N423FE

Part: JACKSCREW — WORN (SLATS) · airframe 43,064 hrs · 20,183 cycles

ON APPLICATION OF SLATS 1 & 2, FAULT LIGHT CAME ON. SLATS LESS THAN 15- CYCLED HANDLE & NO CHANGE. RAN CHECKLIST & MADE NO SLAT LANDING. AFTER LANDING TRIED SLATS AGAIN AND THEY CAME DOWN. PERFORMED BITE TEST ON NR 1 & 2 SFCC IAW FIM 27-80-01/101. ALL INDICATIONS NORMAL. PERFORMED SLAT/FLAP EXTENSION AND RETRACTION IAW AMM 27-84-05, OPS AND INDICATIONS NORMAL NO FAULTS ON NR 1& 2 SFCC. OK TO CONTINUE. REMOVED AND REPLACED SLAT JACKSCREWS 6L,3R AND 4R IAW WRI 27-80/4772, 27-80/4771 AND 27-80/4774. ALL RIG AND OPS CHECKED GOOD. IAW AMM 27-80-00. OK FOR SERVICE.

Part: SEAL — LEAKING (BLEED DUCT) · airframe 42,864 hrs · 20,036 cycles

AFTER TAKE OFF, BLEED LEAK RT SIDE. REF QRH- LIGHT OUT IN FLIGHT. ON APPROACH LOWER ACCESS DOOR LIGHT CAME ON. FOUND LEAK TO BE COMING FROM THE UPPER RT CORNER OF PACK BAY BLEED SUPPLY LINE. REMOVED RT ENG BLEED DUCT SECTION IN FWD A/C BAY IAW MM 36-11-00-04. FOUND TWO SEALS ROLLED & CRUSHED. REPLACED TWO EXPANSION JOINT SEALS IAW MM 20-26-00-00. REINSTALLED RT AIR SUPPY FEED HROUGH DUCT IAW MM 36-11-00-04-LEAK CHECKED GOOD. REPLACED TWO EXPANSION JOINT SEALS IAW MM 20-26-00-00. REINSTALLED RT AIR SUPPY FEED THROUGH DUCT IAW MM 36-11-00-04-02, LEAK CHECKED GOOD.

Part: SKIN — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 42,834 hrs · 20,021 cycles

RT ELEVATOR NR 2 T/E UPPER SURFACE CORRODED. REPAIRED THE DAMAGE IAW SRM 55-21-11/201 (C-1) FIG 209.

Part: CROSSBEAM — CORRODED (CARGO BAY) · airframe 42,834 hrs · 20,021 cycles

FWD CARGO FR 38.1 -Y140 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW SRM 53-10-15, FIG 207.

Part: TRANSFER SYS — LEAKING (HYD SYSTEM) · airframe 41,200 hrs · 18,966 cycles

INFLIGHT YELLOW SYS RESERVOIR DECREASED TO RED DOT. FLUCTUATED SOME BUT NEVER WENT OUT OF YELLOW BAND. R & R GREEN/YELLOW POWER TRANSFER UNIT AS REQUIRED IAW MM 29-23-11-04.

Part: GCU — FAILED (NR 2) · airframe 41,068 hrs · 18,886 cycles

ON TAKEOFF ROLL AT APPROX 50 KNOTS, GEN NR2 FAILED. ABORTED TAKEOFF. INTEROGATED GPCU, SHOWS RT GENERATOR, UNDER FREQ TRIP, IDG /PMG / WIRING, GCU FAILED CODE 9E. REMOVED AND REPLACED ENG.2 GCU(2XU) AND ENG NR 1 GCU IAW MM 24-22-12-04. RAN ENG PER JRH CHP.6 OPS VERIFED NORMAL, ACCOMPLISHED BITE TEST GPCU NO FAUL NOTICE PER A-310 M/M 24-41-11-04 ACFT OK FOR SERVICE.

Part: TRANSCEIVER — INOPERATIVE (VHF SYSTEM) · airframe 41,021 hrs · 18,863 cycles

STATIC ON RADIOS AT 380 DOWN TO 120 WAS SO BAD AN EMERGENCY WAS DECLARED DUE TO NO RADIO CONDITION. INSTALLED NEW NR1 VHF RECEIVER AND CHECKED GOOD IAW MM 23-12-33-04-0.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 41,137 hrs · 18,921 cycles

EMERGENCY LIGHTS WILL NOT TEST USING PUSH-BUTTON OR OVERHEAD PANEL LIGHT SWITCH. R & R EMERGENCY LIGHT BATTERY LOCATED ADJACENT LT PASSENGER ENTRY DOOR IAW MM 33-51-14-04-0. EMERGENCY LIGHT TEST GOOD IAW MM 33-55-0 0-05. R & R EMERGENCY LIGHT BATTERY LOCATED ADJACENT LT PASSENGER ENTRY DOOR IAW MM 33-51-14-04-0. EMERGENCY LIGHT TEST GOOD IAW MM 33-55-00-5. (CLOSED)

Part: FRAME — CORRODED (ZONE 300) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 87- 89, STR 16L, HORIZ STAB CUTOUT. INNER FWD STRAP HAS EXFOLIATION CORROSION APPROX 4 IN. R & R THS CUTOUT FWD UPPER FITTING IAW DWG A53985135 AND SRM 51-40-21.

Part: SKIN — DAMAGED (RUDDER) · airframe 40,876 hrs · 18,747 cycles

.5" X .5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITTING IAW SRM 55-41-12 PARA 30 WET LAYUP REPAIR. NO CORE DAMAGE EXIST AT 22" AFT OF NR4 ATTACH FITTING OUTER SKIN. COMPLIED WITH EA 6-5540-145559 PART 1.

Part: RIB — CORRODED (LT WING) · airframe 40,876 hrs · 18,747 cycles

LT WING RIB 5 FWD LUG HAS CORROSION. REPAIRED IAW EA 6-5710-145518 WING-AD 2008-17-02 - WING GEAR RIB 5 FWD LUG BORE REWORK (LT SIDE), SB A310-57-2090, EO 6-5710-7-5010.

Part: RIB — CORRODED (RT WING) · airframe 40,876 hrs · 18,747 cycles

RT WING, RIB 5, FWD LUG HAS CORROSION REPAIRED IAW EA 6-5710-145517, WING-AD2008-17-02, WING GEAR, RIB5 FWD LUG BORE REWORK (RT SIDE), SB A310-57-2090, EO 6-5710-7-5010.

Part: PROFILE — CRACKED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO LONGITUDINAL PROFILE CRACKED 1" PN A53974259202, FR64 - 65 24" LT OF CTR OF ACFT. R & R LONGITUDINAL PROFILE FR 64 TO FR65 Y805 IAW SRM 51-72-10, PGS 1-3.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

AFT SEAT TRACK 1 HAS CORROSION FR 71 TO FR 75 (ABOUT 70 SQUARE INCH). REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, PAGE 101-103. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK NR1 BETWEEN FR71 & FR 75, FABRICATED SEAT TRACK IAW SRM 51-21-11 PG1, SRM 51-27-00, PG 1, SRM 51-40-40, PG1. INSTALLED SEAT TRACK BETWEEN FR 71 AND FR 75 IAW SRM 51-40-21, PAR 7, PAGE 24.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 40,876 hrs · 18,747 cycles

UPON REMOVAL OF RUBSTRIP ON NR N00391 RT WING OTBD FLAP UPPER MAIN SKIN BETWEEN RIBS 4 AND 5 ALSO BETWEEN THE MAIN SPAR CHORD AND REAR SPAR CORD HAS 8 DENTS WHICH 2 EA ARE VISABLE UNDER THE RUBSTIPS. DAMAGE IS IN A 10 IN X 12 IN AREA. CUTOUT DAMAGE AREA AND REPAIRED IAW SRM 57-53-12, PARA 14, PG 255-260, FIG 210 C/W EA 6-5750-145550.

