N12538

ATA 5311

Part: FRAME — CRACKED (BS 484)

INSPECTION FOUND A 2.5 CRACK IN FORWARD PIT FRAME AT STA 484 BETWEEN STRINGER 26L AND 27L. THE CRACKED AREA OF FRAME WAS CUT OUT IAW ECRA 5320-01263. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.

ATA 5320

Part: JAMB — CORRODED (CARGO DOOR)

INSPECTION FOUND INNER AFT CARGO DOOR PAN CUTOUT CORRODED. THE DOOR PAN AND THRESHOLD TRIM WERE REMOVED IAW SRM 51-30-2. THE THRESHOLD WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A THRESHOLD WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5. THE DOOR JAMB PAN WAS INSTALLED IAW SRM 51-30-2.

ATA 5730

Part: DOOR — GOUGED (WS 240)

INSPECTION FOUND RT WING LEADING EDGE SLAT DOOR GOUGED AT XOS 240. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01568.

ATA 5320

Part: WEB — CRACKED (BS 756)

INSPECTION FOUND A CRACK IN CABIN INTERIOR WEB AT STA 756, RBL 53. THE WEB WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4.

ATA 5230

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK IN OUTER PAN RADIUS OF FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD STOP FITTING. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 2-03, FIGURE 8.

ATA 5730

Part: SKIN — CORRODED (RT WING)

INSPECTION FOUND RT WING PANEL NR 1246 CORRODED AND DELAMINATED. THE OUTER SKIN WAS REMOVED AND HONEYCOMB WAS CLEANED. NEW SKIN AND HONEYCOMB WERE FABRICATED AND INSTALLED IAW SRM 51-31-1, FIGURE 1 AND 51-70-2.

ATA 5230

Part: BEAM — CRACKED (CARGO DOOR)

INSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF BEAM NR 1 FASTENER LOCATION AND A .5 INCH CRACK AT FORWARD END OF BEAM NR 5 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. THE CRACKS WERE STOP DRILLED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 52-03.

ATA 5240

Part: BEAM — CRACKED (FWD SERV DOOR)

INSPECTION FOUND A 2 INCH CRACK IN FORWARD END OF NR 6 BEAM OF FORWARD SERVICE DOOR. THE BEAM WAS REPAIRED IAW EA 5240-01192.

ATA 5540

Part: WEDGE — CRACKED (RUDDER TE)

INSPECTION FOUND A .5 INCH CRACK IN RUDDER TRAILING EDGE WEDGE. THE AREA WAS REPAIRED IAW SRM 55-03 AND 51-70-2.

ATA 5753

Part: FAIRING — CRACKED (LT TE FLAP TRACK)

INSPECTION FOUND A 2.5 INCH CRACK IN LT FLAP INBOARD FLAP TRACK FAIRING TRAILING EDGE. THE FAIRING WEB AND ANGLE WERE REMOVED. A NEW WEB AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.

ATA 5720

Part: FRAME — CRACKED (RT WING)

INSPECTION FOUND A .5 INCH CRACK IN FRAME AT RT WING REFUELING STATION. THE CRACK WAS ROUTED OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5730-01564.

ATA 5320

Part: WEB — CORRODED (BS 980-996)

INSPECTION FOUND LAV FLOOR WEB CORRODED BETWEEN STA 980 AND 996 AT RBL 59. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

ATA 5330

Part: SKIN — CRACKED (BS 980)

INSPECTION FOUND A 1/2 CRACK AT FASTENER HOLE OF FUSELAGE SKIN AT AFT CABIN LT SIDE STA 980 ABOVE LONGERON 15L. THE CRACKED AREA OF SKIN WAS CUT OUT. A FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 32 AND 51-10-38.

ATA 5230

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1/2 CRACK AT AFT END OF BEAM NR 3 FASTENER LOCATION OF AFT CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5261C-01000.

ATA 5321

Part: FLOOR — CORRODED (BS 279-378)

INSPECTION FOUND FLOOR PANEL IN FORWARD PIT CORRODED AND DELAMINATED AT STA 378 TO 279. A NEW PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.

ATA 5753

Part: SKIN — CORRODED (LT TE FLAP)

INSPECTION FOUND LT TRAILING EDGE INBOARD FLAP INTERIOR CORRODED AND FINGER DOUBLERS SEPARATED. THE T/E FLAP SKIN WAS REMOVED. NEW SKIN AND BONDED DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-50-9, FIGURE 6, 51-70-2, AND 51-30-2.

ATA 5321

Part: FLOORBOARD — DELAMINATED (BS 389-465)

INSPECTION FOUND CABIN FLOORBOARD NR 41 DELAMINATED AT LT SIDE FS 389-465. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05, 53-21-0, 51-30-2, 51-10-3, 51-70-2, AND 51-20-0.

ATA 5210

Part: ANGLE — CRACKED (PAX DOOR)

INSPECTION FOUND THREE CRACKED ANGLES ON RT SIDE OF AFT ENTRY DOOR. THE DOOR SKIN AND ANGLES WERE REMOVED. NEW ANGLES WERE AND DOOR SKIN WERE INSTALLED IAW SRM 51-10-4 AND 51-30-2.

