N810FD

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 398 hrs · 13,011 cycles

DURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER TAKEOFF & WHEELS UP, THE ALERT CAME BACK ON. NO ADVERSE CONTROL WAS NOTICED. COMPLIED WITH ECAM. BROUGHT NR 2 ENGINE TO IDLE & RETURNED TO LAND WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 THRUST REVERSER STOW & DEPLOY SWITCH IAW AMM 78- 31-40-04. PERFORMED HIGH POWER RUN IAW AMM 71-00-00-05 & JRH. PERFORMED OPS TEST OF THRUST REVERSER TRANSLATING SLEEVES, FOUND NORMAL IAW AMM 78-32-11-05.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 394 hrs · 12,809 cycles

REPEAT WRITE UP, STBY ALTIMETER WITHIN 30' OF PRIMARY ALTIMETERS ON THE GND. AT FL 300 STBY ALTIMETER WAS 160 FT HIGHER, AT FL 148 STBY ALTIMETER WAS 250 FT HIGHER. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW AMM 33-13-00-05. ACFT OK FOR SERVICE.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 394 hrs · 12,809 cycles

AT CRUISE ALTITUDE 35,000, STBY ALTIMETER INDICATES 250 HIGHER THAN BOTH CAPTAINS & COPILOTS ALTIMETERS. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW AMM 33-13-00-05. ACFT OK FOR SERVICE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 393 hrs · 12,729 cycles

COMPLY WITH WRI 25-50/0216 & 0217, REPAIR THE SEAT TRACK ASSEMBLY OF MDC FRAME 54.2 - 58 RESTRAINT ID N1199. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 202. THIS REPAIR CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 38,226 hrs · 12,197 cycles

DURING DESCENT, RECEIVED AN INTERMITTENT CHIME, WITH NO ECAM ALERT, INVESTIGATION FOUND LOW FUEL TANK AT 1.5 & RO AT 1.7. THE CENTER TANK WAS FEEDING & TRIM TANK TRANSFERRING FWD. UNABLE TO RECOVER INNER FUEL TANK & APPROXIMATELY 17600 LBS OF FUEL WAS TRAPPED AT SLAT EXTENSION. THE FUEL FEED DID NOT REVERT TO THE INNER TANKS & CENTRE TANKS CONTINUED TO BURN. LEFT & RT OUTER MAINTAINED 1.5 & 1.7 RESPECTIVELY, AT APPROXIMATELY 400. ON APPROACH THE FUEL FEED SWITCHED TO INNER TANK & THE CTR TANK PUMPS SHUT DOWN. R & R RELAYS IAW SMP. PERFORMED AUTO FUEL FEED OPS & FUNCTIONAL TESTED IAW AMM 28-21-00-05. CENTER TANK LOW LEVEL SENSOR CHECKED NORMAL IAW AMM 28-46-00-05, FUNCTIONAL TEST, ACFT OK FOR SERVICE.

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 37,878 hrs · 12,037 cycles

EQUIPMENT BAY SMOKE INDICATION, SEVERAL MINUTES AFTER, HEARD A LOUD BANG. UNKNOWN WHERE SOUND COME FROM. FIRE WARNING ILLUMINATED SEVERAL TIMES. DID NOT SMELL SMOKE. PERFORMED SMOKE DETECTION OPS TEST IAW AMM 26-15-00-05, FOUND SMOKE ECAM WARNING AND COULD NOT RESET. R & R MIN EQUIPMENT BAY SMOKE DETECTOR (12WA) IAW AMM 26-15-12-04, PERFORMED OPS TEST IAW AMM 26-15-00-05,SATISFIED. EXAMINED MIN EQPT BAY RACK AND WIRING BUNDLE, NORMAL, NO SIGN OF HEATING OR OTHER DAMAGE. ACFT EXTERNAL INSPECTION NORMAL, ALSO INSPECT ALL CARGO COMPARTMENTS AND ALL WHEELWELLS, AVIONICS COMP, AIR CONDITIONING COMPARTMENT, ALL NORMAL. PERFORMED APU BLEED AIR OPS TEST IAW AMM 36-12-00-05, SATISFIED, NO LEAK FOUND.

