N903SJ

ATA 5320

Part: CHINE CAP — DAMAGED (BS 425-817)

DURING C-CHECK/BRIDGING INSPECTION, FOUND SEVERAL CHINE CAPS, FS 245E TO 817E LT AND RT, WITH ELONGATED HOLES AT 10K TIE DOWNS, CORROSION, CRACKS, ANCHOR NUT RIVET HOLES. REPLACED ALL CHINE CAPS, EXCEPT ONE REPAIRED.

ATA 5330

Part: SKIN — CRACKED (BS 480)

DURING C-CHECK/BRIDGING INSPECTION, SPIDER CRACKS FOUND ON THE MLG WHEEL WELL RT PANEL SKIN, FS 480 AND WL 198. CRACKS IN SKIN PANEL TRIMMED OUT, REPAIR DOUBLER INSTALLED.

ATA 5313

Part: LONGERON — CRACKED (FUSELAGE)

DURING C-CHECK/BRIDGING INSPECTION, LT SLOPING LONGERON FOUND CRACKED AT RS1 RETAINER HOOK. LONGERON REPLACED.

ATA 5510

Part: CAP — CRACKED (HORIZ STAB)

DURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKED TANG AT HSS 180.0. DAMAGE AREA CLEANED UP AND TANG REPLACED WITH LS30661 EXTRUSION.

ATA 5320

Part: WEB — CRACKED (BS 590)

DURING C-CHECK/BRIDGING INSPECTION, CRACKS LOCATED IN THE WEB AT WL 200, FS 590 ON BOTH LT AND RT SIDES. REPLACED WEB.

ATA 5720

Part: BEAM — CRACKED (BS 597)

DURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING REAR BEAM CRACKED AT CWS 72R, FS 597, APPROX WL 268. INSTALLED NEW INBD SECTION OF WEB, DOUBLER, AUXILIARY DOUBLER, SPACER STRAP, RADIUS BLOCK, REPAIR FINISHED.

ATA 5400

Part: BULKHEAD — WORN (NR 4 ENGINE)

DURING C-CHECK/BRIDGING INSPECTION, NR 4 ENGINE QEC FRONT BULKHEAD ASSEMBLY WORN ON BOTH SIDES OF FILLER, TOP CENTER. REPLACED EXISTING FILLER, INSTALLED WEAR STRIP.

ATA 5400

Part: ANGLE — CRACKED (NR 1/2/3/4 NAC)

DURING C-CHECK/BRIDGING INSPECTION, FOUND ANGLE AT LOWER AFT NACELLE ASSY CRACKED NEAR FORWARD MOST SPOT WELD NR 1, 2, 3, 4 ENGINES FS 517, PPBL 5.0.

ATA 5412

Part: FIREWALL CAP — WORN (NR 3 ENGINE)

DURING C-CHECK/BRIDGING INSPECTION, FOUND NR 3 ENGINE FIREWALL CAP WORN AT WL 225. BLENDED GROOVE, APPLIED FILLER, INSTALLED DOUBLER.

ATA 5730

Part: SKIN — WORN (LT WING)

DURING C-CHECK/BRIDGING INSPECTION, LT AUX TANK CAVITY LOWER WING SKIN UPPER AND LOWER SURFACE HAS WEAR MARKS. WEAR MARKS BLENDED SMOOTH, EDDY CURRENT INSPECTED, AND ROTO-PEENED.

ATA 5313

Part: LONGERON — CRACKED (BS 410-485)

DURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKS ON A LONGERON, NR 2 AND NR 3 ENGINE, FS 410 TO FS 485, PPBL 10.00L, AND WEAR ALONG THE LONGERON WHICH IS .030 TO .035 INCHES DEEP. EXISTING REPAIR REMOVED, CRACKED PORTION OF LONGERON TRIMMED OUT, FILLER INSTALLED, REPAIR DOUBLER INSTALLED.

ATA 5400

Part: EXTRUSION — WORN (BS 410)

DURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE, LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.

ATA 5350

Part: FAIRING — CRACKED (WS 174)

DURING C-CHECK/BRIDGING INSPECTION, CENTER WING LEADING EDGE TO INBOARD ENGINE NACELLE FAIRING ASSY WEB HAS 2 CRACKS AT CW STA 174. TRIMMED OUT CRACKS, INSTALLED FILLER AND DOUBLER.

ATA 5412

Part: BULKHEAD — CRACKED (NR 1/2/3 NACELLE)

DURING C-CHECK/BRIDGING INSPECTION, FOUND 2 CRACK RADIATING ACROSS THE NR 1, 2, 3 AFT NACELLE BULKHEAD ASSY LOWER OUTBOARD SIDE, FS 485.9, PPWL 3.5. STOP DRILLED AND INSTALLED REPAIR DOUBLER.

ATA 5320

Part: WEB — CRACKED (BS 597-617)

DURING C-CHECK/BRIDGING INSPECTION, A CRACK AT WEB CTR FUS, FS 597.0 TO 617.0, BL 61.625 UPPER, EXTENDING FROM ONE WIRE BUNDLE CUTOUT HOLE TO ANOTHER, APPROXIMATELY 1 INCH LENGTH AND AN ADDITIONAL CRACK WHICH HAS EXTENDED JUST PAST A CREW HOLE ABOVE THE 1 INCH CRACK. THE WEB WAS REPLACED WITH A CHANNEL STIFFENER INSTALLED IN THE CENTER OF THE WEB.

ATA 5400

Part: TEE — WORN (BS 410)

DURING C-CHECK/BRIDGING INSPECTION, TEE EXTRUSION IS WORN, NR 3 ENGINE, FS 410, PPBL 0.0 AND PPWL 11.0, AT THE TOP OF THE BULKHEAD. THE WORN AREA WAS BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.