N434FE

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT STRINGER SEGMENT C65, P56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION ON STRINGER SEGMENT P 43, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT STRINGER SEGMENT C 72, P45 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSS STRUT C 87 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSSBEAM C 63 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,253 hrs · 19,690 cycles

FOUND CORROSION AT RT EMERGENCY EXIT DOOR FRAME SEGMENT 3.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT DOUBLER C54, P14, P15, P16, P25 (LT) AND P14, P15, P17, P25 (RT). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT AFT CARGO DOOR INNER SKIN, BETWEEN LONGERON 4-5. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT STRINGER SEGMENT C 72, P45 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT STRINGER SEGMENT C65, P54 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CORNER FITTING C 63, P 44 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSS STRUT AT C87 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,253 hrs · 19,690 cycles

FOUND CORROSION AT EMERGENCY EXIT DOOR FRAME SEGMENT 2.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 300) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSS STRUT C 84 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT STRINGER SEGMENT C 65, P43LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSS STRUT C 84 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

CORROSION FOUND AT CROSS STRUT C 86 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION ON STRINGER P44 RT, C 34-35 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,250 hrs · 19,689 cycles

FOUND CORROSION AT CROSS BEAM C67 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FRAME — DAMAGED (ZONE 100) · airframe 44,250 hrs · 19,689 cycles

FOUND MISDRILLED HOLES AT FRAME SEGMENT C 59, P47 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 44,253 hrs · 19,691 cycles

FOUND OLD INTERNAL DOUBLER REPAIR AT FWD CARGO DOOR SKIN WITH ADDITIONAL DENTS AND SCRATCHES. REPAIR RENEWED BY EXTERNAL DOUBLER IAW SRM 52-30-00 FIG 203, APPROVED BY EA 6-5230-73905.

Part: SKIN — WORN (ZONE 600) · airframe 44,246 hrs · 19,687 cycles

FOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, RT WING BOTTOM SKIN REPAIR PERFORMED IAW DRAWING R572-59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT FITTING OF CROSSBEAM C 55/58 , P45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: BEAM — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT RT EMERGENCY EXIT DOOR, BEAM NR 5. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON RUN OUT FITTING AT STRINGER P 44, C 16A-17. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P44, C60-62 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P56 LT, C65-69 STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201.

Part: PANEL — DELAMINATED (ZONE 300) · airframe 44,246 hrs · 19,687 cycles

VERTICAL STABILIZER LEADING EDGE PANEL 322CL WAS DELAMINATED. THE DIMENSION FOR REPAIR IAW SRM TO GREAT. REPAIR PERFORMED IAW SRM 55-32-00 FIG 203 AND FIG 216, APPROVED BY EA 6-5532-81077 AND RAS/DAHAM/4018735/2004.

Part: SKIN PANEL — CHAFED (ZONE 500) · airframe 44,246 hrs · 19,687 cycles

FRETTING DAMAGE ON LT BOTTOM SKIN PANEL NR 2, RIB 8-9 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-81068 AND RAS/BAE/1126/2004 ISS A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT CROSS BEAM C 60, REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 52LT, C 38.1-38.2. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT FRAME C75A, P11. REPAIR PERFORMED IAW SRM 53-18-13 FIG 202.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P 45 LT, C67-69 AND P 48 LT, C 65-66 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P 56 LT, C69-70 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P57 , C69-71 AND P56 RT, C 70-72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 31RH, C 54.2. STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201.

