N684FE

Part: NONE — DAMAGED (ZONE 700) · airframe 31,030 hrs · 17,544 cycles

UPON POST FLIGHT INSPECTION, FOUND #6 MLG TIRE BLOWN AND BEAD UNSEATED. STILL IN TACT AND ON WHEEL. NO DAMAGE. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: Z32-002-03 POS: 6 SRL: 25001 TAG NBR: 6485F1 ON MPN: Z32-002-03 CPN: 3211843 SRL: F3664 TAG NBR: 76G342 . FOUND PUNCTURE IN #6 MLG TIRE PICTURES UPLOADED. REMOVED AND INSTALLED SERVICEABLE TIRE REF AMM 32-41-11-04. OK FOR SERVICE. DUE TO TIRE BEING OFF BEAD, CHANGED #5 MLG TIRE ALSO.

Part: NONE — NONE (N/A) · airframe 30,973 hrs · 17,508 cycles

MAIN DECK FLOOR SEAT TRACK FOUND GOUGE AT FR60 9" Y953 ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W A300-600F SRM 53-10-16-201, PARA4, P203-208, FIG201

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

MAIN CARGO COMPT FLOOR PANEL #242ZH WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.

Part: FLOOR PANEL — DAMAGED (N/A) · airframe 30,973 hrs · 17,508 cycles

MAIN CARGO COMPT FLOOR PANEL #232VH WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201- 205, FIG201.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

MAIN CARGO COMPT FLOOR PANEL #232YG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

AFT CARGO COMPT FLOOR PANEL #151QF WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

FWD CARGO COMPT FLOOR PANEL #131RG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 30,973 hrs · 17,508 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 26AFT AREA(FWD) OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8 - ALI 575306-01 & A300-600F SRM 57-50-00-201, PARA4E, P217-220, FIG205 & 57-50-00-201, PARA4A, P201-205 FIG201

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 30,973 hrs · 17,508 cycles

1EA CRACK WAS FOUND AT LH WING CENTER FLAP 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO:6-5750-T0364642, TITLE:WING-FLIGHT SURFACES- LHCENTER FLAP, CRACK IN UPPER FLANGE OF RIB27 AT STRINGERS2.8 -ALI575306-01 & A300- 600F SRM 57-50-00-201, PARA4E, PAGE217-220, FIG205 & 57-50-00-201, PARA4A, PAGE201-205, FIG201.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 30,973 hrs · 17,508 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8 - ALI 575306-01 & A300-600F SRM 57-50-00-201, PARA4E, P217-220, FIG205 & 57-50-00-201, PARA4A, P201-205 FIG201

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 30,973 hrs · 17,508 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8 - ALI 575306-01 & A300-600F SRM 57-50-00-201, PARA4E, P217-220, FIG205 & 57-50-00-201, PARA4A, P201-205 FIG201

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 30,973 hrs · 17,508 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 26AFT AREA(REAR) OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8 - ALI 575306-01 & A300-600F SRM 57-50-00-201, PARA4E, P217-220, FIG205 & 57-50-00-201, PARA4A, P201-205 FIG201

Part: NONE — UNKNOWN (ZONE 500) · airframe 30,973 hrs · 17,508 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-15-63-201, PARA.5.A, PAGE 201-216, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS."MAJOR REPAIR"

Part: NONE — UNKNOWN (ZONE 500) · airframe 30,973 hrs · 17,508 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING O/B FLAP UPR SURFACE SKIN LOCATED AT RIB15 AND FRONT SPAR DATUM. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 57-50-00-201, PARA.H, PAGE 231-236, FIG 208, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY B REPAIR WITH SUPPLEMENTAL INSPECTION REQUIREMENTS, THE INITIAL THRESHOLD IS 51000 FC, REPETITIVE INTERVAL AND METHOD ARE TO BE DETERMINED BY OEM."MAJOR REPAIR"

Part: NONE — UNKNOWN (ZONE 300) · airframe 30,973 hrs · 17,508 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.19 AND NO.20 FASTENER COUNT FROM LOWER SIDE. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 55-41-12-201, PARA.13, PAGE 237-239, FIG 209, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY B REPAIR WITH SUPPLEMENTAL INSPECTION REQUIREMENTS, THE INITIAL THRESHOLD IS 30000FC, REPETITIVE INTERVAL AND METHOD ARE TO BE DETERMINED BY OEM REF TO SRI 55-41-12-2-001-00, PARA.3.A, PAGE.202-204, TABLE.202."FOR RECORD PURPOSES ONLY""MAJOR REPAIR"

Part: NONE — UNKNOWN (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR49 TO FR50 AND STR37L TO STR39L. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-15-12-201, PARA.5.D, PAGE 230-232, FIG.204, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS."FOR RECORD PURPOSES ONLY""MAJOR REPAIR"

Part: NONE — UNKNOWN (ZONE 600) · airframe 30,973 hrs · 17,508 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-15-63-201, PARA.5.A, PAGE 201-216, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS."MAJOR REPAIR"

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

AFT CARGO COMPT FLOOR PANEL #152QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

MAIN CARGO COMPT FLOOR PANEL #231EF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

FWD CARGO COMPT FLOOR PANEL #132LG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,973 hrs · 17,508 cycles

FWD CARGO COMPT FLOOR PANEL #132RG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

MAIN CARGO COMPT FLOOR PANEL #241GJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.

Part: NONE — WORN (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

N00303 FR54/FR54.2 RH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.

Part: NONE — WORN (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

N00302 FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.

Part: NONE — WORN (ZONE 200) · airframe 30,973 hrs · 17,508 cycles

N00301 FR38.2/FR40 RH NO.4 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.

Part: WEB — CRACKED (N/A) · airframe 30,973 hrs · 17,508 cycles

#2 PYLON O/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2

Part: WEB — CRACKED (N/A) · airframe 30,973 hrs · 17,508 cycles

#2 PYLON I/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2

Part: IDG — FAULTED (NR 2) · airframe 30,926 hrs · 17,488 cycles

REJECTED TAKEOFF AT APPROXIMATELY 50 KNOTS FOR GEN 2 FAULT. IDG2 FAULT LIGHT WAS FLICKERING PRIOR TO GEN2 FAULT. AFTER TAXIING CLEAR, GEN FAULT RESET PER ECAM/QRH, BUT IDG2 FAULT CONTINUED TO FLICKER FOR 10 MINUTES. MEL 17SEP21 00:38 MEM U RELEASED FOR SERVICE PER MEL : 24-11-01-B CATEGORY : B EXPIRATION : 19SEP21 "MEL 24-11-01-B: GEN 2 - INOP. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, AND APU ARE CHECKED ONCE EACH FLIGHT DAY." RH IDG DISCONNECTED AND PLACED ON MEL 24-11-01-B. FOUND RH IDG OIL LOW AND APPEARS TO HAVE BEEN LEAKING BEFORE DISCONNECTING. C/7286448 RH IDG DISCONNECTED AND PLACED ON MEL 24-11-01-B