ATA 5230

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 0.7 CRACK AT FORWARD END OF BEAM NR 2 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 8.

ATA 5754

Part: PANEL — DELAMINATED (LT LE FLAP)

INSPECTION FOUND LT FLAP LEADING EDGE PANEL NR 3 DELAMINATED AT XFL 267. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-70-2.

ATA 5754

Part: PANEL — CORRODED (RT LE FLAP)

INSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE PANEL CRACKED AND CORRODED AT XFLS 283. THE CORROSION WAS REMOVED AND THE AREA WAS REPAIRED IAW SRM 51-30-2 AND 51-70-2.

ATA 5230

Part: WEB — CORRODED (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR INNER WEB CORRODED. THE CORROSION WAS REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 52-01, 51-10-3, AND 52-30-0.

ATA 5210

Part: ANGLE — CRACKED (PAX DOOR)

INSPECTION FOUND A 1.25 CRACK IN L-ANGLE FOR AFT ENTRY DOOR. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-2A.

ATA 5320

Part: ANGLE — CORRODED (BS 996)

INSPECTION FOUND L-ANGLE ON BULKHEAD FRAME CORRODED AT STA 996, STRINGER 19L. THE ANGLE WAS REMOVED IAW SRM 51-30-02, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, 51-10-4, 51-10-3 AND 51-30-02.

ATA 5350

Part: FAIRING — CRACKED (LT MLG WW)

INSPECTION FOUND AFT INBOARD SIDE OF LT WHEEL WELL FORWARD FAIRING CRACKED. THE CRACK WAS STOP DRILLED, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.

ATA 5321

Part: FLOORBOARD — CORRODED (CABIN)

INSPECTION FOUND CORROSION AROUND SCREW HOLES OF CABIN FLOORBOARD PANEL NR 44. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-21-0, AND 51-70-2.

ATA 5320

Part: CUSP — CORRODED (BS 980-996)

INSPECTION FOUND CUSP CORRODED AT LT SIDE OF STA 980 TO 996. THE CORRODED SECTION OF CUSP WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE25.

ATA 5330

Part: SKIN — CORRODED (BS 937)

INSPECTION FOUND SKIN CORRODED AT STA 937, LONGERON 20L. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02673.

ATA 5230

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF THE BEAM NR 3 DOOR STOP CUTOUT OF AFT CARGO COMPARTMENT DOOR OUTER PAN. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 3.

ATA 5321

Part: FLOORBOARD — CRACKED (BS 680-756)

INSPECTION FOUND LT FLOORBOARD PANEL BETWEEN STA 680 AND 756 CRACKED AT THE LT FORWARD NR 5 ATTACH HOLE. A NEW FLOOR PANEL WAS FABRICATED. TWO HAT SECTIONS WERE REMOVED, CLEANED, AND REBONDED TO NEW FLOOR PANEL IAW SRM 53-05, PAGE 1.

ATA 5530

Part: PANEL — CRACKED (VERT STAB)

INSPECTION FOUND VERTICAL STABILIZER PHENOLIC PANEL CRACKED AT STA 96. THE PANEL WAS REMOVED IAW SRM 51-30-2, A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 55-01, PAGE 1 AND 51-30-2.

ATA 5321

Part: FLOOR — CORRODED (BS 237)

INSPECTION FOUND CABIN FLOOR PANEL NR 29 CORRODED ON UPPER AND LOWER SURFACES AT STA 237, BL 0 TO RBL 22. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND 51-70-2.

ATA 5320

Part: CLIP — BROKEN (BS 996)

INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD SIDE STA 996 THIRD HORIZONTAL STIFFENER FROM FLOORING HAD CLIP BROKEN OFF. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND CRACKS AT THREE SCREW HOLES IN RT FLOORBOARD NR 41. A STRAP WAS FABRICATED AND INSTALLED ON FLOOR PANEL IAW SRM 51-10-2 AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND FLOORBOARD NR 70 CRACKED. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.

ATA 5320

Part: DOUBLER — CRACKED (BS 996)

INSPECTION FOUND TWO .25 INCH CRACKS IN TITANIUM FINGER DOUBLER AT STA 996, LONGERON 20L. THE FINGER DOUBLER WAS REMOVED AND A NEW FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ENGINEERING ORDER 98-888.

ATA 5754

Part: RIB — CRACKED (LT LE FLAP)

INSPECTION FOUND FLAP RIB LEADING EDGE OF LT WING AT XRS 270 CRACKED AND CORRODED. THE FLAP RIB WAS REMOVED IAW SRM 51-30-2. A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.

ATA 5523

Part: HOUSING — CRACKED (LT ELEVATOR)

INSPECTION FOUND THE LT ELEVATOR OUTBOARD TRIM TAB INBOARD TRIM ROD HOUSING SHIELD CRACKED AT THE INBOARD UPPER COUNTERSUNK HOLE. THE CRACK WAS STOP DRILLED IAW SRM 55-01, FIGURE 2. A PATCH DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-3, AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND HAT SECTION OF 49 FLOORBOARD CRACKED AT BOTH ENDS. THE HAT SECTION WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 51-70-2.

