CAA of NZ - Example - Aircraft Type PTR

CAA of NZ - Example - Aircraft Type PTR

ContentsPage

1Personal Details...... 3

2Purpose of PTR...... 3

3Prerequisites for a Part 66 Maintenance Approval...... 3

4Prerequisites for Part 66 AMEL Type Ratings...... 3

5Instructions for use...... 4

6Record of Courses / Examinations...... 5

7QA PTR Review...... 5

8Register of Certifying Engineers...... 6

ATAEXPERIENCE LOG – by ATA Chapter

05Maintenance Checks...... 7

12Servicing...... 8

21Air-conditioning...... 9

22Auto Pilot...... 10

23Communication...... 11

24Electrical Power...... 12

25Equipment & Furnishings...... 13

26Fire Protection...... 14

27Flight Controls...... 15

28Fuel...... 16

29Hydraulic Power...... 17

30Ice & Rain Protection...... 18

32Landing Gear...... 19

34Navigation...... 20

35Oxygen...... 21

36Pneumatics...... 21

52Doors...... 22

53Fuselarge...... 22

55Stabilisers...... 23

56Windows...... 23

61Propellers...... 24

71/72Powerplant / Engine...... 25

73Engine Fuel & Controls...... 26

74Ignition...... 26

75Engine Air...... 27

76Engine Controls...... 27

77Engine Indicating...... 28

79Oil...... 28

80Starting...... 29

49APU...... 29

ADDITONAL EXPERIENCE...... 30

ATA CHAPTER – List of Typical TasksApp. 1

ATA CHAPTER LISTINGApp. 2

1. Personal Details

Name:Lic. / App. No:

2. Purpose of PTR (Practical Training Record)

To demonstrate/record that the engineer meets the experiencerequirements for the issue of a NZCAA Part 66 Maintenance Approval and subsequent Limited company name Approval while gaining experience for the issue of appropriate ratings and Full company name Approval
To demonstrate/record that the engineer meets the experience requirements for the issue of NZCAA Part 66 AMEL Type Ratings for the aircraft typein the appropriate categories and subsequent Full company name Approvals

3. Prerequisites for a Limited Company Authorisation /

Part 66 Maintenance Approval

Group 6 aircraft rated engineer
Meets the requirements for the issue of a Part 66 Maintenance Approval.
Completed appropriate aircraft typeAircraft /Powerplant / Avionics Courses
Completed Technical Oral examination
Completed sufficient experience – PTR to be reviewed and signed off by QA prior to application for Maintenance Approval

It will be limited to xx months from entry into operation of aircraft typeaircraft. This will allow enough time for applicants to gain sufficient experience to apply for a full aircraft type ratings and company name authorisation.

4. Prerequisites for Full Company Authorisation /

Part 66 AMEL Type Ratings

Additional to the above requirements,documented experience needs to be a broad cross section ofmaintenance tasks at both Line and Base (Hanger) Maintenance Levels.

Experience should be across all relevant systems (appropriate ATA Chapters) for the category(s) applying for and typically should include:

Completing all aspects of a number of line and base level routine inspections
This should include a minimum of three different C level type checks
A broad cross section of the following representative tasks on the various aircraft systems;
fault isolation / trouble shooting,
repair,
rigging and adjustments,
component changes,
functional/operational checks.
use of special tooling and test equipment.

The range and depth of experience should be evident from a review of the PTR.

This PTR should be reviewed and signed off by QA prior to application for Ratings

Note:Refer to the CAA web site for Type Rating requirements

5. Instructions for use

5.1 Completing Experience Section

There should be sufficient detail to describe the task to allow an assessment to verify that a range of various maintenance tasks have been completed for the category of rating being applied for.

In the ‘Maintenance task’ column indicate one of the following actions has been carried out:

(P) - Personally performed the task

(A) - Taken an active interest in

(T) - Received instruction or on the job training

Each maintenance task must be validated by an appropriately licensed or approved Engineer or Instructor

5. 2 Definitions:

Functional or Operational Check- means: to power up the system, carry out normal operation and functional check as per the Maintenance Manual (ICAs )and shut the system down. Test Equipment is not used.

