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I. Airframe Wing
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EFTA00684131.pdf
1 mentionEFTA00684131
erational Test 24 MOS O MAN 1 98 Days O1 532067 (P) [. Airframe Tail Compartment Above Floor - Inspection 24 MOS O MAN 1 98 Days O 571064 I. Airframe Wing to Fuselage Attachments (Left) - Ultrasonic and Visual Corrosion Damage Tolerance Inspection 24 MOS O MAN 1 98 Days O 571065 Airframe Wing to
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