AIRCRAFT MAINTENANCE MANUAL...• Component Maintenance Manuals (CMMs) It is the responsibility of the owner or operator to ensur e that the latest revision of the manual is used for

�PLATUSEF

PC-6 B2-H2/B2-H4

AIRCRAFT MAINTENANCE MANUAL

Document No. 01975

Initial Issue: June 14 1991

©PILATUS AIRCRAFT LIMITED 1991 All rights reserved

Pilatus Aircraft Ltd. CH-6370 Stans. Switzerland

PUBLICATION TRANSMITTAL LETTER

FILE THIS TRANSMITTAL IN FRONT OF THE MANUAL

CHECK THAT ALL PREVIOUS TRANSMITTALS HAVE BEEN INCORPORATED

If any Transmittals have not been received, please advise Technical Publications Department, Pilatus Aircraft Ltd Page 1 of 2

PC-6

Pilatus Aircraft Ltd

CH-6371 Stans

Switzerland

Tel +41 41 619 61 11

Fax + 41 41 619 65 93

Email: [email protected]

TO HOLDERS OF:

PC-6 AIRCRAFT MAINTENANCE MANUAL

DOCUMENT NUMBER 01975

REVISION 30

DATED OCT 30/20

HIGHLIGHTS

Pages which have been added or revised are given below together with the highlights of the revision. Remove

and insert the affected pages as listed.

Remove Insert Reason for Change

Chapter 04 - Airworthiness Limitations

04-LEP 1 and 2 1 and 2 Updated.

04-00-00 1 thru 6 1 thru 6 Inspection note added.

Chapter 05 - Time Limits/Maintenance Checks


05-10-10 1 thru 4 1 thru 4 Text updated.


Chapter 06 - Dimensions and Areas



Chapter 20 - Standard Practices


20-10-01 201 thru 206 201 thru 214 Procedures updated.

20-10-06 201 thru 216 201 thru 220 Procedures updated.

20-31-00 1 thru 38 1 thru 38 Consumables updated.

Chapter 27 - Flight Controls

27-LEP 1 thru 4 1 thru 4 Updated.

27-00-00 601 thru 604 601 thru 604 Procedure updated.

PUBLICATION TRANSMITTAL LETTER

FILE THIS TRANSMITTAL IN FRONT OF THE MANUAL

CHECK THAT ALL PREVIOUS TRANSMITTALS HAVE BEEN INCORPORATEDIf any Transmittals have not been received, please advise Technical Publications Department, Pilatus Aircraft LtdPage 2 of 2

PC-6

Chapter 53 - Fuselage




Chapter 57- Wings




Record of Revisions Sheet Record incorporation of this revision and date of incorporation.

Record of Temporary

Revisions Sheet

No changes.

ROR Page 1

PC-6MAINTENANCE MANUAL

RECORD OF REVISIONS

Rev No.

Date of Issue:

Date Inserted:

Signature:Rev No.

Date of Issue:

Date Inserted:

Signature:

1 Incorporated at Issue 26 Incorporated at Issue





6 Incorporated at Issue 31




















ROR Page 2


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ROTR Page 1


RECORD OF TEMPORARY REVISIONS

Temp Rev No.

Date of Issue:

Date Inserted: Signature:

Date Removed / Incorporated in: Signature:

05-01 Oct 25/95 Included Pilatus TR 05-03 Pilatus


05-02 Oct 30/95 Included Pilatus Rev 4 Pilatus

05-03 Feb 03/97 Included Pilatus TR 05-04 Pilatus

05-04 Feb 24/97 Included Pilatus Rev 4 Pilatus

27-02 Oct 23/98 Included Pilatus Rev 5 Pilatus

32-01 Nov 30/99 Included Pilatus Rev 5 Pilatus

05-06 Aug 28/01 Included Pilatus Rev 5 Pilatus

28-01 Sep 04/01 Included Pilatus Rev 5 Pilatus


27-03 Jan 15/02 Included Pilatus Rev 5 Pilatus


27-04 Mar 28/02 Included Pilatus Rev 5 Pilatus

71-01 Jun 07/02 Included Pilatus TR 71-02 Pilatus

71-02 Jun 20/02 Included Pilatus Rev 5 Pilatus

05-07 Jul 05/02 Included Pilatus Rev 5 Pilatus

24-01 Jun 11/04 Included Pilatus Rev 6 Pilatus





27-06 Dec 07/05 Included Pilatus Rev 7 Pilatus


ROTR

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Temp Rev No.

