Aviation Safety Action Message

CH-47-05-01

 

         
Aft Critical Dynamic Components

 

             CH-47-04-ASAM-02 was issued on 29 April 04 to advise flight crews on the operational limits of the Cruise Guide Indicator (CGI), to remark the CH-47D CGI and to require the inspection of the instrumented aft fixed link. This ASAM provides additional inspections and corrective action.

 

	
UNCLASSIFIED
.
MSG DTG 141414Z OCT 04
.
FROM CDRAMCOM, REDSTONE ARSENAL, AL  //AMSAM-SF-A//  
.
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE
MANDATORY, RCS CSGLD-1860(R1), CH-47 AIRCRAFT, AFT CRITICAL
DYNAMIC COMPONENTS, CH-47-05-ASAM-01. 
....
                   NOTE                   
....This message is effective until rescinded or superseded.  
....
                   NOTE                   
....This message is issued IAW AR 95-1 and has not been 
....transmitted to units subordinate to addressees.  
....Addressees will immediately retransmit this message 
....to all subordinate units, activities or elements 
....affected or concerned.  MACOMs will immediately 
....verify this transmission to the AMCOM SOF Compliance 
....Officer (AMSAM-SF-A, safeadm@redstone.army.mil).  
....
                   NOTE                   
....MACOM commanders may authorize temporary exception from 
....message requirements IAW AR 95-1, Ch 6.  Exception may 
....only occur when combat operations or matter of life or 
....death in civil disasters or other emergencies are so 
....urgent that they override the consequences of continued 
....aircraft operation.  
....
1.  SUMMARY - 
1.1.  Background - 
1.1.1. CH-47-04-ASAM-02 was issued on 29 April 04 to advise 
flight crews on the operational limits of the Cruise Guide 
Indicator (CGI), to remark the CH-47D CGI and to require the 
inspection of the instrumented aft fixed link.  This ASAM 
provides additional inspections and corrective action.  
1.1.2.  Following combat operation of CH-47D aircraft in Iraq 
and in the mountains of Afghanistan, pilots reported that 
continuous flight operations were conducted with the cruise 
guide indicator (CGI) in the transient region, accompanied by 
excursions into the avoid region, usually encountered in 
turbulence.
1.1.3.  The CGI instrument provides a visual indication of loads 
incurred on critical dynamic components in flight.  It is 
divided into three bands; normal (green band), transient (yellow 
band), and avoid (red/yellow striped band).  Numerous 
operations, were reportedly conducted on specific aircraft at 
high gross weights, extreme aft center of gravity conditions, 
high torques, airspeeds exceeding VH, and at high density 
altitudes.  The impact of operation in the upper regions of the 
yellow (transient) band and any area in the red/yellow (avoid) 
band of the CGI resulted in a significant decrease in the 
available fatigue life for critical safety items on the rotor 
controls and drive components.  The reductions in available 
fatigue lives are dependent upon component loads, aircraft 
loads, and the amount of time spent under these conditions. 
1.2.  MESSAGE PURPOSE - Require mandatory parts replacement on 
affected aircraft within specified aircraft hours and ensure 
affected parts previously turned in for maintenance/overhaul are 
captured for de-militarization.
