N719FD

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 51,605 hrs · 31,024 cycles

AVIONICS SMOKE LIGHT ILLUMINATED. ECAM SHOWED AVIONICS SMOKE PROCEDURE. NO SMOKE OBSERVED. RETURNED TO DEPARTURE. AVIONICS SMOKE LIGHT HAD EXTINGUISHED ON TAXI IN, PREFORMED ADJ/TEST AVIONICS COMPARTMENT SMOKE DETECTION SYSTEM IAW MM 26-15-00-05. NO DISCRFEPANCIES NOTED. PREFORMED GVI OF AVIONICS COMPARTMENT, NO WATER FOUND, SUSPECT SMOKE DETECTOR. REMOVED AND REPLACED THE SMOKE DETECTOR 13WA IAW MM 26-15-12-04. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FRAME 58) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO BAY FLOORBEAM FRAME 58, -Y1470 FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-15, FIG 208. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

DURING OK TO CLOSE FOUND FLOOR SUPPORT CORRODED AT FR 57.2 RT BETWEEN -Y140 AND -Y805. REMOVED DAMAGE SECTION FROM FLOOR SUPPORT AT FRAME 57.2 FROM -Y140 TO -Y805 IAW SRM 53-10-16, FABRICATE REPAIR PARTS IAW SRM 53-10-15, INSTALLED REPAIR PARTS IAW SRM 51-40-21, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO COMPT FLOOR PANEL 152DF BROKEN/DELAM. FABRICATED NEW FLOOR PANEL 152DF ON T17/1299063 PER SRZ 25-005, CLASSIFIED AS CAT A AND MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO-COMPT FLOOR PANEL 152HF BROKEN/DELAM. FABRICATED NEW FLOOR PANEL 152HF ON T17/1299865 PER SRZ 25-005, CLASSIFIED AS CAT A AND MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

DURING OK TO CLOSE FOUND FLOOR PANEL 162HF CORRODED. FABRICATED NEW FLOOR PANEL 162HF ON T17/1298516 PER SRZ 25-005. CLASSIFIED AS CAT A AND MAJOR REPAIR.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

FWD PIT FR38-38.1 LT O/B WEB UNDER ROLLER TRAY CRACKED. REMOVED AND REPLACED NEW SHEAR PLATE (WEB) IAW SRM 51-40-21, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151CF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151SF FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151FF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152LF HAD A BROKEN CORNER. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 51,386 hrs · 30,910 cycles

BULK CARGO FLOOR PANEL 161GF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BULK CARGO) · airframe 51,386 hrs · 30,910 cycles

BULK CARGO FLOOR PANEL 161HF CORNER DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151LF PUNCTURED ON UPPER SKIN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152GF CORNER CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152JF PUNCTURED. FABRICATED A NEW FOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAME 57) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR SUPPORT FRAME 57.1, Y 0, UNDER LOADING TRAY CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-10-15. CLASSIFED AS A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152FF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131HG DELAMINATED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151JF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 151BF CRACKED ON EDGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152BD DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO BAY) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152RF FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 161CF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152AF PUNCTURED ON UPPER SKIN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR PANEL 152KF FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAME 55) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO FLOOR SUPPORT FRAME 55, Y0, UNDER LOADING TRAY CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-10-15.

Part: SEAT TRACK — CORRODED (FRAMES 28-29) · airframe 51,386 hrs · 30,910 cycles

MAIN DECK, FRAMES 28 & 29, Y1959, SEAT TRACK FLANGE HAS CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. LOCATED AND DRILLED A REPAIR IAW SRM 51-40-44 AND INSTALLED IAW SRM 53-10-16, FIG 208. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132YF PUNCTURED. FABRICATED A NEW FLOOR PANEL PER DWG SRZ25-005, CLASSIFED AS A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131QF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131YF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132ZF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 251YG HAS CRACK. FABRICATED FLOOR PANEL 251YG ON 17/1296193 IAW SRZ 25-005, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 242ZJ HAS CRACK. FABRICATED FLOOR PANEL 242ZJ ON 17/1296057 IAW SRZ 25-005, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131RF CRACKED. FABRICATED NEW FLOOR PANEL 131RF ON T17/1296305 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 251BH HAS CRACK. FABRICATED FLOOR PANEL 251BH ON 17/1296194 IAW SRZ 25-005, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 232EF HAS CRACK. FABRICATED FLOOR PANEL 232EF ON 17/1296083 IAW SRZ 25-005, CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131ZF DELAM / PUNCTURED. FABRICATED NEW FLOOR PANEL 131ZF ON T17/1296245 PER SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 242VG HAS CRACK. FABRICATED FLOOR PANEL 242VG ON 17/1296192 IAW SRZ 25-005, CLASSIFIED AS CAT A, MAJOR REPAIR.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

FWD PIT FR 36-37 RT OUTBD WEB BELOW ROLLER TRAY CRACKED. REMOVED AND REPLACED FWD PIT FR 36-37 RT OUTBD WEB IAW SRM 51-40-21. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