ATA 5320

Part: ANGLE — CRACKED (DORSAL FIN)

INSPECTION FOUND A .5 INCH CRACK IN LT DORSAL FIN PANEL ATTACH ANGLE. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.

ATA 5320

Part: WEB — CRACKED (BS 756)

INSPECTION FOUND A 2 INCH CRACK IN CABIN WEB AT STA 756, LBL 53. THE WEB WAS REMOVED IAW SRM 51-30-2. TWO REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-4, AND 51-30-2.

ATA 5730

Part: PANEL — GOUGED (RT WING)

INSPECTION FOUND A GOUGE IN LOWER RT WING ACCESS PANEL. THE GOUGED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-6, FIGURE 13.

ATA 5321

Part: FLOORBOARD — CRACKED (BS 756/680)

INSPECTION FOUND RT SIDE FLOORBOARD HAD FOUR CRACKS AT SCREW HOLES OF FS 756 AND THREE CRACKS AT SCREW HOLES OF FS 680. THE HAT SECTIONS WERE REMOVED, A NEW FLOOR PANEL WAS FABRICATED AND HAT SECTIONS WERE BONDED TO NEW PANEL IAW SRM 51-30-2, 51-10-2, 51-10-3, 53-05, AND 51-20-0.

ATA 5321

Part: FLOORBOARD — GOUGED (CABIN)

INSPECTION FOUND FLOORBOARD PANEL NR 86 GOUGED AND CORRODED. A PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-05 PAGE 1, 51-20-0 AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND CRACKS AT FORWARD AND AFT ENDS OF FLOORBOARD NR 45. THE FLOORBOARD WAS REPAIRED IAW SRM 53-01, PAGE 9.

ATA 5320

Part: STRAP — CORRODED (CABIN)

INSPECTION FOUND RT AFT CEILING PANEL ATTACHING STRAPS CORRODED. NEW STRAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.

ATA 5320

Part: FITTING — CORRODED (BS 851)

INSPECTION FOUND FITTING UNDER FRAME AT STA 851, LONGERON 27 TO 28R CORRODED. THE FITTING WAS REPAIRED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND CABIN FLOORBOARD NR 45B FORWARD LEADING EDGE LIP CRACKED AND TORN. THE TORN AREA WAS ROUTED OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 122, FIGURE 4, 51-10-3 AND 51-10-4.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND FLOORBOARD PANEL NR 79 CRACKED AT THE RT FORWARD EDGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, 53-01 PAGE 12-18.

ATA 5321

Part: FLOORBOARD — SPLITTING (BS 465-579)

INSPECTION FOUND NR 48 FLOORBOARD SKIN SPLITTING AT FS 465 TO 579. SKIN AND FOUR HAT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 51-70-2.

ATA 5414

Part: SKIN — CRACKED (NR 1 ENGINE)

INSPECTION FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED AND CHAFED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.

ATA 5311

Part: FRAME — CRACKED (BS 1074)

INSPECTION FOUND FRAME STA 1074 CRACKED AT FASTENERS AT LONGERON 3R, 4R, 5R, AND 4L. THE CRACKED SECTION OF FRAME WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 30.

ATA 5320

Part: CLIP — CRACKED (BS 996)

INSPECTION FOUND TIE CLIP CRACKED AT STA 996, RBL 56. A NEW TIE CLIP WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3.

ATA 5720

Part: BRACKET — CRACKED (WS 332-232)

INSPECTION FOUND TWO CRACKS IN RT WING FLAP LEADING EDGE SUPPORT BRACKET AT XRS 332 TO 232. THE SUPPORT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-0, 51-10-2, 51-10-1, AND 51-10-3.

ATA 5320

Part: CLIP — CRACKED (BS 980)

INSPECTION FOUND A 2 INCH CRACK OUT OF UPPER FASTENER HOLE IN SHEAR CLIP AT FS 980 BELOW LONGERON 14L. THE SHEAR CLIP WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-22, 51-30-2, AND 51-30-5.

ATA 5311

Part: FRAME — CRACKED (BS 639)

INSPECTION FOUND A 3 INCH CRACK IN CABIN FRAME AT STA 639, LBL 60. THE CRACK WAS STOP DRILLED IAW SRM 53-03, PAGE 40. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03.

ATA 5321

Part: FLOORBOARD — DENTED (CABIN)

INSPECTION FOUND THREE DENTS WITH A CRACK IN FLOORBOARD PANEL NR 83. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW GMM 10-900-01, PAGE 1, SRM 51-70-1, 51-10-3, AND 53-05.

ATA 5321

Part: FLOORBOARD — DELAMINATED (BS 389-465)

INSPECTION FOUND NR 40 FLOORBOARD DELAMINATED AT CENTER AISLE STA 389 TO 465. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.

ATA 5280

Part: SKIN — DAMAGED (NLG DOOR)

INSPECTION FOUND RT NLG REAR DOOR DAMAGED BY LIGHTNING STRIKE. THE DAMAGED SKIN WAS REMOVED AND REPAIR SKIN WAS INSTALLED IAW SRM 52-81-0 AND 51-30-2.

