***(MANUAL IDENTIFICATION*)**

***INSTRUCTIONS FOR CONTINUED AIRWORTHINESS TEMPLATE***

***(COMPANY NAME)***

**INSTRUCTIONS FOR CONTINUED AIRWORTHINESS**

*(DRAWING/PHOTOGRAPH)*

*(OPTIONAL)*

**(*ROTORCRAFT MAKE AND MODEL*)**

**REVISION:** ***(DATE)***

*Revision 4 Page i*

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**REVISION: (*PAGE NUMBER)***

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+-------+------+-------+----------+-------+-----+-------+-----------+
| **REV | **I  | *     | **BY**   | **REV | **I | **D   | **BY**    |
| ISION | SSUE | *DATE |          | ISION | SSU | ATE** |           |
| NUM   | DA   | INSER |          | NUM   | E** |       |           |
| BER** | TE** | TED** |          | BER** |     | **    |           |
|       |      |       |          |       | **  | INSER |           |
|       |      |       |          |       | DAT | TED** |           |
|       |      |       |          |       | E** |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
| Ori   | 08/0 | 09/   | E. R.    |       |     |       |           |
| ginal | 4/97 | 03/97 | THOMAS   |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
| 1     | 01/3 | 02/   | E. R.    |       |     |       |           |
|       | 0/98 | 14/98 | THOMAS   |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
| 2     | 06/1 | 07/   | E. R.    |       |     |       |           |
|       | 8/98 | 02/98 | THOMAS   |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
| 3     | 10/2 | 11/   | E. R.    |       |     |       |           |
|       | 1/99 | 01/99 | THOMAS   |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
| 4     | 08/0 | 08/   | E. R.    |       |     |       |           |
|       | 4/00 | 24/00 | THOMAS   |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
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+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+
|       |      |       |          |       |     |       |           |
+-------+------+-------+----------+-------+-----+-------+-----------+

**REVISION: (*PAGE NUMBER)***

*Revision 4* *Page iii*

***(MANUAL IDENTIFICATION)***

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**REVISION: (*PAGE NUMBER)***

*Revision 4* *Page iv*

***(MANUAL IDENTIFICATION)***

**LIST OF EFFECTIVE PAGES**

LIST OF REVISIONS Revision 0 (Original Issue)..
\...\...\...\...\....*August 4, 1997*

Revision 1 \...\...\...\...\...\...\...\...\...\...\..........*January
30,1998*

Revision 2 .......................................*June 18,1998*

Revision 3 ...................................*October 21,1999*

Revision 4 .....................................August 4, 2000

LIST OF EFFECTIVE PAGES

[Title]{.underline} [Pages]{.underline} [Revision No.]{.underline}

*COVER i, ii BLANK 4*

*RECORD OF REVISION iii, iv BLANK 4*

*LIST OF EFFECTIVE PAGES v THRU vi 4*

*TABLE OF CONTENTS vii THRU x 4*

*CHAPTER 1 INTRODUCTION 01-00-00 1 THRU 8 4*

*CHAPTER 4 AIRWORTHINESS LIMITATION*

> *SECTION 04-00-00 1, 2 BLANK 4*

*CHAPTER 5 INSPECTIONS 05-00-00 1 THRU 4 4*

*CHAPTER 6 DIMENSION AND ACCESS 06-00-00 1, 2 BLANK 3*

*CHAPTER 7 LIFTING AND SHORING 07-00-00 1, 2 BLANK 2*

*CHAPTER 8 LEVELING AND WEIGHING 08-00-00 1, 2 BLANK 3*

*CHAPTER 9 TOWING AND TAXIING 09-00-00 1, 2 BLANK 2*

*CHPATER 10 PARKING AND MOORING 10-00-00 1, 2 BLANK 4*

*CHAPTER 11 PLACARDS AND MARKING 11-00-00 1, 2 BLANK 4*

*CHAPTER 12 SERVICING 12-00-00 1, 2 BLANK 2*

*CHAPTERS 20, 51, 60, 70, STANDARD PRACTICES ( )-00-00 1, 2 BLANK 3*

*CHAPTERS 21, 22, 23, 24, 25, 26, 27, 29, 30, 31, 33, 34,*

*35, 36, 37, 45, 49, AIRFRAME SYSTEM ( )-00-00*

> *52, 53, 54, 55, 56, STRUCTURES ( )-00-00*
>
> *62, 63, 64, 65, 66, 67 ROTORS ( )-00-00*
>
> *71, 72, 73, 74, 75, 76, 77, 78, 79, 80, and*

*83 POWERPLANT ( )-00-00 1,2 ,3, 4, 5, 3*

*6, 7, 8 4*

*Attachment 1 PART 29 REQUIREMENTS 1, THRU 5, 6 BLANK 4*

*Attachment 2 INSTRUCTIONS FOR CONTINUED*

> *AIRWORTHINESS PROCEDURE INFORMATION 1 AND 2 3*

### Attachment 3 ATA CHAPTER LISTING 1, 2 BLANK 3

*Attachment 4 TYPE DESIGN CHANGE ICA RECOMMENDED*

*PROCEDURE 1, THRU 9,10 BLANK 4*

**REVISION: (*PAGE NUMBER) ****Revision 4* *Page v*

***(MANUAL IDENTIFICATION)***

**LIST OF EFFECTIVE PAGES**

*a. The applicant should provide a means of identifying each page of the
Instructions for Continued Airworthiness (ICA) so maintenance personnel
know they have a complete and current ICA. There is no requirement for a
specific format; however, there is an established standard format that
has been used by industry for many years. This standard is the List of
Effective Pages.*

*b. The applicant should list all pages, revision number, and revision
date contained in the applicant's ICA on a "List of Effective Pages"
page either, for the complete manual or by each chapter. If individual
chapter method is used, the manual should have a master "List of
Effective Pages" page containing all the chapters and revision numbers.*

*c. A page means a single side of a leaf within the ICA. When no text is
intended for a page the following statement should be on the blank
page:* THIS PAGE INTENTIONALLY LEFT BLANK. *In addition, the
intentionally left blank page should contain the manual identification,
revision number, and page number.* *If a page has not been revised from
the original issue, this will always be designated with revision number
"O." It is standard industry practice to list "Revision O" to indicate
an original issue page. The revision number will remain the same until
ICA is accepted by the FAA/AUTHORTY regardless of the number of draft
changes made prior to acceptance.*

d\. *The section that lists multiple chapters and has parentheses (
)-00-00, indicates the information is applicable to any of those
chapters; i.e., Chapters 21, 33, 52, 67, or 71 of the ATA chapter
format. The chapter numbers are not sequential because those missing
chapters are not applicable to rotorcraft.*

**REVISION: (*PAGE NUMBER)***

*Revision 4* *Page vi*

***(MANUAL IDENTIFICATION)***

**TABLE OF CONTENTS**

**Identification Title Page**

*CHAPTER 1 INTRODUCTION 01-00-00 1*

*1. ACCEPTABLE TO THE FAA /AUTHORITY 1*

*2. MANUALS 2*

*3. CONTENTS 2*

*4. SCOPE 2*

*5. PURPOSE 2*

*6. ARRANGEMENT 2*

*7. SUPERSEDED DOCUMENTS 3*

*8. APPLICABILITY 3*

*9. DEFINITIONS 3*

*10. ABBREVIATIONS 3*

*11.ACRONYMS 3*

*12. SYMBOLS 4*

*13. PRECAUTIONS 4*

*14. UNITS OF MEASUREMENT 4*

*15. ICA FOR EACH ENGINE 4*

*16. ICA FOR EACH ROTOR 4*

> *17. ICA FOR EACH APPLIANCE REQUIRED BY THIS*
>
> *CHAPTER 4*

*18. INFORMATION ESSENTIAL TO THE CONTINUED*

*AIRWORTHINESS OF THE ROTORCRAFT 5*

*19. REFERENCED PUBLICATIONS 6*

*20. DISTRIBUTION 7*

*21. ROTORCRAFT FEATURES 7*

*22. CORRECTIONS TO ORIGINAL INSTRUCTIONS FOR*

*CONTINUED AIRWORTHINESS 8*

*23. INDICATING CHANGES TO INSTRUCTIONS FOR*

> *CONTINUED AIRWORTHINESS 8*

*CHAPTER 4 AIRWORTHINESS LIMITATIONS SECTION 04-00-00 1*

*1. AIRWORTHINESS LIMITATIONS INFORMATION 1*

*2. NO AIRWORTHINESS LIMITATIONS INFORMATION*

*REQUIRED. 1*

*CHAPTER 5 INSPECTION REQUIREMENTS AND OVERHAUL*

*SCHEDULE 05-00-00 1*

*1. INSPECTION REQUIREMENTS 1*

*2. COMPONENT OVERHAUL SCHEDULE 3*

*3. NO OVERHAUL REQUIRMENTS 3*

*4. INSPECTION EXAMPLE 3*

**REVISION: *(PAGE NUMBER)***

*Revision 4* *Page vii*

***(MANUAL IDENTIFICATION)***

**TABLE OF CONTENTS**

**(Continued)**

**Identification Title Page**

*CHAPTER 6 DIMENSIONS AND ACCESS 06-00-00 1*

*1. AN EXPLANATION OF THE ROTORCRAFT FEATURES 1*

*2. LOCATION OF ACCESS PANELS 1*

*3. DIAGRAM OF STRUCTURAL ACCESS PLATES AND*

*INFORMATION NEEDED TO GAIN ACCESS FOR*

*INSPECTION WHEN ACCESS PLATES ARE NOT*

*PROVIDED 1*

*CHAPTER 7 LIFTING AND SHORING 07-00-00 1*

*1. LIFTING 1*

*a. JACKING INFORMATION 1*

*b. LIFTING INSTRUCTIONS 1*

*2. SHORING INSTRUCTIONS 1*

*CHAPTER 8 LEVELING AND WEIGHING 08-00-00 1*

*1. LEVELING INFORMATION 1*

*2. WEIGHING AND DETERMINING THE CENTER OF*

*GRAVITY INSTRUCTIONS. 1*

*CHAPTER 9 TOWING AND TAXIING 09-00-00 1*

*1. TOW INSTRUCTIONS 1*

*2. TAXIING INSTRUCTIONS 1*

*CHAPTER 10 PARKING AND MOORING 10-00-00 1*

*1. MOORING INFORMATION 1*

*2. PARKING INFORMATION 1*

*3. STORAGE LIMITATIONS 1*

*CHAPTER 11 PLACARDS AND MARKINGS 11-00-00 1*

*1. PLACARD AND MARKING INFORMATION 1*

*CHAPTER 12 SERVICING 12-00-00 1*

*1. SERVICING INFORMATION 1*

*2. LUBRICATION INFORMATION 1*

*3. EQUIPMENT REQUIRED FOR SERVICING 1*

*4. CONSUMABLE MATERIALS 1*

*CHAPTERS 20,51,60,70 STANDARD PRACTICES ( )-00-00 1*

1.  *STANDARD PRACTICES* *1*

2.  *STANDARD PRACTICES INFORMATION 1*

**REVISION: *(PAGE NUMBER)***

*Revision 4* *Page viii*

***(MANUAL IDENTIFICATION)***

**TABLE OF CONTENTS**

**(Continued)**

**Identification Title Page**

*CHAPTERS 21, 22, 23, 24, 25, 26, 27, 29, 30, 31,33, 34, 35, 36, 37,
45,*

> *49 AIRFRAME SYSTEMS ( )-00-00*
>
> *52, 53, 54, 55, 56. STRUCTURES ( )-00-00*
>
> *62, 63, 64, 65, 66, 67, ROTORS ( )-00-00*
>
> *71, 72, 73, 74, 75, 76, 77, 78, 79, 80, and 83 POWERPLANT ( )-00-00
> 1*

*REQUIREMENTS 1*

*1. INTERFACE INFORMATION 1*

> *2. DESCRIPTION OF ROTORCRAFT AND ITS SYSTEMS AND INSTALLATIONS 1*

*3. DESCRIPTION OF ROTORCRAFT'S ENGINE(S) 1*

*4. DESCRIPTION OF ROTORCRAFT'S ROTOR(S) 2*

*5. DESCRIPTION OF ROTORCRAFT'S APPLIANCES 2*

*6. BASIC CONTROL AND OPERATING INFORMATION 2*

*7. SERVICING INFORMATION 3*

*8. LOCATION OF ACCESS PANELS 3*

*9. LUBRICATION INFORMATION 3*

*10. EQUIPMENT REQUIRED FOR SERVICING 4*

*11. RECOMMENDED PERIODS 4*

*12. DEGREE OF THE INSPECTION 4*

*13. WORK RECOMMENDED 5*

*14. APPLICABLE WEAR TOLERANCE 5*

*15. TROUBLESHOOTING 5*

*16. ORDER AND METHOD OF REMOVAL 6*

*17. ORDER AND METHOD OF REPLACING 6*

*18. GENERAL PROCEDURAL INSTRUCTIONS - TESTING 6*

*19. GENERAL PROCEDURAL INSTRUCTIONS - CHECKING 7*

*20. STORAGE LIMITATIONS 7*

*21. SPECIAL INSPECTION TECHNIQUES 7*

*22. PROTECTIVE TREATMENT 7*

*23. STRUCTURAL FASTENERS 8*

*24. SPECIAL TOOLS 8*

*Attachment 1 PART 29 REQUIREMENTS 1*

*Attachment 2 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS PROCEDURES*

> *INFORMATION 1*

*Attachment 3 ATA CHAPTER LISTINGS 1*

*Attachment 4 TYPE DESIGN CHANGE ICA RECOMMENDED PROCEDURE 1*

**REVISION: *(PAGE NUMBER)***

*Revision 4* *Page ix*

***(MANUAL IDENTIFICATION)***

**TABLE OF CONTENTS**

**(Continued)**

*There is no requirement for a specific format for the Table of
Contents. The Table of Contents may be for the complete manual, chapter,
or for both. When a Table of Contents for each chapter is used, there
should be a Table of Contents listing all chapters in the ICA.*