Part: CHANNEL — CORRODED (ZONE 300) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

FRAME LOCATION 87, BETWEEN STR 15 AND 16 FOUND CORROSION ON LT SIDE AFT UPPER "U" CHANNEL (CROSS STRUT). 1 AREA OF CORROSION ON UPPER FLANGE APPROX 1 SQ IN. R & R CROSS STRUT AT FR87 BETWEEN STR15 AND 16 IAW SRM 51-40-21.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

MAIN CABIN FLOORBEAM CRACKED IN RADIUS FR36 BETWEEN L2 AND L3 SEAT TRACK. REPAIRED CROSSBEAM AT FR36 BETWEEN SEAT TRACKS 2L AND 3L IAW SRM 53-10-15.

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO FLOOR SUPPORT LONGITUDINAL PROFILE BROKEN BETWEEN FRAMES 65 AND 66 LT STR 52 LT. R & R PROFILE SECTION FR65 TO FR66 LT ABOVE STR52L IAW SRM 51-72-10.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FR 85 , APPROX 15 INCHES INBD OF STR16 RT, HORIZONTAL CROSSBEAM HAS EXFOLIATION CORROSION ON LOWER FLANGE REMOVED CORROSION FROM CROSSBEAM AT FR 85 INBD OF STR 16R AND CHECKED LIMITS IAW SRM 53-19-47 AND SRM 53-10-00, FIG 105 . REMOVED CROSSBEAM AND REPLACED WITH FABRICATED CROSS BEAM IAW SRM 53-19-47 AND SRM 51-72-10 P1-3.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

AFT SEAT TRACK 1-R HAS CORROSION, FR78 - FR79, 20 SQUARE INCHES. R & R SEAT TRACK BETWEEN FR76 AND FR79 SEAT TRACK 1 IAW SRM 51-40-21, PG 24, 51-27-00, PG1, 51-40-40, PG1, 51-74-10, PG210, 51-21-10, PG6 -7, 53-10-16, PG101 - 103, 51-75-10, PG206.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

AFT SEAT TRACK 1 HAS CORROSION FR 75 TO FR 77 ABOUT 30 SQUARE INCHES, REMOVED, FABRICATED AND INSTALLED SEAT TRACK 1, FR75 TO FR79 ALL IAW SRM 51-40-21, PG 24 PARA 7, 51-27-00, PG 1, 51-27-11 PG 1, 51-40-40 PG 1, 51-75-10 PG 206, PARA 4.

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

AFT CARGO FLOORBEAM RUNNING FWD AND AFT BETWEEN FR66 AND FR65 APPROX 2' RT OF ACFT CTR IS BROKEN. R & R PROFILE SECTION FR65 TO FR66, RBL18 TO RBL24 IAW SRM 51-72-10, PGS 1-3.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO COMPARTMENT UNDERFLOOR, FR69, 17" TO 19" RT OF ACFT CENTERLINE, AXIAL FLOOR PANEL SUPPORT ANGLE HAS CORROSION/SWELLING ABOUT 6 SQUARE INCHES. BULK CARGO COMPARTMENT R & R PROFILE SECTION FR66 TO FR69 RBL17 TO RBL19 IAW SRM 51-72-10, PGS 1-3.

Part: BEAM — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO, AFTER REMOVING LATERAL BEAM AT FR67 FOUND AXIAL BEAM CORRODED THROUGH 100 PERCENT PN A53974261202, BULK CARGO. R & R PROFILE BEAM FR66 - FR69 (Y535) IAW SRM 51-72-10, PGS 1-3.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO UNDERFLOOR AXIAL FLOOR SUPPORT ANGLE HAS CORROSION/SWELLING, LT 4" TO 7" FR67 ABOUT 6 SQUARE INCHES. R & R PROFILE SECTION FR66 TO FR69 LT 4" TO 7" IAW SRM 51-72-10, PGS 1-3.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

FWD CARGO COMPARTMENT FOUND 1EA CRACK (.1250" DEEP) IN RADIUS OF UPPER FLOORBEAM FR38, BETWEEN UPPER SEAT TRACK 4L AND 5L CROSSBEAM REPAIRED AT CRACKED STIFFENER FR38 BETWEEN SEAT TRACKS 4L AND 5L IAW A310 SRM 53-10- 15 PGS 246 - 251/252 FIG. 203

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

CORROSION ON OTBD FLANGE OF SEAT TRACK 4R 2" AFT OF FRAME 34 1"X4 ". REMOVED DAMAGED SEAT TRACK 4R FR26 -FR36 IAW SRM 53-10-16, FIG 208. INSTALLED REPLACEMENT SEAT TRACK AND SPLICES IAW SRM 53-10-16, FIG 208.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

MAIN CABIN CORROSION ON SEAT TRACK 5L APPROX 1"X 2" BETWEEN FRAME 35 AND 36. R & R SEAT TRACK 5L AT FR35-FR36 AND 4EA SEAT TRACK SPLICES IAW SRM 53-10-16, PG 244, PGS 250A/250B FIG 208A.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO UNDERFLOOR, FR69 CORROSION ON CARGO NET CLEVIS SUPPORT ANGLE, (ABOUT 2 SQUARE INCHES) R & R BULK CARGO UNDERFLOOR CARGO NET CLEVIS SUPPORT FITTING, FR69 IAW SRM 51-72-10, PGS 1-3.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

FWD CARGO COMPARTMENT, UPPER FLOORBEAM FR33 HAS 1EA CRACK IN RADIUS BETWEEN SEAT TRACKS 2R AND 3R. CROSSBEAM REPAIRED AT FR33 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 53-10-15, FIG 203.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

MAIN CABIN COURIER AREA UNDER FLOOR, CORROSION ON LONGITUDINAL MEMBER AT FLOOR SUPPORT ANGLE 7" FWD OF FLOORBEAM AT FR13, 40" TO LT FROM ACFT CENTERLINE. AMM 53-12-00-06, 57" FROM ACFT CENTERLINE ABOUT 2 SQARE INCHES. REMOVED AND INSTALLED NEW T-CAP TO LONGERON AND SPLICE ANGLES FR12 TO FR15 AT Y1456 IAW SRM 53-12-15, FIG 207 AND 51-72-10 PGS 1-3.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 40,876 hrs · 18,747 cycles

BULK CARGO UNDERFLOOR FR69 10" LT FROM ACFT CENTERLINE, FLOOR SUPPORT ANGLE HAS CORROSION ABOUT 3 SQUARE INCHES. FABRICATED 1 EA FITTING IAW DWG A53974329. R & R FITTING AT FR69 10" LBL IAW SRM 51-72-10, PGS 1-3.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

CORROSION IN CTR TOP OF SEAT TRACK 2L FRAME 51 ABOUT 5"X1". R & R DAMAGED SEAT TRACK 2L FR49.5 TO FR54 AND INSTALLED A SPLICE REPAIR ON SEAT TRACK 2L AT FR49.5 ALL IAW SRM 53-10-16, FIG 205.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

