N12510

ATA 5248

Part: RELEASE SYSTEM — WORN (TAIL CONE) · airframe 54,558 hrs · 54,566 cycles

COMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05

ATA 5210

Part: WEB — CRACKED (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

AFT ENTRY DOOR RT WEB IS CRACKED. FABBED AND INSTALLED NEW WEB.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FS 990) · airframe 54,411 hrs · 42,174 cycles

CRACKED CEILING SUPPORT FS 990 RBL 20. INSTALLED REPAIR DOUBLERS.

ATA 5320

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AREA FS 160 LBL 54 TO RBL 54. SUPPORT LIKE PART INSTALLED.

ATA 5315

Part: FLOORBEAM — CHAFED (CABIN) · airframe 54,411 hrs · 42,174 cycles

CHAFING ON FLOOR BOARD SUPPORT STATION 460 BL 0 TO XL22 BEAM. BLENDED, TREATED AND PRIMED AREA.

ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CHAFED AND WORN FLOORBEAM STATION 541. BLENDED, TREATED AND PRIMED.

ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A 22 INCH CHAFED AREA AT FS 484 FLOORBEAM. INSTALLED FLOORBEAM REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING ON FLOOR SUPPORT. BLENDED TREATED AND PRIMED.

ATA 5320

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACK ON FLOOR BOARD SUPPORT BRACKET STATION 560. FABBED AND REPLACED BRACKET.

ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

VARIOUS CORRODED AREAS AND PUNCTURES, WEB. FABBED AND REPLACED WEB.

ATA 5347

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 175 INCH STRIP OF CORROSION AFT CARGO RT TRACK FS 775 - 900.

ATA 5320

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 1 INCH WIDE AREA OF CORROSION AROUND CIR FS 370 FWD CARGO FWD DOOR JAMB PANEL. FABBED NEW PANEL.

ATA 5320

Part: BEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

REPAIR DOUBLER ON BEAM CHAFED AT STATION 917 BL 0 LOWER FLANGE AT BEAM. REPLACED DOUBLER.

ATA 5313

Part: LONGERON — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGE AT LONGERON SPLICE 29 LT AT STATION 160. INSTALLED LONGERON SPLICE.

ATA 5320

Part: INTERCOSTAL — BENT (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

INTERCOSTAL BENT STATION 351 - 370 LONG 29. FABBED NEW INTERCOSTAL.

ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACK AT STATION 1155 RT SIDE 4 OCLOCK POSITION. INSTALLED DOUBLER REPAIR.

ATA 5313

Part: LONGERON — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACK AT FS 579 LONG 30. REPLACED LONGERON WITH IDENTICAL PART.

ATA 5321

Part: WEB — CRACKED (CABIN FLOOR) · airframe 54,411 hrs · 42,174 cycles

CRACK IN FLOOR WEB STATION 160 RBL 54 FLOOR WEB. FABBED NEW WEB.

ATA 5310

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

TWO CRACKS AFT ENTRY DOOR JAMB UPPER LT CORNER. SPLICED IN NEW SECTION.

ATA 5311

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

MISDRILLED HOLE FS 389 LONG 29 LT. FILLER AND DOUBLER REPAIR.

ATA 5210

Part: DOOR FRAME — GOUGED (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

GOUGE IN RADIUS ON L1 DOOR INTERIOR FRAME STACKED ANGLE REPAIR.

ATA 5230

Part: BEAM — CRACKED (AFT CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACK IN AFT PIT DOOR NR 4 BEAM FWD BEAM END. REPLACED WITH IDENTICAL PART.

ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED INTERCOSTAL STATION 900 BETWEEN LONGERON 28 RT. FABBED AND INSTALLED NEW INTERCOSTAL.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGE 1 X .006 INCH DEEP FUSELAGE SKIN STATION 218 LONGERON 17 LT. BLENDED, TREATED AND PRIMED.

ATA 5315

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FLOORBEAM UPPER FLANGE DOUBLE DRILLED AT FUS STA 160 RBL 50. REAMED OUT NUT PLATE HOLE TO NEXT SIZE.

ATA 5320

Part: WEB — PUNCTURED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

PUNCTURE AT FS 150 LBL 10. PLUGGED PUNCTURE.

ATA 5320

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGE .25 INCH DIA X .033 INCH DEEP FS 245 LONG 2 RT ON DOUBLER. FABBED AND INSTALLED NEW DOUBLER.

ATA 5210

Part: PAN — DAMAGED (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

L1 DOOR SILL PAN GOUGED, DENTED AND PUNCTURED. REPLACED WITH IDENTICAL PART.

ATA 5321

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CRACK PANEL 49. INSTALLED FILLER AND DOUBLER.

ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED INTERCOSTAL LONGERON 28 RT BETWEEN STATION 897 - 937. FABBED AND INSTALLED NEW INTERCOSTAL.

ATA 5320

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

BENT INTERCOSTAL AND GUSSETT STATION 560 LT TO 579 LT BL 28 LT AND 27 LT. REMOVED, REPAIRED AND INSTALLED INTERCOSTAL.

ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CHAFING STATION 405 BL 0 TO 22 LT. INSTALLED ANGLE REPAIR.

