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INSTALLATION INSTRUCTIONS OIL RESIDUE COLLECTION SYSTEM KING AIR 200, B200 SERIES

Beechcraft King Air 200 · Maintenance Manual

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Overview

This document provides detailed installation instructions for the Butterfield Industries Oil Residue Collection System, specifically designed for the Beechcraft King Air 200 and B200 series aircraft. It is intended for use by installation facilities and technicians responsible for the modification of these aircraft. The installation is approved by the FAA under Supplement Type Certificate (STC) SA4362NM, and it is crucial that the installation conforms to the FAA-approved drawings and instructions provided within this manual. The document outlines the necessary preparations, required documentation, and step-by-step procedures for the installation of the oil residue collection system, which aims to improve cleanliness and safety by collecting oil residue in a designated sump assembly.

  • The installation is approved under STC SA4362NM.
  • Applicable models include King Air 200, B200, A200, B200GT, and B200CGT.
  • Installation requires specific Butterfield supplied documents and customer documentation.
  • The oil residue collection system collects drain fluid into a single sump assembly with a drain valve.
  • Periodic inspection of the oil residue tank is necessary to ensure continued airworthiness.

Document

Source

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

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Document details

Type
Maintenance Manual
Year
2007
Pages
17
File size
175 KB
Publisher
ipsl.aero
How rare is it?
2Beechcraft King Air 200 registered worldwide · 0 active

Common. Rarer than 17% of the aircraft models we track.

Documentation completeness
3/7

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In this document

Introduction

The introduction section outlines the purpose of the document, which is to provide installation instructions for the Butterfield Industries Oil Residue Collection System on the King Air 200 and B200 family of aircraft.

Required Documentation

This section lists the necessary documentation required for the installation, including Butterfield supplied documents and customer supplied documentation, such as the Beechcraft King Air 200 Maintenance Manual.

General

The general section describes the eligibility of the Oil Residue Collection System for installation on various models of the King Air 200 and B200 series, detailing the serial numbers of authorized aircraft.

Kit Installation

This section provides a detailed sequence of steps for installing the oil residue collection system, including sump assembly installation, hose assembly installation, and final inspection procedures.

Continued Airworthiness Instructions

This section emphasizes the importance of periodic inspections of the oil residue tank and associated components, as well as guidelines for maintaining the system's airworthiness.

Safety notes

  • Installation must conform to FAA approved Butterfield Industries installation drawings and instructions.
  • Deviations from approved instructions require FAA and Butterfield Industries approval.