SEAT TRACK 4R HAS CORROSION AT 8" AFT OF FR51 (-1959) R & R SEAT TRACK SEGMENT AND SPLICE REPAIR AT FR51 TO FR52 SEAT TRACK 4R IAW SRM 51-72-10, PGS1-3 AND 53-10-16 FIG 205.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 86, STR 16, LT TO THS DRIVE UNIT SUPPORT, FWD CROSSBEAM HAS EXFOILIATION CORROSION. REMOVED LEVEL 1 CORROSION. REWORKED CROSSBEAM ON FR 86 AT STR 16 LT IAW SRM 51-74-10. MATERIAL LOSS .006 IN. REMAINING THICKNESS WITHIN LIMITS IAW SRM 51-73-11, PG 1-17. REPROTECTED IAW SRM 51-75-10.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 87-89, STR 16 RT, THS CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 INCHES AT AFT ATTACH. R & R THS CUTOUT UPPER FWD CORNER FITTING FR87 TO FR89, STR 16R IAW SRM 51-72-10.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 85, APPROX 15 INCHES INBD OF STR 16 RT HORIZ CROSSBEAM HAS EXFOILIATION CORROSION ON LOWER FLANGE. REMOVED LEVEL 1 CORROSION. FRAME R & R IAW SRM 53-19-47 WITH FABRICATED PART REF SDR NR 11-0303.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 87-88, STR 16, RT HORIZ STAB CUTOUT SUPPORT BEAM INBD FACE CORRODED AT 1 EA LOCK FASTENER APPROX 1 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, FOUND TO BE WITH IN MFG TOLERANCES IAW DWG A53985426 AND DAN11304 NDT INSP IAW NTM 51-10-08 NO CRACKS. REPROTECTED AREA IAW SRM 51-21-10, PARA B AND 51-75-10 PARA C. INSTALLED NEW FASTENER IAW SRM 51-40-21, PARA 7B.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

REAR FUSELAGE FRAME 87-89, STR 16, LT HORIZ STAB CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 SQ INCHES. R & R THS CUTOUT FWD FITTING IAW DWG A53985135 AND A310 SRM 51-40-21, PG 46.

Part: RIB — CORRODED (VERTICAL STAB) · airframe 40,876 hrs · 18,747 cycles

VERTICAL STABILIZER, RIB 1 TOP SURFACE HAS CORROSION (ABOUT 4 SQ INCHES) RT STRINGER 5 RT TO STR 7 RT. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-31-19, PG 209-211, FIG 203.

Part: MOUNT — CORRODED (VERTICAL STAB) · airframe 40,876 hrs · 18,747 cycles

VERTICAL STABILIZER LT AFT MOUNT LUG HAS CORROSION FROM STR 1 LT TO STR 4 LT, ABOUT 70 SQ INCHES. REPAIRED VERT STAB LT AFT MOUNT LUG BETWEEN S1L TO S4L IAW EA 6-5530-145538.

Part: MOUNT — CORRODED (VERTICAL STAB) · airframe 40,876 hrs · 18,747 cycles

VERT STABILIZER AFT RT MOUNT LUG FITTING HAS CORROSION ON INTERIOR SURFACE BETWEEN STRINGER 1 RT AND STRINGER 2 RT,ABOUT 2 SQ INCHES. REPAIRED VERT STAB AFT RT LUG FITTING INTERIOR SURFACE BETTWEEN STR1R AND STR2R IAW EA 6-5530-145539.

Part: PROFILE — CORRODED (VERTICAL STAB) · airframe 40,876 hrs · 18,747 cycles

RT VERTICAL STABILIZER T/E HORIZ PANEL LANDING SUPPORT STRAP BETWEEN RIBS 21-22 HAS 8 INCH CORROSION IN AND AROUND 3 EA FASTENERS AND ALONG UPPER INTERIOR MATING SURFACE. R & R EDGE PROFILE RT VERT STAB T/E PANEL LANDING BETWEEN RIBS 21 AND 22 IAW SRM 51-72-10, PGS 1-3. MINOR REPAIR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

BULK CARGO FLOOR SUPPORT LATERAL ANGLE AT FR66 HAS CORROSION AT NUT PLATE LOCATIONS, 10 PLACES, FROM RT 19" TO LT 48" FORM CTR LINE OF ACFT TOTALING 10 SQUARE INCHES. AFT CARGO COMPARTMENT R & R FR66 LATERAL FLOORBEAM AND VERTICAL STIFFENER IAW SRM 51-72-10, PG 1-3.

Part: RIB — CORRODED (ZONE 300) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

VERTICAL STABILIZER RIB 1 WEB TOP SURFACE HAS CORROSION ( ABOUT 4 - SQUARE INCHES) RT STRINGER 5R TO STRINGER 7R VERT STAB RT SIDE REMOVED CORRODED SECTION ON RIB1 WEB BETWEEN STR 5R AND 7R IAW SRM 55-31-19, PG 209 - 210 FIG 203. FABRICATED AND INSTALLED REPAIR IAW SRM 55-31-19, PG 209-211, FIG 203.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 40,876 hrs · 18,747 cycles

DUMMY SEAT TRACK RT NR6 AT FR 54.2 HAS GAP AT SLOTTED END. ATTACH BOLT OF .026". REMOVED, REPAIRED AND REINSTALLED DUMMY SEAT TRACK RT NR6 IAW EO 6-5310-7-3322, P2 INSTRUCTIONS.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

MAIN DECK CARGO COMPARTMENT ZONE 230, FR 32 BETWEEN SEAT TRACK 5R AND 6R PAN CORRODED TOP SKIN APPROX 1 SQ INCH. REMOVED CORROSION FROM PAN AND CHECKED LIMITS IAW SRM 53-10-00, PAGE 113 FOUND TO BE OUT OF LIMIT. R & R THRUST PLATE AND STIFFENERS IAW SRM 51-40-21, PARA 6 AND PARA 7.

Part: SEAT TRACK — WORN (ZONE 500) · airframe 40,876 hrs · 18,747 cycles

DUMMY SEAT TRACK L3 AT FRAME 38.2 HAS A GAP AT SLOT OF 0.020 INCH. REMOVED DUMMY SEAT TRACK NR3L, AT FR 38.2. REPAIRED AND REINSTALLED IAW E0 6-5310-7-3322, P2 INSTRUCTIONS.

Part: FLOORBEAM — MISREPAIRED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN FLOORBEAM FRAME 25 FWD UPPER FLANGE BETWEEN SEAT TRACKS NR2 AND NR3 RT WAS DETERMINED TO NOT BE IAW SRM 53-10-15, FIG 206 (SHEET 4) PAGES 231-232, REPAIRED IAW SRM 53-10-15 (SHEET 4) PAGES 221-224 & 231-232.

Part: SEAT TRACK — WORN (CABIN) · airframe 40,876 hrs · 18,747 cycles

DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 AT FR 38.2 HAS A GAP AT THE SLOT OF .031" REMOVED, REPAIRED AND REINSTALLED THE DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 BETWEEN FR 38.2 TO FR 40/41 IAW EO 6-5310-7-3322 P2 INSTRUCTIONS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

AFT MDCC SEAT TRACK NR1 (Y -0) HAS CORROSION AT 9" TO 12 " FWD OF FR 70 (ABOUT 3 SQ INCHES). REMOVED SEAT TRACK SECTION NR1 (Y -0) FROM BETWEEN FR 66 TO FR 73. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION NR1 (Y - 0) FROM BETWEEN FR 66 TO FR 73 USING THE ORIGINAL PRODUCTION SPLICE SECTIONS, IAW SRM 53-10-16, FIG 101.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

BULK CARGO UNDERFLOOR FLOOR PANEL LATERAL SUPPORT, FR 67 ANGLE HAS CORROSION, LT 4" TO 9" FROM ACFT CENTERLINE ABOUT 6 SQUARE INCHES. R & R SUPPORT BEAM IAW SRM 53-10-15, FIG 104, 51-40-21, PARA 6 & 7.