ATA 5320

Part: STRUCTURE — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

134 INCHES OF TRIM BENT AND CORRODED FS 427 FWD CARGO COMP CEILING. FABBED REPLACEMENT TRIM.

ATA 5753

Part: COVER — GOUGED (RT FLAP TRACK) · airframe 54,411 hrs · 42,174 cycles

A .063 INCH GOUGE RT I/B FLAP TRACK FAIRING COVER PLATE. FILL WELDED COVER PLATE.

ATA 5320

Part: DOUBLER — CRACKED (PRESS BULKHEAD) · airframe 54,411 hrs · 42,174 cycles

CRACK AFT PRESSURE BULKHEAD -11 DOUBLER. INSTALLED DOUBLER AND FILLER.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FUSELAGE SKIN DENTED AND CREASED AT STATION 1076. INSTALLED FILLER AND DOUBLER ON INNER WALL.

ATA 5320

Part: DOUBLER — CHAFED (FLOOR PAN) · airframe 54,411 hrs · 42,174 cycles

CHAFED REPAIR AREA FS 200 - 218 LBL 10 ON DOUBLER. FABBED AND INSTALLED FLOOR PAN.

ATA 5320

Part: WEB — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A .25 INCH GOUGE IN LIP OF LIGHTNING HOLE WEB AT STATION 935 AND LONGERON 28 LT. INSTALLED DOUBLER.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DAMAGE AFT PIT DOOR STATION 908 FUSELAGE SKIN. BLENDED, TREATED AND PRIMED.

ATA 5280

Part: DOOR — CHAFED (RT MLG) · airframe 54,411 hrs · 42,174 cycles

CHAFED AREA ON RT STRUT DOOR. BLENDED, CHAFED AREA, TREATED AND PRIMED.

ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 27 INCH AREA OF CORROSION FS 200 TO 227 RBL 44 SEAT TRACK. SPLICED REPAIR.

ATA 5320

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED HAT CHANNEL ON FLOORBOARD. INSTALLED STACKED ANGLE REPAIR.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

TWENTY SQ INCHES OF CORROSION FLOOR PNL 47. FABBED FILLERS AND DOUBLERS.

ATA 5320

Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING STATION 680 FLOOR SUPPORT. BLENDED CHAFED AREAS.

ATA 5230

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACK ON AFT CARGO DOOR BEAM NR 2 AFT END CRACKED ON FITTING. REPLACED WITH NEW IDENTICAL PART.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

TWO INCH AREA OF CORROSION ON FRAME. ROLLED Z-FRAME FLANGE REPAIR.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TWO GOUGES AT FS 718 LONGERON 18 RT. BLENDED OUT GOUGES.

ATA 3830

Part: FITTING — CORRODED (AFT LAVATORY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED LAV SERVICE FITTING RT AFT ALV FLOOR PAN. REPLACED WITH IDENTICAL PART.

ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AN 8 INCH AREA OF CORROSION FS 996 BETWEEN LONGERON 27 AND 28 LEFT. FABBED AND INSTALLED INTERCOSTAL.

ATA 5230

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACKED PAN FWD CARGO DOOR. REPLACED WITH NEW IDENTICAL PART.

ATA 5320

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 1 X 35 INCH CORRODED AREA FS 165 TO 200 LBL 54 THRESHOLD. FABBED NEW THRESHOLD.

ATA 5347

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A 152 INCH SECTION WITH ELONGATED HOLES FWD CARGO FS 218 - 370 LT TRACK. FABBED NEW TRACK.

ATA 5720

Part: STRUCTURE — CHAFED (WING BUTTE DOOR) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING RT WING BUTTE DOOR AT XRS 145 AND 276. INSTALLED 3 DOUBLERS AND FILLERS.

ATA 5753

Part: VANE — GOUGED (RT TE FLAP) · airframe 54,411 hrs · 42,174 cycles

GOUGE RIGHT /IB FLAP VANE. BLENDED, TREATED AND PRIMED.

ATA 5320

Part: STIFFENER — CHAFED (AC BAY) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING LT SIDE OF AC BAY STIFFENER. BLENDED REPAIR.

ATA 5531

Part: SKIN — CHAFED (VERTICAL STAB) · airframe 54,411 hrs · 42,174 cycles

CHAFING ON SKIN LT VERTICAL STAB WHERE VERT L/E MEETS HORTIZONTAL L/E. BLENDED, TREATED AND PRIMED.

ATA 5530

Part: FAIRING — CHAFED (VERTICAL STAB) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING VERTICAL STAB TIP CAP FAIRING LT END. BLENDED, TREATED AND PRIMED.

ATA 5510

Part: FAIRING — CHAFED (HORIZONTAL STAB) · airframe 54,411 hrs · 42,174 cycles

LT HORIZONTAL STAB UPPER FAIRING CHAFED AFT END. REPAIRED PER DRAWING FVT DWG 55-00536-4.

ATA 5521

Part: SKIN — GOUGED (ELEVATOR LE) · airframe 54,411 hrs · 42,174 cycles

GOUGED AREA RT ELEVATOR L/E.

