N716FD

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,053 hrs · 35,495 cycles

DURING SERVICE CHECK, FOUND COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS, TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW MM 33-51-14-04-09. OP'S CHECKED SERVICEABLE.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG DOOR) · airframe 36,903 hrs · 35,415 cycles

AFTER TAKEOFF AND DURING GEAR RETRACTION, AN AMBER NOSE DOOR LIGHT ILLUMINATED ON FORWARD PANEL AND OVERHEAD PANEL. LIGHTS WENT OUT ON TAXI IN. TROUBLESHOT IAW TSM 32-30-00 FIG 102. INSPECTED SEQUENCE VALVE, NO DEFECTS NOTED. INSPECTED SWITCHES TO BOTH SYS 1 AND 2 FOR DEFECTS, NONE FOUND. RAN DOORS SEVERAL TIMES, NO DEFECTS, OPS AND ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: CYLINDER — FAILED (NLG DOOR) · airframe 36,904 hrs · 35,416 cycles

AFTER TAKE-OFF, DURING GEAR RETRACTION, AMBER LIGHT DOOR OPEN ON FORWARD PANEL AND UPPER PANEL, VIBRATIONS AFTER LEVEL-OFF AT FL330, AND LOWER ALTITUDES UNTIL LANDING GEAR WAS EXTENDED FOR LANDING, DOOR AMBER LIGHT CONTINUED ILLUMINATION DURING ENTIRE SEQUENCE, ALL QRH PROCEDURES APPLIED. R & I RT NOSE GEAR DOOR ACTUATING CYLINDER IAW AMM REF 32-31-16-04. PERFORMED ADJUSTMENT AND TEST IAW AMM 32-31-00-05. NO DEFECTS NOTED. ALL HYD FLUID LEVELS CHECKED GOOD.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 36,545 hrs · 35,159 cycles

UPON REMOVAL OF SKIRT ANGLE ON NR 2 PYLON INBD SIDE, 2 EA DOUBLE DRILLED HOLES, 1 HOLE WITHIN .1 OF ANOTHER HOLE. REPAIRED HOLES IAW TD 70548824/012/2011, ISSUE A.

Part: ROLLER TRACK — CORRODED (CARGO BAY) · airframe 36,545 hrs · 35,159 cycles

L1 ROLLER TRAY IN FWD CARGO COMPT BETWEEN FRAMES 29 AND 30 HAS 2 EA AREAS OF CORROSION ON OTBD FLANGE BLENDED CORROSION IAW SRM 517-74-10 AND FOUND CORROSION TO BE OUT OF LIMITS IAW 53-10-15, PG 108. REPAIR ROLLER TRACK IAW SRM 53-10-15, FIG 202.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 36,545 hrs · 35,159 cycles

FLUSH REPAIR LOCATED ON LT WING CENTER FLAP UPPER T/E SKIN BETWEEN RIBS 22 TO 24 & AFT OF REAR SPAR IS NOT A VALID REPAIR. REMOVED FLUSH REPAIR AND REPAIRED SKIN WITH AN EXTERNAL DOUBLER PER EA 6-5750-145623.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 36,545 hrs · 35,159 cycles

RT HORIZONTAL STAB L/E PANEL 341CB HAS SEVERAL SMALL GOUGES AND NICKS ON L/E FROM INBD TO OTBD END. SMOOTHED AND BLENDED 4 AREAS OF L/E AREA. NR 1 AND 4 ARE WITHIN LIMITS AND NR 2 AND 3 ARE OUT OF LIMITS IAW SRM 51-10-00 TABLE 1. FABRICATED AND INSTALLED REPAIR PARTS IN NR 2 AND #3 AREAS IAW A300-600 SRM 55-12-12 FIG 203. REPROTECTED ALL AREAS IAW SRM 51-75-10.

Part: ROLLER TRACK — CORRODED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

CARGO ROLLER TRAY IN FWD CARGO COMPT. LT CENTER CORRODED AT FRAMES 23 AND 18 AFTER CORROSION REMOVAL, ROLLER TRAY FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, PG 108. REPAIRED ROLLER TRAY IAW SRM 53-10-15, FIG 202.

Part: SKIN — CORRODED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

8 SQ IN OF FUSELAGE INTERNAL SKIN CORROSION ON FWD CARGO AFT BILGE BETWEEN STR 55 AND STR 54R FWD OF FR 38.2. REMOVED CORROSION IAW SRM 51-74-10. FOUND AREA OUT OF LIMITS IAW SRM 53-14-12 FIG. 101. REPAIRED MANHOLE INTEGRAL PLATE IAW SRM 53-14-12 FIG. 208 WITH 5 EA. INTERNAL DOUBLERS AND 1 EA. EXTERNAL DOUBLER.

Part: ROLLER TRACK — CORRODED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

ROLLER TRAY 2L INBD FLANGE HAS CORROSION BETWEEN FRAMES 34 AND 35 IN FWD CARGO COMPT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF ROLLER TRACK IN FWD LOWER CARGO COMPARTMENT, ROLLER TRAY 2 LT BETWEEN FR 34 AND FR 35 AND INSTALLED CARGO COMPARTMENT ROLLER TRACK SPLICE REPAIR IAW SRM 53-10-15, FIG 202,PAGE 209/210.

Part: ROLLER TRACK — CORRODED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

ROLLER TRACK 2R BETWEEN FRAMES 29 AND 30 CORRODED IN FWD CARGO COMPT. AFTER REMOVAL OF LEVEL 1 CORROSION, TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 PG 107. REPAIRED ROLLER TRACK IAW SRM 53-10-15 FIG 203. REPROTECTED IAW A300-600 SRM 51-75-10.