Full document text

Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 1 INSTALLATION INSTRUCTIONS P/N BI 1013 OIL RESIDUE COLLECTION SYSTEM KING AIR 200, B200 SERIES KIT P/N BI 1011-1 11/12/07 REV: C Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 2 IMPORTANT NOTICE THE BUTTERFIELD INDUSTRIES OIL RESIDUE COLLECTION SYSTEM INSTALLATION HAS BEEN APPROVED BY THE FEDERAL AVIATION ADMINISTRATION (FAA) UNDER SUPPLEMENT TYPE CERTIFICATE (STC) THIS INSTALLATION MUST CONFORM TO THE FAA APPROVED BUTTERFIELD INDUSTRIES INSTALLATION DRAWINGS AND THE INSTRUCTIONS CONTAINED IN THIS DOCUMENT. CONFORMITY VERIFICATION OF THE INSTALLED SYSTEM TO THE BUTTERFIELD INDUSTRIES INSTALLATION DRAWINGS AND INSTRUCTIONS IS THE RESPONSIBILITY OF THE INSTALLATION FACILITY. DEVIATIONS TO THE FAA APPROVED BUTTERFIELD INDUSTRIES INSTALLATION DRAWINGS AND INSTRUCTIONS MUST BE APPROVED BY BOTH THE FAA AND BUTTERFIELD INDUSTRIES. THE INSTALLATION FACILITY IS RESPONSIBLE FOR BOTH COORDINATING AND OBTAINING THAT APPROVAL. DRAWN BUTTERFIELD INDUSTRIES, INC. N. HENNING 08/02/88 CHECKED INSTALLATION INSTRUCTIONS A. ERDAHL 08/31/88 ENGINEER OIL RESIDUE COLLECTION J. WHITCOMB 08/31/88 STRESS SYSTEM APPROVED KING AIR 200 SERIES AIRCRAFT J. WHITCOMB 08/31/88 BUTTERFIELD INDUSTRIES PROPRIETARY RIGHTS ARE INCLUDED IN THE INFORMATION DISCLOSED HEREIN. NEITHER THIS DOCUMENT NOR THE INFORMATION DISCLOSED HEREIN SHALL BE REPRODUCED, USED OR DISCLOSED IN WHOLE OR PART WITHOUT THE WRITTEN PERMISSION OF BUTTERFIELD INDUSTRIES, INC. . Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 3 REVISIONS LTR DESCRIPTION APPROVALS A REVISION TO ADD A200 SERIES OF AIRCRAFT TO LIST OF APPLICABLE AIRCRAFT FOR THIS KIT CHECKED: REASON: ADDITIONAL KIT APPLICABILITY J. WHITCOMB 01/27/04 PRODUCTION INFO: EXISTING INSTALLATIONS APPROVED: SATISFACTORY W. BUTTERFIELD 01/27/04 B REVISION TO ADD B200GT/B200CGT SERIES OF AIRCRAFT TO LIST OF APPLICABLE AIRCRAFT FOR THIS KIT REASON: ADDITIONAL KIT APPLICABILTY PRODUCTION INFO: EXISTING INSTALLATIONS APPROVED: SATISFACTORY W. BUTTERFIELD 11/12/07 C REVISION TO ADD B200GT/B200CGT SERIES OF AIRCRAFT TO LIST OF APPLICABLE AIRCRAFT FOR THIS KIT REASON: ADDITIONAL KIT APPLICABILTY PRODUCTION INFO: EXISTING INSTALLATIONS APPROVED: SATISFACTORY W. BUTTERFIELD 11/12/07 Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 4 TABLE OF CONTENTS SECTION TITLE PAGE SUPPLEMENT TYPE CERTIFICATE TITLE PAGE 2 REVISIONS 3 TABLE OF CONTENTS 4 1.0 INTRODUCTION 6 2.0 REQUIRED DOCUMENTATION 6 2.1 BUTTERFIELD SUPPLIED 6 2.2 CUSTOMER SUPPLIED 6 3.0 GENERAL 7 3.1 KIT DESCRIPTION 7 3.2 KIT CONTENTS 8 3.3 TOOLS REQUIRED 8 4.0 AIRPLANE PREPARATION 8 5.0 REMOVALS 9 6.0 KIT INSTALLATION 9 Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 5 6.1 SUMP ASSY INSTALLATION 10 6.2 HOSE ASSY INSTALLATION 10 6.3 FINAL INSTALLATION 10 6.4 INSPECTION 11 7.0 RETURN TO SERVICE 11 KIT PACKING LIST 12 CONTINUED AIRWORTHINESS 13 INSTRUCTION Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 6 1.0 INTRODUCTION THIS DOCUMENT IS INTENDED TO PROVIDE DETAILED INSTRUCTIONS FOR THE INSTALLATION OF THE BUTTERFIELD INDUSTRIES ‘OIL RESIDUE COLLECTION SYSTEM’, ON THE KING AIR 200 AND B200 FAMILY OF AIRCRAFT. 