N445FE

Part: FRAME — CORRODED (E/E BAY) · airframe 45,025 hrs · 20,982 cycles

FOUND LEVEL ONE CORROSION IN AVIONICS BAY AT FRAME 12A AND BETWEEN SRTINGER 44L AND 45L, APPROXIMATELY 22" SQ IN. REMOVED CORROSION FROM FRAME 12A AND BETWEEN 44L AND 45L IAW SRM 51-14-10 PAR 5. FRAME 12A FORMER WAS .085" BEFORE AND AFTER CORROSION REMOVAL WAS .045" A LOSS OF .040", FOUND FORMER TO BE OUT OF LIMITS IAW A310 SRM 53-12-13 FIG 201 AND 202. REMOVED FASTENERS FROM AREA AND HAD NDT INSPECT THE HOLES FOR CRACKS, NO DEFECTS NOTED IAW NTM 51-10-01. REMOVED AND REPLACED FRAME 12A IAW A31 SRM 51-72-10 PAGE 1-3 AND A310 SRM 51-40-21 PAR 5 AND 6. REF DRAWING A53611389 AND A53610567. REPAIR WAS A MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FOUND A CRACK FLOOR SUPPORT AT FRAME 54.2 ON RT SIDE BETWEEN SEAT TRACKS 2R AND 3R, CRACK IS (.25") LONG. REMOVED DAMAGE AREA AT FRAME 54.2 ON RT FLOOR SUPPORT BETWEEN SEAT TRACKS 3R AND 2R IAW SRM 53-10-15, NDT VERIFIED NO CRACK INDICATIONS IAW NTM 51-10-02, FABBED REPAIR ANGLES AND INSTALLED REPAIR IAW SRM 53-10-15 FIG 204, ALODINED AND TOP COATED REPAIR IAW SRM 51-75-10. THIS REPAIR IS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 45,025 hrs · 20,982 cycles

FOUND 2EA AREAS OF DELAMINATION ON RT OUTBOARD FLAP TRAILING EDGE, ONE AREA WAS 4"L X .78"W X .093" D. THE SECOND AREA WAS 1.34"L X 1.28"W WITH A BULGE OF .50" ON THE TOP SIDE OF THE SKIN. BOTH AREAS WERE ON THE TOP SKIN OF THE TRAILING EDGE BETWEEN RIB 2 AND RIB 10. AREA ONE WAS WORKED ON NON ROUTINE N00426, REMOVED PREVIOUS BONDED DOUBLER AND SKIN IAW SRM 57-53-12. FABRICATED DOUBLER, POTTED CORE, ALODINED AND PRIMED REPAIR AREA AND RESTORED TOPCOAT IAW SRM 57-53-12. AREA NR 2 - WORKED ON NON ROUTINE N00427, REMOVED DAMAGED SKIN AND CORE IAW SRM 57-53-12. POTTED CORE, FABRICATED DOUBLER, ALODINED AND PRIMED REPAIR AREA AND RESTORED TOPCOAT IAW SRM 57-53-12. THIS REPAIR WAS WORKED IAW EA 6-5750-135282, THIS REPAIR IS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FLOOR SUPPORT ON MDC AREA FORM FRAME 12 TO FRAME 14 AND LT SEAT TRACK NUMBER 3 HAS 7 EA DOUBLE DRIILLED HOLES. REMOVED FLOOR SUPPORT AND SEAT TRACK, LOCATED AND DRILLED NEW SUPPORT/SEAT TRACK AND INSTALLED FLOOR SUPPORT/SEAT TRACK ON LT SEAT TRACK NR 3 (Y 450) BETWEEM FRAME 12 AND FRAME 14 IAW A310 SRM 51-72-10 AND SRM 51-40-21. TOPCOATED AREA IAW SRM 51-75-10. ALL WORK PERFORMED ON N01355 UNDER WO 00048963. THIS REPAIR IS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FOUND 4EA MISDRILLED HOLES IN MDC AT FRAME 18, INBOARD OF LT SEAT TRACK NR 4. REMOVED DAMAGED TEE CAP FROM INBOARD OF FRAME 18 FROM SEAT TRACK (Y-2462) TO (Y- 953). FABRICATED PARTS IAW DRAWING A5377449 & A53611736 AND LOCATED AND DRILLED IAW DRAWING ABOVE, INSTALLED TEE CAP FROM SEAT TRACK (Y-2462) TO SEAT TRACK ( Y-953) IAW SRM 51-40-21 PAR 2,3. ALODINED, PRIMED AND TOPCOATED REPAIR IAW SRM 51-75-10. THIS REPAIR WAS MAJOR IAW GMM 6-2-100. ALL WORK PERFOFRMED UNDER WO 00048963.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