Part: FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 37,873 hrs · 12,034 cycles

RT WING MLG FITTING OF RIB 5 FORWARD LUG CORRODED, COMPLY WITH EA6-5710-T0302341A.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 37,873 hrs · 12,034 cycles

LT WING MLG FITTING OF RIB 5 FORWARD LUG FOUND CORROSION, COMPLY WITH EA 6-5710-T0302340.

Part: HYDRAULIC SYSTEM — WARNING MESSAGE (GREEN) · airframe 36,212 hrs · 11,254 cycles

DURING CLIMB, HAD GREEN SYS OVERHEAT ECAM. COMPLIED WITH CHECKLIST, MANUALLY EXTENDED LANDING GEAR TOWED OFF RUNWAY. DRAINED AND SERVICED GREEN SYS HYD RESERVIOUR PER MM 29-14-00-03. RAN NR 1 AND 2 ENGINES IAW JRH. ALL INDICATIONS AND PARAMETERS NORMAL. PERFORMED FLT CONTROLS CHECK PER MOCC WITHOUT GREEN SYSTEM PRESSURIZED. ALL FLIGHT CONTROLS SURFACE MOVEMENT WAS SMOOTH AND PHYSICALLY MATCHED WITH ECAM INDICATIONS.

Part: HYDRAULIC SYSTEM — MULTIPLE FAIL (NR 1 GREEN SYS) · airframe 35,871 hrs · 11,094 cycles

DURING CRUISE FLIGHT, HYD GREEN SYS RESERVOIR OVERHEAT ILLUMINATED ON ECAM. GREEN HYD PUMPS SECURED UNTIL APPROACH. TURNED BACK ON LOW POWER LIGHTS ILLUMINATED, NO GREEN HYD QUANTITY INDICATED. R & R NR 1 AND NR 2 ENGINE PUMPS OF GREEN SYS IAW MM 29-11-32-04-01, R & R NR 1 AND NR 2 ENGINE PUMP CASE DRAIN FILTERS IAW MM 29-11-36-04-01. R & R NR 1 AND NR 2 ENGINE GREEN PUMP DELIVERY FILTERS IAW MM 29-11-42-03. R & R GREEN RESERVOR FILTER IAW MM 29-11-15-03. DRY MOTOR ENGINES IAW JRH AND CHECK NO LEAKAGE. R & R NR 1 ENGINE PUMP CASE DRAIN FILTER AGAIN, PERFORMED GREEN HYD LINE FLUSH IAW MM 12-36-29-00. DRY MOTOR CHECK NO LEAKAGE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 34,138 hrs · 10,355 cycles

1 HR INTO FLIGHT, CABIN PRESSURE EXCEEDED TOLERANCE (AROUND 9.0 ON DEFFERENTIAL PRESSURE) AND BOTH CONTROLLERS FAILED. HAD TO SELECT MANUAL AGAIN TO BRING PRESSURE BACK DOWN. REACTIVED AFT OUTFLOW VALVE IAW MEL21-31-04-01-A, PERFORMED BITE TEST FOUND "AFT VALVE" TEST FAIL ON BOTH CPCS. R & R AFT PUTFLOW VALVE AND TEST ALL SATIS IAW AMM 21-31-12. REGARDING THE CONTINUITY OF THE WIRINGS, FOUND THERE ARE DIODES BETWEEN PN:14A, 14B AND GROUND. BYPASSED THE DIODES, CHECKED WIRINGS NORMAL,TESTED THE DIODES ALOO NORMAL REF ASM 21-31-00.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132YF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132YF PER SAMPLE IAW SRZ 25-005,ON TRAVELER NR T8/773385.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 232, FLOOR PANEL 323RG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 232RG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773437.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231QG HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL NR 231QG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773436.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132RF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132RF PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773389.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132ZF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132ZF PER SAMPLE IAW SRZ 25-005,ON TRAVELER T8/773387.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS ZONE 131, FLOOR PANEL 131QG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 131QG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773386.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