2.0 REQUIRED DOCUMENTATION IN ADDITION TO THIS INSTRUCTION MANUAL, THE FOLLOWING DOCUMENTS WILL BE REQUIRED TO INSTALL THE OIL RESIDUE COLLECTION SYSTEM. 2.1 BUTTERFIELD SUPPLIED DOCUMENTS THE FOLLOWING DRAWINGS OF THE CORRECT REVISION ARE SUPPLIED AS PART OF THIS DOCUMENTATION. BI-1011 SHEET 1, 2 AND 3 ENGINE DRAIN SUMP INSTALLATION BI-1012 DRAWING LIST 2.2 CUSTOMER SUPPLIED DOCUMENTATION THE FOLLOWING DOCUMENTS OF THE LATEST REVISION IN EFFECT AT THE TIME OF THE KIT INSTALLATION SHALL BE SUPPLIED BY THE CUSTOMER OR THE INSTALLATION FACILITY: 101-590010-19 BEECHCRAFT KING AIR 200 MAINTENANCE MANUAL FAA-AC 43.13-1A ACCEPTED METHODS, TECHNIQUES AND PRACTICES FOR AIRCRAFT ALTERATION, INSPECTION AND REPAIR. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 7 3.0 GENERAL THE OIL RESIDUE COLLECTION SYSTEM, PART NUMBER BI-1011-1, IS ELIGIBLE FOR INSTALLATION ON BEECHCRAFT KING AIR 200 AND B200 FAMILY OF AIRCRAFT UNDER AUTHORIZATION OF THESE INSTRUCTIONS AND STC # SA4362NM. SERIAL NUMBER OF AUTHORIZED AIRCRAFT ARE AS FOLLOWS BB-2 AND AFTER MODEL 200 AND B200 BL-1 AND AFTER MODEL 200C AND B200C BT-1 AND AFTER MODEL 200T AND B200T BN-1 AND AFTER MODEL 200CT AND B200CT BC-1 AND AFTER MODEL A200 BD-1 AND AFTER MODEL A200 BJ-1 AND AFTER MODEL A200C BP-1 AND AFTER MODEL A200CT BT-1 AND AFTER MODEL A200CT BY-1 AND AFTER MODEL B200GT BZ-1 AND AFTER MODEL B200CGT PRE-MODIFIED AIRCRAFT MUST CONFORM TO INSTALLATION DRAWING BI-1011 (SHEET 1 “MANIFOLD REMOVAL”, SHEET 2 “TYP. HOSE ROUTING”). 3.1 KIT DESCRIPTION INSTALLATION OF THE BUTTERFIELD INDUSTRIES OIL RESIDUE COLLECTION SYSTEM ALLOWS THE COLLECTING OF DRAIN FLUID INTO A SINGLE SUMP ASSEMBLY. THE SUMP HAS A DRAIN VALVE, WHICH CAN BE USED PERIODICALLY TO DRAIN THE TANK. THE SYSTEM WILL ELIMINATE THE OIL MESS ON THE BOTTOM OF THE NACELLE AND ON THE MAIN LANDING GEAR. IT WILL ALSO CLEAN UP THE MESSY OIL SPOTS ON THE HANGAR FLOOR AND RAMP WHEN THE AIRCRAFT IS PARKED. THIS IS A MESS AS WELL AS AN EPA HAZARD. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 8 3.2 KIT CONTENTS THE CONTENTS OF THE BI-1011-1 KIT ARE AS SPECIFIED IN THE LIST OF MATERIALS ON SHEET 1 OF THE DRAWING LISTED IN PARAGRAPH 2.1. ADDITIONALLY, THE KIT CONTAINS A DATA PACKAGE CONTAINING: 1) BI 1013 - “ INSTALLATION INSTRUCTIONS “ 2) A COPY OF THE PACKING LIST ( PAGE 12) 3) DRAWINGS LISTED IN PARAGRAPH 2.1 4) ONE COPY OF THE STC BUTTERFIELD INDUSTRIES SHOULD BE NOTIFIED IMMEDIATELY OF ANY SHORTAGES OR OTHER DISCREPANCIES. 3.3 SPECIALIZED TOOLING REQUIRED