AFT CARGO COMPT FLOOR SUPPORT AT Y 0 FR 56, TOP FLANGE CORRODED. FOUND ON REMOVAL OF ROLLER TRAY. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-15, FIG 105, FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT IAW SRM 53-10-15, INSTALLED REPAIR IAW SRM 51-40-21 AND REPAIRED FLOOR SUPPORT AT FR 56 Y 0 IAW SRM 53-10-15, REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 131JG DELAM FABRICATED NEW FLOOR PANEL 131JG ON T17/1296237 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132QF DELAM. FABRICATED NEW FLOOR PANEL ON T17/1296303 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231RH HAS CRACK. FABRICATED FLOOR PANEL 231RH ON 17/1296191 IAW SRZ 25-005, CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132HG DELAM. FABRICATED NEW FLOOR PANEL 132HG ON T17/1296308 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

FWD PIT FR37 TO 38 RT O/B WEB BELOW ROLLER TRAY CRACKED. REMOVED DAMAGE WEB (SHEAR PLATE) IAW SRM 51-40-21. FABRICATED NEW SHEAR PLATE ON T17/1296691, INSTALLED NEW SHEAR PLATE IAW SRM 51-40-21 AND DWG A 533778338.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

FWD PIT FR 34-35 R/H O/B WEB BELOW ROLLER TRAY CRACKED. RECEIVED NEW WEB ON T17/1296681, REMOVED AND REPLACED WEB IN FWD PIT R/H O/B BELOW ROLLER TRAY IAW SRM 51-40-21. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231LG HAS CRACK. FABRICATED FLOOR PANEL 231LG ON T17/1295998 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132RF DELAMINATED / PUNCTURED. FABRICATED FLOOR PANEL 132RF ON T17/1296700 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231AH HAS CRACK. FABRICATED FLOOR PANEL 231AH ON T17/1296095 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

FWD CARGO FLOOR PANEL 132JG DELAMINATED. FABRICATED FLOOR PANEL 132JG ON T17/1296307 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FRAMES 19-22) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231FG HAS A CRACK. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231HG HAS CRACK. FABRICATED FLOOR PANEL 231HG ON T17/1296692 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 241MF HAS CRACK. FABRICATED FLOOR PANEL 241MF ON T17/1296065 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

MAIN CARGO FLOOR PANEL 231EF HAS CRACK. FABRICATED FLOOR PANEL 231EF ON T17/1296092 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 51,386 hrs · 30,910 cycles

SUPPORT WEB UNDER FWD CARGO COMPT FLOOR HAS CRACK FR21 Y1456 APPROX. REMOVED SHEAR PLATE IAW SRM 51-40-21. FABRICATED NEW SHEAR PLATE ON T17/1296683. INSTALLED NEW SHEAR PLATE P/N FX-531418-50 IAW A300 SRM 51-40-21. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221PF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221PF ON T17/1295933 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 222QF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222QF ON T17/1295876 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL222RF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222RF ON T17/1295877 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 222HF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222HF ON T17/1295880 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221RF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221RF ON T17/1295937 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221LF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221LF ON T17/1295935 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221GF HAS MULTIPLE PUNCTURES AND DELAMINATION’S FABRICATED COURIER FLOOR PANEL 221GF ON T17/1295936 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221QF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221QF ON T17/1295938 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221HF HAS MULTIPLE PUNCTURES AND DELAMINATION’S FABRICATED COURIER FLOOR PANEL 221HF ON T17/1295931 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 221MF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221MF ON T17/1295993 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 51,386 hrs · 30,910 cycles

COURIER FLOOR PANEL 222NF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222NF ON T17/1295994 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: DAMPER — UNDERSERVICED (MLG) · airframe 50,550 hrs · 30,435 cycles

ON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. COMPLIED WITH ECAM QRH AND RETURNED TO DEPARTURE. THE GEAR HANDLE WOULD ONLY GO UP TO THE NEUTRAL MIDDLE POSITION ON BOTH SYSTEMS. REMOVED AND REPLACED PITCH DAMPER ON THE RT GEAR IAW AMM 32-11-15-04-0. SERVICED THE DAMPER WITH NITROGEN IAW AMM 12-12-32-00. ACFT OK FOR SERVICE.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 50,080 hrs · 30,152 cycles

RECEIVED GREEN HYD RESERVOIR OVERHEAT DURING CRUISE. TURNED GREEN PUMPS OFF. IAW QRH, TURNED ONE PUMP ON TO DETERMINE AFFECTED PUMP. FOLLOWED BY GREEN HYD RESERVOIR LOW LEVEL WITH ASSOCIATED ECAM WARNING. GRAVITY EXTENDED GEAR, TOWED TO GATE. ALSO NR 1 ENGINE OIL QTY INCREASED APPROXIMATELY 7 QTS. REMOVAL FROM ACFT ONLY. NO INSTALLATION. REMOVED THE NR 1 ENGINE HYD PUMP. INSTALLED NR 1 ENGINE GREEN HYDRAULIC PUMP REF MM 29-11-32-04-01. OPS AND LEAK CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 488 hrs · 29,425 cycles

