N157UP

Part: FLOOR PANEL — DAMAGED (ZONE) · airframe 25,388 hrs · 15,190 cycles

FAULT: APG / Z100 / DURING MAIN WHELL WELL INSPECTION FOR HYDRAULIC SYSTEM LEAK CHECKS A FLOOR PANEL (P/N: A2551027700100) FOUND SOFT AND DELAMINATED INSTALLED MAIN WHELL WELL FLOOR PANEL (P/N: A2551027700100) IAW AMM 53-15-31/401

Part: FRAME — CRACKED (ZONE 400) · airframe 25,387 hrs · 15,189 cycles

NR 2 ENGINE PANEL 485AL HAS CRACK ON I/B SIDE #7 FRAME FROM FRONT. INSTALLED FRAME #7 AT 485AL USING FASTENERS IAW A300-600-SRM-51-40-21

Part: FRAME — CRACKED (ZONE 400) · airframe 25,387 hrs · 15,189 cycles

NR 1 ENGINE PPANEL 475AL I/B SIDE #7 STRINGER FROM FRONT CRACKED DT 1/042 INSTALLED FRAME #7 AT 475AL USING FASTNERS IAW SRM-51-40-21

Part: PROFILE — CRACKED (ZONE 200) · airframe 25,387 hrs · 15,189 cycles

MAIN DECK FLOOR STRUCTURE, UNDER PANEL 261PF AT FR 74 AND FR75, LT FLOOR SUPPORT HAVE 2EA CRACKS. DOT 90-095. REMOVED MAIN DECK FLOOR STRUCTURE, UNDER PANEL 261PF AT FR 74 AND FR75 L/H FLOOR SUPPORT IAW SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW GMM 09-08.INSTALLED NEW Z-PROFILE AT MAIN DECK FLOOR STRUCTURE, UNDER PANEL 261PF AT FR 74 AND FR75, L/H, IAW SRM 51-40-21

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 25,387 hrs · 15,189 cycles

FRAME BASE FITTING R/H FR45 AREA 1 HAS A CRACK 1.5" LONG.SJ-30 VERIFIED REPAIR PARTS INSTALLED IAW E0-46789-JIC008 REV1(SB A300-57-6177) STEPS 51-68 COMPLETED. JOB COMPLETE

Part: FRAME — CRACKED (ZONE 400) · airframe 25,387 hrs · 15,189 cycles

NR 2 ENGINE PANEL 485AL O/B SIDE #1 STRINGER CRACKED. INSTALLED PART STRINGER #2 ENGINE PANEL 485AL O/B SIDE #1 IAW A300-600 SRM 51-40-21

Part: PROFILE — CRACKED (ZONE 200) · airframe 25,387 hrs · 15,189 cycles

MAIN DECK FLOOR STRUCTURE, UNDER PANEL 262PF AT FR 74 AND FR75, R/H FLOOR SUPPORT HAVE 2EA CRACKS. REMOVED Z-PROFILE AT MAIN DECK FLOOR STRUCTURE, UNDER PANEL 262PF BTW FR 74 AND FR75, IAW A300-600 SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW GMM 09-08.INSTALLED NEW Z-PROFILE AT MAIN DECK FLOOR STRUCTURE, UNDER PANEL 262PF, FR 74 AND FR75, IAW SRM 51-40-21

Part: WEDGE — DAMAGED (ZONE 600 SLAT) · airframe 25,388 hrs · 15,190 cycles

NR 2 SLAT I/B T/E WEDGE LWR SURFACE HAS GOUGE DOT 55-012 REPAIR RH WING #2 SLAT P/N: A57864200173, S/N: FH1636, IAW A300-600F SRM 57-43-11 PARAGRAPH 4.B AND FIGURE 202, APPLICABLE REPAIR PER SRM. REMOVED DAMAGED SKIN AND FABRICATED REPLACEMENT PARTS IAW-A300-SRM-57-43-11. INSTALLED REPAIR PARTS IAW-A300-SRM-51-40-21.

Part: SKIN — GOUGED (NR 1 SLAT) · airframe 25,387 hrs · 15,189 cycles

MAJOR REPAIR. LEFT WING SLAT #1 WITH 2EA GOUGES AND PERFORATED DAMAGE AT LOWER SKIN, O/B SIDE. ACCOMPLISHED PERMANENT REPAIR IR ACCORDANCE WITH EO-95028-REQ1 AND VT-MAE EA 300-5742-27-A4127, REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB12. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB19. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB16. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB25. ACCOMPLISHED REPAIR IR ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4127, REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB15.CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB11. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB26. ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB27. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 25,387 hrs · 15,189 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB13. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.

Part: LOCK — BROKEN (ZONE 800) · airframe 24,755 hrs · 14,810 cycles

LOCKING DEVICE BROKEN ON CREW ENTRY DOOR OUTER HANDLE. ORDERED FROM A300 IPC 52-11-11-09B ITEM 630. HARDWARE IN PARTS BAG HANGING FROM HANDLE. REMOVED AND REPLACED EXTERIOR CONTROL HANDLE PER AMM 52-11-21. OPS CHECK GOOD.

