Predicting Disposal Costs for United States Air Force Aircraft (Presentation)

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INSTITUTE FOR DEFENSE ANALYSES Predicting Disposal Costs for United States Air Force Aircraft (Presentation) Mark F. Kaye Bruce R. Harmon Alexander O. Gallo John E. MacCarthy May 2015 Approved for public release; distribution is unlimited. IDA Document NS D-5478 Log: H 15-000371 INSTITUTE FOR DEFENSE ANALYSES 4850 Mark Center Drive Alexandria, Virginia 22311-1882

About this Publication The views, opinions, and findings should not be construed as representing the official position of either the Department of Defense or the sponsoring organization. Copyright Notice 2015 Institute for Defense Analyses 4850 Mark Center Drive, Alexandria, Virginia 22311-1882 (703) 845-2000. This material may be reproduced by or for the U.S. Government pursuant to the copyright license under the clause at DFARS 252.227-7013 (a)(16) [Jun 2013].

Predicting Disposal Costs for United States Air Force Aircraft Western Economics Association International Mark F. Kaye Bruce R. Harmon Alexander O. Gallo John E. MacCarthy June 2015

2 Outline Background Research Approach Aerospace Maintenance and Regeneration Group (AMARG) Process Model Model Assumptions AMARG Data IDA Model and Regressions Conclusions

Life cycle cost estimates for USAF aircraft include disposal of assets, but little information is available on how to estimate disposal costs in cases in which disposal of assets is not imminent. The Boneyard Davis-Monthan AFB 3 Background Storage Status 1000: War Reserve 2000: Parts Reclamation 3000: Flyable Hold 4000: Disposal Prep

4 Research Approach Develop Disposal Life Cycle Cost Work Breakdown Structure (WBS) based on AMARG disposal process Collect AMARG data Only able to obtain last 10 years of data Revenue and labor rates Overhead was included in labor rates Identify systems for which adequate data existed to perform regression analysis Use labor hours as basis for regression analyses and cost model

AMARG Process Model AMARG in-processes ~200 AC/year ~4000 aircraft on site at AMARG Storage for ~20 years Maintenance occurs 2 times/year Category 1000 for ~10 years ( re-preservation every 4 years) Each aircraft will see re-preservation twice Category 2000/4000 for ~10 years 1000 Storage Other Factors Peculiar support equipment (PSE) is disposed of separately Storage of production tooling disposed of separately Ordnance and weapons removed before arrival at AMARG In-process includes initial HAZMAT removal (fuel, coolants, explosives) Engines are stored/disposed of with aircraft Major HAZMAT removed at disposal preparation 2000 Storage Reclamation AC In-Processing 4000 Storage Demil/Scrapping Disposal Prep 3000 Storage Hazardous Waste Disposal 5

IDA Disposal Life Cycle Cost Model Assumptions 6 Disposal Model Assumptions: 1 in-process and 1 disposal prep project/tail 2 in-storage maintenance projects/tail/year t s years in storage (nominal value of 20) Aircraft are in inviolate (War Reserve) storage (1000 category) for t i years (t i can be 0 if the aircraft is never in 1000 status) Re-preservation (rp) occurs every 4 years A total of Nrp times (nominal value of 2) Reclamation Assumptions: Programmed/savelist reclamation: 1 per tail Priority reclamation: Analysis indicates P(x) 0.05 based on total in storage

7 AMARG Data Data Tail number (aircraft serial number) Mission design Work phase (in-process, storage, etc.) Work hours Revenue AMARG Process Labor Hour Distribution Disposal Phase Hours Process-In 35% Storage Maintenance 6% Re-Preservation 15% Disposal Prep 27% Parts Reclamation 17%

Predicted Cost = Disposal (D) + Reclamation (R) 8 IDA Disposal Life Cycle Cost Model D=PI+S+R+D, where PI = process-in hours (1 time event) S = storage maintenance hours (2xs per year during time in storage) R = re-preservation hours (2xr during time in storage) D = disposal preparation hours (1 time event) R = sl + P(x)*t s *pr, where sl = programmed/savelist (1 time event) pr = priority reclamation, P(x) =.05 and t s = years in storage All regressions in labor hours Independent labor rate applied The IDA Model is flexible and can be adjusted to reflect number of years in storage, re-preservations, labor rates, etc.

