N108AX

Part: FUEL TANK — LEAKING (RT WING) · airframe 122,355 hrs · 23,980 cycles

RT WING LEAKING FUEL IN FLIGHT.

Part: FLOORBEAM — CORRODED (BS 815) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

LIGHT CORROSION ON FLOOR SUPPORT AT STA 815 X-18. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG 7696 AND ADA7548 AND SRM 51-35-01 STEP 1, VOL II REV 94.

Part: TRACK — CORRODED · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

FOUND CORROSION ON DOWN TRACK AT STA 1902 - 2007 AND X=75.25. CORROSION REMOVED IAW SRM 51-21-01 V G REV 94 DIMENTIONS ARE OUT OF LIMITS (240 X 8T X 2,4 MM) FABRICATED AND INSTALLED TRACK PN AGA7086-506 IAW DWG AGA7086 AND DWG ASA 7127 AND MM 205002 REV 81.

Part: FLOOR SUPPORT — CORRODED (BS 1820-1887) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

LIGHT CORROSION ON FLOORBEAM SUPPORT BETWEEN STA 1820-1887 X36. REMOVED BEAM IAW SRM 51-31-01 VOL II REV 94. FABRICATED PN AGA7085-1 ED INSTALLED IAW DWG ASA 7127 AND MM 20-50-02 REV 81.

Part: SUPPORT — CRACKED (BS 459) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

GALLEY SUPPORT CORRODED AT STA 459 XX24. REPLACED PN ACA7366-501 IAW DWG ACA7365 AND SRM51-35-01, VOL II, REV 94.

Part: FITTING — CORRODED (BS 879) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CORROSION ON FITTING GALLEY AT STA 879, X44. REMOVED CORROSION IAW SRM 51-21-24 VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3.5 MM. FABRICATED PN AWD7743-503, REF DWG AWD 7743 AND INSTALL NEW PN IAW SRM 51-31-03, VOL II, REV 94, PAGES 1 THRU 66 AS APPLICABLE.

Part: PANEL — CRACKED (LT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

LT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.

Part: FLOORBEAM — CRACKED (BS 1523) · airframe 120,927 hrs · 23,957 cycles

CTR CARGO COMPT, FLOOR STRUCTURE, AT STA 1523 (FWD BULKHEAD) NR 4 ANGULARS CRACKED. OPEN PANELS 183JE-183FE FWD BULKHEAD CTR CARGO COMPARTMENT IAW AMM 20-50-02 REV 81. PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHI REV 93 VOL I OK DONE. CLOSE PANELS 183JE, 189FE FWD BULKHEAD CTR CARGO COMPT IAW AMM 20-50-02 REV 81.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 120,927 hrs · 23,682 cycles

CTR CARGO DOOR EXTERNAL FAIRING SUPPORT CRACKED (AFT POSITION). PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2, REV 94.

Part: SUPPORT — CRACKED (LT WING) · airframe 120,927 hrs · 23,682 cycles

LT OTBD FLAP, INBD HINGE STRUCTURE UNDER PANEL 535JL, SUPPORT CRACKED. REPLACED SUPPORTS CRACKED UNDER PANEL 535JL IAW SRM 51-35-01 VOL II REV 93.

Part: FLOOR SUPPORT — CORRODED (BS 440-453) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CORROSION ON FLOOR SUPPORT BETWEEN STA 440 / 453, XO. FABRICATED AND INSTALLED NEW PN ACA7374-1 IAW DWG ACA7374 AND 7365 AND SRM 51-35-01 V I REV 94 STEP 1.

Part: TRACK — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

FOUND CORROSION ON DOWN TRACK AT STA 1887-2007 AND X=27.50. REMOVED BEAM IAW SRM 51-31-01, VOL II, REV 94 AND MM 20-50-02 REV 81. FABRICATED PN ASA7087-1 IAW DWG ASA7087 AND INSTALLED IAW DWG AGA7127 AND MM 20-50-02 REV 81.

Part: PANEL — DAMAGED (NR 2 PYLON) · airframe 120,927 hrs · 23,682 cycles

PYLON NR 2 PANEL, 457BT DAMAGED. REPAIRED IAW SRM 54-00-01, FIG 1A SHEET 1 REV 94 VOL J.

Part: FLOORBEAM — CORRODED (BS 815) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CORROSION ON FLOOR SUPPORT AT STA 815 X19. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG ADA7326 AND 7548 AND SRM 51-35-01, STEP 1, VOL II, REV 94.

Part: SKIN — DENTED (BS 724) · airframe 120,927 hrs · 23,682 cycles

DENT ON FUSELAGE SKIN STA 729 - LONGERON 43. PERFORM REPAIR IAW SRM 53-20-00 FIG SH3, REV 45, VOL I, OK PERFORM REPAIR AS REQUIRED.