FOUND LEVEL ONE CORROSION IN LOWER FORWARD CARGO COMPARTMENT AROUND MANHOLE COVER BETWEEN FRAME 38.1 AND FRAME 38.2, FROM STR 53L TO STR 53R. REMOVED CORRODIED POCKET REPAIRS FORM MANHOLE COVER AREA IN FORWARD LOWER CARGO COMPARTMENT SKIN AT FR 38 TO FR 39, STR 53L TO 53R. FABRICATED REPAIRS FOR THE POCKET AREAS IAW SRM 53-14-12 FIG 203., SOLUTION NR 4 REV DATED 01 DEC 2009. THIS REPAIR WAS WORKED ON N00846 AND N00845 UNDER WO 00048963. THIS REPAIR WAS WORKED IAW EA 6-5310-135285, FR38/1/38.2 MANHOLE AND REFERENCED AIRBUS RAS/DAHAM/4032347/2010 ISSUE A. THIS WAS A MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — BENT (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FLOOR SUPPORT BETWEEN FRAME 11 AND FRAME 12A AT BUTT LINE Y-953 AND Y-450 IS BENT AND SUPPORT ANGLE IS MISSING. LOCATED SUPPORT ANGLES AND FABRICATED PARTS IAW DRAWING, REMOVED BENT ANGLE AND LOCATED AND DRILLED FABBED ANGLES IAW SRM 51-40-44, INSTALLED PARTS BETWEEN FRAME 11 AND FRAME 12 A AND BETWEEN BUTT LINE Y-953 AND Y-450 IAW SRM 51-72-10. REPROTECTED ALL PARTS IAW SRM 51-21-10 & 51-75-10. WORK WAS ACCOMPLISHED ON N01361 UNDER WO 00048963. THIS IS A MAJOR REPAIR PER FEDEX GMM 6-02-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

FOUND LEVEL ONE CORROSION AT MAIN DECK CARGO AREA FROM FRAME 11A TO FRAME 14C ON L/H SEAT TRACK 4L. REMOVED CORROSION AT L/H SEAT TRACK 4L BETWEEN FRAME 11A AND FRAME 14C AND FLOOR SUPPORT IAW A310 SRM 51-74-10. PARTWAS OUT OF LIMITS IAW A310 SRM 53-12-15 DIA 101. REMOVED AND REPLACED 4L SEAT TRACK FROM FRAME 11A TO FRAME 14C IAW A310 SRM 51-72-10. MAJOR REPAIR IAW FEDEX GMM 06-2-100. THIS WORK PERFORMED ON N01368 UNDER WO# 00048963.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MAIN CABIN AT FRAME 52 RT SEAT TRACK 4 HAS A MISDRILLED HOLE THAT GOES THROUGH FITTING. REPAIRED SEAT TRACK 4R USING SPLICED REPAIR IAW SRM 53-10-16.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MDC AT FR35 SEATTRACK NR4 IS GOUGED AT EDGE OF SCALLOP.2500 IN EACH SIDE. REPAIRED SEAT TRACK R4 AT FR 35 IAW A310 -200, SRM 53-10-16.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

MDC FR 13A TO FR 17 LT SEAT TRACK 5 HAS CORROSION ON BOTH SIDES OF UPPER FLANGE. R & R SEAT TRACK NR5 BETWEEN FR 13 AND FR 17 IAW SRM 53-12-16 DUE TO EXFOLIATION CORROSION , MAT LOSS WAS 100 PERCENT IAW SRM 53-10-16, FIG 101.