Date of Issue:












25-02 Jan 28/09 Mar 11/09 Pilatus Rev 10 Pilatus

25-03 Jan 28/09 Mar 11/09 Pilatus Rev 10 Pilatus

05-13 Mar 23/10 Mar 29/10 Pilatus Rev 12 Pilatus

55-01 Sep 20/11 Sep 25/11 Pilatus Rev 15 Pilatus


71-03 Feb 27/17 Feb 27/17 Pilatus Rev 25 Pilatus

05-14 Jan 19/18 Jan 19/18 Pilatus Rev 26 Pilatus

53-01 Jun 05/18 Jun 05/18 Pilatus Rev 27 Pilatus


ROTR Page 3


Temp Rev No.

Date of Issue:



ROTR

Page 4


Temp Rev No.

Date of Issue:



EFFECTIVITY: All

CONT

Page 1May 14/10


CONTENTS

Subject Chapter

INTRODUCTION -

SERVICE BULLETIN LIST -

AIRWORTHINESS LIMITATIONS 04

TIME LIMITS / MAINTENANCE CHECKS 05

DIMENSIONS AND AREAS 06

LIFTING AND SHORING 07

LEVELLING AND WEIGHING 08

TOWING AND TAXIING 09

PARKING AND MOORING 10

PLACARDS AND MARKINGS 11

SERVICING 12

STANDARD PRACTICES 20

AIR CONDITIONING 21

ELECTRICAL POWER 24

EQUIPMENT / FURNISHINGS 25

FLIGHT CONTROLS 27

FUEL 28

ICE PROTECTION 30

INDICATING / RECORDING 31

LANDING GEAR 32

LIGHTS 33

NAVIGATION 34

OXYGEN 35

VACUUM 37

DOORS 52

FUSELAGE 53

STABILIZERS 55

WINDOWS 56

WINGS 57

PROPELLER 61

POWERPLANT 71

ENGINE FUEL AND CONTROL 73

EFFECTIVITY: All

CONT

Page 2May 14/10


Subject Chapter

IGNITION 74

ENGINE CONTROLS 76

ENGINE INDICATING 77

EXHAUST 78

OIL 79

STARTING 80

EFFECTIVITY: All

INTRO

Page 1Jan 30/16


INTRODUCTION

1. General

This manual has been prepared using the Air Transport Association of America Specification 100 (ATA 100).

The maintenance manual gives instructions for maintenance personnel to service and maintain the aircraft. It provides sufficient information to inspect, fault isolate and to complete the removal / installation and adjustment / test of equipment as well as the repair of certain systems. To provide as complete a coverage as possible, optional equipment has been included in the manual.

Information which is beyond the scope of this manual may be found in the following manuals:

• Illustrated Parts Catalog (IPC)

• Wiring Diagram Manual (WDM)

• Structural Repair Manual (SRM)

• Component Maintenance Manuals (CMMs)

It is the responsibility of the owner or operator to ensure that the latest revision of the manual is used for servicing and maintenance of the aircraft.

If it is necessary to contact Pilatus Aircraft Ltd. about your aircraft, it is important to include the aircraft serial number in any correspondence. The serial number can be found on the manufacturers data placard, the location of the placard is given in Chapter 11 of the IPC.

Use only parts that have been approved and certified by Pilatus and obtained from Pilatus approved sources for maintenance on the aircraft. Salvaged or reworked parts obtained from non Pilatus approved sources are unsuitable and unsafe for use on the aircraft.

In the event that the aircraft should be maintained and/or operated with parts and/or components which are not approved by the Seller and/or its supplier and vendor, all warranties will be rendered null and void upon installation of such parts and/or components. Pilatus expressly disclaims any and all liability including but not limited to liability for any loss or damage of property, injury or death, in association with any and all malfunctions and/or failures and/or incidents and/or accidents involving such non approved parts and/or components.

CMMs giving overhaul information for components should be obtained direct from the manufacturer or his distributor. The address of component manufacturers can be found in the introduction of the IPC.