Part: SEAT TRACK — CORRODED (ZONE 300) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

AFT MDCC SEAT TRACK NR1 (Y-0) HAS CORROSION AT FWD END 10" TO 12" FROM FR 71 (APPROX 4 SQ INCHES). REMOVED OLD SEAT TRACK SECTION, NR1 (Y -0) BETWEEN FR 66 & FR 73. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION, NR1 (Y -0) BETWEEN FR 66 & FR 73 USING THE ORIGINAL SPLICE SECTIONS IAW SRM 53-10 16, FIG 101.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,876 hrs · 18,747 cycles

BULK CARGO UNDER FLOOR FR 69 LATERAL FLOOR SUPPORT ANGLE HAS CORROSION AT 17 TO 19 INCH RT OF A/C CENTER LINE (ABOUT 8 SQ. INCH) REMOVED SUPPORT BEAM, FR 69 BULK CARGO FLOOR IAW SRM 51-72-10 PAR NR 2 , LOCATED AND DRILLED UP NEW BEAM IAW SRM 51-72-10 , INSTALLED NEW BEAM IAW SRM 51-72-10, PAGE 2, PARA.6.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,876 hrs · 18,747 cycles

AFT MDCC SEAT TRACK NR3 (-Y953) HAS CORROSION AT 7.5 INCH FWD OF FRAME FR 55/58 TO 10.5 INCH AFT OF FR 55/58 ABOUT 72 SQ IN. REMOVED CORROSION FROM SEAT TRACK SEC 55/58 IAW SRM 51-74-10, PAGE 210. CHECKED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PAGE 103. R & R SEAT TRACK SECTION IAW SRM 53-10-16, PAGE 103.

Part: AUTOBRAKE SYS — MALFUNCTIONED (MLG) · airframe 39,552 hrs · 17,850 cycles

AUTO-BRAKE FAULT. FAULT CLEARED ON FINAL APPROACH BACK TO LAX DEBRIEFED FLIGHT CREW AS TO SYMPTOMS. PERFORMED BITE CHECK OF CONTROLLER WITH NO FAULTS LOGGED. SYSTEM ARMS AS NORMAL, NO FAULTS, ACFT OK FOR FURTHER FLIGHT. MOCC TRACKED 4 GOOD LEGS.

Part: LANDING GEAR — MALFUNCTIONED (NR 1) · airframe 39,137 hrs · 17,550 cycles

DURING GEAR EXTENSION ON SYSTEM NR 1 GEAR DID NOT EXTEND (THREE RED INDICATIONS) WENT AROUND CYCLED GEAR HANDLE UP AND THEN BACK DOWN AND GEAR EXTENDED NORMALLY (ALL ON SYSTEM NR 1).

Part: FITTING — CORRODED (ZONE 400) · airframe 38,978 hrs · 17,443 cycles

NR 2 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 2 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121273, RELEASE DATE 20 MAY, 2008.

Part: FITTING — CORRODED (ZONE 400) · airframe 38,978 hrs · 17,443 cycles

NR 1 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 1 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121272, RELEASE DATE 20 MAY, 2008.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 38,978 hrs · 17,443 cycles

BULK CARGO DOOR SKIN HAS GOUGE MEASURING 1.0 SQ IN BY .030 IN DEEP, LOWER AFT EXTERNAL SURFACE SMOOTHED OUT GOUGE AND INSTALLED EXTERNAL SKIN REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR 68 AND FR 69 LOWER AFT IAW A310-200 SRM 52-30-00, FIG 203, PG 215/216.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 38,978 hrs · 17,443 cycles

RT HORIZONTAL TRAILING EDGE SUPPORT RIB AT RIB 11 HAS CORROSION AROUND FASTENER HOLES ON LOWER AND UPPER FLANGES REMOVED LEVEL 1 CORROSION AND INSTALLED FORMED SECTION REPAIR ON RT HORIZONTAL TRAILING EDGE BETWEEN RIB 11 AND RIB 12 IAW A310-200 SRM 55-13-11, FIG 1 AND 51-71-40, FIG 201.

Part: SKIN — FAILED (TE FLAP) · airframe 38,978 hrs · 17,443 cycles

PREVIOUS REPAIR BONDED REPAIR DOUBLER LOCATED ON LT WING INBD FLAP TRAILING EDGE LOWER SKIN BETWEEN TRACK 1 TO TRACK 2 AND AT THE AFT EDGE MEASURES 38.3 INCH BY 10.2 INCH WITH A TRIPLER MEASURING 3.3 INCH BY 10.2 INCH ON TOP BETWEEN RIB 4 AND RIB 5 REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR AT LT INBD FLAP TRAILING EDGE BETWEEN TRACK 1 AND TRACK 2 IAW FED EX EA 6-5750-121311 RELEASE DATE 19 JUNE,2008. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION.

Part: FITTING — CORRODED (ZONE 400) · airframe 38,978 hrs · 17,443 cycles

LT PYLON LOWER LUG FITTING, RIB 18, HAS PITTING CORROSION ON 4 FASTENER HOLES REMOVED LEVEL 1 CORROSION AND REPAIRED LT PYLON RIB 18 LUG FITTING IAW FED EX EA 6-5450-121279, RELEASE DATE 29 MAY, 2008

Part: FITTING — CORRODED (ZONE 400) · airframe 38,978 hrs · 17,443 cycles

RT PYLON LOWER LUG FITTING, RIB 18, HAS 4 EA HOLES WITH CORROSION REMOVED LEVEL 1 CORROSION AND REPAIRED RIB 18 FITTING IAW FED EX EA 6-5450-121280, RELEASE DATE 29 MAY, 2008

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 38,978 hrs · 17,443 cycles

PREVIOUS EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RT WING O/B FLAP TRAILING EDGE LOWER SKIN BETWEEN RIBS 3 AND 4 MEASURING 5.7 INCH BY 5.7 INCH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RT WING O/B FLAP TRAILING EDGE LOWER SKIN BETWEEN RIBS 3 AND 4 IAW SRM 57-53-12 FIG 207 SHEETS 1 AND 2.

Part: STRINGER — CORRODED (ZONE 300) · airframe 38,978 hrs · 17,443 cycles

4 SQ INCHES OF CORROSION EXIST AT RT HORIZONTAL STAB L/E UPPER FLANGE APPROXIMATELY RIB 5 IN AND AROUND 2 EACH NUTPLATES. "PREVIOUS REWORK SURFACE" REMOVED LEVEL 1 CORROSION AND INSTALLED REPAIR STRAP AND SHIM AT RT HORIZONTAL STAB L/E UPPER FLANGE APPROXIMATELY RIB 5 IAW A310-200 SRM 55-11-21 FIG 205/206.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 38,978 hrs · 17,443 cycles

PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 6 RT - Y2462 BETWEEN FRAMES 34 TO 36, HAS 4 EACH REPAIR SPLICES, THE AFT INBD AND OTBD REPAIR SPLICES MEASURE 8.4 INCHES LONG BY 3 INCHES TALL, THE FWD INBOARD AND OUTBOARD REPAIR SPLICES MEASURE 8.4 INCHES LONG BY 3 INCHES TALL AND 1 EACH SEAT TRACK REPAIR SECTION MEASURING 21 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT SEAT TRACK REPAIR AT MAIN CABIN SEAT TRACK NR 6 RT - Y2462 BETWEEN FRAMES 34 TO 36 IAW A310-200 SRM 53-10-16 FIG 208.