Part: HANDLE — LOOSE (ZONE 800) · airframe 24,735 hrs · 14,799 cycles

CREW ENTRY DOOR EXTERIOR DOOR HANDLE LOSES TENSION AND CANNOT LOWER AND LATCH DOOR. REMOVED AND REPLACED EXTERIOR CONTROL HANDLE PER AMM 52-11-21. OPS CHECK GOOD. STICKER REMOVED. DMP REVERSED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 24,640 hrs · 14,749 cycles

FLIGHT CREW STOWAGE AREA/LOCKER LIGHT INOP RE-LAMPED STOWAGE AREA LT - OPS CHECK GOOD IAW MM 33-27-00

Part: SEAL — DAMAGED (ZONE 500 SLAT) · airframe 24,570 hrs · 14,714 cycles

SLAT JACK SEAL RIPPED LT WING RIB 27. LOWERED SLAT AND INSPECTED RIB 27 SLAT SEAL, REPOSITIONED CORNER OF SEAL IAW M/M 27-81-41-0601. RAISED SLATS AND SEAL LOOKS NORMAL IN TRACK

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 24,429 hrs · 14,654 cycles

CREW ENTRY DOOR WILL NOT CLOSE FROM THE OUTSIDE. PERFORMED INSPECTION AND CHECK OF CREW ENTRY DOOR IAW AMM 52-00-00/601 3. B. 3. INSPECTION AND CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. DOOR CLOSED SEVERAL TIMES WITH NO ISSUES.

Part: WARNING LIGHT — MALFUNCTIONED (ESCAPE SLIDE) · airframe 24,072 hrs · 14,445 cycles

EMERGENCY EVACUATION SLIDE ASSEMBLY WARNING LIGHT INOPERATIVE-BUZZER OPERATIVE PERFORMED OPS CHECK OF SLIDE TEST SWITCH PER AMM 52-73-14/401. OPS CHECK NORMAL. LIGHT AND HORN FUNCTION NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,651 hrs · 14,216 cycles

*** SDR FILED OPEN *** LIGHT OUT IN SUPERNUMERARY COAT CLOSET. DEFERRED COAT CLOSET LIGHT PER MEL 33-21-01-3-0-2. INSTALLED PLACARD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,681 hrs · 14,237 cycles

LIGHT OUT IN SUPERNUMERARY COAT CLOSET. RELAMPED LIGHT AND FOUND THAT DOOR SWITCH WAS OUT OF ADJUSTMENT, ADJUSTED SWITCH OPS CK GOOD , PLACARD REMOVED. THIS CLEARS THE DEFERRAL PER MEL 33-21-01-3-0-2

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 23,487 hrs · 14,106 cycles

INSPECTION TYPE: NA AUTONOMOUS POWER SUPPLY DOES NOT BITE TEST.R&R BOTH EMERGENCY PWR SUPPLY BATTERIES PER AMM 52-73-18 BITE TEST WORKS BUT NO GOOD. FAULTS THE UNIT AND NO OUTPUT SINGAL. R&R APSU PER AMM 52-73-18. BITE TEST GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: FLAP SYSTEM — FAULTED (WING) · airframe 23,345 hrs · 14,013 cycles

INSPECTION TYPE:NA*EMERGENCY DECLARED* CONFIGURING FOR LANDING, UPON SELECTION OF FLAP 15Ï¿½. ECAM "FLAPS SYS 2 FAULT" APPEARED. RAN QRH PROCEDURE FOR FLAPS FAULT. PER PROCEDURE FLAPS EXTENDED TO 30/40 FOR APPROACH AND LANDING. FLAPS EXTENDED SLOWER THAN NORMAL TO 30/40R&R PRESS S/W AT BLOCK VLV 24CV, NO HELP. R&R BLOCK VALVE 24CV PER AMM 27-54-33-0401, OPS CHECK NORMAL AT THIS TIME, NO LEAKS NOTED, OPERATED FLAPS TO 40 DEG & TO FULL UP POSITIONS SEVERAL TIMES, NO FAULTS NOTED. PER TECH SUPPORT BLOK VLV P/N ON/OFF 658A0000-02, S/N ON 1980, S/N OFF 1906,

Part: RESERVOIR — INOPERATIVE (WING) · airframe 23,271 hrs · 13,963 cycles

INSPECTION TYPE:NA*EMERGENCY DECLARED* HYD-GREEN RSVR LOW LEVEL-COMPLIED WITH QRH.RESERVOIR INDICATOR SHOWED COMPLETELY DELETEDFOUND #2 ENGINE PYLON GREEN HYD.PIPELINE WITH PIN HOLE MID SECTION OF PYLON.REMOVED & REPLACED PIPELINE IAW AMM.29-11-69-0401 & IPC REF.29-11-06-01B ITEM # 250.P/N OFF & ON: A2911503000400.LEAK CHECK FOUND SATISFACTORY.OK FOR CONTINUE IN SERVICE.

