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Reviewing asK. Reyes, A&P/IA
Module
CFM56-7B · Line Insp
Current Version
v2.1
Last Updated
Nov 12, 2026
Approval Status
Approved
Training Content

Procedure Sections

3 sections
Fan Blade Damage Limits
AMM 72-31-00 · Rev 2.1

Inspect all 22 fan blades for nicks, dents, and leading-edge erosion. Allowable nick depth: 0.020 in max within blend limits. Cracks: none permitted.

Spinner Inspection Procedure
AMM 72-11-04 · Rev 2.0

Rotate spinner through 360°. Inspect for surface cracks radiating from fastener holes. Torque check on all 6 attachment bolts to 45 in-lb.

Cowling Latch Verification
AMM 71-11-06 · Rev 1.9
1 flag

Verify all cowling latches are engaged and safety-wired per figure 4. Confirm no chafing on hinge assemblies.

Image Annotation

Engine Diagram Markup

Tap image to annotate
CFM56-7B turbofan engine reference diagram for SME annotation
1
1
Confirm fan blade count matches AMM figure — currently shows 20, should be 22.

Flag Outdated Content

Cowling Latch Verification
major
Cowling latch torque value missing — required per current SB.

Suggest Procedure Update

Submit a revision note. It will enter the ID review queue as a new pending version.

Revision History

  1. v2.1· Nov 12, 2026Approved
    K. Reyes, A&P/IA
    Lead SME · Powerplant

    Updated nick blend limits per SB 72-0384. Added torque values to spinner procedure.

  2. v2.0· Aug 03, 2026Approved
    M. Osei, DER
    SME · Structures

    Reworked cowling latch verification steps. Added figure references.

  3. v1.9· Apr 21, 2026Superseded
    J. Whitfield, A&P
    Instructional Designer

    Initial competency-based rewrite from legacy CBT module.