Part: TRACK — CORRODED · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

FOUND CORROSION ON DOWN TRACK AT STA 1871-2007 AND X=107.25. REMOVED CORROSION IAW SRM 51-21-01 V II REV 94 DIMENSIONS OUT OF LIMITS (120 X 50 X 2,3 MM). REPLACED PN NRA6222-9 IAW DWG NFA6222. INSTALLED PN AFA7789-535 IAW SRM 51-35-01 AND 51-33-01 V II INSTEAD OF NFA6222-43.

Part: FLOORBEAM — CRACKED (BS 1690) · airframe 120,927 hrs · 23,682 cycles

CTR CARGO COMP FLOOR UNLOAD BEAM CRACKED AT STA 1690 (UPPER FLANGE) PERFORMED REPAIR IAW SRM 53-70-00 FIG 3 REV 93 VOL J. PERFORMED PAINTING IAW SRM 51-21-02 VOL II REV 94.

Part: FLOORBEAM — CORRODED (BS 859) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

LIGHT CORROSION ON FLOORBEAM AT STA 859 X-72. REMOVED CORROSION IAW SRM 51-21-01, ERV 94, VOL II OUT OF LIMITS. REPLACED PN ADD 7160-2 IAW SRM 51-35-01, VOL II, REV 94, STEP 1 (REF DWG ADD 7163).

Part: SKIN — CRACKED (STAB) · airframe 120,927 hrs · 23,682 cycles

HFEC INSP ON HS IAW J/C 10AD-904 SB 455-18. FOUND ONE CRACK INDICATION 37MM LENGTH ON OUTER SECTION UPPER AFTER SKIN PANEL RT SIDE. PERFORMED STOP DRILL AS REQUIED IAW SB A55-18 STEP 11C PAG 7 REV 6. FOR REPLACEMENT SEE ODL PGO-067.

Part: STRUCTURE — DENTED (ZONE 100) · airframe 120,927 hrs · 23,682 cycles

DENT AT STA 1853.93 LONG 47 REPAIR NEXT C CHK. PERFORMED SANDING AS REQUESTED AS DPS 9.316. PERFORMED REPAIR IAW SRM 53-20-00, FIG 6 (SHT 3) V.I. REV 93. PERFORMED PAINTING OF REPAIRED AREA IAW SRM 51-21-02 VOL 2 REV 94.

Part: BEAM — CRACKED (BS 1781) · airframe 120,927 hrs · 23,682 cycles

CTR CARGO COMP STA 1781 NR 3 LT BEAM OF ZONE PLENUM CRACKED. REMOVED BEAM IAW MM 20-50-02 REV 81. PERFORMED DRILL NEW BEAM IAW DWG AF)7011-3. REPLACED BEAM IAW AMM 20-50-02 REV 81 AND INSTALLED ALL OMNI DIRECTIONAL ROLLERS.

Part: SUPPORT — CORRODED (BS 435) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

NR 2 GALLEY SUPPORT CORRODED AT STA 435, RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01, VOL II, REV 94 (PAGE 1 THRU 66 AS APPLICABLE).

Part: SUPPORT — CORRODED (BS 465) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

NR 2 GALLEY SUPPORT CORRODED AT STA 465 RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 4 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01 VOL II REV 94 (PAGES 1 - 66 AS APPLICABLE) (AND REPLACED NEW PART ORDERED).

Part: CARGO TRACK — CORRODED (BS 1931-2007) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

FOUND CORROSION ON DOWN TRACK AT STA 1931.500 -2007 AND X=8.50. REMOVED BEAM IAW SRM 51-31-01 VOL I REV 94 AND MM 20-50-02 REV 81. FABRICATED PN AGA7088-1 IAW DWG ASA7088 AND INSTALLED IAW DWG ASA7127 AND SRM 51-35-01 VOL II REV 94 AND MM 20-50-02 REV 81.

Part: PANEL — DELAMINATED (LT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

LT INBD FLAP, OTBD HINGE, PANEL 541JL UNGLUED. PERFORMED REPAIR IAW DWG ARC 2541.

Part: STIFFENER — CORRODED (BULKHEAD) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CTR WHEEL WELL AFT CLOSING BULKHEADS WITH A STIFFENER CORRODED. REPLACED PN AYB7080-9, REF DWG BOE AYB 7080 IAW SRM 51-35-01, REV 94, VOL I, STEP 9.

Part: PANEL — CRACKED (LT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.

