CTHIn ForceLegislation
AD/S-PUMA/57 Amdt 1 - Tail Servo-Control
Eurocopter AS 332 (Super Puma) Series HeEurocopter AS 332 (Super Puma) Series Helicopters
Start here
Get a plain-English read of Eurocopter AS 332 (Super Puma) Series He
Turn the raw legal text into a practical explanation grounded in AD/S-PUMA/57 Amdt 1 - Tail Servo-Control.
Eurocopter AS 332 (Super Puma) Series Helicopters
| AD/S-PUMA/57 Amdt 1 | Tail Servo-Control | 11/2005 TX |
|---|
| Applicability: | AS 332 L, L1, C, C1 and AS 332 L2 helicopters fitted with tail servo-controls part number (P/N) SC7251 before amendment J or P/N SC7270 before amendment F. |
|---|---|
| Requirement: | 1. If not previously accomplished in accordance with AD/S-PUMA/57, perform a one time manual check for absence of axial play of the two levers along the distributor shafts of the tail servo-control in accordance with the instructions described in paragraph 2.B.3 of Eurocopter AS332 ASB 67.00.31.2. For installed servo-controls which have accumulated more than 535 hours times in service (TIS) since new at the effective date of this Directive, carry out the tightening torque check detailed in paragraph 2.B.2 of Eurocopter AS332 ASB 67.00.31.3. Manually check for absence of axial play of the two control levers along the distributor shafts of the tail servo-control, in accordance with paragraph 2.B.3. of Eurocopter AS332 ASB 67.00.31.4. In case of axial play, replace the servo-control before resuming flights, in accordance with paragraph 2.B.3. of Eurocopter AS332 ASB 67.00.31.5. For tail servo controls held as spares carry out the tightening torque check detailed in paragraph 2.B.2 of Eurocopter AS332 ASB 67.00.31.Note: DGAC AD F-2005-137 EASA approval No. 2005-6119 dated 27 July 2005 refers. This Directive supersedes UF-2004-197. |
| Compliance: | 1. Remains unchanged as detailed in the original issue of this Directive.For installed servo-controls which have accumulated more than 535 hours time in service (TIS) since new; Within 15 hours TIS after the effective date of the original issue of this Directive.For installed servo-controls which have accumulated less than 535 hours TIS since new; No later than 550 hours TIS since new.2. No later than within the 110 flying hours as from the effective date of this AD. |
| 3. For installed servo-controls which have accumulated more than 535 hours time in service (TIS) since new at the effective date of this Directive; No later than within a period of 135 to 165 flying hours following the check detailed in Requirement 2 of this Directive has been completed.For installed servo-controls which have accumulated less than 535 hours TIS since new at the effective date of this Directive; No later than within a period of 135 to 165 flying hours following the torque check detailed in Requirement 2 of this Directive has been completed.4. Before further flight following the effective date of this Directive.5. Before installation in a helicopter after the effective date of this Directive. |
|---|