OLS, Dependent Variable is Average Labor Hours for each Mission-Design (e.g., F-16) Transports, Trainers and Attack Actual: Transport, Trainers and Attack Actual: Fighter 9 One-Time Event Regressions Process-In Disposal Prep PI = 1.99 WWWWWWWWWWW 0.428 2.59 BBBBBBBBBBBB 1.56 FFFFFFFFFFFFF 0.425 WWWWWWWWWWW 0.267 D = 4.25 WWWWWWWWWWW FFFFFFFFFFFFFFFFFF Process-In Model Bombers 350 300 Fighters 250 Fighters Average Unit Labor Hours Transports, Trainers and Attack Actual: Transport, Trainers and Attack Average Unit Labor Costs 200 150 100 Actual: Fighter Actual: Bomber 50-50,000 100,000 150,000 200,000 250,000 300,000 350,000 Aircraft Empty Weight (lbs) - - 50,000 100,000 150,000 200,000 250,000 300,000 350,000 Aircraft Empty Weight (lbs) Regression Metric Resulting Value R 2 0.89 Adjusted R 2 0.85 Standard Error of the Estimate (σσ ) 0.31 σσ expressed as +/- percentages +36%/-26% p value (baseline other) <0.01 p value (bomber) <0.01 p value (fighter) <0.10 Regression Metric Resulting Value R 2 0.68 Adjusted R 2 0.62 Standard Error of the Estimate (σσ ).27 σσ expressed as +/- percentages +32%/--24% p value (weight) <0.01 p value (weight/footprint) <.05

Storage Maintenance Re-Preservation 10 Recurring Event Regressions ss = 1.70 + 0.0000168 WWWWWWWWWWW rr = 116.7 + 0.00268 WWWWWWWWWWW 7.5 7.0 800 6.5 6.0 700 Average Unit Labor Hours 5.5 5.0 4.5 4.0 3.5 3.0 2.5 2.0 1.5 1.0 0.5 - y =.0000168 + 1.7011 R² = 0.86 Transport, Trainers and Attack Fighter Bomber - 50,000 100,000 150,000 200,000 250,000 300,000 350,000 Aircraft Empty Weight (lbs) Average Unit Labor Hours 600 500 400 300 200 100 - y = 0.0027x + 116.73 R² = 0.88-50,000 100,000 150,000 200,000 Aircraft Empty Weight (lbs) Regression Metric Resulting Value R 2 0.86 Adjusted R 2 0.85 Standard Error of the Estimate (σσ ) 0.62 Coefficient of Variation. +/-20 p value (weight) <0.01 Regression Metric Resulting Value R 2 0.89 Adjusted R 2 0.87 Standard Error of the Estimate (σσ ) 65.6 Coefficient of Variation +/-.22 p value (weight) <0.01

Save List Priority Reclamations ssss = 0.051 WWWWWWWWWWW 0.818.51 NNNN pppp = 7.56 + 0.000225 WWWWWWWWWWW 11 Reclamation Event Regressions 90 Average Unit Labor Hours 1,000 100 Operational Aircraft No Longer Operational Average Unit Labor Hours 80 70 60 50 40 30 20 y = 0.0002x + 7.5594 R² = 0.6916 10 10 1,000 10,000 100,000 Aircraft Empty Weight (lbs) - - 50,000 100,000 150,000 200,000 250,000 300,000 350,000 Regression Metric Resulting Value R 2 0.88 Adjusted R 2 0.85 Standard Error of the Estimate (σσ ).51 σσ expressed as +/- percentages +66%/--40% p value (weight) <0.01 p value (no longer operated) <0.10 Regression Metric Resulting Value R 2 0.69 Adjusted R 2 0.66 Standard Error of the Estimate (σσ ) 15.5 Coefficient of Variation +/-.55 p value (weight) <0.01

Sample Results: IDA Model Estimates for 3 Systems Priority Reclamation (1x) 10 10 25 Project Reclamation 40 75 240 TOTAL 575 835 1280 When AMARG labor rates are applied, costs are less than.05% of flyaway costs However, for a large fleet, total costs could exceed $100M 12 Step Hours T-38 F-16 C-130 Process-In 90 200 235 Storage (20 years) 70 80 100 Re-preservation (2x) 265 310 545 Disposal 100 160 135 Sub-total 525 750 1015

13 Conclusions IDA model for estimating future disposal costs Empty weight Mission Density Assuming no major changes in AMARG process future disposal costs can be predicted with sufficient accuracy using the above independent variables In terms of total aircraft lifecycle cost, the disposal costs are relatively modest; however, still significant in the aggregate by a given fleet

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