Part: FLAP — CHAFED (INNER FLAP) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING INNER FLAP P/N A57960000010 S/N FH1297 O/B EDGE HAS A REPAIR DOUBLER WITH 2 EACH CHAFE DAMAGESWORKED PER UPS EO A300-5750-86183-A AND UPS RCD 269862

Part: UNKNOWN — UNKNOWN (FRAME 12) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* FRAME 12 LAVATORY VENTURI EXTERNAL DOUBLER INSTALLATION FOR RCD PURPOSES ONLYCOMPLIED WITH UPS EO A300-5330-72601-B AND RCD 269970

Part: ADAPTER — BROKEN (MAIN CARGO) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1CR/H MAIN CARGO COMP - Y1959 FRAME 20 FLOOR TIEDOWN (CLS ADAPTER) IS BROKEN, P/NB53774133820200.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CPANEL 242CF IS DAMAGEDFABBED PANEL 242CF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552

Part: ADAPTER — BROKEN (MAIN CARGO) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1CR/H MAIN CARGO COMP-Y1959 FRAME19 FLOOR TIEDOWN (CLS ADAPTER) IS BROKEN P/N B5377413820200.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CPANEL 242BJ IS CRACKEDFABBED 242BJ FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552

Part: PYLON — CRACKED (PRE-COOLER) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C#1 PYLON RIB FWD OF PRE-COOLER CRACKED, (RIB 3)REMOVED AND INSTALLED RIB ARCH IAW SRM 51-40-21.

Part: STIFFENER — CRACKED (AFT PIT/FWD BLKH) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CAFT PIT FWD BULKHEAD STIFFENER P/N A5341076521700 IS CRACKED.REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21.

Part: BRACKET — BROKEN (RH WING CTR FLAP) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CR/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: ADAPTER — BROKEN (MAIN DECK) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CCLS ADAPTER BROKEN AT FRAME 32-Y2200 P/N B5377413620490.REMOVED AND REPLACED CLS ADAPTER AT FR32-Y2200 IAW SRM 51-40-21.

Part: ADAPTER — BROKEN (MAIN DECK) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CCLS ADAPTER AT FRAME 33-Y2200 P/N B53774136204 IS BROKENREMOVED AND REPLACED, CLS ADAPTER AT FR33-Y2200 IAW SRM 51-40-21.

Part: STIFFENER — CRACKED (FWD BLKHD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: UNIVERSAL JOINT — CRACKED (RH WING) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* RH WING FLAP DRIVE UNIVERSAL JOINT O/B FITTING BRACKET CRACKEDREMOVED, FABRICATED, AND INSTALLED PER UPS EO A300-5750-86448-A AND RCD

Part: DOUBLER — DAMAGED (RUDDER TIP) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:SEGRUDDER R/H SIDE UPPER T/E HAS LIGHTENING STRIKEFABRICATED DOUBLER IAW SRM-44-11

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.

Part: ADAPTER — DAMAGED (FRAME 66) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* MAIN DECK SEAT TRACK ADAPTER HAS DAMAGE AT FRAME 66 AT Y0.REMOVED, FABRICATED AND INSTALLED PER EO A300-5310-86281-A AND UPS RCD 270044.

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CPANEL 252ZG IS BROKENFABBED PANEL 252ZG FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1CFABBED PANEL 252WG IS BROKENFABBED PANEL 252ZG FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 151LG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 151KG DAMAGEDFABRICATED NEW PANELPER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 15VF DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 152LG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 152MG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E

Part: STIFFENER — CRACKED (FWDBULKHD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: BRACKET — CRACKED (L/HFLAP) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CL/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKETREMOVED AND REPLACED IAW SRM 51-40-21

Part: STIFFENER — CRACKED (FWDBULKHD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: STIFFENER — CRACKED (FWDBULKHD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: STIFFENER — CRACKED (NOSECOWLBLKHD) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CDOG BONE CRACKED AT 38.1REMOVED AND REPLACED IAW SRM 51-40-21

Part: DOUBLER — CRACKED (COWL INLET) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CH1C#2 ENG BOTTOM OF NOSE COWL AIR INLET LANDING CUT OUT IS CRACKED.FABRICATED DOUBLER IAW CMM 71-11-05.

