbar with aircraft weighing in excess of this specific limitation may result in excessive loads and stresses being applied to the towbar and/or the aircraft. These excessive loads may cause failure of the towbar which could cause damage (INCLUDING WITHOUT LIMITATION to the aircraft) and/or personal injury OR DEATH. TRONAIR MAKES NO REPRESENTATION, WARRANTY OR GUARANTEE AS TO SUCH MISUSE AND DISCLAIMS ANY AND ALL LIABILITY FOR INJURY, LOSS OR DAMAGE ARISING FROM OR RELATING TO SUCH MISUSE. INS-1582 Towbar Usage Instructions 11/2003 | Rev. 03 Page | 2 (If Applicable) FIGURE 2 NOTE: Typical towbar. Your towbar and/or head may not have all of the features shown NOTE: Typical towbar. Your towbar and/or head may not have all of the features shown FIGURE 1 INS-1582 Towbar Usage Instructions 11/2003 | Rev. 03 Page | 3 BEFORE USING TOWBAR, COMPLETE THE FOLLOWING CHECKLISTS: Reference Figures 1 & 2 on Page 2. TOWBAR: Area of Towbar: Check: Shock Assembly: 1. Weld between eye and tube (Are there cracks?) 2. Bolts attaching shock to towbar (Loose, missing, stripped, etc.) 3. Eyebolt (Is it bent, worn down, or deformed? Towbar Weldment: 1. Tube (Is it bent, dented, bowed, and/or have cracks?) 2. Weld at head end (Are there any cracks in the welds?) 3. Head hole (Is it elongated? Is the ball lok pin attached to the towbar?) Caster/Skid Plate: 1. Casters (Are they missing or bent?) 2. Handles (Are they broken, bent, or missing?) 3. Bolts (Are they missing or loose?) Wheel Assembly: 1. Wheels (Are they flat? Is the rim bent?) 2. Axle (Is it bent?) HEAD: Area of Head: Check: Bolts & Lanyards: 1. Are they loose, missing, or stripped? Are they attached to the head? Weldment: 1. Welds holding side rails to head rail (Are there any cracks?) 2. Shear Plates (Are there cracks in welds? Are the plates bent?) Shear Pin Mechanism: 1. Shear Pin (Is it bent or deformed? Are there spares?) 2. Bushings (Are they cracked, chipped, secure?) 3. Pivot Bolt (Are the nuts tight? Are there washers present?) Area of Head: Check: Aircraft Attach Point: 1. Sliding Pin(s) (Are they bent, cracked? Do they slide freely?) 2. Locking Pin (Are they loose? Do they hold the sliding pins securely?) 3. Wear sleeves (Are the welds cracked?) 4. Roll Pins(s) (Are they rusted? Are they missing? Are they loose?) 5. Ball Lok Pin (Is it attached to head? Is it rusted? Is it bent?) 6. Axle Adapter (Is it bent? Is the slot deformed? Are bolts tight?) SNAP-BAK AND UNIVERSAL TOWBARS: Area of Towbar: Check: Towbar: 1. Spring (Has it taken a set? Loose in the assembly?) 2. Eyebolt (Is it bent, worn down, or deformed?) 3. Tube (Is it bent, dented, bowed, or cracked? Is it rusted badly?) 4. Welds (Are there any cracks in the welds?) 5. Head Hole (Is it elongated? Is the bolt attached correctly?) Function: 1. Does it snap back? Head: 1. Pivot Bolt (Is it present along with washers? Is the nut tight? Is it rusted?) 2. Roll Pin(s) (Are they rusted? Are they missing? Are they loose?) 3. Weldment (Is it deformed, bent, or rusted beyond reasonable use?) 4. Lanyard (Is it attached to weldment?) 5. Sliding Pin(s) (Are they bent, cracked or rusted? Does it slide?) INS-1582 Towbar Usage Instructions 11/2003 | Rev. 03 Page | 4 USAGE PROCEDURE Aircraft Attachment: It is recommended that your towbar be attached to the aircraft first, and then connected to the tug to avoid possible aircraft damage. Ensure sliding pins are locked in place before towing aircraft. Tug Attachment: Damage to the towbar or aircraft can result from an excessive towbar angle during towing operations (See Figure 3). If aircraft with both high and low tow points are encountered, consider using two pintle hooks, as shown in Figures 4 & 5, so that the towbar is as level as possible during towing. Also pintle hook height should prevent contact of towbar wheels with the ground, during towing. (See Figure 5). Type Of Coupler: Damage to the towbar or aircraft can result while towing with the following type of couplers: - Lift Head - Vertical Side Swing Latch - Standard Duty Latch - Swivel Hook These types of couplers are known to cause binding and failure in the eyebolt. Indicators of eyebolt binding are wear on the outside diameter of the eye and indentations on the inside diameter. The failure will begin at the head of the eye. See Figure 6. FIGURE 3 - INCORRECT FIGURE 4 - CORRECT FIGURE 5 - CORRECT FIGURE 6 INS-1582 Towbar Usage Instructions 11/2003 | Rev. 03 Page | 5 USAGE PROCEDURE (continued) Type Of Coupler: Damage to the towbar or aircraft can result while towing with the following type of couplers: - Lift Head - Vertical Side Swing Latch - Standard Duty Latch - Swivel Hook These types of couplers are known to cause binding and failure in the eyebolt. Indicators of eyebolt binding are wear on the outside diameter of the eye and indentations on the inside diameter. The failure will begin at the head of the eye. See Figure 6. Figure 7 illustrates a pintle hook arrangement that is known to eliminate eyebolt binding. Tronair recommends using this type of hook on your tug. Eyebolt and Pintle Pin Size: Damage to the towbar or aircraft can result by towing or pushing an aircraft with an incorrect size eyebolt or pintle pin. A correct size eyebolt will make contact with the pintle pin. A gap between the eyebolt outside diameter and the coupler face plate should be easily seen. An eyebolt which is too large will cause the eyebolt to make contact with the face plate of the coupler. When the eyebolt is too large for the coupler, a gap between the inside diameter of the eyebolt and the coupler face plate will be seen. See Figure 8. To ensure proper towing and pushing, check to make sure that the pintle pin diameter is not too large for the eyebolt's inside diameter. Approximately a one-half inch (1/2") gap between the pin diameter and the eyebolt should be seen. If any of these conditions are not met, please contact Tronair for information to obtain a new coupler. Towing Angle: Damage to the towbar or aircraft can result from pushing an aircraft while maintaining too sharp of an angle between the tug and the towbar. Contact between the towbar weldment and tug must be avoided. It is recommended that the angle between the tug and towbar not exceed 90º. See Figure 9. FIGURE 9 FIGURE 8 FIGURE 7 APPENDIX II Declaration of Conformity Tronair, Inc. Phone: (419) 866-6301 | 800-426-6301 1 Air Cargo Pkwy East Web: www.tronair.com Swanton, OH 43558 Email: sales@tronair.com DECLARATION of CONFORMITY The design, development and manufacture is in accordance with European Community guidelines Multi-Head 01-0511-0000 Relevant provisions complied with by the machinery: 2006/42/EC Relevant standards complied with by the machinery: EN ISO 12100-1 Identification of person empowered to sign on behalf of the Manufacturer: Quality Assurance Representative

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