CONTINUOUS AIRWORTHINESS MAINTENANCE PROGRAM (CAMP) ATTACHMENT A

TASK NUMBER

DESCRIPTION

R 1

TAIL ROTOR RIGGING CHECK

R 2

42° GEARBOX INSTALL

R 3

90° GEARBOX INSTALL

R 4

AERODYNAMICALLY ACTUATED ELEVATOR

R 5

AFCU

R 6

ANTI-TORQUE FRICTION ADJUSTMENT

R 7

BLADE BOLT TENSIONI ADJUSTMENT

R 8

UN-FOLDING MAIN ROTOR BLADES

R 9

COLLECTIVE MINIMUM FRICTION INSPECTION

R 10

CYCLIC MINIMUM FRICTION ADJUSTMENT

R 11

GOVERNOR

R 12

LOWER SERVO BOLT ALIGNMENT INSPECTION

R 13

MAIN DRIVE SHAFT

R 14

INSTALLATION OF MFCU

R 15

MAIIN ROTOR PITCH CHANGE LINKS

R 16

N1 RIGGING

R 17

N2 RIGGING

R 18

MAXIMUM NG TOPPING CHECK

R 19

TAIL ROTOR PITCH CHANGE BEARING INSPECTION

R 20

TAIL ROTORL REMOVAL/REPLACEMENT

R 21

TCU TORQUE LIMITING

R 22

TAIL ROTOR HANGER BEARING REPLACEMENT

R 23

TAIL ROTOR HUB AND BLADE

R 24

TAIL ROTOR COUPLING INSPECTION

R 25

TAIL ROTOR DRIVE SHAFT INSTALL

R 26

MAST ASSSEMBLY

R 27

ROTOR BRAKE QUILL

R 28

MAIN ROTOR BLADE INSTALLS

R 29

MAIN ROTOR SPINDALS

R 30

MAIN ROTOR HUB

R 31

ENGINE INSTALL (TWIN PACK)

R 32

TRANSMISSION INSTALL

R 33

SWASHPLATE ASSEMBLY

R 34

TAIL ROTOR RIGGING CHECK

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 01.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 01.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

This RII card is not for use on 412EP helicopters

2.7.2

A POC is required if any adjustment is made to the TR rigging and that it is entered into the aircraft Log Book.

2.7.3

This card is written assuming you do not have access to hydraulic power cart. Refer to MM if hydraulic cart is used.

2.7.4

Verify stops on bell crank below Tail Rotor servo are retracted completely prior to start.

2.7.5

Verify the length of series actuator when centered prior to rigging procedure.

2.7.6

Refer to Tail Rotor fiction RII task card

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 01.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

The rod end thread exposure is within limits on any control rod adjusted.

3.1.2

Rod end jam nuts are properly torqued on any control rod adjusted.

3.1.3

Control rods are free to rotate several degrees about the longitudinal axis on any control rod adjusted.

3.1.4

Control rod between pilot and copilot pedal adjuster is the correct length.

3.1.5

Clearance between link and bell crank below TRGB.

3.1.6

Control tube below engine CBOX is adjusted correctly.

3.1.7

Stops on bell crank below servo are adjusted correctly.

3.1.8

Clearance between TR blade and flap stop.

3.1.9

Anti torque magnetic brake arm is installed correctly.

3.1.10

Force gradient to pilot pedal adjuster is adjusted correctly.

3.1.11

Clearance of force gradient while moving the pedals stop to stop.

3.1.12

CMT transducers are adjusted to the correct length.

R 01.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Force gradient and transducer at the pilots pedal adjuster

4.2.2

Control tube at copilots pedal adjuster

4.2.3

Control tube at bell crank below the CBOX

4.2.4

Link at TRGB

4.2.5

PC link

RII INSPECTOR

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 02.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 02.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

A POC has been entered in aircraft Log Book for installation of 42° gearbox.

2.7.2

A post installation torque check has been entered in aircraft Log Book.

2.7.3

A leak check has been entered in aircraft Log Book.

2.7.4

Flex couplings are lubricated.

2.7.5

Grease is not expired.

2.7.6

Backlash and absence of binding of input and output quill.

Refer to MM

2.7.7

Oil was flushed if GB was preserved.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

2.7.8

Shims are bonded to tailboom structure.

2.8

Refer to Tail Rotor Drive Shaft RII task card for installation of Tail Rotor Drive Shaft.

R 02.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

GB mounting flange gaps.

Refer to MM

3.1.2

Bolt length is correct

3.1.3

Bolt grip bottom test is CW.

Refer to MM

3.1.4

Washer stack up is correct.