A. Copyright and Legal Statements

Pilatus Aircraft Ltd. This document contains proprietary information that is protected by copyright. All rights are reserved. No part of this document may be copied, reproduced or translated to other languages without the prior written consent of Pilatus Aircraft Ltd.

In connection with the use of this document, Pilatus does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential and/or proprietary information of Pilatus and technical data subject to export control laws and regulations, including the U.S. Export Administration Regulations (EAR). Disclosure or distribution of this document contrary to the EAR, and other laws and regulations, is strictly forbidden. The above restrictions may apply to data on all pages of this document.

EFFECTIVITY: All

INTRO

Page 2Jan 30/16


2. Revisions

When necessary, new or replacement pages will be issued to keep the manual up to date.

Normally all pages of each revised topic (page block) are issued in a revision. This is to make the incorporation of the revision into the manual simpler, i.e. remove a complete topic, insert a complete topic.

Regular revisions are supplied with a Transmittal Letter which details the pages which are removed and those replaced by the revision. A brief summary of the changes contained in the revised pages and temporary revisions removed by the revision are also given.

The incorporation of the revision is recorded on the Record of Revisions sheet and removal of temporary revisions is recorded on the Record of Temporary Revisions sheet, both of which are in the front of the manual.

Revisions are shown in the new pages by a revision bar in the left margin against the part of the text or illustration which is changed. If changes make unchanged text move to the next page the revision bar is put next to the page number.

Temporary Revisions are issued when the manual must be revised between normal regular revisions. They are issued on yellow paper and must be filed in the position given on the front sheet. The incorporation of temporary revisions is recorded on the Temporary Revisions Record Sheet. Temporary revisions must only be removed from the manual when instructed on a transmittal letter or when superseded by a temporary revision.

3. Page Dates

The date on a page indicates the date of issue. If changes are done to a page or the text is moved due to changes on other pages, the page date is changed to the date of the revision at which it is issued.

4. List of Effective Pages

The List of Effective Pages, which is at the front of each chapter, lists all pages which appear in the chapter, together with their current date of issue. Each revision has a new List of Effective Pages for the chapters with new or revised pages.

5. Warnings, Cautions and Notes

These are used to stress important items in the text. Warnings and Cautions come immediately before the text to which they refer. Notes are put after the text to which they refer. The uses are given below:

WARNING: GIVES DETAILS OF MATERIALS, PROCESSES, PROCEDURES OR LIMITS WHICH MUST BE FOLLOWED TO AVOID INJURY TO PERSONNEL.

CAUTION: GIVES DETAILS OF METHODS OR PROCEDURES WHICH MUST BE FOLLOWED TO AVOID DAMAGE TO EQUIPMENT.

NOTE: Used to give details of hints or tips which make the task easier for maintenance personnel.

EFFECTIVITY: All

INTRO

Page 3Jan 30/16


6. Manual Breakdown

A. Chapter / Sub-Chapter Guide

The following chapter / system guide is prepared in accordance with both GAMA Specification No. 2 and ATA Specification No. 100 for use with this manual.

04 AIRWORTHINESS LMITATIONS

05 TIME LIMITS / MAINTENANCE CHECKS

06 DIMENSIONS AND AREAS

07 LIFTING AND SHORING

08 LEVELLING AND WEIGHING

09 TOWING AND TAXIING

10 PARKING AND MOORING

11 PLACARDS AND MARKINGS

12 SERVICING

20 STANDARD PRACTICES

21 AIR CONDITIONING

24 ELECTRICAL POWER

25 EQUIPMENT AND FURNISHINGS

27 FLIGHT CONTROLS

28 FUEL

30 ICE AND RAIN PROTECTION

31 INDICATING / RECORDING SYSTEMS

32 LANDING GEAR

33 LIGHTS

34 NAVIGATION

35 OXYGEN

51 STRUCTURES

52 CANOPY

53 FUSELAGE

54 ENGINE COMPARTMENT

55 STABILIZERS

57 WINGS

61 PROPELLER

71 POWERPLANT

73 FUEL AND CONTROL

74 IGNITION

76 ENGINE CONTROLS

77 ENGINE INDICATING

78 EXHAUST

79 OIL

80 STARTING

EFFECTIVITY: All

INTRO

Page 4Jan 30/16


B. Chapter - Section - Subject

The numbering system uses a chapter - section - subject number with the page number to identify each part of the manual.