Part: FRAME — DAMAGED (ZONE 200) · airframe 38,978 hrs · 17,443 cycles

PREVIOUS FRAME REINFORCING PLATE REPAIR LOCATED IN MAIN CABIN ON FRAME 54.2 INNER FLANGE BETWEEN STRINGERS 11 TO 15 LT, HAS 1 EACH EXTERNAL FORMED REPAIR PLATE MEASURING 21.8 INCHES LONG BY 2.2 INCHES TALL AND THE FRAME INNER FLANGE HAS A CUT OUT MEASURING 11 INCHES LONG. REPAIR NOT IAW EA6-5321-50501 REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR IN MAIN CABIN ON FRAME 54.2 INNER FLANGE BETWEEN STRINGERS 11 TO 15 LT IAW EA6-5310-121285.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,978 hrs · 17,443 cycles

1/4 INCH CRACK IN FLOORBEAM C25 BETWEEN SEAT TRACK 2R AND 3R AT UPPER RADIUS IN FRONT FACE STIFFENER. REMOVED CRACK AND INSTALLED FLOORBEAM REPAIR ON FLOORBEAM FR C25, BETWEEN SEAT TRACKS 2RT AND 3RT IAW A310-200 SRM 53-10-15 FIG, 206.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,978 hrs · 17,443 cycles

MAIN CARGO DECK THRU FWD CARGO COMP CEILING FLOORBEAM HAS .250 INCH CRACK ON VERTICAL STIFFENER BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT AT FR 36 CUT OUT DAMAGE AND INSTALLED CROSSBEAM REPAIR AT FR 36 BETWEEN SEAT TRACKS NR 4LT AND NR 5LT IAW A310-200 SRM 53-10-15, FIG 206, PAGE 231/232.

Part: ENGINE — VIBRATION (NR 1) · airframe 38,859 hrs · 17,361 cycles

CLIMBING THROUGH FL 320 TO FL 350 WITH ALL CONDITION NORMAL, ACFT SHUDDERED AND SWERVED SLIGHTLY, THEN BEGAN CONTINUOUS THUMPS, BOTH AUDIBLE AND CLEARLY FELT THROUGH AIRFRAME. THERE WERE NO ECAM ADVISORIES, BUT NR 1 ENGINE N1 DECREASED TO APPROX 60 PERCENT. BROUGHT NR 1 THROTTLE TO IDLE AND THUMPS STOPPED. STILL NO OBVIOUS INSTRUMENT INDICATIONS AND NO VIBRATION INDICATION ON ECAM ENGINE PAGE. ADVANCED THROTTLE SLIGHTLY AND GOT IMMEDIATE RETURN OF VIBRATIONS. SHUT DOWN ENGINE, DECLARED EMERGENCY, AND DIVERTED. R&R NR 1 ENGINE IAW WORK CARD 44T0701-1, OPS CHECK NORMAL IAW WORK CARD 44T0701-1.

Part: FCU — MALFUNCTIONED · airframe 37,222 hrs · 16,540 cycles

AFTER DISPATCHING W/NR 6 SPOILERS INOP DURING PUSHBACK, THE NR 2 AND NR 3 SPOILERS FAULTED AT CRUISE. AFTER 1 MINUTE, ATTEMPTED RESET WITH NO CHANGE CONTINUED W/NR'S 2, 3, 6, 7 INOP ALL SWITCHES REMAINED OFF. PER TSM 27-61-00 RECORDED FAULTS FROM EFCU 1 "C2'2'" EFCU2 "M1 '1'". OPERATED SPOILERS WAS ABLE TO RESET FAULTS ON SPOILERS NR 2 AND NR 3 AND ALSO RESET FAULT "C2'2'" ON EFCU 2. REMOVED AND REPLACED EFCU IAW MM 27-61-34-4.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 36,401 hrs · 16,171 cycles

JUST BEFORE TAKEOFF RECEIVED A MIN EQUIPMENT BAY SMOKE LIGHT, FOLLOWED BY A MAIN DECK CARGO SMOKE WARNING. AIR SYSTEM SERVICING IAW A310-200 AMM 21-51-00-3,TSM 26-15-00. REMOVED AND REPLACED NR 1 & 2 COALESCER BAGS IAW AMM 21-51-16-3. PERFORMED ENGINE RUNS IAW A310-200 JRH. FOUND COOLING AIR TUBE AT MIN EQUIP BAY LOOSE. RECONNECTED TUBE IAW AIRBUS SMP. RECOMMEND AVI ASSIST TO PUT A/C IN FLYING STATUS WITH ALL EQUIP FUNCTIONING DURING HIGH POWER TO ENSURE NO RETURN OF SMOKE WARNINGS. DETERMINED ENGINE WASH TASK CARD C/W FOR EGT MARGIN C/W IN B CK. ADDITIONAL PROCEDURES UNDER REVIEW TO PREVENT REPEAT OF SIMILIAR OCCURANCE.

Part: SLIDE — FAILED (RIGHT) · airframe 36,401 hrs · 16,171 cycles

RIGHT EVACUATION SLIDE FAILED TO DEPLOY WHEN DOOR OPENED. F/O PULLED MANUAL INFLATION LANYARD AND SLIDE INFLATED. THIS RT DOOR SLIDE NEEDS TO BE HELD FOR FLIGHT SAFETY & THE NTSB FOR IMPOUNDING. PLEASE REMOVE, TAG & ID WHERE PARTS ARE LOCATED AFTER REMOVAL.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE FWD OF FS 17 STA 1315 BETWEEN STR 35R AND 38R FLUSH DOUBLER NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00718. REPAIR IAW EA 6-5312-95504.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 36,056 hrs · 15,993 cycles

LT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00541. REPAIRED LT UPPER IB THS SPAR CORD IAW A310-200 SRM 55-11-21 PARA 7.H PAGES 315TO, 320 FIG 211,213 AND 219 SHEET 2.

Part: BEAM — DAMAGED (NLG WW) · airframe 36,056 hrs · 15,993 cycles

IN NOSE WHEEL WELL FWD VERTICAL BEAM RT HAS 1 EA ELONGATED HOLE ON LOWER FLANGE REF N00811. ACCOMPLISHED BUSHING REPAIR IAW EA 6-5312-95444 AND A310-200 SRM 51-40-51 PAGE 12.

Part: REPAIR — IMPROPER (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE EXT DOUBLER AFT OF BULK CARGO DOOR STA 3885 FR 72 STR 38 RT TO 39 RT NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00699. REPAIR NOT IAW A310-200 SRM 53-10-12 FIG 225 AND 233. REPAIRED AREA IAW EA 6-5310-95479.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 36,056 hrs · 15,993 cycles

RT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00542. REPAIRED RT HORIZONTAL T/E UPPER SPAR CORD IAW SRM 55-11-21 PARA 7.H PAGES 315 TO 324 FIG SHEET 2 AND FIG 213.

Part: REPAIR — NONE (L/E SLAT) · airframe 36,056 hrs · 15,993 cycles

PREVIOUSLY REPAIR INSTALLED ON L/W NR 1 SLAT IB LEADING EDGE, SKIN BLIND FASTENER FLUSH. REPAIR WS RIB 2 TO RIB 3, NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00708. REPAIR EVALUATED AS GOOD IAW EA 6-5750-95471.

Part: PANEL — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

NOSE GEAR WELL, FWD WALL HAS 13 SPOTS OF LIGHT CORRODED AND SEVERAL SMALL SPOTS OF BARE METAL. REF N00747, REPAIRED NOSE LANDING GEAR BAY FORWARD PANEL BY REPLACING IAW REPAIR INSTRUCTION R53611077 AND NLG BAY PANEL REPLACEMENT, DWG R53610532. (K)

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

BELLY OF AC RT SIDE FWD OF NR 2 PACK PORTABLE WATER SERVICE HAS CORROSION ON CUTOUT REF N00031. REPAIRED DAMAGE IAW EA 6-5330-94498 AND SRM 51-72-10 AND SRM 53-10-14.