**REVISION: (*PAGE NUMBER)***

*Revision 4* *Page x*

> **(*MANUAL IDENTIFICATION)***

**CHAPTER 1**

**INTRODUCTION**

*The requirements of Appendix A to Part 29 are identified in **bold
type** and are contained in the Introduction Chapter of this document.
These requirements should be included in the Instructions for Continued
Airworthiness (ICA). Items in regular type are not required by the
Federal Aviation Regulations (FAR)/Joint Airworthiness Regulation (JAR),
but recommend the applicant include those items in the ICA for
standardization and clarity. [The underlined words and sentences are to
emphasize the information]{.underline}. The same requirements exist for
a Type Certificate (TC), Supplemental Type Certificate (STC), or other
changes to the type design as specified in the Type Certificate Data
Sheet accepted under a Field Approval (FA). The term Type Design Change
refers to changes to the type design of the rotorcraft made under TC,
STC, or FA. ICA for Type Design Change (TDC) need not include ATA
chapters not affected by the modification. Appropriate text in regular
type can be copied from the ICA template. Text in italics and the
appendices are for instruction and are not to be copied.*

*This guidance is intended for applicants who are required to comply
with § 29.1529, Amendment 20, to prepare an ICA acceptable to the
FAA/AUTHORITY, and applicants required to prepare an ICA for a major
alteration accepted under a FA. The ICA template may be used by an
applicant preparing an ICA.*

***1. ACCEPTABLE TO THE FAA/AUTHORITY***

***a. The applicant must prepare Instructions for Continued
Airworthiness in accordance with Appendix A to FAR/JAR Part 29 that are
acceptable to the FAA/AUTHORITY. [Reference § 29.1529. ]{.underline}**-
As appropriate.*

*b. For the applicant's proposed ICA to be [acceptable to the
FAA/AUTHORITY]{.underline}, it should contain:*

*(1) The applicable requirements specified in Appendix A to FAR/JAR Part
29.*

*(2) Correct terminology and/or correct references.*

*(3) A Cover Page that will readily identify the publication as the
applicant's ICA for that make and model rotorcraft.*

*(4) A revision control procedure and Record of Revisions that will show
currency of the ICA.*

*(5) A means of identifying each page of the publication and a List of
Effective Pages that lists each page and its revision number.*

*(6) A Table of Contents indicating the subject and location and
providing ease of use for maintenance personnel.*

*c. [FAA/AUTHORITY cannot make a determination of acceptability of the
ICA without a complete ICA and all publications referenced in the
applicant's ICA.]{.underline} [ICA review will be discontinued when it
is determined:]{.underline}*

> *(1) [The ICA is not complete.]{.underline}*
>
> *(2) [That all referenced publications were not submitted with the
> ICA.]{.underline}*

**REVISION: *(PAGE NUMBER)***

*Revision 4* 01-00-00 *Page 1*

**(*MANUAL IDENTIFICATION)***

**CHAPTER 1**

######## INTRODUCTION

**(Continued)**

> *(3) [The applicant did not audit the ICA to ensure it met the
> requirements specified in Appendix A of FAR/JAR Part 29 and this ICA
> template. ]{.underline}*

*d. [No determination of correct spelling, proper grammar, or accuracy
of the information will]{.underline}* *[be made by the
FAA/AUTHORITY]{.underline}*

*e. FAA/AUTHORITY reviews and determines the acceptability of ICA. This
ICA template contains the requirements specified in Appendix A to
FAR/JAR Part 29 and other items which are not specifically required by
the FAR/JAR, but are needed to ensure that maintenance personnel have
complete, correct, and current ICA.*

*f. Acceptance of the ICA is indicated by a signed and dated acceptance
statement on the List of Effective Pages.*

**2. MANUALS. *The ICA must be in the form of a manual or manuals as
appropriate for the quantity of data to be provided. [Reference Appendix
A, A29.2 (a).]{.underline}***

**3. CONTENT. *The contents of the ICA must be prepared in the English
language and must contain all items specified in Appendix A of Parts 29.
[Reference Appendix A, A29.3.]{.underline}***

4\. SCOPE.

a\. *Describe the scope of the ICA.*

*b. The scope normally includes the necessary information to carry out
maintenance on the applicable rotorcraft or modification to a
rotorcraft.*

5\. PURPOSE. De*scribe the purpose of the ICA*.

**6. ARRANGEMENT.**

**a. *The applicant must provide a practical arrangement in the
manual.*** ***[Reference Appendix A, A29.2 (b).]{.underline}***

*b. The Introduction of the ICA should explain the manual arrangement
and how to use it. There is no requirement for any specific format or
arrangement of the manual or manuals.*

c\. For standardization, we recommend using the ATA-100 numbering system
and the format and content of this ICA template.

**REVISION: *(PAGE NUMBER)***

*Revision 4 01-00-00 Page 2*

**(*MANUAL IDENTIFICATION)***

**CHAPTER 1**

**INTRODUCTION**

**(Continued)**

*d. The manual should not be in a mixed arrangement, i.e., a mixture of
written text on both sides of a page and written text on one side of a
page. The preferred method is written text on both sides of a page.*

e*. When there is no written text for a page, the page should contain
the following statement:*

THIS PAGE INTENTIONALLY LEFT BLANK

*The page should be identified in the same manner as the rest of the
pages in the manual and the page listed in the List of Effective Pages.*

7\. SUPERSEDED DOCUMENTS*. For TDCs, the ICA should contain the
following statement:*

> Superseded Documents: The information, procedures, requirements, and
> limitations contained in this Instructions for Continued Airworthiness
> for this type design change supersede the information, procedures,
> requirements and limitations contained in the rotorcraft's maintenance
> manual when the type design change is installed on the Type
> Certificate Holder's rotorcraft.

8\. APPLICABILITY. *The ICA should include the make, model, and serial
number (if applicable) of rotorcraft to which the ICA apply.*

9\. DEFINITIONS. Some w*ords or terms used in the ICA require defining
in the Introduction.*

AUTHORITY means another airworthiness authority that has adopted this
ICA.

10\. ABBREVIATIONS. *Abbreviations used in the ICA should be listed with
their words/terms in the Introduction of the ICA.*

a.  *FAA/AUTHORITY = Federal Aviation Administration or another
    airworthiness authority*

b.  *FAR = Federal Aviation Regulation*

c.  *ICA = Instructions for Continued Airworthiness*

d.  *JAR = Joint Airworthiness Regulations*

e.  *LOAP = List of Applicable Publications*

f.  *TDC = Type Design Changes*

11\. ACRONYMS. *Acronyms used in the ICA should be listed with their
terms in the Introduction of the ICA.*

**REVISION: *(PAGE NUMBER)***

*Revision 4 01-00-00* *Page 3*

**(*MANUAL IDENTIFICATION)***

**CHAPTER 1**

**INTRODUCTION (continued)**

12\. SYMBOLS. *Symbols used in the ICA should be listed with
explanations in the Introduction of the ICA.*

**13. PRECAUTIONS.** Precaution means a measure taken beforehand to
prevent harm.

***a. Any necessary precautions to be taken must be included in the ICA.
[Reference Appendix A, A29.3 (b)(3).]{.underline}***

b.  *The following precautions will differ due to the seriousness of the
    hazard or condition:*

\(1\) **WARNING:** *Could be a maintenance procedure, practice,
condition, etc., that could result in personal injury or loss of life.*

\(2\) **CAUTION:** *Could be a maintenance procedure, practice,
condition, etc., that could result in damage or destruction of
equipment.*

\(3\) **NOTE:** *Could be a maintenance procedure, practice, condition,
etc., or a statement which needs to be highlighted.*

14\. UNITS OF MEASUREMENT

a\. *The ICA contains units of measurements. These measurements could be
instrument readings, temperatures, pressures, tolerances, limits, or
torque values.*

*b. It is recommended the ICA contains both United States standard
measurements and Metric measurement, for each measurement, tolerance, or
torque value. A general conversion chart is not acceptable.*

***15. ICA FOR EACH ENGINE***

***a. The ICA must include ICA for each engine. [Reference Appendix A,
A29.1 (b).]{.underline}***

*b. ICA for type certificated engines are accepted by the FAA/AUTHORITY
responsible for engines and could be included by reference in the
applicant's ICA.*

c\. ICA for non-type certificated engines are prepared by the applicant
and submitted to appropriate FAA/AUTHORITY for review and evaluation.

***16. ICA FOR EACH ROTOR***

***a. The ICA must include ICA for each rotor. [Reference Appendix A,
A29.1 (b).]{.underline}***

b\. ICA for rotors is normally included in the rotorcraft ICA.

***17. ICA FOR EACH APPLIANCE REQUIRED BY THIS CHAPTER***

**a. *The ICA must include ICA for each appliance required by
FAR/JAR.***

> ***[Reference Appendix A, A29.1 (b).]{.underline}***

**REVISION: *(PAGE NUMBER)***

*Revision 4 01-00-00* *Page 4*

**(*MANUAL IDENTIFICATION)***

**CHAPTER 1**

**INTRODUCTION (continued)**

*b. FAA/AUTHORITY‑accepted ICA for* *an appliance could be included by
reference in the applicant's ICA.*

*c. [When an appliance is required to be installed by a TDC, the
appliance is required by FAR/JAR and the applicant must prepare ICA that
is acceptable to the FAA/ AUTHORITY.]{.underline}*

*d. The FAA/AUTHORITY‑accepted appliance ICA normally does not address
interface information. The applicant should prepare information on how
that appliance interfaces with the rotorcraft. Interface information
should include appliance location, appliance attachment, if applicable,
the system(s) from which the appliance receives it electrical power,
fluid (fuel, oil, hydraulic, etc.), vacuum, pneumatic, etc., and how the
appliance is controlled.*

*e. When the ICA for an appliance is not FAA/AUTHORITY accepted, the
applicant should prepare the ICA for that appliance which meets the
requirements specified in Appendix A to FAR/JAR Part 29. The ICA for
each appliance could be a stand-alone document or could be included in
the applicant's ICA document for that TDC.*

*f. When an original appliance is replaced with a different appliance as
part of the TDC, the applicant should prepare the ICA for that appliance
which meets the requirements specified in Appendix A to FAR/JAR Part 29.
A different appliance is one that has a different part number, model
number, or is made by the same manufacturer or different manufacturer.*

g*. As defined in FAR/JAR Part 1, [Appliance]{.underline} means any
instrument, mechanism, equipment, part, apparatus, appurtenance, or
accessory, including communications equipment, that is used or intended
to be used in operating or controlling an aircraft in flight, is
installed in or attached to the aircraft, and is not part of an
airframe, engine, or propeller. Avionics equipment is an appliance.*

> *NOTE: Some applicants may wish to include Amendment 20 to FAR/JAR
> Part 29 in the certification basis for their TDC and prepare the ICA
> for their TDC even though the certification basis for the rotorcraft
> does not require acceptance of the ICA by the FAA/AUTHORITY. These
> applicants will be required to obtain FAA/AUTHORITY acceptance for
> their ICA.*

**18. INFORMATION ESSENTIAL TO THE CONTINUED AIRWORTHINESS OF THE
ROTORCRAFT**

> **a. If ICA are not supplied by the manufacturer of an appliance or
> product (engine or rotor), t*he ICA must include the information
> essential to the continued airworthiness of the rotorcraft. [Reference
> Appendix A, A29.3 (b)(3).]{.underline}***

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**CHAPTER 1**

**INTRODUCTION (continued)**

*b. The applicant should include in their ICA the information necessary
to service, maintain, and inspect the rotorcraft, its engines, rotors,
and appliances, in an airworthy condition and ensure they meet type
design. Appendix A to FAR/JAR Part 29 specifies minimum requirements.
The applicant determines the information essential to the continued
airworthiness.*

*c. The information essential to the continued airworthiness of the
rotorcraft its engines, rotors, and appliances could be contained in the
applicant's ICA, engine ICA, appliance ICA, or other
applicant‑associated publications, i.e., overhaul manuals, illustrated
parts catalog, or flight manual. Those ICAs and associated publications
that are listed in the applicant's [List of Applicable Publications
(LOAP]{.underline}) constitute the required information essential for
continued airworthiness for that rotorcraft, its engines, rotors, and
appliances or that TDC. The LOAP is contained in the Introduction
section of the applicant's ICA. The LOAP should contain one of the
following statements:* "The publications listed in the LOAP constitute
the required information essential for continued airworthiness for the
rotorcraft" or "The publications listed in the LOAP constitute the
required information essential for continued airworthiness for the TDC."

**19. REFERENCED INFORMATION**

a.  **Appendix A to FAR/JAR Part 29 allows an applicant to refer to an
    [accessory, instrument]{.underline}, or [equipment]{.underline}
    manufacturer as the source of this information [if the applicant
    shows that the item has an exceptional high degree of complexity
    requiring specialized maintenance techniques, test equipment, or
    expertise.]{.underline}**

b\. When the applicant has shown that the accessory, instrument, or
equipment meets the requirements of 19a above, the manufacturer's
information could be referred to as the source of the information. The
information refers to those specified in Appendix A, Section A29.3,
Contents, Paragraph (b)(1). [The applicant has responsibility for
securing authorization to use that information in their
ICA.]{.underline}

c\. The information is limited to scheduling for each of the
accessories, instruments, and equipment providing the recommended
periods at which they should be cleaned, inspected, adjusted, tested,
and lubricated. In addition, they could be the source of information for
the degree of inspection, applicable wear tolerances, and work
recommended at these periods.

d\. The FAR/JAR allows an applicant to refer to Engine ICA and Appliance
ICA, which are FAA/AUTHORITY‑accepted, and the applicant's associated
publications in the applicant's ICA. See Introduction Section,
Paragraph's 15, 16, and 17.

e\. Any ICA or associated publications referenced in the applicant's ICA
should be submitted with the applicant's ICA.