Part: SEAT TRACK — DAMAGED (ZONE 600) · airframe 45,025 hrs · 20,982 cycles

MAIN CABIN AT FRAME 50 RT SEAT TRACK 3 HAS MISDRILLED HOLE IN SEAT TRACK AND FITTING. REMOVED DAMAGED SECTION OF SEAT TRACK 3R AT FR 50.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MAIN DECK CARGO COMPARTMENT- SEAT TRACK 2R AT FRAME 61 HAS ONE EACH ELONGATED, SCALLOP MEASURING .991". R & R SEAT TRACK SECTION NR 2R BETWEEN FRAMES 59-61.

Part: SUPPORT ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

FWD CARGO COMPT FR 38 SUPPORT ANGLE BETWEEN STRG 53L & 53R HAS CORROSION, ABOUT 20 SQ INCH. REMOVED CORROSION FROM SUPPORT CLIP IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-14-13 FOUND TO BE OUT OF LIMIT. R & R SUPPORT CLIP IAW SRM 51-40-21.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MDC SEAT TRACK 1 BETWEEN FR 30 AND FR 31 OTBD FLANGE HAS 19 EA HOLES DRILL THRU IT. R & R DAMAGED PROFILED TRACK IAW SRM 53-10-16.

Part: SKIN — DENTED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FOUND LT AFT FUSELAGE SKIN DENT L=1.0", W=1.0", D=0.015" 6" FWD OF FR 78 AND STRINGER 26L. EVALUATED DENT AND FOUND TO BE NOT PERMISSABLE DUE TO DENT WAS LOCATED ON A STRINGER. STRINGER DIRECTLY OVER THE RIVET IAW SRM 53-10-12 PG 1. CUT OUT DAMAGED SKIN, VERIFIED MATERIAL THICKNESS, 2024T3 CLAD .071" AND .063" IAW SRM 53-10-12. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-10 PAR. 2 AND INSTALLED REPAIR IAW SRM 53-10-12. ALODINED AND REPROTECTED AREA IAW SRM 51-74-10. ALL WORK PERFORMED UNDER WO 00048963.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

AFT CABIN UNDER FLOOR COMPARTMENT FRAME 72 AT BOTTOM BUTT LINE 0 HAS 10 SQ INCH LIGHT SURFACE CORROSION ON FWD AND AFT SIDE OF FRAME. R & R CORRODED SPLICES ,CORRODED SHEAR TIES AND SKIN BUTT SPLICE BETWEEN STRINGERS 56L, STRINGER 57 AND STINGER 56R IAW SRM 51-72-11. CHECKED FRAME 72 FOR CORROSION NO CORROSION NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

MAIN CARGO DECK RT SIDE SEAT TRACK 5R FRAME 14 TO FRAME 18 HAS 3 SPOTS (0.5 X 2.0) OF EXFOLIATION CORROSION. R & R SEAT TRACK AT RT R5 FROM FR 14 TO FR 18 IAW SRM 51-72-10, PARA 5 & 6. LOCATED AND DRILLED AND DEBURED NEW SEAT TRACK IAW SRM 51-40-44.

Part: SKIN — DELAMINATED (RT ELEVATOR) · corrosion level 2 · airframe 45,025 hrs · 20,982 cycles

RT ELEVATOR LOWER SURFACE HAS 3 SPOTS BULGED PAINT WITH LIGHT SURFACE CORROSION AT STA 622 AND 2 SPOTS OF BULGED PAINT, LIGHT SURFACE CORROSION AT STA 472. REMOVED CORROSION IAW SRM 51-74-10, NDT CHECK COMPLIED FOUND SKIN DELAMINATED. REPAIRED RT ELEVATOR LOWER SKIN IAW SRM 55-21-11, FILLER AND DOUBLER REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