Fault Isolation- means familiarity and understanding of the ICAs procedures and requirements in troubleshooting and rectification.

5.3 Items to be Completed (Minimum requirements):

Maintenance Approval

For the task to be certified - items marked with asterisk (*) must be:

(P) - Personally performed

(A) - Taken an active interest in

Items not marked may be completed by:

(T) - Received instruction or on the job training

Ratings

For the task to be certified - items marked in the applicable ATA Chapter, as below,must be:

(P) - Personally performed

(A) - Taken an active interest in

A- Aeroplane
LRU- Line Replaceable Units
P - Powerplant
Av - Avionics

Items not marked may be completed by:

(T) - Received instruction or on the job training
6. Record of Courses and Examinations

Note: All practical training completed during courses should be entered into PTR and signed off by the appropriate instructor.

Insert similar table if required

Date / Course / qualification details / Training provider / Result

7. QA PTR Review

Maintenance Approval

This PTR has been reviewed for the issue of aLimited company name Approval and Part 66 Maintenance Approvaland meets the experience requirements.

QA Manager Date

……………………….………….

Ratings

This PTR has been reviewed for the issue of a fullcompany name Approval and Part 66 AMEL Type Rating listed below and meets the experience requirements

CATEGORY / RATINGQA Manager Date

Aeroplane/ Aircraft Type……………………….…………..

Powerplant / Engine Type……………………….…………..

Electrical/ Aircraft Type Elec.……………………….…………..

Instrument / Aircraft TypeInst.……………………….…………..

Radio/ Aircraft Type Rad.……………………….…………..

8. Register of Certifying Engineers

Each task must be certified by anappropriately licensed or approved Engineer or Instructor

The validating engineer shall complete the register below, one time only, to verify status of certification authority. When certifying validations in the experience section use initials and line number from this

Certification in the verification column of the experience section indicates that the validating engineer has directly supervised the holder carrying out one of the following:

(P)- personally performed the task, or
(A) - taken an active interest in, or
(T) - received instruction or on the job training.