TAKEOFF CONFIG TESTED NORMAL FOR TAKEOFF ON INITIAL TAKEOFF. PASSING APPROX 25 KNOTS WITH POWER ADVANCING, RED ECAM ALERTED FOR PARKING BRAKE SET, TAKEOFF REJECTED. WARNING EXTINGUISHED WHEN FIRST OFFICER TOUCHED THE PARKING BRAKE HANDLE WHICH WAS DOWN. NO WARNING INDICATED ON THE SUBSEQUENT TAKEOFF, COULD NOT DUPLICATE. PERFORMED OPERATIONAL TEST OF PARKING BRAKE IAW MM 32-45-00-05. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 487 hrs · 29,361 cycles

BOTH PITCH TRIM LEVERS FAULTED OFF JUST AFTER TAKEOFF, NO RESET. PERFORMED AUTO PILOT LAND IAW AMM 22-40-00-05, CAT III. TEST CHECKED OK. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 486 hrs · 29,313 cycles

FLIGHT TEST, SHORTLY AFTER TAKEOFF AT 1000 FEET COCKPIT & COURIER AREA FILLED WITH MODERATE TO HEAVY SMOKE, FUMES WITH AN ACRID OIL SMELL. IAW NORMAL TEST FLIGHT PROCEDURE, APU AIR USED AS BLEED SOURCE FOR AIR CONDITIONING. SEVERAL LEVEL 3 ECAM CARGO COMPARTMENT SMOKE WARNINGS ACTIVATED INCLUDING MID & AFT COMPARTMENTS. ECAM & QRH PROCEDURES FOLLOWED WHICH CLOSES MAIN DECK ISO VALVES, BULK CARGO ISOLATION VALVES & NR 2 PACK FLOW VALVES. AFTER 5 MINUTES SMOKE WARNINGS CEASED & SMOKE DISSIPATED. EMERGENCY LANDING EXECUTED. REPLACED THE SIX AIR CHECK VALVES OF HYD RESERVOIR PRESSURIZATION PER AMM 29-11- 11-04 REPALCED THE THREE VALVES-DEPRESSURIZATION/RELIEF PER AMM 29-12-21- 04 ,CLEANED THE INTERNAL AREA OF LT AND RT WATER SEPARATORS AND REPLACED THE COALESCERS PER AMM 21-51-16-03. CHECKED THE APU BLEED DUCTS PER AMM 36-12-00-06. OPERATED BOTH A/C PACKS USING APU BLEED ,ENG BLEED &GROUND PNEUMATIC SOURCE PER AMM 21-51-00-05 & AMM71-00-00-05, TESTED NORMAL ,NO LEAKAGE AND NO SMELL. MINOR REPAIR IAW FEDEX GMM-6-2-100

Part: CHECK VALVE — FAILED (HYD SYSTEM) · airframe 486 hrs · 29,313 cycles

FLIGHT TEST SHORTLY AFTER TAKEOFF AT 1000 FEET COCKPIT & COURIER AREA FILLED WITH MODERATE TO HEAVY SMOKE & FUMES WITH AN ACRID OIL ODOR. IAW NORMAL TEST FLIGHT PROCEDURE APU AIR USED AS BLEED SOURCE FOR AIR CONDITIONING SEVERAL LEVEL 3 ECAM CARGO COMPARTMENTS SMOKE WARNINGS ACTIVATED INCLUDING MID & AFT COMPARTMENTS ECAM & QRH PROCEDURES FOLLOWED WHICH CLOSES MAIN DECK ISO VALVES, BULK CARGO ISOLATION VALVES & NR 2 PACK FLOW VALVES. AFTER 5 MINUTES SMOKE WARNINGS CEASED & SMOKE DISSIPATED. EMERGENCY LANDING EXECUTED. PERFORMED VISUAL CHECK THE AIR PRESSURE OF ALL THE HYD RESERVOIRS IAW AMM 29-14-00-06 2. DEPRESSURIZED ALL THE HYD RESERVOIR SYSTEM IAW AMM 29-14-00-03 . REPLACED THE CHECK VALVE.

Part: FRAME SPLICE — CRACKED (FRAME 47) · airframe 486 hrs · 29,312 cycles

FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24R & 26R HOLE N & ONE EACH ADJACENT HOLE WITH CRACK SIGNAL.

Part: SKIN — CRACKED (FRAME 54) · airframe 486 hrs · 29,312 cycles

HFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44R LATERAL PANEL.

Part: SKIN — CRACKED (FRAME 54) · airframe 486 hrs · 29,312 cycles

HFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44L LATERAL PANEL.

Part: BOLT — MISSING (FUSELAGE) · airframe 486 hrs · 29,312 cycles

CTR WING JOINT AT FRAME 40. FOUND LT & RT SIDE HAS SIX BOLTS MISSING. REPAIRED IAW EA 6-5710-T0317008 P1. MAJOR REPAIR IAW GMM6-2-100.

Part: BEAM — CRACKED (FUSELAGE) · airframe 486 hrs · 29,312 cycles

HFEC FOUND CTR FUSELAGE LONGITUDINAL BEAM 4 WITH CRACK INDICATION AT FRAME 49LT.

Part: SPAR — CRACKED (WING) · airframe 486 hrs · 29,312 cycles

FUSELAGE CTR WING BOX. INSPECTION OF REAR SPAR & BOTTOM PANEL FASTENER HOLE L WITH CRACK SIGNAL, LT SIDE. COMPLIED WITH EA6-5710-T0317395 PT 1. MINOR REPAIR IAW GMM6-2-100.