Refer to MM

3.1.5

Proper torque of bolts.

R 02.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Gear box is properly serviced.

4.2.2

Correct run in procedure was done during the POC.

4.2.3

Temp indicators have no indications after POC.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 03.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 03.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

POC required for installation of 90° gearbox is entered in aircraft Log Book.

2.7.2

Post installation torque check is in logbook.

2.7.3

Leak check is entered in log book.

2.7.4

Flex couplings are lubricated. (Refer to Paperwork)

2.7.5

Grease is not expired. (Refer to Paperwork)

2.7.6

Backlash and absence of binding of input quill.

Refer to MM.

2.7.7

Oil was flushed if GB was preserved.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

2.8

Refer to RII task card for installation of Tail Rotor Drive Shaft.

R 03.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

Mounting flange is free of sealant.

3.1.2

Correct torque procedure is used.

3.1.3

Proper torque of bolts.

3.1.4

Correct thread length of stud through nut.

3.1.5

Gap between shim and input quill is correct.

3.1.6

TR pitch change mechanism washer stack up is correct.

3.1.7

TR pitch change mechanism torque is correct.

3.1.8

TR pitch change mechanism hardware is safety.

R 03.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Gear box is properly serviced.

4.2.2

Correct run in procedure was done during the POC.

4.2.3

Temp indicators have no indications after POC.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 04.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 04.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Ensure a POC required for adjustment or installation of elevator is entered in the aircraft Log Book.

R 04.3

INPROCESS INSPECTIONS

3.1

Prior to installation of access panel;

3.1.1

Confirm bolts have been installed and safety.

3.1.2

Apply torque strip after bolts have been checked for torque. (this is not required on hardware that contains safety’s)

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 04.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Check that elevator moves freely with no binding of spring. Check for excessive play in elevator horn shimming.

Bell MM Chapter 67

4.3

Check access panel bolts for attachment and security.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 05.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 05.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

POC required for installation of the AFCU is entered in the aircraft Log Book.

2.7.2

Refer to N1 rigging task card.

2.7.3

Refer to Fuel pump task card (if removed).

2.7.4

Refer to MFCU task card (if removed)

2.7.5

Checks in “After Component Replacement Table” of P&W MM are entered in the log book.

2.7.6

Leak check is written up in aircraft Log Book.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

NOTE: The AFCU may be changed independently or as a complete AFCU, MFCU, fuel pump assembly.

2.7.7

Verify if AFCU will require “reconditioning after storage”.

R 05.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

All previously installed components of the AFCU are safetied.

3.1.2

Jam nuts are torqued.

3.1.3

Tubes are aligned with fittings.

3.1.4

Screen is installed in AFCU

3.1.5

Coupling shaft is installed between AFCU and fuel pump.

R 05.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Retention nuts on AFCU are torque.

4.2.2

Torque on all B nuts.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 06.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 06.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify that the Anti-Torque Force Gradient has been disconnected at the pilot side TR pedal assembly.

R 06.3

INPROCESS INSPECTIONS

3.1

Verify friction force of 4.25 to 4.75 pounds, measured at TR pedals, when pedals are moved through the neutral position.

3.2

Ensure full travel of TR Pedals can be achieved without binding or interference after any adjustments.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 06.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Ensure Force Gradient has been re-installed, torqued and safetied.

4.3

Ensure lower access panel on bottom of aircraft is properly re-installed.

4.4

A POC Log Book entry is required if an adjustment is made to the Tail Rotor friction.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 07.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 07.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Read the MM section describing the task Specific.

2.8

Refer to ASB for procedures to this task.

2.9

Verify part of ASB (25 hr torque check) is in log book.

R 07.3

INPROCESS INSPECTIONS

3.1

Verify expandable bolt segments are installed in correct order.

3.2

Verify bolt tension is adjusted correctly.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 07.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Bolt is fully seated in Main Rotor head

4.2.2

Bolt and handle is installed in correct position in Main Rotor head.

4.2.3

Safety is installed in Main Rotor blade bolt handle.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 08.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 08.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

R 08.3

INPROCESS INSPECTIONS

3.1

None.

R 08.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Blade bolts are color coded to the Main Rotor blades they are installed in.

4.2.2

Spring clip is seated over the tension adjustment nut and secured with the safety pin.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

4.2.3

Blade racks are removed. (if used)

4.2.4

Droop restraint tube, locking pins, spindle pins, and blade locks are removed from top of helicopter. (if used)

4.3

If droop restraint tube is used confirm Main Rotor Pitch Change links are reinstalled. Verify torque and safety.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 09.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 09.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Check for POC entry in the discrepancy section of the log book for the maintenance task.