Part: DOUBLER — CRACKED (R/H FLAP RIB 26) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: FILLER — CRACKED (FWD SPAR) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: FILLER — CRACKED (FWD SPAR) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: PLATE — CRACKED (FWD SPAR) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A REV

Part: PLATE — CRACKED (FWD SPAR) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 26REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: DOUBLER — CRACKED (R/H FLAP RIB 27) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: FILLER — CRACKED (FWD SPAR) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* L/H WING CENTER FLAP HAS A CRACK IN THE RIB FLANGE 27REPAIRED PER UPS EO A300-5750-86564-A AND FINAL EA 300-5750-27-A3180 REV

Part: SPLICE — CRACKED (O/B NOSECOWL AFT) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED SPLICE IAW SRM 51-40-21

Part: SPLICE — CRACKED (I/B NOSECOWL AFT) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C#2 ENG I/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED SPLICE IAW SRM 51-40-21

Part: WEB — CRACKED (O/B NOSECOWL AFT) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED WEB IAW SRM 51-40-21

Part: WEB — CRACKED (I/B NOSECOWL AFT) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CK1C#2 ENG I/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED WEB IAW SRM 51-40-21

Part: BRACKET — BROKEN (L/HPYLON) · airframe 23,133 hrs · 13,882 cycles

INSPECTION TYPE:CPYLON L/H REAR SIDE BRACKET BROKENREMOVED, FABRICATED, AND REPLACED IAW SRM 57-26-10 AND SRM 51-40-21

Part: HORN — INOPERATIVE (PAX DOOR) · airframe 22,267 hrs · 13,422 cycles

UPON DISARMING THE DOOR (CABIN) ON BLOCK IN, THE WARNING HORN WOULD NOT TEST. DEFERRED SLIDE WARNING BUZZER PER MEL 52-73-01-2 NO DMP REQUIED. PLACARD INSTALLED. M788685 ASSIGNED.REPLACED WARNING BUZZER PER SWPM 20-51-40. TEST NORMAL PER AMM 52-73-00

Part: FUEL TANK — LOW PRESSURE (WING) · airframe 21,593 hrs · 13,017 cycles

INSPECTION TYPE:N/A** ATB ** SHORTLY AFTER TAKE-OFF ECAM MSG "FUEL ECAM FUEL PAGE INDICATED LEFT INNER FUEL ISOLATION VALVE FAULT.TROUBLESHOT PER ASM 28 21 00 FOUND FAULTS TO BE INDICATION ONLY. FOUND RELAY 41QA FAULTY. REPLACED PER ESPM 20 46 50 OPS CHECK NORMAL PER AMM 28 21 12 0501.

Part: NONE — NONE (DOORS) · airframe 21,334 hrs · 12,876 cycles

INSPECTION TYPE:NAMAIN ENTRY DOOR DISARM SAFETY PIN IS DIFFICULT TO INSERT AND REMOVEMAIN ENTRY DOOR DISARM SAFETY PIN REMOVED REINSTALLED FREELY DOOR MECHANISMS OPEN GOOD IAW AMM 52-10-30

Part: POWER SUPPLY — FAULTED (AUTOMOMOUS) · airframe 20,755 hrs · 12,532 cycles

AUTONOMOUS STANDBY POWER UNIT FAIL, LIGHT ILLUMINATED .R/R AUTONOMOUS PWR SUPPLY UNIT PER AMM 52-73-18 OPS CHECK GOOD.

Part: LANYARD — OUT OF POSITION (SLIDE BOTTLE) · airframe 20,375 hrs · 12,299 cycles

INSPECTION TYPE:N/A FWD ENTRY DOOR SLIDE ARMING LEVER WILL NOT ENGAGE.REPOSITIONED SLIDE BOTTLE DISCHARGE LANYARD FROM INTERFERRING WITH SLIDE GIRT BAR. OPERATED SLIDE ARMING HANDLE SEVERAL CYCLES. OPS CK GOOD PER AMM 05-61-054 THIS CLEAR M739339

Part: FLOOR PANEL — DAMAGED (AVIONICS COMPT) · airframe 20,231 hrs · 12,216 cycles

INSPECTION TYPE: SEG FWD AVIONICS COMPARTMENT FLOOR PANEL 121WF IS DAMAGED/DELAMINATED AT CORNER, AS MARKED, SREO A300-5320-42722.

Part: HANDLE — BINDING (SLIDE) · airframe 20,213 hrs · 12,207 cycles

SLIDE HANDLE BINDS WHEN DISARMING. PERFORMED OPERATIONS CHECK, IAW AMM 52 10 30, NO DEFECTS NOTED.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 20,034 hrs · 12,120 cycles

ON TAXI OUT, DURING FLIGHT CONTROL CHECK, FREEDOM OF MOVEMENT OF RUDDER WAS RESTRICTED BOTH LEFT AND RIGHT PEDALS SEEMED TO PASS A DETENT WHICH REQUIRED ABNORMALLY HIGH FOOT PRESSURE. FOUND SEVERAL HI LOCKS SHEERED, AS WELL AS BOTH UPPER AND LOWER ATTACH FITTING ARMS TO NR 4 RUDDER SERVO ACTUATOR MISSING. HINGE ARM HAD 7" CRACK AT LT SIDE. R & R PER DWG A55371 778 SHEET 3,6,7 SRM 55-36-42 & 51-40-23 & 51-72-10. LOWER HINGE ARM 4"CRACK LT SIDE. R & R PER DWG A55571778, SRM 55-36-42 & 51-40-23 & 51-72-10. EO A300-2720-13915-O & A300-5540-14040-D FOR REPAIR.