ATA 5320

Part: JAMB — CRACKED (PAX DOOR)

INSPECTION FOUND A 2.25 INCH CRACK IN FORWARD PASSENGER ENTRANCE DOOR JAMB UPPER FORWARD CORNER INSIDE SKIN. A REPAIR WAS INSTALLED IAW ECRA 5330-02619 AND SRM 53-05, FIGURE 25A. A DIP WAS ISSUED FOR PERMANENT REPAIR PRIOR TO 1,000 LANDINGS OR NEXT SCHEDULED S-CHECK OR HIGHER, WHICHEVER COMES FIRST.

ATA 5321

Part: FLOORPANEL — DELAMINATED (BS 365-430)

INSPECTION FOUND FLOOR PANEL AT BS 365 TO 430 IN FORWARD PIT DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 2551-01010.

ATA 5321

Part: FLOORBOARD — CORRODED (BS 218-284)

INSPECTION FOUND CORROSION ON NR 1 FLOORBOARD IN FORWARD PIT WITH DELAMINATION ON EDGES AT STA 218 TO 284. TWO HAT SECTIONS AND SIX NUT PLATE STRIPS WERE REMOVED. A FLOORBOARD WAS FABRICATED. THE FLOORBOARD, HAT SECTION, AND NUT PLATE STRIPS WERE INSTALLED IAW ECRA 2551-01010, SRM 51-30-2, AND 51-10-3.

ATA 5321

Part: FLOORPANEL — CRACKED (BS 579-680)

INSPECTION FOUND NR 42 LT CENTER FLOOR PANEL IN FORWARD PIT CRACKED AT FS 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 53-05, PAGE 1, AND 51-70-1.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 980)

INSPECTION FOUND FLOORBEAM CORRODED AT BS 980, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-05, FIGURE 20A, AND 51-30-2.

ATA 5330

Part: SKIN — CORRODED (BS 740-755)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 740 TO 755, LONGERON 29L TO 29R. THE CORRODED AREA WAS CUT OUT, A REPAIR SPLICE DOUBLER AND EXTERNAL REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-04, FIGURE 42, AND 51-30-1.

ATA 5321

Part: FLOOR — CRACKED (BS 627-657)

INSPECTION FOUND LT FLOOR MEMBRANE DISTORTED AND CRACKED AT STA 627 TO 657. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WEB WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-3, AND 51-30-2.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 908)

INSPECTION FOUND RIGHT OUTBOARD SEAT TRACK CORRODED AT STA 908. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.

ATA 5320

Part: CUSP — CORRODED (BS 980-996)

INSPECTION FOUND CUSP CORRODED AT STA 980-996, RT SIDE. THE CORRODED SECTION OF CUSP WAS CUT OUT IAW SRM 53-05, FIGURE 25. A REPAIR CUSP WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 25 AND 51-30-2.

ATA 5320

Part: WEB — CORRODED (BS 218)

INSPECTION FOUND CORROSION AROUND RIVETS IN WEB AT STA 218, STRINGER 18R. THE WEB WAS REMOVED, A REPAIR WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30.

ATA 5321

Part: FLOOR — CRACKED (CABIN)

INSPECTION FOUND FLOORBOARD NR 82 HAT SECTIONS WORN THROUGH AND CRACKED. A FLOOR PANEL AND HAT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-2.

ATA 5321

Part: FLOOR — CORRODED (BS 980-996)

INSPECTION FOUND LT AFT LAV FLOOR WEB CORRODED AT BS 980 TO 996, LBL 18. THE FLOOR WEB WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 51-30-1.

ATA 5315

Part: FLOORBEAM — GOUGED (BS 968)

INSPECTION FOUND FLOORBEAM GOUGED AT STA 968. THE GOUGED SECTION OF FLOORBEAM WAS CUT OUT. AN L-ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A, 53-05, 51-10-3, 51-30-2, AND 51-20-0.

ATA 5320

Part: SUPPORT — CRACKED (BS 332)

INSPECTION FOUND THREE .5 INCH CRACKS IN FORWARD PIT RT FLOOR SUPPORT AT STA 332 ABOVE LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.

ATA 5320

Part: SUPPORT — CRACKED (BS 351)

INSPECTION FOUND FLOOR SUPPORT CRACKED IN FORWARD PIT AT STA 351 ABOVE LONGERON 26R. THE FLOOR SUPPORT WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263 AND SRM 51-10-3.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 240)

INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 240. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 53-05, FIGURE 4F.

ATA 5210

Part: ANGLE — CRACKED (PAX DOOR)

INSPECTION FOUND A 2 INCH CRACK IN L-ANGLE ON AFT ENTRY DOOR. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-10-4, AND 51-30-2.

ATA 5311

Part: FRAME — CRACKED (BS 1104)

INSPECTION FOUND A .25 INCH CRACK AT FASTENER IN FRAME AT STA 1104, LONGERON 3R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

ATA 5712

Part: RIB — CRACKED (RT WING)

INSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE RIB. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-00-00.

ATA 5280

Part: HINGE — CRACKED (RT MLG DOOR)

INSPECTION FOUND A .375 INCH CRACK IN AFT LOBE OF RT MLG DOOR UPPER HINGE. A NEW HINGE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-4.

