N682FE

Part: WIRE — DETACHED (ZONE 800) · airframe 34,612 hrs · 19,410 cycles

EMERGENCY ACCESS SWITCH AND MOMENTARY DOOR BELL BUTTON INOP. DURING T/S FOUND WIRE JMPR-22 BROKEN AT EMERGENCY ENTRY SWITCH TERM 1. RETERMINATED WIRE JMPR-22 AND 9005-20 AT EMERGENCY ENTRY SWITCH TERM 1 . OPS CHK REQ'D. ACCOMPLISHED OPS TEST OF COCKPIT DOOR LOCKING MECHANISM. AC OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 100) · airframe 34,064 hrs · 19,040 cycles

WINGS - BASIC WING STRUCTRUE - INSPECTION OF FR40 LOWER OUTBOARD RADIUS, LH SIDE, OUND CRACK AT AREA A STARTED FROM THE HOLE A LWR EDGE COMPILED WITH EO 6-5710-E0333575 D P5. REPAIRED THE CRACKED AREA A ON LH SIDE FR40 FWD FITTING LOWER OUTBOARD RADIUS. THIS IS CATEGORY B REPAIR AND TRACKED BY EO 6-5710-E0333575. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: WEB — CRACKED (FRM 47) · airframe 34,064 hrs · 19,040 cycles

MAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVALOF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: WEB — CRACKED (FRM 47) · airframe 34,064 hrs · 19,040 cycles

MAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVALOF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: WEB — CRACKED (FRM 47) · airframe 34,064 hrs · 19,040 cycles

MAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVALOF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: CROSSBEAM — CRACKED (FRM 61) · airframe 34,064 hrs · 19,040 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR61 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: WEB — CRACKED (FRM 47) · airframe 34,064 hrs · 19,040 cycles

MAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVALOF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: LUG — CORRODED (RT WING) · corrosion level 2 · airframe 33,986 hrs · 18,992 cycles

R/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE REPAIRED R/H MLG RIB 5 FWD LUG PER AIRBUS R57240425 SEE JPF PAGES 1-2, ITEMS 1-16 FOR WORK COMPLETED, EA # 6-5710-T0378296 P1 TITLE: WINGS - RH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFTY PINTLE FWD LUG BORE CORROSION IAW AIRBUS REPAIR DRAWING R57240425

Part: LUG — CORRODED (LT WING) · corrosion level 2 · airframe 33,986 hrs · 18,992 cycles

L/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE. REPAIRED IAW AIRBUS REPAIR INSTRUCTIONS R57240425. SEE FINAL EA 6-5710-T0378283. TITLE: WINGS - LH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFT PINTLE FWD LUG BORE CORROSIION IAW AIRBUS REPAIR DRAWING R57240425.

Part: ENGINE — LEAKING (N/A) · airframe 33,844 hrs · 18,913 cycles

ENG 1 OIL LO PRESS. PRESSURE INDICATED NORMAL ON ENG PAGE AND GAUGE. HOWEVER, WE NOTICED OIL QUANTITY DECREASING. DECREASING APPROX 2 QUARTS PER 10 MINUTES. AFTER LANDING BACK AT KMEM WE HAD 5 QUARTS REMAINING. 8 QUARTS AFTER ENG SHUTDOWN. ADDED 12 QTS OIL. RAN ENG 1 FOR 10 MIN 2 40% N1. LOST 1 QT OIL DURING RUN. FOUND LUBE/SCAVENGE PUMP LEAKING. UNABLE TO DETERMINE IF PUMP HOUSING OR TUBING SEAL CAUSING LEAK. AS A PRECAUTION R & R ENG 1 LUBE/SCAVENGE PUMP & SEALS. RESERVICED ENG OIL TK TO FULL RAN ENG @ 40% N1 FOR 10 MIN. NO OIL LOSS. NO LEAKS.

Part: FITTING — CORRODED (UNKNOWN) · airframe 33,986 hrs · 18,992 cycles

RH RIB 5 FITTING HAS CORROSION. REPAIR PER AIRBUS REPAIR DRAWING R57240425

Part: FITTING — CORRODED (UNKNOWN) · airframe 33,986 hrs · 18,992 cycles

LHRIB 5 FITTING HAS CORROSION REPAIRED PER AIRBUS REPAIR DRAWING R57240425

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,834 hrs · 18,907 cycles

R1 SLIDE INDICATION NOT SHOWING ON ECAM WHEN DOOR IS CLOSED AND ARMED, ALL OTHER DOOR CLOSED AND LOCKED INDICATIONS ARE FINE. PERFORMED T/S FOUND NO R1" SLIDE" INDICATION ON ECAM. PERFORMED TEST OF AUTOMOMOUS STBY PWR UNIT AND R1 "SLIDE" INDICATION RETURNED TO NORMAL ON ECAM . ARMED/DISARMED R1 DOOR SLIDE SEVERAL TIMES R1 "SLIDE" INDICATIONS NORMALON ECAM IAW A300 TSM 52-73-00. OK FOR SERVICE.

Part: IDG — FAILED (NR 2 GEN) · airframe 33,227 hrs · 18,500 cycles

ON DESCENT LOST GEN 2. GEN DID NOT RESET. REMOVED AND REPLACED #2 ENGINE IDG OPS CHECK GOOD AT THIS TIME REF A 300 AMM 24-11-11-04-01.

Part: METER — NO TEST (O2 MASK) · airframe 32,816 hrs · 18,225 cycles

#4 COURIOUR O2 MASK FLOW METER BLINKER DOES NOT OPERATE DURING TEST. REPLACED #4 COURIER OXYGEN MASK STOWAGE BOX.

Part: TRANSMITTER — FAULTED (YELLOW HYD SYS) · airframe 31,788 hrs · 17,594 cycles

ON TAKE OFF ROLL @ 60 KNOTS RECIEVED ECAM ALERT FOR YELLOW SYSTEM LOW PRESSURE. REJECT THE TAKE OFF AND RETURN TO GATE (NOTE: CREW REPORTED SYSTEM PRESSURE RETURN TO NORMAL DURING TAXI IN) REMOVED AND REPLACED YELLOW SYSTEM HYD QTY TRANSMITTER. REF AMM 29- 31-11-04. OPS AND LEAK CHECKS GOOD. PERFORMED ENG RUN IAW JRH CHAPT 6, WITH 40K OF FUEL ON BOARD AND EIGHT LOADED TO SIMULATE PAST CONDITIONS. ENGINE RUN DURATION WAS 25MINUTES, AND ACCOMPLISHED AT VARIED POWER SETTINGS. CYCLED ALL FLIGHT CONTROLS, FLAPS/SLATS AND STAB AND DID NOT RECIEVE A YELLOW ENG PUMP LOW PRESSURE ECAM OR OVERHEAD ALERT. INDICATED PRESSURE FOR YELLOW SYSTEM WAS STABLE BETWEEN 2900- 3050PSI. YELLOW SYST FIRE SOV INDICATION ON MAINTENCE PANEL WAS SHOWN AS OPEN AND DID NOT FLICKER OFF DURING RUN. YELLOW QTY INDICATION WAS STABLE WITHIN THE TOP HAT OF THE INDICATAOR DURING RUNS AND DID NOT VARY AS NOTED ON PREVIOUS DISCREPANCIES. AIR PRESSURE ON RESERVOIR WAS 50 PSI PRIOR TO AND AFTER ENG RUNS. NO FAULTS NOTED AT THIS TIME FOR YELLOW ENG DRIVEN PUMP. PERFORMED FUNCTIONAL TEST OF YELLOW SYSTEM FIRE VALVES AND ASSOCIATED INDICATION SYSTEM ANDOPS TEST OF YELLOW HYD SYSTEM REF A300 AMM 29-10-00-05. NO FAULTS NOTED.

Part: PRESSURE SWITCH — FAILED (N/A) · airframe 31,773 hrs · 17,583 cycles

PDIS 682 29-10 0412 23DEC21 MEM FACT U SHORTLY AFTER TAKEOFF, CLIMBING THRU 5000 FEET, ECAM DISPLAYED HYD LOW PRESSURE YELLOW SYSTEM. ECAM AND QRH WERE FOLLOWED AND AN UNEVENTFUL LANDING WAS MADE BACK TO RWY 18C KMEM. A300-600 AMM 29-24-00-05. RAN ENGINES PER JRH AND MONITORED HYDRAULIC PRESSURES FOR 10 MINUTES WITH NO FAULTS OR DISCREPANCIES NOTED REF A300-600 AMM 29-32-00-05. T/S PER TSM 29-32-00.REPLACED PRESSURE SWITCH 31WW PER AMM 31-53-51-04. OPS CK AND LEAKS CK GOOD AT THIS TIME

Part: POWER SUPPLY — INOPERATIVE (N/A) · airframe 31,857 hrs · 17,635 cycles

MDIS 682 33-50 0405 22DEC21 GSP FACT U EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY IS DEAD. R/I 22DEC21 01:03 GSP U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-31 POS: 3 SRL: 278291 TAG NBR: 51G876 ON MPN: AD-3214-31 CPN: 3310373 SRL: 256497 TAG NBR: 4I8607 FACT 22DEC21 01:03 GSP U REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW A300-600 AMM REF#33-51-14-04. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (N/A) · airframe 31,857 hrs · 17,635 cycles

MDIS 682 33-50 0400 19DEC21 MEM FACT U EMERGENCY LIGHTS NOT WORKING. R/I 19DEC21 20:26 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 120148 TAG NBR: 28H905 ON MPN: AD-3214-31 CPN: 3310373 SRL: 278291 TAG NBR: J58300 FACT 19DEC21 20:26 MEM U REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY 29WL REF AMM 33-51-14-04. OPS CHECKS GOOD. A/C OK FOR SERVICE.