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**CHAPTER 1**

**INTRODUCTION**

**(Continued)**

**20. DISTRIBUTION**

**a. *The ICA must include a program to show:***

***(1) Distribution of changes to the ICA made by the applicant.***

***(2) Distribution of changes to the ICA made by the manufacturer of
the engine or engines, rotor or rotors, and appliances installed on the
rotorcraft**.*

***[Reference Appendix A, A29.1 (c)]{.underline}.***

*b. The introduction of the applicant's ICA should contain the procedure
used to distribute changes to persons who maintain the rotorcraft or who
have incorporated the TDC.*

*c. When the applicant has referenced FAA/AUTHORITY accepted
publications in their ICA, the procedure used to ensure changes to those
referenced publications are distributed to persons who maintain the
rotorcraft or who have incorporated the TDC. The procedures should be
explained in the introduction of the applicant's ICA.*

*d**.** ICA normally includes a procedure for making changes to the
applicant's ICA. The introduction should include a description of the
revision procedure. The procedure should contain information on the type
of revisions, composition of the revision, revision control procedure,
revision log page, updating procedure, and procedure for purchase of
revisions and renewal of subscription.*

**21. ROTORCRAFT FEATURES**

**a. *The ICA must include introduction information that includes:***

***(1) An explanation of the rotorcraft's features; and,***

***(2) Data to the extent necessary for maintenance and preventive
maintenance.** **[Reference Appendix A, A29.3 (a)(1).]{.underline}***

*b. The ICA normally contain a description which includes:*

*(1) The explanation of the rotorcraft's features:*

*(a) General information about the rotorcraft features.*

*(b) Exterior features.*

*(c) Interior features including cockpit, and cabin.*

*(d) Other features.*

*c. A figure showing the features is helpful and does not require
detailed explanation.*

*d. The data necessary for maintenance and preventive maintenance is
normally described in the applicable chapter and is determined by the
applicant.*

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**CHAPTER 1**

**INTRODUCTION**

**(Continued)**

*22. CORRECTIONS TO ORIGINAL INSTRUCTIONS FOR CONTINUED AIRWORTHINESS.*

22. 

*a. [Any correction made to Draft Instructions for Continued
Airworthiness prior to FAA/AUTHORITY acceptance should have the same
revision number and date as the draft page originally
submitted]{.underline}.*

b\. *Changes or corrections made to ICA after FAA/AUTHORITY acceptance
of ICA are considered to be a revision.*

*23. INDICATING CHANGES TO INSTRUCTIONS FOR CONTINUED AIRWORTHINESS.*

*The applicant could use any means to indicate changes to their ICA. The
following is an example used in the ICA template.*

*a. Any change to the ICA should be indicated as follows:*

> *(1) Changes made to a line should be indicated by a vertical bar in
> the left margin next to the line.*
>
> *(2) Changes made to a paragraph should be indicated by a vertical bar
> in the left margin*

*next to the paragraph letter or number.*

3.  *Changes made to a complete page should be indicated by a vertical
    bar to the right of the page number.*

*b. Only revisions should contain change bars*. *Change bars are used to
indicate changes for that revision. Previous change bars should be
removed at the next revision.*

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**CHAPTER 4**

**AIRWORTHINESS LIMITATION SECTION**

1.  **AIRWORTHINESS LIMITATIONS INFORMATION**

***a. The ICA must have in the principal manual a section titled
"Airworthiness Limitations." This section should be segregated and
clearly distinguishable from the rest of the maintenance manual and
contain:***

***(1) Each mandatory replacement time.***

***(2) Each structural inspection interval and related structural
inspection procedure approved under §§ 29.571.***

***(3) A legible statement in a prominent location indicating that the
Airworthiness Limitations section is FAA/AUTHORITY approved and
specifies required maintenance and/or inspections. The exact, required
wording of this statement is found in the FAR/JAR. [Reference Appendix
A, A29.4]{.underline}***

*b. The Airworthiness Limitations Section will be evaluated and approved
by FAA/AUTHORITY.*

*2. NO AIRWORTHINESS LIMITATIONS INFORMATION REQUIRED:*

*When the applicant's TDC has no airworthiness limitations, the
Airworthiness Limitations Section of the ICA should contain the
following statement:*

"No airworthiness limitations associated with this type design change."

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**CHAPTER 5**

**INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE**

**1. INSPECTION REQUIREMENTS -**

**a. T*he ICA must include:***

***(1) The recommended period at which each part of the rotorcraft and
its engine(s), auxiliary power unit, rotor(s), accessories, instruments
and equipment shall be inspected. [Reference Appendix A, A29.3
(b)(1).]{.underline}***

***(2) The degree (scope) of the inspection for each part of the
rotorcraft and its engine(s), auxiliary power unit, rotor(s),
accessories, instruments and equipment. [Reference Appendix A, A29.3
(b)(1).]{.underline}***

***(3) An inspection program that includes the frequency and extent of
the inspection necessary to provide for the continued airworthiness of
the rotorcraft. [Reference Appendix A, A29.3 (b)(1).]{.underline}***

*b. This chapter should contain a schedule of the interval for all
inspections. The inspection intervals may be in hours and/or calendar
time.*

*c. In the introduction of this chapter, it should explain all required
inspections and should include:*

1.  *The different type of inspections.*

*(a) Scheduled inspections.*

b.  *Special inspections.*

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b.  *Conditional inspections.*

*(2) An explanation of each inspection.*

3.  *A list of all inspections (daily, 300‑hour, 600‑hour, annual,
    special inspection, etc.).*

*d. This chapter should contain the scope of the inspection(s). It
should also describe the intent of the inspection and should address at
least the following:*

1.  *What the inspector should be looking for when inspecting the
    product or appliance (cracks, corrosion, delamination, dents, bends,
    wear, etc.).*

2.  *Location of the product or appliance to be inspected.*

3.  *Any special techniques required to inspect the product or
    appliance.*

4.  *Instructions to be followed when inspecting the product or
    appliance.*

5.  *Any tools or equipment required to accomplish the inspection of the
    product or appliance.*

6.  *The wear tolerances for a product or appliance when the inspection
    requires the product or appliance to meet a standard.*

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e.  *This chapter should contain an inspection program which contains an
    outline of the order of the inspections and instructions to be
    followed during the inspection and should include:*

> *(1) General information such as:*

(a) *The title of the inspection.*

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**CHAPTER 5**

**INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE**

**(continued)**

> *(b) Aircraft information (registration number, serial number, total
> time in service).*
>
> *(c) General information about the inspection.*

d.  *Provide a block for the inspector or maintenance personnel to
    initial when each item has been inspected or action taken.*

e.  *Provide a signature line for the inspector and maintenance
    personnel to sign when the inspection has been accomplished.*

f.  *Provide a place to enter the date the inspection was completed.*

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2.  *Pre‑inspection activities such as:*

> *(a) Maintenance records review.*

b.  *Airworthiness Directive review.*

c.  *Overhaul and life limits requirements review.*

> *(3) Maintenance practices are associated with an inspection such as:*

*(a) Removal of cowling, panels, plates, and covers to access items
being inspected.*

> *(b) Cleaning of the item to be inspected. Specify type and number of
> cleaning*
>
> *material.*
>
> *(c) Specify tools and/or equipment required for the particular
> inspection, i.e., torque wrench, hydraulic unit, etc.*

4.  *The inspection should include:*

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a.  *Locate the item(s) to be inspected.*

b.  *Identify what the inspector should be inspecting (security, wear,
    damage, corrosion, etc.).*

c.  *Instructions specified for that inspection.*

d.  *Using the required inspection techniques.*

e.  *Using tools and equipment specified for that inspection.*

f.  *Determine that the item(s) being inspected meet the airworthiness
    standard established for that product or appliance.*

g.  *Recording of inspection findings.*

> *\# NOTE: Most of the above information is normally contained in an
> inspection form which inspection personnel could copy and use.*

*(5) Type of action to be taken when inspected item is unsatisfactory.*

> *(6 Post inspection actions such as:*

a.  *Application of protective coatings removed for inspection.*

b.  *Servicing and lubrication requirements.*

c.  *Installation of cowling, panels, plates, and covers removed for
    inspection.*

d.  *Post inspection run up and system operation.*

e.  *Maintenance record entry.*

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**CHAPTER 5**

**INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE**

**(continued)**

> *f. If applicable this chapter should include any special inspection
> techniques such as:*
>
> *(1) Radiographic.*

2.  *Ultrasonic.*

> *g. Inspection interval extension statement in the ICA is not
> acceptable to the FAA. For those airworthiness authorities that allow
> extensions, the following statement should be included in this
> chapter:*

"Inspection interval extension may be used if approved by the
airworthiness authority."

**2. COMPONENT OVERHAUL SCHEDULE**

**a. *The ICA must include:***

***(1) The recommended overhaul periods.***

***(2) Necessary cross-references to the Airworthiness Limitations
Section.***

***[Reference Appendix A, A29.3 (b)(1)]{.underline}.***

*b. The Component Overhaul Schedule normally includes:*

*(1) Component's part number.*

*(2) Component's nomenclature.*

*(3) Time Between Overhaul Interval in hours or calendar time.*

*c. Notes may be used to provide information about the requirements.*

*3. NO OVERHAUL REQUIREMENTS*

*a.* When there are no overhaul requirements, the following statement
should be included in Chapter 5 of the ICA.

"No component overhaul required for this type design change."

*4. INSPECTION EXAMPLE*

a\. To assist in preparing an inspection program, an Inspection Example
is provided on the next page. We recommend making the Inspection Example
an appendix and last page of the ICA, so maintenance personnel can copy
the Inspection Program, add the STC inspection to the rotorcraft's
inspections, and use it to inspect the appliance.

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**INSPECTION EXAMPLE: 100-Hour Inspection**

N\_\_\_\_\_\_\_\_ Serial Number \_\_\_\_\_\_\_\_\_\_\_\_\_\_ Aircraft
Hours\_\_\_\_\_\_\_\_\_ Total Time \_\_\_\_\_\_\_\_\_\_

The 100-hour inspection shall be accomplished each 100 hours
time-in-service.

Initial each item after accomplishing the inspection.

Record all findings and attach a copy to this inspection form.

After correction of all findings, make maintenance record entry.

+--------------------------------------------------------------+-------+
| ## PRE‑INSPECTION INITIAL EACH ITEM AFTER ACCOMPLISHMENT     | IN    |
|                                                              | ITIAL |
+--------------------------------------------------------------+-------+
| 1\. *Describe pre‑inspection actions*                        |       |
|                                                              |       |
| Example 1. Review Rotorcraft and Engine Maintenance Records. |       |
+--------------------------------------------------------------+-------+
| Example 2. Review Airworthiness Directives.                  |       |
+--------------------------------------------------------------+-------+

  -------------------------------------------------------------- ---------
  **MAINTENANCE PRACTICES** INITIAL EACH ITEM AFTER              INITIAL
  ACCOMPLISHMENT                                                 

  1\. *Describe access panel to be removed and door to be        
  opened.*                                                       

  Example 1. Remove access panel P3, P4, P5, P6, P7, P8, D1, D5, 
  D10, D15 etc.                                                  

  2\. *Describe maintenance action required to accomplish the    
  inspection.*                                                   

  Example 1. Clean (appliance) using Arro ACR-223 solvent.       

  Example 2. Lubricate (appliance) in accordance with Chapter    
  12.                                                            

  *3. Describe special tool and equipment required for the       
  inspection.*                                                   

  Example 1. Place jacks under helicopter and jack up aircraft.  

  Example 2. Use a 10-power magnifying glass and bright light    
  required for inspection.                                       
  -------------------------------------------------------------- ---------

+--------------------------------------------------------------+-------+
| ## INSPECTION INITIAL EACH ITEM AFTER ACCOMPLISHMENT         | IN    |
|                                                              | ITIAL |
+--------------------------------------------------------------+-------+
| *1. Describe the item being inspected, its location, and     |       |
| what the item is being inspected for. Provide any special    |       |
| instructions or technique to be used, identify special tool  |       |
| required, and provide information on the standard that the   |       |
| item should meet.*                                           |       |
|                                                              |       |
| Example 1. (Appliance)                                       |       |
|                                                              |       |
| Inspect (appliance) for cleanliness, corrosion and security. |       |
+--------------------------------------------------------------+-------+
| Example 2. (Appliance)                                       |       |
|                                                              |       |
| > Inspect (appliance) for scratches, dent, delamination and  |       |
| > cracks. Cracks up to .040 may be repaired. Appliance with  |       |
| > cracks longer than .040 part should be replaced.           |       |
+--------------------------------------------------------------+-------+
| Example 3. (Appliance)                                       |       |
|                                                              |       |
| Inspect (appliance) for due dates and expiration.            |       |
+--------------------------------------------------------------+-------+
| Example 4. (Appliance)                                       |       |
|                                                              |       |
| > Inspect (appliance) for security, lack of lubrication, and |       |
| > freedom of                                                 |       |
| >                                                            |       |
| > Movement, and wear. Acceptable wear is .003 to .005.       |       |
+--------------------------------------------------------------+-------+
| Example 5. (Appliance)                                       |       |
|                                                              |       |
| > Inspect (appliance) attachment nuts for correct torque.    |       |
| > Set torque wrench to 22-inch lbs. and torque nut. If nut   |       |
| > moves, replace (appliance).                                |       |
+--------------------------------------------------------------+-------+
| Example 6. (Appliance)                                       |       |
|                                                              |       |
| Inspect (Appliance) for correct operations, etc.             |       |
+--------------------------------------------------------------+-------+

+--------------------------------------------------------------+-------+
| ## POST INSPECTION INITIAL EACH ITEM AFTER ACCOMPLISHMENT    | IN    |
|                                                              | ITIAL |
+--------------------------------------------------------------+-------+
| *Describe post actions such as protective coating, servicing |       |
| or lubrication appliances, installation of access panels and |       |
| doors, run up and system operations.*                        |       |
+--------------------------------------------------------------+-------+
| Example 1. Complete maintenance practices for the            |       |
| inspection, i.e., install access panels and close doors      |       |
| opened for the inspection, remove aircraft form jacks, etc.  |       |
+--------------------------------------------------------------+-------+
| Example 2. Perform run up or system operation and verify     |       |
| correct function and operation.                              |       |
+--------------------------------------------------------------+-------+
| Example 3. Complete and sign aircraft's maintenance record   |       |
| entry                                                        |       |
+--------------------------------------------------------------+-------+