This should be described in the ‘Maintenance task’ column of experience section

Name / Company / Licence /Approval Number / Signature / Initials
1
2
3
4
5
6
7
8
9
10
TASK / A/C Reg / Certified by / Date
CHAPTER 05 - MAINTENANCE CHECKS
Line Checks
*A Checks - detail which check numbers and area(s) of checks completed below
C Checks- detail which check numbers and area(s) of checks completed below
Lightning Strike Check
Turbulence Check
Heavy Landing Check
Weigh Aircraft
TASK / A/C Reg / Certified by / Date
CHAPTER 12 - SERVICING
Aircraft Documentation
Aircraft Log and Deferred Procedures
MEL (knowledge required of associated procedures)
Standard Practices
* Jack Aircraft (x2)
* Towing aircraft
Aircraft Servicing Requirements
Detailed review of safety requirements
Oil (Engine)
Oil (Hydraulic)
Water / waste
Tyres
Refuelling and Defuelling
Aircraft Access - All
APU
TASK / A/C Reg / Certified by / Date
CHAPTER 21 - AIRCONDITIONING
* Operational and Functional Check
Service A.C.M. Oil
TASK / A/C Reg / Certified by / Date
CHAPTER 22 - AUTO PILOT
Full functional check
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 23 - COMMUNICATION
Operational and Functional Check
VHF
Interphone Systems, Pax Address and Entertainment
Cockpit Voice Recorder
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 24 - ELECTRICAL POWER
Operational and Functional Checks
AC & DC Systems
Fault Isolation
*Battery Change
*Inspect SG brushes for wear
*Change Starter Generator
*Change G.C.U.
*Change A/C generator
TASK / A/C Reg / Certified by / Date
CHAPTER 25- EQUIP. & FURNISHINGS
Location of Loose Equipment
TASK / A/C Reg / Certified by / Date
CHAPTER 26 - FIRE PROTECTION
Operational and Functional Check
* Engine Fire Detection & Extinguishing
Smoke Detection System
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 27 - FLIGHT CONTROLS
Operational and Functional Check
Fault Isolation
* Rigging Procedures - Aileron, Elevator or Rudder may be done.
* Flap Rigging Procedures
* Balancing - Aileron, Elevator or Rudder may be done.
* Rudder maintenance associated with powered system, e.g. functional check.
Spoiler system
Disconnect systems
TASK / A/C Reg / Certified by / Date
CHAPTER 28 - FUEL
Operational and Functional Checks
* Refuel, Defuel and transfer Procedures
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 29 - HYDRAULIC POWER
* Operational and Functional Checks
* Hydraulic System Servicing – safety procedures working with skydrol
TASK / A/C Reg / Certified by / Date
CHAPTER 30 - ICE & RAIN PROTECTION
* Operational and Functional Checks
Wing & Stab Boot De-ice System
Engine Anti-ice System
Windshield Anti-ice System
Probe Anti-ice System
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 32 - LANDING GEAR
* Operational and Functional Check Servicing
* Wheel change
* Brake change
TASK / A/C Reg / Certified by / Date
CHAPTER 34 - NAVIGATION
Operational and Functional Checks
Air Data System
* Pitot Static System
Altimeter
Airspeed and Overspeed
Vertical Speed Indicator
Attitude and Direction
Navigation Display
EHSI Indicator
Electronic Attitude
Standby Altimeter
Flight Director Systems
V.O.R. System (LOC/GS/MB)
A.T.C. System
D.M.E. System
Weather Radar System
A.D.F. System
Low range Radio Altimeter System
Ground Proximity Warning System
Compass STBY
ACAS / TAWS
Compensation of Direct and Remote Compass
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 35 - OXYGEN
Operational and Functional Checks
Crew Oxygen
CHAPTER 36 - PNEUMATIC
Operational and Functional Check
Fault Isolation
TASK / A/C Reg / Certified by / Date
CHAPTER 52 - DOORS
* Operational and Functional Check
Passenger and Cargo Doors
CHAPTER 53 - FUSELARGE
Damage Limits
TASK / A/C Reg / Certified by / Date
CHAPTER 55 - STABILISERS
Damage Limits
CHAPTER 56 - WINDOWS
Window Replacement Procedure
Damage Limits
TASK / A/C Reg / Certified by / Date
CHAPTER 61 - PROPELLERS
Operational and Functional Check
*Oil Level check
* Propeller Change
* PCU Change
TASK / A/C Reg / Certified by / Date
CHAPTERS 71 /72- POWERPLANT
Operational and Functional Check
(a)Engine Running Procedure (Min 10 runs) (include simulator time)
(b)Engine Rigging Procedure
Fault Isolation
Engine Change
MFC Change
TASK / A/C Reg / Certified by / Date
CHAPTER 73 - ENGINE FUEL & CONTROL
Operational and Functional Check
Replace High Pressure Fuel Filter
Replace Low Pressure Fuel Filter
CHAPTER 74 - IGNITION
Operational and Functional Check
Replace ignitors
TASK / A/C Reg / Certified by / Date
CHAPTER 75 – ENGINE AIR
Operational and Functional Check
CHAPTER 76 – ENGINE CONTROLS
Operational and Functional Check (ref chapter 72 above)
Rigging
TASK / A/C Reg / Certified by / Date
CHAPTER 77 - ENGINE INDICATING
Operational and Functional Check
CHAPTER 79 - OIL
Servicing
Replace engine oil High pressure filter
TASK / A/C Reg / Certified by / Date
CHAPTER 80 - STARTING
Description / operation
CHAPTER 49 - APU
Operation
ATA / ADDTIONAL EXPERIENCE / A/C Reg / Certified by / Date
ATA / ADDTIONAL EXPERIENCE / A/C Reg / Certified by / Date

Rev 04 - March 2010Page 1 of 31