Part: WEB — CRACKED (ZONE 400) · airframe 31,561 hrs · 17,469 cycles

NO.1 PYLON BOX OUTSIDE SKIN HAS CRACKS ON THE RIB 8 BOTH SIDE. CRACKED RIB 8 WEB REPLACED NEW PART . INSTALLED WITH RIVETS AND FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001 ,PARA 6 PAGE 7B -PAGE 23

Part: WEB — CRACKED (ZONE 400) · airframe 31,561 hrs · 17,469 cycles

NO.2 ENG EXTERAL PYLON BOX (R/H) HAVE CRACK ON THE RIB8 REPLACED THE DAMAGED WEB WITH NEW ONE BY FASTENERS I.A.W. A300-600F SRM 51-72-10- 001, P. 2 AND 51-40-21-001, PARA. 6, P. 7B-23.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 31,561 hrs · 17,469 cycles

RH PYLON FORWARD FAIRING STIFFENER CRACKED AT THE RIB JO0 FWD AREA REINFORCED REPAIR DOUBLER & ANGLE WORK INSTRUCTION I.A.W. A300-600F SRM 54-54-11- 201- 2, PARA. 5A, PAGE 201-207, FIG. 201.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE #252UH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE #232HG FLOOR PANEL OF MDC WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE 241BK PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE 231FH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR30 TO FR31,-Y1456 POSITION. 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 53-10-16-201, PARA.4, PAGE 203-208, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR29 TO FR30,-Y953 POSITION. 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 53-10-16-201, PARA.4, PAGE 203-208, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE 251RH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

THE 251XG FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR36 TO FR37,-Y450 POSITION. 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 53-10-16-201, PARA.4, PAGE 203-208, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: ACCESS DOOR — CRACKED (ZONE 800) · airframe 31,561 hrs · 17,469 cycles

AFTER PAINT REMOVAL FOUND EQUIPMENT COMPARTMENT ACCESS DOOR 1 EA CRACK AT AFT UPPER LATCH CUTOUT AREA. CUT OUT THE DAMAGED AREA. FABRICATED THE REPAIR DOUBLER AND INSTALLED THEM WITH RIVETS I.A.W. A300-600F SRM 52-41-12-201, PARA. 5, FIG. 201, P. 202-205.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR101 TO FR103 AND STR-2L TO STR-5L POSITION. 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 53-19-12-201, PARA.7, PAGE 219-224, FIG 203, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 600) · airframe 31,561 hrs · 17,469 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 202-216, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 500) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON LH WING LWR L/E PANEL 513AB CUTOUT FWD O/B POSITION. 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 202-216, FIG 201, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. "MAJOR REPAIR"

Part: NONE — UNKNOWN (ZONE 300) · airframe 31,561 hrs · 17,469 cycles

AIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.20 AND NO.21 FASTENER COUNTED 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 239-239, FIG 209, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY B REPAIR WITH SUPPLEMENTAL INSPECTION REQUIREMENTS, THE INITIAL THRESHOLD IS 30000 FC, REPETITIVE INTERVAL AND METHODS ARE TO BE DEFINED BY OEM. "MAJOR REPAIR"

Part: STIFFENER — BENT (ZONE 200) · airframe 31,561 hrs · 17,469 cycles

AGING AIRCRAFT RECORDS REVIEW:AT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON W/O 67250,SNRM N00580, PRIMARY STRUCTURE REMOVED AND REPLACED, PRIMARY STRUCTURE LOCALLY FABRICATED, SEE JPF ITEM 5, AND TRAVELER T16/1235154, SNRM BLOCK 16 NOT IDENTIFIED RII, SNRM BLOCK 17 NOT IDENTIFIED MAJOR REPAIR, SNRM BLOCK 21/21A NO SDR INFORMATION ENTERED. SNRM NOT BOUGHT BACK RII. JPF ITEM 5,6,7,8 AND 9 RII BLOCK MARDED (N/A), NOT IDENTIFIED RII, RDR BLOCK 9A IDENTIFIED AS MINOR REPAIR. PER AGING A/C RECORDS REVIEW FINDINGS, W/O #67250, SNRM #N00580 JPF STEP 5,6,7,8,9 WERE NOT IDENTIFIED AS RII, GENERATED W/O #80764, NRC #N00256 TO VERIFY ABOVE REQUIRED STEPS AND FOUND IT TO BE OK, SEE ATTACHED JPF ITEM 1,2,3,4,5,6.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 31,561 hrs · 17,469 cycles

1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB 26AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364452 P1, TITLE: WING-FLIGHT SURFACES-LH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB26 AT STRINGERS 2.8-ALI 575306-01 & A300-600F SRM 57-50-00-201, PARA4E, P217-220, FIG205 & 57-50-00-201, PARA4A, PAGE201- 205, FIG201.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,561 hrs · 17,469 cycles

FWD CARGO COMPT #131LG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,561 hrs · 17,469 cycles

FWD CARGO COMPT #131QG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,561 hrs · 17,469 cycles

FWD CARGO COMPT #131KG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 31,561 hrs · 17,469 cycles

THE #147CF KEEL BEAM FLOOR WAS FOUND SOFTEN AND CAUSE BY HYD FLUID CONTAMINATION FABRICATED FLOOR PANEL #147CF I.A.W FEDEX DWG SRZ-25-005 REV.R

Part: ISOLATION VALVE — LEAKING (HYD SYSTEM) · airframe 31,249 hrs · 17,278 cycles

PDIS 682 29-10 9603 08JUN21 JFK OPEN U AT FL 240 RECEIVED ECAM WARNING FOR YELLOW HYD SYSTEM LO PRESSURE. AFTER ANALYZING WE FOUND LOSS OF ALL YELLOW HYDRAULIC FLUID. RAN QRH, DECLARED EMERGENCY AND LANDED. AMM: 27-14-21-04 REMOVED AND REPLACED YELLOW ISOLATION VALVE LOCK AS PER M.M. 27-14-21-04. OPS CHECK ANDLEAK OK. RAN BOTH ENGS AND EXCERSISED FLT CONTROLS TO BLEED SYS. SERVICED HYD SYS TO HOP HAT M.M. 12-12-29-00 AND RE- EXCERSIDED FLT CONTROLS.

Part: MANIFOLD — CRACKED (HYDRAULIC SYS) · airframe 29,312 hrs · 16,120 cycles

ABOUT 15-20 MINS AFTER LEVEL OFF AT 350FL WE NOTICED THAT THE GREEN HYD LEVEL WAS LOW. 10 MINS LATER WE GOT A GREEN LOW FLUID LEVEL ON THE ECAM. FOLLOWED PROCEDURES AND SECURED THE GREEN SYSTEM. DURING THE REST OF THE FLIGHT WE RECIEVED MANY GREEN LOW LEVEL ECAM ALERTS. HAND CRANKED THE LANDING GEAR DOWN. AFTER LANDING THE GREEN SYSTEM SHOWED NORMAL FLUID LEVELS. COMPLETED SWAPOVERS AND INSTALL OF THE GREEN SYSTEM HP MANIFOLD PER AMM 29-11-12-04. OPS CHECK AND LEAK CHECK GOOD.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 251WG HAS CRACK. FABRICATED NEW FLOOR PANEL 251WG ON T19/1403084 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CABIN FLOOR PANEL 231QG IS BROKEN FABRACATED NEW FLOOR PANEL 231QG ON T19/1403671 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 241HK DAMAGED. FABRICATED NEW FLOOR PANEL 241HK ON T19/1402897 IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 252VF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252VF ON VT MAE TRAVELER T19/1403082 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 262AH DAMAGED. FABRICATED NEW FLOOR PANEL 262AH ON T19/1402900 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 252TH HAS CRACK. FABRICATED NEW FLOOR PANEL 252TH ON T19/1403191 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 252GF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252GF ON VT MAE TRAVELER T19/1403192 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 242ZH HAS CRACK. FABRICATED NEW FLOOR PANEL 242ZH ON T19/1403081 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 241TH DAMAGED FABRICATED NEW FLOOR PANEL 241TH ON T19/1402672 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CABIN FLOOR PANEL 261XF AFT INBD INSERT PULLED THROUGH PANEL. FABRICATED NEW FLOOR PANEL 261XF ON T19/1403254 IAW DWG SRZ-25-005 MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 261AH DAMAGED. FABRICATED NEW FLOOR PANEL 261AH ON T19/1402899 IAW SRZ-25-005 DWG. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 242FJ HAS DAMAGE. FABRICATED NEW FLOOR PANEL 242FJ ON T19/1402954 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO FLOOR PANEL 242FK HAS CRACK. FABRICATED NEW FLOOR PANEL 242FK ON T19/1402894 IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 241QH DAMAGED. FABRICATED NEW FLOOR PANEL 241QH ON T19/1402895 IAW SRZ-25-005. CAT ""A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242MF DAMAGED. FABRICATED NEW FLOOR PANEL 242MF ON T19/1402952 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 28,411 hrs · 15,582 cycles

MAIN CABIN SEAT TRACK LBL 450 BETWEEN FR63 AND FR64 SCALLOP BROKEN. REPAIRED SEAT TRACK WITH #A53274005-SFS-DAP BATCH #0003335892 AND SEAT TRACK SPLICES (4EA) #R5327049020000 BATCH 0003391773. IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242EK DAMAGED. FABRICATED NEW FLOOR PANEL 242EK ON T19/1402677 IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242GF DAMAGED. FABRICATED NEW FLOOR PANEL 242GF ON VT MAE TRAVELER T19/1402671 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242RG DAMAGED. FABRICATED NEW FLOOR PANEL 242RG ON VT MAE TRAVELER T19/1402896 IAW SRZ-25-005 CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 20) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 251WH DAMAGED FABRICATED NEW FLOOR PANEL 251WH ON VT MAE TRAVELER T19/1402377 IAW DWG SRZ-25- 005 CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 252WH DAMAGED. FABRICATED NEW FLOOR PANEL 252WH ON T19/1402379 IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242BF DAMAGED. FABRICATED NEW FLOOR PANEL 242BF ON T19/1402893 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 252RH DAMAGED. FABRICATED NEW FLOOR PANEL 252RH ON T19/1402378 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,411 hrs · 15,582 cycles

MAIN CARGO DECK FLOOR PANEL 242KF DAMAGED FABRICATED NEW FLOOR PANEL 242KF ON T19/1402380 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231NG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL 231NG IAW DWG SRZ-25-005 REV N AND GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231ZG HAS DAMAGE TO HONEYCOMB CORE AT PANEL EDGE. FABRICATED NEW FLOOR PANEL 231ZG IAW DWG SRZ-25-005 REV N AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO FLOOR PANEL 232BH HAD IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005, REV N, AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO FLOOR PANEL 231LG HAD IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005, REV N, AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO FLOOR PANEL 232CF HAD IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005, REV N, AND GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,727 hrs · 15,164 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 232VH HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL 232VH IAW DWG SRZ-25-005 REV N AND GMM 7-0-1000.