2.  END ITEMS AFFECTED - All CH-47D and F series aircraft.
3.  ASSEMBLIES/COMPONENTS/PARTS AFFECTED - 
3.1.  Suspect/discrepant assemblies/components/parts - 
..Nomenclature                 PN                NSN
  Aft Rotary Wing Head       145R2004-18    1615-01-315-3972
                             145R2004-20    1615-01-391-4399
..Aft Rotor Shaft            145D3300-3     1680-01-119-3361
                             145D3300-5     1680-01-307-4844
                             145D3300-6     1680-01-320-1191
..Pitch Housing              234R2075-2     1615-01-335-2697
                             145R2075-12    3040-01-115-3608
                             145R2075-14    3040-01-307-8964
                             145R2075-16    3040-01-407-7298
3.2.  Additional assemblies/components/parts to be inspected - 
..Aft Fixed Link Assembly    414C3056-3     1615-01-117-1135
..Aft Pitch Link Upper Bolt  114R3650-13    5306-00-003-1152
                             114R3650-16    5306-01-301-7793
..Aft Pitch Link Lower Bolt  114R3650-15    5306-00-003-1149
                             114R3650-17    5306-01-301-7794
  Aft Trim Actuator, Plain Rod End Bearing
                             114CS123-1     3120-00-110-8542
..Aft Pivoting Actuator to Support Fitting Bolt
                             BACB30ST8-31   5306-00-008-5025
..Aft Pivoting Actuator to Support Fitting Bolt
                             BACB30ST8-35   5306-00-008-5027
..Aft Fixed Link to Stationary Swashplate Bolt
                             114R3650-7     1615-00-003-1156
....
                   NOTE                   
....When complying with the requirements of this message, 
....complete forms and records entries IAW DA PAM 738-751.  
....ULLS-A units will use appropriate "E" forms.
....
4.  INITIAL TAMMS (THE ARMY MAINTENANCE MANAGEMENT SYSTEM) 
COMPLIANCE REQUIREMENTS - 
4.1.  Upon receipt of this message make the following entry on 
the DA Form 2408-13-1:  Enter a Red Horizontal Dash //-// status 
symbol with the following statement: "Comply with requirements 
of CH-47-05-ASAM-01 before [####.#] aircraft hours, but NLT 29 
October 2004."  Calculate [####.#] as current aircraft flight 
hours plus 10 hours.  Commanders who are unable to comply with 
the requirements of this message within the time frame specified 
will upgrade the affected aircraft status symbol to a Red //X//.
                   NOTE                   
....The TAMMS compliance reporting form is available at 
...."www.redstone.army.mil/sof/tamms.xls" (use lower case 
....letters only) or may be obtained from the units 
....servicing LAR.  Alternate forms may be approved by 
....the AMCOM SOF Compliance Officer.  
....
                   NOTE                   
....The TAMMS Compliance Report only confirms the unit has 
....made the initial logbook entry for assigned aircraft.  
....TAMMS Compliance Reports will include aircraft serial 
....numbers (in numerical order), date of entry on DA Form 
....2408-13-1, unit address, local POC name and phone number.
....
4.2.  TAMMS Compliance Report - Submit TAMMS compliance report 
via priority email to "safeadm@redstone.army.mil" 21 October 
2004 IAW AR 95-1.  If email is not available, the report may be 
faxed to:  SOF Compliance Officer at DSN 897-2111 or (256) 313-
2111.
5.  TASK/INSPECTION COMPLIANCE REPORTING REQUIREMENTS - 
...................NOTE...................
....The Task/Inspection Reporting Form is available at 
...."www.redstone.army.mil/sof/log.xls" (use lower case 
....letters only) or may be obtained from the units 
....servicing LAR.  This report will cite the message 
....number, date of inspection, aircraft serial number, 
....aircraft hours, component serial number, component 
....hours, and results of the inspection.  
5.1.  Aircraft - 
5.1.1. Submit Initial Task/Inspection Report for this message to 
Log POC NLT 1 November 2004.  
5.1.2. Submit Task Compliance Reports for this message to Log POC 
in Para 13 no later than 15 calendar days from completion of 
each part replacement on an aircraft.
5.2.  Retail Stock (Installation level and below) - Provide unit 
POC, address and phone number.  Submit Task/Inspection 
Compliance Report for this message to Log POC NLT 1 November 
2004.  
5.3.  Wholesale Stock (Including Depot stock, Depot Maintenance 
and Single Stock Fund) - Report compliance with this message IAW 
para 8 to Wholesale POC NLT 1 November 2004.
6.  SPECIAL PROVISIONS TO MESSAGE REQUIREMENTS (AIRCRAFT) - 
6.1.  Aircraft in AVIM, Or Depot Level Maintenance - Commanders, 
Facility Managers and Contractors will not issue aircraft until 
they are in compliance with this message.