Mechanic Name \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Signature\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_ \#
\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Inspector Name \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Signature\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_ \#
\_\_\_\_\_\_\_\_\_\_\_\_\_\_

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**CHAPTER 6**

**DIMENSIONS AND ACCESS**

**1. AN EXPLANATION OF THE ROTORCRAFT FEATURES**

a.  ***The ICA must include the features of the rotorcraft.***

***[Reference Appendix A, A29.3 (a)(1).]{.underline}***

*b. The dimensions are part of the rotorcraft's features and normally
include:*

*(1) Principal dimensions of the rotorcraft.*

*(2) Dimensions of the rotorcraft.*

*(a) Exterior dimensions.*

*(b) Interior dimensions.*

*(3) Layout of the rotorcraft.*

*(4) Divisions of the structure - zones and zonal groups.*

*(5) Airframe reference lines.*

*(a) Stations lines.*

*(b) Water Lines.*

*(c) Buttocks Lines.*

**2. LOCATION OF ACCESS PANELS**

**a. *The ICA must include the location of access panels for inspection
and servicing. [Reference Appendix A, A29.3 (a)(4).]{.underline}***

*b. Access information normally includes:*

*(1) Description of access panel, plates, doors, and cowlings.*

*(2) Location of access panels plates, doors, and cowlings.*

*(3) Procedure for removing and installing access panels and doors.*

*(4) Figures showing dimensions and locations of access panels and
doors.*

*c. To prevent removal of all access panels, plates, doors, and cowling
for each inspection, the access panels, plates, doors, and cowling
should be identified. Only those identified would need to be removed for
each inspection. The use of a figure to identify those access panels,
plates, doors, and cowling is recommended.*

**3. DIAGRAM OF STRUCTURAL ACCESS PLATES AND INFORMATION NEEDED TO GAIN
ACCESS FOR INSPECTION WHEN ACCESS PLATES ARE NOT PROVIDED.**

a.  **The ICA must include structural access plate information.**

***[Reference Appendix A, A29.3 (c).]{.underline}***

*b. If applicable, the ICA should identify those structural access
plates.*

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**CHAPTER 7**

**LIFTING AND SHORING**

**1. LIFTING. *The ICA must include instructions including procedures
for lifting. Lifting instructions are divided in two areas - jacking
information and lifting instructions. [Reference Appendix A, A29.3
(b)(4).]{.underline}***

**a. JACKING INFORMATION**

**(1) *The ICA must include information for jacking. ***

*(2) Jacking information normally includes:*

*(a) A description of the jacking system.*

*(b) Location of jack pads.*

*(c) Procedure for installing and removing jack pads.*

*(d) Procedure for installation and removal special fixtures.*

*(e) Specify special tools and equipment required for jacking.*

> *(f) The minimum capacity of the jacks required.*
>
> *(g) Procedure for jacking includes: action to be accomplished before
> jacking, the*

*order and method of jacking helicopter, and actions to be accomplished
after jacking.*

*(h) Precautions to be taken.*

**b. LIFTING INSTRUCTIONS**

**(1) *The ICA must include instructions for lifting. ***

*(2) Lifting instructions normally include:*

*(a) A description of the lifting system.*

*(b) Location of hoist attachments.*

*(c) Procedure for installing and removing lifting tools and equipment.*

*(d) Special tools and equipment required for lifting.*

*(e) The minimum capacity of the lifting equipment.*

*(f) Procedure for lifting includes: actions to be accomplished before
lifting, the order and method of lifting the helicopter, and actions to
be accomplished after lifting.*

*(g) Precautions to be taken.*

**2. SHORING INSTRUCTIONS**

**a. *The ICA must include instructions including* procedures for
shoring. *[Reference Appendix A, A29.3 (b)(4) . ]{.underline}***

*b. Shoring instructions normally include:*

*(1) A description of the task to be accomplished prior to shoring the
rotorcraft.*

*(2) A description of the order and method of shoring the rotorcraft.*

*(3) Special procedures to be used during shoring of the rotorcraft.*

*(4) Specify precautions to be used during shoring of the rotorcraft.*

*(5) Specify tool(s), special tool(s), or equipment required for
shoring.*

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**CHAPTER 8**

**LEVELING AND WEIGHING**

**1. LEVELING INFORMATION**

**a. *The ICA must include leveling information. [Reference Appendix A,
A29.3 (a)(4).]{.underline}***

*b. Leveling information normally includes:*

*(1) A description of the leveling system.*

*(2) Location(s) of the leveling points.*

*(3) Procedure for installation and removal of special fixtures required
for leveling.*

*(4) Description of the fixtures and their location.*

*(5) Special tools and equipment required for leveling.*

*(6) Procedure for leveling including: actions required before leveling;
the order and method of leveling the helicopter; and actions required
after leveling.*

*(7) Any precaution to be taken.*

**2. WEIGHING AND DETERMINING THE CENTER OF GRAVITY INSTRUCTIONS**

**a. *The ICA must include weighing and determining center of gravity
instructions. [Reference Appendix A, A29.3 (a)(4).]{.underline}***

*b. Weighing and determining the center of gravity instructions should
include:*

*(1) A description of the weighing system.*

*(2) Location(s) of the weighing points.*

*(3) Special tools or equipment required for weighing.*

*(4) Procedure for weighing includes actions to be taken before
weighing, the order and method of weighing the helicopter, and actions
to be taken after weighing.*

*(5) Procedure for determining the basic weight and center of gravity.*

*(6) Samples of weighing forms.*

*(7) Any precautions to be taken.*

*c. When a TDC is made and the weight and balance procedure in the
rotorcraft maintenance manual will not change, the applicant need only
provide for each product or appliance the weight and location (arm).*

*d. The use of a table is recommended.*

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**CHAPTER 9**

**TOWING AND TAXIING**

**1. TOW INSTRUCTIONS**

***a. The ICA must include tow instructions and limitations.***

***[Reference Appendix A, A29.3 (a)(4).]{.underline}***

*b. Tow instructions normally include:*

*(1) A description of the landing gear (skids type or wheel type).*

*(2) A description of the towing devices.*

*(3) Procedures for installation and removal of ground handling wheels
and towing devices.*

*(4) Procedures for towing and maneuvering.*

*(5) Towing limitations, including speed, turning radius, and clearance
requirements.*

*(6) Precautions to be taken while towing.*

**2. TAXIING INSTRUCTIONS**

> ***a. The ICA must include basic control and operating information.***
>
> ***[Reference Appendix A, A29.3 (a)(3).]{.underline}***

*b. Taxiing instructions normally include:*

*(1) A description of the controls required to taxi the rotorcraft.*

*(2) A procedure for starting and taxiing the rotorcraft.*

*(3) Taxi limitation - speed turning radius and clearance requirements.*

*(4) Precautions to be taken.*

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**CHAPTER 10**

**PARKING AND MOORING**

**1. MOORING INFORMATION**

**a. *The ICA must include mooring information. [Reference Appendix A,
A29.3 (a)(4).]{.underline} ***

*b. Mooring information normally includes:*

*(1) A description of mooring points and fittings.*

*(2) Location of mooring points and fittings.*

*(3) Procedures for removing and installing fairings.*

*(4) Procedures for installing and removing mooring fittings.*

*(5) Procedures for mooring rotorcraft in standard and rough weather.*

*(6) Procedures for mooring rotorcraft on land or on a ship.*

*(7) Limitations associated with mooring.*

*(8) Precautions to be taken while mooring the rotorcraft.*

*c. Figures may be used to describe mooring points, fitting locations,
and limitations.*

2\. PARKING INFORMATION

a\. *The FAR/JAR do not require parking information. It is recommended
that parking information be included.*

*b. Parking information normally includes:*

*(1) A description of the controls required to park the rotorcraft.*

*(2) A procedure for parking the rotorcraft.*

*(3) Equipment required for parking.*

*(4) Parking limitation: slope and clearance requirements.*

*(5) Precautions to be taken during parking.*

**3. STORAGE LIMITATIONS**

**a. *The ICA must include storage limitations. [Reference Appendix A,
A29.3 (b)(4).]{.underline} ***

*b. Only storage limitations are required, but storage information
normally includes:*

*(1) Type of storage: short term, long term.*

*(2) Storage environments: desert, salt air, cold weather, etc.*

*(3) Identification of parts and system which should be preserved during
storage.*

*(4) A description of order and method of preparing the rotorcraft for
storage.*

*(5) Storage limitations.*

*(6) Procedures for installing and removing covers.*

*(7) Procedures for interim maintenance or inspection task of the
rotorcraft during storage.*

*(8) Procedures for preparing the rotorcraft for operations after
storage.*

*(9) Precautions to be taken while storing the rotorcraft.*

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**CHAPTER 11**

**PLACARDS AND MARKINGS**

*1. PLACARD AND MARKING INFORMATION*

*a. Although there is no requirement for placards or markings to be in
the ICA, placards and markings for the rotorcraft are part of the type
design of the rotorcraft and are contained in type design drawing.*

*b. The placards and markings information normally include:*

*(1) General information about placards and markings.*

*(2) Index of exterior placards and markings.*

*(3) Index of interior placards and markings.*

*(4) Location of placards and markings.*

*(5) A procedure for installing and removing placards and markings.*

*(6) Figures may be used to show placards and markings, and their
location.*

c\. *Maintenance personnel are required to ensure the rotorcraft meets
its type design. To accomplish this, maintenance personnel need to know
what placard and markings are required to be on the rotorcraft;
therefore, the information on placards and markings should be in the
ICA.*

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**CHAPTER 12**

**SERVICING**

**1. SERVICING *INFORMATION***

**a. *The ICA must include servicing information. [Reference Appendix A,
A29.3 (a)(4). ]{.underline}***

***b. Servicing Information***

***(1) Servicing information covers details regarding servicing points,
capacities of tanks and reservoirs, types of fluids to be used, and
pressures applicable to the various systems.***

*(2) Servicing information normally includes:*

*(a) Information applying to fuel system and to other systems if ICA
describes other tanks. If the tank capacity is not on the tank, the
location of the information should be provided.*

*(b) The type of fluid, specification, and name of fluid identification
number. Figures and tables may be used for fluid identification.*

***2. LUBRICATION INFORMATION***

***a. Lubrication information covers details regarding locations of
lubrication points and the type of lubricants to be used.***

*b. Lubrication information normally includes the type of lubricant,
specification, name of lubricant, identification number, and precautions
to be taken. Figures and tables may be used to identify lubricants.*

**3. EQUIPMENT REQUIRED FOR SERVICING**

**a. The ICA must include the equipment required for servicing.**

b\. *Service information normally includes information on the equipment
required for servicing, lubricating, draining, and pressurizing the
applicable systems installed in the rotorcraft. These systems could
include fuel system, engine oil system, gearbox oil system, hydraulic
system, landing gear system, battery, rotor system, rotor drive, tires,
etc. This equipment should be included in the List of Special Tools.*

**4. CONSUMABLE MATERIALS**

***The ICA must include the types of fluids to be used, types of
lubricant to be used, and any storage limitations.***

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**CHAPTERS 20, 51, 60, 70**

**STANDARD PRACTICES**

1\. STANDARD PRACTICES:

*a. Chapters containing standard practices are:*

*Chapter 20, Airframe Standard Practices 20-00-00*

*Chapter 51, Structures Standard Practices 51-00-00*

*Chapter 60, Rotor Standard Practices 60-00-00*

*Chapter 70, Powerplant Standard Practices 70-00-00*

*b. There are no specific requirements for a Standard Practices
Chapter.*

*2. STANDARD PRACTICES INFORMATION. Standard practices information
normally includes the following:*

*a. General maintenance procedure.*

*b. Information on standard hardware.*

*c. Tightening procedure.*

*d. Torque value and torquing Procedures.*

*e. Use of torque wrench.*

*f. Safety methods.*

*g. Other subjects.*

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**CHAPTERS**

***21, 22, 23, 24, 25, 26, 27, 29, 30, 31, 32, 33, 34, 35, 36, 37,
45,***

***49; Airframe Systems ( )-00-00***

***52, 53, 54, 55, 56, Structures ( )-00-00***

***62, 63, 64, 65, 66, 67; Rotors ( )-00-00***

***71, 72, 73, 74, 75, 76, 77, 78, 79, 80, and 83. Powerplant (
)-00-00***

***REQUIREMENTS***

***The applicant must review requirements for each chapter, determine
items that are applicable, and prepare appropriate ICA.***

1.  **INTERFACE INFORMATION**

***Any required information relating to the interface of appliances,
engine or engines, rotor or rotors with the rotorcraft. [Reference
Appendix A, A29.1 (b).]{.underline}** This is required when appliances,
engine or engines, and rotor or rotors are mounted, attached, or
connected to rotorcraft. Applicant should provide information relating
to the installation. Interface information should include the system(s)
from which it receives electrical power, fluids (fuel, oil, hydraulic,
etc.), indications, and the controls that interface with rotorcraft.*

2.  **DESCRIPTION OF ROTORCRAFT AND ITS SYSTEMS AND INSTALLATIONS**

***A description of the rotorcraft and its systems and installations.***

***[Reference Appendix A, A29.3 (a)(2).]{.underline}** This is always
required as applicable.*

*a. The description of the rotorcraft should include the type of
rotorcraft (passenger, cargo), type of structure (metal, composite),
number of rotors, number of engines, and type of*

*landing gear (retractable or skids)*

*b. The description of the rotorcraft's systems should include the
component or parts of the*

*system and how systems interface with the rotorcraft or other systems.*

*c. The description of the installations should include the location of
the installation, and how the system is installed.*

3.  **DESCRIPTION OF ROTORCRAFT'S ENGINE(S)**

***A description of the rotorcraft's engine(s) and its systems and
installations. [Reference Appendix A, A29.3 (a)(2).]{.underline}** This
is always required as applicable.*

