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S-92®HELICOPTER 

ALERT SERVICE 

BULLETIN 

NOTICE TO ALL PERSONS RECEIVING THIS DOCUMENT: 

WARNING: THIS DOCUMENT, OR AN EMBODIMENT OF IT IN ANY MEDIA, DISCLOSES INFORMATION WHICH IS PROPRIETARY, IS THE PROPERTY OF SIKORSKY AIRCRAFT CORPORATION AND/OR ITS SUBSIDIARIES, IS 

AN UNPUBLISHED WORK PROTECTED UNDER APPLICABLE COPYRIGHT LAWS, AND IS DELIVERED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED, DISCLOSED, REPRODUCED, IN WHOLE OR IN PART 

(INCLUDING REPRODUCTION AS A DERIVATIVE WORK), OR USED FOR MANUFACTURE FOR ANYONE OTHER THAN SIKORSKY AIRCRAFT CORPORATION AND/OR ITS SUBSIDIARIES WITHOUT ITS WRITTEN CONSENT,

AND THAT NO RIGHT IS GRANTED TO DISCLOSE OR SO USE ANY INFORMATION CONTAINED HEREIN. ALL RIGHTS RESERVED. ANY ACT IN VIOLATION OF APPLICABLE LAW MAY RESULT IN CIVIL AND CRIMINAL 

PENALTIES. 

S-92®IS A REGISTERED TRADEMARK OF SIKORSKY AIRCRAFT CORPORATION. 

ASB 92-67-006 

February 16/16 

Revision A ▪ February 19/16 

SUBJECT: FLIGHT CONTROLS – Pushrods – One-Time Inspection of Main Rotor and Tail Rotor Servo 

Pushrods

Section 1. PLANNING INFORMATION 

A. Effectivity S-92A model helicopters with serial numbers 920006 through 920291. 

B. Purpose To provide instructions to inspect for proper pushrod assembly. 

C. Background Main rotor servo input pushrods and tail rotor servo pushrods were found with 

incorrect safety cable routing, incorrect jam nut torque, and/or incorrect locking 

device serrations and keys engagement. 

D. Description Helicopter is prepared for inspection. Flight control rods are inspected for safety 

cable routing, engagement of serrations of locking device, engagement of keys on 

locking device, thread engagement, and torque of jamnuts. Non-compliant 

inspection results are documented on Pushrod Data Sheet. If any discrepancies 

are found, applicable pushrod is removed, reworked, reinstalled, or replaced. Rig 

check is performed, as required. Helicopter is returned to service. 

E. Compliance Compliance is essential. The inspection outlined herein must be accomplished no 

later than May 16, 2016. 

Sikorsky Aircraft Corporation

6900 Main StreetP.O. Box 9729

Stratford, Connecticut 06615-9129

(203) 386-4000

 S-92

WARNING ‒ This information contains technical data subject to the EAR. Diversion contrary to US Law is prohibited. ECCN: 9E991
S-92 ALERT ASB 92-67-006 

SERVICE BULLETIN Revision A ▪ February 19/16 

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Section 1. PLANNING lNFORMATION (Continued) 

F. Approval Inspection item. 

G. Manpower (Estimated) 

Task No. of Men No. of Hours Man-Hours*

Inspection of Flight Control Pushrods 1 2.0 2.0

Rework of Flight Control Pushrods 1 2.0 2.0

Performance of Rig Check 2 1.0 2.0**

Total Man-Hours 6.0

*Estimate does not include time required to prepare helicopter or return it to flight status.

**Estimated time is for passing a rig check on the first attempt.

H. Tooling 

Qty Nomenclature Part No. Source

1 Lighted Borescope Commercially available or equivalent (1)

1 Inspection Mirror Commercially available or equivalent (1)

1 Torque Wrench (30 - 150 in. lbs.) Commercially available or equivalent (1)

1 Torque Wrench (150 - 750 in. 

lbs.)

Commercially available or equivalent (1)

(1) Available through normal supply channels. 

I. Weight and Balance 

Not affected. 

J. Electrical Load Data 

Not affected. 

K. Software Load Data 

Not changed. 

L. References 

(1) Maintenance Manual, SA S92A-AMM-000, Task 21-23-02-900-003/-004. 