Part: VALVE — LEAKING (HYD SYSTEM) · airframe 29,943 hrs · 16,890 cycles

PDIS 684 29-02 9691 04DEC20 DEN OPEN U LOGPAGES:3359248. AT FL350 1.25 HRS AFTER T/O, GREEN SYS HYD QTY WAS OBSERVED 2 NEEDLE WIDTHS ABOVE THE YELLOW ARC. AT 1.5 HRS NEEDLE WAS 1 NEEDLE WIDTH INTO YELLOW ARC. DIVERT TO KDEN. BLEED GRN SYS AND FOUND GRN SYS RESERVOIR DEPRESSURIZATION VALVE LEAKING. R & R SAME, REF MM 29-11-27-04. GROUND OPERATIONS AND LEAK CHECK GOOD AT THIS TIME, NO LEAKS NOTED.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 27,940 hrs · 15,624 cycles

RH AILERON UPPER SURFACE FROM O/B TO I/B 10 IN , FROM T/E TO L/E 11 IN FOUND BULGE REPAIRED THE RH AILERON UPPER SURFACE FROM O/B TO I/B 10 IN , FROM T/E TO L/E 11 IN BULGE PER A300-600F SRM57-61-11-101 FIG103 AND SRM51-77-12 PARA.4.D.(3) . EA # 6-5750- T0345986 P1 RAISED FOR RSC TRACKING. EA TITLE: WING - FLIGHT SURFACES - RH AILERON TRAILING EDGE WEDGE UPPER SURFACE BULGE REPAIR - RSC TRACKING . MAJOR REPAIR IAW FEDEX GMM 6-2-100

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 27,940 hrs · 15,624 cycles

LEFT WING O/B FLAP O/B TRAILING EDGE UPPER SKIN JUST UNDER THE STATIC DISCHARGER FITTING FOUND CORRODED. COMPLIED WITH EA 6-5750-T0345881 P1. MAJOR REPAIR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 27,940 hrs · 15,624 cycles

LEFT WING I/B FLAP RIB 3 UPPER FLANGE FOUND CRACK BETWEEN STRINGER 2.5 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0345820 PT1. REPAIRED THE LT WING I/B FLAP RIB. MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 27,940 hrs · 15,624 cycles

MAIN DECK FR57.3 STR 12-13R FRAME CHAFED REPAIRED THE MAIN DECK FR57.3 STR 12-13R FRAME PER SRM 53-10-13 FIG 202. THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 53-10-13-2-002-00. THE FIRST INSPECTION IS 42500FC AFTER REPAIR ENBODIMENT. SUBSEQUENT INSPECTIONS AT INTERVALS TBD. MAJOR REPAIR IAW GMM 6-2-100.

Part: WEB — CRACKED (FUSELAGE) · airframe 27,940 hrs · 15,624 cycles

MAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR 1EA WEB CRACKED REPAIRED THE MAIN DECK FR47 Y0~-Y450 UNDERFLOOR WEB PER SRM 53-15-15 FIG 201. THE REPAIR IS CATEGORY B AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 53-15-15-2-002-00. INSPECTION THRESHOLD IS 24000FC FROM REPAIR EMBODIMENT. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC. MAJOR REPAIR IAW GMM 6-2-100.

Part: RIB — CRACKED (LE SLAT) · airframe 27,749 hrs · 15,548 cycles

MDIS 684 57-40 7425 08JAN19 MEM FACT U NR 2 LT L/E SLAT FOUND NR 1 RIB CRACKED SHGN 08JAN19 11:15 MEM U REMOVED RIB IN REF TO SRM 51-40-20 REF. WRI 27-80/7424 FOR PICTURE AND PART ORDERED FOR REPAIR. MSN: 1951225 PART 09JAN19 11:14 MEM U IDENTIFIED PARTS MPN: 2219-0-040 QTY: 1 PART 09JAN19 11:14 MEM U ORDER PART MPN: 2219-0-040 QTY: 1 MSN: 1951254 SHGN 09JAN19 13:28 MEM U MATERIAL I.D. FOR DOUBLER REPAIR MATERIAL 2014T6X.050. MP3790134. REF EA 6-5750-T0344515 PT1 WING-LT NR 2 SLAT INBOARD CLOSING RIB-PERMANENT REPAIR OF WEB CRACK AT ACCESS HOLE. SHGN 09JAN19 22:11 MEM U INSATLLED REPAIR DOUBLER ON RIB REF EA 6-5750-T0344515 PT1. STEP 3. WING- LT NR 2 SLAT INBOARD CLOSING RIB- PERMANENT REPAIR OF WEB CRACK AT ACCESS HOLE. OK TO INSTALL CLOSING RIB ON NR 2 SLAT INBOARD SIDE. FACT 10JAN19 04:16 MEM U INSTALLED CLOSING RIB AND SEAL ON NR 2 LH LE SLAT IN REF TO EA 6-5750-T0344515 COMPLIED WITH EA 6-5750-T0344515 PERMANENT REPAIR OF CRACKED WEB.

Part: BOLT — SHEARED (WHEEL) · airframe 27,526 hrs · 15,425 cycles

#4 MLG WHEEL IS HAS 3 EA WHEEL HALF BOLTS BROKEN. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: Z32-002-03 POS: 4 SRL: U2911 TAG NBR:ON MPN: Z32-002-03 CPN: 3211843 SRL: 19894 TAG NBR: 8026E1. REF MM32_41_11_04, REMOVED & REPLACED #4 MLG TIRE. ACFT OK FOR SERVICE. PHOTOS ADDED TO WRI. THIS ITEM CLOSED/FACTED. REF SMP.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 25,750 hrs · 14,357 cycles

LEVEL CRUISE AT 340, RECEIVED A HYD QTY LOW FOLLOWED BY A LOW PRESSURE GREEN SYSTEM. LOW PRESSURE LIGHT GREEN SYSTEM REMAINED ILLUMINATED. COMPLIED WITH ECAM AND QRH. DECLARED AN EMERGENCY AND CONTINUED FLIGHT TO DESTINATION. GREEN QTY IN RED ZONE, INCREASED ON SHORT FINAL. FOUND A PIN HOLE IN THE B LINE. REMOVED THE LINE IAW MM 20-23-11-00, REPAIRED AND REINSTALLED. REMOVED AND REPLACED SERVO CONTROL PRESSURE SWITCH 19CB IAW AMM 27-14-18-04.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 25,202 hrs · 14,012 cycles

EXPERIENCED MULTIPLE AC BUSS 2 FAULTS DURING ARRIVAL. DECLARED EMERGENCY AND LANDED. CHANGED NR 2 AC BUSS GCU. OPS CHECKED NORMAL ON ENGINE RUN. OPS CEHCKED GPCU ALL TESTS OK. ACFT OK FOR SERVICE

Part: IDG — FAILED (NR 2) · airframe 25,157 hrs · 13,990 cycles

WHILE DESCENDING AT APPROX 17000 FT, ECAM SHOWED NR 2 IDG LOW OIL PRESSURE . DISCONECTED THE NR 2 IDG IAW ECAM AND REFERRED TO QRH PROCEDURE. FOUND IDG SIGHT GAGE TO INDICATE FULL OIL, ELECTRICAL CONNECTIONS SECURE AND DPI INDICATOR SET. REMOVED CONNECTORS, VISUALLY INSPECTED AND FOUND TO BE CLEAN, SECURE AND NORMAL. R & R NR 2 IDG, LEAK AND OPS CHECK NORMAL IAW AMM 24-11-11-04-01.

