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KI-233 Revision E

Robinson R66 Turbine · Service Bulletins

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Overview

This document provides installation instructions for the Chin Access Cover Installation Kit specifically for the Robinson R66 Turbine and R44-series helicopters. It outlines the necessary tools, materials, and step-by-step procedures required to successfully install the chin access cover. The document emphasizes safety precautions, proper installation techniques, and the importance of verifying kit contents before beginning the installation process. It is intended for use by certified technicians and maintenance personnel familiar with helicopter maintenance procedures.

  • The access hole dimensions for the R66 are 4.00 inches by 8.00 inches with 0.5-inch radius corners.
  • Disconnect the battery by removing the negative cable first, then the positive cable.
  • Use a vacuum cleaner to minimize debris when cutting the access hole.
  • Install the C795-1 cover using (6) B526-6 screws after completing the installation.
  • Ensure all nutplates are installed parallel with the helicopter's centerline.

Document

Source

Originally published by robinsonstrapistorprod.blob.core.windows.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Service Bulletins
Year
2021
Pages
8
File size
459 KB
Publisher
robinsonstrapistorprod.blob.core.windows.net
How rare is it?
16Robinson R66 Turbine registered worldwide · 0 active

Common. Rarer than 5% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Robinson R66 Turbine.

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In this document

Kit Instructions

The kit instructions detail the steps for installing the chin access cover on the R66. Key steps include disconnecting the battery, cutting an access hole of 4.00 inches by 8.00 inches, and drilling specific rivet holes for the cover and shingle. The instructions also specify the use of certain tools and materials, such as a blind rivet installation tool and specific rivet types.

Safety Precautions

The document includes several safety notes, such as the proper sequence for disconnecting and connecting the battery to minimize electrical discharge risks. It also advises reviewing Safety Data Sheets (SDS) when working with hazardous materials.

Kit Contents

The installation kit includes various components such as screws, covers, shingles, and rivets. For the R66, specific quantities of each part are listed, ensuring that technicians have the necessary materials for the installation.

Special Tools Required

A list of special tools needed for the installation is provided, including a blind rivet installation tool, a manual squeeze-type rivet tool, and a thin-kerf cutting disc for fiberglass. These tools are essential for completing the installation correctly.

Installation Steps

The installation process is broken down into detailed steps, including preparing the helicopter, cutting the access hole, drilling rivet holes, and securing the cover and shingle. Each step is accompanied by warnings and notes to ensure proper execution.

Safety notes

  • Disconnect the negative battery cable first to minimize electrical discharge risk.
  • Review Safety Data Sheets (SDS) when working with hazardous materials.