Part: BOX BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

CORROSION AND CRACKS FOUND ON RT AFT PAX DOOR UPPER TORSION BOX BEAM, C 73-75A, P 9-11. REPAIR PERFORMED BY CUT OUT THE DAMAGED PARTS, INSTALLING REPAIR PART AND FILLER IAW EA 6-5318-81066 AND RAS/DAHAM/4018653/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P 50 RT, C 23-25 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT EMERGENCY EXIT DOOR, BEAM NR 5 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

CORROSION FOUND AT LT AFT PAX DOOR FRAME INNER FLANGE C73A, P 26-27 LT. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW EA 6-5318-81048 AND RAS/DATLS/0002044/2004 ISS. A

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION OUT OF LIMIT AT CROSSBEAM C 65 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION IN AFT CARGO COMPARTMENT AT CROSSBEAM C 55/58 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 201.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT SEAT TRACK C 15A-C19, Y-1959. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: PANEL — DENTED (ZONE 400) · airframe 44,246 hrs · 19,687 cycles

DURING ACCOMPLISHMENT OF EO 6-5450-7-3304 (SB 54-2026 EMBODIMENT) FOUND AT PYLON NR 2 AN OLD CRACK REPAIR AND LOWER SKIN WAVINESS. REPAIR PERFORMED BY STRAIGHTEN OUT THE DENTED AREA AND INSTALLING REPAIR PARTS AND DOUBLER IAW DRAWING R546-10305, APPROVED BY EA6-5450-81073 AND RAS 032684/009/2004 ISS A.

Part: SKIN — DENTED (TE FLAP) · airframe 44,246 hrs · 19,687 cycles

DENT FOUND AT LT INBOARD FLAP, RIB 18-19, P 4-5 REPAIR PERFORMED IAW SRM 57-52-12 FIG 205, APPROVED BY RAS/DABRE/7004356/2004 ISS A.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT CROSS BEAM C 63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER P52 LT, C59 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: PANEL — CRACKED (NR 2 NACELLE) · airframe 44,246 hrs · 19,687 cycles

CRACK (ABOUT 8MM) FOUND AT INBOARD SIDE WALL PANEL, RIB 8, PYLON NR 2 REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON STRINGER SEGMENT P46RH, C 64-65 STRINGER SEGMENT REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW EA 6-5317-81052 AND RAS/DATLS/0002039/2004 ISS A.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON SPLICE C39, P 47 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: REINFORCEMENT — CHAFED (ZONE 500) · airframe 44,246 hrs · 19,687 cycles

FOUND CHAFING DAMAGE TO REINFORCING PLATE ADJACENT TO THRUST AND SIDE LOAD FITTING RIB 9 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5720-81076 AND RAS/BAE/1125/2004 ISS A.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION ON CENTER TANK TOP SKIN C 45-46 LT, C 41-46 RT REPAIR PERFORMED IAW SRM 57-10-12 FIG 201 AND IN ADDITION THE HOLES OVERSIZED IAW EA 6-5710-81049 AND RAS//AS/0256/2004 ISS A.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT EMERGENCY EXIT DOOR, FRAME SEGMENT 3.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 26 LT, C54-54.1 REPAIR PERFORMED BY PARTIAL REPLACEMENT OF CORRODED STRINGER IAW A300-600 FREIGHTER SRM 53-10-14 , APPROVED BY EA 6-5310-81053 AND RAS/DATLS/0002051/2004 ISS A.

Part: SKIN — DAMAGED (ZONE 600) · airframe 44,246 hrs · 19,687 cycles

FOUND ON RT WING UPPER SKIN PANEL RIB 15 T/E WAS CUT OUT AND A SEALING STRIP HAD COME A DRIFT. REPAIR PERFORMED BY REMOVING THE SEALING STRIP, ENSURE CUT OUT TO SMOOTH PROFILE AND INSTALL A NEW REPAIR STRIP ON UPPER SURFACE IAW EA 6-5720-81075 AND RAS/BAE/1105/2004 ISS A.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT C39,P 55, BOTTOM SPLICE. REPAIR PERFORMED BY REWORK OF CORROSION IAW RAS 032422/009/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER 50L, C 37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 27 LT, C 75-76 REPAIR PERFORMED IAW A300-600 FREIGHTER SRM 53-10-14 FIG 201, APPROVED BY EA 6-5310-81054 AND RAS/DATLS/0002051/2004 ISS A .