(2) Maintenance Manual, SA S92A-AMM-000, Task 53-70-00-900-001. 

(3) Maintenance Manual, SA S92A-AMM-000, Task 54-72-03-900-003/-004. 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
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Section 1. PLANNING INFORMATION (Continued) 

(4) Maintenance Manual, SA S92A-AMM-000, Chapter/Section 67-00-07. 

(5) Maintenance Manual, SA S92A-AMM-000, Task 67-11-04-960-009. 

(6) Maintenance Manual, SA S92A-AMM-000, Task 67-12-03-960-005. 

(7) Maintenance Manual, SA S92A-AMM-000, Task 67-14-04-960-002. 

(8) Maintenance Manual, SA S92A-AMM-000, Task 67-14-05-900-001/-002. 

(9) Maintenance Manual, SA S92A-AMM-000, Task 67-14-06-960-001. 

(10) Maintenance Manual, SA S92A-AMM-000, Task 67-21-04-960-007. 

(11) Maintenance Manual, SA S92A-AMM-000, Task 67-23-01-960-007. 

M. Publications Affected 

(1) Temporary Revision No. 5-173 against Maintenance Manual, SA S92-AWL-000, Task 5-

20-00-200-007, is issued concurrently with this ASB. 

(2) Temporary Revision No. 67-09 against Maintenance Manual, SA S92-AMM-000, Task 67-

11-04-960-009, will be issued at a later date. 

(3) Temporary Revision No. 67-10 against Maintenance Manual, SA S92-AMM-000, Task 67-

12-03-960-005 and 67-12-03-300-002, will be issued at a later date. 

(4) Temporary Revision No. 67-11 against Maintenance Manual, SA S92-AMM-000, Task 67-

14-04-960-002, will be issued at a later date. 

(5) Temporary Revision No. 67-12 against Maintenance Manual, SA S92-AMM-000, Task 67-

14-06-960-001, will be issued at a later date. 

(6) Temporary Revision No. 67-13 against Maintenance Manual, SA S92-AMM-000, Task 67-

21-04-960-007, will be issued at a later date. 

(7) Temporary Revision No. 67-14 against Maintenance Manual, SA S92-AMM-000, Task 67-

23-01-960-007, will be issued at a later date. 

(8) Temporary Revision No. 67-15 against Maintenance Manual, SA S92-AMM-000, Task 

Chapter/Section 67-00-00, is issued concurrently with this ASB. 

N. Attachment 

None. 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
S-92 ALERT ASB 92-67-006 

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Section 2. MATERIAL INFORMATION 

A. Basis for Material Data 

Per helicopter. 

B. Bill of Material 

None. 

C. Consumable Material 

Qty Nomenclature Part No. Source

A/R 0.02 Inch Diameter Safety Cable Commercially available or equivalent (1)

A/R 0.02 Inch Diameter Safety Wire Commercially available or equivalent (1)

(1) Procure locally. 

Section 3. ACCOMPLISHMENT INSTRUCTIONS 

A. Prepare helicopter for modification: 

(1) Turn off all helicopter electrical and hydraulic power. 

(2) Engage rotor brake. 

TO PREVENT ELECTRICAL SHOCK OF PERSONNEL OR POSSIBLE 

DAMAGE TO HELICOPTER COMPONENTS, MAKE SURE TO TURN 

OFF ALL ELECTRICAL POWER.

WHEN ANY COMPONENT OF ANY FLIGHT CONTROL SYSTEM IS 

DISCONNECTED, REMOVED, AND REINSTALLED OR REPLACED, 

A RIGGING CHECK OF THE AFFECTED SECTION MUST BE MADE 

TO BE SURE THAT CONTROL RANGES ARE WITHIN SPECIFIED 

LIMITS.

OBSERVE ALL CAUTIONS AND WARNINGS ON CONTAINERS 

WHEN USING CONSUMABLES. WHEN APPLICABLE, WEAR 

NECESSARY PROTECTIVE GEAR DURING HANDLING AND USE. IF 

A CONSUMABLE IS FLAMMABLE OR EXPLOSIVE, MAKE CERTAIN 

CONSUMABLE AND ITS VAPORS ARE KEPT AWAY FROM HEAT, 

SPARK AND FLAME. MAKE CERTAIN FIREFIGHTING EQUIPMENT 

IS READILY AVAILABLE PRIOR TO USE. FOR ADDITIONAL 

INFORMATION ON TOXICITY, FLASHPOINT AND FLAMMABILITY 

OF CHEMICALS, CONSULT YOUR MEDICAL PEOPLE OR THE 

MANUFACTURER OF THE CONSUMABLE.