Part: SLIDE — MALFUNCTIONED (PAX DOOR) · airframe 19,831 hrs · 12,002 cycles

SLIDE WILL NOT GO INTO THE ARMED POSITION. OK TO DEFER DOOR SLIDE, PER MEL 52-11-04-4 DMP 52-11-01-5 ACCOMPLISHED. THIS OPENS DMI M723431. REPOSITIONED GIRT BAR RETAINING CLIP DOOR. OPERATIONS TEST NORMAL, PER 52-10-30-501, DEFERRAL CLEARED.

Part: SLIDE — BINDING (L1 DOOR) · airframe 19,803 hrs · 11,983 cycles

INSPECTION TYPE: NA SLIDE WILL NOT ARM-LEVER JAMS AT HALF TRAVEL. REALIGNED SLIDE COVER TO ALLOW OPERATION OF GIRT BAR, PER AMM 52-10-00. OPERATIONS CHECK GOOD.

Part: CONTROL HANDLE — LACK OF LUBE (DOOR) · airframe 19,686 hrs · 11,914 cycles

INSPECTION TYPE: NA, SUPPLEMENTAL SDR, DOOR SLIDE WILL NOT ARM. ITEM DEFERRED, PER MEL 52-11-01-4. PLACARD INSTALLED, NO DMP. DOOR OPENS FINE W/NO INTERFERENCE. M 720310 CREATED. CLEANED & LUBED EMERGENCY CONTROL HANDLE. L1 DOOR SLIDE FUNCTION CHECK NORMAL, IAW AMM 52-10-30-0601. THIS CLOSES M720310. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 18,608 hrs · 11,285 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHT AUTO TEST FUNCTION IS INOP, WILL NOT COMPLETE TEST, ALL LIGHTS AND MANUAL AND AUTO CONTROLS FUNCTIONS NORMAL. DEFERRED COURIER KUPERNUMERARY AREA INTERIOR EMERGENCY LIGHT -TEST FUNCTION, IAW MEL 33-51-05-2 ACCOMPLISHED DMP 33-51-05-2 PLACARD INSTALLED.ACCOMPLISHED SUPPERNUMARY. AREA EMER / LIGHTING ADJ/TEST IAW AMM. OPS CK OK, DI REMOVED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 17,505 hrs · 10,646 cycles

INSPECTION TYPE:N/A EMERGENCY EXIT SIGN LOWER LAMP INOP. RELAMPED. OPS OK. REF. AMM 33-51-13.

Part: WARNING LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 17,068 hrs · 10,408 cycles

ENTRANCE DOOR SLIDE WARNING LIGHT INOPERATIVE. REPLACED THE WARNING LIGHT.

Part: DOUBLER — CRACKED (VHF ANTENNA) · airframe 16,991 hrs · 10,363 cycles

NR 3 VHF ANTENNA PLATE WAS CRACKED, INSIDE THE MAIN CABIN. REMOVED & REPLACED THE DOUBLER IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 16,991 hrs · 10,363 cycles

BULK CARGO COMPARTMENT FLOOR PANEL 162HF WAS DENTED AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW EO A300-5320-16407-E.

Part: FITTING — CRACKED (RUDDER) · airframe 16,991 hrs · 10,363 cycles

RUDDER FRONT SPAR UPPER SERVO FITTING WAS CRACKED AT THE LEFT LOWER FLANGE. REMOVED AND REPLACED THE FITTING IAW DWG A55471734.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 16,991 hrs · 10,363 cycles

MAIN CABIN FLOORBOARD 232LF WAS DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552.

Part: SKIN — CRACKED (LT WING ROOT) · airframe 16,991 hrs · 10,363 cycles

LEFT WING ROOT UPPER SKIN WAS CRACKED AT A FASTENER. REPAIRED IAW SRM 57-51-12.

Part: ATTACH ANGLE — CRACKED (FRAME 79) · airframe 16,991 hrs · 10,363 cycles

SEAT TRACK ATTACH ANGLE AT FRAME 79, -Y1589 WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW EO A300-5130-70228-A.

Part: SEAL DEPRESSOR — GOUGED (DOOR FRAME) · airframe 16,991 hrs · 10,363 cycles

AFT CARGO DOOR CUTOUT AFT FRAME UPPER SEAL DEPRESSOR WAS GOUGED. REMOVED AND REPLACED SEAL DEPRESSOR IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 16,991 hrs · 10,363 cycles

EXTERNAL FUSELAGE FAIRING 144FR AFT SUPPORT CRACK BETWEEN FR 45 AND FR 46. REMOVED AND REPLACED SUPPORT PER SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 16,991 hrs · 10,363 cycles

EXTERNAL FUSELAGE FAIRING 143FL AFT SUPPORT CRACK BETWEEN FR 45 AND FR 46. REMOVED AND REPLACED SUPPORT PER SRM 51-40-21.