Part: GCU — FAILED (APU) · airframe 25,042 hrs · 13,926 cycles

DURING TAXI OUT, NR 1 GENERATOR FAULTED. PERFORMED PDM PROCEDURE. STARTED THE APU ALL ELECTRICAL POWER WAS LOST REMOVED AND REPLACED LT AND RT GCU IAW AMM 24-23-12. REMOVED AND REPLACED THE APU GCU IAW AMM 24-22-12. RAN ENGINES AND APU, OPS CHECKED GOOD IAW AMM 24-22-00.

Part: FRAME — CRACKED (FRAME 61A) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO DOOR ACTUATOR BRACKET CRACKED. REMOVED AND REINSTALLED AFT CARGO DOOR IAW A300-600 AMM 52-32-11-04-01. PERFORMED OPS TEST IAW A300-600 AMM 52-32-11-05-01, 52-71-11-05-02, AND 52-73-00-05-02.OPS TEST GOOD. REMOVED AND REPLACED AFT CARGO DOOR ACTUATOR FITTING BRACKET 61A IAW A300- 600 SRM 51-40-21.CLASSIFIED AS CAT "A" MAJOR REPAIR

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 24,902 hrs · 13,844 cycles

LOWER SPAR OF CANTILEVER STRUCTURE IS CRACKED BETWEEN RIB A11 & RIB J08 REPAIRED AREA ON NR 1 PYLON LOWER SPAR BETWEEN RIBS A11 & J08 IAW SRM 54- 52-11 FIG 201. MAJOR REPAIR

Part: FRAME — DAMAGED (FRM 13) · airframe 24,902 hrs · 13,844 cycles

E & E BAY RT SIDE UPPER CORNER MAIN DECK FLOORBEAM AT FRAME 13 IS LOOSE REMOVED DAMAGED FRAME BETWEEM STRINGERS 24R & SPLICE IAW SRM 51-40-21 & DAMAGED FITTING. INSTALLED & REPAIRED IAW SRM 53-12-13 FIG 201. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 252PH CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 24,902 hrs · 13,844 cycles

CORROSION ON NR 1 PYLON FWD MOUNT. REPAIRED BY INSTALLATION OF BUSHINGS IAW SRM 54-51-81 MAJOR REPAIR .

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241BF DELAMINATED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 24,902 hrs · 13,844 cycles

NR 2 PYLON FWD MOUNT CORRODED. REPAIRED IAW SRM 54-51-81. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 231EF CRACKED. A NEW FLOOR PANEL FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 24,902 hrs · 13,844 cycles

NR 1 ENGINE FWD MOUNT AFT INBD SPOT FACE HAS CORROSION. COMPLIED WITH EA 6-5450-T0329592. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 24,902 hrs · 13,844 cycles

NR 1 ENGINE FWD MOUNT AFT INBD SPOT FACE HAS CORROSION. COMPLIED WITH EA 6-5450-T0329592. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 24,902 hrs · 13,844 cycles

NR 2 ENGINE FWD MOUNT INBD AND OTBD SPOT FACE AREAS HAS CORROSION. COMPLIED WITH EA 6-5450-T0329596.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 24,902 hrs · 13,844 cycles

NR 1 ENGINE FWD MOUNT AFT OTBD SPOT FACE CORRODED. COMPLIED WITH EA 6-5450-T0329592.

Part: FLOOR PANEL — DELAMINATED (FRAMES 62-65) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 251YG DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131QG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER AREA) · airframe 24,902 hrs · 13,844 cycles

COURIER FLOOR PANEL 221PF HAS AREA OF DELAMINATION. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-00. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131RG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152MF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152UF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131MG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131SG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132MG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152RF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151QF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151UF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152PF DAMAGED . A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131PG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131KG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152SF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 24,902 hrs · 13,844 cycles

MAIN DECK CARGO FLOOR PANEL 241QH CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132PG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 232SG CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131NG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132LG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132NG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151WF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN DECK CARGO FLOOR PANEL 241KJ DENTED & DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241GJ CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 231YG HAS CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132KG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151MF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151PF DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132QG DAMAGED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 252BF CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152WF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 242ZJ HAS SEVERAL ELONGATED HOLES. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 242EK CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151VF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ - 25-005 CAT "A" REPAIR MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 242GF HAS A CRACK. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241JF CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 242GK IS CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 252ZH DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25- 005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 241AJ CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25 -005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 152VF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 242UJ HAS CRACKED. MAIN CARGO FLOOR PANEL 242UJ, FABRICATED ON T16/1237292 IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 242VG CRACKED. MAIN CARGO FLOOR PANEL 242VG, FABRICATED ON T16/1237327 IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241DF HAS CRACKED. MAIN CARGO FLOOR PANEL 241DF, FABRICATED ON T16/1237288 IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 231TG HAS CRACK. MAIN CARGO FLOOR PANEL 231TG, FABRICATED ON T16/1237350 IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO, CARGO FLOOR PANEL 151XF DAMAGED/BROKEN. FABRICATED FLOOR PANEL 151XF ON T16/1237006 & SRZ 25-005. CAT "A" REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 131LG DAMAGED/BROKEN. FWD CARGO FLOOR PANEL 131LG FABRICATED ON T16/1237562 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

FWD CARGO FLOOR PANEL 132SG DAMAGED/BROKEN. FWD CARGO FLOOR PNL 132SG FABRICATED ON T16/1237567 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 24,902 hrs · 13,844 cycles

AFT CARGO FLOOR PANEL 151TF DAMAGED/BROKEN. AFT CARGO FLOOR PNL 151TF FABRICATED ON T16/1237003 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241WH CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 252VF CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 241HK CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 252BH BROKEN AROUND CUT-OUT. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241TH CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 241MJ HAS A CRACK. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,902 hrs · 13,844 cycles

MAIN CABIN FLOOR PANEL 242MF CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 251RH HAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 232YG HAS A CRACK. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,902 hrs · 13,844 cycles

MAIN CARGO FLOOR PANEL 252UH HAS SEVERAL ELONGATED FASTENER HOLES. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Part: LEG ASSY — DEFECTIVE (LT MLG) · airframe 24,668 hrs · 13,687 cycles

LANDING GEAR WOULD NOT RETRACT IN SYS 1 OR SYS 2. FOLLOWED ECAM AND QRH PROCEDURES. GEAR HANDLE WOULD NOT GO PAST MID-POINT. PERFORMED BITE CHECK ON PROXIMITY DETECTOR UNIT REF MM 32-61-00, FAULT BL IS DISPLAYED. R&R LT MLG LEG ASSEMBLY PER WORK CARD 3211000-01-71. ALL OPERATION CHECKS COMPLIED WITH WORK CARDS 3244000-00-70 AND 3230000-00-70. AIRCRAFT OKAY FOR SERVICE

