OO-ALCI21-107 governs engine management, reporting, accountability, and control for propulsion units at OO-ALC and JBSA.
View OO-ALCI21-107 on armypubs.army.mil
The publication covers CEMS status, condition, configuration, location, and TCTO compliance reporting for engines and tracked components. It requires timely processing of engine runs, aircraft flights, and engine movements, and prohibits flight or delivery before CEMS reporting.
Each time the engine is run, the engine is downloaded and processed in the CETADS work center computer, then reconciled to the SRAN EM/BEM host computer and recorded in CEMS, IAW with TO 00-25-257-1, Engine Health Management Plus (EHM+) User’s Manual Instructions for Turbofan Engine Model: F100-220; TO 00-25-257-2, Engine Health Management Plus (EHM+) User’s Manual Instructions for Turbofan Engine Model: F100229; TO 00-25-257-3, Engine Health Management Plus (EHM+) User’s Manual Instructions for Turbofan Engine Model: TF34-100A; and TO 00-25-257-4, Engine Health Management Plus (EHM+) User’s Manual Instructions for Turbofan Engine Model: F110-129. (paragraph 1)
Reporting by any method must be accomplished no later than COB the next business day following the date/time of the occurrence. (paragraph 1)
OO-ALC Form 206, F100-PW-220 Data Run Sheet, OO-ALC Form 207, F100-PW-229 Data Run Sheet, or test cell printout is submitted to the SRAN EM/BEM for processing through CEMS after completion of the test cell run. (paragraph 1)
No aircraft will be flown or delivered until the engine and/or components are reported in CEMS. (paragraph 1)
One of the engine management section’s primary responsibilities is timely reporting in CEMS pertaining to asset status, condition, and location at all times. (paragraph 1)