FRAME 72 HAS 0.25 INCH PUNCTURE ON OUTER FLANGE AT STRG 55L REPAIRED FR 72 AT STR 55L IAW SRM 53-10-13, FIG 101.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MAIN DECK CARGO COMPARTMENT - SEAT TRACK 5R AT FRAME 61 HAS ONE EACH ELONGATED SCALLOP MEASURED AT .985. R & R DAMAGED SEAT TRACK SECTION FRAME 58 TO 62 SEAT TRACK 5R IAW SRM 53-10-16, PARA 10 AND 51-72-10.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 45,025 hrs · 20,982 cycles

MAIN CARGO DECK SEAT TRACK NR 1 FRAME 61 HAS ONE EACH SCALLOP ON SEAT TRACK OUT OF ROUND MEASURES .8750 INCH. REPAIRED SEAT TRACK NR1 IAW SRM 53-10-16 BY REPLACING DAMAGED SECTION OF SEAT TRACK FROM FR 58 TO FR 61.9.

Part: SWITCH — MISALIGNED (TE FLAPS) · airframe 44,913 hrs · 20,892 cycles

DURING FLAP RETRACT ON TAKEOFF GOT FLAPS SYS 2 JAM AND FLAP VANE JAM FAULTS. CYCLED FLAPS WITH NO CHANGE. FLAPS WOULD LOWER, BUT NOT RAISE ABOVE 10 DEGREES. DURING TROUBLE SHOOTING FOUND THE RT WING INBD FLAP VANE EXTEND JAMMING SWITCH 42CV OUT OF ADJUSTMENT. NO DAMGE TO HONEYCOMB BLOCK STRUCTURE NOTED. R & R SWITCH PRECAUTIONARY. ADJUSTED NEW SWITCH AND SAFTIED IAW AMM 27-56-15-4. OP'S CHECKED FLAP EXTENSION AND RETRACTION WITH NO FAULTS WITH ENG HYD POWER. ALL OP'S CHECKS GOOD. FINAL CLOSED- NO TRACKING

Part: ADIRU — MALFUNCTIONED (NR 1) · airframe 43,891 hrs · 20,153 cycles

REJECT ON T/O ROLL DUE TO LOSS OF AIRSPEED READOUT ON CAPT PFD (40KTS). COMPLIED WITH QRH REMOVED AND REPLACED NR 1 ADIRU IAW AMM 34-25-34-4. OP CHECKS GOOD. PERFORMED LOW LEVEL LEAK CHECK OF NR 1 PITOT SYSTEM. NO DEFECTS NOTED.

Part: DOUBLER — FAILED (R1 DOOR) · airframe 43,133 hrs · 19,692 cycles

THE DOUBLERS AT THE AFT LOWER AND FWD LOWER CORNERS OF THE R1 DOOR ARE ALUMINUM AND REQUIRE REMOVAL FOR COMPLYING INSPECTION OF AD TASK CARD EO E6-5310-7-3318. REMOVED EXISTING DOUBLERS BELOW R1 DOOR, FWD AND AFT LOWER CORNERS. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW AIRBUS DRAWING R5361166 AND FEDEX EA6-5310-121243, DATED 11 APRIL, 2008.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RIGHT SIDE FUSELAGE SKIN BETWEEN FRAMES 16A TO 18 AND BETWEEN STRINGERS 41 AND 43 RT MEASURES 11 INCH BY 8.1. "REPAIR NOT IAW WITH SRM 53-12-12 FIG 201, REPAIR NOT APPLICABLE TO AREA. REMOVED AND REPLACED REPAIR IAW EA 6-5310-118112. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 43,133 hrs · 19,692 cycles

REPAIR FOUND TO NOT BE IAW SRM 53-12-12- FIG 201 SHEET 1. REPAIR NOT APPLICABLE TO AREA. RESULT OF AGING AIRCRAFT INSPECTION REMOVED AND REPLACED REPAIR IAW EA 6-5310-118130. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT.