Full document text

KI-233 Revision E KI-233-1 R44-series Chin Access Cover Installation Kit Instructions KI-233-2 R66 Turbine Chin Access Cover Installation Kit Instructions To comply with R44 Service Bulletin SB-102 or R66 Service Bulletin SB-35. NOTE Visit www.robinsonheli.com to verify kit instructions are current revision. Review instructions before installation; contact RHC Technical Support with questions. Verify kit contents match list; contact RHC Customer Service if parts are missing or damaged. NOTE Rivets included in kit are provided as a courtesy and at lengths most commonly used on production helicopters. Proper rivet length is determined by installer during installation. 1 KI-233Instr. Kit Instructions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1 2 B526-6 Screw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 6 3 C795-1 Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1 4 C795-2 Shingle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1 5 MS20426AD3-4+ Rivet (Note: “+” in part number indicates 50-qty pack) . . . . . . . . . . 1 1 6 MS20470AD3-4.5+ Rivet (Note: “+” in part number indicates 50-qty pack) . . . . . . . . . . 1 1 7 MS20605R3W3 Rivet, blind . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 0 8 MS21069L08 Nutplate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 6 9 NAS1149FN232P+ Washer (Note: “+” in part number indicates 20-qty pack) . . . . . . . . 1 1 10 NAS1474A08 Nutplate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 0 Consumables Refer to R44 Maintenance Manual (MM) § 1.400 or R66 MM § 20-70 approved materials list. • One pint of paint; C795-1 cover & C795-2 shingle are supplied primered only. Refer to the inside cover of factory-supplied maintenance record (logbook) for paint code(s) of specific helicopter serial number. NOTE C795-1 cover and C795-2 shingle may be painted before or after installation on helicopter. ITEM PART NUMBER KIT CONTENTS (R44) QTY PER KI-233-1 (R66) QTY PER KI-233-2 22 OCT 2021 Chin Access Cover Installation Kit Page 1 of 8 KI-233 Revision E Page 2 of 8 Chin Access Cover Installation Kit 22 OCT 2021 Special Tools • Blind rivet installation tool • Manual squeeze-type rivet installation tool • Thin-Kerf (or equivalent) cutting disc for fiberglass • Drum (cylindrical) sander, 1-inch (or smaller) diameter • Clecos (sheet metal fastener) size #40 (silver) and #18 (black) Kit Instructions CAUTION To minimize risk of electrical discharge: When disconnecting battery, disconnect negative (ground) cable from the battery first, then disconnect positive cable. When connecting battery, connect positive cable first, then connect negative (ground) cable. 1. Turn battery switch off. If nose battery installed, refer to R44 Illustrated Parts Catalog (IPC) Figures 96-19, 96-23, or 96-27 and R44 MM § 37-10. Using standard maintenance procedures, remove battery and battery box assembly & box drain. 2. Refer to Figures 1A, 1B, or 1C, as applicable. Lay out dimensions for access hole on chin as shown. Inspect proposed hole area for fasteners and note location(s). WARNING Refer to appropriate Safety Data Sheet (SDS) and take necessary safety precautions when working in proximity to hazardous materials. 3. Open upper console. Remove avionics as required and inspect proposed hole area for impediments such as, but not limited to: wiring, heater control cable & clamp(s), heater hose(s) & clamps, radar altimeter components, and antenna(e). Temporarily reposition or remove impediments as required. 4. Using cutting disc, create small hole within marked boundaries sufficient to allow passage of an inspection mirror. Simultaneous use of vacuum cleaner is recommended to minimize debris accumulation. 5. Using inspection mirror, inspect chin interior for impediments. Temporarily reposition or remove impediments as required. 6. Using cutting disc and drum sander, cut out hole to specified 4.00 inches by 8.00 inches dimensions with 0.5-inch radius corners. Simultaneous use of vacuum cleaner is recommended to minimize debris accumulation. 7. Refer to Figures 1A, 1B, or 1C, as applicable. Using C795-1 cover as template and a drill stop, lay out and drill (6) 0.169–0.175 inch diameter holes around access hole as shown. KI-233 Revision E 22 OCT 2021 Chin Access Cover Installation Kit Page 3 of 8 Kit Instructions (continued) 8. Layout C795-2 shingle installation rivet holes as shown in Figures 1A, 1B, or 1C. Postion shingle on chin at planned rivet holes and verify shingle will be centered on, and overlap cover. Using a drill stop, drill (3) 0.097–0.102 inch diameter holes. NOTE Ensure all nutplates are installed parallel with centerline of helicopter. a. For R44-series: Refer to Figure 2. Temporarily hold (2) NAS1474A08 nutplates in aft positions on exterior using screws. Using nutplates as template, drill (4) 0.097–0.102 inch diameter rivet holes. Remove nutplates and create 0.170–0.190 inch diameter, 100º countersinks on outside of chin. Install nutplates using (4) MS20426AD3-4 rivets, or MS20605R3W3 blind rivets, at installer’s discretion. Position (4) MS21069L08 nutplates in place on exterior with screws temporarily inside chin. Using nutplates as template, drill (8) 0.097–0.102 inch diameter rivet holes. Remove nutplates & screws and create 0.170–0.190 inch diameter, 100º countersinks on outside of chin. Install nutplates using (8) MS20426AD3-4 rivets. On R44 s/n 0357 and prior, the clamp securing the heater control cable may require minor repositioning and a new screw hole. If required: i. Remove and retain AN742-3 clamp (and hardware) securing cabin heat cable to belly of

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helicopter. ii. Locate and drill (1) 0.169–0.175 inch diameter hole as shown in Figure 1A. iii. Reposition cable and secure to new location using retained AN742-3 clamp and hardware. iv. fill/plug old hole with sealant or hardware. b. For R66-series: Refer to Figure 3. Position (6) MS21069L08 nutplates in place on exterior with screws temporarily inside chin. Using nutplates as template, drill (12) 0.097–0.102 inch diameter rivet holes. Remove nutplates & screws and create 0.170–0.190 inch diameter, 100º countersinks on outside of chin. Install (6) MS21069L08 nutplates using (12) MS20426AD3-4 rivets. 9. Ensuring raised flange is aft, install C795-2 shingle using (3) MS20470AD3-4.5 rivets, with (3) NAS1149FN232P washers under bucked end (inside chin). Clean up debris. 10. Via newly created hole, clean & inspect accessible portions of tail rotor flight controls and structure. Verify operating clearance throughout full range of tail rotor control travel. Repair as required. 11. Install C795-1 cover using (6) B526-6 screws, with forward edge underneath shingle flange. 12. Install removed avionics, if applicable. Install battery and battery box assembly & box drain, if removed. Close & secure upper console. 13. Make appropriate maintenance record entries. Weight and Balance change is negligible. KI-233 Revision E Page 4 of 8 Chin Access Cover Installation Kit 22 OCT 2021 FIGURE 1A R44-series (with aft battery) dimensions for access hole & nutplate locations (view looking up from underneath helicopter) KI-233 Revision E 22 OCT 2021 Chin Access Cover Installation Kit Page 5 of 8 FIGURE 1B R66-series dimensions for access hole & nutplate locations (view looking up from underneath helicopter) KI-233 Revision E Page 6 of 8 Chin Access Cover Installation Kit 22 OCT 2021 FIGURE 1C R44-series (with nose battery) dimensions for access hole & nutplate locations (view looking up from underneath helicopter) KI-233 Revision E FIGURE 2 R44-series installation (view looking up from underneath helicopter) 22 OCT 2021 Chin Access Cover Installation Kit Page 7 of 8 KI-233 Revision E FIGURE 3 R66-series installation (view looking up from underneath helicopter) Page 8 of 8 Chin Access Cover Installation Kit 22 OCT 2021