MAIN CARGO COMPARTMENT ZONE 241, FLOOR PANEL NR 241BK HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773452.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231LH HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005,ON TRAVELER NR T8/773432.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252UH HAS STRUCTURAL DAMAGES FABRICATED NEW FLOOR PANEL NR 252UH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773453.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231NH HAS STRUCTURAL DAMAGES FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005, ON TRAVELER 3 T8/773431.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241QJ HAS STRUCTURAL DAMAGES. FABRICATED NEW CARGO PANEL NR 241QJ PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773440.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252CH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK PANEL NR 252CH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773455.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241WH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 241WH PER SAMPLE IAW SRZ 25-005 ,ON TRAVELER NR T8/773451.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132QF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132QF PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773388.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231VH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 231VH PER SAMPLE, ON TRAVELER NR T8 /773390.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

BULK CARGO COMPARTMENT, ZONE 161 FLOOR PANEL 161BF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 161BF PER SAMPLE, IAW SRZ 25-011 ON TRAVELER.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773439.

Part: RIB — CRACKED (ZONE 500) · airframe 31,762 hrs · 9,141 cycles

LEFT WING TIP RIB WY489 CRACKED REMOVED CRACKED RIB WY489.0 IAW SRM 51-40-21. FABRICATED NEW RIB ON TRAVELER NR T8/773917, BATCH NR 436186A1. INSTALLED RIB IAW SRM 51-40-21, AND 57-30-11.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN DECK CARGO COMARTMENT, ZONE 231 FLOOR PANEL 231 AJ HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN CARGO DECK COMPARTMENT FLOOR PANEL 231 AJ PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773438

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773439.

Part: FLOOR PANEL — DAMAGED (ZONE 400) · airframe 31,762 hrs · 9,141 cycles

BULK CARGO COMPARTMENT ZONE 161,FLOOR PANEL 161GF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 161GF PER SAMPLE IAW SRZ 25-011.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANEL, ZONE 131 FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL PER SAMPLE , PANEL 131 HG IAW SRZ 25-005 ON TRAVELER T8/ 773384.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,762 hrs · 9,141 cycles

MANI DECK CARGO COMPARTMENT,ZONE 251 FLOOR PANEL 251 ZH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251 ZH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773454

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

AFT CARGO COMPARTMENT FLOOR PANELS ZONE 151, FLOOR PANEL 151AF HAS STRUCTURAL DAMAGE. FABRICATED NEW FLOOR PANEL 151AF PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/775133.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 31,762 hrs · 9,141 cycles

BULK CARGO COMPARTMENT ZONE 162, FLOOR PANEL 162HF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 162HF PER SAMPLE IAW SRZ 25-011 ON TRAVELER.

Part: DOUBLER — DAMAGED (LT MLG WW) · airframe 31,762 hrs · 9,141 cycles

THE LT MAIN GEAR WHEEL WELL DOOR INNER AFT TIRE RECESS HAS A 1 INCH GROVE AT THE FWD OTBD SIDE BLENDED AREA ORIG MAT .063 REMAINING MAT IS OUT OF LIMITS, REMOVED DAMAGE. HFEC, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER IAW SRM51-71-30 FIG 102.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 31,762 hrs · 9,141 cycles

FWD CARGO COMPARTMENT FLOOR PANELS, ZONE 131, FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL, IAW SAMPLE,PANEL 131 HG, IAW SRZ-25-005,ON TRAVELER, NR T8/773384.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,762 hrs · 9,141 cycles

AIR CONDITIONING COMPT BETWEEN FR44 AND FR45, STR 38R AND 39R HAS SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10, MATERIAL LOSS .001 IN. TREATED AND PRIMED IAW SRM 51-21-10, PAINTED IAW MM 75-10-08.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,762 hrs · 9,141 cycles

MAIN CARGO DECK SEAT TRACK AT RBL 18 HAS EXFOLIATION FROM FR 19 TO FR 14B. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44, P/N A538320202400 BATCH 0001549861. INSTALLED SEAT TRACK IAW SRM 51-40-21.