Part: LANDING GEAR — LACK OF LUBE (LEFT) · airframe 24,666 hrs · 13,685 cycles

LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, IN POSITION DETECTOR, SYSTEM 1, SWITCHED TO POSITION DETECTOR 2 AND ATTEMPTED TO RETRACT WITH NO SUCCESS. REF TSM 32-61-00, CHECK PROXIMITY BOX FOR FAULTS, FOUND BL, FAULT. CLEARED FAULT AND TESTED PROXIMITY SENSORS. ALL SENSORS CHECK CORRECT, REF: 07-11-00-00. JACKED ACFT WITH GEAR IN AIR AND EXTENDED, CHECKED PROXIMITY BOX. ALL SENSORS READ CORRECTLY. PERFORMED A GEAR SWING IN BOTH SYSTEM 1 AND SYSTEM 2, REF: MM 32-31-00-05. GEAR SWING WAS NORMAL WITH ALL INDICATIONS NORMAL. CHECKED PROXIMITY BOX AND ALL SENSORS AGAIN WERE READING IN THE CORRECT POSITION. EXTENDED THE GEAR AND HAD THE WIRE HARNESS FOR THE LT BOOGIE BEAM SENSORS SHAKEN TO SEE IF THAT WOULD TRIP A FAULT. RETESTED THE PROXIMITY BOX AND ALL SENSORS READ CORRECTLY. INSPECTED THE MOUNTING BRACKET FOR THE BOGIE BEAM PROXIMITY SENSORS. BOTH SENSORS ARE SECURE. WHILE INSPECTING THE LT GEAR NOTICED THAT GEAR LOOKED LIKE IT HAD BEEN WASHED AND WAS VERY DRY OF GREASE. PERFORMED FULL LANDING GEAR LUBE OF ALL 3 GEARS REF AMM 12-22-32-00. REF: MM 12-12-32-00, PERFORMED INSPECTION OF LT MLG PITCH DAMPER, FOUND WITHIN LIMITS REF: MM 32-31-00-05. PERFORMED A GEAR SWING IN SYS 1 AND 2. GEAR SWINGS NORMAL IN BOTH SYSTEMS.

Part: LEVER — EXCESS PLAY (FLAP FAIRING) · airframe 24,457 hrs · 13,525 cycles

HARMONIC VIBRATION LASTED FOR 1 MIN WENT AWAY FOR 10 SECONDS & THEN CAME BACK. VIBRATION WAS WORSE AT HIGHER SPEEDS, LEAST AT 290 KNOTS & BELOW. VIBRATION FREQUENCY WAS MEDIUM & ENTIRE AIRFRAME WAS SHAKING. DID NOT FEEL VIBE IN CONTROL COLUMN, NOR THROTTLES OR RUDDER PEDALS, VIBRATION INTENSITY WAS MILD TO MODERATE. DURING INSPECTION OF FAIRINGS WITH FLAPS & SLATS UP, FOUND RT NR 2 FAIRING WITH EXCESSIVE PLAY COMPARED TO OTHERS. DROPPED FLAPS TO INVESTIGATE & FOUND RT NR 2 OTBD FAIRING ROD & LEVER WITH EXCESSIVE PLAY. DURING COMPARING NR 2 RT WITH LT NR 2, FOUND LT NR 2 MISSING RETAINING BOLT, 2 SLEEVES, 2 WASHERS, NUT & COTTER PIN, REF IPC 27-51-51-03 ITEMS 10 - 50.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 24,116 hrs · 13,330 cycles

DURING TAXI, IN HEAVY THUNDERSTORM CONDITIONS, REC'D MAIN DECK CARGO SMOKE WARNING OF MID-2, LOOP B, WITH LOOP A MEL'D OFF. DONNED O2 MASKS & RAN ECAM CHECKLIST, SHUTTING DOWN RT PACK & ISOLATING HOT AIR. SMOKE WARNINGS & INDICATIONS CEASED. DID NOT EVACUATE DUE TO SEVERE RAIN, WIND & LIGHTNING CONDITIONS, WIND GUST O 47 KNOTS, INTO THE TAIL. SUSPECT EXTREME TAILWIND CAUSED PACK OVERHEAT. PERFORMED INSPECTION OF RT PACK AREA, NO DEFECTS NOTED. PERFORMED OPERATIONS CHECK OF CARGO SMOKE WARNING MID LOOP B IAW MM 26-16-11-04. OPERATIONS CHECKED NORMAL. RAN RT PACK IAW MM 21-00-0-00-00 & 21-20-00-00. PERFORMED SNIFF CHECK, NO ABNORMALITIES NOTED. ACFT OK FOR SERVICE.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 23,822 hrs · 13,182 cycles

CRUISE FLIGHT AT FL 350L, ENG NR 2 N 1, EGT & FUEL FLOW BECAME UNSTABLE, CONTINUOUSLY FLUCTUATING. ENG STABILIZED ONCE ON DESCENT BEGAN & WAS NORMAL THROUGH LANDING & TAXI. REPLACED HMU & FUEL PUMP.

Part: MOISTURE TRAP — LEAKING (AIR SPEED) · airframe 232 hrs · 12,836 cycles

REVIEWED QRH ON TAXI OFF ROLL, HAD ABOUT 5 KTS SPLIT BETWEEN CAPTAINS PFD & STBY, FOR UNRELIABLE AT 80 KTS, SPLIT GOT GREATER AS AIRSPEED NEVER CALLED INCREASED. ROTATED ON FIRST OFFICERS CALL, 144 WITH 144 ON STBY AIRSPEED. NEVER GOT ADC FAULT. INFLIGHT 230 KTS WAS >180 ON CAPTAINS PFD. PERFORMED LEAK CHECK AND LEAK CHECK FAILED. AFTER FURTHER TROUBLESHOOTING, FOUND COMPONENT IDENTIFIED AS A TRAP LEAKING. THE MOISTURE TRAP WITH AN ATTACHED ELBOW FITTING WAS REPLACED AND THE DRAIN LINE CLEARED. LEAK CHECKED GOOD IAW MM 34-10-00-05.

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 229 hrs · 12,679 cycles

DURING TAKEOFF ROLL APPROX 80 KTS, MASTER CAUTION LIGHT & CHIME CAME ON INDICATING GREEN, 1 & 2, HYD PRESSURE INOPERATIVE. PERFORMED REJECT & QRH. REMOVED AND REPLACED GREEN HP MANIFOLD PRESSURE SWITCH 30WW AS A PRECAUTION IAW AMM 29-11-12-04. REPLACED GRN PRESSURE TRANSMITTER 17WV IAW AMM 29-32-13-04. BOTH LEAKED CHECKED AND OPS CHECKED GOOD DURING ENG RUNS IAW AMM 29-10-00-05.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 22,123 hrs · 12,243 cycles

FWD CARGO COMPARTMENT CUT OUT FWD FRAME FRAME 20A STRINGER 39R - 41R FOUND 1 EACH DENT. COMPLIED WITH EA 6-5310-T0310888 PART1, TITLE: FUSELAGE - MAINFRAME. ONE DENT ON FRAME FR20A WEB AT STRINGER 39R-41R. REPAIRED THE FWD CARGO COMPARTMENT CUTOUT FWD FRAME FR20A S39R-S41R DENT. THIS REPAIR CATEGORY IS "C", REPAIR LIFE LIMITATION IS 6 MONTHS. MAJOR REPAIR IAW GMM6-2-100.

Part: HOOK — CHAFED (CARGO DOOR) · airframe 22,123 hrs · 12,243 cycles

AFT CARGO DOOR NR 2 LOCKING HOOK WORN. PER AMM52-30-21-01-01 REPLACED THE HOOK OF AFT CARGO DOOR NR 2 LOCKING, TEST OF THE LOCKING MECHANISM FOR INSTALLATION,TEST OK.