Part: SPAR — CRACKED (WING) · airframe 486 hrs · 29,312 cycles

FUSELAGE CTR WING BOX. INSPECTION OF REAR SPAR & BOTTOM PANEL FASTENER HOLE H WITH CRACK SIGNAL, LT SIDE. COMPLIED WITH EA6-5710-T0317395 PT 1. MINOR REPAIR IAW GMM 6-2-100.

Part: FLEX LINE — LOOSE (NR 2 ENGINE) · airframe 47,695 hrs · 28,804 cycles

IN CRUISE FLIGHT ENG 2 WOULD NOT RETARD BELOW 1.30 EPR, CREW RAN THE LACK OF THROTTLE RESPONSE INFLIGHT CHECKLIST. THIS RESULTED IN ENG 2 EPR NO LOWER THAN 1.22. THIS WAS ACCEPTABLE FOR CRUISE FLIGHT, BUT TOO MUCH THRUST FOR THE APPROACH ENVIRONMENT. IAW THE CHECKLIST, WE SHUTDOWN ENG 2. FOUND BP LINE AT ECU NOT TIGHT. R & R FLEX LINE TO ECU BP. R & R ECU AS PREVENTATIVE IAW MM 73 21 01 4. OPERATIONS CHECKED GOOD, WILL TAKE ACFT TO HIGH POWER.

Part: FMU — FAULTY (NR 2 ENGINE) · airframe 47,693 hrs · 28,803 cycles

ON DESCENT, NR 2 ENG REMAINED STUCK AT CRUISE POWER & COULD NOT BE CONTROLLED IN AUTO THROTTLE OR MANUAL THROTTLE. ENG HAD TO BE SHUT DOWN FOR LANDING. HAD POSITIVE OIL PRESS BEFORE & AFTER SHUTDOWN. ENG WAS SHUT DOWN FOR APPROX 10 MINUTES. R&R NR 2 ENGINE FUEL PUMP AND FUEL METERING UNIT REF AMM 73-12-01-04 AND AMM 73-23-00-04, OPS CHECKS NORMAL REF AMM 71-00-00-05. OK TO CONTINUE. RAN ENGINES, REF JRH ALL PARAMETERS NORMAL

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 46,550 hrs · 28,170 cycles

REJECTED TAKEOFF AT 90 KTS, AT 80 KTS CROSS CHECK CAPTAIN`S AIRSPEED TAPE HAD NOT MOVED. NO FLAGS. STANDBY AIRSPEED NORMAL. FLUSHED CAPTAIN'S TOTAL PRESSURE LINES IAW AMM 34-10-00-03 NO BLOCKAGE NOTED. PERFORMED SYSTEM LEAK TEST PER AMM 34-10-00 P BLOCK 501 ALL TESTS PASSED. PERFORMED AFS LAND TEST PER AMM 22-40-00-05. NO DEFECTS NOTED.

Part: PITOT TUBE — DAMAGED (CAPTAIN'S) · airframe 46,550 hrs · 28,170 cycles

REJECTED TAKEOFF AT 70 KTS FOR NO AIRSPEED ON CAPTAIN`S TAPE. REMOVED AND REPLACED PITOT PROBE IAW MM 34-11-15-04. LEAK AND OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 46,303 hrs · 28,013 cycles

GREEN HYD SYS FAILURE IN FLIGHT, DIVERTED. NORMAL APPROACH AND LANDING. ALL EMERGENCY CHECKLIST COMPLIED. GREEN SYS QTY DROPPED TO LOWER END OF GREEN RANGE & ENGINE DRIVEN HYD PUMPS WERE SELECTED OFF AS SOON AS HYD QTY STARTED TO DROP, QTY NEVER CAME CLOSE TO THE "RED DOT" AREA. FOUND ONE CONNECTING LINE JAM NUTS GOING TO THE SELECTOR SOLENOID VALVE LEAKING. REPLACED DAMAGED O-RINGS AND LEAKS CHECKS NORMAL. RAN BOTH ENGINES & CYCLED FLAP/SLATS SEVERAL TIMES, ALL IAW MM CH 29-00-00-03. OK FOR SERVICE.

Part: LONGERON — CRACKED (ZONE 200) · airframe 45,606 hrs · 27,717 cycles

FOUND THREE CRACKS IN AREA"C" OF INNER FLANGE OF THE LONGERON AT STRINGER 11 B/W, FR75 AND FR75A ON LT SIDE CUT OUT THE CRACK FLANGE AND SPLICE REPAIR IAW SRM53-18-18/201, FIG 205C.

Part: LUG — CORRODED (ZONE 600) · airframe 45,606 hrs · 27,717 cycles

RT MLG SUPPORT RIB FWD LUG BORE AND FACES FOUND CORROSION COMPLY WITH EA 6-5710-163177.

