Gulf War Air Power Survey



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Before the Gulf War, increased demands on the C-141 fleet (primarily low-level flying and increased heavy-weight refueling) ac­celer­ated structur­al damage to the aircraft, with a corresponding reduc­tion in service life.690 The severity of the problem led the Military Airlift Com­mand Council to conclude in May of 1990 that maintaining a viable fleet would not be possible beyond the turn of the century.691 Naturally, the increased flying tempo during the Gulf War held the possibility of exac­erbating the prob­lem. To minimize impact, Hq MAC and 21st Air Divi­sion both put zero fuel weight and gross takeoff weight limitations on the aircraft.692 The impact of these decisions (although the precise trail of logic is not recover­able) was to restrict C-141 loads to twenty short tons.693 The Command later estimated that this restriction reduced C-141 airlift capabil­ity by six to ten percent.694 Although the Gulf War resulted in about three years worth of flying hours during a one-year period, the effect on the C-141 fleet was to shorten fatigue life by about one year. The reason for the moderate impact was reduced exposure during the Gulf War to stressful flight profiles such as air refueling, air drop, and low-level flying.695
Industrial Maintenance
Air Force Logistics Command and its contractors participated in the Gulf War primarily by (1) increasing production of repair parts, (2) accel­erating the output of aircraft from program depot maintenance lines, and (3) fielding combat logistics support squadrons. The first of these is called repairable surging.
The normal peacetime production rate of repairable (sometimes called “exchangeable”) items is 60,000 per month.696 “Repairable surg­ing” is increasing the rate at which Air Force Logistics Command “turns around” repairable items such as avionics line replaceable units and aircraft engines. An item was considered surged if it was either already undergoing repair and turned out faster than normal or entered earlier than normal into the repair process (and then repaired). Overall Logistics Command surge performance is depicted in Figure 68. As can be seen from the figure, the surge production (i.e., production over and above normal) rate was approxi­mately 6,700 per month from late August through mid-January and then climbed to 18,000 per month after mid-January.697 Note that production was linear in the two periods before and after mid-January and fairly independent of the requirement. Throughout the January, February, and March periods, production trailed demand by about 10,000 components. It is not certain why this was so, but a reason­able conjecture based on after-action reporting is lack of carcasses to repairthe same problem the Air Force Queen Bee engine shops in Eu­rope experienced.698 Overtime rates varied widely, with some units reporting rates as low as seven percent and others as high as eighty percent.699

Figure 68

Surge Requirements and Production (Cumulative)

36


Quantity produced is one consideration; a second is: were the right things being produced? To quote from two after action reports from the same Air Logistics Center (ALC):
This [Command and Control Information] system was used to electroni­cally transmit surge requirements to the Avionics Surge Center. The electronic data interface greatly speeded the surge notification process.700
Each ALC has their own rules on how to compute surge candidates. MAJCOMs and ALCs need to agree on how to identify surge candidates and how requirements will be computed. The local CCIS was complete­ly ineffective in identifying quantities and tracking.701
The implication is that although requirements identification was fast, it was not necessarily accurate. The view that surge requirement identifi­cation and tracking was problematic is corroborated in other after-action reporting.702 However, it is also apparent that by the phase II deployment (mid-September 1990), much of the initial confusion had died down as customers (e.g., Air Force Special Operations Command, Tacti­cal Air Command, Strategic Air Command, and Military Airlift Com­mand scrubbed the initial lists generated by the Weapon System Manage­ment Information System and switched to using reports of actual War Readi­ness Spares Kit shortages and mission capability limiting items.703
Finally, confusion existed over how surge was to be implemented and the purpose of Air Force Logistics Command's Surge Contingency Plan 70. The plan, as viewed by Logistics Command Headquarters and as stated in the introduction to the plan, was not intended to be imple­mented but was a guide for writing air logistics center-level plans.704 This intent was consistent with a concept of decentralized decision mak­ing on when and what to surge. But at the level of the air logistics centers, the expectation evidently was that Headquarters would make the decision to surge and that “Plan 70 should be implemented early to ensure consistent implementation across the command.”705 One result of the confusion over who was supposed to decide to surge was an initial delay (of some weeks duration) as each weapon-system program manager “convinced” other ALCs and peer directorates within the same ALC to respond to surge requirements.706
The Air Force referred to production of an aircraft undergoing pro­gram depot maintenance earlier than originally planned as “accelera­tion.” AFLC accelerated approximately seventy aircraft during Desert Shield and Desert Stormsixty-four within AFLC industrial facilities and another six that were undergoing program depot maintenance at contrac­tor facili­ties.707 Of the seventy aircraft, four were C-5 aircraft and thirty-five were C-141s.708 The acceleration provided for almost 1,000 addition­al flying days. However, the additional flying days were not fully used.709 For example, Military Airlift Command used approximately one-third of the 174 addi­tional flying days made available on C-141 aircraftthe rest of the addi­tional C-141 flying days were unused. Chapter 3 shows that, except at peak periods, more C-141 mission-capable aircraft were avail­able than required; this should not be a surprise, but it does reinforce the point that industrial maintenance capability exceeded the demands placed on it.
Quantitative Logistics Indicators
One of the impressions apparently created during the Gulf con­flict and then perpetuated afterwards is that Air Force aircraft had mis­sion-capable rates “equal to or better than” peacetime rates. Often, the empha­sis was on “better than.”710,711 The mission-capable rates were generally good, but they were not that good. With the exception of a few aircraft such as C-141swith rates slightly higher in Desert Shield and Desert Storm than in peacetimethe mission-capable rates of all other aircraft appear to have stayed about the same or decreased when com­pared to peacetime rates.712 The text below assesses mission-capable rates, break rates, and fix rates. Mission-capable rate is a composite of many factors and thus inherently integrates the effects of design, policy, spares levels, manning levels, and other influences. The break rate is the number of returning sorties that need repair and is driven mostly by the basic reli­ability of the aircraft. Repair rate is the number of returning aircraft ready to go in a given amount of time (e.g., eight hours) after landing. Although repair rate is a function of inherent maintainability, it also reflects maintenance capability and spares availability. By consider­ing all three rates (fully mission-capable, break, and fix) it is possible to get a feel for the influence of more immediate factors as well as those of longer duration. Air Force mission-capable rates can be compared with those of other Services, since the definition of the term is generally consistent across Services.