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

(3) Open main rotor pylon sliding fairing. (Refer to Maintenance Manual, SA S92A-AMM-000, 

Task 53-70-00-900-001). 

(4) Remove tail rotor servo fairing assembly. (Refer to Maintenance Manual, SA S92A-AMM000, Task 54-72-03-900-003).

(5) Remove mixer top plate. (Refer to Maintenance Manual, SA S92A-AMM-000, Task 67-14-

05-900-001). 

(6) If necessary, remove air conditioning crossover duct (92309-04818-101/-104). (Refer to 

Maintenance Manual, SA S92A-AMM-000, Task 21-23-02-900-003). 

(7) If necessary, remove applicable interior panels. (Refer to Maintenance Manual, SA S92AAMM-000, Chapter 25). 

NOTE: Perform all of the following inspections before correcting any non-conformities. 

B. Inspect flight control pushrods listed in Table 1 as follows (Figure 1): 

(1) Visually inspect adjustable ends of pushrods for proper safety cable routing. Right hand 

threads shall have safety cable routed as shown in Figure 2. Left hand threads shall have 

safety cable routed as shown in Figure 3. If safety cable is installed incorrectly, record 

results on Pushrod Data Sheet. (Refer to Pushrod Data Sheet, step K.). 

NOTE: Use of a lighted borescope (commercially available or equivalent) may aid 

during inspection. 

(a) For upper deck quadrant pushrod (92400-04802-105) only, if safety cable is 

incorrect, access must be gained to the pushrod and steps B.(2), B.(3), and B.(4) 

must be performed. Steps B.(3)(a) and B.(4)(a) cannot be applied. 

NOTE: Use of a lighted borescope (commercially available or equivalent) may aid while 

inspecting upper deck quadrant pushrod (92400-04802-105). 

(2) Where locking devices are used, visually inspect adjustable ends of pushrods for proper 

engagement of serrations and keys of the locking device. If serrations and keys of locking 

device are not properly engaged, record results on Pushrod Data Sheet. (Refer to Pushrod 

Data Sheet, step K.). (Refer to Figure 4).

(3) Inspect adjustable ends of pushrods for minimum thread engagement. Check that 

adjustable rod end, or clevis, is threaded beyond the inspection hole and that 0.02 inch 

diameter safety wire (commercially available or equivalent) cannot be inserted through the 

hole.If adjustable ends of pushrods do not have proper thread engagement, record results 

on Pushrod Data Sheet. (Refer to Pushrod Data Sheet, step K.). 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

NOTE: Use of a lighted borescope (commercially available or equivalent) may aid 

while inspecting upper deck quadrant pushrod (92400-04802-105). 

(a) For upper deck quadrant pushrod (92400-04802-105) only, if safety cable is installed 

correctly, locking devices pass visual inspection, and an acceptable maintenance 

phase inspection that would allow access to the pushrod does not coincide with the 

accomplishment of this ASB, step B.(3) can be deferred until the pushrod is 

accessible and step B.(3)(b) and B.(3)(c) can be performed as an alternate means of 

compliance. The procedure in step B.(3) above shall be accomplished the next time 

the pushrod is accessible, not to exceed the next 1500 hour inspection if not done at 

this time 

(b) If B.(3) is deferred for the upper deck quadrant pushrod (92400-04802-105), a visual 

inspection is required to confirm that threads are visible in the inspection hole. If 

threads are not visible, record results on Pushrod Data Sheet and proceed to step 

B.(4). Step B(4)(a) cannot be applied. 

(c) If B.(3) is deferred for the upper deck quadrant pushrod (92400-04802-105), record 

the inspection requirement in the helicopter logbook. 

NOTE: Do not turn pushrod tube to determine looseness of jamnut or fasteners. 

(4) For all adjustable pushrods, check jamnut for looseness using finger pressure with safety 

cable removed. Jamnut shall not turn in either direction. If jamnut moves with finger 

pressure, record results on Pushrod Data Sheet. (Refer to Pushrod Data Sheet, step K.). 