6.2.  Aircraft at Contractor Facility - Contractor facilities 
will inspect CH-47D aircraft prior to CH-47 F Modification and 
ensure that aircraft have no suspect parts IAW CH-47-05-ASAM-01 
installed prior to DD 250 and will inspect DD 250 aircraft prior 
to those aircraft departing for ferry to final destination.  
6.3.  Aircraft In Transit - Unit commanders in receipt of 
deployment orders and are unable to comply prior to the date 
specified in para 4.1. may defer initial requirements IAW 
Surface/air shipment or Ferry status instructions, as 
appropriate.  
6.3.1.  Surface/Air Shipment - Comply with message requirements   
within 10 flight hours / 14 days of arrival. 
6.3.2.  Ferry Status/Aircraft Away From Home Station - Comply 
with message requirements upon arrival at final destination.   
6.4.  Aircraft on Red //X// Status Symbol may be maintained in 
flyable storage.  Ground run-ups at normal operating rotor rpm 
are authorized.
7.  TECHNICAL PROCEDURES/INSTRUCTIONS - 
7.1.  Inspect all CH-47D/F aircraft to determine if the 
following suspect parts are installed.  
....
...................NOTE...................
....Aircraft may have affected assemblies/components/parts
....that may have been obtained through controlled exchange
....or the supply system and installed on any aircraft
....in the field.
....
7.1.1.  Suspect Aft Rotary Wing Head (PNs 145R2004-18 and -20) 
with the following Serial Numbers - 
...A5-34     A5-56     A5-70     A5-79     A5-178    A5-295
...A5-362    A5-403    A5-404    A5-405    A5-464    A5-479
...A5-668    A5-748    A5-769    A5-834    A5-906    A5-971
...A5-1043   A5-1052   A5-1064   A5-1088   A5-1100   A5-1124
...A5-1129   A5-1154   A5-1203   A5-1237   A5-1258   A5-1415
...A5-1548
7.1.2.  Suspect Pitch Housing (PNs 234R2075-2, 145R2075-12,-14 
and -16) with the following Serial Numbers - 
...AM144   AM262   AM290   AM446   AM458   AM480   AM524
...AM582   AM666   AM670   AM724   AM752   AM832   AM840
...AM852   AM868   AM914   AM1052  AM1060  AM1080  AM1110
...AM1124  AM1132  AM1178  AM1218  AM1222  AM1228  AM1260
...AM1262  AM1266  AM1286  AM1320  AM1368  AM1470  AM1516
...AM1564  AM1638  AM1646  AM1654  AM1672  AM1710  AM1764
...AM1814  AM2002  AM3214  AM4711  TM277   TM313   TM322
...TM325   TM327   TM336   TM358   TM380   TM467   TM473
...TM492   TM513   TM660   TM667   TM676   TZ103   TZ122
...TZ222   TZ276   TZ296   TZ298   TZ336   TZ600   TZ688
...TZ778   TZ866   TZ952   TZ1002  TZ1120  TZ1138  TZ1212
...TZ1388  TZ1678  TZ1696  TZ1712  TZ1992  TZ2052  TZ2384
...TZ2414  TZ2754  TZ2758  TZ2762  TZ2830  UW3228  UW3387
...UW3905  UW4087  UW4318  UW4489  UW4491  UW4492  UW4576
...UW4581  UW4602  UW4644  UW4658  UW4659  UW4678  UW4710
...UW4757  UW4810  UW4815  UW4856  UW4869  UW5013  UW5051
...UW5081  UW5134  UW5135  UW5359  VM4157.
7.1.3.  Suspect Aft Rotor Shaft PNs 145D3300-3, -5, -6) with the 
following Serial Numbers - 
...A-117   A-124   A-139   A-148   A-149   A-169   A-182
...A-188   A-198   A-222   A-226   A-257   A-261   A-268
...A-367   A-412   A-433   A-438   A-441   A-448   A-471
...A-475   A-482   A-483   A-505   A-523   A-576   A-635
...A-654   A-680   A-727   A-733   A-947   A-996   A-997.