Part: ROLLER TRACK — DAMAGED (CARGO BAY) · airframe 36,545 hrs · 35,159 cycles

FWD CARGO COMPT. ROLLER TRAY R1 HAS DOUBLE DRILLED HOLE BETWEEN FRAME 35 AND 36 REMOVED AND REPLACED ROLLER TRACK SECTION IAW SRM 53-10-15 PG 211/212.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,545 hrs · 35,159 cycles

UPON REMOVAL OF ROLLER TRAY ON N01207 IN FWD CARGO COMPT BETWEEN FR 35 AND 36, FOUND CORROSION ON TOP OF FLOOR SUPPORT AT FRAME 35. REPAIRED FLOOR SUPPORT AT FRAME 35 IAW SRM 53-10-15, FIG 207.

Part: FRAME — CORRODED (PRESS BLKHD) · airframe 36,545 hrs · 35,159 cycles

AFT PRESSURE BULKHEAD BOTTOM FWD SIDE AT FR 80/82 CIRCUMFERENTIAL STRAP CORRODED 7 IN LENGTH X 4 IN WIDTH BETWEEN STR 54R TO 56R. REMOVED CIRCUMFERENTIAL STRAP STRINGER 51R TO 54L IAW SRM 51-40-21. VERIFIED NO FURTHER CORROSION DAMAGE FOUND. INSTALLED NEW SECTION AND TWO EACH REPAIR DOUBLERS PER EA 6-5310-145608. REPROTECTED PER SRM 51- 75-10.

Part: ROLLER TRACK — MISREPAIRED (CARGO BAY) · airframe 36,545 hrs · 35,159 cycles

EXISTING ROLLER TRACK REPAIR HAS INCORRECT ANGLES SHAPE AND THICKNESS AND MS20470D6 RIVETS INSTALLED FROM BOTTOM SURFACE UP AND NO COUNTERSUNK RIVETS AT OUTER FLANGES AFT CARGO ROLLER TRACK LT NR 3 Y1470 BETWEEN FR 55 TO FR 56 EXISTING REPAIR REMOVED AND REPLACED 2 EA REPAIR ANGLES AND REMOVED AND REPLACED ALL RIVITS WITH CORRECT TYPE AND DIRECTION OF INSTALL PER A300-600 SRM 53-10-15 FIG 203 PAGES 207 TO 212.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

STRINGER 53L BETWEEN FRAMES 63 TO 64 EXISTING REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED EXISTING REPAIR SPLICE ON STRINGER 53LT BETWEEN FRAMES 63 TO 64 AND REMOVED AND REPLACED FWD STRINGER SECTION BETWEEN FRAME 62 TO 64 PER SRM 53-10-14 FIG 201 PAGES 203 TO 206.

Part: STRINGER — MISINSTALLED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

STRINGER 52L BETWEEN FRAMES 63 TO 64 REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED REPAIR SPLICE ANGLE ON STRINGER 52L/H BETWEEN FRAMES 63 TO 64 PER A300-600 SRM 53-10-14 FIG 201 PAGES 203 TO 206.

Part: STRINGER SPLICE — FAILED (ZONE 100) · airframe 36,545 hrs · 35,159 cycles

STRINGER 44 RT SPLICE ANGLE BETWEEN FRAMES 38.2 TO 39 HAS INCORRECT THICKNESS INSTALLED REMOVED AND REPLACED STRINGER 44RH SPLICE ANGLE BETWEEN FRAME 38.2 TO 39 WITH CORRECT REPAIR MATERIAL PER A300-600 SRM 53-10-14 FIG 201 PAGES 203 TO 206

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 36,545 hrs · 35,159 cycles

PREVIOUS REPAIR LOCATED INCORRECTLY BETWEEN FRAMES 60 AND 61 OTBD SIDE AT SEAT TRACK 2R -Y450. REMOVED AND REPLACED SEAT TRACK 2R -Y450 FROM FRAME 58 TO 62 WITH NEW SECTION AND SPLICES PER A300-600 SRM 53-10-16 FIG 208 SHEET 1 PAGES 243 TO 248

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 36,545 hrs · 35,159 cycles

LT ELEVATOR UPPER SURFACE AT STA 253/ RIB NR 8 UPPER SKIN HAS A HOLE PUNCTURE APPROX 0.25 IN. LONG THROUGH INTO HONEYCOMB. REPAIRED LT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, PARA I, PAGES 248 THRU 252.

Part: ENGINE — FAILED (NR 2) · airframe 35,702 hrs · 34,698 cycles

NR 2 ENG CATASTROPHIC FAILURE. (DURING CRUISE, ECON, COST INDEX 55) MC1 U IAW POWERPLANT ENGINEER THIS ENGINE IS APPROVED FOR ENGINE CHANGE. NR 2 ENGINE CHANGED REF WC 64T0711-2. ITEM CLOSED.

