Fuselage

Scratch damage

Scratch damage - Aero-Engineering
 
Damage report

Aircraft Mark XX-XXX, SN XXXX

damage report:

Scratch found near the AFT PAX door between FS XX and FS XX and between the stringer STR XXL and XXL .
Dimension XX” length , X,XX” depth
The damage is considered within the limits of SRM chapter XX-XX-XX and is classified permanent or temporary and need to be repaired

AOG structural evaluation

AOG structural evaluation - Aero-Engineering
 
Structural damage Analysis

Aircraft Mark XX-XXX SN XXXX

Analysis:
After the tail strike the following damages still on:

Between FS XX and FS XX STR XX and STR XX
Frame found cracked stringer found craked
Internal inspection performed as per AMM chapter XX-XX-XX
Additional damage found

liason with TCH for repair instruction and evaluation

Repair to be accomplished as per SRM chapter XX-XX-XX
 
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