Part: DOUBLER — NONE (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT EXT DOUBLER ABOVE AND AFT OF CAPT,S SIDE WINDOW, STA. 881 TO 904 FR 7 TO FR 8 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00696 REPAIR GOOD IAW EA 6-5330-95466.

Part: FASTENER — INCORRECT (NR 1 PYLON) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00705. EVALUATION OF REPAIR REVEALED INCORRECT FASTENERS INSTALLED REPLACED REPAIR IAW SRM 54-54-51, FIG 203, SH 1.

Part: FASTENER — INCORRECT (NR 1 PYLON) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA, REF N00705. REPAIR REVEALED INCORRECT FASTENER INSTALLED REMOVED AND REPLACED REPAIR IAW 54-54-51.

Part: COVER — DAMAGED (ZONE 200) · corrosion level 2 · airframe 36,056 hrs · 15,993 cycles

MAIN CARGO COMPARTMENT, FS 75L, ABOVE AFT PAX DOOR CORRODED. REPLACED FILLER, ANGLE AND SHIM IAW A310-200 SRM 53-18-18. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00207.

Part: REPAIR — UNKNOWN (ZONE 200) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE FLUSH REPAIR AFT OF MAIN DECK CARGO DOOR STA 1923 - 1976 FS 35-36, STR 10-11, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR INSTALLED AS PART OF P-F CONVERSION AND MEETS REQUIREMENTS OF DWG R537B1607. NO FURTHER ACTION REQUIRED. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00697.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE FS 12A STA1091 - 40" BELOW MAIN DECK FLOOR, FLUSH DOUBLER NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR NOT IAW A310-200 SRM 53-12-12 PB201 FIG 202. REMOVED EXISTING REPAIR IAW A310-200 SRM 51-40-21. REPAIRED SKIN IAW A310-200 SRM 53-12-12 PB201 FIG 202. MINOR REPAIR IAW GMM 6-2-100. WORKED ON NRC N00715.

Part: FITTING — CORRODED (LT MLG WW) · corrosion level 2 · airframe 36,056 hrs · 15,993 cycles

LT MAIN GEAR WHEEL WELL LOWER AFT CORNER FITTING HAS 15 SQ" OF CORROSION. FABRICATED NEW SPLICE FITTING IAW 6-5315-94776. REPLACED CORRODED SPLICE FITTING IAW EA 6-5315-94755. MINOR REPAIR IAW GMM 6-2-100. WORK PERFORMED ON NRC N00739.

Part: REPAIR — UNKNOWN (ZONE 600) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON RT WING TE PANEL EXTERNAL SKIN AFT OF PYLON, EXTERIOR DOUBLER, STA 482-513 RIB 8-9, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUSLY INSTALLED REPAIR ON RT WING T/E PANEL AFT OF PYLON WAS ACCOMPLISHED ON EA 5710-29479. VISUAL EVALUATION CONSISTED OF CORRECT LOCATION, SHAPE, SIZE, FASTENER SPACING/NUMBER, MATERIAL THICKNESS/TYPE AND GOOD WORKMSNSHIP. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. WORK DOCUMENTED ON NRC N00712.

Part: REPAIR — UNKNOWN (FUSLEAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE, EXTERNAL DOUBLER AT FR15 BELOW R1 DOOR SCUFF PLATE, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED IAW A310-200 SRM 53-12-12 PB 201. EXISTING REPAIR INSTALLED ON EA6-5330-46467 AND REQUIRES NO FURTHER ACTION.

Part: FLOORBEAM — NONE (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIRS ON MAIN DECK CARGO FLOORBEAMS AT FS 34, FS 35, AND FS 36, RT OF CENTER, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATION DETERMINED REPAIRS TO BE IAW EA 6-5310-29466. NO FURTHER ACTION REQUIRED. MINOR REPAIR IAW GMM 6-2-100. WORKED ON NRC N00727.

Part: REPAIR — UNKNOWN (HORIZONTAL STAB) · airframe 36,056 hrs · 15,993 cycles

REPAIR ASSESSMENT. HORIZONTAL STAB LE PANEL 331AB. EXISTING REPAIR BETWEEN RIB 2 - 3 LOWER SURFACE. EXISTING REPAIR NOT IAW A310-200 SRM 55-12-12. REMOVED 2 REPAIR ANGLES IAW A310-200 SRM51-40-21. FABRICATED AND INSTALLED NEW ANGLES IAW A310-200 SRM 55-12-12. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00758.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE FS 39, LT STR 51 - 54, EXTERNAL DOUBLER FWD OF NR 1 AC PACK INLET FAIRING NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR HAS BEEN ACCOMPLISHED IAW A310-200 SRM 53-15-12 FIG 201. NO FURTHER ACTION REQUIRED. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00693.

Part: REPAIR — UNKNOWN (ZONE 500) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON LT WING IB L/E IB OF NR 1 SLAT, EXTERNAL DOUBLER WS 139 RIB3, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUS REPAIR WAS NOT AN APPROVED REPAIR. REMOVED SKIN IAW A310-200 SRM 51-72-10. FABBED NEW SKIN IAW DWG A572462402 AND INSTALLED IAW A310-200 SRM 51-72-10.

Part: REPAIR — UNKNOWN (ZONE 200) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIRS INSTALLED ON MAIN CARGO DECK FLOORBEAM AT FS 37 30" LEFT OF CENTER, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUS REPAIRS INSTALLED ON EA 6-5310-48685 AND EA 6-5321-50489. NO FURTHER ACTION REQUIRED. WORKED ON NRC N00723. CLASSIFIED AS MINOR REPAIRS PER GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 600) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON RT IB FLAP UPPER SURFACE RIB 17-19, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. THE REPAIR AS NOTED CONFORMS TO SRM 57-52-12 FIG 204 WITH THE EXCEPTION OF FASTENER PITCH. LOCATED AND DRILLED FASTENER HOLE TO COMPLY WITH FASTENER PITCH PER A310-200 SRM 51-40-45. INSTALLED NEW FASTENERS MS20426 A4D IAW A310-200 SRM 51-40-21. NOW PREVIOUSLY INSTALLED REPAIR IS DETERMINE TO BE IAW A310-200 SRM 57-52-11 FIG 204 BASED ON EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING/NUMBER, AND MATERIAL TYPE/THICKNESS. WORK DOCUMENTED ON NRC N00713.

Part: REPAIR — UNKNOWN (NR 1PYLON) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON NR 1 PYLON LT SIDE OB AFT LWR FAIRING EXTERNAL DOUBLER AT RIB 20, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR FOUND NOT TO BE I/A/W A310-200 SRM 54-54-51 FIG 203. REMOVED EXISTING REPAIR I/A/W A310-200 SRM 51-40-21. FABRICATED AND INSTALLED NEW DOUBLER IAW A310-200 SRM 54-54-51 FIG 203. MINOR REPAIR IAW GMM 6-2-100. WORK PEFORMED ON NRC N00704.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,056 hrs · 15,993 cycles

AIR COND BAY LT SIDE FS 44-FS 47 LT STRINGER 47 HAS 15 SPOTS OF LT CORROSION AS MARKED. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW A310-200 SRM 53-10-00. OVERSIZED HOLE REPAIRED BY INSTALLING 2 BUSHINGS AND REPAIR ANGLE IAW EA 6-5310-94773. MAJOR REPAIR PER GMM 6-2-100. WORK PERFORMED ON NRC N00657.

Part: REPAIR — IMPROPER (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIRS ON MAIN DECK CARGO SEAT TRACK SPLICE FROM FR 58 TO 61 3RD TRACK LT OF CENTER LINE NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00725. FOUND REPAIR NOT IN CONFORMANCE OF SRM, 53-10-16 FIG 208 R7R REPAIR IAW SRM 53-10-16 FIG 208. MINOR REPAIR IAW GMM 6-2-100.