*a. The description of the engine should include the type (piston or
turbine), the manufacturer, engine model, horsepower, etc.*

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***REQUIREMENTS***

**(continued)**

*b. The description of the engine's systems should include the component
or parts of the*

*system and how systems interface with the rotorcraft or other systems.*

*c. The description of the engine installations should include the
location of the installation and how the system is installed.*

4.  ***DESCRIPTION OF ROTORCRAFT'S ROTOR(S)***

***A description of the rotorcraft's rotor(s) and its systems and
installations. [Reference Appendix A, A29.3 (a)(2).]{.underline}** This
is always required as applicable.*

*a. The description of the rotors should include the type (two blade or
more), structural (metal or composite), the rotor manufacturer, rotor
model, dimensions, etc.*

*b. The description of the rotor systems should include the component or
parts of the*

*system and how systems interface with the rotorcraft or other systems.*

*c. The description of the rotor installations should include the
location of the installation and how the system is installed.*

5.  **DESCRIPTION OF ROTORCRAFT'S APPLIANCES**

***A description of the rotorcraft's appliances and its systems and
installations. [Reference Appendix A, A29.3 (a)(2).]{.underline}** This
is always required as applicable.*

*a. The description of the appliances should include the type of
appliance, the manufacturer, model, and identification, etc.*

*b. The description of the appliance systems should include the
component or parts of the*

*system and how systems interface with the rotorcraft or other systems.*

*c. The description of the appliance installations should include the
location of the installation and how the system is installed.*

***6. BASIC CONTROL AND OPERATING INFORMATION***

***Basic control and operating information describing:***

a.  ***How the rotorcraft components and systems are controlled.***

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b.  ***How the rotorcraft components and systems are operated.***

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***REQUIREMENTS***

**(Continued)**

c.  ***Any special procedures and limitations that apply.***

***[Reference Appendix A, A29.3 (a)(3).]{.underline}** This is required
if engine(s), rotor(s), and/or appliances require controlling or
operating.*

> *d. The information should identify the appliance or component and
> should identify the control(s) and system used to control the
> appliance or component.*
>
> *e. The ICA should provide instructions on operating the appliance or
> component and any limitation or precautions. Operations information
> can be found in the Rotorcraft Flight Manual or Pilot Operating
> Handbook. However, basic control and operating information is an
> Appendix A requirement and should be contained in the ICA.*

***7. SERVICING INFORMATION***

***Servicing information that covers details regarding:***

***a. Servicing points and their locations.***

> ***b. Types of fluids to be used.***
>
> ***c. Capacities of tanks and reservoirs.***
>
> ***d. Pressures applicable to the various systems.***

***[Reference Appendix A, A29.3 (a)(4).]{.underline}** This is required
when applicant determines the rotorcraft and its engine(s), rotor(s),
and appliances will require servicing. The information is normally
included in chapters that address servicing and in Chapter 12**.***

***8. LOCATION OF ACCESS PANELS***

***Location of access panels for inspection and servicing.***

***[Reference Appendix A, A29.3 (a)(4).]{.underline}** This is required
when panels, plates, fairing, cowling, etc. should be removed to provide
access to the rotorcraft, its engine(s), rotor(s), and appliances for
inspection and servicing. This information is normally included in
chapters that address access and in Chapters 6 and 12.*

***9. LUBRICATING INFORMATION***

***Lubricating information that covers details regarding:***

> ***a. Lubrication points and their location.***

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***REQUIREMENTS***

**(Continued)**

> ***b. Types of lubricants to be used.***

***[Reference Appendix A, A29.3 (a)(4).]{.underline}** This is required
when applicant determines the rotorcraft and its engine(s), rotor(s),
and appliances will require lubrication. The information is normally
included in chapters that address lubrication and in Chapter 12**.***

***10. EQUIPMENT REQUIRED FOR SERVICING***

***Equipment required for servicing and lubricating. [Reference Appendix
A, A29.3 (a)(4).]{.underline}** This is required when applicant
determines equipment will be required for servicing and lubricating the
rotorcraft and its engine(s), rotor(s), and appliances. The information
is normally included in chapters addressing equipment for servicing or
lubrication and in Chapter 12. In addition, the equipment required for
servicing and lubricating should be listed in the List of Special Tools
contained in Chapter 1.*

***11. RECOMMENDED PERIODS***

***The recommended period at which each part of the rotorcraft and its
engine(s), auxiliary power unit, rotor(s), accessories, instruments, and
equipment should be:***

***a. Cleaned.***

> ***b. Inspected.***

***c. Adjusted.***

***d. Tested.***

***e. Lubricated.***

**[Reference Appendix A, A29.3 (b)(1).]{.underline}** *This is always
required as applicable.*

f\. There is no specific format for the recommended periods, however,
the ICA should include the time and/or interval the above items are to
be accomplished.

***12. DEGREE OF THE INSPECTION***

***The degree (scope) of the inspection for each part of the rotorcraft
and its engine(s), auxiliary power unit, rotor(s), accessories,
instruments and equipment. [Reference Appendix A, A29.3
(b)(1).]{.underline}** It is required for each part of the rotorcraft
and its engine(s), auxiliary power unit, rotor(s), accessories,
instruments, and equipment, which is required to be inspected. This
information is normally contained in the chapters of the item being
inspected and Chapter 5.*

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***REQUIREMENTS***

**(Continued)**

***13. WORK RECOMMENDED***

***The work recommended at these periods when each path of the
rotorcraft was cleaned, inspected, adjusted, tested, and lubricated.
[Reference Appendix A, A29.3 (b)(1).]{.underline}** This is required
when applicant determines that work will be recommended for that part of
the rotorcraft at that period. When maintenance tasks are associated
with cleaning, inspecting, adjusting, testing or lubrication of each
part of the rotorcraft and its engine(s), auxiliary power unit,
rotor(s), accessories, instruments and equipment, then those tasks
should be included in the ICA. This information is normally contained in
the chapters that the work is required.*

**14. APPLICABLE WEAR TOLERANCES**

***The applicable wear tolerances. [Reference Appendix A, A29.3
(b)(1).]{.underline}** This is required when applicant determines that
wear tolerances will be required for the rotorcraft, its engine(s),
rotor(s), and appliances. When a procedure requires maintenance
personnel to determine whether the item being inspected or maintained
meets a standard, the ICA should include the standard and specify how
much wear is acceptable. The tolerances are normally contained in the
chapter addressing the tolerance.*

***15. TROUBLESHOOTING***

***Troubleshooting information describing:***

> ***a. Probable malfunctions.***
>
> ***b. How to recognize those malfunctions. (Probable Cause)***
>
> ***c. The remedial (corrective) action for those malfunctions.***

***[Reference Appendix A, A29.3 (b)(2).]{.underline}** This is required
when applicant determines the rotorcraft, its engine(s), rotor(s), and
appliances require troubleshooting.*

d.  *The use of a table is recommended. A sample is shown below*

  ----------------------- ----------------------- -----------------------
  *Malfunction*           *Probable Cause*        *Corrective Action*

  *Describe the           *List all probable      *Provide a corrective
  malfunction.*           causes of the           action for all probable
                          malfunction.*           causes.*
  ----------------------- ----------------------- -----------------------

> *e. Troubleshooting information is normally contained in the chapters
> where troubleshooting is required.*

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***REQUIREMENTS***

**(Continued)**

***16. ORDER AND METHOD OF REMOVAL***

***Information describing the order and method of removal of products
and parts with any necessary precautions to be taken. [Reference
Appendix A, A29.3 (b)(3).]{.underline}** This is required when products
and parts can be removed as part of maintenance. This includes the
removal of products and parts in conjunction with a repair.*

a.  *The order is a step-by-step procedure: what is the first thing you
    do, then what is next, until the product or part is removed.*

*b. The method is the procedure or process used to remove the product or
part. If the removal of a product or part could result in injury to
personnel or damage to the rotorcraft if not done correctly, the ICA
should include precaution. See Chapter 1, Paragraph 13.*

*c. The information is normally contained in the chapters requiring
removal of the product or part.*

17. ***ORDER AND METHOD OF REPLACING***

***Information describing the order and method of replacing products and
parts with any necessary precautions to be taken. [Reference Appendix A,
A29.3 (b)(3).]{.underline}** This is required when products and parts
can be replaced.*

*a. The order is a step by step procedure, what is the first thing you
do, then what is next until the product or part is replaced
(reinstalled).*

*b. The method is the procedure or process used to replace (reinstall)
the product or part. If the replacement of a product or part could
result in injury to personnel or damage to the rotorcraft if not done
correctly, the ICA should include precaution. See Chapter 1,*

*Paragraph 13.*

*c. The use of the phrase "Install in reverse order" does not meet the
requirements of the FAR/JAR and should not be used in the ICA.*

*d. The information is normally contained in the chapters requiring
replacement of the part.*

***18. GENERAL PROCEDURAL INSTRUCTIONS -TESTING***

***General procedural instructions including procedures for system
testing during ground run. [Reference Appendix A, A29.3
(b)(4).]{.underline}** This is required when system testing during
ground run is specified. The information is normally contained in the
chapters requiring the test, or applicant may have a section for special
inspections, tests, and checks.*

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***REQUIREMENTS* (continued)**

***19. GENERAL PROCEDURAL INSTRUCTIONS -- CHECKS***

***General procedural instructions including procedures for symmetry
checks. [Reference Appendix A, A29.3 (b)(4).]{.underline}** This is
required when applicant specifies that symmetry checks are required. The
information is normally contained in the chapters addressing the
symmetry checks, or applicant may have a section for special
inspections, tests, and checks.*

**20. STORAGE LIMITATIONS**

***Storage Limitations. [Reference Appendix A, A29.3
(b)(3).]{.underline}** This is required when the rotorcraft, engine,
appliance manufacturer, or consumable materials manufacturer determines
there is a storage limitation.*

*a. There are various storage limitations. The applicant needs to
identify those storage limitations, provide procedure for storage, and a
means to ensure the storage limitations are not exceeded.*

*b. The information is normally contained in the chapter specifying the
storage.*

***21. SPECIAL INSPECTION TECHNIQUES. Details for the application of
special inspection techniques including radiographic and ultrasonic
testing where such processes are required. [Reference Appendix A, A29.3
(d).]{.underline}** This is required when applicant specifies special
inspection techniques will be required.*

*a. The ICA should include the equipment required for the special
inspection.*

> b\. *The ICA should include the procedure for conducting tests,
> including any precautions. See Chapter 1, Paragraph 13.*

*c. The information is normally contained in the chapters requiring
special inspection techniques, or the applicant may have a section for
special inspections, tests, and checks.*

**22. PROTECTIVE TREATMENT**

***Information needed to apply protective treatment to a structure after
inspection. [Reference Appendix A, A29.3 (e).]{.underline}** This is
required when applicant determines protective treatment will be required
for structure.*

*a. The ICA should include procedures for applying protective
treatment.*

*b. The ICA should specify type of materials to be used.*

> *c. The ICA should include the precautions associated with the
> protective treatment.*

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***REQUIREMENTS***

**(continued)**

*d. The information is normally contained in the chapters that require
the treatment.*

***23. STRUCTURAL FASTENERS***

***Information relative to structural fasteners such as identification
of structural fasteners, structural fasteners discard recommendations,
and torque values. [Reference Appendix A, A29.3 (f).]{.underline}** This
is required when structural fasteners are used and torque values are
required.*

> *a. The ICA should identify all structural fasteners, i.e., rivets,
> screws, bolts, or others.*
>
> *b. The ICA should specify the requirements for discarding structural
> fasteners.*

*c. When a structural fastener is required to be torqued, the ICA should
contain those specific torques and the procedure to torque the
structural fastener.*

> *d. Torque values must be specific and in United States or metric
> standards.*

*e. The information is normally contained in the chapters specifying
structural fasteners and torque values.*

***24. SPECIAL TOOLS***

***A List of Special Tools. [Reference Appendix A, A29.3
(g).]{.underline}** This is required when special tools or equipment are
specified in the chapters of the ICA.*

*a. When a procedure in the ICA requires the use of a special tool(s),
that tool should be listed in the List of Special Tools.*

*b. The List of Special Tools is normally contained in the
Introduction.*

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**ATTACHMENT 1**

**PART 29 REQUIREMENTS**

The following is a breakdown of Appendix A to FAR/JAR Part 29 and is
intended to provide guidance to assist an applicant for a Type Design
Change under a Type Certificate (TC), Supplemental Type Certificate
(STC), or Field Approval (FA) requiring Instructions for Continued
Airworthiness (ICA). This breakdown is intended to provide guidance to
assist an applicant in understanding the ICA requirements of § 29.1529.
An applicant may use the guidance to prepare the ICA. Completion of this
appendix will provide information needed for the evaluation and will
reduce the time required for evaluation of the proposed ICA. The open
parentheses ( ) in the Requirement column indicates the status of ICA
Requirements: Y = applicable; N/A = non-applicable. In the Location
column, list the page number in the applicant's ICA that contains the
information.