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 45LH BETWEEN C 63-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,246 hrs · 19,687 cycles

FOUND CORROSION AT STRINGER P 51 LT, C 37-38 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SKIN — WORN (ZONE 500) · airframe 44,246 hrs · 19,687 cycles

FOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, LT WING BOTTOM SKIN. REPAIR PERFORMED IAW DRAWING R572-59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 32RT 35-37 STRINGER REPAIR PERFORMED IAW EA 6-5314-81040 AND RAS/DATLS/0002032/2004 ISS. A 9 CUT OUT THE CORRODED PART AND SPLICE REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 43LH, C 22-23. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 53 LT, C 63-65. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION AT MANHOLE INTEGRAL PLATE C 38.1-39, P 49RH-54 LT AND OLD POCKET REPAIRS, NOT CONFORM TO SRM 53-14-12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R537-06164-000 AND SRM 51-72-10 AND INSTALLING OF ALTERNATE FASTENER, APPROVED BY EA 6-5314-81070 AND RAS/DABRE/004470/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 44LT AND P 45LT, C 79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

CORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT CIRCUMFERENTIAL STRAP AND FLANGE REPAIR PERFORMED IAW SRM 53-19-17 FIG 201 AND DRAWING R539-707100.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION AT INTERNAL DOUBLER C 17-18, P 42-44 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND NTD INSPECTION OF CRACK FREE IAW EA 6-5312-81047 AND RAS/AS/246/2004 ISS A.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

CORROSION FOUND BEHIND AFT PRSSURE BULKHEAD C80 AT INNER RIM ANGLE. REPAIR PERFORMED BY RELACEMENT OF PART IAW SRM 51-72-10.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION AT MANHOLE INTEGRAL PLATE C 23-24, P 49RH-54 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R537-06163 AND INSTALLING ALTERNATE FASTENER HL111VF8, APPROVED BY EA 6-5313-8106 AND RAS/DABRE/7004239/2004 ISS B.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 40LH AND P 42, C 79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

FOUND CORROSION ON STRINGER P 52LT, C 65-66 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,242 hrs · 19,683 cycles

FOUND CORROSION ON CROSS STRUT C 84 RT AND LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — DAMAGED (NLG DOOR) · airframe 44,242 hrs · 19,683 cycles

DURING UNCONTROLLED MOVEMENT OF HYDRAULIC CYLINDER THE RT NLG FWD DOOR SKIN WAS DAMAGED. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A DOUBLER WITH SHIM IAW EA 6-5282-81079 AND RAS/AS/307/2004 ISS A

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 44,243 hrs · 19,684 cycles

FOUND EXTERNAL DOUBLER REPAIR AT C65-66, P 39-42 RT NOT CONFORM TO SRM. REPAIR RENEWED IAW SRM 53-10-12 FIG 203.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

CORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT INNER STRAP. REPAIR PERFORMED BY RELACEMENT OF PART IAW SRM 51-72-10.

Part: STRUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,242 hrs · 19,683 cycles

FOUND CORROSION ON CROSS STRUT C 87 RT AND LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,243 hrs · 19,684 cycles

CORROSION FOUND ON AFT CARGO DOOR SILL BEAM OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: ANGLE — NONE (ZONE 100) · airframe 44,033 hrs · 19,557 cycles

FS 40 LT PICKUP ANGLE EFFECTIVITY NOT CONSISTENT WITH SB ANGLE REQUIRES EXCESS MATERIAL TO BE TRIMMED OFF PER EA 6-5310-110489 PG NR 2 COMPLIED WITH EA 6-5310-110489 PG NR 2. TRIMMED EXCESSIVE MATERIAL OFF OF PN A53810318.