Part: MONITOR — MALFUNCTIONED (HYDRAULIC SYS) · airframe 27,580 hrs · 15,074 cycles

SHORTLY AFTER TAKE OFF FROM AFW RECEIVED ECAM FOR YELLOW SYSTEM RSV OVERHEAT. COMPLIED WITH ECAM AND CHECK LIST OVERHEAT LIGHT REMAIN ON UNTIL AFTER LANDING AT LAX. R&R RESERVOIR OVERHEAT MONITORING UNIT, OP TESTS GOOD. RAN ENGINE AND NO FAULTS. REF MM 29-33-12-04, MM 29-33-00-05, JRH CHP 5/6, TSM 29-33, ASM 29-33-00, IPC 29-33-01-01 ITEM 050.

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 25,604 hrs · 13,946 cycles

AFTER LANDING, RECEIVED AN AVIONICS SMOKE WARNING, FOLLOWED BAY AN ECAM AND DID NOT DETECT SMOKE. CONTINUED TO THE GATE. R & R AVIONICS SMOKE DETECTOR 13WA, PERFORMED A SYSTEM TEST, AND FOUND TO BE OK IAW MM 26-15-21-04. ACFT OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FRAME 40) · corrosion level 2 · airframe 25,281 hrs · 13,765 cycles

MAIN DECK SEAT TRACK SUPPORT CORRODED AT FRAME 40 BETWEEN Y2462 AND Y1959. REMOVED AND REPLACED THE SEAT TRACK SUPORT IAW SRM 51-40-21. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,281 hrs · 13,765 cycles

MAIN CARGO DECK FR27 TO FR28 UNDER PANEL 231HH SEVERAL SPOTS OF CORROSION AROUND BOTH ADAPTERS AND SEVERAL SPOTS ON DECK PLATE. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS L=1.75 W=1.5 D=.017 FOUND TO BE OUT OF LIMITS IAW SRM 53-13-15. R&R DECK PLATE IAW SRM 51-40-21. FABRICATED DECK PLATE FROM 2024-T3.080C BATCH 0002962014 IAW SRM 53-14-15 FIG 5 ITEM 65. MAJOR REPAIR

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242QJ BROKEN. FABRICATED FLOOR PANEL 242QJ IAW SRZ 25-00. CLASSIFIED AS A CAT"A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242VJ BROKEN. MAIN CABIN FLOOR PANEL 242VJ FABRICATED IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 132MG IS CRACKED. FABRICATED FLOOR PANEL 132MG FWD CARGO COMP IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 251UH BROKEN. MAIN CABIN FLOOR PANEL 251UH FABRICATED IAW SRZ-25-005. MAJOR REPAIR.

Part: THRUST PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,281 hrs · 13,765 cycles

MAIN DECK BETWEEN FR28 AND FR31 AND FROM Y2462 TO Y1959, THRUST PLATE AND SEAT TRACK ADAPTER BASE CORRODED. REMOVED CORROSION ON THRUST PLATE AND ADAPTER BASE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS. NO ESTABLISHED LIMITS. REMOVED AND REPLACED 2EA THRUST PLATES IAW SRM 51-40-21.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 132KG IS CRACKED. FABRICATED FLOOR PANEL 132KG IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 25,281 hrs · 13,765 cycles

COURIER FLOOR PANEL 221QF HAS MULTIPLE AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 221QF ON T16/1235361 IAW DWG SRZ-25-005. CLASS "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242ZJ BROKEN. MAIN CABIN FLOOR PANEL 242ZJ FABRICATED ON T16/1234519 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 251YG BROKEN. MAIN CABIN FLOOR PANEL 251YG FABRICATED ON T16/1235068 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242TH BROKEN. FABRICATED FLOOR PANEL 242TH ON T16/1235066 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241WH BROKEN. MAIN CABIN FLOOR PANEL 241WH FABRICATED ON T16/1235069 IAW SRZ-25-005. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 25,281 hrs · 13,765 cycles

NR 2 ENG FWD MOUNT FITTING (PYRAMID) INBD AFT BOLT HOLE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 54-51-81. OVERSIZED HOLE TO 25.323MM, HFEC INSPECTED, CAD PLATED BOLT HOLE, FABRICATED BUSH ON T16/1235747 AND INSTALLED IAW SRM 54-51-81. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242UJ BROKEN. MAIN CABIN FLOOR PANEL 242UJ FABRICATED ON T16/1235065 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242SF BROKEN. MAIN CABIN FLOOR PANEL 242SF FABRICATED ON T16/1235067 IAW SRZ-25-005. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 25,281 hrs · 13,765 cycles

NR 1 ENG FWD MOUNT FITTING (PYRAMID) INBD AFT BOLT HOLE CORRODED REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 54-51-81, OVERSIZED BORE TO 25.323MM, HFEC INSPECTED AND NO CRACK INDICATIONS NOTED. CAD PLATED AND PRIMED BORE, FABRICATED BUSH ON T16/1235749 AND INSTALLED IAW SRM 54-51-81. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 232DF BROKEN. FABRICATED FLOOR PANEL 232DF IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241WJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 252UH BROKEN. FABRICATED FLOOR PANEL 252UH IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241VH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241TH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 10) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 232RG BROKEN. FABRICATED FLOOR PANEL 232RG IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 231FH BROKEN. FABRICATED FLOOR PANEL231FH IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — DAMAGED (ZONE 20) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241GJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 232FF BROKEN. FABRICATED FLOOR PANEL 232FF IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241MJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 231EH BROKEN. FABRICATED FLOOR PANEL 231EH IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 251XH BROKEN. FABRICATED FLOOR PANEL 251XH IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 241ZJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 252AH BROKEN. FABRICATED FLOOR PANEL 252AH IAW SRZ-25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 231CF BROKEN. FABRICATED FLOOR PANEL 231CF IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 232TG BROKEN. FABRICATED FLOOR PANEL 232TG IAW SRZ-25-005. CAT"A" MAJOR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 25,281 hrs · 13,765 cycles

MAIN CABIN FLOOR PANEL 242GJ BROKEN. FABRICATED FLOOR PANEL 242GJ IAW SRZ-25-005. CAT "A" MAJOR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 132SG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 131KG IS CRACKED FABRICATED FWD CARGO FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 131LG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 25,281 hrs · 13,765 cycles

AFT CARGO FLOOR PANEL 151SF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

FWD CARGO FLOOR PANEL 132RG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 25,281 hrs · 13,765 cycles

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

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 25,281 hrs · 13,765 cycles

AFT CAGO FLOOR PANEL 152RF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 25,281 hrs · 13,765 cycles

AFT CARGO FLOOR PANEL 151TF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (FRAME 25) · airframe 25,281 hrs · 13,765 cycles

MAIN CARGO DECK BETWEEN SEAT TRACKS 1 AND 2R AT FRAME 25, HAS CORROSION ON MAIN DECK PANEL. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS ON DECK PLATE IAW SRM 53-13-15. REMOVED PANEL IAW SRM 51-40-21 AND STIFFNER. FABRICATED PANE IAW SRM 53-13-15 ITEM 60. INSTALLED A NEW PANEL AND STIFFNER IAW SRM 51-40-21. MAJOR REPAIR

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN DECK) · airframe 25,188 hrs · 13,708 cycles

MAIN DECK CARGO SMOKE, AFT COMPARTMENT INDICATION. COMPLIED WITH ECAM AND WARNING EXTINGUISHED. NO EXCESSIVE TEMPS ON ECAM AIR CONDITION PAGE. VISUAL INSPECTION REVEALED NO SMOKE ON MAIN DECK. ACCESSED AFT MAIN CARGO DECK. NO EVIDENCE OF SMOKE WAS PRESENT. INSPECTED AND CLEANED SMOKE DETECTOR AIR INTAKE FILTERS IAW AMM 26-19-13-06-0. PERFORMED MAIN DECK CARGO COMPARTMENT SMOKE DETECTION SYSTEM ADJUSTMENT AND TEST IAW AMM 26-19-00-05-0. NO DEFECTS NOTED. NO 90 DAY HISTORY. ACFT OK FOR SERVICE.

Part: COMPUTER — FAULTED (LE SLAT) · airframe 239 hrs · 13,041 cycles

ON APPROACH ON SLAT EXTENSION 1 & 2 SLATS & FLAPS FAULT, CYCLED NO HELP. WHILE PERFORMING QRH PROCEDURE SLAT & FLAPS EXTENDED NORMALLY. DURING POST FLIGHT CHECKS FOUND FAULTS ON BOTH SFCC'S. SFCC 1 & SFCC 2, BOTH INDICATED SLAT JAM. RESET BOTH SFCC'S & CYCLED SLATS & FLAPS TO FULL EXTENSION & BACK TO RETRACTED, NO FAULT. SFCC 1 & SFCC 2 PRECAUTIONARY RE-RACKED IAW SPM & AMM 27-51-18-04. SLAT & FLAP EXTENSION & RETRACTION CUT OUT, NO FAULTS. OK FOR SERVICE. RESET SFCCS, OPERATED SLATS & FLAPS WITH NO FAULTS FOUND.

Part: RIB — CORRODED (LT WING) · airframe 232 hrs · 12,656 cycles

LEFT MLG FWD LUG HAS CORROSION ON BOTH FACES & BORE COMPLIED WITH EA 6-5710-T0316549, REPAIR OF RIB 5 FWD LUG LT.