7.1.4.  If any suspect serial numbered parts are installed, 
replace as applicable, within 400 aircraft hours (not to exceed 
Maximum Allowable Operating Time [MAOT]) but NLT 31 Oct 06.  
Make appropriate logbook entry as required in para 7.7.  Proceed 
to para 7.2.
7.1.5.  If no suspect serial numbered parts are found, proceed 
to next paragraph.
....
...................NOTE...................
.....Procedures in this message specify the use of
.....hazardous chemicals, ensure safe handling procedures
.....and appropriate manual references are consulted.
.....Refer to Material Safety Data Sheets (MSDS) for the
.....items being used.
....
7.2.  The following serial numbered aircraft require replacement 
of additional suspect parts.  The suspect aircraft are 
identified by 2 groups (A/B).  
7.2.1.  Group A Aircraft are identified as: 
...8324124   8424154   8424157   8424158   8424175   8424187
...8524326   8524331   8524333   8524334   8524336   8524343
...8524345   8524348   8524349   8601666   8601669   8700082
...8700083   8700091   8700096   8900130   8900135   8900147 
...9200368.
7.2.2.  Group B Aircraft are identified as - 
...8424165   8424167   8424168   8424184   8424186   8524330
   8601649   8601677.
7.3.  Conduct records review to determine if the parts listed in 
para 7.4. and 7.5. were installed since 1 Feb 2004.
7.3.1.  If records review confirms the part was replaced with a 
new part since 1 Feb 2004, contact the Log POC listed in para 13 
to determine if the part requires replacement.
7.3.2.  If the records review shows the part has not been 
replaced since 1 Feb 04, the parts will be replaced IAW 
paragraphs 7.4. and/or 7.5. as applicable.
7.4.  Group A and B aircraft will replace the following parts 
within 400 aircraft hours (not to exceed MAOT) but NLT 31 Oct 
06.  Make appropriate logbook entry as required in para 7.7.  
..Nomenclature                 PN                NSN
..Aft Fixed Link Assembly    414C3056-3     1615-01-117-1135
..Aft Pitch Link Upper Bolt  114R3650-13    5306-00-003-1152
                             114R3650-16    5306-01-301-7793
..Aft Pitch Link Lower Bolt  114R3650-15    5306-00-003-1149
                             114R3650-17    5306-01-301-7794
  Aft Trim Actuator, Plain Rod End Bearing
                             114CS123-1     3120-00-110-8542
7.5.  Group B aircraft will replace the parts listed in 
para 7.4. above PLUS the following parts.  Replacement will be 
within 400 aircraft hours (not to exceed MAOT) but NLT 31 Oct 
06.  Make appropriate logbook entry as required in para 7.7.
..Nomenclature                 PN                 NSN
..Aft Pivoting Actuator to Support Fitting Bolt
                             BACB30ST8-31   5306-00-008-5025
..Aft Pivoting Actuator to Support Fitting Bolt
                             BACB30ST8-35   5306-00-008-5027
..Aft Fixed Link to Stationary Swashplate Bolt
                             114R3650-7     1615-00-003-1156
7.6.  If no suspect parts are identified, the inspection is 
complete.  Proceed to para 7.9.
7.7.  If a suspect part is installed, make appropriate entry for 
each suspect part on the DA Form 2408-13-1.  Enter a Red 
Horizontal Dash //-// status symbol with the following 
statement: "Replace (Nomenclature/SN) IAW CH-47-05-ASAM-01 
before [####.#] aircraft hours, but NLT 31 Oct 06."  Calculate 
[####.#] as current aircraft flight hours plus 400 hours, or 
MAOT, whichever comes first.  Report documentation of each 
assembly/component/part replacement to the Log POC IAW Para 
5.1.2.
7.8.  All assemblies/components/parts removed from aircraft IAW 
this message shall be disposed of IAW Para 10.7.
7.9.  Clear the initial entry from Para 4.1 and note compliance 
on DA Form 2408-5-1 (Component) or DA Form 2408-15.