Part: HOOK — CHAFED (CARGO DOOR) · airframe 22,123 hrs · 12,243 cycles

AFT CARGO DOOR NR 1 LOCKING HOOK WORN. PER AMM 52-30-21-04-01 REPLACED THE AFT CARGO DOOR NR 1 LOCKING HOOK. PERFORM INSTALLATION TEST OF THE LOCKING MECHANISM ,TEST OK.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 39 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACE THE CRACKED CROSSBEAM AT MDCC FR39 B/W Y-450 TO Y-953 PER AMM 20-21-12- 00,MAJOR REPAIR IAW GMM 6-2-100.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 49 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACE THE CORRODED CROSSBEAM PER A300-600F SRM51-40-21,(MDCC FR49 B/W Y-1959 TO Y-2462 CROSSBEAM) ,THIS REPAIR CATEGORY IS "A",MAJOR REPAIR IAW GMM 6-2-100.

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 39 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR39 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTATOR PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 38.2 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR38.2 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 42 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACED THE MDCC FR42 B/W Y-450 TO Y-953 CROSSBEAM PER AMM20-21-12-00. MAJOR REPAIR IAW GMM6-2-100

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 48 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR48 B/W Y-1959 TO Y-2462 CROSSBEAM PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 41 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACED THE MDCC FR41 B/W Y-450 TO Y-953 CROSSBEAM PER AMM20-21-12-00. MAJOR REPAIR IAW GMM6-2-100

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,123 hrs · 12,243 cycles

FUSELAGE CTR SECTION LT FRAME 44 STRINGER 24 TO 28, HOLE B WITH CRACK SIGNAL. COMPLIED REPAIR PER EO 6-5310-7-5006 B PART1, TITLE: FUSELAGE - CENTER SECTION - AD 2004-23-20 - INSPECT BETWEEN FR41 TO FR46 FROM STGR 24 TO STGR 28 ON LT & RT. SB A300-53-6122, A300-53-6125R02, REFER TO WRI FOR WORK DETAILS. REPAIRED FUSELAGE CENTER SECTION LT FRAME 44 STGR 24 TO 28, HOLE B. THIS REPAIR CATEGORY IS "B". SUBSEQUENT INSPECTION AT INTERVALS OF 3400FC OR 8800FH. MAJOR REPAIR IAW GMM6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 22,123 hrs · 12,243 cycles

CENTER WING JOINT AT FRAME 40 LT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. REAMED THE HOLE OF CENTER WING JOINT FRAME 40 LT SIDE UPPER FASTENER TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5710-T0310695APT1 TITLE:WING-BASIC WING STRUCTURE -CRACK HOLE IN CENTER WING JOINT -FR40 LT /RT. THIS REPAIR IS CATEGORY "B" ,SUBSEQUENT INSPECTION AT INTERVALS OF 2910 FC OR 4400FH. MAJOR REPAIR IAW GMM6-2-100.

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 34 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR34 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 22,123 hrs · 12,243 cycles

CENTER WING JOINT AT FRAME 40 RT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. REAMED THE HOLE OF CENTER WING JOINT FRAME 40 RT SIDE UPPER FASTENER TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5710-T0310695APT1 TITLE:WING-BASIC WING STRUCTURE -CRACK HOLE IN CENTER WING JOINT -FR40 LT /RT. THIS REPAIR IS CATEGORY "B" ,SUBSEQUENT INSPECTION AT INTERVALS OF 2910 FC OR 4400FH. MAJOR REPAIR IAW GMM 6-2-100.

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,123 hrs · 12,243 cycles

MDCC FRAME 38.1 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR38.1 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100

Part: LINE — LEAKING (HYD SYSTEM) · airframe 22,069 hrs · 12,211 cycles

AFTER DEPARTURE, ECAM & OVERHEAD SHOWED LOSS OF GREEN HYD PRESSURE & QTY. COMPLIED WITH ECAM & QRH. CONFIGURED FOR LANDING WITH GRAVITY EXTENSION. DURING APPROACH, GREEN HYD QTY SHOWED SOME FLUID REMAINING. PUMPS OFF LESS THAN ONE MINUTE AFTER ECAM. CONFIRMED THAT THE GREEN SYS QTY NEVER WENT COMPLETELY TO ZERO. SERVICED GREEN SYSTEM HYDRAULICS. OPERATED HYDRAULICS WITH NO LARGE LEAKS LOCATED. FOUND SMALL LEAK AT GREEN FILTER BOWL ASSY. RESET GEAR EMERGENCY EXTENSION SYS. R & R FILTER AND BOWL ASSY. LEAK CHECKED GOOD. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES. HYDRAULIC RESERVOIR INDICATION WENT TO OVER SERVICED. ADJUSTED LEVEL ON RESERVOIR. SWUNG GEAR SEVERAL MORE TIMES QTY. INDICATION AND PRESSURE INDICATIOR CHECKED GOOD. LET SYSTEM PRESSURIZED WITH GEAR UP FOR EXTENDED PERIOD AND NO LEAKS NOTED ON SYSTEM. CHECKED RESERVOIR PRESSURIZATION LINE FROM NR 1 ENGINE, FOUND LEAK ON FLEX LINE. R & R LINE IAW SMP. LINE LEAK CHECKED GOOD.

Part: TRANSMITTER — FAULTY (HYDRAULIC SYS) · airframe 22,068 hrs · 12,210 cycles

IN DESCENT HAD ECAM & OVERHEAD SHOWED LOSS OF FLUID & LOSS OF PRESS IN GREEN SYS. COMPLIED WITH ECAM FOR LOSS OF PRESS IN GREEN SYS. FULLY CONFIGURED FOR LANDING HYD FLUID LEVEL INDICATION CAME BACK TO NORMAL, LANDED UNEVENTFUL. R & R GREEN SYS RESERVOIR TRANSMITTER, NEEDS LEAK CHECK. R & R GREEN SYS MANIFOLD HYD FILTERS & BOWLS FOR GREEN BRAKE & HYD ELEC PRESS, WILL NEED LEAK CHECK. INSPECTED HYD SYS, NO DEFECTS NOTED. RAN BOTH ENGS IAW JRH & LEAK OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 21,298 hrs · 11,803 cycles

FL340, LT WINDOW HEAT CAME ON, TURNED HEAT OFF. OUTER WINDOW SCREEN CRACKED. FOLLOWED ECAM PROCEDURES & LANDED. REMOVED AND REPLACED L1 WINDOW IAW MM 56-11-11-04.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 20,865 hrs · 11,568 cycles

PRIOR TO TOP OF DESCENT, RECEIVED AN ECAM "HYD BLUE LO QTY" WARNING. BOTH OVERHEAD BLUE SYS QUANTITY AND ON ECAM WAS AT REDLINE. WARNING CAME AND WENT NUMEROUS TIMES. TURNED OFF BLUE SYS PUMP AND DIVERTED TO LAX. AFTER PUMP TURNED OFF, BLUE SYS QTY WENT UP TO LINE BETWEEN AMBER AND GREEN. INSPECTED LOWER FUSELAGE AND GEAR WELLS, FOUND NO EVIDENCE OF LEAKS. FOUND INDICATOR OF HYD RESERVOIR (BLUE) SHOWING 1.75 GALLONS. REMOVED AND REPLACED BLU HYD SYSTEM TRANSMITTER IAW MM 29-31-11-04, DRAINED BLUE SYSTEM RESEVOIR AND MEASURED AT 3 GALLONS, FILLED BLUE SYSTEM RESERVOIR WITH MEASURED THREE GALLONS FLUID ALL COCKPIT INDICATIONS SHOWED MIDDLE OF TOP HAT PERFORMED HYD FLUID LEVEL INDICATION TEST REF M.M. 29-31-00-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,866 hrs · 10,480 cycles