Part: TRUNNION — GOUGED (ZONE 600) · airframe 43,133 hrs · 19,692 cycles

RT MLG RIB 5 CENTER TRUNNION LUG FWD FACE HAS 2 GOUGES, 1 IS 3/8 IN WIDE BY 1.25 IN LONG BY .020 DEEP, AND 1 IS .25 IN WIDE BY 1 IN LONG BY .032 DEEP. ACCOMPLISHED REPAIR ON RT MLG TRUNNION LUG IAW FEDEX EA 6- 5710-118108, RELEASE DATE 19 MARCH, 2008.

Part: TRUNNION — CHAFED (ZONE 600) · airframe 43,133 hrs · 19,692 cycles

RT MLG RIB 5 CENTER TRUNNION LUG FWD INBD RADIUS CHAFED APPROX .60 IN LONG BLENDED CHAFED AREA IAW FEDEX EA 6-5710-118108, RELEASE DATE 19 MARCH, 2008.

Part: BUSHING — CORRODED (ZONE 600) · airframe 43,133 hrs · 19,692 cycles

RT MLG RIB 5 FWD BORE ON TRUNNION LUG IS CORRODED ON INSIDE AFTER BUSHING WAS REMOVED. REMOVED LEVEL 1 CORROSION AND REPAIRED WITH OVERSIZE BUSHINGS IAW FEDEX EA 6-5710-118108, RELEASE DATE 19 MARCH, 2008.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,133 hrs · 19,692 cycles

LT MLG WHEEL WELL BETWEEN FRAME 48 AND 49 INTERIOR OF SKIN AT STRINGER 38 HAS CORROSION APPROX 1 SQ IN. REMOVED LEVEL 1 CORROSION AND INSTALLED REPAIR DOUBLER BETWEEN FRAMES 49 AND 50 AND STRINGERS 37 AND 38 LT IAW FEDEX EA 6-5310-118099, RELEASE DATE 17 MARCH, 2008.

Part: SKIN — DAMAGED (ZONE 100) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LOWER CTR FUSELAGE SKIN MANHOLE FITTING CUTOUT AT FRAMES 23 TO 24 AND BETWEEN STRINGERS 48 RT TO 52 RT, MEASURES 24.4 IN X 15 IN WITH 4 EA INTERNAL POCKET REPAIRS BETWEEN STRINGERS 54 LT TO 49 RT REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PRVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW EA 6-5310-118095. THIS IS A REPAIR WITH NO ASSIGNED PN AND IS A RESULT OF AGING ACFT INSP.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT -Y1456 BETWEEN FRAMES 62 TO 63, HAS 2 EACH REPAIR SPLICES MEASURING 7 IN LONG BY 3 IN TALL AND 1 REPAIR SECTION 52 IN LONG FROM FRAME 65 TO BETWEEN FRAMES 62 AND 63. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW A310 SRM SUPPLEMENT 53-10-16, FIG 202, PG 209/210. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION.

Part: RIB — CORRODED (ZONE 500) · airframe 43,133 hrs · 19,692 cycles

THE RIB 5 FWD BORE ON THE LT MLG IS CORRODED ON THE INSIDE, FOUND AFTER BUSHING WAS REMOVED. THE MAX DIAMETER OF 4.8405 HAS BEEN REACHED, REMOVED LEVEL 1 CORROSION, AND REPAIRED LT MLG RIB 5 IAW EA 6-5710-118108. THIS IS A REPAIR WITH NO ASSIGNED PN.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LOWER CENTER FUSELAGE SKIN MANHOLE FITTING CUTOUT AT FRAMES 23 TO 24 AND BETWEEN STRINGERS 48 RT TO 52 RT MEASURES 24.4 IN BY 15 IN WITH 4 INTERNAL POCKET REPAIRS BETWEEN STRINGERS 54 LT TO 49 RT REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW FED EX EA 6-5310-118095 THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION.