8.  PROCEDURES/INSTRUCTIONS FOR ASSEMBLIES/COMPONENTS/PARTS IN 
WORK OR IN STOCK (AT ALL LEVELS INCLUDING WAR RESERVES) - All 
facilities will inspect in work and in stock items for presence 
of serial numbered components listed in Para 7.  If these 
serialized items are discovered, they are to be removed from 
service, reported to the Log POC in Para 13, and dispositioned 
IAW Para 10.7.  
8.1.  Items in Retail Stock - Commanders and facility managers 
that maintain retail stock at installation level and below will 
submit a Task/Inspection report to Log POC IAW para 5.  
8.2.  Items in Single Stock Fund and in Work (Overhaul/Repair 
Facility) - Commanders and facility managers will submit 
Task/Inspection Compliance Report to Wholesale POC IAW para 5.  
8.3.  Items in Wholesale Stock - Depot storage facilities will 
Inspect for suspect serial numbers IAW para 7.1. and submit 
Task/Inspection Compliance Report to Wholesale POC IAW para 5.
9.  SPECIAL TOOLS AND FIXTURES REQUIRED - N/A.
10.  SUPPLY/PARTS (REQUISITION/DISPOSITION) - 
10.1.  Parts required to replace serial numbered parts -
..Nomenclature     PN / NSN       Qty      Cost Ea.    Total $
..Pitch Housing                   3 ea     $5825.00   $17,475.00
          145R2075-16 / 3040-01-407-7298 
or
  Aft Rotor Head                  1 ea  $276,623.00  $276,623.00
          145R2004-20 / 1615-01-391-4399
..Aft Rotor Shaft                 1 ea  $111,007.00  $111,007.00
          145D3300-3 / 1680-01-119-3361
          145D3300-5 / 1680-01-307-4844
          145D3300-6 / 1680-01-320-1191
10.2.  Parts Required for Group A and B Aircraft - 
..Nomenclature     PN / NSN       Qty      Cost Ea.    Total $
  Aft Fixed Link                  1 ea    $6,312.00    $6,312.00
          414C3056-3 / 1615-01-117-1135
..Aft Pitch Link Upper Bolt       3 ea       $382.18    $1146.54
          114R3650-13 / 5306-00-003-1152
          114R3650-16 / 5306-01-301-7793
..Aft Pitch Link Lower Bolt       3 ea      $373.42     $1120.26
          114R3650-15 / 5306-00-003-1149
          114R3650-17 / 5306-01-301-7794
  Aft Trim Act Plain Rod End Brg  1 ea     $194.00       $194.00
          114CS123-1 / 3120-00-110-8542
10.3.  Additional Parts Required for Group B aircraft - 
..Nomenclature     PN / NSN       Qty      Cost Ea.    Total $
..Aft Pvtg Actr to Spt Ftg Bolt   2 ea       $36.58       $73.16
          BACB30ST8-31 / 5306-00-008-5025
  Aft Pvtg Actr to Spt Ftg Bolt   1 ea       $61.45       $61.45
          BACB30ST8-35 / 5306-00-008-5027
..Aft Fxd Lnk to Sta Swshplt Bolt 1 ea      $119.59      $119.59
          114R3650-7 / 1615-00-003-1156
10.4.  Total cost per aircraft - 
..Total Cost if all parts are replaced - $395,109.22
..*Total cost per aircraft will vary dependent upon number of 
..parts requiring replacement.
10.5.  Bulk and consumable materials - 
..Nomenclature                   PN              NSN
..Sealing Compound            730RTV         8030-00-251-2312
..Assembly Fluid,             AFS TURBO 10   9150-00-159-5012
..Lockwire                    MS20995NC20    9525-00-618-0257
..Lockwire                    MS20995N32     9525-00-355-6072
..Lockwire                    MS20994N40     9525-00-990-7799 
..Oil, Lubricating            MIL-PRF-7808   9150-00-782-2627
..Cloths                      A-A-2522       7920-00-205-1711
..Methyl-Ethyl-Ketone         ASTM D 740     6810-00-281-2785
..Primer, No.                 1200 RTV       8040-00-845-4304
..Sealing Compound            ASTM D5363     8030-01-055-6126
..Primer, Grade T             MIL S-473          NA.