FRAME 1, STRINGER 25 + 10" FOUND ONE DENT 4.25"X5.5". FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-11-12. 2. NDI WAS COMPLETED. NO CRACK WAS FOUND REF. TO AB6 NTM PART 6 51-10-07 PAGE 601. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 18,866 hrs · 10,480 cycles

AFT CARGO BAY FLOOR PANEL 152PF HAS EDGE AREA WITH IMPACT DAMAGE. REMOVED AFT CARGO BAY FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20, DWG 16 A53279902. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-33-04. GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 18,866 hrs · 10,480 cycles

AFT CARGO FLOOR PANEL HAS A 1 INCH PUNCTURE OF THE UPPER SURFACE AT FR 54.1 AND -Y1400.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 18,866 hrs · 10,480 cycles

NR 241TH FLOOR PANEL UPPER SURFACE HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-25-4. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, MC. INSTALLED FLOOR PANEL IAW AMM 53-10-25-4. THE REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 18,866 hrs · 10,480 cycles

AFT CARGO COMPARTMENT 151WF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL AND INSTALLED INSERTS WITH ADHESIVE IAW SRM 53-10-20, AND DWG 17 A53279913. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-33-04. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 18,866 hrs · 10,480 cycles

AFT CARGO COMPARTMENT 151XF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED THE NEW FLOOR PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20, NSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-33-04 IAW GMM 6-2-100, REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — WORN (MAIN DECK) · airframe 18,866 hrs · 10,480 cycles

MAIN DECK FLOOR AREA, FOUND SEAT TRACK, IS EXCESSIVELY WORN AT FR44 AND Y1456 POSITION . R & R THE SEAT TRACK IAW SRM 51-40-21. THE REPAIR EVLUATED IAW GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 18,866 hrs · 10,480 cycles

AFT CARGO COMPARTMENT 152XF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL AND INSTALLED INSERTS WITH ADHESIVE IAW SRM 53-10-20, IRM 9701 AND DWG 17 A53279913. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-33-04 IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,335 hrs · 9,680 cycles

F/O SMELLED SOMETHING ABNORMAL JUST A MOMENT PRIOR TO AVIONICS SMOKE INDICATION DURING TAXI-OUT. SUBSEQUENT CHECK OF SNIFFER FAN WAS NEGATIVE FOR SMOKE OR FUMES. WARNING EXTINGUISHED AFTER APPROX 2 MINUTES. CHECKED AVIONICS AREA WITH SEVERAL SYSTEMS ON, COMPLETED VISUAL ALSO. NO INDICATION OF SMOKE DETECTED .NO ODORS OR SMOKE NOTED.NO FURTHER INDICATIONS.OK FOR SERVICE.

Part: COALESCER BAG — ODOR · airframe 16,175 hrs · 9,017 cycles

APROX 50 MINUTES INTO FLIGHT HAD MAIN DECK AFT LOOP A FAULT. FOLLOWED QRH WITH GOOD TEST. BUT THEN LATER REPEATED SMOKE WARNING FROM MAIN DECK AFT. FOLLOWED BY VISIBLE BLUE SMOKE HAZE IN COCKPIT AND LATERBY SMOKE WARNING FROM MAIN DECK MID 1 AND MID 2 ACCOMPLISHED EMERGENCY LANDING AT KOKC. AFTER LANDING ALL WARNINGS WENT AWAY. R & R 1 &2 COALESCER BAGS I.A.W. 21-51-16-03, NO CONTAMINATION FOUND. PERFORMED VISUAL INSPECTION OF NR 1 & 2 ENGINES FOR OIL LEAKS, NO LEAKS NOTED. CHECKED OIL LEVELS AND HYDRAULIC LEVELS AS REQUESTED BY MOCC NR 1 ENGINGE SERVICE WITH 3 QTS. CREW REPORTED THAT NR 1 ENG WAS AT MINIMUMS ON DEPT FROM MEM.REMOVED AND REINSTALLED NR 1 IP CHECK VALVE IAW 36-11-13-04 PER MOCC REQUEST. ACFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,174 hrs · 9,016 cycles

AFTER 45 MINUTE GOT MAIN DECK LOOP FAULT AND ALMOST IMMEDIATELY MAIN CARGO SMOKE. DONNED O2 MASKS. AFTER A FEW SECONDS GOT AVIONICS SMOKE. ENROUTE WE HAD DETECTED WHAT SEEMED LIKE HOT AIR COMING FROM THE AIR CONDITIONING, EVEN THOUGH THE TEMPERATURES WERE SHOWING LOW. AFTER LANDING ALL INDICATIONS CEASED. NO INDICATION OF SMOKE ANYWHERE. RAN BOTH PACKS ON APU. OIL ODOR IN COCKPIT. R & R AVIONICS BLOWER FILTER IAW MM 21-21-16-04-0. OIL ODOR STILL EVIDENT, NOT AS BAD. RAN BOTH ENGS PER JRH. NO OIL ODOR WITH APU BLEED OFF. NO SMOKE, 'HAZE', OR 'BLOWDRYER' ODOR DETECTED IN COCKPIT OR AVIONICS BAY.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 15,668 hrs · 8,700 cycles

FWD CARGO FRAME 30 UPPER FLOORBEAM BETWEEN S/T 2R AND 3R IS CRACKED ON FWD SIDE. PERFORMED CROSSBEAM REPAIR AT FWD FACE OF FLOORBEAM FRAME 30 BETWEEN SEAT TRACK 2R AND 3R BY REMOVING DAMAGE, FABRICATING, LOCATING AND DRILLING A FILLER AND REPAIR CHANNEL AND INSTALLING IAW SRM 51-75-10, SRM 51-21-10, SRM 53-10-15 FIGURE 212, NTM 51-10-08.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 15,668 hrs · 8,700 cycles

AFT CARGO FR 64 UPPER FLOORBEAM BETWEEN 4L & 5L IS CRACKED ON AFT SIDE. REMOVED DAMAGE ON AFT CARGO FR 64 UPPER FLOORBEAM BETWEEN 4L & 5L AFT SIDE CHEM MILL, FABRICATED, DRILLED AND INSTALLED REPAIR CHANNEL IAW FREIGHTER SRM 53-10-15 FIG 21. REMOVED AND REINSTALLED CLS ADAPTER FOR ACCESS IAW SRM 53-10-15 FIG 21. NDT VERIFIED, CRACK REMOVED IAW NTM 51-10-08, RESTORED SURFACE PROTECTION IAW SRM 51-75-10 AND 51-21-10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 15,668 hrs · 8,700 cycles

AFT CARGO PIT FLOORBEAM FR 58 BETWEEN SEAT TRACK 2&3 RT CRACK, PREVIOUS REPAIR IN AREA WITH 1EA HYLOCK COLLARS MISSING & 1 EA COLLAR BROKEN. R & R CROSSBEAM SECTION AT FR 58. INSTALLED 4 EA REPAIR COUPLING AND 4 EA COUPLING STRAPS IAW SRM 53-10-15 FIG 207.