2.8

Confirm the correct section of the MM is being used for the serial number of the AC.

R 09.3

INPROCESS INSPECTIONS

3.1

Ensure all collective control bolts are installed and cotter pins and lockwire are installed, where applicable.

R 09.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Check all access panels for installation and security.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 10.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 10.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

Cyclic Friction Nut on cyclic stick is loosened completely, (Rotated counter- clockwise fully) before friction force measurement is observed.

2.7.2

Force Trim is turned off.

R 10.3

INPROCESS INSPECTIONS

3.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

3.2

Verify;

3.2.1

Cyclic fore/aft breakout force measurement of .50-1.0 lbs.

3.2.2

Cyclic lateral cyclic breakout force measurement of .50-1.0 lbs.

R 10.4

POST TASK INSEPCTIONS

4.1

Verify;

4.1.1

Friction clamp halves on cyclic stick are equally spaced

4.1.2

With Force Trim on observe cyclic fore/aft breakout force of 2.25-2.75lbs.

4.1.3

Force Trim on observe cyclic lateral breakout force of .50-2.00 lbs.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 11.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 11.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

A POC is required for replacement of the governor. Refer to checks after component replacement table in PW MM.

R 11.3

INPROCESS INSPECTIONS

3.1

Verify coupling installation in Combining Gearbox.

R 11.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

4.2

Verify:

4.2.1

Nuts are torqued.

4.2.2

Safeties on all air lines.

4.2.3

Min and Max stops are set correctly.

4.3

Refer to N2 rigging Task card.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 12.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 12.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

R 12.3

INPROCESS INSPECTIONS

3.1

With lower servo piston rod bolt removed, verify that there are no side loads present on lower piston rod where it aligns with bolt hole. Piston rod must be able to travel freely, up and down without any pressure, forcing, binding, or bending of piston rod in for, aft, left or right direction. If alignment adjustments are made to servo comply with steps 2-4 of this section.

3.2

Verify:

3.2.1

Torque Bearing Nut has been torqued 900-1100 inch-pounds

3.2.2

Torque Jam Nut has been torqued 900-1100 inch-pounds.

3.2.3

Both Torque Nuts have been properly secured with lockwire to the keyed washer.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 12.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Ensure lower servo bolt has been installed and torqued 95-100 in-lbs.

4.3

Verify cotter key is installed in lower servo bolt.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 13.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 13.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

POC is required for installation of main drive shaft. Verify entry in log book.

2.8

Leak check is required for installation of main driveshaft. Verify entry in log book.

2.9

Verify couplings are lubricated. Refer to paperwork.

2.10

Verify grease is within expiration date. Refer to paperwork.

R 13.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

Correct torque sequence is used.

3.1.2

Correct torque is used.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 13.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify the temp indicators have no indications after POC.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 14.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 14.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Prior to Installation verify integrity of lock wiring and locking seals on unit.

R 14.3

INPROCESS INSPECTIONS

3.1

For PT6T-3B Engines verify MFCU seal drain port is installed.

3.2

Verify that strainer (34) and seat (33) have been installed prior to installing fuel inter- connect tube into AFCU port.

3.3

Ensure retaining plate(28) has been installed, torqued, and safetied.

3.4

Ensure proper packings are placed in fuel ports at MFCU/Fuel Pump mating surfaces. (If there are still old packings in these recesses they must be discarded and replaced)

3.5

On all Post-SB5041 and PT6T-3B/-3BE engines ensure Pressure Regulating Valve has been properly installed.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

3.6

Before MFCU/AFCU linkage is installed ensure that a fits and clearances check has been performed IAW P&W PT6T-3B MM.

R 14.4

POST TASK INSEPCTIONS

4.1

Verify;

4.1.1

MFCU/AFCU interconnect linkage is attached.

4.1.2

Ensure Bolts securing MFCU to Fuel Pump have been properly torqued and torque striped.

4.1.3

Ensure all attached fuel lines have been secured and torqued properly.

4.1.4

All lines with holes drilled in the B-Nut have been safetied wired properly.

4.1.5

That following engine checks are written up in the logbook;

4.1.5.1

Dry Motoring Run

4.1.5.2

Wet Motoring Run

4.1.5.3

Max Ng. and Manual/Automatic Interconnect Linkage Adjustment

4.1.5.4

Power Turbine Governor Check

4.1.5.5

Power Check

4.1.5.6

Acceleration Check

4.1.5.7

Deceleration Check

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 15.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 15.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

R 15.3

INPROCESS INSPECTIONS

3.1

None

R 15.4

POST TASK INSEPCTIONS

4.1

Verify;

4.1.1

PC links are installed in correct location.