Part: DETECTOR — FAILED (NR 1 NACELLE) · airframe 34,368 hrs · 33,948 cycles

ON CLIMBOUT IN HEAVY RAIN AT 3000 FT, NR 1 ENG FIRE LIGHT ILLUMINATED. C/W EMERGENCY PROCEDURES. LANDED 23L. LIGHT STAYED ON AFTER LANDING. FIRE DEPT CONFIRMED VISUALLY AND INFRARED NO FIRE. TOWED IN. DISCONNECTED CONNECTOR D1909VC AT ENGINE NR 1 PYLON. PIN C AND U OF 11WD CTL UNIT CONNECTOR WENT COMPLETE OPEN. DISCONNECTED PINS A AND C FROM 27WD SENSING LOOP B NACELLE. FOUND THAT THE STUD IS BROKEN AND WHEN WIGGLED WOULD SHORT TO GROUND. NEED NEW NACELLE LOOP B. REPLACED NR 1 ENGINE LOOP B (27WD) IAW MM 26-12-12-4 UP TO STEP G (LOOP TEST). FOWARD CLAMP WAS FOUND LOOSE. REPOSITIONED CLAMP AND TIGHTENED. SUSPECT THAT CLAMP WAS LEAKING HOT AIR ONTO "A" FIRE LOOP. ACFT OK FOR SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 NACELLE) · airframe 34,094 hrs · 33,796 cycles

DURING CRUISE FLT AT 340 HAD FIRE WARNING ON NR1 ENGINE, COMPLIED W/RED ECAMS. FIRE WARNING CEASED AFTER DISCHARGING NR 1 AGENT. 37 MINUTES OF WIND MILLING AT 0 PSI. CHECKED LOOP RESISTANCE AND INSULATION AND WIRING REF TSM 26-12-00 NO FAULTS FOUND. CLEANED LOOP CONNECTORS AND REINSTALLED. LEAK CHECKED STARTER DUCT USING APU AIR NO LEAKS FOUND. FOIL WRAPPED REMAINING DUCT CLAMPS. RAN ENGINE AT CRUISE SETTING (1.33 EPR) FOR 30 MIN. NO FIRE WARNINGS AND NAC. TEMP NORMAL 95 SAME AS NR 2 ENGINE. RECHECKED DUCTS AND FOUND 1 CLAMP ON ENGINE BLEED VALVE WITH BLOWN FOIL. REWRAPPED CLAMP AND RAN ENGINE AGAIN PER JRH.

Part: FITTING — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "N". STARTED REAMING HOLE "N" TO 0.816. COLD WORKED HOLE "N " USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "N" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-5710-123689.

Part: RIB — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "G". STARTED REAMING HOLE "G" TO 0.816. COLD WORKED HOLE "G" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "G" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-5710-123689.

Part: RIB — CRACKED (ZONE 600) · airframe 33,428 hrs · 33,404 cycles

RIGHT WING RIB 5 AT HOLE "N" HAS A CRACK INDICATION. STARTED REAMING HOLE TO 0.816. COLD WORKED HOLE USING STDN 26-2-N TOOLING. FINAL REAMED HOLE TO 0.844. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER R570.40017.212 IAW EO 6-5710-123688.

Part: FITTING — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING PICK-UP FITTING AT THE AFT SPAR, RIB 4 HAS A CRACK INDICATION AT HOLE "E". STARTED REAMING HOLE "E" TO 0.723. COLD WORKED HOLE "E" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "E" TO 0.750. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-5710-123690.

Part: RIB — CRACKED (RT WING) · airframe 33,428 hrs · 33,404 cycles

RIGHT WING RIB 5 AT HOLE "J" HAS A CRACK INDICATION. STARTED REAMING HOLE TO 0.816. COLD WORKED HOLE "J" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE TO 0.844. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER R570.40017.206 IAW EO 6-5710-123688.

Part: RIB — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "N". STARTED REAMING HOLE "N" TO 0.816. COLD WORKED HOLE "N" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "N" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-5710-123689.

Part: FITTING — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING PICK UP FITTING AT THE AFT SPAR RIB 4 HAS A CRACK INDICATION AT HOLE "A". STARTED REAMING HOLE "A" TO 0.973. COLD WORKED HOLE "A" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "A " TO 1.00. ROTOPROBE INSPECTED HOLE IAW NTM 51-10- 01. INSTALLED NEW FASTENER IAW FEDEX EO 6-5710-123690; "WINGS, AD 99-16-01-EO 6-5710-7-5005-LT WING R/S; MLG FWD PICK-UP FITTING BOLT HOLE "A"; "C" AND "E".

Part: FITTING — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING PICK-UP FITTING AT THE AFT SPAR; RIB 4 HAS A CRACK INDICATION AT HOLE "C". STARTED REAMING HOLE "C " TO 0.666. COLD WORKED HOLE "C" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "C" TO 0.687. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW FEDEX EO 6-5710-123690.

Part: RIB — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "L". STARTED REAMING HOLE "L" TO 0.816. COLD WORKED HOLE "L" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "L" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10- 01. INSTALLED NEW FASTENER IAW EO 6-5710-123689.

Part: RIB — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "K". STARTED REAMING HOLE "K" TO 0.816. COLD WORKED HOLE "K". FINAL REAMED HOLE "K" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NEW FASTENER IAW EO 6-5710-123689.

Part: SKIN — CRACKED (ZONE 600) · airframe 33,428 hrs · 33,404 cycles

RIGHT WING OUTBD FLAP; INBD SECTION; UPPER SKIN IS GOUGED. REMOVED DAMAGED SKIN. FABRICATED & INSTALLED NEW SKIN IAW EA 6-5750-123685 & SRM 51-40-21 PG 13. ALODINED PRIMED & PAINTED IAW SRM 57-21-10; PARA 2-B & 51-10-13. PART MARKED SKIN IAW GMM 7-0-1001.

Part: SUPPORT FITTING — CRACKED (SEAT TRACK) · airframe 33,428 hrs · 33,404 cycles

SEAT TRACK SUPPORT CRACKED, LOCATED BETWEEN FR 49 AND FR 50, OTBD OF NR 4 LT GANTRY. FABRICATED SEAT TRACK FITTING SUPPORT IAW E.A. 6-5321-123539. SEAT TRACK FITTING INSTALLED IAW SRM 51-40-00; PARA 3.