..Adhesive,                   MMM-A-132      8040-00-200-4390
..Solvent                     MIL-PRF-680    6850-01-474-2309
                                             6850-01-474-2302
..Adhesive,                   RTV730         8040-00-867-5804
..Grease                      MIL-PRF-81322  9150-00-944-8953
..Antisieze Compound,         MIL-PRF-83483  8030-00-087-8630
..Naphtha                     TT-N-95        6810-00-238-8117
..Epoxy Primer                MIL-P-85582    8010-01-218-0856
..Oil, Lubricating, Helicopter DOD-L-85734   9150-01-209-2684
..Barrier Material, Water Proof MIL-PRF-131  8135-00-282-0565
..Tape Masking                L-T-100        7510-00-721-9756
..Cloth, Cleaning             CCC-C-46A       8305-00-753-2967
..Dry Cleaning Solvent        P-D-680         6850-00-285-8011
..Gloves, Chemical and Oil Prot MIL-G-87066     8415-01-147-6263
 .Gloves, Kevlar              MIL-M-11199     8415-01-092-0039
..Gloves, Anticontact         MIL-G-10902      8415-00-227-1220 
10.6.  Requisitioning instructions - 
10.6.1  Requisition replacement parts using normal supply 
procedures.  Aft Rotor Head Pitch Housings will be supplemental 
addressed to your servicing OLR.  Rotor Heads will be removed 
before suspense and provided to OLR for Pitch Housing 
replacement.  All requisitions shall use Project Code (CC 57-59) 
"X2W" (X-Ray-02-Whiskey).
                              NOTE                        
....Project Code "X2W" is required to track and establish 
....a data base of stock fund expenditures incurred by 
....the field as a result of message actions.  
10.7.  Disposition of discrepant parts/components - Unit will 
submit the serial number of the part and aircraft serial number 
to the Log POC in para 13.2.  All component/parts removed, other 
than Aft Vertical Shaft with Part Number 145D3300-6 and Aft 
Rotor Pitch Housings with Part Number 145R2075-16, shall be 
demilitarized IAW TM 1-1500-328-23 and disposed of using normal 
procedures to DRMO.  Aft Vertical Shafts and Aft Rotor Pitch 
Housing shall be red tagged as Condemned and shipped to the OLR 
San Angelo, Texas POC in para 13.7 for storage.  OLR San Angelo, 
Texas will record serial numbers, notify the Log POC in Para 13 
of serial numbers received on a monthly basis, store the 
received parts, and await additional instructions from the Log 
POC.
10.8.  Disposition of hazardous material - IAW Environmental 
Protection Agency directives as implemented by your servicing 
environmental coordinator (AR 200-1). 
11.  MAINTENANCE APPLICATION - 
11.1.  Categories of maintenance - AVUM and Depot.
11.2.  Estimated time required - 
11.2.1.  Time to complete inspection - total of 2 man-hours 
using 1 person with 0 hours downtime per end item.
....
                   NOTE                   
....The time stated below does not include time for 
....Maintenance Operational Checks, Maintenance Test 
....Flights, or Flight Crew briefings.
....
