5343VL25 DID A005 DI-MISC-81391A.pdf

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This document is a Data Item Description (DID) for the Analytical Condition Inspection (ACI) Report, designated DI-MISC-81391A, approved March 26, 2018, by the Air Force Life Cycle Management Center (AFLCMC/EZFS). The ACI Report is a deliverable template that establishes the format and content requirements for aircraft structural inspections conducted under Task V of MIL-STD-1530 (Aircraft Structural Integrity Program) and Subtask 3 of MIL-STD-1798 (Mechanical Equipment and Subsystems Integrity Program).

The ACI Report must be prepared in the contractor's format and include two primary sections: ACI Work Instructions and ACI Inspection Results. The Work Instructions section requires identification of each inspection location with part identification numbers, criticality classification (safety-critical, durability-critical, or normal controls), inspection area/location, reason for inspection, inspection frequency, type of inspection methodology, access instructions, and detailed inspection procedures with anticipated damage types. The Inspection Results section must document pertinent aircraft identifying information (mission design series, serial number, base assignment history, planned and actual inspection dates, flight hours, and last programmed maintenance date), condition descriptions for each inspected article, damage classification (minor, major, or critical) with detailed documentation including sketches, photographs, part numbers, work unit codes, root cause analysis, and engineering records, and a summary of findings with a prioritized list of critical and major findings and recommendations for revisions to depot and field-level maintenance requirements. The document applies to federal aircraft maintenance programs and provides no specific response dates, pricing terms, or contract vehicles.

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DATA ITEM DESCRIPTION

Title: ANALYTICAL CONDITION INSPECTION (ACI) REPORT

Number: DI-MISC-81391A Approval Date: 20180326 AMSC Number: F9914 Limitation: N/A DTIC Applicable: No GIDEP Applicable: No Preparing Activity: 11 (AFLCMC/EZFS) Project Number: MISC-2018-008 Applicable Forms: N/A Use/Relationship: The Analytical Condition Inspection (ACI) Report will be used to reveal damage (flaw, defect, crack, corrosion, disbond, delamination, discontinuity, or other type that degrades or has the potential to degrade the performance of the affected component) that may not otherwise be detected through normal technical order (TO) and programmed depot maintenance (PDM) inspections and to provide data for engineering and technical evaluations of the relative condition of the mission, design and series (MDS) aircraft. Data generated through ACI Reports is used to refine mandatory aircraft inspection programs (field and depot).

This DID contains the format, content and intended use information for the data deliverable resulting from the technical requirements described in Task V of MIL-STD-1530, Aircraft Structural Integrity Program (ASIP), and Subtask 3 of MIL-STD-1798, Mechanical Equipment and Subsystems Integrity Program.

(Copies of these documents are available online at http://quicksearch.dla.mil.)

Requirements:

1. Reference Documents. The applicable issue of the documents cited herein, including their approval dates and dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.

2. Format. The ACI Report shall be in the contractor’s format.

3. Content. The ACI Report shall include the following information:

3.1 ACI Work Instructions - for each inspection/inspection location:

a. Identification number.

b. Part name/description of article to be inspected.

c. Part number(s).

d. Part criticality – safety or fracture critical, durability or maintenance (Mx) critical, normal controls, etc.

e. Area/location of inspection.

f. Reason for inspection.

DISTRIBUTION STATEMENT A. Approved for public release. Distribution is unlimited.

Source: http://assist.dla.mil -- Downloaded: 2019-08-07T17:16Z Check the source to verify that this is the current version before use.

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DI-MISC-81391A

g. Frequency of inspection.

h. Type of inspection.

i. Instructions for accessing article to be inspected.

j. Inspection procedures and potential/anticipated damage.

3.2 ACI Inspection Results:

a. Pertinent aircraft identifying information:

(1) Aircraft mission design series (MDS).

(2) Aircraft serial number (SN).

(3) Base assignment history.

(4) Planned ACI start and end date.

(5) Actual ACI start and end date.

(6) Actual flight hours.

(7) Equivalent flight hours.

(8) Last programmed depot Mx date.

b. Information for each inspection location:

(1) ACI work instruction identification number.

(2) Date of inspection.

(3) Description of inspected article condition.

(4) If damage found, damage classification (minor, major, or critical):

(a) Detailed description, sketches, drawings, and photographs documenting damage, for damage types, sizes, locations, and orientations.

(b) Part number and criticality classification.

(c) Work Unit Code for item with defect.

(d) How malfunction codes/root cause determination.

(e) Engineering and nondestructive inspection records.

(f) Action taken code/damage disposition (no action required, repair, replace, etc.)

with documentation.

(5) Record of inspection:

(a) Date and time of inspection.

(b) Name and organization of inspector.

(c) Location of inspection (e.g., RAFB (Robins Air Force Base), HAFB (Hill Air Force Base), TAFB (Tinker Air Force Base), location of contractor facility, etc.).

c. Summary of results and recommendations.

(1) Summary of inspection findings.

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DI-MISC-81391A

(2) Prioritized list of critical and major findings.

(3) Recommendations for revisions to maintenance requirements at the depot and/or field levels.

End of DI-MISC-81391A.

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