Part: SKIN — DENTED (RT TE FLAP LE) · airframe 16,991 hrs · 10,363 cycles

RIGHT WING CENTER FLAP LE HAD A DENT APPROXIMATELY 24 INCHES FROM THE INBD EDGE. REPAIRED THE FLAP IAW EO A300-5750-70248-A.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 16,991 hrs · 10,363 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, LBL 77 WAS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: INTERCOSTAL — CRACKED (E/E DOOR FRAME) · airframe 16,991 hrs · 10,363 cycles

AVIONICS COMPARTMENT ACCESS DOOR 121BL LEFT INTERCOSTAL WAS CRACKED INSIDE THE DOOR FRAME. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-21 AND DWG A52110744.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 16,991 hrs · 10,363 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, LBL 40 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 16,991 hrs · 10,363 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRAKET AT FRAME 54, RBL 40 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRAKET IAW SRM 51-40-21.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 16,991 hrs · 10,363 cycles

NR 1 PYLON, AFT LOWER WEB WAS CRACKED. REPLACED THE WEB IAW SRM 51-40-44,51-40-21, AMM 20-23-12-001, 29-14-00-0301, AND DWG A54515063, ISSUE K.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 16,991 hrs · 10,363 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, RBL 36 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: ANGLE — CRACKED (FRAME 38.2) · airframe 16,987 hrs · 10,360 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, LBL 41 ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21

Part: ANGLE — CRACKED (FRAME 38.2) · airframe 16,987 hrs · 10,360 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FRAME 38.2, LBL 22 ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SEAL DEPRESSOR — DAMAGED (FWD CARGO DOOR) · airframe 16,987 hrs · 10,360 cycles

FWD CARGO COMPARTMENT DOOR FRAME UPPER AFT SEAL DEPRESSOR WAS DAMAGED. REMOVED AND REPLACED.

Part: ANGLE — CRACKED (FRAME 38.2) · airframe 16,987 hrs · 10,360 cycles

FWD CARGO COMPARTMENT AFT BULK HEAD UPPER FRAME SUPPORT FRAME 38.2, RBL 41 ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: ANGLE — CRACKED (FRAME 10) · airframe 16,987 hrs · 10,360 cycles

AVIONIC COMPARTMENT FLOOR SUPPORT ANGLE AT FRAME 10, RBL 37 WAS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM 51-40-21.

Part: SEAL DEPRESSOR — DAMAGED (FWD CARGO DOOR) · airframe 16,987 hrs · 10,360 cycles

FWD CARGO DOOR FRAME, UPPER FWD SEAL DEPRESSOR AT FRAME 20 WAS DAMAGED. REMOVED AND REPLACED THE SEAL DEPRESSOR IAW SRM 51-40-21.

Part: SKIN — DENTED (FRAME 85) · airframe 15,381 hrs · 9,402 cycles

FUSELAGE SKIN DENTED AT FRAME 85 BETWEEN STRINGERS 44-45L. REPAIRED IAW EO A300-5330-62584-B

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 15,265 hrs · 9,322 cycles

LAVATORY AUXILIARY MIRROR LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21-0401. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FRAME 20A) · airframe 14,954 hrs · 9,124 cycles

FUSELAGE SKIN DAMAGED AT FR 20A. REMOVED DAMAGE AND REPAIRED THE SKIN IAW EO A300-5330-63377-B.

Part: BRACKET — CRACKED (FRAME 54) · airframe 14,339 hrs · 8,720 cycles

INSPECTION TYPE: 1C, AFT CARGO BRACKET AT FRAME 54 BL 0 FWD BULKHEAD WALL CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: BRACKET — CRACKED (FRAME 54) · airframe 14,339 hrs · 8,720 cycles

INSPECTION TYPE: 1C, AFT CARGO BRACKET AT FRAME 54, LBL 37 FWD BULKHEAD WALL CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: BRACKET — CRACKED (FRAME 54) · airframe 14,339 hrs · 8,720 cycles

INSPECTION TYPE: 1C, AFT CARGO BRACKET AT FRAME 54 LBL 39 FWD BULKHEAD WALL CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: O-RING — LEAKING (FILTER BOWL) · airframe 12,690 hrs · 7,677 cycles

SLOW LOSS OF BLUE HYDRALIC SYSTEM QUANTITY, STARTED MID "HAT", FINALLY GOT "HYD RSVR LO LVL" ON BLUE SYSTEM ECAM. RAN ECAM AND DIVERTED. NO OTHER PROBLEMS FOUND O-RING ON BLUE SYSTEM SERVO MANIFOLD FILTER BOWL POOCHED OUT AND NOT SEATED PROPERLY. R & R O-RINGS ON FILTER BOWL, REF MM 29-11-42-0301.