Part: FITTING — CRACKED (ZONE 200) · airframe 33,428 hrs · 33,404 cycles

CRACKED FITTING UNDER FWD. CARGO FLOOR, FR 38.2 RBL 8 REMOVED & REPLACED FITTING UNDER THE FLOOR AT FRAME 38.2; RBL 8 IAW SRM 51-40-21; PG 7.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 33,428 hrs · 33,404 cycles

NR 1 PYLON SKIN PNL. CRACKED AT FASTENER, AT RIB 8 O/B SIDE. REPAIRED CRACKED SKIN IAW AIRBUS REPAIR DWG R54610124.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,428 hrs · 33,404 cycles

EXTERNAL FUSELAGE HAS STATIC DISCHARGE AT FRAME 10, LEFT SIDE APPROX 18 INCH ABOVE THE WINDOW. BLENDED AREA IAW SRM 53-10-12 FIG. 220 SHT 1 REMOVED DAMAGE IAW SRM 53-11-12. FABRICATED FILLER AND DOUBLER IAW SRM 53-11-12 FIG. 202 SHT 1. ALODINED IAW SRM 51-21-10 PG2. PRIMED IAW SRM 51-23-10. INSTALLED FILLER AND DOUBLER IAW SRM 53-11-12 FIG. 202 SHT 1.

Part: STIFFENER — GOUGED (LT WING) · airframe 33,428 hrs · 33,404 cycles

LEFT WING VERTICAL STIFFENER LOWER AREA IS GOUGED AFT OF THE FALSE SPAR AND RIB 6A. REMOVED DAMAGED STIFFENER, LOCATED AND DRILLED NEW STIFFENER IAW DWG A57244644. INSTALLED NEW STIFFENER IAW SRM 51-40-21, PARA 7.

Part: SKIN — BULGED (RT WING) · airframe 33,428 hrs · 33,404 cycles

RIGHT WING LOWER SKIN, LOWER SURFACE OTBD OF RIB 11 (OTBD OF THE FLAP TRACK) 19 INCHES FWD OF THE REAR SPAR, THE SKIN IS BULGING, FWD SIDE OF THE FASTENERS. REMOVED CORROSION. FLAP PEENED AREA. ALODINED, PRIMED AND PAINTED IAW EA 6-5730-123533. REMOVED AND REPLACED FASTENERS IAW SRM 51-41-21; PG 7.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 33,428 hrs · 33,404 cycles

LT WING L/E LOWER PANEL NR 513AB SUPPORT CRACKED, LT WING L/E LOWER PANEL NR 513AB SUPPORT FWD CRACK STOPPED ON EXISTING HOLE; REPAIRED AREA IAW A300-600 SRM 53-15-63 PG 201.

Part: SKIN — CRACKED (ZONE 600) · airframe 33,428 hrs · 33,404 cycles

RT WING LOWER LEADING EDGE CRACKED AT CUTOUT FOR PANEL 613AB, CRACK EXTENDS AT BOTH ENDS OF FASTENER HOLE. DRILLED CRACK STOP HOLE IAW SRM 53-15-63 PG 202 STEP 2. FABRICATED DOUBLERS IAW SRM 53-15-63 PG 209-210. ALODINED, PRIMED, AND PAINTED IAW AMM 51-23-10-0. INSTALLED DOUBLERS IAW SRM 53-15-63 PG 209-210.

Part: INTERCOSTAL — WORN (RT WING) · airframe 33,428 hrs · 33,404 cycles

RIGHT WING LOWER INTERCOSTAL ANGLE INBD OF AILERON WORN SEVERAL PLACES. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE IAW DWG A57244531 AND SRM 51-70-12 PG 1-8. LOCATED AND DRILLED IAW DWG A57244531. ALODINED AND PRIMED NEW ANGLE IAW SRM 51-21-10 PG 8 AND 11 AND 51-23-10. PART MARKED NEW ANGLE A5724453120000 IAW GMM 7-0-1000. INSTALLED NEW ANGLE IAW SRM 51-40-21 PARA 8.

Part: ANGLE — GOUGED (LT WING) · airframe 33,428 hrs · 33,404 cycles

LT WING AFT OF REAR FALSE SPAR APPROX RIB 6A AREA HAS VERTICAL WEB GOUGED AND DOUBLE DRILLED HOLES. REMOVED LOWER SKIN PANEL AND DAMAGED ANGLE REF SRM 51-40-21 PARA 6 AND 13. FABRICATED NEW ANGLE REF SRM 57-51-11 AND DWG A57244531. ALODINED REF SRM 51-21-10. PRIMED AND PAINTED REF SRM 51-23-10. PARTS MARKED REF GMM 7-0-1000. INSTALLED NEW ANGLE AND LOWER SKIN REF SRM 51-40-21 PARA 6, 7, AND 13.

Part: PANEL — CORRODED (LT WING) · airframe 33,428 hrs · 33,404 cycles

LT WING T/E PANEL NR 575DB HAS FRETTING CORROSION, WORN AREAS, AROUND FASTENER MATTING SURFACE AFT OF RIB 7A. REPAIRED LT WING T/E PANEL 575DB BY BONDING A PICTURE FRAME DOUBLER TO PANEL IAW EA 6-5750-123683 AND SRM 51-77-10. REMOVED AND REATTACHED PANEL TO ACFT IAW SRM 51-40-21 PARA 5.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 33,428 hrs · 33,404 cycles

CABIN FLOOR BOARD BROKEN IN 3 PIECES, BETWEEN FR 47 - 51, 4TH BOARD FROM LEFT. FABRICATED NEW FLOOR BOARD USING OLD BOARD AS TEMPLATE IAW FEDEX DWG SRZ 25- 005 REV G.

Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 33,428 hrs · 33,404 cycles

RT THS REAR SPAR UPPER TEE CAP UPPER SURFACE HAS CORROSION BETWEEN RIB 14 - 15. REMOVED CORROSION IAW A300-600 SRM 51-74-10. ORIG THICKNESS .080 IAW AIRBUS DWG A55177703. MAT REMAINING .054. FOUND AREA TO BE OUT OF LIMITS IAW A300-600 SRM 55-10-00 PG 106 TOOL: T8225T, REPAIRED AREA IAW A300-600 SRM 55-11-21 FIG 212.

Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 33,428 hrs · 33,404 cycles

R/H THS REAR SPAR UPPER TEE CAP HAS CORROSION AT RIB 3. REMOVED PANELS & NECESSARY SUB STRUCTURE TO FACILITATE MANTENANCE IAW SRM 51-40-21; ( RE-INSTALLED IAW SRM 51-40-21). REMOVED & RE-INSTALLED THE ELEVATOR PRESSURE & RETURN LINES & ELEVATOR CONTROL RODS TO FACILITATE MANTENANCE IAW AMM 27-31-23-4 & 20-23-12-0. FABRICARED & INSTALLED NEW TEE CAP PROFILE IAW DWG A55177703 & SRM 55-11-21; FIG 226; PAGES 377-384.

Part: SKIN — CRACKED (ZONE 600) · airframe 33,428 hrs · 33,404 cycles

RT INBD FLAP INBD UPPER SKIN NR A57960007000 IS CRACKED. FABRICATED NEW SKIN IAW EA 6-5750-123529 AND DWG A57960007. ALODINED AND PRIMED IAW SRM 51-21-10. INSTALLATION OF SKIN TO BE ACCOMPLISHED ON J/C NR 6-5750-7-5003 PT 1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,428 hrs · 33,404 cycles

MAIN CABIN, AT FRAME 48 AND GANTRY 4 RT, SEAT TRACK, "LINAGE FITTING" IS CRACKED, UNDER FLOOR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,428 hrs · 33,404 cycles

MAIN CABIN, AT FRAME 48 AND GANTRY 4 RT, SEAT TRACK, "LINAGE FITTING" IS CRACKED, (UNDER FLOOR) REMOVED SEAT TRACK SPLICES AND DAMAGED LINKAGE FITTING IAW A300-600 SRM 51-30-00. LOCATED AND DRILLED NEW LINKAGE FITTING IAW A300-600 SRM 51-30-40. INSTALLED NEW LINKAGE FITTING AND OLD SEAT TRACK SPLICES IAW A300-600 SRM 51-30-00 PART NR A5381206720000 PO NR 640729.3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,428 hrs · 33,404 cycles

MAIN CABIN, AT FRAME 49 AND GANTRY 4 LT, SEAT TRACK, "LINKAGE FITTING" IS CRACKED, UNDER FLOOR. REMOVED AND REPLACED THE SEAT TRACK LINK FITTING IAW A300-600 SRM 51-40-21, PARA 5, P/N A5381206720100, PO NR 640729.1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,428 hrs · 33,404 cycles

MAIN CABIN, AT FRAME 48 AND GANTRY 4 LT, SEAT TRACK, "LINKAGE FITTING" IS CRACKED, UNDER FLOOR. REMOVED AND REPLACED THE SEAT TRACK LINK FITTING IAW SRM 51-40-21, PARA 5.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 33,428 hrs · 33,404 cycles

THE BULKPIT FLOOR PANEL 161 BF IS PUNCTURED. REPAIRED PUNCTURE ON FLOOR PANEL 161 BF IN REF TO A300-600 SRM 53-10-20, STEP 10A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 33,428 hrs · 33,404 cycles

THE BULKPIT FLOOR PANEL 161 GF IS PUNCTURED.

Part: SMOKE DETECTOR — FAILED (ZONE 100) · airframe 33,250 hrs · 33,299 cycles

AV SMOKE ALARM ON TAXI OUT. ACFT SUFFERED RAIN INGRESSION, DRIED OUT COURIER AREA AND AVIONICS BAY AREA. VERIFIED THAT FLOOR AND DRIP PAN DRAINS ARE CLEAR AND DRAIN NORMALLY. REMOVED AND REPLACED AVIONICS DUCT SMOKE DETECTOR 13WA PER AMM 26-15-12-4. PERFORMED SATISFACTORY OPS CHECK PER AMM 26-15-00. OK FOR CONTINUED SERVICE.

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 33,250 hrs · 33,299 cycles

AV SMOKE ALARM ON TAXI OUT. ACFT SUFFERED RAIN INGRESSION DRIED OUT COURIER AREA AND AVIONICS BAY AREA. VERIFIED THAT FLOOR AND DRIP PAN DRAINS ARE CLEAR AND DRAIN NORMALLY. REMOVED AND REPLACED AVIONICS DUCT SMOKE DETECTOR 13WA PER AMM 26-15-12-4. PERFORMED SATISFACTORY, OPS CHECK PER AMM 26-15-00.