Part: RIB — CORRODED (RT WING) · airframe 232 hrs · 12,656 cycles

RIGHT MLG FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0316574 REV NO POS P1.

Part: HOSE — CRACKED (FIRE BOTTLE) · airframe 232 hrs · 12,648 cycles

DG EXTINGUISHER HOSES NR 1 & 3, CRACKED & COLLAPSING WHERE HOOKED TO DG CAN & NEED TO BE REPLACED. R & R HOSES NR 1 & 3 IAW AMM 26-28-00, OK FOR SVC.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 22,333 hrs · 12,147 cycles

RIGHT WING AILERON UPPER SURFACE HAS ONE DENT 5.5 INCHES FROM AFT SIDE & 6 INCHES FROM INBD SIDE. IAW NTM 51-10-08 CHECK FOR CRACK & NO CRACK FOUND. TAP TEST INSPECT THE DENT & FOUND DELAMINATION 20MMX20MM IAW SRM 57-61-11 & SRM 51-77-12 PARA 4 D REMOVE THE DISBONDED SKIN & PREPARE THE EXTERNAL DOUBLER & INSTALLED THE DOUBLER.

Part: SKIN — DAMAGED (LT WING) · airframe 22,333 hrs · 12,147 cycles

LEFT PYLON AFT FAIRING LOWER GREEN HYD TUBE CONNECTOR LOOSED AT WING SKIN POS. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORKED AREA AND NO CRACK FOUND PER A300-600 NTM51-10-08. MANUFACTURE A FREEZE PLUG BUSH AND TWO STEEL RETAINING WASHERS AND INSTALLED THE FREEZE PLUG BUSH & THE TWO WASHERS PER REPAIR DRAWING: R57150532 ISSUE A & EA6-5730-T0309578 B PART1. THIS IS A CATEGORY B REPAIR.

Part: SKIN — DAMAGED (RT WING) · airframe 22,333 hrs · 12,147 cycles

RIGHT ENG PYLON AFT FIRING ONE HYD TUBE LOOSED. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORKED AREA AND NO CRACK FOUND PER A300-600 NTM51-10-08. MANUFACTURE A FREEZE PLUG BUSH AND TWO STEEL RETAINING WASHERS AND INSTALLED THE FREEZE PLUG BUSH & THE TWO WASHERS PER REPAIR DRAWING: R57150532 ISSUE A & EA6-5730-T0309579 PART1. CATEGORY B REPAIR.

Part: SKIN — DAMAGED (LT WING) · airframe 22,333 hrs · 12,147 cycles

LEFT PYLON AFT FAIRING LOWER BLUE HYD TUBE CONNECTOR LOOSED AT WING SKIN POS. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORKED AREA AND NO CRACK FOUND PER A300-600 NTM51-10-08. MANUFACTURE A FREEZE PLUG BUSH AND TWO STEEL RETAINING WASHERS AND INSTALLED THE FREEZE PLUG BUSH & THE TWO WASHERS PER REPAIR DRAWING: R57150532 ISSUE A & EA6-5730-T0309578 B PART1. THIS IS A CATEGORY B REPAIR.

Part: GCU — FAILED (NR 1 ENGINE) · airframe 22,198 hrs · 12,076 cycles

LOST AC BUS NR 2 IN FLIGHT 5 MIN AFTER T/O AT 8,000'. RETURNED TO KMEM. R & R NR 1 ENG GCU IAW AMM ATA 24-22-12-04. OPERATIONS CHECKED GOOD ON ENG RUN IAW A300-600 JRH. .

Part: UNKNOWN — UNKNOWN (ELECTRICAL) · airframe 22,197 hrs · 12,075 cycles

ON ARRIVAL, LOST AC BUSS 2 AND ALL ASSOCIATED EQUIPMENT & FLIGHT CONTROLS. NOT ABLE TO RESET ANYTHING. ACFT FLOWN ON GEN 1 & APU GEN ENTIRE FLT IAW MEL 24-11-01-A. SUGGEST GEN 2 IS NOT THE PROBLEM. PERFORMED TROUBLESHOOTING PROCEDURES TO AC BUSS NR 2, FOUND NO DISCREPANCIES OR FAULTS, AS A PRECAUTION, REMOVED AND REPLACED RELAY 14XU AND CONTROL-AC 10XU, PERFORMED SYS OPS CHECKED NORMAL, ALL IAW ASM 24-22-00, AMM 24-22-15-04, & 24-27-00-05.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 22,046 hrs · 11,984 cycles

NR 2 FUEL FILTER CLOG ECAM & AMBER FUEL CLOG LIGHT ILLUMINATED ON CTR ENGINE PANEL. FOLLOWED ECAM, QRH & LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-11-04. OPS AND LEAK CHECKED GOOD IAW AMM 71-00-00-05.

Part: TRU — FAILED (NR 2) · airframe 21,860 hrs · 11,863 cycles

ON FINAL APPROACH TO KMEM, FIRST OFFICER`S INSTRUMENTS LOST ALONG WITH SPOILERS, NR 2 PITCH TRIM, NR 2 YAW DAMPER, FIRST OFFICER`S WINDOW HEAT LOSS WAS ONLY MOMENTARY. SHORTLY FOLLOWED BY ELEC ODOR IN THE COCKPIT. DECLARED EMERGENCY & LANDED. DURING FLIGHT CREW DEBRIEF, NOTICED BOTH FIRST OFFICER`S SIDE PFD & SFD WORKING NORMALY. FOUND 3 FAULTS IN MTP BOX, DISPLAY BUTTON, FCC NR 1, RA 3, FLAG 26 & VAC POWER SUPPLY 2 LOST. ALSO FOUND TR NR 2 FAULT ON MTP. ALL LIGHTS IN THE COCKPIT WORKED AS ADVERTISED. R&R TR 2 PU. OPERATIONS CHECKED NORMAL IAW AMM 24-32-11-04 PERFORMED AFS LAND TEST IAW MM 22-40-00-5, LAND TESTED OK.

Part: TRANSDUCER — FAILED (BRAKES) · airframe 21,204 hrs · 11,475 cycles

CONFIGURED FOR LANDING, AT MED AUTOBRAKES SELECTION, ECAM AUTO BRAKE FAULT ILLUMINATED. DESELECTED AND RESELECTED WITH SAME RESULT., GO AROUND AND DIVERTED FOR TROUBLESHOOTING. AT GEAR EXTENSION, SAME RESULT. ACCOMPLISHED BITE CHECK OF BSCU IAW TSM 32-42-00. FAULT CODE FOUND-091. IAW TSM CODE INDICATES LT PRESSURE TRANSDUCER 1 EQUIP NR 91GG. R & R THE NORMAL BRAKE PRESSURE TRANSDUCER, RAN HYDRAULICS AND HAD NO LEAKS. ACCOMPLISHED THE NORMAL BRAKING OPS TEST, REF AMM 32-42-00-05, AND BITE TEST OF BSCU, REF AMM 32-42-00-05. ACFT OK TO CONTINUE.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 19,363 hrs · 10,416 cycles

ON ARRIVAL, FOUND LARGE AMOUNT OF FUEL DRAINING FROM DRAIN MAST OF NR 1 ENGINE. OPENED NR 1 ENGINE CORE COWL AND FOUND MAIN FUEL LINE SPRAYING FUEL AT THE FIREWALL CONNECTION. PULLED FIRE HANDLE AND DISCONNECTED FUEL LINE AT THE FIREWALL AND FOUND RETAINER RING BENT. NEEDS NEW FUEL LINE ASSY FROM FUEL PUMP TO FIREWALL AND BOTH GASKETS. PULLED AND TAGGED NR 1 ENGINE FIRE BOTTLE AND SQUIB C/B. PULLED AND TAGGED IGN C/B. FIRE HANDLE REMAINS PULLED. NR 1 RT FAN COWL AND CORE COWL REMAIN OPEN. BAGGED FUEL LINE AT PYLON AND ATTACHED HARWARE BAG TO THE FUEL LINE. REPLACED MAIN FUEL SUPPLY LINE REF M/M 73-12-04-04, RAN ENGINE REF JRH CHECKED NORMAL. R & R LINE, LEAK CHECKED OK.

Part: SKIN — DAMAGED (AILERON) · airframe 19,294 hrs · 10,379 cycles

RT WING ALL SPEED AILERON LOWER SURFACE PUNCTURED AT T/E 23" FROM OTBD EGDE 0.10 DEEP, REF AMM 27-10-00-06M, REPAIRED PUNCTURE ON LOWER SURFACE OF R/T WING ALL SPEED AILERON, ALODINED PRIMED, AND TOP COAT REPAIR IAW SRM 51-77-12 4C, 51-21-10 AND 51-75-10 AND SRM 57-61-11, PARA 4E AND EA6-5750-156099 PT1.

Part: DOOR FRAME — GOUGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO COMPT DOOR FRAME AT FR20A, 6 IN LONG GOUGE APPROX 1 INCH WIDE. COMPLIED WITH EA 6-5310-156091 PART 1.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

UPON REMOVAL OF THRUST PLATE BETWEEN FR26-27, SEAT TRACK 4R AND 3R, FOUND 3 ELONGATED HOLES ON OTBD FLANGE OF SEAT TRACK AT SPLICE POINT, 1 EA DRILL START, AND REPAIR SPLICE UPPER FLANGE IS BENT. REPAIR SPLICE AND SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 103, FIG 101. PERFORMED SEAT TRACK SPLICE REPAIR BETWEEN FR 26 AND FR 30, -Y953 IAW SRM 53-10-16, PG 207/208, AND SRM 51-23-10 PG 20.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 19,294 hrs · 10,379 cycles

RIGHT WINGLET T/E INBD STATIC DISCHARGER HAS CORROSION EXTENDING FROM UNDERNEATH THE BASE ESTIMATED DEFECT MEASURES 4 SQ IN, REMOVED LEVEL 1 CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-30-11. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR IAW SRM 57-30-11. MINOR REPAIR IAW GMM 6-2-100.