Project Number(s) \_\_\_\_\_\_\_\_\_\_\_ \_\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_\_

ACO/FSDO\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_ Project Engineer
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

**Applicant\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Make\_\_\_\_\_\_\_\_\_\_\_\_ Model\_\_\_\_\_\_\_\_\_\_
Date\_\_\_\_\_\_\_\_\_\_**

  ---------------------------------------------------- ------------------- ----------
  Requirement                                          Regulation          Location

  ***( ) ICA for each engine.***                       ***A29.1(b)***      

  ***( )** **ICA for each rotor.***                    ***A29.1(b)***      

  ***( ) ICA for each appliance required by this       ***A29.1(b)***      
  chapter.***                                                              

  ***( ) Any required information relating to the      ***A29.1(b)***      
  interface of the ( ) appliances, ( ) engines and ( )                     
  rotors with the rotorcraft**.*                                           

  ***( ) If ICA are not supplied by the manufacturer   ***A29.1***         
  of an* *( ) appliance, ( ) engine or ( ) rotor                           
  installed in the rotorcraft, the ICA for the                             
  rotorcraft must include ( ) the information                              
  essential to the continued airworthiness of the                          
  rotorcraft.***                                                           

  ***( ) A program showing how changes to the          ***A29.1(c)***      
  applicant's ICA will be distributed.***                                  

  ***( ) A program showing how changes to the ICA of   ***A29.1(c)***      
  the manufacture of the engine(s), rotor(s) and                           
  appliances installed in the rotorcraft will be                           
  distributed, if referenced in applicant's ICA***                         

  ***( ) ICA must be in the form of a manual or        ***A29.2(a)***      
  manuals as appropriate for the quantity of data.***                      

  ***( ) A format of the manual or manuals which must  ***A29.2(b)***      
  provide for a practical arrangement.***                                  

  ***( ) Content must be prepared in the English       ***A29.3***         
  language.***                                                             

  ***( ) Introduction information that includes ( ) an ***A29.3(a)(1)***   
  explanation of the rotorcraft's features and ( )                         
  data to the extent necessary for maintenance and                         
  preventive maintenance**.*                                               
  ---------------------------------------------------- ------------------- ----------

FIGURE 1

**REVISION:** ***(DATE)***

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**ATTACHMENT 1**

**PART 29 REQUIREMENTS**

+---------------------------------------------------+---------+-------+
| Requirement                                       | Reg     | Loc   |
|                                                   | ulation | ation |
+---------------------------------------------------+---------+-------+
| ***( ) A description of the ( ) rotorcraft and    | ***     |       |
| its systems and installations, ( ) engines and    | A29.3(a |       |
| its systems and installations, ( ) rotors and its | )(2)*** |       |
| systems and installations, and ( ) appliances and |         |       |
| its systems and installations.***                 |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Basic control and operating information    | ***     |       |
| describing ( ) how the rotorcraft components and  | A29.3(a |       |
| systems are controlled and ( ) how the rotorcraft | )(3)*** |       |
| components and systems are operated including ( ) |         |       |
| any special procedure and limitations.***         |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Servicing information that covers details  | ***     |       |
| regarding ( ) servicing points, ( ) capacities of | A29.3(a |       |
| tanks, ( ) capacities of reservoirs, ( ) types of | )(4)*** |       |
| fluids to be used, and ( ) pressures applicable   |         |       |
| to the various systems.***                        |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Location of access panels for ( )      | *       |       |
| inspection and ( ) servicing.***                  | **A29.3 |       |
|                                                   | (a      |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Servicing information that covers      | ***     |       |
| details regarding ( ) locations of lubrication    | A29.3(a |       |
| points, and ( ) the lubricant to be used.***      | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Equipment required for servicing.***   | ***     |       |
|                                                   | A29.3(a |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Tow instructions and limitations.***   | ***     |       |
|                                                   | A29.3(a |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Mooring information.***                | ***     |       |
|                                                   | A29.3(a |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Jacking information.***                | ***     |       |
|                                                   | A29.3(a |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Leveling information.***               | ***     |       |
|                                                   | A29.3(a |       |
|                                                   | )(4)*** |       |
+---------------------------------------------------+---------+-------+
| ***( ) Scheduling information for each part of    | ***     |       |
| the ( ) rotorcraft that provides the recommended  | A29.3(b |       |
| periods at which they should be***                | )(1)*** |       |
|                                                   |         |       |
| ***( ) cleaned, ( ) inspected, ( ) adjusted, ( )  |         |       |
| tested, ( ) lubricated and ( ) the work           |         |       |
| recommended at these periods.***                  |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Scheduling information for the ( )     | ***     |       |
| rotorcraft's engine(s) that provides the          | A29.3(b |       |
| recommended periods at which they should be ( )   | )(1)*** |       |
| cleaned, ( ) inspected, ( ) adjusted, ( ) tested, |         |       |
| ( ) lubricated and ( ) the work recommended at    |         |       |
| these periods. ***                                |         |       |
|                                                   |         |       |
| *NOTE: This information may be in the             |         |       |
| FAA/AUTHORITY‑accepted engine ICA.*               |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Scheduling information for the ( )         | ***     |       |
| rotorcraft's auxiliary power unit(s) (APU) that   | A29.3(b |       |
| provides the recommended periods they should be ( | )(1)*** |       |
| ) cleaned, ( ) inspected, ( ) adjusted,***        |         |       |
|                                                   |         |       |
| ***( ) tested, ( ) lubricated, and ( ) the work   |         |       |
| recommended at these periods.***                  |         |       |
+---------------------------------------------------+---------+-------+

Figure 1 (continued)

**REVISION:** ***(DATE)***

*Revision 4 Page 2*

> **(MANUAL IDENTIFICATION)**

**ATTACHMENT 1**

**PART 29 REQUIREMENTS**

+---------------------------------------------------+---------+-------+
| Requirement                                       | Reg     | Loc   |
|                                                   | ulation | ation |
+---------------------------------------------------+---------+-------+
| ***( ) Scheduling information for the ( )         | ***     |       |
| rotorcraft's rotor(s) that provides the           | A29.3(b |       |
| recommended periods at which they should be ( )   | )(1)*** |       |
| cleaned, ( ) inspected, ( ) adjusted, ( ) tested, |         |       |
| ( ) lubricated, and ( ) the work recommended at   |         |       |
| these periods.***                                 |         |       |
+---------------------------------------------------+---------+-------+
| ***(** ) **Scheduling information for the ( )     | ***     |       |
| rotorcraft's accessories that provides the        | A29.3(b |       |
| recommended periods at which they should be ( )   | )(1)*** |       |
| cleaned, ( ) inspected, ( ) adjusted, ***         |         |       |
|                                                   |         |       |
| ***( ) tested, ( ) lubricated, and ( ) the work   |         |       |
| recommended at these periods.***                  |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Scheduling information for the ( )     | ***     |       |
| rotorcraft's instruments that provides the        | A29.3(b |       |
| recommended periods at which they should be ( )   | )(1)*** |       |
| cleaned, ( ) inspected, ( ) adjusted, ***         |         |       |
|                                                   |         |       |
| ***( ) tested, ( ) lubricated, and ( ) the work   |         |       |
| recommended at these periods.***                  |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Scheduling information for the ( )         | ***     |       |
| rotorcraft's equipment that provides the          | A29.3(b |       |
| recommended periods at which they should ( )      | )(1)*** |       |
| cleaned, ( ) inspected, ( ) adjusted, ( )         |         |       |
| tested,***                                        |         |       |
|                                                   |         |       |
| ***( ) lubricated, and ( ) the work recommended   |         |       |
| at these periods.***                              |         |       |
+---------------------------------------------------+---------+-------+
| ***(** **) The degree of inspection for each part | ***     |       |
| of the ( ) rotorcraft and its ( ) engine(s), ( )  | A29.3(b |       |
| auxiliary power unit, ( ) rotor(s), ( )           | )(1)*** |       |
| accessories, ( ) Instruments, and ( )             |         |       |
| equipment.***                                     |         |       |
+---------------------------------------------------+---------+-------+
| ***(** **)** **The applicable wear tolerances***  | ***     |       |
|                                                   | A29.3(b |       |
|                                                   | )(1)*** |       |
+---------------------------------------------------+---------+-------+
| ***The applicant may refer to an ( )accessory, (  | ***     |       |
| ) instrument, or ( ) equipment manufacturer as    | A29.3(b |       |
| the source of this information if the applicant   | )(1)*** |       |
| shows ( ) that the item has an exceptionally high |         |       |
| degree of complexity requiring specialized        |         |       |
| maintenance techniques, test equipment, or        |         |       |
| expertise.***                                     |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) The recommended overhaul periods and       | ***     |       |
| necessary cross references to the Airworthiness   | A29.3(b |       |
| Limitation Section.***                            | )(1)*** |       |
+---------------------------------------------------+---------+-------+
| ***( ) An inspection program that includes ( )    | ***     |       |
| the frequency and ( ) extent of the inspection    | A29.3(b |       |
| necessary to provide for the continued            | )(1)*** |       |
| airworthiness of the rotorcraft.***               |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Troubleshooting information describing ( ) | ***     |       |
| problem malfunctions, ( ) how to recognize those  | A29.3(b |       |
| malfunctions, and ( ) the remedial action for     | )(2)*** |       |
| those malfunctions.***                            |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Information describing the order and       | ***     |       |
| method of ( ) removing and ( ) replacing          | A29.3(b |       |
| engine(s) with any necessary precautions to be    | )(3)*** |       |
| taken.***                                         |         |       |
+---------------------------------------------------+---------+-------+

Figure 1 (continued)

**REVISION:** ***(DATE)***

*Revision 4 Page 3*

**(MANUAL IDENTIFICATION)**

**ATTACHMENT 1**

**PART 29 REQUIREMENTS**

+---------------------------------------------------+---------+-------+
| Requirement                                       | Reg     | Loc   |
|                                                   | ulation | ation |
+---------------------------------------------------+---------+-------+
| ***( ) Information describing the order and       | ***     |       |
| method of ( ) removing and ( ) replacing rotor(s) | A29.3(b |       |
| with any necessary precautions to be taken.***    | )(3)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Information describing the order and   | ***     |       |
| method of ( ) removing and ( ) replacing parts    | A29.3(b |       |
| with any necessary precautions to be taken.***    | )(3)*** |       |
+---------------------------------------------------+---------+-------+
| **( *) Other general procedural instructions      | ***     |       |
| including ( ) storage limitations and procedures  | A29.3(b |       |
| for ( ) testing system during ground running, ( ) | )(4)*** |       |
| making symmetry checks, ( ) weighing and          |         |       |
| determining the center of gravity, ( ) lifting,   |         |       |
| and ( ) shoring. ***                              |         |       |
+---------------------------------------------------+---------+-------+
| ***( ) Diagrams of structural access plates and   | ***A29. |       |
| information needed to gain access for inspections | 3(c)*** |       |
| when access plates are not provided.***           |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **Details for the application of special | ***A29. |       |
| inspection techniques including radiographic and  | 3(d)*** |       |
| ultrasonic testing where such processes are       |         |       |
| specified.***                                     |         |       |
+---------------------------------------------------+---------+-------+
| **( ) *Information needed to apply projective     | ***A29. |       |
| treatment to structure after inspection.***       | 3(e)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **All data relative to structural        | ***A29. |       |
| fasteners such as ( ) identification, ( )         | 3(f)*** |       |
| discarded recommendations, and ( ) torque         |         |       |
| values.***                                        |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **A list of special tools needed.***     | ***A29. |       |
|                                                   | 3(g)*** |       |
+---------------------------------------------------+---------+-------+
| ***( )** **The Instructions for Continued         | ***A    |       |
| Airworthiness must contain a section, titled      | 29.4*** |       |
| Airworthiness Limitations that is***              |         |       |
|                                                   |         |       |
| ***( ) segregated and ( ) clearly distinguishable |         |       |
| from the rest of the document.** NOTE**:** [The   |         |       |
| Airworthiness Limitations Section in the          |         |       |
| applicant's ICA will be evaluated by the          |         |       |
| appropriate FAA/AUTHORTY.]{.underline}*           |         |       |
+---------------------------------------------------+---------+-------+
| ***( )** **The Airworthiness Limitations Section  | ***A    |       |
| must set forth each mandatory replacement time,   | 29.4*** |       |
| structural inspection procedure approved under §  |         |       |
| 29.571.***                                        |         |       |
+---------------------------------------------------+---------+-------+
| ***(** **) If the Instructions for Continued      | ***A    |       |
| Airworthiness consist of multiple documents, the  | 29.4*** |       |
| Airworthiness Limitations Section required by     |         |       |
| this paragraph must be included in the principal  |         |       |
| manual.***                                        |         |       |
+---------------------------------------------------+---------+-------+

Figure 1 (continued)

**REVISION:** ***(DATE)***

*Revision 4 Page 4*

> **(MANUAL IDENTIFICATION)**

**ATTACHMENT 1**

**PART 29 REQUIREMENTS**

  ---------------------------------------------------- ------------- ----------
  Requirement                                          Regulation    Location

  ***( ) The Airworthiness Limitations Section must    ***A29.4***   
  contain a legible statement in a prominent location                
  indicating that the Airworthiness Limitations                      
  Section is FAA/AUTHORITY‑approved and specifies                    
  required maintenance and/or inspections. The exact,                
  required wording of this statement is found in the                 
  FAR/JAR.***                                                        
  ---------------------------------------------------- ------------- ----------

Figure 1 (continued)

*NOTE: The Airworthiness Limitations Section (ALS) is evaluated and
approved by the FAA/AUTHORITY. The applicant's proposed ICA is submitted
to the FAA/AUTHORITY.*

**REVISION:** ***(DATE)***

*Revision 4 Page 5*

**(MANUAL IDENTIFICATION)**

THIS PAGE INTENTIONALLY LEFT BLANK

**REVISION:** ***(DATE)***

*Revision 4 Page 6*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 2***

***INSTRUCTIONS FOR CONTINUED AIRWORTHINESS***

***PROCEDURES INFORMATION***

*The procedures information in this appendix is not a requirement. It is
intended as*

*guidance to assist the applicant in preparing procedures for
Instructions for Continued*

*Airworthiness (ICA).*

*An ICA is required when field maintenance personnel are authorized to
remove, disassemble, assemble, clean, inspect, check, repair, replace,
install, service, lubricate, test, troubleshoot, adjust, or apply a
protective treatment to a rotorcraft, its engine(s), rotor(s), or
appliances.*

*The following topics should be considered when preparing procedures for
an ICA.*

*1. Provide general information about the appliance.*

*2. Provide a description of the appliance in the procedures.*

*3. Specify necessary precautions to be taken during the procedures and
include them in Notes, Cautions, and Warnings.*

*4. Specify tool(s), special tool(s), or equipment required for the
procedures.*

*5. Specify torque value(s) for the appliances and attaching hardware.*

*6. Provide information to gain access to the appliance.*

*7. Consumable materials should be identified by specification/part
number, product name, or manufacturer.*