Part: LUG — CORRODED (ZONE 500) · airframe 45,606 hrs · 27,717 cycles

LT MLG SUPPORT RIB FWD LUG BORE AND FACES FOUND CORROSION COMPLY WITH EA 6-5710-163175.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 45,606 hrs · 27,717 cycles

LEFT AILERON T/E INBD CORNER FOUND DELAMINATION ON UPPER & LOWER SKIN. REPAIRED THE DELAMINATED AREA PER EA#6-5750-163173.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 45,606 hrs · 27,717 cycles

FOUND TRAPPED WATER IN RUDDER LT SIDE PANEL TRAILING SCREW LINE. REMOVED OUTER SKIN AND CORE IN THE DAMAGED AREA MADE HONEYCOMB CORE PLUG PER SRM 55-41-12/201 FIG 222. DRIED THE REPAIR AREA AT 60 DEGREE FOR AT LEAST 20 HOURS PER SRM 51-77-10. INSTALLED HONEYCOMB CORE PLUG , SMOOTHED HONEYCOMB CORE PLUG, MADE THE OUTER SKIN DOUBLER, & RESTORED THE OUTER DOUBLER PER SRM55-41-12/201 FIG 222. RESTORED FINISH PER SRM51-75-10

Part: RIB — CRACKED (ZONE 600) · airframe 45,156 hrs · 27,539 cycles

RIGHT MLG RIB 5, CRACKED 22MM LENGTH. COMPLIED WITH EA 6-5710-163140.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 43,643 hrs · 26,754 cycles

CRACK RT CENTER FLAP UPPER SKIN BETWEEN RIBS 11 AND 12 REPAIRED IAW SRM 57-50-00 FIG 205, EA 6-5750-153027.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 42,371 hrs · 26,043 cycles

LT WING OTBD FLAP INBD L/E GOUGED APPROX 0.500 IN LENGTH X 0.250IN WIDTH BLENDED AREA ON LT OTBD FLAP INBD L/E REF SRM 51-73-00 NDT FOUND NO CRACK REF NTM 51-10-08 BEFORE BLEND 0.053 MAT LOSS 0.017 IN MAT REMAINING 0.036 IN OUT OF LIMITS REF SRM 57-50-00 REMOVED L/E REPAIR REF SRM 50-40-21 FABBED NEW L/E OUT OF 2024T3-CLAD 0.056 IN TREATED AND PRIMED NEW PART. INSTALLED PART AND TOP COATED IAW SRM 57-50-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION · airframe 42,278 hrs · 25,986 cycles

ON CLIMBOUT, RECEIVED AN AVIONICS SMOKE ECAM, WITH NO SMOKE DETECTED IN COCKPIT. RETURNED TO DEPARTURE. PERFORMED OPS CHECK IAW 26-15-00-05. ALL OPS NORMAL. R & R DETECTORS 11WA, 12WA,13WA AS PRECAUTION, OPS CHECKED NORMAL IAW MM 26-15-00-05. OK TO CONTINUE.

Part: ROLLER — WORN (E/E BAY DOOR) · airframe 41,601 hrs · 25,586 cycles

RIGHT AFTER T/O, GOT AN ECAM WARNING FWD AVIONICS DOOR NOT CLOSED. BOTH PILOTS HAD ABNORMAL PRESSURE IN THE CABIN. IAW QRH. MX FOUND DOOR CLOSED, INSP OF LOCKING ROLLER ON DOOR FOUND WORN REPLACED SAME & CHECKED IAW IPC 52-71-00-01B, ABMM 52-41-14-5, ABMM 52-71-11-4-01. ALSO REPLACED DIODE MODULE 178VD IAW ASM 52-71-00, & FWC 1 ALSO REPLACED & CHECKED IAW ABMM 31-53-34-4, CHECKS GOOD. FOUND EXCESSIVE MOVEMENT & WEAR IN LATCH & WARNING SYS. R & R BEARING. INSPECTED CONNECTOR 11WS, NO FAULTS FOUND. REPLACED 178VD DIODE MODULE AS PRECAUTIONARY IAW WDM 31-53-85. CHECKED SDAC FOR SECURITY & FOUND SDAC SLIGHTLY LOOSE FORE AND AFT IN RACK. TIGHTENED SDAC, ALL OPS NORMAL.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

AIR COND BAY HAS CORROSION ON UPPER SURFACE OF "T" ON FR 39 BETWEEN STR 50 AND STR 51 RT SIDE. REMOVED AND REPLACED "T" SECTION FROM STRINGER 53 RHS TO STRINGER 49 RHS. THE NEW "T" SECTION HAS BEEN SPLICED WITH ANGLE ON AFT FACE AND PLATE ON FORWARD FACE. IN COMPLIANCE WITH EA 6-5310-110880 PT 1.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

BULK CARGO BAY UNDER FLOOR AREA STA FR 66, AND BETWEEN LBL 26 TO LBL43, FLOOR SUPPORT AND "T" CHANNEL HAS CORROSION. REMOVED AND REPLACED "T" CHANNEL/FLOOR SUPPORT ASSEMBLY IAW SRM 51-40-44 AND 51-40-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

MAIN CARGO FLOOR SUPPORT AT RBL 77 HAS CORROSION AROUND FASTENER HOLES FOR FLOORBOARD FROM FR 13A TO FR 16A. REMOVED AND REPLACED FLOORBOARD SUPPORT IAW SRM 51-73-10 AND 51-40-21.