Part: COMPUTER — FAILED (CARGO DOOR) · airframe 32,454 hrs · 32,847 cycles

ECAM WARNING OF MAIN DECK DOOR UNLOCKED TWICE CLIMBING THROUGH FL240 AND WENT OUT DESCENDING THROUGH 14000, ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01. NO PRESSURIZATION PROBLEMS NOTED. TSI OPENED FOR T/S. LT ECAM SHOWED CARGO DOOR OPEN WARNING, BUT THE RH ECAM DR PAGE SHOWED CLOSED AND LOCKED. PERFORMED FWC BITE DISPLAY IAW A300 TSM 31-50-00. FOUND FWC1 WITH CURRENT FAULTS. R&R FWC1 IAW A300 AMM

Part: RUDDER — BINDING · airframe 31,016 hrs · 32,088 cycles

ON TAKEOFF ROLL, TOGA SELECTED PUSHED RUDDER FOR FREEDOM OF MOVEMENT AND THEY WOULD NOT MOVE LEFT AND RIGHT VERY STIFF, (FELT LIKE TRYING TO OVERRIDE THE AUTOPILOT ON AN AUTOLAND AUTO PILOT ON WITH ROLLOUT ON LANDING AND TRYING TO USE MANUAL RUDDER WITH A/P ON. ABORTED TAKEOFF. I/W RAN BOTH ENGINES PER JRH, TAXI A/C WHILE MOVING RUDDER PEDALS, FOUND NO BINDING. PERFORMED ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING ADJUSTMENT TEST ACCORDING TO AMM 27-23-00-5 WITH THE EXCEPTION OF THE TEST OF THE VARIABLE STOP UNIT CYLINDER EXTENSION AND RUDDER DEFLECTION, PG 519 STEP D. ALL TESTS PASS AND INDICATIONS ARE NORMAL.

Part: WIRE HARNESS — FAULTED (FUEL PUMP) · airframe 30,997 hrs · 32,081 cycles

RT INNER TANK NR 2 PUMP FAULTED DURING TAXI OUT. (SUPP DATE: 15 MARCH 2007) RAN COMPLETE NEW WIRE RUN FROM 50QA PINS A,B,&C TO 62VC PINS H,G & F PER WDM 28-21-10 PG 2. ALL LT INNER BOOST PUMPS ADJUSTMENT /TESTS ARE NORMAL. IAW MM 28-21-12-5 A/C OK FOR SERVICE.

Part: FIRE LOOP — DAMAGED (NR 1 ENGINE) · airframe 30,030 hrs · 31,541 cycles

CLIMBING THROUGH 16000 FT GOT RED ECAM "ENG 1 FIRE" FOLLOWED ECAM AND QRH. NR 1 AGENT WOULD NOT DISCHARGE, USED NR 2. FIRE WARNING LIGHT STAYED ON THROUGHOUT FLT. MADE EMERGENCY RETURN. UPON ARRIVING AT AIRCRAFT, FIRE WARNING STILL ACTIVE, HANDLE LIGHTS ILLUMINATED AND A AND B LOOP FAULTED. FIRE DETECTOR CONTROL BOX SHOWED FAULTS ON BOTH LOOP A AND B. REMOVED AND REPLACED NR 1 AND NR 2 FIRE BOTTLES ON NR 1 ENG PER A300-600 MM 26-21-15-4. REPLACED SQUIBS ON EACH BOTTLE PER A300-600 MM 26-21-13-4, CONNECTORS OFF ON SQUIBS AND PSI SWITCHES FOR BOTH BOTTLES, ALSO REQUIRE SAFTEY WIRE. REMOVED/REPLACED NR 1 ENG FIRE DETECT CONTROL UNIT PRECAUTIONARY PER MM 26-12-11-4 OPS CHECK NORMAL.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 28,846 hrs · 30,888 cycles

SHORTLY AFTER T/O NR 1 ENGINE HP BLEED VALVE FAULTED. TEMP ON ECAM BLEED PAGE SHOWED 255-260 DEGREES. WITHIN 30 SECONDS REGULAR BLEED VALVE FAULTED. REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE, ALL CHECKS NORMAL PER MM 36-11-16-4-03. ACCOMPLISHED NR 1 ENGINE RUN PER A300 JRH, NO FAULTS NOTED.

Part: ROD — BROKEN (NLG) · airframe 28,797 hrs · 30,861 cycles

AFTER T/O, LANDING GEAR WOULD NOT RETRACT. SELECTED SYS 2 ON POSITION SELECTOR AND ATTEMPTED TO RETRACT. GEAR WOULD NOT RETRACT, NEXT PITCH TRIM 1&2 TRIPPED OFF AND WOULD NOT RESET. AUTOTHROTTLES 1&2 TRIPPED OFF AND WOULD NOT RESET. CREW DECLARED EMERG, RETURNED. ALL ELEC/HYD INDICATIONS WERE NORMAL. NO C/B`S OPEN. AFTER LANDING, ALL SWITCHES WOULD RESET. SYS ACTED LIKE A/C NEVER LEFT GROUND. CHECKED PROX BOX FOUND SN INDICATION FOR NOSE SHOCK ABSORBER. FOUND BEARING WORN ON NOSE SHOCK EXTENSION TARGET ARM. REPLACED BROKEN ROD ASSY ON CONNECTING ARM FOR NOSE GEAR PROX DETECTOR SWITCH ASSY IAW A300AMM 32-00-00. GEAR SWING OPS CHECK NORMAL.