ATA 5320

Part: CHANNEL — CRACKED (RT NLG)

INSPECTION FOUND A 1 INCH CRACK IN AFT CHANNEL OF RT NLG WHEEL WELL FORWARD FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-10-6.

ATA 5321

Part: FLOORBOARD — DELAMINATED (BS 200-244)

INSPECTION FOUND FLOORBOARD AT STA 200 TO 244 DELAMINATING. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.

ATA 5720

Part: SUPPORT — CRACKED (WS 280)

INSPECTION FOUND LT WING STA 280 FLAP LEADING EDGE SUPPORT CAP CRACKED AND CORRODED. THE SUPPORT CAP WAS REMOVED, A NEW SUPPORT CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-2.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 996)

INSPECTION FOUND LT FLOORBEAM AT BS 996, LBL 18 CORRODED. AN UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0 AND 51-10-1.

ATA 5753

Part: BRACKET — CRACKED (LT TE FLAP)

INSPECTION FOUND A CRACK WITH CORROSION IN LT WING FLAP XRS 270 LEADING EDGE SUPPORT BRACKET CAP. THE SUPPORT BRACKET CAP WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (BS 465-579)

INSPECTION FOUND CRACKS AT SCREW HOLES OF FLOORBOARD NR 51, STA 465 TO 579 AND FLOORBOARD NR 40, STA 578 WITH SCREWS PULLING THROUGH. NEW FLOORBOARDS WERE FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 1, 51-20-0, 51-30-2, 51-10-2, 51-10-3, AND 51-70-2.

ATA 5320

Part: WEB — CRACKED (BS 589)

INSPECTION FOUND A 2 INCH CRACK IN WEB AT STA 589 ON LT SIDE OF FUSELAGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-2, AND 53-10-2.

ATA 5712

Part: RIB — CRACKED (WS 280)

INSPECTION FOUND A 1.5 INCH CRACK WITH CORROSION ON LT WING STA XRS 280 FLAP RIB ON LEADING EDGE PANEL FLANGE. THE RIB WAS REMOVED FROM SUPPORT CAP, A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.

ATA 5315

Part: FLOORBEAM — GOUGED (BS 917)

INSPECTION FOUND AFT PIT UPPER FLOORBEAM GOUGED AT STA 917. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 86, 51-30-1, AND 51-30-2.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 260)

INSPECTION FOUND LT OUTBOARD SEAT TRACK CORRODED AT STA 260. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT, A NEW REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F.

ATA 5321

Part: FLOORBOARD — PUNCTURED (CABIN)

INSPECTION FOUND A HOLE IN FLOORBOARD PANEL NR 71. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, PAGES 15-16, AND 51-30-2, PAGES 1-30.

ATA 5320

Part: STRAP — CORRODED (BS 851-870)

INSPECTION FOUND STRAP CORRODED BETWEEN LONGERONS 27L AND 28L AT STA 851 TO 870. THE STRAP WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-2A, 51-10-04, 51-10-3, 51-30-2, AND 53-01.

ATA 5313

Part: LONGERON — GOUGED (BS 207)

INSPECTION FOUND LONGERON 5L GOUGED AT STA 207. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND CRACKS IN LT FLOORBOARD NR 58. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-70-1, AND 51-70-3, PAGE 1 AND 2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND .5 INCH CRACKS AT SCREW HOLES OF FLOORBOARD NR 51. REPAIRED IAW SRM 53-01, FIGURE 2, PAGE 3.

ATA 5320

Part: SUPPORT — CRACKED (BS 351)

INSPECTION FOUND A .75 INCH CRACK IN FORWARD PIT RT FLOOR SUPPORT FRAME ABOVE LONGERON 9R AT STA 351. THE CRACKED SECTION OF STANDOFF FLOOR SUPPORT WAS REMOVED. A STANDOFF FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.

ATA 5320

Part: STIFFENER — CRACKED (BS 313)

INSPECTION FOUND CABIN FLOORBOARD STIFFENER CRACKED AND BENT AT FLOOR SUPPORT BS 313, RT CENTER OF CEILING. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND NEW SKIN WAS INSTALLED IAW SRM 53-05, 51-30-2, AND 51-70-2.

ATA 5720

Part: DOUBLER — CRACKED (BS 438)

INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT STA 438. THE ANGLE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.

ATA 5320

Part: ANGLE — CORRODED (BS 996)

INSPECTION FOUND L-ANGLE CORRODED AT STA 996, RBL 28. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10, 51-10-2, 51-30-1, AND 51-10-3.

ATA 5753

Part: RIB — CRACKED (WS 270)

INSPECTION FOUND A 2 INCH CRACK IN LT WING FLAP RIB AT WS XRS 270 WITH CORROSION AT INBOARD END OF RIB. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.

ATA 5321

Part: FLOORBOARD — CORRODED (BS 130)

INSPECTION FOUND CO-PILOT'S FLOORBOARD CORRODED AT STA 130, RBL 34 TO RBL 50. THE FLOORBOARD AND SKIN WERE REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, FIGURE 2F, 51-30-2, 51-10-2, 51-10-4, 51-10-3 AND MM 53-20-1.