Part: SKIN — GOUGED (ZONE 100) · airframe 39,431 hrs · 24,390 cycles

RT LOWER FUSELAGE AFT OF FR 16A ABOVE STRINGER 40R HAS A 1 INCH GOUGE. INSTALLED DOUBLER REPAIR IAW SRM 53-12-12 FIG 201, PAINTED IAW SRM 53-23-10. STRUCTURAL REPAIR INSPECTION INTERVALS IAW SRI 53-12-12-2-003-0.

Part: SEAT TRACK — CORRODED (ZONE 800) · airframe 39,431 hrs · 24,390 cycles

MAIN CARGO SEAT TRACK EXFOLIATED FROM FR14 C TO FR 19 LBL 37 (YD). REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21 AND 51-40-44.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

MAIN CARGO SEAT TRACK CORRODED FROM FR 14 C TO FR 19, RBL 37 (-YD). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED HOLES AND DRILLED IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

AIRCON BAY AT BILGE AREA BETWEEN FR 41 AND 42 STR 51R HAS CORROSION, BELOW WATER SEPARATOR. REMOVED AND REPLACED STR 51R IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,431 hrs · 24,390 cycles

MAIN CARGO SEAT TRACK EXFOLIATED FROM FR 14C TO FR 19 LBL 17 (YE). REMOVED AND REPLACED SEAT TRACK P/N A53612518200 IAW SRM 51-40-21 AND SRM 51-40-40.

Part: COMPUTER — UNKNOWN · airframe 38,843 hrs · 24,077 cycles

AT FL/340 GOT ECAM FUEL ADVISORY FOR 8000 LBS IMBALANCE. LEFT INNER TANK DECREASING SLOWLY THROUGH 2000 LBS IAW QRH, PULLED AND RESET FQI CHAN 1 AND 2 C/B, NO HELP. ALL COCKPIT INDICATIONS: QTY, FUEL USED, MANUAL FUEL CALCULATIONS INDICATED LOSS OF 8-10,000 LBS OF FUEL. DIVERTED TO KMCI. PERFORMED A VISUAL CHK FOR EVIDENCE OF FUEL LEAK AND NONE FOUND. ALL FUEL INDICATIONS AND STICK READINGS AGREE. FQIS BITE SHOW NO HARD CODE. FUELED LT INNER TANK TO A KNOWN QTY USING STICK READING OF 67, OR 10.600 LBS. APPLIED MEL 28-42-01-04.

Part: SKIN — CHAFED (ZONE 500) · airframe 38,404 hrs · 23,857 cycles

FOUND ABRASION AT SLAT NR 1 LT ON TRAILING EDGE LOWER SKIN RIB 21. REPAIR PERFORMED BY INSTALLING A EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-70335 AND RAS/FOK172/2003 ISS A.

Part: SKIN — DELAMINATED (ZONE 300) · airframe 38,404 hrs · 23,857 cycles

FOUND DELAMINATION AT RUDDER SIDE PANEL IN THE AREA OF HINGE ATTACHMENT FITTINGS, LT: BR1, BR4, BR5, BR6, BR7 RT: BR1-BR6 REPAIR PERFORMED IAW SRM 55-41-12 FIG 216.

Part: STRINGER — FAILED (ZONE 100) · airframe 38,404 hrs · 23,857 cycles

FOUND OLD STRINGER REPAIR C20-21, P 54 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10-14 FIG 201.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT PROFILE C 54.2-54.3 P51 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT SPLICE C 19, P 52 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT CORNER FITTING C32 LT AND RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT STRINGER P 51 LT, C 59-60; P 52 LT AT C58-59 AND P 53 LT AT C58-59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: WEDGE — CORRODED · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT WEDGE C 59-60, P 52 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT CROSS BEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT FITTING C63. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND AT LT PYLON SPAR RIB 18 AT PYLON TO WING FITTING CORROSION. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5440-70338 AND RAS 027276/007/2003.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 38,404 hrs · 23,857 cycles

FOUND ABRASION AT SLAT NR 1 RT TRAILING EDGE LOWER SKIN RIB 21 REPAIR PERFORMED BY INSTALLING AN EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-7034 AND RAS/FOK/173/2003 ISS A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT TOP CAP BEAM UPPER FLANGE 27. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT STRINGER SEGMENT C65 P 35 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT TOP CAP BEAM C64 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: SKIN — DENTED (ZONE 500) · airframe 38,404 hrs · 23,857 cycles

FOUND DENT AT SLAT NR 1 LT ON LOWER TRAILING EDGE SKIN NEAR RIB 23 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5742-70345 AND RAS/FOK/197/2003 ISS A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT FLANGE OF TOP CAP BEAM C 32. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: STRINGER — FAILED (ZONE 100) · airframe 38,404 hrs · 23,857 cycles

FOUND OLD STRINGER REPAIRS C20-21, P 53 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10-14 FIG 201.