Part: ROD — BROKEN (NLG) · airframe 28,801 hrs · 30,864 cycles

AFTER T/O LANDING GEAR WOULD NOT RETRACT. SELECTED SYSTEM 2 ON POSITION SELECTOR AND ATTEMPTED TO RETRACT. GEAR WOULD NOT RETRACT. NEXT PITCH TRIM 1&2 TRIPPED OFF AND WOULD NOT RESET. AUTOTHROTTLES 1&2 TRIPPED OFF AND WOULD NOT RESET. CREW DECLARED EMERGENCY, RETURNED AND LANDED. FOUND BEARING WORN ON NOSE SHOCK EXTENSION TARGET ARM. REPLACED BROKEN ROD ASSY ON CONNECTING ARM FOR NOSE GEAR PROX DETECTOR SWITCH ASSY IAW A300AMM 32-00-00. GEAR SWING OPS CHECK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 28,092 hrs · 30,457 cycles

MADE T/O WITH T/O CONFIG TEST SW SHOWING MAIN DECK DOOR NOT CLOSED PER MEL MX HAD VERIFIED ALL DOORS CLOSED & LOCKED AND DOORS ON ECAM WERE INDICATING CLOSED AND LOCKED. ON CLIMBOUT AT APPROX 4 PSI & 13,000 FT MSL MAIN CARGO DECK LIGHT ON ECAM WENT AMBER. NO CHANGE IN PRESSURE AND RIGHT ECAM DOOR PAGE VERIFIED AMBER LIGHT MAIN CARGO DOOR. EMERGENCY RETURN TO KOAK AND ECAM LIGHT WENT OUT ON LANDING. LANDING WEIGHT 327.3 DESCENT RATE= 220FT/MIN. HEAVY LANDING INSPECTION / WRI 05-50/2169. ALL SYSTEMS NORMAL.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 28,082 hrs · 30,451 cycles

RIGHT HAND WING INBOARD FLAP TOP SKIN COMPLY WITH EA 6-5750-85635. REMOVED AND REINSTALLED SKIN WITH REPLACEMENT FASTENERS PER SB 300-57-6098 FIG 3 SHEET 2, IAW FEDEX EA 6-5750-85635 REV-A AND DRAWING A579600005.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 28,092 hrs · 30,456 cycles

AFTER TAKEOFF MAIN DECK CARGO DOOR OPEN CAME ON. CABIN ALT WAS CLIMBING ALSO. DEFERRED PER MEL 52-71-01. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C. MAIN DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOP. MAIN PERFORMED OPERATIONAL ADJUSTMENT, AND TEST PROCEDURES IAW A300-600 AMM 52-71-00-5, FOUND SWITCH 49WS OUT OF RIG, ADJUSTED, AND VERIFIED SWITCH ADJUSTMENT IAW A300-600 AMM 52-71-11-5 SUPP AMM 52-71-11-5, DOOR INDICATION OPERATIONAL CHECKS NORMAL.

Part: PLATE — CRACKED (ZONE 600) · airframe 28,082 hrs · 30,451 cycles

RIGHT WING T/E INBOARD FLAP UPPER SURFACE INBOARD END FLAP TRACK ROLLER CHAFING PLATE IS CRACKED. REMOVED AND REPLACED CHAFING PLATE IAW DWG A579-60005.

Part: FITTING — CRACKED (ZONE 800) · airframe 28,082 hrs · 30,451 cycles

WHILE COMPLYING WITH HIDDEN DAMAGE INSPECTION FOR S00012, FOUND CORNER FITTING (ITEM 30 FIG 2 SHEET 1 SRM 52-31-00 PG 12) CRACKED WITH PREVIOUS REPAIR, AND CRACK HAS MIGRATED 1 INCH PAST STOP DRILL. REMOVED AND REPLACED CORNER FITTING IAW A300-600 SRM 51-72-10.

Part: SKIN — CRACKED (ZONE 600) · airframe 28,082 hrs · 30,451 cycles

AFTER REMOVAL OF CHAFF PLATE ON RIGHT I/B FLAP, DID HIDDEN DAMAGE INSP FOR N00064, AND FOUND I/B FLAP TOP SKIN HAS 2 EA CRACKS. REPLACED SKIN IAW DWG A57960007 AND EA 6-5750-85635.

Part: RIB — CRACKED (ZONE 600) · airframe 28,082 hrs · 30,451 cycles

AFTER REMOVAL OF I/B FLAP TOP SKIN, PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND NR 2 AIRFOIL RIB AFT SECTION HAS CRACKED APPROX 8.5 INCHES LONG AND NR 3 RIB ON TOP SIDE ANGLE SUPPORT STRUCTURE HAS CRACKED APPROX 2.5 INCHES LONG AND 2 EA STIFFENERS WITH CRACKS ON CORNER WEB AS MARKED. REMOVED AND REPLACED RIB 25A. FABRICATED 2 EA BRACKETS P/N A57960114-209 & A57960114-221. REMOVED AND REPLACED 2 EA BRACKETS IAW DWG A57960114, A57960005 AND EA 6-5750- 85635.

Part: PLATE — DENTED (ZONE 800) · airframe 28,082 hrs · 30,451 cycles

POST FLT WALKAROUND FOUND DENT ON LOWER FWD CORNER OF LOWER FWD CARGO DOOR. DENT IS O/B OF DOOR SEAL. DENT MEASURES 2.75 INCHES LONG AND .75 INCH DEEP. TERMINATING ACTION ACCOMPLISHED FOR EA 6-5230-85502 AT 28,081:53 H 30,451 C. REMOVED AND REPLACED CORNER PLATE OF FWD CARGO, LOWER FWD CORNER. COMPLIED WITH FED EX EA 6-5230-85502 PT3.