(a) For upper deck quadrant pushrod (92400-04802-105) only, if safety cable is installed 

correctly, locking devices pass visual inspection, threads are visible through the 

inspection hole, and an acceptable phase inspection that would allow access to the 

pushrod does not coincide with the accomplishment of this ASB, step B.(4) can be 

deferred until the pushrod is accessible and step B.(4)(b) and B.(4)(c) can be 

performed as an alternate means of compliance. The procedure in step B.(4) above 

shall be accomplished the next time the pushrod is accessible, not to exceed the 

next 1500 hour inspection if not done at this time. 

(b) If B.(4) is deferred for the upper deck quadrant pushrod (92400-04802-105), a visual 

inspection in the interim is required to confirm that there is no clearance between the 

jam nut, locking device, and pushrod insert around the entire periphery of these 

items. If clearance is present, gain access to the pushrod and check jamnut for 

looseness using finger pressure, with safety cable removed. Jamnut shall not turn in 

either direction. If jamnut moves with finger pressure, record results on Pushrod 

Data Sheet. 

(c) If B.(4) is deferred for the upper deck quadrant pushrod (92400-04802-105), record 

the inspection requirement in the helicopter logbook. 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

PUSHROD IDENTIFICATION - TABLE 1 

NOMENCLATURE PART NUMBER TORQUE VALUE TASK NUMBER

Yaw Boost Input Pushrod 92400-04801-108 60-100 inch 

pounds

67-21-04-960-007

Pitch Boost Input Pushrod 92400-04801-107 43 inch-pounds 67-11-04-960-009

Collective Boost Input Pushrod 92400-04801-107 350 inch-pounds 67-12-03-960-005

Roll Boost Input Pushrod 92400-04801-109 43 inch pounds 67-11-04-960-009

Yaw Boost Out Pushrod 92400-04802-109 40-46 inch-pounds 67-14-04-960-002

Roll Boost Out Pushrod 92400-04803-103 40-46 inch-pounds 67-14-04-960-002

Pitch Boost Out Pushrod 92400-04803-102 40-46 inch-pounds 67-14-04-960-002

Collective Boost Out Pushrod 92400-04802-108 40-46 inch-pounds 67-14-04-960-002

Limiter Pushrod 92400-04803-106 40-46 inch-pounds 67-14-04-960-002

Pitch to Roll Pushrod 92400-04803-107 40-46 inch-pounds 67-14-04-960-002

Left Hand Main Rotor Servo Pushrod 92400-04801-110 350 inch-pounds 67-14-06-960-001

Forward Main Rotor Servo Pushrod 92400-04801-111 350 inch-pounds 67-14-06-960-001

Right Hand Main Rotor Servo Pushrod 92400-04801-112 350 inch-pounds 67-14-06-960-001

Upper Deck Quadrant Pushrod 92400-04802-105 60-100 inchpounds67-21-04-960-007

Tail Rotor Servo Input Pushrod 92400-04802-107 40-46 inch-pounds 67-23-01-960-007

NOTE: If safety cable is routed properly, keys and serrations are properly engaged, thread is 

properly engaged, and jamnut does not move, proceed to step D. 

C. Disposition of Non-Conforming Material: 

(1) If jamnut inspected in step B.(4) failed the finger pressure check, perform the following: 

(a) Remove and replace pushrod per applicable AMM task. If a replacement part is not 

readily available, contact Sikorsky Aircraft Corporation for inspection instructions to 

determine if pushrod may be suitable for limited use. 

(2) If threads inspected in step B.(3) are not properly engaged, perform the following: 

(a) Gain access to applicable control rod, as required. 

(b) Remove applicable pushrod. (Refer to task listed in Table 1). 

(c) Measure and record length from mounting centers. 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

(d) Measure and record rod end, or clevis, orientation. 

(e) If required, remove safety cable. 

NOTE: Make sure serrations and key are properly engaged. 

(f) Reassemble rod end, jamnuts, and locking device. 

(g) Adjust to recorded length and rod end, or clevis, orientation. 

(h) Install applicable pushrod. (Refer to task listed in Table 1). 

