N6857X

ATA 7110

Part: STIFFENER — CRACKED (NR 1 ENG COWL)

INSPECTION FOUND A 2 INCH CRACK IN NR 1 ENGINE NOSE COWL VERTICAL STIFFENER L-ANGLE. THE CRACKED ANGLE WAS REMOVED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01 AND 51-31-01.

ATA 5414

Part: SKIN — CRACKED (NR 2 PYLON)

INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT LEFT FAIRING SKIN AT AFT CORE COWL HINGE POINT. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, FIGURE 1 AND 54-00-01.

ATA 5730

Part: SKIN — CORRODED (LT WING)

INSPECTION FOUND LT WING INBOARD FLAP PANEL NR 541BB SKIN CORRODED. THE TOP SKIN OF PANEL WAS REPLACED IAW SRM 51-70-00.

ATA 5400

Part: SUPPORT — CRACKED (NR 2 PYLON)

INSPECTION FOUND A 6 INCH CRACK IN CHANNEL SUPPORT OF NR 2 ENGINE PYLON AFT FAIRING. THE CHANNEL SUPPORT WAS REMOVED, A REPLACEMENT CHANNEL SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 54-12-02.

ATA 5753

Part: SKIN — DENTED (LT TE FLAP VANE)

INSPECTION FOUND THREE DENTS IN MID SECTION OF LT INBOARD FLAP VANE LOWER SURFACE. THE DENTED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-71-00, FIGURES 32, 33, AND 35.

ATA 5350

Part: TAIL CONE — DENTED (BS 2265)

INSPECTION FOUND A DENT ON RT SIDE OF TAIL CONE AT STA 2265. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, FIGURE 1 AND 53-00-01.

ATA 5320

Part: JAMB — CORRODED (CARGO COMPT)

DURING D-CHECK, FOUND CORROSION BEYOND LIMITS AT FWD CARGO DOOR JAM. REPAIRED AND REPLACED PER SRM 53-05 FIGURE 44, 51-30-01.

ATA 5320

Part: ANGLE — CORRODED (CENTER MLG WW)

INSPECTION FOUND Z-ANGLE IN CENTER WHEEL WELL ON RT SIDE BELOW TRUNNION CORRODED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-14-01, FIGURE 2 AND 53-31-01.

ATA 5320

Part: ANGLE — CORRODED (CENTER MLG WW)

INSPECTION FOUND DOUBLER SPLICE ANGLE AT CENTER WHEEL WELL RIGHT TRUNNION CORRODED. A DOUBLER ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-14-01, FIGURE 2 AND 51-31-02.

ATA 5330

Part: PANEL — CORRODED (BS 1701-1721)

INSPECTION FOUND CENTER CARGO COMPARTMENT BILGE PANEL CORRODED AT FS 1701 TO 1721. A NEW BILGE PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-15-01 AND 51-21-01.

ATA 5330

Part: SKIN — DENTED (BS 775)

DURING D-CHECK INSPECTION, FOUND DENT/GOUGE AT R-2 DOOR FWD SIDE OF SCUFF PLATE FS 775 29R. REWORKED DENT, FABRICATED AND INSTALLED INTERNAL DOUBLER PER SRM 53-20-00 FIGURE 13 SHEET 14.

ATA 5720

Part: WING TIP — CRACKED (LT WING)

DURING D-CHECK INSPECTION, FOUND CRACK .5 LT WING TIP FASTENER FWD OF AFT NAV LIGHT. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 57-31-01.

ATA 5320

Part: ANGLE — CORRODED (BS 939)

DURING D-CHECK INSPECTION, FOUND FWD CARGO COMPT STA 939 LONG 51 RT TO 52 L ANGLE CORRODED. REPAIR/REPLACED PER SRM 53-30-00 FIG 5 51-21-01 AND 51-31-01.

ATA 5210

Part: WEB — CRACKED (L3 DOOR)

DURING D-CHECK INSPECTION, FOUND 1.5 CRACK AT THE L-3 DOOR INNER WEB L-27L. STOP DRILLED AND FABRICATED REPAIR PER SRM 53-00-01, 51-31-01, 51-33-01.

ATA 5512

Part: SKIN — DENTED (HORIZ STAB)

DURING D-INSPECTION, FOUND A DENT LT UPPER SURFACE HORIZ STAB STATION 54 L/E .125 DEEP 1.5 LONG .3125 WIDE. REPAIRED PER SRM 55-00-01 FIGURE 3.

ATA 5320

Part: SUPPORT — CORRODED (BS 1909)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1909, LBL 62 TO 87. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-00 AND 51-31-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1965)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1965, RBL 80. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01, 53-16-01, AND 51-30-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1885)

INSPECTION FOUND ZONE 290 FLOOR SUPPORT CORRODED AROUND CLIP NUTS AT STA 1885. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-16-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1918-2007)

INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1918 TO 2007, LBL 20. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01 AND 51-31-01.

ATA 5320

Part: ANGLE — CRACKED (BS 1841)

INSPECTION FOUND A 2 INCH CRACK IN FLOORBOARD SUPPORT ANGLE AT STA 1841, RBL 50. THE SUPPORT WAS REMOVED, A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 53-16-01, AND 51-21-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1966-1982)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1966 TO 1982, LBL 78. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, FIGURE 10D AND 51-21-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1966-1982)

CORROSION AT FLOOR SUPPORT FS 1966 TO 1982 LBL 78. FABRICATED AND INSTALLED FLOOR SUPPORT IN ACCORDANCE WITH SRM 53-16-01 FIG 10D AND 51-21-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 1950-2006)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1950 TO 2006, RBL 19. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01 AND 51-21-01.

ATA 5320

Part: FLOOR — CORRODED (BS 1950-2006)

CORROSION AT FLOOR SUPPORT FS 1950 TO 2006 RBL 19. FABRICATED AND INSTALLED FLOOR SUPPORT IN ACCORDANCE WITH SRM 53-16-01 AND 51-21-01.

ATA 5320

Part: SUPPORT — CORRODED (BS 455)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 455, RBL 2 TO 18, A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-11-01 AND 51-31-01.

ATA 5330

Part: SKIN — DENTED (BS 475)

DURING D-CHECK INSPECTION, FOUND DENT IN FS AT FS 475 ABOVE RT NLG FWD DOOR. SKIN DENT FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 4.

ATA 5320

Part: ANGLE — CRACKED (BS 1521)

INSPECTION FOUND A .5 INCH CRACK IN L-ANGLE AT LEFT WHEEL WELL CUTOUT STA 1521. THE CRACK WAS STOP DRILLED, A STACK ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 2, VOL 1.

ATA 5347

Part: SEAT TRACK — DAMAGED (BS 495-520)

DAMAGED SEAT TRACK FS 495 TO 520 LBL 8.5. FABRICATED AND INSTALLED SEAT TRACK IN ACCORDANCE WITH SRM 53-70-00 FIG 1, 53-42-01, 51-31-01, AND EA 2520-03222.