Part: THRUST PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR THRUST PLATE BETWEEN FR 26 AND FR27 AND -Y450 TO -Y 953 (SEAT TRACK 2R AND 3R), HAS .5 INCH OF CORROSION. THRUST PLATE FOUND TO BE OUT OF LIMITS IAW DWG A53781984. R & R THRUSTPLATE IAW SRM 51-40-21, PARA 5 AND DWG A53781984.

Part: SEAT TRACK — DISTORTED (FUSELAGE) · airframe 19,294 hrs · 10,379 cycles

MDCC SEAT TRACK 5L DISTORTED BELOW INBD FLANGE FR 20 DEFECT MEASURES 10" LONG. REPAIRED IAW EA6-5310-157810 PT 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

SEAT TRACK 2L AT FRAME 29 HAS WORN SCALLOPS APPROX 2EA AREA 1". CUT AND REPAIRED MDCC SEAT TRACK 2L BETWEEN FRAMES 26 AND 30 IAW SRM 53-10-16.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 19,294 hrs · 10,379 cycles

LEFT WING INBD FLAP HAS 4EA DENTS AT LOWER SURFACE BETWEEN RIBS 14A AND 15 APPROX 4", 15", 25", AND 26" AFT OF AFT SPAR. REPAIRED IAW EA 6-5750-156093.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FRAME 31 BETWEEN SEAT TRACK 2R AND 3R HAS A .25" CRACK AT UPPER MILLSTEP IN RADIUS FWD FACE. REPAIRED CRACK ON FRAME 31 BETWEEN SEAT TRACKS 2R AND 3R IAW FSRM 53-10-15.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBEAM FRAME 30 BETWEEN SEAT TRACKS 2R AND 3R HAS A 1" CRACK AT UPPER MILLSTEP IN RADIUS OF FWD FACE. REPAIRED IAW FSRM 53-10-15 PAGES 393-399, FIG 212.

Part: FLOORBOARD — CRACKED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 151JH HAS 1 BROKEN CORNER AND 15 CRACKS ALONG BOTTOM OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBEAM AT FRAME 28 BETWEEN SEAT TRACKS 2R AND 3R HAS A 1" CRACK AT UPPER MILLSTEP IN RADIUS FWD FACE. REPAIRED CRACKED MILLSTEP ON FRAME 28 IAW FSRM 53-10-15, PAGES 393-399 FIG 212.

Part: BRACKET — CORRODED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR THRUST PLATE BETWEEN SEAT TRACK 3R AND 4R AND FR 26 AND FR 27 HAS 3 EA 1 SQ IN, AREAS OF CORROSION. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND THRUST PLATE TO BE OUT OF TOLERANCE IAW DWG A53781984, REV A, AND SRM 51-73-11. REMOVED, FABRICATED REPLACEMENT, AND REPLACED THRUST PLATE AT FR 26 -FR 27, -Y953 TO -Y1456 IAW DWG A53781984, REV A, AND SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

UPON REMOVAL OF BULK CARGO BAY FLOOR STRUCTURE FOAM TAPE, CORROSION WAS FOUND ON "T" EXTRUSION FLOORBEAM UPPER SURFACE AT FR 66, FROM Y250 TO Y375 (APPROX. 8 SQ IN TOTAL) AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, PG 115. R & R FLOORBEAM AT FR 66 FROM Y1375 TO -Y1375 IAW SRM 51-72-10, PG 2.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC SEAT TRACK 5R BETWEEN FR 47 AND FR 51 HAS 6 EA GOUGES AT FLANGE ON INBD SIDE, AROUND FASTENER HOLES. (NOTE: HOLES ELONGATED AND CHAFED BEYOND 50 PERCENT OF FLANGE THICKNESS) AFTER REMOVAL OF GOUGES, FOUND 5 OF 6 AREAS TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED, FABRICATED REPLACEMENT, AND REPLACED SEAT TRACK FR 45 TO FR 54 AT-Y1959, IAW DWG A53832211 AND SRM 51-72-10.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 241JF CRACKED 2EA AT LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD 241JF IAW DWG SRZ 25-005 REV. J

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 232 JG IS CRACKED AT CUTOUT APPROX 9". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO FLOORBOARD 132 QG HAS IMPACT DAMAGE AT LWR SURF TOTAL DEFECT MEASURES 60 IN LONG W/PUNCTURE. FABRICATED FLOORBOARD 132 QG IAW DWG SRZ 25-005 REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR PANEL 242 RG HAS 3 EA CRACKS 2" TO 8" CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL 242 RG IAW DWG SRZ 25-005, REV J.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,294 hrs · 10,379 cycles

MDCC RT SEAT TRACK 4 R OTBD FLANGE FRAME 28 HAS 1" SQUARE CORROSION AFTER CORROSION REMOVAL AREA FOUND TO BE OUT OF LIMITS. ORIGINAL ALLOWABLE MAX DAMAGE IS 0.12 AFTER REMOVAL IS 0.017. CUT SECTION OF SEAT TRACK OUT AT MDCC RT 4R OTBD FLANGE FR 26-FR 30 ALONG WITH THE REMOVAL OF 2 EA PRODUCTION SPLICES AND 4 EA SPLICE CHANNELS. FABBED NEW SEAT TRACK AND 2 EA SPLICES. ALL PARTS INSTALLATED ON ACFT IAW SRM 53-10-16 AND 51-21-10 AND 51-75-10.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 19,294 hrs · 10,379 cycles

LT WING INBD FLAP LOWER SURFACE DENT 1EA BETWEEN RIB9A-RIB10 AND STR 2.1-STR 2.2, APPROX D=0.5" & D=0.010". DENT OUT OF LIMITS IAW A300-600 SRM 57-50-00 FIG 101 P 107. CUTOUT DENT FABRICATED REPAIR DOUBLER 8.5X14.0 INCHES. LOCATED AND DRILLED AND INSTALLED IAW SRM 57-50-00 FIG 205.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO COMPT FLOORBOARD 132 NG HAS IMPACT DAMAGE AT ENTIRE OUTER EDGE. FABRICATED FLOORBOARD 132NG IAW DWG, SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO COMPT FLOORBOARD 132 RG HAS BROKEN MATERIAL AT OUTER EDGE OF ENTIRE FLOORBOARD. FABRICATED REPLACEMENT FLOORBOARD 132, RG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 151FG HAS 15 PUNCTURES ON BOTTOM OF PANEL. FABRICATED REPLACEMENT FLOORBOARD FG IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FLOOR PANEL 152 WF HAS ONE BROKEN CORNER AND 5 PUNCTURES IN BOTTOM OF PANEL, FABRICATED REPLACEMENT FLOOR PANEL 152 WF IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR PANEL 231 FF HAS 40" SQ IN OF UPPER SURFACE DELAMINATION WITH 2" PUNCTURE DAMAGE AND 5 " EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 231 FF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 151 DL HAS SEVERAL AREAS THAT ARE CRUSHED. FABRICATED REPLACEMENT FLOORBOARD 151DL IAW SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

KEEL BEAM FLOODBOARD 147EF HAS EDGE ON 3 SIDES WITH DELAMINATED AND SKYDROL INTRUSION, 60 SQ IN APPROX. FABRICATED FLOORBOARD 147 EF, DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 151 WF 15 PUNTURES AND ALL CORNERS CRUSHED. FABRICATED REPLACEMENT FLOORBOARD 151WF IAW DWG SRZ 25-005, REV J.

Part: RETAINER — CRACKED (ZONE 600) · airframe 19,294 hrs · 10,379 cycles

RT WING L/E RIB 8 HAS A .75 INCH CRACK EXTENDING FROM RECEPTICAL. REPAIRED LANDING ON RT WING L/E RIB 8 RECEPTICAL IAW SRM 57-41-12, SECTION 3 H,J,K, AND N.

Part: THRUST PLATE — CORRODED (FUSELAGE) · airframe 19,294 hrs · 10,379 cycles

MDCC THRUST PLATE AT FRAME 28 - 28 HAS 1" OF CORROSION BETWEEN SEAT TRACKS 4R AND 5R. REMOVED CORROSION IAW SRM 51-74-10, MATERIAL LOSS OUT OF TOLERANCE IAW DWG A53781986. R & R THRUST PLATE IAW FSRM 51-72-10 PAGES 1 THRU 3.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 19,294 hrs · 10,379 cycles

R1 DOOR BOTTOM FWD, SCUFF PLATE NUTPLATE RETAINER HAS A .5 IN CRACK AT FWD END. R & R RETAINER R-1 DOOR SILL AREA IAW FSRM 51-72-10 AND 51-40-21, PARA 5 AND 6.

Part: FLOORBOARD — CRACKED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 152 JG, HAS 11 CRACKS ON BOTTOM OF PANEL AND 2 CORNERS BROKEN. FABRICATED REPLACEMENT FLOORBOARD 152 JG IAW DWG SRZ 25-005.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

CARGO COMPT FLOORBOARD, 132 SG HAS BROKEN EDGE FILLER, IMPACT DAMAGE AT LWR SURFACE TOTAL DEFECT 10 IN LONG. FABRICATED REPLACEMENT FLOORBOARD 132 SG IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR PANEL 242 SF HAS 2 EACH CRACKS AT CLS CUTOUT ARROX 8" LONG FABRICATED REPLACEMENT FLOOR PANEL 242SF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 241 GF BROKEN INTO 2 PIECES FABRICATED FLOORBOARD 241 GF IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOOR PANEL 231 YG HAS 1 AREA CRUSHED WERE CLEVIS ATTACHES. FABRICATED FLOOR PANEL 231 YG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 242PF, BROKEN AT 2 PLACES AND TEFLON SEAL TORN. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN CABIN FLOORBOARD 232 CF HAS A CRACK IN COMPOSITE SKIN. FABRICATED REPLACEMENT FLOORBOARD 232 CF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO COMPT FLOORBOARD 132MG HAS IMPACT DAMAGE. TOTAL DEFECT, 50" LONG. FABRICATED FLOORBOARD 132 MG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 232 YG HAS 3 6" CRACKS A CLEVIS ADAPTERS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD 232 YG IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOOR PANEL 241 RJ END SECTION OF PANEL IS BROKEN OFF FABRICATED REPLACEMENT FLOOR PANEL 241 RS IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 251 RG HAS 1" CRACK AT CLEVIS CUTOUT AND .5" PUNCTURE SAME AREA FABRICATED REPLACEMENT FLOORBOARD 251 RG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 242 QJ HAS 4 AREAS CRUSHED WERE CLEVIS ATTACHES FABRICATED FLOORBOARD 242 QJ IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

FWD CARGO COMPT FLOORBOARD 132 PG CRACKED 25" LONG AT UPPER SURFACES. FABRICATED FLOORBOARD 132 PG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 242 MF HAS 7 EA CRACKS AROUND 4 EA CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOORBOARD 242 MF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 242 BF CRACKED AT 4 PLACES AND PUNCTURES AT 1 PLACE UPPER AND LOWER SURFACE. FABRICATED FLOORBOARD 242 BF IAW DWG SRZ 25-005, REV J.