ATA 5313

Part: END CAP — CRACKED (BS 996)

INSPECTION FOUND A 1 INCH CRACK IN END CAP OF LONGERON 19L AT AFT PRESSURE BULKHEAD STA 996. THE END CAP WAS REMOVED AND REPLACED IAW SRM 51-10-4.

ATA 5321

Part: FLOORPANEL — CORRODED (CABIN)

INSPECTION FOUND COCKPIT FLOORBOARD PANEL NR 12 CORRODED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 53-05, PAGE 1.

ATA 5520

Part: FAIRING — CRACKED (RT ELEVATOR)

INSPECTION FOUND A 1 INCH CRACK IN INBOARD AFT CORNER OF RT ELEVATOR GEAR TAB CONTROL ROD FAIRING. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-2, 51-30-2, AND 51-10-3.

ATA 5414

Part: PANEL — CRACKED (NR 1 ENG PYLON)

INSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.

ATA 5312

Part: BULKHEAD BEAM — CRACKED (BS 996)

INSPECTION FOUND A .5 INCH CRACK IN HORIZONTAL BEAM OF RT AFT LAV AFT PRESSURE BULKHEAD. THE CRACK WAS LOCATED JUST AFT OF STA 996, 62 INCHES UP FROM THE FLOOR AT THE OUTBOARD CORNER. THE CRACK WAS STOP DRILLED IAW SRM 53-01. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 6, 53-10-3, 51-30-4, AND 51-20-0.

ATA 5320

Part: FITTING — CRACKED (MLG DOORWAY)

INSPECTION FOUND A 2 INCH CRACK IN SUPPORT FITTING ON LT AFT END MLG DOOR CUTOUT. THE CRACK WAS TRIMMED OUT IAW SRM 53-05, FIGURE 71. A REPAIR WAS FABRICATED AND INSTALLED SRM 53-05, FIGURE 71 AND 51-10-3.

ATA 5320

Part: ANGLE — CORRODED (L1 DOORWAY)

INSPECTION FOUND L-1 DOOR SILL ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5.

ATA 5320

Part: STRAP — CORRODED (BS 945-996)

INSPECTION FOUND AFT CARGO PIT RT SIDEWALL PANEL STRAP CORRODED AT STA 945 TO 996. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-10-2.

ATA 5330

Part: SKIN — CRACKED (BS 1121)

INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 1121, FIFTEEN INCHES BELOW RT NEGATIVE PRESSURE LOUVERS. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.

ATA 5330

Part: SKIN — CRACKED (APU COMPT)

INSPECTION FOUND A CRACK IN SKIN OF APU COMPARTMENT AT LT SIDE FORWARD BELOW INSPECTION PANEL ACCESS. THE CRACK WAS STOP DRILLED IAW SRM 51-10-44. TWO REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-01.

ATA 5320

Part: ANGLE — CORRODED (BS 160)

INSPECTION FOUND CORROSION ON ATTACH ANGLE BELOW GENERATOR AT STA 160. THE CORRODED SECTIONS OF ANGLE WERE REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-01, FIGURE 2, 51-10-3, AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (CABIN)

INSPECTION FOUND FLOORBOARD NR 71 WITH THREE EACH BLOWN OUT HOLES AND ONE CRACKED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED ON FLOORBOARD OVER BLOWN OUT HOLES AND CRACK IAW SRM 53-01, FIGURE 2, 51-10-3, PAGE 15 AND 16, 51-10-4, AND 51-30-2, PAGES 1-36.

ATA 5350

Part: FILLET — CORRODED (BS 756-832)

INSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.

ATA 5530

Part: FAIRING — CRACKED (VERT STAB)

INSPECTION FOUND TWO 1 INCH CRACKS IN RADIUS OF ATTACH FLANGE ON LT VERTICAL STABILIZER LOWER FAIRING. THE CRACKS WERE STOP DRILLED IAW SRM 51-01. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.

ATA 5320

Part: WEB — CRACKED (BS 617)

INSPECTION FOUND CABIN INTERIOR WEB CRACKED AT FS 617, RBL 50 TO 55. THE CUSP WEB WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 53-01, FIGURE 9.

ATA 5330

Part: SKIN — CRACKED (BS 1104)

INSPECTION FOUND THREE 1 INCH CRACKS AT FASTENER HOLES IN FUSELAGE SKIN AT STA Y= 1104, X= 30. THE CRACKS WERE STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.

ATA 5321

Part: FLOORBOARD — CORRODED (BS 15)

INSPECTION FOUND COCKPIT FLOORBOARD CORRODED ON PILOT'S SIDE IN CORNER FORWARD OF E AND E COMPARTMENT ACCESS DOOR AT STA 15L. THE FLOOR PANELS WERE REMOVED IAW SRM 51-30-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2.

ATA 5321

Part: FLOORBOARD — PUNCTURED (CABIN)

INSPECTION FOUND SURFACE SKIN OF CABIN FLOORBOARD PANEL NR 77 PUNCTURED. A DOUBLER, HAT SECTION, AND REPAIR PANELS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-70-2, 51-10-3, AND 51-20.