(i) Check that adjustable rod end, clevis, and adjuster are threaded beyond the 

inspection hole such that a 0.02 inch diameter safety wire cannot be inserted 

through hole. 

(j) Using torque wrench (commercially available or equivalent), torque jamnut. (Refer to 

task and torque value listed in Table 1). 

NOTE: Make sure safety cable is routed in the proper direction for left hand or right 

hand thread. (Refer to Figures 2 and 3). 

(k) Install safety cable. 

(l) If required, perform quick rigging check. (Refer to Maintenance Manual, SA S92AAMM-000, Chapter/Section 67-00-07). 

(m) Proceed to step E. 

(3) If serrations and keys of the locking device inspected in step B.(2) are not properly 

engaged, perform the following: 

(a) Gain access to applicable control rod, as required. 

(b) If required, remove safety cable. 

(c) Back off jamnut and inspect locking device for damage. Replace locking device as 

required. (Refer to task listed in Table 1). 

(d) Using torque wrench (commercially available or equivalent), torque jamnut. (Refer to 

task and torque value listed in Table 1) 

NOTE: Make sure safety cable is routed in the proper direction for left hand or right 

hand thread. (Refer to Figures 2 and 3). 

(e) Install safety cable. 

(f) If required, perform quick rigging check. (Refer to Maintenance Manual, SA S92AAMM-000, Chapter/Section 67-00-07).

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

(g) Proceed to step E. 

(4) If safety cable inspected in step B.(1) is installed incorrectly, perform the following: 

(a) Gain access to applicable control rod, as required. 

(b) If required, remove safety cable. 

(c) Using torque wrench (commercially available or equivalent), torque jamnut. Record if 

jamnut moves at minimum torque. (Refer to task and torque value listed in Table 1). 

NOTE: Make sure safety cable is routed in the proper direction for left hand or right 

hand thread. (Refer to Figures 2 and 3). 

(d) Install safety cable. 

(e) Proceed to step E. 

D. Disposition of Conforming Material: 

NOTE: For upper deck quadrant pushrod (92400-04802-105) only, proceed to step E if 

inspections B.(3) and B.(4) were deferred. Add the torque wrench verification 

below to the logbook to be performed the next time the pushrod is accessible, not 

to exceed the next 1500 hour inspection if not done at this time, as an alternate 

means of compliance to step D.(1). 

(1) If safety cable is routed properly, keys and serrations are properly engaged, thread is 

properly engaged, and jamnut does not move with finger pressure, perform the following: 

(a) Using torque wrench (commercially available or equivalent), torque jamnut. (Refer to 

task and torque value listed in Table 1). 

NOTE: Make sure safety cable is routed in the proper direction for left hand or right 

hand thread. (Refer to Figures 2 and 3). 

(b) Install safety cable. 

E. Install tail rotor servo fairing assembly. (Refer to Maintenance Manual, SA S92A-AMM-000, Task 

54-72-03-900-004).

F. Install mixer top plate. (Refer to Maintenance Manual, SA S92A-AMM-000, Task 67-14-05-900-

002). 

G. If removed, install air conditioning crossover duct (92309-04818-101/-104). (Refer to 

Maintenance Manual, SA S92A-AMM-000, Task 21-23-02-900-004). 

H. If removed, install applicable interior panels. (Refer to Maintenance Manual, SA S92A-AMM-000, 

Chapter 25). 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

I. Close main rotor pylon sliding fairing. (Refer to Maintenance Manual, SA S92A-AMM-000, Task 

53-70-00-900-001). 

J. Return helicopter to service. 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

K. Pushrod Data Sheet: 

(1) Report the non-conforming data, fax to facsimile number (860-998-7565) or scan and email 

to: GPSIKSASProductSafet@utc.com. 