Part: RIB — CORRODED (ZONE 500) · airframe 43,133 hrs · 19,692 cycles

THE RIB 5 FWD BORE ON THE LT MLG IS CORRODED ON THE INSIDE, FOUND AFTER BUSHING WAS REMOVED. THE MAX DIAMETER OF 4.8405 HAS BEEN REACHED REMOVED LEVEL 1 CORROSION, AND REPAIRED LT MLG RIB 5 IAW FED EX EA 6-5710-118108. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT -Y1456 BETWEEN FRAMES 62 TO 63, HAS 2 EACH REPAIR SPLICES MEASURING 7 IN LONG X 3 IN TALL AND 1 EA REPAIR SECTION 52 IN LONG FROM FRAME 65 TO BETWEEN FRAMES 62 AND 63 REPAIR NOT IAW SRM REQUIREMENTS.REMOVED PRVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW SRM SUPPLEMENT 53-10-16, FIG 202, PG209/210. THIS IS A REPAIR WITH NO ASSIGNED PN AND IS A RESULT OF AGING ACFT INSP.

Part: SPAR — MISREPAIRED (ZONE 300) · airframe 43,133 hrs · 19,692 cycles

PREVIOUS REPAIR LOCATED ON RIGHT THS UPPER REAR SPAR CHORD BETWEEN RIBS 4 AND 5 HAS 1 EACH REPAIR ANGLE ON LOWER SURFACE OF FLANGE MEASURING 15.2 INCH LONG BY 1.65 INCH TALL REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ANGLE IAW A310 SRM 55-11-21 FIG 211, 213 AND 218. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING, AIRCRAFT INSPECTION.

Part: CONTROL UNIT — FAILED (MLG) · airframe 41,727 hrs · 18,941 cycles

AUTOBRAKES WORKED FINE TIL TOP OF DESCENT, WITH GEAR HANDLE NEUTRAL TRIED TO ARM (MED) AUTOBRAKES. GREEN PN CAME ON FOLLOWED IMMEDIATE W/AUTO BRAKES INOP. TRIED SEVERAL RESETS. GOC DIRECTED KMSP RETURN DUE TO SHORT DLH RWY. BSCU SHOWED CODE FOR ALT SERVO VALVE. BOX WOULD NOT RESET. REMOVED AND REPLACED BSCU IAW A310-200 AMM 32-42-72-4 AND OPS TESTED IAW 32-42-00-5. ITEM REMAINS ON DEFERRAL DUE TO HISTORY. ACN RELEASED FOR SERVICE IAW MEL/CDL: 32-42-05.

Part: VERTICAL BEAM — DAMAGED (BULKHEAD) · airframe 40,661 hrs · 18,390 cycles

COMPLY WITH EA 6-5310-92347 FUSELAGE - FR 54 BULKHEAD VERTICAL STIFFENER REPAIR. COMPLIED WITH EA 6-5310-92347 FUSELAGE FR 54 BULKHEAD VERTICAL STIFFENER REPAIR.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 40,661 hrs · 18,390 cycles

NR 2 PYLON LWR RT SIDEWEB CRACKED 28" FROM NOSE COWL.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 40,661 hrs · 18,390 cycles

NR 2 ENG LWR LT SIDE WEB 28" FROM NOSE COWL.

Part: FLANGE — CRACKED (NR 1 PYLON) · airframe 40,661 hrs · 18,390 cycles

NR 1 PYLON FLANGE CRACKED BELOW COLD AIR DUCT.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 40,661 hrs · 18,390 cycles

NR 2 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 40,661 hrs · 18,390 cycles

NR 1 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED.

Part: ATTACH BRACKET — CRACKED (THRUST REVERSER) · airframe 40,661 hrs · 18,390 cycles

NR 2 ENG LT T/R FWD UPPER COMPRESSOR PAD ATTACHED BRACKET CRACKED AROUND MOUNTING HOLE.

Part: SKIN — DENTED (RT WING) · airframe 40,661 hrs · 18,390 cycles

RT WING L/E HAS DENT ABOVE NR 3 FLAP TRACK. REMOVED DAMAGE, FABED REPAIR PARTS, TREATED AND PRIMED, INSTALLED REPAIR PARTS IAW SRM 57-53-12, 51-21-10, AND 51-40-2.