Part: COMPUTER — FAILED (TE FLAPS) · airframe 31,503 hrs · 8,974 cycles

ON APPROACH TO KBUR APPROX 5000' MSL, WHEN SELECTING 20 DEGREES FLAP, T/E FLAPS STUCK AT 15 DEGREES WITH SYS 1 AND 2 FLAP FAULT LIGHTS ILLUMINATED. DIVERTED TO LAX. LANDED WITH 30/15 IAW QRH PROCEEDURES. PERFORMED THE REMAINING OF THE T/S AND FOUND NO DEFECT. REMOVED AND REPLACED SFCC 1 AND 2 IAW MM 27-51-18-4.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 31,321 hrs · 8,850 cycles

HYD GREEN SYSTEM LOW LEVEL IN FLIGHT. ECAM WARNING, MANUAL EXTENTION OF L/G. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE IAW AMM 20-23-11-0, LEAK CHECK GOOD. REPLENISHED GREEN HYDRAULIC SYSTEM IAW AMM 29-10-00-3. CREW SHUT HYD SYS DWN, NO PUMP CAVITATION/DAMAGE. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE IAW AMM 20-23-11-0. LEAK CHECK GOOD. REPLENISHED GREEN HYDRAULIC SYSTEM IAW AMM 29-10-00-3.

Part: BULKHEAD — DAMAGED (ZONE 100) · airframe 29,920 hrs · 8,012 cycles

SCRATCH IN PRESSURE BULKHEAD AT C54, TR 4 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101318 AND RAS/045121/010/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,920 hrs · 8,012 cycles

CORROSION ON SEVERAL AREAS AT AIR CONDITIONING COMPARTMENT, C39-C47, P44-P54 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101310 AND RAS/045255/008/2006 ISSUE "A".

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,920 hrs · 8,012 cycles

FOUND CORROSION AT MILLED FRAME C49, P14-P15 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101284 AND RAS/DATLS/00032002006 ISSUE "B".

Part: ANGLE — CRACKED (ZONE 800) · airframe 29,920 hrs · 8,012 cycles

CRACKED ANGLE ON EMERGENCY EXIT DOOR INTERNAL STRUCTURE, UNKNOWN CRACK LENGTH. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — DENTED (ZONE 200) · airframe 29,920 hrs · 8,012 cycles

DENT IN OUTER SKIN AT C20, P24-25, RHS. REPAIR PERFORMED BY SMALL BLEND OUT IAW EA 6-5313-101308 AND RAS/DABRE/7006763/2006 ISSUE "A".

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,920 hrs · 8,012 cycles

DUE TO REMOVAL OF SOME FASTENERS DURING REMOVAL OF CORROSION ON OUTER SKIN AT C80, P5-6 RHS IT WAS IMPOSSIBLE TO REINSTALL SOME FASTENERS WITHOUT DAMAGING THE AFT PRESSURE BULKHEAD. REPAIR PERFORMED BY INSTALLATION OF FOUR ALTERNATE BOLTS NSA 6603-5, APPROVED BY EA 6-5319-103240 AND RAS/DAHAM/4020934/2006 ISSUE "A".

Part: VANE — CHAFED (ZONE 600) · airframe 29,920 hrs · 8,012 cycles

CHAFING MARKS AT INBOARD FLAP VANE, RHS. REPAIR WAS PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5752-101309 AND RAS/DABRE/7006736/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,920 hrs · 8,012 cycles

SEVERAL AREAS OF CORROSION IN AIR CONDITIONING COMPARTMENT, C39-C44, P37-50 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101310 AND RAS/045255/008/2006 ISSUE "A".

Part: SKIN PANEL — CORRODED (ZONE 300) · corrosion level 2 · airframe 29,920 hrs · 8,012 cycles

FOUND CORROSION AT UPPER SKIN PANEL C91, P4 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5319-103315 AND RAS/DAHAM/4020861/2006 ISSUE "A".