ATA 5541

Part: SKIN — DENTED (RUDDER) · airframe 54,411 hrs · 42,174 cycles

DENT RT SIDE OF RUDDER STATION XR 97, 36 INCHES FROM TRAILING EDGE .018 X .170 INCHES LONG. INSTALLED DOUBLER REPAIR.

ATA 5230

Part: SKIN — DAMAGED (FWD CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

PUNCTURES AND CRACKS IN A 52 X 53 INCH AREA ON FWD CARGO BARRIER DOOR I/B SKIN. REPLACED SKIN.

ATA 5320

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

APPROX 62 INCHES OF CORROSION AFT CARGO COMP CEILING TRIM STRIP. FABBED TRIM STRIPS.

ATA 5347

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 120 INCH OF CORROSION AFT CARGO LT TRACK FS 790 - 910. FABBED NEW TRACK.

ATA 5541

Part: SKIN — DENTED (RUDDER) · airframe 54,411 hrs · 42,174 cycles

DENT 5 X 14 INCH ON RUDDER SKIN. INSTALLED DOUBLER REPAIR.

ATA 5510

Part: FAIRING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AND GOUGED FAIRING LT HORIZONTAL STAB I/B LEADING EDGE FAIRING. FABBED NEW FAIRING.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A .041 DEEP GOUGE FS 111.5 LONG 19 RT. INSTALLED DOUBLER REPAIR.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION ON FLOOR PANEL AT FS 570. FABBED AND REPLACED FLOOR PANEL WEB.

ATA 5320

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A .5 INCH BENT CORNER INTERCOSTAL AT STA 749 LONGERON 11 RT. CROSS SECTIONALLY BLENDED OUT DAMAGE.

ATA 5320

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

BENT CORNER ON INTERCOSTAL AT STA 832 LONGERON 11 LT. BLENDED CROSS SECTIONALLY, MAT LOSS IN LIMITS.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AREA ON FLOOR SUPPORT FS 198 BL 0 TO LBL 44. FABBED AND INSTALLED SUPPORT.

ATA 5320

Part: WEB — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED PUNCTURE STATION 365 LONG 18. INSTALLED REPAIR DOUBLER.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION AND CRACKS ON FLOOR PANEL. FABBED NEW SKIN.

ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AREAS OF CORROSION ON INTERCOSTAL. FABBED AND INSTALLED INTERCOSTAL.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AREAS OF CORROSION ON FLOOR PANEL NR 62. FABBED AND INSTALLED SKIN AND CHANNEL SPLICES.

ATA 5311

Part: FRAME — TOOL DAMAGE (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DRILL START IN FRAME STATION 897 AND LONGERON 19 LT. PLUGGED HOLE AND INSTALLED STRAP.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AND DENTED FRAME. REPLACED WITH IDENTICAL PART SPLICE REPAIR.

ATA 5753

Part: ANGLE — GOUGED (LT TE FLAP) · airframe 54,411 hrs · 42,174 cycles

A .065 INCH GOUGE LT FLAP I/B FAIRING SUPPORT ANGLE. REPLACED WITH IDENTICAL PART.

ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION STATION 190 LBL 12 ON SKIN. REMOVED AND REPLACED DOUBLER.

ATA 2823

Part: CONTROL CABLE — CORRODED (FUEL SOV) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CABLES CORRODED RT WING FUEL SHUT OFF VALVE. REMOVED AND REPLACED CABLES.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

EIGHT SMALL CRACKS AND 1 IMPROPER REPAIR ON GILLINER SUPPORT AT STATION 870. WELDED REPAIR AND INSTALLED REPAIR DOUBLER.

ATA 7120

Part: ISOLATOR — GOUGED (NR 2 ENGINE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED GOUGE NR 2 FWD ENGINE ISOLATOR. REPLACED ISOLATOR.

ATA 5751

Part: AILERON — NICKED (RT SIDE) · airframe 54,411 hrs · 42,174 cycles

TWO NICKS ON AILERON RT AILERON LEADING EDGE TOP SURFACE. INSTALLED FILLER AND DOUBLER AND REBALANCED SURFACE AFTER REPAIR.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 60 BY 10 INCH AREA OF CORROSION AND ELONGATED HOLES ON FLOOR PNL 37. FABBED FLOOR PANEL SKIN.

ATA 5321

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 54,411 hrs · 42,174 cycles

CRACKED FLOOR PANEL SKIN NR 77. FABBED AND REPLACED SKIN.

ATA 5320

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

VARIOUS AREAS OF CORROSION FS 140 TO 160 LBL 15 TO BBL 15. INSTALLED REPAIR DOUBLERS.

ATA 5320

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION AFT PIT THRESHOLD. FABBED NEW PANEL.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DAMAGE FS 1084 BELLY. INSTALLED DOUBLER REPAIR.

ATA 5320

Part: PANEL — CRACKED (CARGO BAY) · airframe 54,411 hrs · 42,174 cycles

TWO CRACKS STATION 794 ON GILLINER SUPPORT. WELDED CRACKS AND INSTALLED REPAIR DOUBLER.

ATA 7160

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 54,411 hrs · 42,174 cycles

FOUR LOCALIZED DENTS NR 2 ENGINE NOSE COWL. INSTALLED DOUBLERS.

ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CHAFED AREA ON FLOORBEAM FS 503. INSTALLED REPAIR ANGLE.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGED AREA FUS SKIN AFT PIT DOOR. REMOVED DAMAGED, TREATED AND PRIMED.

ATA 5720

Part: SUPPORT BRACKET — GOUGED (LT WING) · airframe 54,411 hrs · 42,174 cycles

THREE INCH LONG CRACK LEFT WING O/B LEADING EDGE SUPPORT. WELDED REPAIR.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGE .005 DEEP FS 680 LONGERON 18RT ON FRAME. BLENDED OUT GOUGE.

ATA 5320

Part: DOUBLER — CORRODED (PRESS BULKHEAD) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED DOUBLER AFT PRESSURE BULKHEAD STR 30. REPLACED DOUBLER.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FUSELAGE SKIN GOUGED 4 INCHES LONG AND .002 DEEP AT STATION 380 LONGERON 28 RT. BLENDED AND TREATED.

ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AREAS OF CORROSION LEVEL 2 FS 148 UNDER F/O SEAT. FABRICATED AND REPLACED DAMAGED WEB SECTION.

ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CRACK STATION 765 LONGERON 18 RT CUSP WEB. INSTALLED DOUBLER REPAIR.

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DENT IN UPPER FLANGE OF FRAME AT STATION 332 BETWEEN LONG 29 LT AND 29 RT. INSTALLED DOUBLER REPAIR AND FILLER.

ATA 5320

Part: SUPPORT BRACKET — IMPROPER (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

IMPROPER REPAIR FS 313 BETWEEN 25 RT AND 26 RT LONGERONS. STACKED ANGLE REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AREA ON FLOOR SUPPORT FS 200 - 237 LBL 18. FABBED AND INSTALLED NEW SUPPORT.

ATA 5320

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 6 BY 10 INCH AREA OF CORROSION BETWEEN LONG 29 RT AND 30 RT AT FS 585. FILLER INTERNAL AND EXTERNAL DOUBLER INSTALLED.

ATA 5312

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING AT RADOME PRESSURE BULKHEAD WEB. REMOVED DAMAGE, TREATED AND PRIMED.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A .5 INCH GOUGE FS 851 LONG 29 RT ON FRAME. FABBED AND INSTALLED REPAIR FILLER SPACER AND DOUBLER.

ATA 5310

Part: BEAM — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FS 200 LBL 22 BEAM GOUGED. EXTRUSION REPAIR.

ATA 5530

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 54,411 hrs · 42,174 cycles

CRACK FWD UPPER EDGE OF LT LWR HORIZ STAB FAIRING PANEL. INSTALLED STACKED ANGLE REPAIR.

ATA 5320

Part: PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION ON CEILING PANEL STRIPS LT SIDE STATION 917 - 966. FABBED NEW STRIPS.

ATA 5280

Part: SKIN — MISREPAIRED (NLG DOOR) · airframe 54,411 hrs · 42,174 cycles

IMPROPER REPAIR RT AFT NLG DOOR HINGE CUTOUT FUSELAGE SKIN. INSTALLED SRM REPAIR.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGES AND SCRATCHES FS 446 LONG 28R FRAME. REMOVED GOUGES AND SCRATCHES.

ATA 5320

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION ON FLOOR PAN FS 160 RBL 49. FABRICATED AND INSTALLED PAN.

ATA 5315

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 22 INCH AREA OF CHAFING ON FLOORBEAM. REMOVED CORROSION, TREATED AND PRIMED AND REPLACED RUB STRIPS.

ATA 5320

Part: BRACKET — CRACKED (RT MLG WW) · airframe 54,411 hrs · 42,174 cycles

CRACKED PULLEY BRACKET RT WHEEL WELL. REPLACED WITH IDENTICAL PART.

ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION STATION 200 TO 237 LONGERON 18 LT CUSP WEB. INSTALLED DOUBLER.

ATA 5312

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING RADOME PRESSURE BULKHEAD. REMOVED DAMAGE.

ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 114 INCH SECTION WITH 8 CORRODED AREAS AT FS 408 TO 522 RBL 22 SEAT TRACK. SPLICED IN SECTION OF NEW SEAT TRACK.

ATA 5230

Part: STRUCTURE — CRACKED (FWD CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

A .185 INCH CRACK AFT CARGO DOOR FWD LWR FLANGE. ROUTED OUT CRACK.

ATA 5512

Part: SKIN — GOUGED (HORIZ STAB LE) · airframe 54,411 hrs · 42,174 cycles

GOUGE AT RT HORIZONTAL L/E. BLENDED, TREATED AND PRIMED.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TWO INCH CRACK ON SUPPORT AT FS 351 BETWEEN 24 RT AND 24 LT. WELDED REPAIR.

ATA 5753

Part: CAP — CHAFED (RT TE FLAP) · airframe 54,411 hrs · 42,174 cycles

CHAFED RT INBOARD FLAP END CAP. BLENDED, TREATED AND PRIMED.