Part: REPAIR — PROPER (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE AFT OF STATIC PORT EXT DOUBLER AT FR 34 BETWEEN STR 39 RT AND 40 RT NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFACATION AND REPAIR DATA REF N00717. REPAIR FOUND TO BE IAW EA 6-5310-7952, MINOR IAW EA 6-5310-7952.

Part: TRACK — CORRODED (FR 38.2) · airframe 36,056 hrs · 15,993 cycles

CENTER ROLLER TRACK AT FR 38.2 HAS EXFOLIATED CORROSION INSIDE TRAY AND ON AND AROUND FASTENER HOLES OB LEG FR 38.2 TO 38.1 REF N00463. REMOVED AND REPLACED ROLLER TRAY IAW SRM 51-40-21.

Part: ROLLER TRAY — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

RT OB MOST ROLLER TRAY AT FR 38.2 HAS CORROSION ON IB LEG FASTENER HOLE REF N 00466. REMOVED AND REPLACED ROLLER TRAY IAW SRM 53-10-15.

Part: REPAIR — PROPER (ELEVATOR) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR 2 EA EXT DOUBLERS INSTALLED ON RT ELEVATOR IB UPPER SKIN NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00719. REPAIR IS IAW EA 6-2730-50500.

Part: REPAIR — IMPROPER (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

PREVIOUS REPAIR EXT DOUBLER INSTALLED ON L1 DOOR AFT UPPER CORNER NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00722. REMOVED AND REPLACED COVER DUE TO NONCONFORMITY IAW SRM 52-10-00 FIG 203. MINOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN DECK FLOOR LEVEL FS 35 AT SEAT TRACK 6R SEAT TRACK HAS 1 SQ INCH OF CORROSION, REF N00606. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN CABIN BETWEEN FS 15 AND 16 FLOOR LEVEL LBL 2 SEAT TRACK HAS PITTING CORROSION LEFT SIDE REF N00668. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN CABIN LEFT SIDE BETWEEN FS 15 AND 19 SEAT TRACK 1L HAS EXFOLIATION CORROSION IN 3 EA AREAS REF N00669. REMOVED AND REPLACED SEAT TRACK BTW FS 15 AND 19 NR 1L IAW SRM 51-72-10.

Part: SKIN — DENTED (BS 972) · airframe 36,056 hrs · 15,993 cycles

FOUND DENT IN FUSELAGE SKIN AT STA 972 FS 10 AT 12 O`CLOCK POSITION, REF N00688. COMPLIED WITH EA 6-5310-94491.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN CABIN FS 17 TO FS 19 RIGHT SIDE SEAT TRACK 4R HAS 2 AREAS OF EXFOLIATED CORROSION, REF N00662. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-75-10.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

RT SIDE ROLLER TRAY 1 OB OF CENTER AT FS 38 OB LEG HAS 1 EA DOUBLE DRILLED HOLE REF N00468. REPAIRED FLOORBEAM IAW SRM 53-10-15 FIG 207 AND REPLACED ROLLER TRAY IAW SRM 51-75-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

RT SEAT TRACK AT FS 53 NR 5 RT HAS CORROSION IN SCALLOPS REF N00613. REPAIRED SEAT TRACK SECTION IAW SRM 53-10-16 FIG 205.

Part: SEAT TRACK — WORN (FR 61-67) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN DECK CARGO NR 1 SEAT TRACK BETWEEN FRAMES 61 AND 67 HAS 10 AREAS WORN REF N00439. REPAIRED SEAT TRACK IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN DECK RIGHT SIDE FS 15 THRU FS 19 SEAT TRACK 2R HAS SEVERAL AREAS OF CORROSION AND PITTING CORROSION, REF N00664. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · airframe 36,056 hrs · 15,993 cycles

LT SIDE ROLLER TRAY 1 OB OF CENTER HAS 3 EA SPOTS OF CORROSION 2 AT FS 34 TO FS 35 AND 1AT FS 36 REF N00469. REMOVED AND REPLACED ROLLER TRAY IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

MAIN DECK RIGHT SIDE FRAME 16 TO 19 SEAT TRACK 3R HAS SEVERAL AREAS OF EXFOLIATION REF N00663. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN DECK FRAME 45 TO 50 SEAT TRACK 4 LEFT HAS 4 AREAS OF EXFOLIATION, REF N00610. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

MAIN CABIN LEFT SIDE FLOOR LEVEL FRAME 11 TO 14 FLOORBOARD SUPPORT ANGLE HAS SEVERAL AREAS OF EXFOLIATION REF N00670. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FR 45-50) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN DECK FS 45 TO 50 SEAT TRACK 4 LEFT HAS 4 EA AREAS OF EXFOIATION REF N00610. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FR 74-79) · airframe 36,056 hrs · 15,993 cycles

MAIN CABIN SEAT TRACK 3L AT FS 74 TO FS 79 HAS 4 EA AREAS OF CORROSION REF N00522. REPAIRED SEAT TRACK IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN CABIN SEAT TRACK 4R AT FS 76 TO 77 HAS MILD CORR IN 2 AREAS REF N00518. REPAIRED SEAT TRACK IAW SRM 53-10-16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

LT FLOOR SUPPORT BEAM AT FS 23 BETWEEN CENTER AND LT MIDDLE ROLLER TRAY HAS CORROSION AROUND HOLES AS MARKED, REF N00530. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

MAIN CABIN BETWEEN FS 17 AND FS 19 SEAT TRACK 1R RIGHT SIDE HAS 2 SQ INCHES OF CORROSION REF N00665. REMOVED AND REPLACED SEAT TRACK 1R IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

NR 3 SEAT TRACK HAS 3 AREAS OF CORROSION BETWEEN FS 47 AND FS 51, REF N00618. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FOUND MAIN CABIN SEAT TRACK 1 BETWEEN FR 74 TO 79 HAS 6 EA AREAS OF CORR REF N00520. REPAIRED SEAT TRACK IAW SRM 53-10-16.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · airframe 36,056 hrs · 15,993 cycles

LT CENTER ROLLER TRAY OB LEG HAS 8 EA AREAS OF CORROSION AS MARKED FS 38.1 TO FS 33 REF N00465. REMOVED AND REPLACED ROLLER TRAY IAW AMM 25-52-21-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

MAIN DECK CARGO NR 2 L SEAT TRACK AT FRAME 64 HAS MILD CORROSION REF N00440. REMOVED CORROSION CHECK LIMITS IAW SRM 51-74-10 AND 53-10-16 FIG 101. FOUND TO BE WITHIN LIMITS RESTORED FINISH IAW SRM 51-75-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

FLOORBOARD SUPPORT BEAM FS 23 LT SIDE BETWEEN MIDDLE LT AND OB MOST ROLLER TRAY HAS CORROSION AROUND HOLE AS MARKED REF N00529. REMOVED AND REPLACED SUPPORT BEAM IAW SRM 51-72-10.

Part: PAN — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

RT OB MOST FLOOR PAN BETWEEN FS 33 AND 34 HAS 3 AREAS OF CORROSION, REF N00550. REMOVED AND REPLACED THRUST PLATE IAW SRM 51-72-10.

Part: TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

LT CENTER ROLLER TRACK FS 33 TO FS 20 FLOOR BOARD ATTACH HOLES HAVE MINOR CORROSION AND MISSING PROTECTIVE COATING REF N00524. REMOVED AND REPLACED ROLLER TRACK IAW AMM 25-52-21-4.