4.1.2

PC link rod ends thread minimum engagement is correct.

4.1.3

Bolt heads are installed in the direction of rotation.

4.1.4

Correct toque on hardware.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

4.1.5

Bushings are installed in correct locations.

4.1.6

Rod end anti rotation pin is engaged to bracket.

4.1.7

Upper rod end is centered in PC link.

4.1.8

All safeties.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 16.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 16.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

An POC is required for adjustment of the throttles.

R 16.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

Control tube rod ends have not exceeded the maximum exposed thread lengths.

3.1.2

Safeties are installed in all locations.

3.1.3

Correct torque was used on control tube jam nuts.

3.1.4

Control tube rod ends are adjusted so both ends are centered on bellcranks allowing the maximum rotation of the control tube.

3.1.5

Collective flex shaft to gear selector has proper engagement (pilot and copilot. Number one and two throttles).

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

3.1.6

Pilot and co pilot throttles hit the collective lever stops at the same time.

3.1.7

Number 1 and 2 FCU levers are positioned correctly on the shaft.

3.1.8

Correct torque on nut of FCU lever if adjusted.

3.1.9

Correct gap of fuel control interconnect.

R 16.4 POST TASK INSEPCTIONS

4.1 Ve

rify;

4.1.1

Smooth operation of the throttles through the entire range.

4.1.2

Idle speeds are correct.

4.1.3

Tube clearance in the area of the FCU tubing.

4.1.4

Throttle cushions are the correct amount.

4.1.5

Both throttles rotate approx the same degrees from stop to stop.

4.1.6

FCU stops hit prior to collective lever stops.

4.1.7

Cushions are equal on full open and full closed positions.

4.2 C

t t S

heck for entry in the corrective action section of the log book for the maintenance ask. At a minimum the log book entry shall contain the following: A description of he maintenance task. A reference to the acceptable data used. Aircraft TT. Date. ignature. A&P number.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 17.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 17.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

An POC is required for adjustment of the N2 system.

R 17.3

INPROCESS INSPECTIONS

3.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

3.2

Verify;

3.2.1

Linier actuator wires are connected to proper terminals on engine 1 and engine 2.

3.2.2

Governor control arms are installed in correct position on engine 1.

3.2.3

Engine 2 ITT actuator (TB412-93-118) is installed with terminal block facing down.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

3.3

Prior to ground run verify AFCU and MFCU stops make contact. Refer to N1 rigging task card if adjustment is necessary.

R 17.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Jam nuts on rod ends are torqued.

4.2.2

Safeties in bolts and nuts.

4.2.3

Jam nut on actuator is torqued.

4.2.4

Rod ends maximum visible threads are within tolerance.

4.2.5

Control rods are free to rotate several degrees about longitudinal axis.

4.2.6

Firewall and engine deck boot is secure.

4.2.7

Hardware securing all bell cranks, governors, and cam box are torqued.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 18.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 18.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Discuss with the technician to determine if the topping check will be done on the ground or in flight. Determine if part power or slave stops will be installed for the check.

2.8

Confirm the correct section of the MM is being used for the serial number of the AC.

2.9

Check for POC entry in the discrepancy section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description stating what POC procedure is due. Aircraft TT. Date. Signature. A&P number.

R 18.3

INPROCESS INSPECTIONS

3.1

If part power stops or slave stops are installed check that they have been properly secured in the use position.

3.2

If during the check an adjustment is made to the topping adjustment screw check the interconnect linkage for proper AUTO/MAN gap and proper throttle cushions. Check for engagement of the interconnect linkage nut in the lock. Check for freedom of throttle movement.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 18.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the check. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date.

Signature. A&P number.

4.2

Verify the interconnect linkage for proper AUTO/MAN gap and proper throttle cushions. Check for engagement of the interconnect linkage nut in the lock. Check topping screw for proper safety. Check for freedom of throttle movement. Check for clearance of throttle control tubes throughout full travel.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 19.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 19.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Check for POC entry in the discrepancy section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description stating what POC procedure is due. Aircraft TT. Date. Signature. A&P number.

R 19.3

INPROCESS INSPECTIONS

3.1

Inspect pitch change bearing nut for safety prior to reinstallation of the bearing retainer IAW MM.

R 19.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Confirm retainer is torque, the retainer lock is installed and lock screws are safety IAW MM.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 20.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 20.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

If cylinder is a replacement, ensure that clevis installed in top of piston is adjusted so that the correct distance between bolt hole centerline and top of piston is obtained.