ATA 5320

Part: FLOORBOARD — CORRODED (COCKPIT) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

FLOORBOARD SKIN CORRODED UNDER CREW O2 BOTTLE. REMOVED AND FABBED NEW SKIN AND INSTALLED 1 HAT CHANNEL.

ATA 5320

Part: ANGLE — CORRODED (BULKHEAD) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CRACKED AND CORRODED FWD BULKHEAD ANGLE. REPLACED WITH IDENTICAL NEW PART.

ATA 5410

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 54,411 hrs · 42,174 cycles

CRACKED L ANGLE RT ENGINE STRUT PANEL SUPPORT STIFFENER INSTALLED. STACKED ANGLE REPAIR.

ATA 5210

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACK FWD L-1 DOOR FWD UPPER CORNER. INSTALLED FILLER AND DOUBLER.

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DENTS AT FS 64.1 AND 69.5 WL 0 ON SKIN. REMOVED FASTENERS CHECKED DENTS WITHIN LIMITS.

ATA 5320

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AFT CARGO LT TRIM STRIPS CORRODED. FABBED TRIM STRIPS.

ATA 5320

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 500 SQ INCH OF CORROSION AFT CARGO COMP CEILING TRIM STRIP. FABBED NEW TRIM STRIPS.

ATA 5320

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DAMAGE FWD CARGO STATION 351 - 370. REPLACED INTERCOSTAL.

ATA 5320

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED AREA FS 200 LBL 14 FLOOR PAN. FABRICATED AND INSTALLED FLOOR PAN.

ATA 5310

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED SHEAR TIE (FORMER) FS 427 LONG 3 RT. FABBED AND REPLACED FORMER.

ATA 5321

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 54,411 hrs · 42,174 cycles

CRACKS ON FLOOR PANEL 48 FS 522 TO 579 BETWEEN LBL 24 AND BL 0. REPLACED CRACKED CHANNELS.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

TWENTY INCHES OF CORROSION STATION 370 FWD PIT FRAME SPLICE. FABBED AND INSTALLED FRAME SPLICE.

ATA 5320

Part: CHANNEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 3 BY 8 INCH AREA OF CORROSION ON FLOOR PANEL NR 49. REPLACED CHANNELS AND INSTALLED FILLER AND DOUBLER ON SKIN.

ATA 5311

Part: FRAME — GOUGED · airframe 54,411 hrs · 42,174 cycles

GOUGE .005 DEEP AT FS 737 LONG 18 RT. BLENDED OUT GOUGE.

ATA 5753

Part: VANE — GOUGED (TE FLAP) · airframe 54,411 hrs · 42,174 cycles

GOUGE ON RIGHT FLAP I/B VANE SKIN. BLENDED, TREATED AND PRIMED.

ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 137 SQ INCH AREA 7 SPOTS OF CORROSION. SPLICED IN REPAIR TRACK.

ATA 5320

Part: WEB — PUNCTURED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

PUNCTURE IN CUSP WEB STATION 503. INSTALLED REPAIR DOUBLER.

ATA 5321

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

FLOORBOARD SKIN CORRODED AFT OF CO-PILOTS SEAT. FABBED NEW PANEL.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED GOUGE AND CORROSION STA 965 FLOORBOARD SUPPORT. REMOVED AND REPLACED ANGLES.

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DENT IN BELLY SKIN FUSELAGE STATION 110 AND CENTERLINE FUSELAGE ON FRAME. INSTALLED NEW FRAME AND DOUBLER

ATA 5320

Part: CLIP — BROKEN (GUSSET) · airframe 54,411 hrs · 42,174 cycles

BROKEN CLIP ON GUSSET BETWEEN STA 351 AND 365. FABBED AND REPLACED NEW CLIP.

ATA 5321

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION 99 X 10 INCHES RT FLOORBOARD PANEL 61. REMOVED CORROSION AND INSTALLED DOUBLER.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DING FUS STA 125 LONG 19. BLENDED DING.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

FLOOR PANEL CORRODED. FABBED NEW FLOOR PANEL.

ATA 5320

Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING ON FLOOR SUPPORT. BLENDED, TREATED AND PRIMED.

ATA 5320

Part: SUPPORT BRACKET — IMPROPER (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

IMPROPER REPAIR AT FS 813 BETWEEN LONG 23 LT AND 30 LT. INSTALLED SRM REPAIR.

ATA 5313

Part: LONGERON — BENT (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TOOL DAMAGE (BENT) ON LIP OR LONGERON 2RT STATION 256. REMOVED DAMAGE BY BLENDING .040 FROM LIP TAPERED OUT 1.00 INCH.

ATA 5320

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 47 INCH AREA OF CORROSION FLOOR SUPPORT CHANNEL. REPLACED WITH IDENTICAL PART.

ATA 7120

Part: YOKE — GOUGED (NR 1 ENGINE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED GOUGE NR 1 ENGINE MOUNT YOKE ASSY LOWER CUSP. SENT OUT FOR OVERHAUL AND INSTALLED OVERHAULED PART.

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DING .58D X .O42X FUSELAGE SKIN STATION 157 LONGERON 22L. BLENDED, TREATED AND PRIMED.