Part: SKIN — CRACKED (ZONE 500) · airframe 19,294 hrs · 10,379 cycles

LT WING L/E LOWER SURFACE HAS A CRACK APPROX .5" IN LENGTH AT PANEL 513AB CUTOUT FWD FACE. REPAIRED LT WING FIXED L/E LOWER SURFACE AT PANEL 513AB CUTOUT IAW FSRM 53-15-63, FIG 201, SHEET 3.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 252 VF CRACKED AT UPPER SURFACE 3 EA. FABRICATED FLOORBOARD 252 VF IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR PANEL 242 VG HAS 3 EA 8" CRACKS AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL 242 VG IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

AFT CARGO FLOORBOARD 151 VF HAS A SECTION 1 IN BY 10 IN BROKEN OFF AT EDGE FABRICATED REPLACEMENT FLOORBOARD 151 VF IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FLOOR PANEL 241 WH HAS 3 SECTION THAT ARE CRUSHED WHERE CLEVIS ATTACHES. FABRICATED FLOOR PANEL 241 WH IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR PANEL 232 NG HAS TWO, ONE INCH CRACKS AROUND CLEVIS ADAPTER CUTOUTS FABRICATED FLOOR PANEL 232 NG IAW DWG SRZ 25-005.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK, FR 43 TO 54 SEAT TRACK, 5L HAS 17 EA, NUT CLIP HOLES THAT HAVE CHAFING MARKS AROUND FASTENER HOLES. R & R SEAT TRACK SECTION 5L IAW DWG A53832211 AND SRM 51-40-21, PG 19, FIG 5 AND PG 26, FIG 9.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 231 ZG CRACKED AT UPPER AND LOWER SURFACES AND 2 EA SCREW HOLES CRUSHED. FABRICATED REPLACEMENT FLOORBOARD 231 ZG IAW DWG SRZ 25-005.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FWD FUSELAGE UPPER DECK FRAME 12A 18" LEFT OF CENTERLINE, FLOOR SUPPORT HAS 2 SQ" OF CORROSION. AFTER REMOVAL OF LEVEL 1 COROSION FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-10 AND REPROTECTED IAW SRM 51-75-10.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FLOOR PANEL 241QH CENTER SECTION WERE CLEVIS ATTACHES IS CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL 241 QH IAW DWG SRZ 25-005, REV J.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FWD FUSELAGE UPPER DECK, FR 12A PLUS 18",48" LEFT OF CENTERLINE FLOOR SUPPORT HAS 1 SQ IN OF CORROSION AROUND FASTENER HOLE.

Part: FLOORBOARD — CRACKED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

AFT CARGO FLOORBOARD 151 X F HAS 2 EA CRACKS ALONG EDGE 2 IN LONG ON BOTTOM SIDE FABRICATED REPLACEMENT FLOORBOARD 151 XF IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FLOOR PANEL 241 AJ, 3 SECTIONS WHERE CLEVIS ATTACHES ARE CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL 241 AJ IAW DWG, SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOOR PANEL 242 UJ HAS 5 AREAS THAT ARE CRUSHED WHERE CLEVIS ATTACHES. FABRICATED REPLACEMENT FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,294 hrs · 10,379 cycles

MDCC SEAT TRACK 3L BETWEEN FR 57 AND 57 - 1 HAS 2 EA WORN SCALLOPS. REMOVED CORROSION IAW SRM 51-74-10, AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-10-16.

Part: FLOOR SUPPORT — CORRODED (UPPER DECK) · airframe 19,294 hrs · 10,379 cycles

FWD FUSELAGE UPPER DECK, FR 12A, PLUS 18", 28" LT OF CENTERLINE. FLOOR SUPPORT HAS 1 SQ" OF CORROSION AROUND FASTENER HOLE. AFTER REMOVAL OF LEVEL 1 CORROSION FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11 PG 1. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-10

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MACC FLOOR PANEL 241 GJ HAS 2 EA, 8" CRACKS CLEVIS ADAPTER CUTOUT FABBED FLOOR PANEL 241 GJ IAW DWG SRZ 25-005, REVJ.

Part: SEAT TRACK — GOUGED (MAIN DECK) · airframe 19,294 hrs · 10,379 cycles

MDCC SEAT TRACK 5R BETWEEN FRAMES 47 AND 51 HAS 6 EA GOUGES AT FRAME ON INBD SIDE AROUND FASTENER HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED, FABRICATED REPLACEMENT, AND REPLACED SEAT TRACK IAW DWG A53832211 AND SRM 51-72-10 PGS. 2 AND 3.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOORBOARD 323 TG HAS IMPACT DAMAGE AT UPPER SURFACE TOTAL DEFECT MEASURES 8.5" LONG. FABRICATED REPLACEMENT FLOORBOARD 232TG IAW DWG SRZ 25-005.

Part: SEAT TRACK — CHAFED (MAIN DECK) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FR 44 TO 50, SEAT TRACK 2R NUT CLIPS HAVE BEEN CHAFING AROUND FASTENER HOLES. REPAIRED SEAT TRACK IAW FSRM 53-10-16.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FWD FUSELAGE, FR38 4IN., 3IN. OUTBD OF SEAT TRACK 6R, SHEAR PLATE CRACKED 2 INCHES LONG. R & R FWD FUSELAGE SHEAR PLATE SUPPORT IAW FSRM 51-72-10.

Part: FITTING — CRACKED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

RT FUSELAGE FITTING AFT OF FRAME 47 BETWEEN STRINGERS 28 AND 29 RT HAS A 2 INCH LONG CRACK IN LOWER RADIUS. R & R RT FUSELAGE FITTING AFT OF FRAME 47 BETWEEN STRINGERS 28 AND 29 IAW FSRM 51-40-21 AND 51-72-10.

Part: WEB — CORRODED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC 260 ZONE WEB ASSY OTBD OF SEAT TRACK 5R BETWEEN FRAME 79 AND 80/82 HAS A 1.5" CRACK. R & R WEB ASSY IAW SRM 51-72-10.

Part: WEB — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC 260 ZONE WEB ASSY OTBD OF SEAT TRACK 5L BETWEEN FRAMES 79 AND 80/82 HAS A 2" CRACK. R & R WEB ASSY AT FRAME 79 AND 80/82 OTBD OF SEAT TRACK 5L IAW SRM 51-72-10.

Part: PROFILE — CORRODED (ZONE 100) · airframe 19,294 hrs · 10,379 cycles

AFT CARGO COMPARTMENT LT SIDE FRAME 63 TO FRAME 67 LOWER TRANSITION PROFILE HAS 18 SQ INCHES OF CORROSION AROUND FASTENER HOLES. R & R PROFILE AT FRAME 63 T0 FRAME 67 LT SIDE AFT CARGO COMPARTMENT IAW SRM 51-40-21.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252BF, CRACKED AT UPPER SURFACE 4 EA FABRICATED REPLACEMENT FLOORBOARD 252 BF IAW DWG SRZ 25-005. REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 241PF CRACKED 1.5 INCHES AT CLS ADAPTER CUT-OUT. FABRICATED REPLACEMENT FLOORBOARD 241 PF IAW DWG SRZ 25-005 REV J

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FLOORBOARD 241 TH PANEL IS CRUSHED WHERE CLEVIS IS ATTACHED FABRICATED. FLOORBOARD 241TH IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 241 DF CRACKED AT 3 PLACES LOWER SURFACE. FABRICATED FLOORBOARD 241 DF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 242 ZJ HAS 5 AREAS WERE CLEVIS ATTACHES THAT ARE CRUSHED AND ALSO A 9 '. CRACK FABRICATED REPLACEMENT FLOORBOARD 242 ZJ IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK FLOORBOARD 242LK HAS A 9" CRACK, FASTENER HOLE MISSING 1" SECTION OF CORE, AND END SECTION OF FLOORBOARD. FABRICATED REPLACEMENT FLOORBOARD 242 LK IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252GF, CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 GF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN DECK 240, FLOORBOARD 242RJ CLEVIS ATTACHMENT SECTION IS BROKEN OFF. FABRICATED REPLACEMENT FLOORBOARD 242 RJ IAW SRZ 25-005, REV J.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC SEAT TRACK 2L BETWEEN FR57 - FR57.1 HAS 2 EA AREAS WITH WORN SCALLOPS, DAMAGE 8 INCHES LONG. FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, FIG 102. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPLACEMENT SEAT TRACK SECTION AND REPAIR SPLICES, AND INSTALLED IAW FSRM 53-10-16. REPROTECTED REPAIR AREA IAW FSRM 51-75-10, PARA 3. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 251 VF DISBONDED/ DELAMINATED AT UPPER SURFACE FABRICATED. REPLACEMENT PANEL 251VF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 241HK CENTER SECTION IS CRUSHED WERE CLEVIS A TTACHES, FABRICATED REPLACEMENT FLOORBOARD 241 HK IAW DWG SRZ 25-005, REV J.