ATA 5320

Part: FITTING — CRACKED (BS 897)

INSPECTION FOUND A .5 INCH CRACK IN FITTING AT STA 897 BETWEEN LONGERONS 27L AND 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-10-3.

ATA 5720

Part: ANGLE — CRACKED (LT WING)

INSPECTION FOUND A 1 CRACK IN ANGLE OF LT WING FORWARD SIDE AT WING ROOT, WHERE FORWARD SPAR GOES INTO FUSELAGE. THE SEAL BRACKET AND ANGLE AT WING ROOT WERE REMOVED IAW SRM 51-30-3. AN ANGLE WAS FABRICATED IAW SRM 51-10-4. THE ANGLE AND SEAL BRACKET WERE INSTALLED IAW SRM 51-30-3 AND 51-30-2.

ATA 5280

Part: CHANNEL — CRACKED (RT MLG DOOR)

INSPECTION FOUND A 1 CRACK IN Z-CHANNEL OF RT MLG DOOR FORWARD INNER CORNER. THE CRACKED AREA OF CHANNEL WAS CUT OUT IAW SRM 52-05, FIGURE 14. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 14.

ATA 5320

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 CRACK IN AFT CARGO DOOR OVERHEAD PAN AT STA 929. THE CRACK WAS STOP DRILLED IAW SRM 53-01. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 53-01.

ATA 5321

Part: FLOORBOARD — CORRODED (BS 389)

INSPECTION FOUND FLOORBOARD NR 36 HAD CORROSION AT FOUR SCREW HOLES ON END OF PANEL, STA 389. THE FLOORBOARD WAS REPAIRED IAW SRM 53-01, FIGURE 1, SHEET 2, SRM 53-21-0, AND 51-30-2.

ATA 5321

Part: FLOORBOARD — CRACKED (BS 756-832)

INSPECTION FOUND FLOORBOARD NR 72 FORWARD LEADING EDGE AND AFT SCREW HOLES CRACKED AND WORN BETWEEN STA 756 AND 832. TWO EACH REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-21, FIGURE 4, 53-01, FIGURE 2, SHEET 3, 51-10-3, AND 51-30-2.

ATA 5230

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND TWO CRACKS AT AFT END OF BEAM NR 4 OF AFT CARGO COMPARTMENT DOOR OUTER PAN. ONE CRACK WAS .3 LONG IN RADIUS AND THE OTHER WAS .7 LONG AT FASTENER. BOTH CRACKS WERE STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5261-C-01000.

ATA 5312

Part: BULKHEAD ANGLE — CRACKED (BS 218)

INSPECTION FOUND A 2 CRACK IN Z-ANGLE AT LT FORWARD PIT BULKHEAD STA 218, LBL 17. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 10.

ATA 5330

Part: SKIN — CRACKED (BS 695)

INSPECTION FOUND TWO .0625 INCH CRACKS AT RIVETS IN LT FUSELAGE FORWARD NOSE SECTION EXTERIOR SKIN, STA 695. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5330-02413 AND DOUGLAS DRAWING SR09530239.

ATA 5320

Part: SUPPORT — CRACKED (BS 228)

INSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT OF LT FORWARD CARGO COMPARTMENT, STA 228. THE FLOOR SUPPORT WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-10-3, AND 51-30-2.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 980)

INSPECTION FOUND FLOORBEAM CORRODED AT BS 980, RBL 18. THE L-ANGLE, FILLER, AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4A.

ATA 5350

Part: BRACKET — CRACKED (BS 579)

INSPECTION FOUND A 2 INCH CRACK IN FORWARD WING TO FUSELAGE FAIRING ATTACH BRACKET AT STA 579. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-3, AND 51-30-5.

ATA 5753

Part: BRACKET — CRACKED (FLAP FAIRING)

INSPECTION FOUND A 3 INCH CRACK AT OUTBOARD FORWARD RADIUS OF RT WING NR 2 FORWARD FLAP HINGE FAIRING RETAINING BRACKET. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-4, 51-10-2, AND 51-30-2.

ATA 5313

Part: LONGERON — CRACKED (BS 140)

INSPECTION FOUND A 3 INCH CRACK IN LONGERON 3L AT STA 140. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 17.

ATA 5330

Part: PANEL — CRACKED (FUSELAGE)

INSPECTION FOUND A 3 CRACK IN FORWARD ADF SENSE ANTENNA PANEL. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2.

ATA 5320

Part: SHEAR TIE — CRACKED (BS 965)

INSPECTION FOUND A .25 INCH CRACK IN SHEAR TIE AT FS 965 BETWEEN STRINGER 13R AND 12R, FORWARD OF AFT LAV. THE CRACK WAS STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 28.

ATA 5720

Part: BRACKET — CRACKED (RT WING LE)

INSPECTION FOUND A .5 INCH CRACK IN BRACKET OF RT WING LEADING EDGE PANEL FRAME. THE BRACKET WAS REMOVED, A NEW ANGLE BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.