*8. Identify the appliance to be removed, disassembled, cleaned,
inspected, checked, repaired, replaced, assembled, checked, serviced,
tested, adjusted, or operated.*

*9. Develop order and method procedures for removing, and/or replacing
the appliance, including a procedure to protect opening, lines, and
hoses, etc., from contamination.*

*10. Develop order and method procedures for disassembly and assembly of
the appliance, including any special process required and safety
precautions.*

*11. Develop order and method procedures for cleaning the appliance,
including any special process(es) to be used during cleaning. Identify
type of cleaning materials.*

*12. Specify what inspections or checks are required and their interval.
Develop order and method for inspecting the appliance, including special
inspection techniques, standards and limits. Describe what actions are
to be taken when appliance is found unacceptable.*

**REVISION:** ***(DATE)***

*Revision 3 Page 1*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 2***

***INSTRUCTIONS FOR CONTINUED AIRWORTHINESS***

***PROCEDURES INFORMATION***

***(Continued)***

*13. Develop order and method procedures for making the repair. Identify
the type of damage and limits that can be repaired and specify
inspection required before the repair can be made. Specify special
process(es) to be used to make the repair and acceptable repair
materials.*

*14. Develop order and method procedures for applying protective
treatment to the appliance, including any special process(es) to be used
during treatment. Specify the type of protective material to be used.*

*15. Develop order and method procedures for installation of the
appliance. Specify special procedure and process(es) to be used. Specify
measurements, clearances, and torques for the appliance being
installed.*

*16. Develop order and method procedures for servicing, lubricating, or
draining the appliance. Specify the type of servicing material, the
quantity, and limits. Specify safety equipment and safety precautions.*

*17. Develop order and method procedures for testing the part. Specify
the type of test and equipment required for the test, including location
of connection points. Specify test standards and limits for the
appliance being tested. Describe what action should be taken when the
test results are unacceptable.*

*18. Develop order and method procedures for troubleshooting the
appliance. Provide troubleshooting information, problem malfunction, and
remedial actions.*

*19. Develop order and method procedures for adjusting the appliance.
Specify location for adjusting, and the standards and limits of
adjustments. Specify special tool(s) or equipment required to make
adjustments. Describe actions to be taken when adjustment is past
limits. Provide safety precautions and safety equipment required for
adjustment.*

*20. Develop order and method for safetying or securing the appliances
and specify the types of safetying devices.*

**REVISION:** ***(DATE)***

*Revision 3 Page 2*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 3***

***ATA CHAPTER LISTINGS***

*Listed below are the ATA chapters and their titles.*

*AIRCRAFT GENERAL STRUCTURAL*

*Chapter 4 Airworthiness Limitations Chapter 51 Standard Practices -
Structure*

*Chapter 5 Inspection Requirements Chapter 52 Doors*

*Overhaul Requirements Chapter 53 Fuselage*

*Chapter 6 Principal Dimension Chapter 54 Nacelles and Pylons*

*Chapter 7 Lifting and Shoring Chapter 55 Stabilizers*

*Chapter 8 Leveling and Weighing Chapter 56 Windows*

*Chapter 9 Towing and Taxing*

*Chapter 10 Parking and Mooring*

*Chapter 11 Placards and Markings ROTORS*

*Chapter 12 Servicing*

*Chapter 60 Standard Practices -Rotors*

*Chapter 62 Main Rotor*

*AIRFRAME SYSTEMS Chapter 63 Main Rotor Drive*

> *Chapter 64 Anti Torque*

*Chapter 20 Standard Practices - Airframe Chapter 65 Anti Torque Drive*

*Chapter 21 Air Conditioning Chapter 66 Folding Blades*

*Chapter 22 Autoflight Chapter 67 Rotor Flight Controls*

*Chapter 23 Communications*

*Chapter 24 Electrical power POWERPLANT*

*Chapter 25 Equipment and Furnishings*

*Chapter 26 Fire Detection Chapter 70 Standard Practice Engines*

*Chapter 28 Fuel Chapter 71 Powerplant*

*Chapter 29 Hydraulic Power Chapter 72 Engine*

*Chapter 30 Ice and Rain Protection Chapter 73 Engine Fuel and Control*

*Chapter 31 Indicating and Recording Chapter 74 Ignition*

*Chapter 32 Landing Gear Chapter 75 Engine Air*

*Chapter 33 Lights Chapter 76 Engine Controls*

*Chapter 34 Navigation Chapter 77 Indicating*

*Chapter 35 Oxygen Chapter 78 Exhaust*

*Chapter 36 Pneumatics Chapter 79 Oil*

*Chapter 37 Vacuum Chapter 80 Starting*

*Chapter 45 Centralized Maintenance Sys Chapter 83 Gear Boxes*

*Chapter 49 Airborne Auxiliary Power*

**REVISION:** ***(DATE)***

*Revision 3 Page 1*

> **(MANUAL IDENTIFICATION)**

THIS PAGE INTENTIONALLY LEFT BLANK

**REVISION:** ***(DATE)***

*Revision 3 Page 2*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 4***

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

*The following information is intended for guidance to* *assist the
applicant in preparing an ICA.*

*For this sample, we will use a twidget, which is a sounder attached to
an extendible cable assembly* *connected to a pivoting arm, which is
mounted to the side of the fuselage structure at the right cabin* *door
forward frame.*

> *NOTE: The twidget manufacturer\'s ICA does not meet the requirements
> of Appendix* *A and cannot be referenced.*

*The following step-by-step procedure in this sample can be used to
prepare an ICA for that appliance:*

*1. Determine the following:*

> *a. What modifications to the rotorcraft will be required.*
>
> *b. Determine what appliances will be replaced or added to the
> rotorcraft.*

*c. Determine which ATA chapters of the original rotorcraft
manufacturer\'s maintenance manual will be affected by this TDC and
which additional ATA chapters will be affected.*

*2. Review Appendix A, Part 29. Using the information derived in
paragraph 1, determine* *which paragraphs are applicable and which are
not applicable. As defined in Figure 2, provide the status of each
requirement on the applicable paragraph. If the requirement is not
applicable, place an* *N/A within the parentheses ( ). Address the
remaining requirements in the ICA.* *A completed document for the
twidget installation (Figure 2) is* *included.*

*3. Prepare the ICA, which includes the applicable requirements
specified in Appendix A to Part 29.* *This can be done by using the
information provided in the Instructions for Continued Airworthiness*
*template. The regulatory requirements in the sample manual are in bold
type. Information to* *be copied is in normal type. Information in
italics is for information only and should not be copied.* *See
Instructions for Continued Airworthiness* *template.*

*4. Ensure the ICA includes the following:*

*a. A Cover Page, readily identifying the publication as the
applicant\'s ICA for that make* *and model rotorcraft.*

*b. A List of Effective Pages, listing each page in the ICA and its
revision number and revision* *date.*

*c. A Record of Revisions Page listing the revisions which have been
inserted in the ICA.*

**REVISION:** ***(DATE)***

*Revision 3 Page 1*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 4***

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

*5. Table of Contents is not required, but we recommend it be included
in the ICA.*

*6. Audit the proposed ICA to ensure the applicable requirements have
been included. Edit the ICA* *document ensuring it does not contain
incorrect terminology or incorrect references, and determine it* *does
contain correct spelling, proper grammar, and accurate information.*

*7. When referencing another publication, ensure the information in the
referenced publication meets* *the requirements of Appendix A, Part 29.
It is the responsibility of the applicant to* *obtain authorization to
use the information contained in the referenced publication. Submit a
copy of* *each publication referenced in the applicant\'s ICA.*

*8. Submit two complete copies of the proposed ICA in binders, a copy of
the completed Figure 1 document, and a copy of any referenced
publication to the FAA/AUTHORITY, in sufficient time to allow for
evaluation prior to the date acceptance is* *needed. The average
turnaround time is 20 to 30 days depending on the workload.*

*9. When FAA/AUTHORITY receives the applicant\'s proposed ICA, the
applicant* *and the appropriate FAA/AUTHORITY are notified.
FAA/AUTHORITY* *reviews and evaluates the ICA in the order they are
received.*

*10. If FAA/AUTHORITY finds the applicant\'s ICA does not meet the
requirements, the review will be* *discontinued, and the applicant will
be notified.*

*11. When the proposed ICA document, excluding the Airworthiness
Limitations Section, is determined to be* *acceptable, the FAA/AUTHORITY
will stamp, sign, and date the ICA. The applicant will be notified of
the acceptance.*

**REVISION:** ***(DATE)***

*Revision 4 Page 2*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 4***

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

*Twidget Type Design Change Attachment 2*

*1. Use the list of appliances and modifications required for that Type
Design Change (TDC) to determine which ATA* *chapters of the original
rotorcraft manufacturer\'s maintenance manual the TDC will affect and
which* *additional ATA chapters will be affected.*

*2.* *The following are components and systems that will be affected by
the twidget TDC:*

*a. Fuselage structure will be modified to mount twidget arm assembly.*

*b. Cabin door will be modified.*

*c. Electrical power will be required for electrical motor.*

*d. Hydraulic power source will be required for deploying and storing
twidget arm.*

*e. Twidget control assembly will be installed in the cabin.*

*f. Control will be mounted in cockpit for emergency release of the
twidget.*

*g. An instrument will be installed in instrument panel indicating
twidget\'s position.*

*h. Twidget recording equipment and monitor will be mounted in cabin.*

*i. Twidget antenna will be mounted on belly of fuselage.*

*j. Cables and wiring will be routed through rotorcraft.*

*k. Two-way communication will be required between the pilot and twidget
operator.*

*L. Twidget gearbox requires servicing to full mark on site gauge every
50 hours.*

*m. Twidget arm assemblies and clutch requires lubrication every 100
hours.*

*n. Twidget installation requires an inspection every 300 hours*.

*n. Twidget arm assembly requires an ultrasonic test every 600 hours.*

*o. Clutch has a wear tolerance of 1.56 mm.*

*p. Clutch is life-limited to be replaced every l,000 hours time in
service.*

*r. Twidget gearbox is required to be overhauled every l,000 hours time
in service.*

s.  *Twidget gearbox attach bolt torque is 75-ft. lb. and twidget arm
    assembly torque is 110*

> *in. lb.*

t.  *Warning: Twidget should be retracted during takeoff, landing, and
    cruise above 85 knots.*

*u. Caution: Do not tow or taxi the rotorcraft with the twidget arm
deployed.*

*v. Placards are required on the twidget unit and in the cockpit.*

3\. This *example TDC will affect ATA-100 chapters: 4 Airworthiness
Limitations, 5 Inspection,*

*6 Dimensions, 9 Towing and Taxiing, 10 Parking and Mooring, 11
Placards, 12 Servicing,* *23 Communication, 24 Electrical, 25
Furnishings, 29 Hydraulic, 31 Indication and Recording,* *52 Doors, and
53 Fuselage. A Chapter 1 Introduction is also needed.*

**REVISION:** ***(DATE)***

*Revision 4 Page 3*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT 4***

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

*INFORMATION:*

*Attachment 4 includes Figure 2 for Thomas Copter Mods TDC to affix a
twidget installation on Thomas Copter model T-97J helicopter.*

*Figure 2 is intended to assist in determining which requirements are
applicable to this* *certification project. The document contains each
requirement with a set of parentheses,* *the* *appropriate regulation,
and the location of information in the applicant's ICA.*

*Information obtained from Attachment 4 can be used to determine which
requirements are* *applicable. For requirements that are not applicable,
place an N/A in* *the parentheses. All other requirements would be
applicable to the certification project. Place a Y if the required
information is included in ICA. Figure 2 has been completed for the
sample twidget TDC.*

*Applicant using and completing Figure 1 indicating the* *location of
that information in the applicant's proposed ICA, will reduce the time
required to evaluate the ICA.*

*It is important the applicant include the project number or numbers
associated with the ICA, the name of* *the appropriate FAA/AUTHORITY
office, name of the project engineer, applicant\'s company name, make
and model of rotorcraft being* *modified, and date.*

*The completed Figure 1 should be submitted to FAA/AUTHORITY with the*
*applicant\'s ICA.*

**REVISION:** ***(DATE)***

*Revision 4 Page 4*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT* 4**

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

#### APPENDIX A PART 29 REQUIREMENTS

The following is a breakdown of Appendix A to FAR/JAR Part 29 and is
intended to provide guidance to assist an applicant for a Type Design
Change under a Type Certificate (TC), Supplemental Type Certificate
(STC), or Field Approval (FA) requiring Instructions for Continued
Airworthiness (ICA). The breakdown is intended to provide guidance to
assist an applicant in understanding the ICA requirements of FAR/JAR §
29.1529. An applicant may use the guidance in preparing the ICA.
Completion of this appendix will provide information needed for the
evaluation and will reduce the time required for evaluation of the
proposed ICA.

( ) Status of ICA: Y = Yes included; N/A = non-applicable. The Location
column lists the page number in the applicant's ICA containing the
information.