Mission-Capable Rates
Because the Core Automated Maintenance System (CAMS) was never fully fielded, reliable mission-capable rates were difficult to obtain during or after the conflict.713 As a workaround, the CENTAF (Rear) battle staff at Langley AFB telephonically obtained once-per-day snapshots as of midnight in Riyadh.714 The snapshot flying data inflated the mission- capable rates by about five percent to seven percent compared to rates that would have been obtained with the automated system. This inflation may be a source of the impression that the mission-capable rates were better than in peacetime.715 Military Airlift Command collected data manually for a different reason. The combination of CAMS and the Reliability and Maintainability Information System (REMIS) assumed that a Military Airlift Command aircraft remained mission-capable from the time it left home station until it returnedthis practice also produced inflated fully mission-capable rates.716 For the C-5, the inflation was as much as ten percent during the Gulf War. Another factor influencing the validity of the comparisons between wartime and peacetime rates is that a month-to-month variability (of say five percentage points or more) occurs normally without obvious cause. Hence, a value of five percent difference in either direction should be viewed skeptically.
The pattern of the F-16's mission-capable rate is typical of Tacti­cal Air Command aircraft. In Figure 69, the upper line is the reported rate and the lower line is the reported rate less six percent (i.e., the aver­age inflation due to snapshot data collection). July was the last month before deployment. From the figure, the reader can decide that deploy­ment initially degraded mission capability. However, most of the bugs were worked out of the system in roughly four months. Table 36 con­trasts the average fully-mission-capable rates before deployment, during Desert Shield, and during Desert Storm for major U.S. Air Force air­craft.
Break Rates and Fix Rates
Why did the mission-capable rates go down in general after deploy­ment? The answer can be seen in break and fix rates.717 Tactical Air Command aircraft all followed a more-or-less common pattern that

­

Figure 69



F-16 FMC Rate


Table 36

Fully Mission-Capable Rates Compared718


Sourcing

Com­mand

Aircraft

FMC Rate

Be­fore

De­ploy­ment

Desert Shield Avg (adj)

Desert Storm

Avg (adj)

TAC

F-15

84.6

73.2

78.8

TAC

F-15E

79.4

84.6

79.9

TAC

F-16

90.7

87.7

80.8

TAC

OA-10

87.5

88.4

87.5

TAC

A-10

88.9

85.0

81.0

TAC

F-4G

83.3

77.7

72.5

TAC

EF-111

75.8

59.5

47.2

TAC

F-117

82.4

79.5

72.5

TAC

RF-4C

79.7

73.7

61.3

TAC

E-3

81.4

79.6

82.2

USAFE

A-10

88.9

n/a

75.6

Table 36 (Continued)