Part: SKIN — BENT (ZONE 100) · airframe 15,668 hrs · 8,700 cycles

FWD CARGO DOOR EXTERIOR SKIN AT FWD CORNER HAS 3" AREA OF SKIN BENT INTO WIND DAMAGE CLASSIFIED OUT OF LIMITS IAW SRM 52-30-00. REPAIRED DOOR SKINS IAW SRM 52-31-00, FIG 203 BY INSTALLING DOUBLER AND FILLER TO TOP SKIN.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 15,668 hrs · 8,700 cycles

FWD CARGO FR 31 UPPER FLOORBEAM BETWEEN 2R AND 3R CRACKED ON FWD SIDE CHEM MILL. ROUTED OUT CRACK, INSTALLED FILLER CHANNEL, APPLIED PROTECTIVE COATING IAW SRM 53-10-15, FIG 212.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 15,668 hrs · 8,700 cycles

SEAT TRACK 3L HAS (2 EA) BROKEN SCALLOPS LOCATED 2 IN AFT OF FRAME 59, REMOVED DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK AND SPLICE. REPROTECTED ALL PARTS IAW A300 FREIGHTER SRM 53-10-16 FIG 201.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 14,366 hrs · 7,938 cycles

AFTER START GOT ECAM INDICATION FAULT ON MAIN DECK RIGHT AFT CARGO SMOKE DETECTION SYSTEM AND FAULT LIGHT ON OVERHEAD PANEL. CLEARED ITSELF AFTER 2-3 MINUTES. THEN COME ON AGAIN DURING T/O ROLL AT 30-40KIAS. ABORTED T/O. FAULT LIGHT WENT AWAY. RETURNED TO RAMP. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-A CATEGORY: C EXPIRATION: 15MAR09 "MEL 26-17-01-A: MAIN DECK (IDENTIFY MID 1, MID 2 AN D/OR AFT) A SMOKE DETECTOR(S) INOP." REMOVED AND REPLACED LOWER CARGO SMOKE DETECTOR 44WH AND 9 WH REF MM 26-16-11-4. OPS CHECK NORMAL REF 26-16-00-5. REF TSI 26-12 NR 7249 FOR PARTS CHANGE AND T/S INFO.

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 12,888 hrs · 7,099 cycles

2ND INBD LEADING EDGE SECTION ON THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW ANGEL IAW DWG ALC 07052 REV G. LOCATED; DRILLED & DEBURRED NEW ANGLE IAW SRM 51-31-01 VOL II PG 1. ALODINED & PRIMED NEW ANGLE IAW SRM 51-21-01 VOL II PGS - 18. INSTALLED ANGLE IAW SRM 51-33-01 PG 1 & 51-35-01 VOL II PG 1. MINOR REPAIR.

Part: ESCAPE ROPE — NONE (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

F/O ESCAPE ROPE IS STILL IN THE PLASTIC PACKAGING. REMOVED PLASTIC PACKAGING AS REQUIRED. REF FEDEX STANDARD MAINTENANCE PRACTICES.

Part: FRAME — DAMAGED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

COCKPIT WINDSHIELD CENTER FRAME EXTERIOR, 2ND BOLT HOLE FROM THE BOTTOM IS ELONGATED. COMPLIED WITH EA NR 6-5310-113036 PART 1.

Part: SKIN PANEL — CRACKED (THRUST REVERSER) · airframe 12,839 hrs · 7,070 cycles

NR 1 INBD T/R UPPER FWD SKIN PANEL IS CRACKED. REMOVED DAMAGED SKIN PANEL IAW A300-600 SRM 51-40-21. FABRICATED NEW PANEL IAW A300-600 SRM 51-26-00 AND 51-40-40 AND PER FEDEX GMM N7-0-1001. INSTALLED NEW PANEL IAW A300-600 SRM 51-40-21.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN CABIN FLOOR PANEL NR 242 RG IS CRACKED. FABRICATED NEW FLOORBOARD PNL NR 242RG IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION SEE W/C 62C0702.

Part: FAIRING — DAMAGED (NR 1 NACELLE) · airframe 12,839 hrs · 7,070 cycles

NR 1 PYLON LOWER FAIRING FWD LT ATTACH HOLES ARE ELONGATED. REMOVED SKIN PER SRM 51-40-21 PARA 6 & 7 DUE TO FASTENER HOLES ELONGATED BEYOND LIMITS PER SRM 54-55-51. FABRICATED UPPER LONGERON REPAIR SECTION & SPLICE PER SRM 54-55-51, FIG 207. ALODINED AND PRIMED UPPER LONGERON REPAIR SECTION & REPAIR SPLICE PER SRM 51-21-10 & 51-23-10. FABRICATED NEW SKIN PER SAMPLE & PER GMM 7-0-1001. ALODINED & PRIMED NEW SKIN PER SRM 51-21-10 & 51-23-10. REMOVED UPPER LONGERON SECTION PER SRM 54-55-51, FIG 207. INSTALLED UPPER LONGERON SECTION; SPLICE & NEW SKIN PER SRM 51-40-21 PARA 6 & 7. MINOR PEPAIR

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN CABIN FLOOR BOARD 242UJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242UJ IAW FEDEX DWG SRZ 25-005 REV F. FOR INSTALLATION SEE W/C 62C0702.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN CABIN FLOOR PANEL NR 242EK IS CRACKED. FABRICATED NEW FLOOR PNL NR 242EK IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION, SEE W/C 62C0702. MAJOR REPAIR.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN CABIN FLOOR PANEL 242 ZJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242ZJ IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION SEE W/C 62C0702.

Part: SKIN — DAMAGED (RT WING) · airframe 12,839 hrs · 7,070 cycles

RT WING LOWER O/B PANEL 590 BB HAS SCRATCHES ON THE SKIN AROUND THE CUTOUT, AND ON THE ANGLES INSIDE THE CUTOUT.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN CABIN FLOOR PNL 232 YG IS CRUSHED. FABRICATED NEW FLOOR BOARD PNL NR 232 YG IAW FEDEX DWG SRZ 25-005 REV F. FOR INSTALLATION SEE W/C 62C0701.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 12,839 hrs · 7,070 cycles

MAIN CARGO FLOOR PANEL 261AH IS CRACKED ACROSS THE LOWER SURFACE. FABRICATED NEW PANEL 261AH IAW SRZ 25-005 REV F.

Part: SUPPORT ANGLE — CRACKED (BS 972) · airframe 12,839 hrs · 7,070 cycles

AVIONICS COMPARTMENT STRUCTURE UNDER THE COCKPIT FLOOR, INTERCOSTAL AFT SUPPORT ANGLE CRACKED AT THE BEAM ATTACHMENT; BS 972, LBL 39. REMOVED SUPPORT ANGLE IAW SRM 51-40-10 & 51-23-10. FABBED ANGLE IAW SRM 51-40-44 & TPS 1003 REV A. ALODINED, PRIMED & TOP COATED IAW SRM 51-21-10 & 51-23-10. PART MARKED IAW GMM 7-0-1000. INSTALLED ANGLE IAW SRM 51-40-21.