Project Number(s) ST01998RC-R

ACO/FSDO: Rotorcraft ACO Project Engineer: Data Mastermine

**Applicant: Thomas Copter Mods Make: Thomas Copter Model: T97-J Date
June 18, 1998**

  ---------------------------------------------------- ---------------- ----------
  Requirement                                          Regulation       Location

  ***(**N/A**) ICA for each engine***                  ***A29.1(b)***   N/A

  ***(**N/A**)** **ICA for each rotor***               ***A29.1(b)***   N/A

  ***(** Y **) ICA for each appliance required by this ***A29.1(b)***   \* All
  chapter.***                                                           

  ***(** Y **) Any required information relating to    ***A29.1(b)***   See NOTE 1
  the interface of the (** Y **) appliances, (**N/A**)                  
  engines and (**N/A**) rotors with the rotorcraft**.*                  

  ***(** Y **) If ICA are not supplied by the          ***A29.1***      \* All
  manufacturer of an*** ***(**N/A**) appliance,                         
  (**N/A**) engine or (**N/A**) rotor installed in the                  
  rotorcraft, the ICA for the rotorcraft must include                   
  (** Y **) the information essential to the continued                  
  airworthiness of the rotorcraft.***                                   

  ***(** Y **) A program showing how changes to the    ***A29.1(c)***   ATA 0
  applicant's ICA will be distributed.***                               

  ***(**N/A**) A program showing how changes to the    ***A29.1(c)***   N/A
  ICA of the manufacture of the engine(s), rotor(s)                     
  and appliances installed in the rotorcraft will be                    
  distributed, if referenced in applicant's ICA***                      

  ***(** Y **) ICA must be in the form of a manual or  ***A29.2(a)***   \* All
  manuals as appropriate for the quantity of data.***                   

  ***(** Y **) A format of the manual or manuals must  ***A29.2(b)***   \* All
  provide for a practical arrangement.***                               

  ***(** Y **) Content must be prepared in the English ***A29.3***      \* All
  language.***                                                          
  ---------------------------------------------------- ---------------- ----------

##### Figure 2

**REVISION:** ***(DATE)***

*Revision 4 Page 5*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT* 4**

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

  ---------------------------------------------------- ------------------- ----------
  Requirement                                          Regulation          Location

  ***(** Y **) Introduction information that includes  ***A29.3(a)(1)***   ATA 0
  (** Y **) an explanation of the rotorcraft's                             
  features and (** Y **) data to the extent necessary                      
  for maintenance and preventive maintenance**.*                           

  ***(** Y **) A description of the (**N/A**)          ***A29.3(a)(2)***   ATA 25
  rotorcraft and its systems and installations,                            
  (**N/A**) engines and its systems and installations,                     
  (**N/A**) rotors and its systems and installations,                      
  (** Y **) appliances and its systems and                                 
  installations.***                                                        

  ***(** Y **) Basic control and operating information ***A29.3(a)(3)***   ATA 25
  describing (** Y **) how the rotorcraft components                       
  and systems are controlled and (** Y **) how the                         
  rotorcraft components and systems are operated                           
  including (** Y **) any special procedure and                            
  limitations.***                                                          

  ***(** Y **) Servicing information that covers       ***A29.3(a)(4)***   ATA 12
  details regarding (** Y **) servicing points,                            
  (**N/A**) capacities of tanks, (** Y **) capacities                      
  of reservoirs, (** Y **) types of fluids to be used,                     
  (** Y **) pressures applicable to the various                            
  systems.***                                                              

  ***(** Y **)** **Location of access panels for (** Y ***A29.3 (a)(4)***  See NOTE 2
  **) inspection and (** Y **) servicing.***                               

  ***(** Y **)** **Servicing information that covers   ***A29.3(a)(4)***   ATA 12
  details regarding (** Y **) locations of lubrication                     
  points, (** Y **) the lubricant to be used.***                           

  ***(** Y **)** **Equipment required for              ***A29.3(a)(4)***   ATA 12
  servicing.***                                                            

  ***(** Y **)** **Tow instructions and                ***A29.3(a)(4)***   ATA 9
  limitations.***                                                          

  ***(** Y **)** **Mooring information.***             ***A29.3(a)(4)***   ATA 10

  ***(**N/A**)** **Jacking information.***             ***A29.3(a)(4)***   N/A

  ***(**N/A**)** **Leveling information.***            ***A29.3(a)(4)***   N/A

  ***(** Y **) Scheduling information for each part of ***A29.3(b)(1)***   See NOTE 3
  the (** Y **) rotorcraft that, provides the                              
  recommended periods at which they should be (** Y                        
  **) cleaned, (** Y **) inspected, (** Y **)                              
  adjusted, (** Y **) tested, (** Y **) lubricated,                        
  and (** Y **) the work recommended at these                              
  periods.***                                                              

  ***(**N/A**)** **Scheduling information for the      ***A29.3(b)(1)***   N/A
  (**N/A**) rotorcraft's engine(s) that provides the                       
  recommended periods at which they should be                              
  (**N/A**) cleaned, (**N/A**) inspected, (**N/A**)                        
  adjusted, (**N/A**) tested, (**N/A**) lubricated and                     
  (**N/A**) the work recommended at these periods.**                       
  NOTE: This information may be in the FAA/AUTHORITY                       
  accepted engine ICA.*                                                    
  ---------------------------------------------------- ------------------- ----------

**Figure 2 (continued)**

**REVISION:** ***(DATE)***

*Revision 4 Page 6*

> **(MANUAL IDENTIFICATION)**

#### *ATTACHMENT* 4

####### TYPE DESIGN CHANGE

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

+---------------------------------------------------+---------+-------+
| Requirement                                       | Reg     | Loc   |
|                                                   | ulation | ation |
+---------------------------------------------------+---------+-------+
| ***(**N/A**) Scheduling information for the       | ***     | N/A   |
| (**N/A**) rotorcraft's auxiliary power            | A29.3(b |       |
| unit(s)(APU) that provides the recommended        | )(1)*** |       |
| periods at which they should be (**N/A**)         |         |       |
| cleaned, (**N/A**) inspected,***                  |         |       |
|                                                   |         |       |
| ***(**N/A**) adjusted, (**N/A**) tested,          |         |       |
| (**N/A**) lubricated and (**N/A**) the work       |         |       |
| recommended at these periods.***                  |         |       |
+---------------------------------------------------+---------+-------+
| ***(**N/A**) Scheduling information for the       | ***     | N/A   |
| (**N/A**) rotorcraft's rotor(s) that provides the | A29.3(b |       |
| recommended periods at which they should be       | )(1)*** |       |
| (**N/A**) cleaned, (**N/A**) inspected, (**N/A**) |         |       |
| adjusted, (**N/A**) tested, (**N/A**) lubricated, |         |       |
| and (**N/A**) the work recommended at these       |         |       |
| periods.***                                       |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y ) **Scheduling information for the (** Y | ***     | See   |
| **) rotorcraft's accessories that provides the    | A29.3(b | NOTE  |
| recommended periods at which they should be (** Y | )(1)*** | 3     |
| **) cleaned, (** Y **) inspected, (** Y **)       |         |       |
| adjusted, (** Y **) tested, (** Y **) lubricated, |         |       |
| and (** Y **) the work recommended at these       |         |       |
| periods.***                                       |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **Scheduling information for the   | ***     | See   |
| (** Y **) rotorcraft's instruments that provides  | A29.3(b | NOTE  |
| the recommended periods at which they should be   | )(1)*** | 3     |
| (** Y **) cleaned, (** Y **) inspected, (** Y **) |         |       |
| adjusted, (** Y **) tested, (** Y **) lubricated, |         |       |
| and (** Y **) the work recommended at these       |         |       |
| periods.***                                       |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **) Scheduling information for the (** Y | ***     | See   |
| **) rotorcraft's equipment that provides the      | A29.3(b | NOTE  |
| recommended periods at which they should be (** Y | )(1)*** | 3     |
| **) cleaned, (** Y **) inspected, (** Y **)       |         |       |
| adjusted, (** Y **) tested, (** Y **) lubricated, |         |       |
| and (** Y **) the work recommended at these       |         |       |
| periods.***                                       |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **) The degree of inspection for each    | ***     | ATA 5 |
| part of the (**N/A**) rotorcraft and its          | A29.3(b |       |
| (**N/A**) engine(s), (**N/A**) auxiliary power    | )(1)*** |       |
| unit, (**N/A**) rotor(s), (** Y **) accessories,  |         |       |
| (** Y **) instruments, and ***                    |         |       |
|                                                   |         |       |
| ***(** Y **) equipment.***                        |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **The applicable wear              | ***     | ATA   |
| tolerances.***                                    | A29.3(b | 25    |
|                                                   | )(1)*** |       |
+---------------------------------------------------+---------+-------+
| ***The applicant may refer to an (**N/A**)        | ***     | N/A   |
| accessory, (**N/A**) instrument, or (**N/A**)     | A29.3(b |       |
| equipment manufacturer as the source of this      | )(1)*** |       |
| information, if the applicant shows (**N/A**)     |         |       |
| that the item has an exceptionally high degree of |         |       |
| complexity requiring specialized maintenance      |         |       |
| techniques, test equipment, or expertise. ***     |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **) The recommended overhaul periods and | ***     | ATA 5 |
| necessary cross references to the Airworthiness   | A29.3(b |       |
| Limitation Section.***                            | )(1)*** |       |
+---------------------------------------------------+---------+-------+

**Figure 2 (continued)**

**REVISION:** ***(DATE)***

*Revision 4 Page 7*

**(MANUAL IDENTIFICATION)**

***ATTACHMENT* 4**

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

+---------------------------------------------------+---------+-------+
| Requirement                                       | Reg     | Loc   |
|                                                   | ulation | ation |
+---------------------------------------------------+---------+-------+
| ***(** Y **) An inspection program that includes  | ***     | ATA 5 |
| (** Y **) the frequency and (** Y **) extent of   | A29.3(b |       |
| the inspection necessary to provide for the       | )(1)*** |       |
| continued airworthiness of the rotorcraft.***     |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **) Troubleshooting information          | ***     | See   |
| describing (** Y **) problem malfunctions, (** Y  | A29.3(b | NOTE  |
| **) how to recognize those malfunctions, and (**  | )(2)*** | 4     |
| Y **) the remedial action for those               |         |       |
| malfunctions.***                                  |         |       |
+---------------------------------------------------+---------+-------+
| ***(**N/A**) Information describing the order and | ***     | N/A   |
| method of (**N/A**) removing and (**N/A**)        | A29.3(b |       |
| replacing engine(s) with any necessary            | )(3)*** |       |
| precautions to be taken.***                       |         |       |
+---------------------------------------------------+---------+-------+
| ***(**N/A**) Information describing the order and | ***     | N/A   |
| method of (**N/A**) removing and (**N/A**)        | A29.3(b |       |
| replacing rotor(s) with any necessary precautions | )(3)*** |       |
| to be taken.***                                   |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **Information describing the order | ***     | ATA   |
| and method of (** Y **) removing and (** Y **)    | A29.3(b | 25    |
| replacing parts with any necessary precautions to | )(3)*** |       |
| be taken.***                                      |         |       |
+---------------------------------------------------+---------+-------+
| **(** *Y **) Other general procedural             | ***     | ATA 8 |
| instructions including ***                        | A29.3(b |       |
|                                                   | )(4)*** |       |
| ***(**N/A**) storage limitations and procedures   |         |       |
| for (**N/A**) testing system during ground        |         |       |
| running, (**N/A**) making symmetry checks, (** Y  |         |       |
| **) weighing and determining the center of        |         |       |
| gravity, ***                                      |         |       |
|                                                   |         |       |
| ***(**N/A**) lifting, (**N/A**) shoring. ***      |         |       |
+---------------------------------------------------+---------+-------+
| ***(**N/A**) Diagrams of structural access plates | ***A29. | N/A   |
| and information needed to gain access for         | 3(c)*** |       |
| inspections when access plates are not            |         |       |
| provided.***                                      |         |       |
+---------------------------------------------------+---------+-------+
| ***(**N/A**)** **Details for the application of   | ***A29. | N/A   |
| special inspection techniques including           | 3(d)*** |       |
| radiographic and ultrasonic testing where such    |         |       |
| process are specified.***                         |         |       |
+---------------------------------------------------+---------+-------+
| **(**N/A**) *Information needed to apply          | ***A29. | N/A   |
| protective treatment to structure after           | 3(e)*** |       |
| inspection.***                                    |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **All data relative to structural  | ***A29. | ATA25 |
| fasteners such as (** Y **) identification, (** Y | 3(f)*** |       |
| **) discarded recommendations, and (** Y **)      |         |       |
| torque values.***                                 |         |       |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **A list of special tools          | ***A29. | See   |
| needed***                                         | 3(g)*** | NOTE  |
|                                                   |         | 5     |
+---------------------------------------------------+---------+-------+
| ***(** Y **)** **The Instructions for Continued   | ***A    | ATA 4 |
| Airworthiness must contain a section, titled      | 29.4*** |       |
| Airworthiness Limitations that is (** Y **)       |         |       |
| segregated and (** Y **) clearly distinguishable  |         |       |
| from the rest of the document.** [NOTE: The       |         |       |
| Airworthiness Limitations Section in the          |         |       |
| applicant's ICA will be evaluated by the          |         |       |
| appropriate FAA/AUTHORITY.]{.underline}*          |         |       |
+---------------------------------------------------+---------+-------+

**Figure 2 (continued)**

**REVISION:** ***(DATE)***

*Revision 4 Page 8*

> **(MANUAL IDENTIFICATION)**

***ATTACHMENT* 4**

***TYPE DESIGN CHANGE***

***ICA RECOMMENDED PROCEDURES***

***(Continued)***

  ---------------------------------------------------- ------------- ----------
  Requirement                                          Regulation    Location

  ***(**N/A**)** **The Airworthiness Limitations       ***A29.4***   N/A
  Section must set forth each mandatory replacement                  
  time, structural inspection procedure approved under               
  § 29.571.***                                                       

  ***(** Y **) If the Instructions for Continued       ***A29.4***   ATA 4
  Airworthiness consist of multiple documents, the                   
  section required by this paragraph must be included                
  in the principal manual.***                                        

  ***(** Y **) The Airworthiness Limitations Section   ***A29.4***   ATA 4
  must contain a legible statement in a prominent                    
  location indicating that the Airworthiness                         
  Limitations Section is FAA/AUTHORITY‑approved and                  
  specifies required maintenance and/or inspections.                 
  The exact, required wording of this statement is                   
  found in the FAR/JAR.***                                           
  ---------------------------------------------------- ------------- ----------

**Figure 2 (continued)**

*NOTE: The Airworthiness Limitations Section (ALS) is evaluated and
approved by FAA/AUTHORITY. The applicant\'s proposed ICA is submitted to
the FAA/AUTHORITY.*

**REVISION:** ***(DATE)***

*Revision 4 Page 9*

> **(MANUAL IDENTIFICATION)**

THIS PAGE INTENTIONALLY LEFT BLANK

**REVISION:** ***(DATE)***

###### Revision 4 Page 10