Part: ADAPTER — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MDCC FLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R GOUGED AT FR62. CLEVIS ADAPTER LOCATED AT FR62 BETWEEN SEAT TRACK 2R AND 3R HAS SCALLOPS TORN OUT AND IS OUT OF LIMITS IAW SRM 53-10-15, FIG 107. R & R CLEVIS ADAPTER IAW SRM 51-72-10.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252PH CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 PH IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252YG, CRACKED AT UPPER SURFACE 1 EA. FABRICATED REPLACEMENT PANEL 252YG IAW DWG SRZ 25-005, REJ.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252 UH CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 UH IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252ZF, CRACKED AT UPPER SURFACE 2 EA. FABRICATED REPLACEMENT PANEL 252ZF IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOODBOARD 251UH COMPOSITE MATERIAL SEPARATED AT UPPER SURFACE AROUND CLEVIS CUT-OUT, FABRICATED FLOORBOARD PANEL 251UH IAW DWG NR SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOAR 251YG COMPOSITE MATERIAL SEPARATING, 8 IN LONG, UPP SURFACE. FABRICATED REPLACEMENT PANEL 251 YG IAW DWD SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

MAIN CABIN FLOOR PANEL 251 BH HAS 3 EA CRACKS AT CLEVIS CUT OUT. FABRICATED REPLACEMENT PANEL 251BH IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 242EK HAS 4 AREAS THAT ARE CRUSHED, WHERE CLEVIS ATTACHES, FABRICATED FLOORBOARD 242EK IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 19,294 hrs · 10,379 cycles

FLOORBOARD 252WH CRACKED AT UPPER SURFACE 1 EA. FABRICATED REPLACEMENT PANEL 252 WH IAW DWG SRZ 25-005, REV J.

Part: RIB — CRACKED (NR 2 NACELLE) · airframe 19,294 hrs · 10,379 cycles

NR 2 ENG PYLON RT RIB 20 HAS A 3" CRACK EXTENDING FROM RIVET TO PRODUCTION HOLE. REMOVED PRODUCTION DOUBLER, FABRICATED REPLACEMENT PRODUCTION DOUBLER AND 2 EA. REPAIR DOUBLERS, AND INSTALLED ALL DOUBLERS IAW SRM 54-54-11, AND DWG 41A54515196, REV A. MINOR REPAIR IAW GMM 6-2-100.

Part: STRUCTURE — DAMAGED (RUDDER TIP) · airframe 15,814 hrs · 8,455 cycles

RUDDER TIP ATTACH LAND LT AND RT SIDES ARE DAMAGED. COMPLIED WITH E.O. 6-5540-127975.

Part: BRACKET — FAILED (ZONE 200) · airframe 15,814 hrs · 8,455 cycles

LT VERTICAL STAB CLIP NUT BRACKET UNDER FAIRING PANEL 323 AL IS BROKEN. REMOVED ANGLE BRACKET IAW SRM 51-40-21, PARA 6. FABRICATED ANGLE BRACKET IAW DWG F5357011; SHEET 2; REV "A". ALODINED AND PRIMED IAW SRM 51-23- 10; PG 1. APPLIES TOP COAT IAW SRM 51-23-10, PG 1. PART MARKED BRACKET IAW GM 7-0-1001. INSTALLED BRACKET IAW SRM 51-40-21; PARA 6.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,814 hrs · 8,455 cycles

AFT CARGO COMPARTMENT; FWD BULKHEAD PANEL NR 152 DW; ATTACH ANGLE IS CORRODED ON THE END AT STA 3354; FRAME 54 RT. REMOVED PANELS 152 DW AND 151 BW IAW AMM 25-13-31. INSTALLED PANELS 152 DW AND 151 BW IAW AMM 25-13-31. REMOVED BRACKET IAW SRM 51-40-21; PARA 5 FABRICATED NEW BRACKET IAW DWG A53410767. ALODINED AND PRIMED IAW SRM 51-21-10. PAINTED BRACKET IAW SRM 51-23-10. INSTALLED BRACKET IAW SRM 51-40-21; PARA 6.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN FLOOR PANEL 242 TG IS CRACKED. FABRICATED FLOOR PANEL 242 TG USING THE OLD PANEL AS A TEMPLATE; LOCATED PANEL ATTACH HOLES; ROUTED AND POTTED EDGES; INSTALLED INSERTS; APPLIED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25-005, REV "H".

Part: SKIN — CRACKED (ZONE 100) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT BALL MAT 132 XG IS PUNCTURED/CRACKED ON THE BOTTOM SKIN. REMOVED BOTTOM SKIN IAW SRM 51-72-10; PARA 5A. LOCATED AND DRILLED BOTTOM SKIN IAW SRM 51- 72-10; PARA 6A. ALODINED BOTTOM SKIN IAW SRM 51-21-10; PARA 2B3. PRIMED AND TOPCOATED BOTTOM SKIN IAW SRM 51-23-10; PARA 2B. INSTALLED BOTTOM SKIN IAW SRM 51-72-10; PARA 6. PART MARKED IAW GMM 7-0-1001; PARA 7B.

Part: RAIL — CRACKED (ZONE 100) · airframe 15,814 hrs · 8,455 cycles

AVIONICS COMPARTMENT; THE BATTERY RACK INBD RAIL IS CRACKED AT THE CTR SUPPORT. REMOVED AND REPLACED EXTRUSION HAT IAW SRM 51-72-10.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 15,814 hrs · 8,455 cycles

AVIONICS COMPARTMENT; THE BATTERY RACK INBD RAIL IS CRACKED AT THE FWD SUPPORT. REMOVED AND REPLACED SUPPORT TUBE IAW SRM 51-72-10; REMOVED AND REPLACED 2 EA BATTERIES IAW AMM 24-31-11-4.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 15,814 hrs · 8,455 cycles

FRAME 41; LEFT SIDE AT STRINGER 35; HAS A DOUBLE DRILLED HOLE IN THE FOOT FITTING. COMPLIED WITH E.A. 6-5310-127976.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD DENTED / CRACKED ZONE Z241; PANEL GK AT FRAME 51. FABRICATED NEW FLOORBOARD 241 GK IAW DWG SRZ 25-005; REV "H".

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT FLOORBOARD 132 NG HAS MULTIPLE PUNCTURES ON THE BOTTOM AND EDGE DAMAGE. FABRICATED FLOOR PANEL 132 NG IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT FLOORBOARD 132 LG HAS EDGE DAMAGE AND IS MISSING AN INSERT. FABRICATED FLOOR PANEL 132 LG IAW DWG SRZ 25-005, REV "H".

Part: BRACKET — CRACKED (ZONE 100) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT AFT FIRE BOTTLE MOUNT BRACKET BEAM IS CRACKED AT THE MOUNT HOLES. REPLACED BRACKET IAW SRM 51-72-10.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT FLOORBOARD 132 KG CRACKED. FABRICATED FLOOR PANEL 132 KG IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

FWD CARGO COMPARTMENT FLOORBOARD 132 MG HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 132 MG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN FLOOR SUPPORT LINK AT FRAME 48 & BL Y 1456 IS CRACKED. REMOVED AND REPLACED DAMAGED TRACK LINK IN REF TO DWG A53812067.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 15,814 hrs · 8,455 cycles

NR 1 ENGINE OTBD T/R FWD FACE AT THE UPPER END NEAR THE V-BAND IS CRACKED. DISPLACED SEAL DEPRESSOR FOR ACCESS IAW SRM 51-40-21. REPAIRED CRACKED FRAME REF DWG SRZ 78-002. REINSTALLED SEAL DEPRESSOR IAW DWG 78-002.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 15,814 hrs · 8,455 cycles

NR 1 ENGINE RT REVERSER COWL, INNER FWD UPPER U CHANNEL FRAME, HAS 2 CRACKS AT APPROX THE 11 O'CLOCK POSITION BELOW THE V-BAND ASSY; NS 59.305. DISPLACED SEAL DEPRESSOR FOR ACCESS IAW SRM 51-40-21, REPLACED CRACKED FRAME REF DWG SRZ 78-002. REINSTALLED SEAL DEPRESSOR IAW DWG SRZ 78-002.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 15,814 hrs · 8,455 cycles

NR 2 ENGINE RT REVERSER COWL UPPER CORNER IS CRACKED BELOW THE V-BAND LATCH. DISPLACED SEAL DEPRESSOR FOR ACCESS IAE SRM 51-40-21. STOP DRILLED CRACK IAW DWG SRZ 78-002. INSTALLED DOUBLER IAW DWG SRZ 78-002. REINSTALLED SEAL DEPRESSOR IAW DWG SRZ 78-002.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 15,814 hrs · 8,455 cycles

RT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 25A IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A IAW SRM 51-40-21.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 15,814 hrs · 8,455 cycles

NR 2 ENGINE INBD T/R FWD UPPER CORNER IS CRACKED BELOW THE V-BAND LATCH. CRACK WAS FOUND TO BE OUT OF LIMITS. T/R TO BE REPLACED ON N/R N00598.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 15,814 hrs · 8,455 cycles

LT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 24; RIB 25A AND 6EA. WEBS IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A ; OLD RIB 24; THE 6 EA. WEBS AND THE SKIN IAW SRM 51-40-21.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 BF IS CRACKED. FABRICATED FLOORBOARD 252 BF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 BF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 RG IS DENTED. FABRICATED FLOOR BOARD 242 RG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 RG IAW AMM 53-10-25-4. ALL WORK WAS ACCOMPLISHED ON N/R N00166.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 ZJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "H". ALL WORK WAS ACCOMPLISHED ON N/R N00168.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS SPONGY, ZONE Z241, PANEL AJ AT FRAME 46. FABRICATED NEW FLOORBOARD 241 AJ IAW SRZ 25-005 REV "H". REMOVED AND REPLACED FLOOR PANEL 241 AJ IN REF TO AMM 53-10-23-4. PART MARKED PANEL IN REF TO GMM 7-0-1001.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 SF IS DENTED/CRACKED. FABRICATED MAIN CABIN FLOOR BOARD 242 SF USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 SF IAW SRM 53-10-23-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 RG IS CRACKED. FABRICATED FLOORBOARD 242 RG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 RG IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 QJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005; REV "H".