Part: BEAM — CORRODED (DRUEGER FLAP) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT BEAM C 38-39 KRUEGER FLAP FWD FAIRING RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT STRINGER SEGMENT P 44 RT, C 26 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT FITTING OF DOOR SILL BEAM C25 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT CORNER FITTING C33 LT AND RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT STRINGER SEGMENT P 45 LT, C 26. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 500) · airframe 38,404 hrs · 23,857 cycles

FOUND AT LT AFT WING TO PYLON FITTING PITTING MARKS INTO THE PYLON LUG BORE REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5720-70339 AND RAS /BAE/1352/2003 ISS A.

Part: BULKHEAD — DAMAGED (ZONE 400) · airframe 38,404 hrs · 23,857 cycles

FOUND DENTS AT PRESSURE BULKHEAD FLOOR STRUCTURE C 49-50 (WITH CRACK 2MM) AND C 50-51 AT TR 4-5 LT ; C 52-53 AT TR 2-3 LT, C 48-49 AT TR 4-5 RT. REPAIR PERFORMED BY INSTALLING A DOUBLER AT TR 4-5 LT, C49-50 AND LET THAT DENTS AT THE OTHER AREAS AS IT IAW EA 6-5315-70336 AND RAS/AS/0282/2003 ISS A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT STRUT OF TOP CAP BEAM C 38.2, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT FLANGE OF TOP CAP BEAM C 30 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,404 hrs · 23,857 cycles

FOUND CORROSION AT TOP CAP BEAM C63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SHIM — CHAFED (ZONE 200) · airframe 38,387 hrs · 23,847 cycles

FOUND SCRUB MARKS AT TORSION BOX LT/RT CROSS SHIM C 56-57, P 15A-16 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A.

Part: SHIM — DENTED (ZONE 200) · airframe 38,387 hrs · 23,847 cycles

FOUND SCRUB MARKS AT TORSIONS BOX EMERGENCY EXIT ON LT/RT CROSS SHIMS C56-57A, P15A-16. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,387 hrs · 23,847 cycles

FUSELAGE SKIN AT LAP JOINT P 51, C 19-20 INTERNAL CORRODED REPAIR PERFORMED BY CUT OUT THE LAP JOINT AND INSTALL EXTERNAL DOUBLER IAW DRAWING R537-06279, APPROVED BY RAS/DABRE/7003251/2003 ISS A.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,387 hrs · 23,847 cycles

FOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: PANEL — CRACKED (ZONE 100) · airframe 38,387 hrs · 23,847 cycles

CRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,387 hrs · 23,847 cycles

CORROSION ON SKIN INNER COUPLING PLATE AT C19, P53-54 REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW REA 6-5313-70343 AND RAS/DABRE/700324/2003 ISS A.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,387 hrs · 23,847 cycles

FOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CRACKED (ZONE 100) · airframe 38,387 hrs · 23,847 cycles

CRACKS FOUND AT FRAME 47 INTERNAL FITTING LT HOLE NR E (1MM) IN REAR SPAR, HOLE NR G (2MM) IN CORNER FITTING, HOLE NR I (2MM) IN FWD FITTING, HOLE NR N (2MM) IN FWD FITTING, REPAIR PERFORMED BY OVERSIZING THE HOLES (E,G,N) UNTIL CRACK REMOVAL AND CUT OUT THE EXTERNAL FITTING PER SB 57-6049 ON HOLE NR I AND INSTALL A CONICAL WASHER IAW EA 6-5710-73899 AND RAS/AS/310/2003 ISS A.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,387 hrs · 23,847 cycles

FOUND CORROSION AT SKIN PANEL C39-40, P28-32 RT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R538-10533, APPROVED BY EA 6-5315-70344 AND RAS/AS/0273/2003 ISS A.

Part: THRUST REVERSER — UNKNOWN (NR 1) · airframe 38,162 hrs · 23,708 cycles

ON POWER-UP FOR TAKEOFF, NR 1 REVERSE UNLOCK LIGHT ILLUMINATED. EXTINGUISHED AFTER RETURNING THROTTLES TO IDLE. RETURNED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 28JUL07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2. NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." [07-27-07] R & R RESSURE REGULATING AND SHUT OFF VALVE PER MM 78-31-05-4. REACTUATED TR PER MM 78-31-00-9. OP'S CHECKS NORMAL PER MM 78-31-00-5 AND PER A300. OKAY FOR SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 36,805 hrs · 23,004 cycles

ON CLIMBOUT DEPARTURE CONTROL INFORMED US THAT TOWER SAID WE WERE EMITTING BLACK SMOKE OUT OF NR 1 ENGINE. ALL ENGINE PARAMETERS INDICATED NORMAL. ELECTED TO MAKE A PRECAUTIONARY LANDING. PER CREW DEBRIEF- CAPT REPORTED ALL NORMAL INDICATIONS, ON INBND LEG TO LAX TOWER REPORTED NO BLACK SMOKE NOTED, FLIR IMAGING ALSO WAS USED ON FINAL APPROACH BY LAX OPERATION DEPT, WITH NO UNUSUAL HEAT PATTERNS OR FLARE UPS NOTED. INSPECTED ENG - FOUND HYD LEAK AT BLUE SYS MANIFOLD, REPLACED FILTER BOWL AND FILTER - RAN ENG WITH NO EVIDENCE OF SMOKE AMM 29-11-36-3 & JRH CHAP 5-6

Part: REPAIR — UNKNOWN · airframe 35,934 hrs · 22,553 cycles

RIGHT WING NR 3 SLAT EXISTING REPAIR REQUIRES FILLER TO BE REMOVED FOR NDT OF DOUBLER FOR MATERIAL IDENTIFICATION FOR ASSESSMENT OF REPAIR REF N00300. REMOVED AND REINSTALLED FILLER IAW A300-600 SRM 51-40-21.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,934 hrs · 22,553 cycles

DENT IN UPPER FUSELAGE SKIN AT FRAME 69 BETWEEN STR 8L AND 9L APPROX 1.5 X 2" REF N00054. REPAIRED DENT IAW EA 6-5330-97635.