ATA 5313

Part: LONGERON — CRACKED (BS 160)

INSPECTION FOUND A 2 INCH CRACK IN LONGERON 2L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 1, 51-30-2, AND 51-30-5.

ATA 5311

Part: FRAME — CRACKED (BS 180)

INSPECTION FOUND A 4.5 INCH CRACK IN FRAME AT STA 180, LONGERON 5L AND 6L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 36.

ATA 5320

Part: SUPPORT — CRACKED (BS 256)

INSPECTION FOUND A 2.75 INCH CRACK IN LT FORWARD PIT FLOOR SUPPORT AT FS 256, LBL 35. THE CRACK WAS STOP DRILLED AND AN L-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263, SRM 51-30-2 AND 51-10-3.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 610-620)

INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 610 TO 620. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED, A NEW SECTION OF TRACK, SPLICE AND PLATE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.

ATA 5320

Part: ANGLE — CRACKED (BS 237)

INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD PIT RT INTERCOSTAL FRAME L-ANGLE AT FS 237, RBL 17. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-3.

ATA 5313

Part: LONGERON — CRACKED (BS 955.091)

INSPECTION FOUND A 11.25 INCH CRACK IN LONGERON 14R AT STA 955.091. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 2. LONGERON AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-02, FIGURE 18, 51-10-3, 51-30-2, FIGURE 8, AND 51-30-5.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 470-456)

INSPECTION FOUND RT INBOARD CABIN SEAT TRACK CORRODED AT STA 470 TO 456. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, AND 53-20-1, PAGE 205.

ATA 5320

Part: WEB — CRACKED (BS 598)

INSPECTION FOUND CABIN INTERIOR WEB CRACKED AT BS 598, RBL 55. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.

ATA 5320

Part: DOUBLER — CRACKED (BS 598)

INSPECTION FOUND A 4 INCH CRACK IN CABIN INTERIOR DOUBLER AT BS 598, RBL 55. THE DOUBLER WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30.

ATA 5311

Part: FRAME — CRACKED (BS 446)

INSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT FRAME AT STA 446, STRINGER 29R. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.

ATA 5313

Part: LONGERON — CRACKED (BS 955)

INSPECTION FOUND A CRACK OUT OF UPPER FASTENER HOLE BEHIND ANGLE BRACKET IN LONGERON 17L AT FS 955. THE ANGLE BRACKET WAS ALSO CRACKED. THE LONGERON AND ANGLE BRACKET WERE REMOVED. A NEW LONGERON AND BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-1, 51-10-4, 51-10-3, 51-30-2, AND 51-30-1.

ATA 5313

Part: LONGERON — CRACKED (BS 955/945)

INSPECTION FOUND LONGERON 17R AT FS 955.091 AND FS 945. THE CRACKED SECTIONS OF LONGERON WERE REMOVED IAW SRM 51-30-2. NEW SECTIONS OF LONGERON WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5.

ATA 5320

Part: ANGLE — CRACKED (BS 680)

INSPECTION FOUND A .5 CRACK IN FLOOR PANEL ATTACH ANGLE AT FS 680, LBL 4. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.

ATA 5532

Part: SKIN — CRACKED (VERTICAL FIN)

INSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.

ATA 5320

Part: DOUBLER — CRACKED (RT WING/BODY)

INSPECTION FOUND A 3.75 CRACK COMING FROM SCREW HOLE IN RT WING UPPER WING TO BODY FAIRING BONDED DOUBLER. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.

ATA 5320

Part: ANGLE — CRACKED (BS 658)

INSPECTION FOUND A .5 INCH CRACK IN VERTICAL ATTACH ANGLE AT FS 658, BL 45R. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-3, AND 51-30-5.

ATA 5321

Part: FLOOR — CRACKED (CABIN)

INSPECTION FOUND SEVERAL CRACKS IN RT NR 61 FLOORBOARD. A FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-10-3.

ATA 5311

Part: FRAME — CRACKED (BS 466)

INSPECTION FOUND CRACKS IN FORWARD PIT FRAME AT FS 466, STRINGER 29L. THE CRACKS WERE STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.

ATA 5720

Part: DOUBLER — CRACKED (WS 444.5)

INSPECTION FOUND A 1.5 CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT WS 444.5. THE DOUBLER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.

ATA 3260

Part: DNLOCK SWITCH — INOPERATIVE (LT MLG)

WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH, THE LEFT MLG GREEN LIGHT DID NOT ILLUMINATE. THE GEAR WAS CYCLED SEVERAL TIMES, BUT THE LIGHT DID NOT COME ON. THE EMERGENCY GEAR EXTENSION HANDLE WAS PULLED BUT THE LEVER WAS JAMMED. THE LEFT MLG GREEN LIGHT FINALLY CAME ON. A TOWER FLY-BY WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT MLG DOWNLOCK SWITCH IAW MM 32-60-1. THE GEAR WAS SWUNG AND ALL INDICATIONS WERE GOOD. OPERATION OF THE ALTERNATE EXTENSION CONTROL LEVER WAS CHECKED IAW MM 32-31-2 AND OPERATION CHECKED GOOD WITH THE GEAR EXTENDING AND LOCKING INTO POSITION.