R 20.3

INPROCESS INSPECTIONS

3.1

Ensure Trunnion Plates are installed/oriented properly.

3.2

Verify torque of adjustable clevis locking nut.

3.3

Verify Spacer is placed over bolt securing lower portion of servo to bellcrank.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 20.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Torque of nuts

4.2.2

Safety/cotter keys on nuts.

4.2.3

All hydraulic lines on Tail Rotor Servo have been installed and torqued properly.

4.2.4

Torque stripe have been applied to all lines and nuts after ensuring that they are properly torqued

4.2.5

Hydraulic System has been re-serviced.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 21.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 21.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Discuss with the technician to determine if the TCU check will be done on the ground or in flight.

2.8

If TCU check is to be done in flight confirm TCU setting screw is adjusted to the test setting.

2.9

Confirm the correct section of the MM is being used for the serial number of the aircraft.

2.10

Confirm the correct section of the MM is being used for the type of TCU installed.

2.11

Check for POC entry in the discrepancy section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description stating what POC procedure is due. Aircraft TT. Date. Signature. A&P number.

2.12

Refer to checks after component replacement table in PW MM.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 21.3

INPROCESS INSPECTIONS

3.1

Confirm proper table is being used for pressure gauges.

R 21.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the check. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date.

Signature. A&P number.

4.2

Check that all lines removed during the check are reconnected and re safety.

4.3

Apply torque stripe to all lines after the torque has been checked (not required if safety wired).

4.4

If applicable re safety the adjustment dome. (only certain models of TCU)

4.5

If TCU was checked in flight confirm the final adjustment was made to TCU setting screw. (after flight)

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 22.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 22.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

Verify;

2.7.1

Bearing and couplings are lubricated. Refer to paperwork.

2.7.2

Grease is not expired. Refer to paperwork.

2.7.3

Leak check is entered in log book

R 22.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

Correct washers are installed between brace and support. (number 1 hanger only)

3.1.2

Length of bolts.

Refer to MM

3.1.3

Correct washer stack up under bolt head.

Refer to MM

3.1.4

Proper torque was used for bolts.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 22.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Flexible coupling is forward.

4.2.2

Correct ground run in procedure was complied with.

4.2.3

Temp indicators for bearing and coupling have no indications after ground run.

4.3

Refer to RII task card for TR DS install.

INITIALS

SIGNATURE

CERTIFICATE TYPE & NUMBER

Registration No.:

N

Start

Aircraft Start Total Time:

Aircraft S/N:

Date:

Aircraft Start Total Cycles:

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

R 23.1

GENERAL

1.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

1.2

Check for entry in the discrepancy section of the log book/Work Order for RII due. At a minimum the log book entry shall contain the following: A description stating that the RII for the maintenance item is due. Aircraft TT. Date. Signature. A&P number.

R 23.2

PRIOR TO STARTING TASK

2.1

Verify any new parts used have correct paperwork.

2.2

Verify the maintenance manual is the correct revision number. Check MM revision number against the MHI master publications list.

2.3

Check computer tracking system for any item or inspection that could be affected by the maintenance task.

2.4

Inspect all calibrated tool’s inspection decal that will be used in the task to confirm it is in current calibration.

2.5

Verify that any new P/N used is compatible with aircraft S/N.

2.6

Read the MM section describing the task.

2.7

POC is required for the installation of the TR and Hub assembly.

2.8

Verify post installation torque check has been entered into aircraft Log Book.

R 23.3

INPROCESS INSPECTIONS

3.1

Verify;

3.1.1

Cone seat is installed correctly.

3.1.2

TR retention nut is torque correctly and safety.

3.1.3

Special washer is installed in correct direction in crosshead.

3.1.4

TR crosshead bearing was greased prior to install.

3.1.5

TR crosshead bearing nut is torque and safety.

MAINTENANCE ACTION

REFERENCE

RII INSPECTORS INITIALS

3.1.6

Retainer is torqued.

3.1.7

Crosshead bearing was not over greased.

R 23.4

POST TASK INSEPCTIONS

4.1

Check for entry in the corrective action section of the log book for the maintenance task. At a minimum the log book entry shall contain the following: A description of the maintenance task. A reference to the acceptable data used. Aircraft TT. Date. Signature. A&P number.

4.2

Verify;

4.2.1

Retainer lock is installed safety and deformed in the correct locations.

4.2.2

Pitch horn bolts are torqued.

4.2.3

Pitch horn bolt washers are installed correctly.

4.2.4

Blade bolts are torqued.

4.2.5

Pitch link bolts are safety.