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File: 970107_sep96_decls5_0008.txt
Subject: SAFETY AAR OPERATION DESERT SHEILD STORM 17 JUL 91
Unit: 2D ACR
Parent Organization: VII CORPS
Box ID: BX001703
Folder Title: ODS SAFETY AAR
Document Number: 1
Folder Seq #: 43
AETSAC-4SQDN-ASO
SUBJECT: Safety AAF Des
ert Shield/Stor.-n
.-L-.--bnvironment ifid in sorie' cases; near continuoiis'- -:or)era+-:io
equ3.p-.ient required more maintenance than in peacetime operations.
@1) High G@oss Weight Flight. Power limitations of the All-
IF made the aircraft unsuitable for high gross weight operations
from/-@o unimproved areas. AH-LF crashes 7 and 16 February
occurred when maximum available power was applied and the
aircraft settled into the ground from 15 to 30 feet AGL.
Maneuverability was also severely degraded as gross weight
increased. OH-58 aircraft, oar"-icularly ATAS equinped were also
loss maneuverable w;th hi@-er gross weight. The seasonal
increase in amb4-ent temperature was also raoid'--y degrading
aircraft performance a-, high gross weight.
(2) US-60 Passenger Seats. Aaaroved seating was not
available for all Passengers. This @oblem was aggravated by
ground unit changes in the nu.-,iber of passengers to be flown.
Availability of the seat assemblies was also low because -they had
been removed -for antiquated cargo onera-li-ons.
(3) New Equi-p.-,ion@, & Modification Work Orders (MWO). The
't I
un. received several new aircraft survivability systems during
--fhis phase of operations. Adequate tra2'.n2'.ng was provided by
fielding teams for these aircraft components. AF-IF aircraft
were modified by installation of improved particle separator
(IPS) to reduce engine sand ingestion. Limited and conflicting
Most unit CUCV
trucks were turned in for HUMVEEs in January 1991. Driver
training on these vehicles was very lim4-ted prior -lo issue.
(4) Aircraft Engines. Sand ingestion rapidly deteriorated
performance of A.9-lF aircraft engines. Ton unit All-! aircraft
experienced compressor stall during this ohase of operations.
Two engine failures also occurred. IiS modified aircraft
was involved in one of the compressor stalls. AFL-1 operating
times in a dese.-t environment before comoressor stall ranged from
11 to 44 flight hours.
C. Environiental Factors. Rotor induced blowing sand caused
loss of ground reference during many -@ake offs and landings.
Blowing sand couoled with high gross weight operations left
little margin for aircrew error. Sand also erroded rotor blades
and other aircraft cor,.monen"@s. Other environmental factors
included;
(1) Temperature. Slowly rising ambient temperature affected
both human and equipmen, performance. Adjust.,ient of work
schedule and compensation 'or degraded aircraft Performance were
advisable late in the operation.
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Document 12 f:/Week-48/BX001703/ODS SAFETY AAR/safety aar operation desert sheild storm 17 jul :01029718421510
Control Fields 17
File Room = sep96_declassified
File Cabinet = Week-48
Box ID = BX001703
Unit = 2D ACR
Parent Organization = VII CORPS
Folder Title = ODS SAFETY AAR
Folder Seq # = 43
Subject = SAFETY AAR OPERATION DESERT SHEILD STORM 17 JUL
Document Seq # = 1
Document Date =
Scan Date =
Queued for Declassification = 01-JAN-1980
Short Term Referral = 01-JAN-1980
Long Term Referral = 01-JAN-1980
Permanent Referral = 01-JAN-1980
Non-Health Related Document = 01-JAN-1980
Declassified = 02-JAN-1997