Part: SEAT TRACK — GOUGED (BS 543) · airframe 40,661 hrs · 18,390 cycles

SEAT TRACK LOBES ARE GOUGED. REPLACED, PRIMED AND PAINTED IAW SRM 51-40-21, 51-21-10, 53-10-16 AND MM 51-75-10-8.

Part: WARNING SYSTEM — FAULTY (COCKPIT) · airframe 39,276 hrs · 17,596 cycles

ON CLIMBOUT PASSING 6800 FT GOT LEFT FWD COMP DOOR UNLOCK LIGHT (AMBER INDICATION). RETURNED TO LAS. ON APPROACH AT 4000 FEET LIGHT TURNED GREEN (DE-PRESSURIZED AT THIS POINT). LWR FD DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOP. LWR FD DOOR VISUALLY CHECKED CLOSED & LOCKED. INSPECTED AT 0331 Z.

Part: BRACKET — CORRODED (HORIZONTAL STAB) · airframe 37,641 hrs · 16,773 cycles

LT HORZONTAL STABILIZER LEADING EDGE ATTACH APRON IS HEAVILY CORRODED AT AFT UPPER "L" ANGLE. REMOVED AND REPLACED WITH ON SITE FABBRICATED PARTS.

Part: STRUCTURE — CORRODED (MLG DOOR) · airframe 37,641 hrs · 16,773 cycles

MLG DOOR, SKIN HAS CORROSION. REMOVED WITHIN LIMITS CORROSION IAW/SRM 51-74-10 ON OUTER SKIN INNER SURFACE. DOOR SKIN OUT OF LIMITS REPAIRED ON E.A.6-5281-6871.RESTORED DOOR IAW/SRM 51-40- 21 PREPPED AND PAINTED IAW/SRM 51-21-50.

Part: PIVOT ASSY — SEIZED (LT MLG) · airframe 37,242 hrs · 16,552 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. IN SYS 1 OR 2 TROUBLESHOT INTERLOCK SYSTEM. FOR NR 1 AND NR 2 SYSTEMS, FOUND ALL ELECTRICAL FUNCTIONS CHECK GOOD. CHECKS GOOD WITH GROUND ON RECEPTACLE OF PROX BOX AT PINS 44 AND 55. JACKED AIRCRAFT IAW M/M AND FOUND LEFT MAIN LANDING GEAR BOGIE BEAM WILL NOT PIVOT. REMOVED PITCH DAMPER IAW M/M AND BOGIE STILL LOCKED UP. REMOVED ALL 4 BRAKE TORQUE ARMS AND BOGIE STILL LOCKED UP AT CENTER PIVOT POINT. WILL NEED FURTHER DISASSEMBLY TO DETERMINE DAMAGE.

Part: LATCH — STICKING (CARGO DOOR)

INTERMITTENT AFT CARGO DOOR NOT CLOSED, LIGHT CAME ON SHORTLY AFTER T/O. CLEANED AND LUBED DOOR HANDLE BUTTON AND LATCH PER SMP, OP CK NORMAL.

Part: RELAY — FAILED (E & E COMPT)

ON CLIMB, ALL PITOT FAULT LIGHTS, NR 1 PITCH TRIM FAILED NR 2 YAW DAMP, NR 1 & 2 ATS. CABIN PRESS FAILED AUTO & MANUAL. ALL SYS WORKED FINE ON LANDING. *S/D* REPLACED RELAY 10KC, REMOVED AND REPLACED RELAY 14XC PER STD PTCS. TEST NORMAL.

Part: PITOT TUBE — DIRTY (NR 1ADC)

DURING T/O, CAPT AIRSPEED ON NR 1 PFD WAS 30 KTS SLOWER THAN F/O'S AIRSPEED ON NR 2 PFD. *S/D* CLEANED OUT PITOT LINE ON NR 1 ADC. OPS CK GOOD PER AIRBUS MM 34-10-00.

Part: ENGINE — FAILED (NR 2)

NR 2 ENG FAILED IN FLT, LOUD POP HEARD LVL AT 310. COMPLIED WITH ECAM. QRH PROC DUE TO POSSIBLE STRUCTURE DAMAGE.