Part: TRANSMITTER — LEAKING (HYD SYSTEM) · airframe 43,669 hrs · 19,333 cycles

AT TOGA FOR TAKEOFF, LOST BLUE HYD SYSTEM. QTY WENT TO ZERO. REJECTED TAKEOFF,CLEARED RWY WORKED QRH. FOUND LEAK COMMING FROM BLUE SYSTEM PRESSURE TRANSMITTER AREA ON BLUE SYSTEM MODULE. LEAK IS OBVIOUS. R & R BLUE SYSTEM PRIORITY VALVE REF. A310-200 MM 29-12-12-4 AND SERVICE & OPS CHECKED REF. MM29-00-00-3. LEAK CHECKED GOOD AND OPS CHECKED NORMAL. MOTORED NR 1 ENGINE REF. JRH AND OPS CHECKED FLIGHT CONTROLS. ALL CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 43,166 hrs · 19,090 cycles

ON TAKEOFF ROLL, WHEN TOGO WAS SELECTED ON THE THROTTLES, NR 1 ENG WENT TO FLEX PWR, ENG NR 2 HOWEVER WENT TO ABOUT 109 PERCENT OR SO N1 THE ENGINE THRUST PREDICT NEEDLE ON NR 2 DIDN'T MOVE. ALSO, GOT THE ENGINE TRIM FAULT LIGHT. ABORTED TAKEOFF, RNO - MEL/CDL: 22-30-01-02 MEM/23. NOTE: FCC NR 2 CHANGED 08-23-06, SEE MTSI 22-10/1565. REMOVED AND REPLACED NR 2 ENG TORQUE MOTOR FAIL FIXED SOLENOID PASSES OPERATIONAL TEST IN REF OFF MFG 1310-130 POS 2 SRL 275 ON MFG 1310-130 SRL WWC00966. PERFORMED POWER MANAGEMENT CONTROL SYSTEM OPS CHECK. PERFORMED MAX PWR CHECK OF NR 1 AND NR 2 ENGINES.

Part: THROTTLE — OBSTRUCTED (NR 2) · airframe 42,765 hrs · 18,886 cycles

DESCENDING FROM 380 13000 AT YYC, NR 2 THROTTLE WOULDN'T RETARD TO IDLE. COMPLIED WITH QRH "THROTTLE LEVER JAMMED" NR 2 THROTTLE WOULD ADVANCE BUT NOT RETARD TO IDLE. IT WOULD ONLY GO AS LOW AS 10-15 DEGREES ON THE QUADRANT. ENGINE SHUT DOWN AS PER QRH. WINDMILLING TIME OF 15 MINUTES. ON GROUND NR 2 THROTTLE WILL NOT RETARD PAST 10 UNITS ON QUADRANT NOR ADVANCE PAST 41 UNITS. PRIMARY TRANSMISSION INSPECTED PER AMM 76-11-33-6-04. FOUND LINT AND CRUSTED LIQUID IN THE QUADRANT ASSEMBLY, ASSY CLEANED, NOW HAVE FULL MOVEMENT FORWARD AND AFT ON NR 2 THRUST LEVER. RT A/T COUPLING UNIT CHANGED PER AMM 22-33-28-4.

Part: INDICATOR — MALFUNCTIONED (ENGINE EGT) · airframe 42,617 hrs · 18,806 cycles

DURING CLIMBOUT AFTER TAKEOFF NR 1 ENG EGT LIMIT WAS EXCEEDED. EGT POINTER PAST 1000 DEGREE MARK. ON FINAL EGT GAUGE WENT TO ZERO AND BLANK THEN CAME BACK UP TO ABOUT 400 DEGREES SIMILAR TO NR 2 ENG EGT INDICATOR. INSPECTED ENGINE EXHAUST AND INLET FOR FOD AND OR OTHER DAMAGE DUE TO EGT OVERLIMIT. DID NOT FIND ANY DAMAGE OR SIGNS OF OVER TEMP AT THIS TIME. PER POWERPLANT CONVERSATION THE ENGINE DID NOT GO PAST 803 DEGREES PER ACARS READOUT. REMOVED AND REPLACED EGT INDICATOR, ACCOMP PWR ASSURANCE RUN A310 JRH CHPT 6-11. OFF MFG 63600-261-1.