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Japan Air Lines 123

Printed page label not indexed. PDF page 46.

expressed in rivet numbers was from No.30 to No.83. In the cut-off position, an aluminum filler about 0.9 mm in thickness had been inserted and riveted to the stiffener together with the upper web. The cut- off of the lower
Open official document at PDF page 46AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119

Japan Air Lines 123

Printed page label not indexed. PDF page 112.

out in which one splice plate narrower than described in rework instructions, and one filler were applied, instead of one splice plate. No written record, however, was found to the effect that such work was done, It is estimated that
Open official document at PDF page 112AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119

Japan Air Lines 123

Printed page 124. PDF page 135.

intended corrective measure, one splice plate narrower than drawing requirements, and one filler were applied instead of one splice plate. 4.1.3.5 In inspections during and after the repair work, the afore-mentioned improper part of the work could not be found.
Open official document at PDF page 135AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119

Japan Air Lines 123

Printed page label not indexed. PDF page 189.

“TEAR STRAP NO. 4. -s a. ”~ - - 3° o™! * a . a . BAY 5 : oe - . . oe ge ~ - FILLER INSERTED AREA RAY 2 rl a, a - ~ SPLICE PLATE INSERTED
Open official document at PDF page 189AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119

Japan Air Lines 123

Printed page label not indexed. PDF page 262.

instructions having been issued, in the actual repair work, a short splice plate and a filler were used as shown on the right side of the attached figure above, instead of a single splice plate, with the result that the
Open official document at PDF page 262AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119

Japan Air Lines 123

Printed page label not indexed. PDF page 267.

easure - YT top TTS upper dome fwd. we _- fillet seal position of existent rivets «a ‘ filler © = \ = + Ss = 3 4 = = TRE TC rivet down at same in lower dome fillet
Open official document at PDF page 267AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119