Part: SLAT TRACK — WORN (ZONE 600) · airframe 28,082 hrs · 30,451 cycles

M-TYPE-MOD 716-27-80-0264, NR 8 SLAT TRACK HAS SIDE ROLLER WEAR SPOTS. BLENDED AND POLISHED TRACK ROLLER WEAR SPOTS FOUND ONE AREA OUT OF ALLOWABLE DAMAGE LIMITS IAW A-300 SRM 57-40-00 3.A.(3)(D). THE TRACK MAYBE RETURNED TO SERVICE PROVIDED THE AREA IS INSPECTED FOR FURTHER WEAR AT EVERY C-CHECK IAW A300 SRM 57-40 00 3.A.(3)(D). REMOVED AND REPLACED NR 8 RIGHT WING SLAT TRACK IAW A300 -600 AMM 27-80-14-4. REMOVED AND REPLACED NR 8 RIGHT SLAT TRACK ECCENTRIC BOLT IAW A300-600 AMM 27-80-14-4. OPS CHECK GOOD.

Part: BEAM — CRACKED (ZONE 100) · airframe 28,082 hrs · 30,451 cycles

LOWER FLANGE UPPER SURFACE OF LONGITUDINAL BEAM 5 LT AT FRAME 51A HAS A .5 INCH LONG CRACK. VERIFIED BY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND DOUBLE FLUSH PLUGGED HOLE PER EO 6-5310-7-5010 PT1 SECTION C7.

Part: BEAM — WORN (ZONE 500) · airframe 28,082 hrs · 30,451 cycles

LEFT WING NR 2 FLAP TRACK BEAM OUTBOARD SIDE ROLLER PATH HAS THREE WEAR MARKS. REF FED EX EA 6-5720-85940, LT WING NR 2 FLAP TRACK BEAM O/B 3 EA AREAS FOUND TO BE ACCEPTABLE AS IS TO CONTINUE SERVICE, AND TO BE CHECKED AT NEXT C-CHECK.

Part: RIB — CORRODED (ZONE 300) · airframe 28,082 hrs · 30,451 cycles

LT HORIZONTAL STAB T/E, JUST O/B OF RIB 3, 1 EA AREA OF CORROSION ON WEB ATTACH UPPER FLANGE LOWER SURFACE. REMOVED CORROSION PER A300600 SRM 51-74-10, MATERIAL LOSS OUT OF LIMITS PER A300600 SRM 55-10-00. FABRICATED AND INSTALLED REPAIR ANGLE IAW A300600 SRM 55-11-21 FIG 224.

Part: BEAM — CRACKED (ZONE 100) · airframe 28,082 hrs · 30,451 cycles

LOWER FLANGE UPPER SURFACE OF LONGITUDINAL BEAM 5 LT AT FRAME 52A HAS A .5 INCH LONG CRACK, VERIFIED BY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND DOUBLE FLUSH PLUGGED HOLE PER EO 6-5310-7-5010 SECTION C8.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 28,082 hrs · 30,451 cycles

AFT CARGO DOOR AFT FRAME UPPER SIDE AFTER REMOVAL OF UPPER DOOR SILL SECTION TO RECTIFY N00021, FOUND 1 AREA OF CORROSION ON AFT FRAME REAR FACE SURFACE SURROUNDING NUT PLATE. REMOVED CORROSION IAW A300-600 SRM 51-74-10 AND REPAIRED AFT CARGO DOOR AFT FRAME UPPER SIDE IAW A300-600 SRM 53-17-13 FIG 201A, REF EA 6-5310-85605.

Part: SKIN — DENTED (CARGO DOOR) · airframe 28,082 hrs · 30,451 cycles

POST FLT WALK AROUND FOUND DENT ON LOWER FWD CORNER OF LOWER FWD CARGO DOOR. DENT IS O/B OF DOOR SEAL. DENT MEASURES 2.75 INCH LONG AND .75 INCH DEEP. TERMINATING ACTION ACCOMPLISHED FOR EA 6-5230-85502 AT 28,081:53 H 30,451 C. REMOVED AND REPLACED CORNER PLATE OF FWD CARGO, LOWER FWD CORNER. COMPLIED WITH FED EX EA 6-5230-85502 PT3.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 27,670 hrs · 30,202 cycles

BLEED VALVE 1 FAULTED AFTER TAKEOFF. NO RESET, RAN NR 1 ENG AT THE GATE. NO FAULTS NOTED. RAN ENGS AT T/O POWER FOR 5 MIN. NO FAULTS NOTED. INTERROGATED PNEU SYST CONTROLLERS. NO FAULTS STORE IN MEMORY FOR ANY FLIGHT LEG, STILL T/S. TALKED TO MOCC. SINCE THERE WAS NO FAULTS STORED, AGREED TO REMOVE AND REPLACE THE CONTROLLERS AS PRECAUTIONARY. RAN ENG AT THE GATE, PERFORMED VALVE SWITCH OVER FROM HIGH STAGE TO LOW STAGE. OPS CK GOOD. NO FAULT NOTED IAW A300 JRH.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 26,369 hrs · 29,437 cycles

JUST STARTING T/O ROLL GOT ECAM-AFT CARGO DOOR NOT CLOSED. REJECTED T/O LESS THAN 60 KNOTS. RIGHT ECAM SHOWED AFT CARGO DOOR CLOSED. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-30-03, CATEGORY: C EXPIRATION: 24OCT03 (MEL 52-30-03: AFT CARGO DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE) INOP. AFT CARGO DOOR VISUALLY CHECKED, CLOSED AND LOCKED. FACT 15OCT03 17:07 IAH R CHECKED DOOR OPS, CLEANED DOOR RELEASE HANDLE LATCH CAM ASSY, OPERATED DOOR SEVERAL TIMES AND OPERATION NORMAL, INDICATION SYSTEM CHECKS OK. ENT BY: 097974