(2) Record the following information for each pushrod, and attach labeled photographs 

showing the same: 

Customer/Operator Name: 

Helicopter Serial Number: 

Pushrod Part Number: 

Pushrod Serial Number: 

Was safety cable installed correctly? _______Yes _______No 

Were locking device serrations properly engaged? _______Yes _______No 

Was locking device key properly engaged? _______Yes _______No 

Did adjustable ends of pushrod have proper thread engagement?_______Yes_______No 

Was jamnut properly torqued?_______Yes _______No 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
S-92 ALERT ASB 92-67-006 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

COMPONENT LOCATION 

FIGURE 1 (SHEET 1 OF 2) 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

COMPONENT LOCATION 

FIGURE 1 (SHEET 2) 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
S-92 ALERT ASB 92-67-006A 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

RIGHT HAND THREAD SAFETY CABLE ROUTING 

FIGURE 2 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

LEFT HAND THREAD SAFETY CABLE ROUTING 

FIGURE 3 

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S-92 ALERT ASB 92-67-006A 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

LOCKING DEVICE INSTALLATION 

FIGURE 4 

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Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 

L. Record of compliance: 

(1) Make helicopter logbook entries to show compliance with this ASB as follows: 

(a) Make helicopter level logbook entry on form SA7343-15 (Aircraft ASB and CSN 

Release Signoff). 

(b) When ASB modifies a component that can be removed from this helicopter: 

1. Make component log card entries on forms SA7343-22 (Aircraft Component 

Log Cards) and SA7343-21 (Component Log Cards), as applicable. 

2. If a component modified by this ASB does not have a log card and the ASB 

does not create one, then annotate compliance on the next higher assembly 

that the component belongs to which does have a log card. 

NOTE: If access to www.Sikorsky360.com is unavailable, complete attached ALERT 

SERVICE BULLETIN COMPLIANCE RECORD CARD and return it to Sikorsky 

Aircraft Corporation. 

(2) Make an appropriate electronic compliance entry in the E-Notification section at 

www.Sikorsky360.com. Refer to User Guide located on the www.Sikorsky360.com/ENotification Search page. 

This document contains technical data subject to EAR. See WARNING and classifications on first page.
(Fold over and tape closed)

SIKORSKY AIRCRAFT CORPORATION

FACSIMILE NUMBER (860) 998-7565 

EMAIL ADDRESS: GPSIKSASProductSafet@utc.com

ATTENTION: PRODUCT SAFETY MANAGER

SIKORSKY AIRCRAFT CORPORATION

(Fold Up to Arrows)

IMPORTANT NOTICE

Upon COMPLIANCE with the attached ASB, Sikorsky requests your cooperation 

in completing and returning this ENTIRE PAGE by MAIL, FAX, or scan & 

EMAIL.

Please fill in the requested information at the bottom of the page, so we may maintain 

proper records documenting the configuration of your aircraft. This information is useful 

when determining configuration and effectivity of issues affecting fielded aircraft. 

This request is in keeping with our policy to assure that our customers receive the latest 

information applicable for the maintenance of your aircraft. Thank you. 

ALERT SERVICE BULLETIN: ________________ Compliance Record Card

TITLE: ___________________________________________________________________ 

 ___________________________________________________________________ 

 ___________________________________________________________________ 

OWNER/OPERATOR: _____________________________________________________ 

SUBMITTED BY: ___________________________ DATE: ____________________ 

FOLLOWING SERIAL NUMBERS ARE NOT AFFECTED BY THIS ASB

ASB HAS BEEN COMPLIED WITH ON HELICOPTER SERIAL NUMBERS: 

 ___________ ___________ ___________ ___________ ___________ ___________ 

 ___________ ___________ ___________ ___________ ___________ ___________ 

No. 92-67-006A

FLIGHT CONTROLS – Pushrods – One-Time Inspection of Main Rotor and Tail 

Rotor Servo Pushrods

This document contains technical data subject to EAR. See WARNING and classifications on first page.
No Postage 

Necessary

BUSINESS REPLY MAIL

FIRST-CLASS MAIL PERMIT NO. 432 BRIDGEPORT CT

POSTAGE WILL BE PAID BY ADDRESSEE

SIKORSKY AIRCRAFT CORPORATION

Commercial Systems and Services

Mailstop K100

124 QUARRY ROAD

TRUMBULL, CT 06611 U.S.A. 

ATTENTION: PRODUCT SAFETY MANAGER

SIKORSKY AIRCRAFT CORPORATION

Please complete the form on the reverse side and FAX to

FACSIMILE NUMBER (860) 998-7565 

Or scan and email to:

EMAIL ADDRESS: GPSIKSASProductSafet@utc.com 

or fold and return ENTIRE form to Sikorsky Aircraft Corporation

This document contains technical data subject to EAR. See WARNING and classifications on first page.