Part: INTERCOSTAL — CRACKED (BS 972) · airframe 12,839 hrs · 7,070 cycles

AVIONICS COMPARTMENT, INTERCOSTAL UNDER THE FLIGHT DECK FLOOR IS CRACKED ON THE AFT END; LOCATED AT BS 972 (FR 10), LBL 39. REMOVED INTERCOSTAL IAW SRM 51-40-21. FABBED NEW WEB IAW DWG 45-A53611975 ISSUE A, TPS 1003 REV A & SRM 51-40-44. ALODINED, PRIMED IAW SRM 51-21-10 & 51-23-10. PART MARKED IAW GMM 7-0-1000. INSTALLED INTERCOSTAL IAW SRM 51-40-21. MINOR REPAIR.

Part: FLOOR PANEL — TORN (MAIN CARGO BAY) · airframe 12,839 hrs · 7,070 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252 GF IS TORN. FABRICATED NEW PANEL 252 GF IAW FEDEX SRZ 25-005 REV F.

Part: FLOOR PANEL — TORN (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN DECK CARGO COMPARTMENT FLOOR BOARD 251 XF IS TORN. FABRICATED NEW PANEL NR 251 XF IAW FEDEX SRZ-005 REV F. MAJOR REPAIR.

Part: BUSHING — CORRODED (CARGO DOOR) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO DOOR NR 1 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED THE AFT CARGO DOOR NR 1 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR.

Part: FLOOR PANEL — TORN (ZONE 200) · airframe 12,839 hrs · 7,070 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD (SR30B5327071400200252) VF IS TORN. FABRICATED NEW FLOORBOARD PANEL NR 252 VF IAW SRZ 25-005 REV F.

Part: FLOOR PANEL — CRACKED (MAIN CARGO FLOOR) · airframe 12,839 hrs · 7,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL 262NF IS CRACKED. FABRICATED NEW PANEL 262 NF IAW SRZ 25-005 REV F.

Part: BUSHING — CORRODED (CARGO DOOR) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO DOOR NR 4 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 4 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600AMM 52-32-11-5. T/W, TWS8330A.

Part: BUSHING — CORRODED (CARGO DOOR) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO DOOR NR 6 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 6 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A. MINOR REPAIR.

Part: BUSHING — CORRODED (CARGO DOOR) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO DOOR NR 5 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRECTED. REMOVED AND REPLACED AFT CARGO DOOR NR 5 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A.

Part: BUSHING — CORRODED (CARGO DOOR) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO DOOR ECCENTRIC BUSHING SUPPORT INNER BORE CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 2 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 12,839 hrs · 7,070 cycles

AFT CARGO PIT DOOR CUTOUT, FUSELAGE SKIN GOUGED FWD LOWER CORNER OF CUTOUT FR 59A, STR 40-41R. BLENDED GOUGE IAW SRM 51-73-10. FOUND OUT OF LIMITS IAW SRM 51-40-21. REWORKED AREA IAW SRM 53-17-12-101 C-2 FIG. 104. FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED & TOP COATED APPLIED IAW SRM 51-23-20, 51-21-10, 51-40-21.

Part: SKIN — DENTED (FUSELAGE) · airframe 12,839 hrs · 7,070 cycles

FOUND FUSELAGE EXT SURFACE SKIN DENTED BETWEEN FR 90 AND FR 91, BL 21L. CHECKED DENT LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12, PAGE 109. CUT OUT DAMAGE AND FABBED 1 EA REPAIR DOUBLER AND FILLER IAW SRM 53-10-12, FIG 255 SHEET 2, PAGES 357-362. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-12, FIG 225 SHEET 2.

Part: TRANSMITTER — FAILED (OIL PRESSURE) · airframe 12,719 hrs · 6,990 cycles

ON CLIMB-OUT, ECAM ADVISORY INDICATED NR 1 ENGINE ZERO OIL PRESSURE CONFIRMED WITH GUAGE WHICH INDICATED ZERO AS WELL. COMPLIED WITH QRH. SHUT NR 1 ENGINE DOWN. LANDED IND. REMOVED AND REPLACED NR 1 ENG. OIL PRESSURE TRANSMITTER IAW AMM 79-33-11-4-05. PERFORMED ENG POS-WINDMILLING INSP PER AMM 72-00-00-6-05. RAN ENG. APROX 3 TO 5 MINS AND ENG OIL PRESSURE CHK'S GOOD AND NO LEAKS NOTED AT THIS TIME.

Part: UNKNOWN — UNKNOWN (THRUST REVERSER) · airframe 11,384 hrs · 6,243 cycles

ON POWER UP, NO REV UNLK LIGHTS NOTED ECAM. ENG NR 1 R REV PRESSURIZED. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 04FEB07 "MEL 78-30-01-A: ENGINE. NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." REACTIVATED NR 1 T/R AND PERFORMED OPS CK REF JRH USING APU AIR. ALL INDICATIONS NORMAL. REMOVED AND REPLACED PRSOV PRECAUTIONARY REF A300 MM 78-31-05-4. PERFORMED ENG POWER RUN, DID NOT GET "REV PRESSURIZED" INDICATION. CHECKED OPERATION OF T/R USING APU AIR AGAIN WITH ALL INDICATIONS NORMAL. RETURNED VALVE MPN 320522-5 TO TSP.

Part: THRUST REVERSER — MALFUNCTIONED (NR 2) · airframe 8,188 hrs · 4,529 cycles

REJECTED TAKEOFF AT 80 KIAS AFTER RECEIVING AMBER ECAM REV 2 PRESS MEL 24DEC04. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. R&R DPV AND PRESS SW LEAK AND OP CHKS GOOD PER E.O. 7830-7-3316B.

Part: FAN — OUT OF BALANCE (NR 2 ENGINE) · airframe 7,584 hrs · 4,164 cycles

EN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9 VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 - 60 PERCENT. PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGINE VIB INDICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE.

Part: FAN — OUT OF BALANCE (NR 2 ENGINE) · airframe 7,584 hrs · 4,164 cycles

IN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9, VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 - 60 PERCENT. *S/D* PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGINE VIB INDICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 6,193 hrs · 3,363 cycles

MAIN DECK FLOORBEAM AT FRAME 58, 24 INCHES RIGHT OF CENTER, IS CRACKED 3 INCHES DOWN FROM TOP APPROX 1 INCH LONG. REPAIRED IAW FEDEX EA 6-5310-72527.

Part: CONNECTOR — LOOSE (THRUST REVERSER) · airframe 5,073 hrs · 2,753 cycles

GOT ECAM WARNING, NR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, BELOW 80 KNOTS. SECURED CONNECTOR PLUGS AND RAN ENGINES, NO ECAM MESSAGE REPEAT.

Part: SPEAKER — NOISY (COCKPIT RADIO) · airframe 991 hrs · 471 cycles

ABORTED T/O DUE TO LOUD SQUEAL NOISE IN COCKPIT OF UNDETERMINED ORIGIN (NOT RADIO). RECONFIGURED AC- WND TO NORMAL UNABLE TO DETERMINE SOURCE OF NOISE. INFO NOTED 2ND T/O ROLL NORMAL. UNABLE TO DUP NOISE.