11.2.2.  Time to complete each part replacement - 
..1 Aft Fixed Link Assembly -      3 hours X 3 men = 9 man hours
..1 Aft Rotor Head -             16 hours X 3 men = 48 man hours
..1 Aft Rotor Shaft -             6 hours X 3 men = 18 man hours
..3 Aft Pitch Link Upper Bolt -      1 hour X 1 man = 1 man hour
..3 Aft Pitch Link Lower Bolt -      1 hour X 1 man = 1 man hour
  1 Aft Trim Act Plain Rod End Brg - 1 hour X 1 man = 1 man hour
..3 Aft Pvtg Actr to Spt Ftg Bolt - 1 hour X 1 man = 1 man hour
..1 Aft Fxd Lnk to Sta Swshp Bolt - 1 hour X 1 man = 1 man hour
11.2.3.  Maximum Time required if all parts are replaced - 
                                           80 hours per end item
12.  PUBLICATION REQUIREMENTS - 
12.1.  References - 
12.1.1.  AR 95-1.
12.1.2.  AR 200-1.
12.1.3.  DA Pam 738-751.
12.1.4.  TM 55-1520-240-23 and 23P.
12.1.5.  DMWR 55-1615-296.
12.1.6.  TM 1-1500-328-23 /DOD 4160.21-M-1.  
12.2.  Publication Changes - N/A.
13.  POINTS OF CONTACT - 
13.1.  Technical POCs are - 
13.1.1.  Primary - Mr. Neil Sutherland, AMSRD-AMR-AE-C, DSN 645-
0696 Or (256) 955-0696, Fax is (256) 313-4726.  
E-Mail is "neil.sutherland@peoavn.redstone.army.mil".
13.1.2.  Alternate - Mr. Tim Rickmeyer, AMSRD-AMR-AE-C, DSN 897-
8040, or (256) 313-8040.  Fax is 256-313-4726.  
Email is "timothy.rickmeyer@peoavn.redstone.army.mil".
13.2.  Logistical POCs are - 
13.2.1.  Primary - Mr. Bill Olson, SFAE-AV-CH-CS, DSN 897-0721 
or (256) 313-0721.  Fax is 897-4726 or (256) 313-4726.  
Email is "william.olson@peoavn.redstone.army.mil".
13.2.2.  Alternate - Mr. Norm Huston, SFAE-AV-CH-CS, DSN 897-
0752 or (256) 313-0752.  Fax is 897-4348 or (256) 313-4348.  
Email is "norm.huston@peoavn.redstone.army.mil".
13.3.  Wholesale Materiel POCs are -
13.3.1.  Primary - Mr. Phil Batey, AMSAM-MMC-AV-CA, DSN 897-3369 
or (256) 313-3369.  Fax is DSN 897-4726.  Email is 
"phillip.batey@us.army.mil".
13.3.2.  Alternate - Mr. Alan McCandless, AMSAM-MMC-AV-CA, DSN 
645-6706 or (256) 955-6706.  Fax is DSN 897-4726.  Email is 
"alanmccandless@us.army.mil".
13.4.  Forms and Records POC is Ms. Ann Waldeck, AMSAM-MMC-MA-
NM, DSN 746-5564 or (256) 876-5564.  Fax is DSN 746-4904 or 
(256) 876-4904.  Email is "ann.waldeck@redstone.army.mil".  
13.5.  Safety POCs are - 
13.5.1.  Primary - Mr. Frank Rosebery (SAIC), AMSAM-SF-A, DSN 
788-8631 or (256) 842-8631.  Fax is DSN 897-2111 or (256) 313-
2111.  Email is "frank.rosebery@redstone.army.mil".
13.5.2.  Alternate - Mr. Russell Peusch, AMSAM-SF-A, DSN 788-
8631 or (256) 842-8632.  Fax is DSN 897-2111 or (256) 313-2111.  
Email is "russell.peusch@redstone.army.mil".
13.6.  Foreign Military Sales POC is Mr. Ronnie W. Sammons, 
AMSAM-SA-AS-UT, DSN 897-0875 or (256) 313-0875.  Fax is DSN 897-
0411 or (256) 313-0411.  Email is 
"ronnie.sammons@redstone.army.mil".
13.7.  AMCOM Project OLR POC is Mr. Matthew Clark, Building 8154 
Hangar Road, San Angelo, Texas 76904, (325) 944-9491.
13.8.  After hours, contact the AMCOM Operations Center (AOC) 
DSN 897-2066/7 or (256) 313-2066/7.
....
                   NOTE                   
....A listing of published safety messages can be viewed at
...."https://ams14.redstone.army.mil/safety/sof/index.html".
....This is a secured website which requires an Army Knowledge
....Online (AKO) ("www.us.army.mil") ID and password.
....