Part: FLOOR SUPPORT — CORRODED (BS 859-893) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CORROSION ON FLOOR SUPPORT AT STA 859 - 893 X73. REPLACED PN ADA7160-1 IAW DWG ADA7160 AND DWG 7163 AND MM 20-50-02 REV 81.

Part: PANEL — CRACKED (LT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

LT OTBD FLAP, INBD HINGE PANEL 535JL CRACKED. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VII PERFORMED WELD IAW DPS10225. REINSTALLED OLD REPAIR IAW SRM 51-35-02 VII 4REV 94.

Part: SKIN — DENTED (FUSELAGE) · airframe 120,927 hrs · 23,682 cycles

UNDER RT PITOT TUBE HAS FUSELAGE DENT PERFORM PERMANENT REPAIR. REMOVED ELECTRICAL EQUIPMENT TO ACCESS ZONE. REMOVE BRACKET AS AMM 77-13-01 (TRANSDUCER NOT INSTALLED). REMOVED DUCT AS MM 21-26-00 REV 81. PERFORM STRIPPING AS REQUESTED IAW DPS 9.316. PERFORMED DYE PENETRANT AS REQUIRED. NO FINDINGS. REPAIR IAW SRM 53-20-00, FIG13, SHEET 14, VOL I REV 14. INSTALLED DUCT AND BRACKET IAW AMM 77-13-04 REV 81.

Part: FLOORBEAM — CORRODED (BS 2007) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

CORROSION ON FLOOR SUPPORT TEE AT AFTER PRESSURE BULKHEAD, STA 2007. X-40 - X-60, AND X 20. PERFORMED REPAIR IAW SRM 53-40-00, FIG 16, REF 94, VOL I.

Part: FLOOR SUPPORT — CRACKED (BS 1921) · airframe 120,927 hrs · 23,682 cycles

AFT CARGO COMPT FLOOR SUPPORT STRUCTURE AT STA 1921 LT SIDE ANGULAR CRACKED. PERFORMED REPAIR IAW SRM 53-00-01, FIG 8, SHT 1, REV 94 (VOL I).

Part: PANEL — CRACKED (LT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.

Part: DOOR FRAME — CRACKED (BS 1902-2007) · corrosion level 2 · airframe 120,927 hrs · 23,682 cycles

FWD CARGO NEAR DOOR JAMB PANEL NR 127AR CRACKED. REMOVED PANEL 127AR AMM 20-50-02 REV 81. WELD PER DPS 10225 INSTALLED PANEL 127AR IAW MM 20-50-02 REV 81.

Part: SEAT TRACK — CORRODED (BS 1870) · airframe 120,927 hrs · 23,682 cycles

LIGHT CORROSION ON SEAT TRACK (N6) LT UNDER THRESHOLD PAX DOOR 4 LT REMOVE THRESHOLD PLATE AND DRAIN VALVES ON DOOR NR 4 LT OK DONE AS AMM 53-10-01, REV 81. REMOVE CORROSION IAW SRM 51-21-01, VOL II, REV 93 PERFORMED AS REQUIRED MAX DEPTH 2.5 MM OUT OF SRM LIMITS. PERFORMED REPAIR IAW SRM 53-50-01 FIG 1, BOL I, REV 94.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 120,927 hrs · 23,682 cycles

RT OTBD FLAP INBD RIB CLOSURE HAS AN ANGULAR CRACK. REMOVED RT OTBD FLAP, INBD T/E SECTION. REMOVED ALL SCREWS SIZED IAW SRM 51-31-01 VOL 2 REV 93. REMOVED RT OTBD FLAP INBD SECTION T/E IAS MM 20-50-02 REV 81. FABRICATED PN ARC1951-6 IAW DWG ARC1951 AND INSTALLED IAW DWG ARC1652 AND SRM 51-35-01 V II REV 93.

Part: SKIN — DENTED (FUSELAGE) · airframe 120,927 hrs · 23,682 cycles

DENT 30 INCH, FWD OF R1 DOOR SILL - DENT 6 INCH LONG WITHIN LIMITS IAW SRM VOL I-53-20-00 PERFORM PERMANENT REPAIR. REMOVED DUCT IAW 20-50-02 AND MANIFOLD AIR CONDITIONING IAW 21-10-00. PERFORM CUTOUT SKIN DAMAGE IAW SRM 53-20-00 FIG 6, REV 93, VOL I. MADE THE INNER OUTER EXTERNAL DOUBLER FILLER AND FINGER DOUBLER AS SRM 53-20-00 REF 6 REV 94, VOL I. INSTALL REPAIR IAW SRM 53-20-00 FIG 6 REV 91 VOL I. INSTALLED CONDITIONED AIR DUCT AND MANIFOLD DUCT.