Part: CONTROL HEAD — FAILED (ILS RECEIVER) · airframe 35,874 hrs · 22,519 cycles

ILS RECEIVER UNTUNABLE ON DESCENT INTO CLE. DIVERTED TO KPIT. REMOVED AND REPLACED ILS CONTROL HEAD. OPS CHECKS GOOD REF: A300 MM 34-36-15-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 889-2323-006, POS ONL SRL 145 TAG 67288A, ON MFG 889-2323-007, SRL 4131.

Part: SWITCH — LOOSE (PAX DOOR) · airframe 35,704 hrs · 22,429 cycles

AVIONICS LIGHT/CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCH. OPS NORMAL PER A300 MM REF 52-41-14-5 DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT.

Part: SWITCH — LOOSE (PAX DOOR) · airframe 35,708 hrs · 22,432 cycles

AVIONICS LIGHT, CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LANDING WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCH. OPS NORMAL PER A300 MM REF 52-41-14-5 DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT.

Part: SWITCH — LOOSE (E/E BAY DOOR) · airframe 35,700 hrs · 22,428 cycles

AVIONICS LIGHT, CHIME CAME ON PASSING 10000, EXECUTED TURNBACK TO KSMP BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE/ RETIGHTENED. SWITCH OPS NORMAL PER A300 MM REF 52-41-14-5. DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT.

Part: SMOKE DETECTOR — MALFUNCTIONED (AVIONICS) · airframe 35,561 hrs · 22,354 cycles

AVIONICS SMOKE WARN DURING CLIMB-OUT. COMPLIED WITH CHECKLIST. DID NOT SMELL SMOKE. RETURNED TO KMCO. REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR 13WA. OPERATIONAL TEST WAS NORMAL. REF A300 M/M 26-15-12-4 AND 26-15-00-5. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG CG7G0-11 POS AV3 SRL AB1954 TAG A08167 ON MFG CG7G0-11 SRL 728, TAG 172443.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,850 hrs · 21,945 cycles

FRAME 45 RT SIDE JUST ABOVE STRINGER 27 FRAME FITTING HOLE NR H2 MEASURE AT .372 DIA UPON REMOVAL OF FASTENER FOR NDT ON EO NR E6-5310-7-5006 PT 4. REF N CARD N00061. COMPLIED WITH EA 6-5310-90201 PT2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,850 hrs · 21,945 cycles

FRAME 41 LT SIDE BETWEEN STRINGERS 25 AND 26 FRAME FITTING HOLE H1 HAS A BUSHING INSTALLED WITH A FASTENER HOLE AT 2ND OVERSIZE AT .278 DIA FOUND UPON REMOVAL OF FASTENER FOR NDT ON EO 6-5310-7-5006 PT3 REF N CARD N00059. COMPLIED WITH EA 6-5310-90201 PT1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,850 hrs · 21,945 cycles

FRAME 46 RT SIDE AT STRINGER 27 FRAME FITTING HOLE NR H1 HAS A BUSHING IN THE FITTING MEASURING AT .436 DIA WITH A 2ND OVERSIZE HOLE AT .278 DIA FOUND UPON REMOVAL OF FASTENER ON EO 6-5310-7-5006 PT4 REF N CARD N00062. COMPLIED WITH EA 6-5310-90201 PT1.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 33,526 hrs · 21,218 cycles

LOST NEARLY ALL GREEN HYDRAULIC QUANITY DURING CRUISE AT FL 290. FOUND LT HYD PUMP SHAFT SEAL LEAKING. REMOVED AND REPLACED LT OR FWD HYD PUMP ON NR 2 ENG ISW M/M 29-11-32-4-1, OPS AND LEAK CHECK, GOOD.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 33,187 hrs · 21,001 cycles

INFLIGHT AVIONIC SMOKE WARNING AT FL 310 SEVERAL WARNINGS ON AND OFF DURING ICING CONDITIONS THEN OFF WHEN CLEAR FOR SEVERAL MIN THEN ON CONTINUOUSLY. DIVERTED INTO DEN 170NM OUT, FOLLOWED ECAM PROCEDURES NEVER NOTICED ANY SMOKE. UNEVENTFUL LANDING AND TAXI IN. TROUBLESHOT PER TSM261500 P101, REMOVED AND REPLACED CARGO SMOKE DETECTOR 13WA PER AMM-2619124. OPS CHECK NORMAL. CREW ADVISED SNIFFER USED, NO SMOKE DETECTED. MX CHECKED AND CONFIRMED NO SMOKE DURING OPS CHECK.