ATA 5244

Part: SKIN — CRACKED (BULKHEAD DOOR) · airframe 54,411 hrs · 42,174 cycles

THREE CRACKS AFT PRESSURE BULKHEAD ABOVE DOOR JAMB 3 PLACES. INSTALLED DOUBLER.

ATA 5320

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 20 SQ INCHES OF CORROSION AFT CARGO AFT RT LWR BULKHEAD. FABBED WEB PANEL.

ATA 5320

Part: STOP — CRACKED (AFT APB DOOR) · airframe 54,411 hrs · 42,174 cycles

AFT APB DOOR STOP CRACKED RT UPPER. REPLACED WITH NEW IDENTICAL PART.

ATA 5242

Part: PAN — DENTED (E/E BAY DOOR) · airframe 54,411 hrs · 42,174 cycles

DENT IN E & E BAY DOOR FRAME TOP OF PAN FLANGE. INSTALLED STACKED ANGLE REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CRACK AT STA 541 FLOOR SUPPORT. FABBED REPLACEMENT.

ATA 5320

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

TRIM STRIPS CORRODED AFT CARGO LT SIDEWALL. FABBED TRIM.

ATA 5321

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

VARIOUS CRACKS AND GOUGES IN 114 INCH X 10 INCH AREA ON FLOOR PANEL NR 10. FABBED AND INSTALLED NEW SKIN AND HAT CHANNEL SPLICES.

ATA 5320

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 1 X 2 INCH AREA OF CORROSION FS 506 TO RBL 26 FWD CARGO COMP DOUBLER. FABBED DOUBLER.

ATA 5320

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION AT STATION 210 FLOOR PAN LBL 22 - 44. INSTALLED DOUBLER.

ATA 5730

Part: PANEL — CORRODED (RT WING LE) · airframe 54,411 hrs · 42,174 cycles

CORROSION AROUND FASTENER HOLES RT WING L/E PNL 1209. FABBED NEW PANEL. LEVEL 1 CORROSION.

ATA 5315

Part: FLOORBEAM — CHAFED (CABIN) · airframe 54,411 hrs · 42,174 cycles

CHAFED FLOORBEAM STATION 408. BLENDED AND INSTALLED WEAR STRIP.

ATA 5320

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

BENT CORNER ON INTERCOSTAL LONGERON 11 LT AT STATION 908. BLENDED CROSS SECTIONALLY AND FOUND WITHIN LIMITS.

ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION ON WEB INSTALLED FILLER AND DOUBLER.

ATA 5320

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FOUR HAT CHANNELS CRACKED ON FLOOR PANEL 40 FS 389 TO 465 BL 0 TO LBL 24. FABRICATED AND REPLACED HAT CHANNELS.

ATA 5320

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

AREAS OF CORROSION FS 200 TO 218 RBL 44. FABRICATED AND REPLACED DIAPHRAGM.

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DENTS ON ENTIRE SKIN OUT OF LIMITS STATION 1132 - 1143 LONGERON 20. REMOVED AND REPLACED SKIN.

ATA 5320

Part: BEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CHAFING STA 522 BEAM. BLENDED, TREATED AND PRIMED AREA.

ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

GOUGE AND NICKS IN FRAME AT STA 332 AND LONG 17 LT. BLENDED TREATED AND PRIMED.

ATA 5310

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

INPROPER REPAIR FS 294 BETWEEN LONGERON 25 AND 25 LEFT. INSTALLED SRM REPAIR.

ATA 5320

Part: WEB — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

HOLE IN CUSP MEMBRANE STATION 889 LONGERON 18 RT. INSTALLED DOUBLER REPAIR.

ATA 5310

Part: SHEAR TIE — GOUGED (579) · airframe 54,411 hrs · 42,174 cycles

A 1 BY .024 INCH GOUGE FS 579 BETWEEN LONG 27 AND 28 RT FWD CARGO FORMER. DOUBLER REPAIR.

ATA 5540

Part: STRUCTURE — CORRODED (RUDDER) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 1 INCH SQ LOCALIZED AREA OF CORROSION. CUT OUT AREA AND INSTALLED DOUBLER.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION LOCALIZED AREA 2 X 19 STATION 218 - 237 FLOOR SUPPORT. REMOVED AND REPLACED SUPPORT.

ATA 5321

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TWO CRACKS 1 INCH AT FLOOR PANEL 12 FS 137 TO 157 LBL 24 TO LBL 40. INSTALLED REPAIR DOUBLERS.

ATA 5320

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION LONGERON 27 LT STATION 908 GUSSETT. REPLACED GUSSETT.

ATA 5320

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 100 SQ INCH CORROSION AFT CARGO PIT SIDEWALL TRIP STRIP. FABBED TRIM STRIPS.

ATA 5320

Part: ANGLE — MISREPAIRED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

IMPROPER REPAIR FS 813 23 RT TO 30 RT. SUPPORT ANGLE INSTALLED SRM REPAIR.

ATA 5230

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACKED FITTING AFT CARGO DOOR INTERNAL STRUCTURE UPPER BEAM FITTING. REPLACED WITH NEW IDENTICAL PART.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION AND CHAFING STATION 163 - 200 RBL 48 RBL 54 FLOOR PANEL 20. FABBED NEW SKIN AND INSTALLED 2 NEW HAT CHANNELS.