Part: FITTING — CORRODED (ZONE 800) · corrosion level 2 · airframe 29,920 hrs · 8,012 cycles

CORROSION ON FITTING LT FWD PAX DOOR (P/N A521-11301-004, S/N G-1264). REPAIR PERFORMED BY REPLACEMENT OF PART IAW EA 6-5211-103243 AND RAS/AS/104/2006 ISSUE "A".

Part: SPAR — CRACKED (ZONE 400) · airframe 29,920 hrs · 8,012 cycles

A 16MM LONG CRACK WERE FOUND IN THE END OF THE STIFFENER RIB 10 ON PYLON NR 2 LOWER SPAR. REPAIR PERFORMED IAW SB A310-54-2016, APPROVED BY EO 6-5450-7-3302 PT 6.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 29,920 hrs · 8,012 cycles

FOUND CRACKED HOLES DURING ACCOMPLISHMENT OF EO 6-5310-7-5020 PT.1, LHS (C43 HOLE H2 CRACK LENGTH 9MM; C45 HOLE H22 CRACK LENGTH 7MM; C46 HOLE H29 CRACK LENGTH 8MM). REPAIR PERFORMED BY REPLACEMENT OF FITTING A538-70064 FOR HOLE H2, OVERSIZING HOLE H22 AND H29 AND BUSH INSTALLATION IAW EA 6-5315-101331 AND RAS/AS/0133/2006 ISSUE "B".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORRODED TOP CAP FLOORBEAM AT C33 LT. REPAIR PERFORMED BY SPLICING IAW SRM 53-10-15 / FIG.207.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 29,919 hrs · 8,011 cycles

CORROSION ON PYLON NR 2 BEARING HOLE ON RIB 18 LOWER ATTACH FITTING. REPAIR PERFORMED BY REAM UP HOLE AND CHAMFER ON EACH SIDE IAW SB: A310-54-2021 AND EA 6-5451-103241.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORROSION ON SEAT TRACK, C15A-C19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 71-52-10.

Part: FAIRING — CRACKED (ZONE 500) · airframe 29,917 hrs · 8,010 cycles

CRACK FOUND AT INNER SKIN OF NR 4 LT FLAP MOVABLE FAIRING. REPAIR PERFORMED BY BONDING IAW SRM 57-20-35 AND EA 6-5720-99236 AND RAS/FOK/126/2006 ISSUE (A).

Part: SKIN — DENTED (ZONE 800) · airframe 29,917 hrs · 8,010 cycles

OLD DENT ON BULK CARGO DOOR LOWER LT CORNER WITH RAS/DATLS/0002170/2004 WITH TEMPORARY LIMIT OF ONE UNPRESSURIZED FERRY FLIGHT. PERMANENT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW. EA 6-5234-101283 AND RAS/DABRE/7006682/2006 ISSUE (A).

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORROSION FOUND ON LONGERON A536-11644-220, C11-C14, Y 770. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.

Part: SKIN — WORN (ZONE 500) · airframe 29,917 hrs · 8,010 cycles

ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).

Part: SKIN — WORN (ZONE 600) · airframe 29,917 hrs · 8,010 cycles

ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORRODED STRINGER P44 LT AND RT, C16A-C17. STRINGER REPAIR PERFORMED IAW. SRM 53-12-14 / FIG.201. (RUN OUT FITTING INSTALLATION; PN A536-10607-206, -207)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORRODED LONGERON C12A-C14, Y1959. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG 207.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORROSION ON LONGERON C11-C15A, Y-1456. REPAIR PERFORMED BY T-SPLICE REPAIR IAW SRM 53-12-15 / FIG.207.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,917 hrs · 8,010 cycles

CORRODED LONGERON C11-C15A, Y-450. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG.207.

Part: PANEL — DELAMINATED (ZONE 300) · airframe 29,917 hrs · 8,010 cycles

DELAMINATION AT VERTICAL STABILIZER L/E PANEL NR 3. REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW. SRM 51-77-12 / FIG.211, APPROVED BY EA 6-5532-101302 AND RAS/DAHAM/4020826/2006 ISSUE (A).