Fully Mission-Capable Rates Compared


Sourcing Command

Aircraft

FMC Rate

Before

Deployment

Desert Shield

Avg (adj)

Desert Storm

Avg (adj)

USAFE

RF-4C

78.8

n/a

77.2

USAFE

F-4G

78.9

n/a

63.6

USAFE

F-16

86.8

n/a

79.1

USAFE

F-15

84.4

n/a

74.6

SAC

B-52G (Diego Garcia)

not available

0.87

0.83

SAC

B-52G (Moron)

not available







SAC

KC-135

not available







SAC

KC-10

not available







MAC

C-141

79.7

83.3

84.4

MAC

C-5

69.8

68.7

67.8

MAC

C-130

81.5

-----

90.1



can be visualized by examining F-15 data (Figure 70). F-15 aircraft deployed to the AOR broke more often than did aircraft at home. It is not hard to understand why. Over and above being in a harsh environ­ment, aircraft in the AOR were flying longer sorties than peacetime training mis­sions. In addition, the rate at which broken air­craft in the AOR were fixed was worse than the rate at home station (although the AOR rate improved over time as the supply system, interme­diate main­tenance, and other capabilities came fully on line). For the C-5, main­tenance ability to repair aircraft rapidly enough between missions ap­pears to have been the limiting factor. As is discussed in chapter 3, Mili­tary Airlift Com­mand flew all C-5 aircraft that were mission capable.

Figure 70

F-15 Break and Fix Rates

37


Why Were Capability Rates Better Than Expected?
Although capability rates were not as good as appeared from the initial data, they were still better than ones forecast as late as April 1990. In that month, the AFLC Logistics Operations Center assessed Logis­tics Command's ability to support OPLAN 1002-90. The Center concluded that Logistics Command could fully support only two of thirteen aircraft types tasked in the OPLAN; the B-52 and C-141 were actually rated as unsup­ported.719 Because of the disparity between prediction and outcome, the Command performed an after-the-fact assessment during the summer of 1991 to uncover the reasons for the differences. Results are summa­rized in Table 37.720
Three common threads run through Table 37. First, aircraft such as the F-4G and the F-16 simply “got well” between the initial assess­ment and the Desert Shield and Desert Storm deployment. Second, non­deploy­ing aircraft and their WRSKs kits were extensively cannibal­ized.721 Third, only small proportions of the respective fleets usually de­ployed, making extensive cannibalizing practical. Those that remained home became a ready source of supply for those that did deploy. The April assessment assumed there would be no cannibalization from non­deployed aircraft or their WRSKs.
Comparison with Other Services
Navy experience was essentially the same as Air Force experi­ence. Eight carriers participated in Desert Shield and Desert Storm. The Center for Naval Analyses (CNA) analyzed the mission capability data and con­cluded that the Navy mission-capable rates were as high as those normal­ly experienced in peacetime,722 although CNA did not provide the equiva­lent peacetime rates. CNA's summary data for Desert Shield and Desert Storm are presented in Table 38. Reasons given for the sustained mis­sion-capable rates were (1) flying-hour usage rates were near planned wartime numbers, (2) carriers shared intermediate maintenance facilities, (3) and a healthy supply stock was available.723 A quantifiable measure of supply health is the range and depth fill rates of the Navy's Aviation Coordinated Allowance List and rotable pools.724 Fill rates are given in Table 39.
Table 37

Rationale for Differences Between April 1990 OPLAN 1002-90

Assessment and Desert Shield/Desert Storm Results725



Aircraft Type

April 1990

As­sess­ment

Rationale for Difference

and/ or Comments



A-10

Fully supported.

Six squadrons deployed with six WRSKs but kits deployed were meant for a larger number of aircraft. Parts plentiful from the beginning and WRSKs kept filled by resupply. A-10 level of activity could have been sustained for considerably longer than combat phase of Desert Storm.




E-3

Marginally supported for two problem parts.

Peacetime and wartime missions are the same, extensive desert operational experience, effective parts chaser operation at Tinker AFB (possible because of small number of E-3s), Desert Express, and weekly EC-135 rotation aircraft transporting parts, preemptive cannibalization of problem parts from depot aircraft.


F-4G

Unsupported because of 13 problem parts. Also anticipated wind­screen problems.


Of 13 problem parts, 10 had get-well dates before first F-4 deployment. Windscreen problems did not materi­alize.

RF-4

Supported.

No issues.










Table 37 (Contin­ued)


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