Part: TRACK — CORRODED (CARGO BAY) · airframe 36,056 hrs · 15,993 cycles

RT CENTER ROLLER TRACK FROM FS 38.1 TO FS 33 OB SIDE HAS 11 EA HOLES WITH CORROSION ON OR AND AROUND REF N00464. REMOVED AND REPLACED ROLLER TRACK IAW AMM 25-52-21-4.

Part: ROLLER TRAY — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

CENTER ROLLER TRAY FS 33 TO FS 20 RT SIDE FLOOR PANEL ATTACH HOLES HAVE MINOR CORROSION AND MISSING PROTECTIVE COATING, REF N00523. REMOVED AND REPLACED ROLLER TRAY IAW AMM 25-52-21-4.

Part: TRACK — CORRODED (FUSELAGE) · airframe 36,056 hrs · 15,993 cycles

RT SIDE ROLLER TRACK OB OF CENTER AT FS 37 IB SIDE HAS CORROSION ON AND AROUND FASTENERS REF N00467. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-40-21.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 35,424 hrs · 15,637 cycles

NR 2 ENG ANTI-ICE FAULT WHEN ENG NR 2 ANTI-ICE TURNED ON. PULLED AND RESET C/B. NO JOY. RELEASED FOR SERVICE PER MEL/CDL: 30-21-01-C CATEGORY: C EXPIRATION: 11APR05 "MEL 30-21-01-C: ENGINE 2 ANTI-ICE VALVE INOP. ENGINE NACELLE VALVE SECURED OPEN." NO TIME TO TROUBLESHOOT DUE TO HISTORY. ITEM DEFERRED PER MEL 30-21-01-C.

Part: DAMPER — LOW (RT MLG) · airframe 33,536 hrs · 14,640 cycles

LANDING GEAR LEVER WOULD NOT RETRACT ON SYS 2 SWITCHED TO SYS 1, STILL WOULD NOT RETRACT. THREE GREEN DOWN WITH 3 RED UNLK. FOUND RIGHT SIDE PITCH DAMPER INDICATION, RESET PIN & RESERVICED PITCH DAMPER WITH NITROGEN TO 1700 PSI. FOUND THE SYSTEM AT 1000 PSI. ALSO PERFORMED A BITE CHECK ON PROX BOX & ALL SYSTEMS ARE GOOD. A/C OK FOR SERVICE. ALL SERVICING PERFORMED PER M/M 12-12-3 2-0 SECTION 9.

Part: DAMPER — MALFUNCTIONED (RT MLG) · airframe 33,536 hrs · 14,640 cycles

REPEAT WRITE-UP, GEAR WOULD NOT RETRACT. AFTER BLOCK IN, LOOKED AT GEAR TRIM CYLINDERS AGAIN AND THE RIGHT GEAR TRIM CYLINDER WAS POPPED AGAIN. PARTS ORDERED, ADDED MPN D22127000-5 CPN 3212339 QTY 1 DAMPER MSN 862119. REMOVED AND REPLACED RIGHT MLG BOGIE BEAM PITCH DAMPER IAW A310-200 SUPP AMM 32-11-15-4, AND EA 6-3210-74064. NO DISCREPANCIES NOTED.

Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 33,811 hrs · 14,782 cycles

ON CLIMBOUT HAD ENG 1 FUEL FILTER CLOG LIGHT ON APPROXIMATELY 100 N1 OUT AT AROUND 90 N1. REPLACED FUEL FILTER PER A310-200 MM 73-12-03 PG 2. LEAK CHECKED NORMAL. RAN ENGINE AT 100 PERCENT N1, NO CLOG LIGHT AT THIS TIME, OK TO CONTINUE.

Part: VANE — GOUGED (ZONE 600) · airframe 32,907 hrs · 14,309 cycles

RT INBOARD FLAP VANE TOP SURFACE 6 INCHES INBOARD FROM OUTBOARD HOIST POINT IS AN AREA GOUGED AND WORN 2 X 2.5 X .012 INCH (BEEN CHAFING ON NR 2 SPOILER ACTUATOR DRIP PAN). BLENDED OUT DAMAGE IAW SRM 51-73-10. NDT BLENDOUT IAW NTM 51-10-08. FILLED REWORK AREA WITH EA 934 A&B IAW EA 6-5750-69671. FABRICATED AND INSTALLED BONDED STEEL DOUBLER PER SRM 57-52-12 FIG 202 AND FAX 942-023683/005/2003 AND EA 6-5750-69671.

Part: OUTFLOW VALVE — DAMAGED (N/A) · airframe 32,016 hrs · 13,795 cycles

OVBD VALVE FAULT PLACED SWITCH TO OFF PER ECAM A/C WOULD NOT PRESSURIZE MEL 04JUN02 23:17 MEM R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-23-06 EQUIPMENT COOLING OVERBOARD VALVE FAULT LIGHT - INOP. VALVE MANUALLY SET PARTIALLY OPEN. FACT 05JUN02 06:33 MEM R RE-INSTALLED RELAY 69HR, REMOVED AND REPLACED EXTRACT OUTFLOW VALVE, RESET C/B'S, OPS CK'D GOOD ON GROUND. REF A310-200M/M 21-23-13-4 OK FOR SERVICE

Part: DOOR — NOT CLOSED (NLG) · airframe 31,045 hrs · 13,151 cycles

AFT T/O ECAM L/GEAR DOOR NOT CLOSED AMBER NOSE GEAR DOOR LIGHT ON. AS SPEED INCREASE LOUD NOISE AND VIBRATION FROM NOSE WHEEL AREA.

Part: RETRACT MECH — MALFUNCTIONED (LT MLG)

98-297 - LAND GEAR WOULD NOT RETRACT AFT T/O RETURN TO MEM. FOUND LEFT GEAR TRUCK LEVEL CYLINDER CHARGE IND BUTTON POPPED 285862. RESERVICED PITCH DAMPER PER A310 AMM 12-12-32. PERF NORM EXTENSION/RETRACTION PER A310 AMM 32-31-00 OPS CK NORM.

Part: PITCH DAMPER — MALFUNCTION (LANDING GEAR)

DURING CLIMBOUT, LANDING GEAR WOULD NOT RETRACT WITH SYSTEM 1 OR SYSTEM 2. RETURNED TO YMX. REPLACED PITCH DAMPER DUE TO FLUID LEAK, AS PER M/M 32-11-15, CONFIG 01, P 401 AND SERVICED AND CHARGED AS PER M/M 12-12-32, P 24.

Part: CONNECTOR — WATER CONTAM (LT TE FLAP VANE)

DURING FLAP RETRACTION ECAM WARNING FLAPS VANE JAM, FLAP RETRACTION LIMITED. RESET BOTH SFCC'S HAD FAULTS ON LEFT O/B VANE INSPECTED ALL VANES FOR SECURITY, NO DEFECTS. FOUND H20 IN CANNON PLUG OF LT O/B VANE, CLEANED. CYCLED FLAPS USING GREEN PUMPS AND NR 1 ENG, CKD GOOD BOTH TIMES.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

DEPARTING DFW, FLAPS WOULD NOT RETRACT PART APPROX 2 TO 3 DEGREES. BOTH SYSTEM 1 AND 2 FAULT LIGHTS ILLUMINATED. RETURNED TO DFW AND FLAPS EXTENDED NORMALLY, SYS 1 AND 2 FAULT LIGHTS EXTINGUISHED AS SOON AS FLAPS EXTENED. REMOVED AND REPLACED FLAP VANE JAME BUFFER AND VERIFIED ADJ ON VETECTOR IAW MM 27-56-15. OPS FLAPS DOWN AND UP/STOWED POSITIONS SEVERAL TIMES ALL CHECKED GOOD.