Example:

C. Page Numbers

The pages are numbered to indicate the type of information.

The page blocks used are:

7. Punctuation in Units of Weight and Measurement

In this manual the decimal fraction is shown by a point in the Imperial / US units of weight and measurement, and by a comma in metric units.

8. Consumable Materials

Consumable materials used on the aircraft during maintenance procedures are listed in Chapter 20-31-00, Consumable Materials List. The list gives details of the material and the supplier, and also gives a material number which is used throughout the manual.

Page Type of Information

1 to 99 Description and Operation

101 to 199 Fault Isolation

201 to 299 Maintenance Practices

301 to 399 Servicing

401 to 499 Removal/Installation

501 to 599 Adjustment/Test

601 to 699 Inspection/Check

701 to 799 Cleaning/Painting

801 to 899 Approved Repairs

28-20-04

Chapter(28 - Fuel)

Section(20 - Distribution)

Subject(04 - Fuel Booster Pump)

EFFECTIVITY: All

INTRO

Page 5Jan 30/16


9. Requests for Revisions

If operators have suggestions for improvements to the content of the manual or errors are found, please submit the proposed changes on the Publication Revision Request Form shown on the following page.

10. Occurrence Reporting Requirements

EASA Implementing Rule Part 21A.3 ‘Failures, Malfunctions and Defects’ requires Pilatus Aircraft Ltd. to maintain a system for collection, investigation and analysis of aircraft malfunction data that fulfils the EASA Reporting Criteria (AMC 20-8) for any occurrence which is reported to the agency. To fulfil this requirement, Pilatus Aircraft Ltd. requests that Operators and Service Centers report all aircraft failures, malfunctions and defects using either:

• The ‘MyPilatus’ internet portal

• A copy of the Aircraft Malfunction Report form, shown on Page 7.

The data supplied will be used to highlight problems and will allow Pilatus to develop modifications to improve reliability and reduce operating costs.

EFFECTIVITY: All

INTRO Page 6Jan 30/16


PUBLICATION REVISION REQUEST

Manual AIRCRAFT MAINTENANCE MANUAL Revision No.

Chapter/Section/Subject Pages

Topic Title

Reason for Change

Proposed Changes

Company Name Date

REMARKS BY TECHNICAL PUBLICATIONS

Name Signature Date

EFFECTIVITY: All

INTRO

Page 7Jan 30/16


Aircraft

Malfunction occurrence

Please indicate either During Operation or During A/C Servicing. One of these must be selected.

Description of Malfunction Corrective Action Pilot Action taken to continue flight: Was the Malfunction reproducible on ground: Maintenance repair action taken: Maintenance remarks:

Component Details Action on reported malfunctioning component:

Repaired (To be) replaced Tested, no fault found

Adjusted / Recalibrated

Finding:

Component Identification Defective Component Details Replacement Component Details

ATA Chapter: Pilatus P/N: Pilatus P/N:

Description: Vendor P/N: Vendor P/N:

If component has been replaced please provide at least the data of the marked fields.

Serial No: Serial No:

Operating Hrs: Operating Hrs:

Landings: Landings:

Engine Cycles: Engine Cycles: Status: New Exchange

General Malfunction Report/Claim No: Pilot Name:

Warranty Claim attached Signature:

Maintainer or Pil. FSE:

Order No. (If available): Signature:

AIRCRAFT MALFUNCTION REPORT Pilatus Aircraft Ltd

P.O. Box 992

6371 Stans, Switzerland

Type: Serial N°: Reg. N°: Operator:

Hrs: Ldg: Last Service: Service Center:

Date of Malfunction: Flight Aborted: No of occurrences:

During Operation Pre Flight Start up Taxi (pre Flight) Take off

Climb Cruise Aerobatic Descent

Landing Taxi (post Flight) Shut down Post Flight

Time into flight: Min OAT: °C Fuel Flow: LBS/HRS

Altitude: FT Cabin Alt: FT Airspeed: KTS

Torque: PSI ITT: °C NG: %

Weather conditions:

During A/C Servicing Type of Service: HR Special Service:

EFFECTIVITY: All

INTRO

Page 8Jan 30/16


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Documents

AIRCRAFT MAINTENANCE MANUAL...• Component Maintenance Manuals (CMMs) It is the responsibility of the owner or operator to ensur e that the latest revision of the manual is used for