ATA 5320

Part: CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CRACKS AND CORROSION STATION 996 ON CLIP. REPLACED WITH IDENTICAL PART.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED SUPPORT FS 408 LONG 29 RT. INSTALLED DOUBLER REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

FLOORBEAM CORRODED AT NUT PLATES. SPLICED IN NEW UPPER ANGLE.

ATA 5320

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

TRIM STRIPS CTR SECTION AFT CARGO CORRODED. FABBED TRIM.

ATA 5210

Part: DOOR SEAL — BENT (PAX DOOR) · airframe 54,411 hrs · 42,174 cycles

BENT AND GOUGED SEAL DEPRESSOR ON FWD ENTRY DOOR TOP AFT CORNER. RECONTOURED AND BLENDED.

ATA 5753

Part: VANE — DAMAGED (RT TE FLAP) · airframe 54,411 hrs · 42,174 cycles

MAJOR REPAIR, LOCALIZED DING RIGHT I/B FLAP VANE. HOT BOND REPAIR.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

FLOOR SUPPORT CORRODED AT FS 160. FABBED AND INSTALLED FLOOR SUPPORT.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CORROSION LEFT O/B FLOOR PANEL. REMOVED AND REPLACED PANEL.

ATA 5320

Part: DOUBLER — CRACKED (CARGO BAY) · airframe 54,411 hrs · 42,174 cycles

TWO CRACKS FWD CARGO COMP FWD LWR SIDE WALL. REPLACED DOUBLER.

ATA 5320

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKS AND PUNCTURES FLOOR PNL 46A. FABBED AND INSTALLED SKIN.

ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

PUNCTURE WITH CRACKS AT FUS SKIN STATION 555 AND LONGERON 29 LT. INSTALLED DOUBLER REPAIR AND FILLER.

ATA 5320

Part: STRUCTURE — GOUGED (AFT WALKWAY) · airframe 54,411 hrs · 42,174 cycles

GOUGE IN AFT ACCESSORY SECTION OF WALKWAY RT AFT END. FABRICATED AND REPLACED DAMAGED SECTION.

ATA 5320

Part: FLOOR SUPPORT — CHAFED (CABIN) · airframe 54,411 hrs · 42,174 cycles

LOCALIZIED CHAFING STA 522 BL 0 TO 22L FLOORBOARD SUPPORT. REPLACED DAMAGED FLOOR SUPPORT.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 8 INCH AREA OF CORROSION. FABRICATED AND INSTALLED FILLERS AND DOUBLERS.

ATA 5320

Part: WEB — DENTED (CARGO DOORWAY) · airframe 54,411 hrs · 42,174 cycles

DENT FWD CARGO DOOR THRESHOLD WEB. INSTALLED DOUBLER.

ATA 7160

Part: NOSE COWL — CRACKED (NR 1 ENGINE) · airframe 54,411 hrs · 42,174 cycles

A .3 INCH LONG CRACK NR 1 ENG NOSE COWL 11 O CLOCK POS 10 INCHES AFT OF L/E. INSTALLED REPAIR DOUBLER.

ATA 5320

Part: WEB — DAMAGED (AFT CARGO BAY) · airframe 54,411 hrs · 42,174 cycles

AFT CARGO COMP FWD LWR WEB AROUND DOOR JAMB BLENDED BEYOND LIMITS. REPLACED LOWER WEB.

ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

A 22 INCH AREA OF CHAFING AT FS 579 BL 0 TO LBL 22 FLOORBEAM. FABRICATED AND INSTALLED WEAR STRIPS.

ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CRACK RT STATION 617 CUSP WEB. INSTALLED DOUBLER REPAIR.

ATA 5320

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 88 INCH AREA OF CORROSION FS 165 LBL 44 TO RBL 44, FLOOR PAN. REPLACED PAN AND DOUBLER WITH FABBED PARTS.

ATA 5320

Part: SUPPORT BRACKET — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CHAFING FLOORBOARD SUPPORT STATION 465 BL 0 XL 22. FABBED AND REPLACED.

ATA 5230

Part: SKIN — BENT (CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

BENT CORNER AFT CARGO DOOR AFT LWR CORNER. BLENDED DAMAGE AREA CROSS SECTIONALLY.

ATA 5320

Part: DOUBLER — CRACKED (APB DOOR FRAME) · airframe 54,411 hrs · 42,174 cycles

CRACK IN UPPER DOOR JAMB AFT PRESSURE BULKHEAD DOOR JAMB AT STATION 965.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION FLOOR PANEL NR 14. FABRICATED AND INSTALLED PANEL.

ATA 5320

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FLOOR PNL SPLICE BENT AND GOUGED AFT PIT. FABBED NEW SPLICE PNL.

ATA 5320

Part: STIFFENER — CRACKED (PRESS BULKHEAD) · airframe 54,411 hrs · 42,174 cycles

CRACKED STIFFENER APB LT SIDE LWR STIFFENER. REPLACED WITH IDENTICAL PART.