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 UJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005; REV "H".

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 GF IS CRACKED. FABRICATED FLOORBOARD 252 GF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 GF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 ZF IS CRACKED. FABRICATED FLOORBOARD 252 ZF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4. INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 232 BF IS DENTED / CRACKED. FABRICATED FLOOR PANEL 242 BF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 BF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 MF IS DENTED/CRACKED. FABRICATED FLOOR PANEL 242 MF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 MF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS CRACKED. REPAIRED MAIN CABIN FLOOR BOARD 242 EK BY FABRICATING A NEW BOARD USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25-005, REV "H". ALL WORK WAS ACCOMPLISHED ON N/R N00171 (30171).

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 ZJ IS CRACKED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "H".

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 232 YG IS DENTED/CRACKED. REPAIRED MAIN CABIN FLOORBOARD 232 YG BY FABRICATING A NEW FLOORBOARD USING THE OLD FLOORBOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED; CLEANED; INSTALLED ANTI-SKID TAPE AND PART MARKED PANEL IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 232 YG IAW AMM 53-10-23-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 GF IS DENTED/CRACKED. FABRICATED FLOOR PANEL 242 GF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 GF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS DENTED/CRACKED. REPAIRED MAIN CABIN FLOORBOARD 242 EK BY FABRICATING A NEW BOARD USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 EK IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 VG IS CRACKED. FABRICATED FLOOR PANEL 242 VG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 242 VG IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 VF IS CRACKED. FABRICATED FLOORBOARD 252 VF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 VF IAW AMM 53-10-25-4. INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD 252 PH IS CRACKED. FABRICATED FLOORBOARD 252 PH IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 PH IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS DENTED/CRACKED. ZONE Z241 PANEL WH AT FRAME 46. FABRICATED NEW FLOOR PANEL 241 WH IAW DWG SRZ 25-005; REV "H".

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS DENTED/CRACKED, ZONE Z241, PANEL HK AT FRAME 53. FABRICATED FLOOR PANEL 241 HF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 241 HF IAW AMM 53-10-25-4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 UF IS CRACKED. FABRICATED FLOORBOARD 252 UH IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 UH IAW AMM 53-10-25-4.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS PUNCTURED AT FRAME 31, LBL 52. FABRICATED FLOORBOARD 241 MJ IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 241 MJ IAW AMM 53-10-25-4.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 15,814 hrs · 8,455 cycles

MAIN CABIN ARTICULATING SEAT TRACK IS WORN AT FRAME 23; LBL 26. REMOVED FLOOR PANEL IAW AMM 53-10-23-4. BLENDED WORK AREA AND REMOVED 0.001 MATERIAL. MATERIAL REMAINING WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16; FIG 101. REINSTALLED FLOOR PANEL IAW AMM 53-10-23-4. TOOL USED IS T8225T.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 15,814 hrs · 8,455 cycles

MAIN CARGO COMPARTMENT FLOORBOARD 251 NG IS CRACKED. FABRICATED FLOOR PANEL 251 RT IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 251 RT IAW AMM 53-10-25-4.

Part: SKIN — CHAFED (R1 DOOR) · airframe 15,814 hrs · 8,455 cycles

THE R-1 DOOR AREA, FAILSAFE RING UPPER FWD CORNER EXTERNAL SKIN IS CHAFED. COMPLIED WITH E.A. 6-5330-127973.

Part: PICKUP — FAILED (TE FLAPS) · airframe 15,565 hrs · 8,312 cycles

ON APPROACH HAD A FLAPS SYS 1 AND 2 FAULT/FLAPS STUCK. CYCLE HANDLE PER CHECK LIST COULD NOT GET FLAPS TO EXTEND. LAND 0 FLAPS SLATS EXTENDED. BELIEVE EMERGENCY DECLARED. REMOVED AND REPLACED ASYMMETRY POS P/U RT AND FEEDBACK POS P/U. REF MM 27-56-11-4 AND 27-51-19-4. OPS CHECK OF FLAP SYSTEM NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,419 hrs · 7,245 cycles

CAPTS FWD WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED CAPT'S WINDSHIELD PANEL, WINDOW HEAT PROTECTION CONTROLLER AND WINDSHIELD TEMP REGULATOR. WINDOW INSTALLATION COMPLETED IAW MM 56-11-11-4.

Part: TRANSMITTER — MALFUNCTIONED (HYD PRESSURE) · airframe 11,343 hrs · 6,116 cycles

EN ROUTE TO BTR BLUE SYSTEM HYDRAULIC LOSS. UNABLE LDG BTR, SHORT RUNWAY. BLUE HYD PRESS TRANSMITTER LEAKING. REMOVED AND REPLACED BLUE SYS PRESSURE XMITTER. SERVICED SYS RAN ENG OPS CHECKED GOOD AMM29-32-13-4.

Part: GCU — FAULTY · airframe 10,693 hrs · 5,778 cycles

PDIS 682 24-30 0004948 22FEB06 MEM CLOSE R LOGPAGES: 01107636 GEN NR1 FAULT AFTER TAKEOFF WOULD NOT RESET. APU WAS INOP (ON MEL) FACT 23FEB06 07:18 MEM R VERIFIED NR 1 ENGINE IDG OIL SERVICED PROPERLY. PERFORMED BITE TEST OF THE GPCU. FAULTED LT GEN. SYSTEM FAULTS (OVER FREQ TRIP) AND (UNDER FREQ TRIP). REF A300-600 FIM. REMOVED AND REPLACED THE NR 1 GCU IAW MM 24-22-12-4. IAW JRH RAN NR1 ENGINE FOR APPROX 45 MINUTES WITH FULL ELECTRICAL LOAD APPLIED. NO FAULTS OCCURED. PERFORMED BITE TEST OF GPCU, ALL SYSTEMS OK. OFF MFG 764067 POS 1 SRL A168 ON MFG 764067A SRL 0374.

Part: AUTOTHROTTLE SYS — FAILED · airframe 7,617 hrs · 4,054 cycles

ON FINAL APPROACH, NR 1 THROTTLE STUCK AT ABOUT 15 DEGREES. DECLARED EMERGENCY AND FINISHED APPROACH. AFTER LANDING, THROTTLE MOVED FREELY. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01 CATEGORY: C EXPIRATION: 16MAR04 MEL 22-30-01: AUTOTHROTTLE SYSTEM INOP. ALL THRUST MUST BE MANUALLY SET. NO OPS WITHIN METRIC AIRSPACE. DEBRIEFED CREW, APPROACH WAS MADE WITH AUTOTHROTTLES ENGAGED. AUTOTHROTTLE COUPLING UNIT REPLACED

Part: DOOR — GOUGED (NR 1 ENG T/R) · airframe 6,127 hrs · 3,260 cycles

EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. COMPLIED WITH EA 8-7832-68795 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR AT MAE.

Part: ANGLE — GOUGED (THRUST REVERSER) · airframe 6,127 hrs · 3,260 cycles

NR 233 NR 2 ENG I/B THRUST REVERSER LOWER CORE STRUCTURE ANGLE GOUGED 4 AREAS. R/R ANGLE PER IAW SRM 51-40-21 SRM 51-40-21 AT MAE.

Part: TUBE — CRACKED (PRECOOLER) · airframe 6,127 hrs · 3,260 cycles

NR 1 ENGINE PRECOOLER CRACKED AT COOLING TUBE INSTALLED PRECOOLER IAW W/C 64S0202 WO 22877 AT MAE.

Part: STRIP — CRACKED (RT WING SPOILER) · airframe 6,127 hrs · 3,260 cycles

RT WING NR 3 SPOILER T/E STEEL STRIP CRACKED. R & R STRIP PER IPER IAW SRM 51-40-23 & 57-72-11.AND SRM 57-72-11 WO 22877 AT MAE.

Part: RIB — GOUGED (LT WING) · airframe 6,127 hrs · 3,260 cycles

COMPLY WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE- RIB 7A (LT) GOUGE REPAIR, P/N A572-46814. FACT 02MAY03 12:14 BFM U COMPLIED WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE-RIB 7A (LT) GOUGE REPAIR P/N A572-46814 AT MAE

Part: PANEL — GOUGED (RT WING) · airframe 6,127 hrs · 3,260 cycles

DEEP GOUGE IN RT WING L/E PNL 612B, FOUND TO BE OUT OF LIMITS PER IAW SRM 57-41-11. REPLACED PNL, TREATED, PRIMED AND PAINTED PER IAW SRM 51-40-44, SRM 51-75-10 AND SRM 51-21-10.

Part: B-NUT — LOOSE (APU) · airframe 4,944 hrs · 2,638 cycles

NR 1 GEN FAULT ILLUMINATED IN FLIGHT. FOLLOWED ECAM PROCEDURES. UNABLE TO RESET NR 1 GEN STARTED APU. ACN RELEASED PER MEL/CDL: 24-11-01GEN NR 1 - INOP. APU GEN MUST BE USED TO PWR 1 AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN EAML THAT OIL QTY OF IDG IN DISC MODE, REMAINING OPERATIVE IDG, & APU GEN ARE CHECKED ONCE EACH FLIGHT DAY. GPCU BITE INDICATED MPU/WIRING IN FLT APU AUTO-SHUTDOWN. APU INOP. FOLLOWED ECAM AND TURNED APU MSR SW OFF. DIVERTED TO RNO DUE TO NR 1 GEN + APU INOP, REF WRI 24-20/2038. APU SHOWED NO INDICATION OF OIL AT TANK. SERVICED APU TO FULL AND FOUND SEVERAL B-NUTS LOOSE. TIGHTENED B-NUTS WIPED DOWN AREA AND RAN APU WITH NO LEAKS DETECTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,816 hrs · 1,996 cycles

DURING T/O, NR 2 REVR PRESSURIZED WARNING ON ECAM. REVR DEACTIVATED IN FWD THRUST POSITION.