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OTHER THAN STANDARD AIRCRAFT TECHNICIAN’S TOOLS, NO SPECIAL TOOLS REQUIRED. 4.0 AIRPLANE PREPARATION NO SPECIAL AIRPLANE PREPARATION IS REQUIRED PRIOR TO INITIATING INSTALLATION OF THE OIL RESIDUE COLLECTION KIT. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 9 5.0 REMOVALS THE OPERATION DEFINED HERE ARE THOSE NECESSARY TO REMOVE AND ALTER COMPONENTS FROM THE LEFT AND RIGHT HAND NACELLE. THE SEQUENCE OF EVENTS ARE PRESENTED IN A RECOMMENDED SEQUENCE. HOWEVER, THAT SEQUENCE MAY BE ALTERED TO SUIT THE CUSTOMER OR THE INSTALLATION FACILITY. REF. DRAWING BI-1011 SHEET 1 1) GAIN ACCESS TO THE FORWARD SIDE OF THE FIREWALL BY REMOVING COWLING AS REQUIRED. 2) DISCONNECT HOSES FROM EXISTING DRAIN MANIFOLD. 3) REMOVE AND DISCARD MANIFOLD (101-910099-11) AND THE ATTACHING HARDWARE AS SHOWN. 6.0 KIT INSTALLATION THE FOLLOWING PARAGRAPHS DEFINE THE INSTALLATION OF THE OIL RESIDUE COLLECTION SYSTEM. THE ACTIVITIES SPECIFIED HEREIN ARE PRESENTED IN A RECOMMENDED SEQUENCE. HOWEVER, THAT SEQUENCE MAY BE ALTERED TO SUIT THE CUSTOMER OR THE INSTALLATION FACILITY. UNLESS OTHERWISE SPECIFIED, INSTALLATION OF ALL HARDWARE SHALL CONFORM TO FAA-AC 43.13-1A. NOTE: AIRCRAFT MODEL A200 AND EARLY SERIAL NUMBERED AIRCRAFT NOT MODIFIED WITH SERVICE BULLETIN TO DUCT ENGINE VENT LINE THROUGHT THE WHEEL WELL WILL REQUIRE THE BI 4000-5 SUMP ASSEMBLY AND WILL REFER TO DRAWING BI 1011- SHEET 3 FOR INSTALLATION. AN ADDITIONAL HOLE WILL BE REQUIRED IN LOWER COWLING TO ACCOMMODATE VENT TUBE. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 10 6.1 SUMP ASSEMBLY INSTALLATION REF. DRAWING BI 1001 SHEET 2 1) POSITION SUMP ASSEMBLY (BI-4000-1) ON THE ENGINE FIREWALL AS SHOWN. NOTE: THE EXISTING HOLE IN THE COWL MAY REQUIRE ENLARGEMENT TO ACCEPT THE NECK OF THE SUMP ASSEMBLY. 2) ATTACH THE SUMP ASSEMBLY WITH TWO BOLTS (AN3H3A) AND WASHERS (AN960KD10) AT TWO EXISTING NUTPLATE LOCATIONS. 3) SAFETY-WIRE THE TWO BOLTS AS SHOWN. 6.2 HOSE ASSEMBLY INSTALLATION CONNECT HOSES TO SUMP ASSEMBLY IN SAME POSITIONS. 6.3 FINAL INSTALLATION 1) PERFORM A DETAILED INSPECTION OF ALL WORK ACCOMPLISHED. 2) INSTALL ALL COWLING REMOVED TO GAIN ACCESS FOR THE MODIFICATION. NOTE: DRAIN VALVE MAY BE REMOVED DURING COWLING INSTALLATION AND THEN REINSTALLED. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 11 6.4 INSPECTION THERE IS NO INSPECTION CRITERIA FOR THE SUMP. CHECK CONTINUED AIRWORTHINESS INSTRUCTIONS ON PAGE 13 FOR SUGGESTIONS AS TO PERIODIC MAINTENANCE. 7.0 RETURN AIRPLANE TO SERVICE 1) COMPLETE AN APPROPRIATE ENTRY IN THE AIRPLANE LOGBOOK EXAMPLE: INSTALLED BUTTERFIELD INDUSTRIES OIL RESIDUE COLLECTION SYSTEM PART NUMBER 1011-1 AS PER STC SA4362NM. 2) COMPLETE THREE COPIES OF FAA FORM 337. INSERT ORIGINAL IN AIRPLANE FLIGHT MANUAL. MAIL ONE COPY TO LOCAL FAA-FSDO AND RETAIN ONE COPY FOR THE INSTALLER 3) NO WEIGHT AND BALANCE CHANGE Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 12 PACKING LIST KIT P/N BI 1011-1 RESIDUE TANK ASSEMBLY BI 4000-1 2 EA. OR BI 4000-5 (A200) WASHER AN960KD10 4 EA. BOLT AN 3H3A 4 EA. Butterfield Industries, Inc. 208-466-4622 DRAWING NUMBER BI 1013 REV. C PAGE 13 CONTINUED AIRWORTHINESS INSTRUCTIONS THERE ARE NO SCHEDULED INSPECTION PERIODS FOR ANY COMPONENT OF THE BUTTERFIELD INDUSTRIES ‘OIL RESIDUE COLLECTION SYSTEM’. USE THE FOLLOWING GUIDELINES FOR SUCCESSFUL CONTINUED AIRWORTHINESS. ANYTIME THE COWLING IS OPEN FOR INSPECTION, THE OIL RESIDUE TANK SHOULD BE INSPECTED FOR CONDITION AND SECURITY. ALL HOSE CLAMPS TO TANK SHOULD BE INSPECTED FOR CONDITION AND SECURITY. THE TANK SHOULD BE DRAINED ON A PERIODIC BASIS. IF THE TANK IS NOT DRAINED, THE RESIDUE OIL WILL DRAIN FROM THE OVERFLOW TUBE. Butterfield Industries, Inc. 1800 524-3404 ______________________________________________________________ DRAWING NUMBER BI 8025 REV. N/C PAGE 1 INSTRUCTIONS FOR CONTINUED AIRWOTHINESS THERE ARE NO SCHEDULED INSPECTION PERIODS FOR ANY COMPONENET OF THE BUTTERFIELD INDUSTRIES ‘ OIL RESIDUE COLLECTION SYSTEM’. USE THE FOLLOWING GUIDELINES FOR SUCCESSFUL CONTINUED AIRWORTHINESS. ANT TIME THE COWLING IS OPEN FOR INSPECTION, THE OIL RESIDUE TANK SHOULD BE INSPECTED FOR CONDITION AND SECURITY . ALL HOSE CLAMPS TO THE TANK SHOULD BE INSPECTED FOR CONDITION AND SECURITY . THE TANK SHOULD BE DRAINED ON A PERIODIC BASIS. IF THE TANK IS NOT DRAINED, THE RESIDUE OIL WILL DRAIN FROM THE OVERFLOW TUBE. 03/01/11 REV: N/C