ATA 5320

Part: STIFFENER — CRACKED (APB DOOR) · airframe 54,411 hrs · 42,174 cycles

CRACKED STIFFENER RT APB DOOR JAMB WEB AT X 18. REPLACED WITH IDENTICAL PART.

ATA 5541

Part: SKIN — DENTED (RUDDER) · airframe 54,411 hrs · 42,174 cycles

DENT .027 X .250 INCH LONG LT SIDE OF RUDDER STATION XR 109, 18 INCHES FROM T/E. INSTALLED REPAIR DOUBLER.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

E&E BAY DOOR OUTER SKIN NICKED AND GOUGED OUTER SKIN. REPLACED DOOR SKIN, MODIFIED REPAIR WITH 7075-T6 SKIN.

ATA 5347

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORROSION AROUND FASTENER HOLES ON FWD PIT TIE DOWN TRACK. REPLACED WITH NEW IDENTICAL PART.

ATA 5320

Part: DIAPHRAGM — PUNCTURED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TWO PUNCTURES IN FLOOR PAN FS 180 LBL 22 TO LBL 4. FABRICATED AND INSTALLED DIAPHRAGM.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

SKIN DENTED AND GOUGED AT FUSELAGE STATION 396 - 420 LONGERON 28 RT. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER.

ATA 5320

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

TWO CRACKS AT STATION 851 FLOOR SUPPORT. WELDED REPAIR AND REPLACED RT SUPPORT.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

ONE CRACK AND IMPROPER REPAIR STATION 275 LONG 28L TO 28R. WELDED REPAIR AND INSTALLED 2 STACKED ANGLE REPAIRS.

ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DAMAGE GOUGED AND TORN AFT PIT DOOR FUSELAGE SKIN. BLENDED, TREATED AND PRIMED.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

SMALL CRACK GILLINER SUPPORT. WELDED REPAIR.

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACK ON SUPPORT IN AFT CARGO BIN. STOP DRILLED AND WELDED CRACKS.

ATA 5320

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 2 INCH AREA OF CORROSION AND CRACKS ON CHANNEL AT FS 915. REPLACED WITH NEW IDENTICAL PART.

ATA 5320

Part: PLATE — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

CORRODED WEB AFT CARGO FWD DOOR JAMB. REPLACED WITH NEW IDENTICAL PART.

ATA 5320

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED FLOOR BOARD CHANNELS HAT CHANNELS. FABBED AND INSTALLED.

ATA 5320

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

LOCALIZIED CORROSION ON FLOOR PAN. INSTALLED DOUBLER REPAIR AFTER REMOVAL.

ATA 5320

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

FLOOR SUPPORT Z-ANGLE BROKEN AT STATION 639. FABBED NEW ONE.

ATA 5311

Part: FRAME — GOUGED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

SMALL GOUGE IN FRAME AT STATION 698 AND LONGERON 18 RT. BLENDED TREATED AND PRIMED.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

VARIOUS CRACKS AND CORROSION IN 81 X 24 INCHES AREA FLOOR PANEL 29 FS 237 TO 318 BL 0 TO RBL 24. FABBED NEW PANEL.

ATA 5753

Part: VANE — CORRODED (RT TE FLAP) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

A 1.5 X 1.5 INCH CORRODED AREA RT FLAP VANE STATION XFCF 187 LOWER. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

DENT 1.25 X .060 INCH DEEP IN SKIN AT FS 141 AND LONGERON 19L. INSTALLED DOUBLER REPAIR.

ATA 5320

Part: ANGLE — CHAFED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED CHAFING AT STA 579 BL 0 TO 22L FLOOR SUPPORT ZEE ANGLE. FABBED AND INSTALLED NEW ANGLE.

ATA 5321

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKS ON FLOOR BOARD CHANNELS. FABBED NEW HAT CHANNELS AND SKIN.

ATA 5230

Part: SKIN — GOUGED (CARGO DOOR) · airframe 54,411 hrs · 42,174 cycles

GOUGE ON FWD SIDE CARGO DOOR SKIN. BLENDED, TREATED AND PRIMED AREA.

ATA 5310

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED SHEAR TIE STATION 946 BETWEEN LONGERON 15 AND 16 RT. FABBED NEW SHEAR TIE AND INSTALLED.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 54,411 hrs · 42,174 cycles

200 INCHES OF CORROSION FLOOR PANEL 21. FABRICATED NEW SKIN.

ATA 5753

Part: SKIN — GOUGED (LT TE FLAP) · airframe 54,411 hrs · 42,174 cycles

GOUGE .010 INCH DEEP LEFT I/B FLAP UPPER SKIN. REMOVED AND REPLACED SKIN.

ATA 5320

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

CRACKED BRACKET AT FS 200 LONGERON 5L. FABRICATED AND INSTALLED BRACKET.

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

LOCALIZED DENT STATION 1026 AT 6 O CLOCK POSITION. INSTALLED DOUBLER REPAIR.

ATA 5320

Part: ANGLE — MISREPAIRED (FUSELAGE) · airframe 54,411 hrs · 42,174 cycles

IMPROPER REPAIR AT FS 389 BETWEEN LONG 29 LT AND 29 RT. REPLACED WITH IDENTICAL PROPER PART.