Part: FLOORBOARD — DAMAGED (BULK CARGO) · airframe 11,774 hrs · 7,046 cycles

BULK CARGO FLOORBOARD 161GF HAS FASTENER HOLE BROKEN OFF. FABRICATED BULK CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DELAMINATED (FWD CARGO) · airframe 11,774 hrs · 7,046 cycles

FWD CARGO FLOORBOARD 132QG IS DELAMINATED AND CORNERS BROKE OUT. FABRICATED FWD CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,774 hrs · 7,046 cycles

FWD CARGO FLOORBOARD 132RG FWD CORNER IS BROKEN AND DELAMINATED. FABRICATED FWD FLOORBOARD IAW EO A300-5320-16407-E APPENDIX C.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 251WJ HAS BROKEN OUT SCREW HOLE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 232SH HAS LOWER SKIN TORN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 11,774 hrs · 7,046 cycles

RT MLG GANTRY NR 4 AT FRAME 52 OTBD DAMAGED. ACCOMPLISHED REPAIR OF RT MLG GANTRY IAW EO A300-5310-24922-B.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 11,774 hrs · 7,046 cycles

LT MLG GANTRY NR 4 AT FR 50.1 OTBD DAMAGED. ACCOMPLISHED REWORK OF LT MLG GANTRY IAW EO A300-5310-24922-B.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 11,774 hrs · 7,046 cycles

LT MLG GANTRY NR 2 AT FR 49.1 DAMAGED. ACCOMPLISHED REWORK OF LT MLG GANTRY IAW EO A300-5310-24922-B.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 11,774 hrs · 7,046 cycles

RT MLG GANTRY NR 3 AT FR49.1 INBD DAMAGED. ACCOMPLISHED REWORK OF THE RT MLG GANTRY IAW EO A300-5310-24922-B, APPENDIX D.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 11,774 hrs · 7,046 cycles

RT MLG GANTRY NR 4 AT FR50.1 OTBD DAMAGED. ACCOMPLISHED REWORK OF RT MLG GANTRY IAW EO A300-5310-24922-B.

Part: FLOOR SUPPORT — CRACKED (FRAME 12) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOOR SUPPORT FR 12 IS CRACKED. REPAIRED FLOOR SUPPORT IAW EO A300-5310-23539-F

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 252KJ IS CRACKED AT LOWER SURFACE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 222KG IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 11,774 hrs · 7,046 cycles

THERMOGRAPHIC INSPECTION OF RT ELEVATOR UPPER SURFACE HAS FOUR LOCATIONS OF WATER INGRESS. REPAIRED ELEVATOR SKIN IAW SRM 55-21-12 PB 201, PARA 5J AND FIG 212, SHEET 3.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 231PJ IS DELAMINATED ON UPPER SURFACE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 241LJ IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 242EF IS CRACKED AT LOWER SURFACE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 261DM IS CRACKED, DELAMINATED AND MISSING INSERTS. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 242DF IS CRACKED ON LOWER SURFACE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 11,774 hrs · 7,046 cycles

RT ELEVATOR UPPER SKIN HAS TWO AREAS OF WATER INGRESS AT THE ER10 LIGHTNING STRIP. REPAIRED RT ELEVATOR UPPER SKIN IAW EA 300-5520-01-A5130-IR AND EO A300-5520-53712-A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD 251UJ IS DAMAGED AT CORNERS. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBOARD NR 262AH HAS A CRACK AT AFT EDGE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 11,774 hrs · 7,046 cycles

FWD CARGO FLOORBOARD 131AH IS CRACKED IN THREE PLACES, CORNER RIPPED AND DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E APPENDIX C.

Part: FLOORBOARD — DELAMINATED (FWD CARGO) · airframe 11,774 hrs · 7,046 cycles

FWD CARGO FLOORBOARD 132AH IS DELAMINATED ON LOWER SURFACE. FABRICATED FWD CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (BULK CARGO) · airframe 11,774 hrs · 7,046 cycles

BULK CARGO FLOORBOARD 161HF IS CRACKED ON LOWER SURFACE FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — BROKEN (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 151UF HONEYCOMB IS BROKEN OUT. REPAIRED AFT CARGO FLOORBOARD IAW EO A300-5320 42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 152MG IS CRACKED AT CORNER. REPAIRED AFT CARGO FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 151SF IS CRACKED AT LOWER SURFACE. REPAIRED AFT CARGO FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 151LG LOWER SURFACE IS PUNCTURED FABRICATED FLOORBOARD IAW EO A300-5320-16407-E.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 152KG IS CRACKED ON LOWER SURFACE. REPAIRED AFT CARGO FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 152UF IS CRACKED ON LOWER SURFACE ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,774 hrs · 7,046 cycles

AFT CARGO FLOORBOARD 151NG IS CRACKED ON LOWER SURFACE. REPAIRED AFT CARGO FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,774 hrs · 7,046 cycles

MAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, Y1137.1. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: CARGO TRACK — CORRODED (FRAMES 80-82) · airframe 11,774 hrs · 7,046 cycles

MAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: CARGO TRACK — CORRODED (FRAMES 80-82) · airframe 11,774 hrs · 7,046 cycles

MAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: CARGO TRACK — CORRODED (FRAMES 80-82) · airframe 11,774 hrs · 7,046 cycles

MAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, -Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 11,774 hrs · 7,046 cycles

SEAT TRACK CORRODED AT FRAMES 80-82, Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: CARGO TRACK — CORRODED (FRAMES 80-82) · airframe 11,774 hrs · 7,046 cycles

MAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, -Y1137.1. REPAIRED CARGO TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBEAM AT FR 79 IS CRACKED AT -Y1137. REPAIRED IAW EA 300-5310-01-A5096 AND EO A300-5310-53627-A.

Part: SKIN — DAMAGED (FRAME 8) · airframe 11,774 hrs · 7,046 cycles

LT FUSELAGE SKIN BLENDOUT AT FRAME 8, NINE INCHES BELOW LAP JOINT REQUIRES PERMANENT REPAIR. REPAIRED SKIN IAW SRM 53-11-12-201, FIG 202, PARA 5B, REV 25.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,774 hrs · 7,046 cycles

MAIN CABIN FLOORBEAM IS CRACKED AT FRAME 79, Y1137. REPAIRED IAW STA EA 300-5310-01-A5096 IR AND EO A300-5310-53627-A.

Part: CIRCUIT BREAKER — INOPERATIVE (SLIDE LIGHT)

SLIDE TC WARNING LIGHT INOPERATIVE WHEN TESTED IAW TSM 52-73-00, FIG 102, BLK 5. R & R CIRCUIT BREAKER (1WN) ON OVERHEAD PANEL, IAW ESPM 20-46-10. OPS CHECKED GOOD IAW AMM 52-73-00-0501.

Part: FLOOR PANEL — CRACKED (LWR FWD CARGO)

FLOOR PANEL CRACKED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-53054-A.

Part: WARNING SYSTEM — MALFUNCTIONED (EVACUATION SLIDE)

EVACUATION SLIDE RELEASE WARNING SYS BUZZER INOPERATIVE. SLIDE WARNING SYSTEM TESTED NORMAL. TESTED PER TSM 52-73. COULD NOT DUPLICATE DISCREPANCY. REPLACED TEST SWITCH 392N AS PRECAUTION IAW ASM 52-73-00. TESTED PER AMM 52-73-14, PARA 2.3.

Part: INDICATOR — INOPERATIVE (DOOR SLIDE)

ESCAPE SLIDE BUZZER INOPERATIVE. PERFORMED OPS CHECK IAW AMM 52-73-00.

Part: PIN — MISSING (CREW DOOR SLIDE)

CREW DOOR SLIDE SAFETY PIN MISSING. PIN REPLACED.

Part: SKIN — DENTED (BS 1499)

DENT LT LWR FUSELAGE BS 1499, STR 52-53L FRAME 21. REPAIRED IAW EO A300-5330-51316-C.

Part: STRUCTURE — DAMAGED (FUSELAGE)

PREVIOUS BLENDOUT AT FASTENER 1.75" FWD OF FRAME 38.2 AT STR 47R REQUIRES REMOVAL OF ADJACENT REPAIR DOUBLER MATERIAL THICKNESS IS 0.098. REPAIRED IAW EO A300-5310-51178-A.

Part: SKIN — DAMAGED (FUSELAGE)

BLENDOUT ON LT FUSELAGE SKIN AT FRAME 6L 10" BELOW LAP JOINT. REPAIRED SKIN REF EO A300-5330-51182-A.

Part: FLOOR PANEL — DAMAGED (FWD CARGO)

FWD CARGO FLOOR PANEL 13256 DAMAGED. FABRICATED NEW FLOOR PANEL IAW EOA300-5320-16407-C.

Part: SKIN — DAMAGED (FUSELAGE)

L/S DAMAGE FR 28, STR 52 RT DAMAGE REMOVED 1.4X1.2. REPAIRED IAW EO A300-5330-49997-A.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL, POS 13 2" FWD OF AFT LINE 3" INBD OF LT SIDE WALL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-16407-E.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 8,902 hrs · 5,332 cycles

INSPECTION TYPE:3C, FWD CARGO FLOOR PANEL 132QG IS CRACKED AT LOWER SURFACE AND BROKEN AT EDGE. FABRICATED FWD CARGO FLOOR PANEL 132QG IAW EO A300-5320-16407-E.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 8,902 hrs · 5,332 cycles

INSPECTION TYPE:3C, DEFERRED ITEM D-459027 - RT FUSELAGE SKIN INTERIM BLEND REPAIR ACCOMPLISHED 5" AFT OF FR38.2, S47R. REPAIRED RT FUSELAGE SKIN 5" AFT OF FR 38.2, S47R IAW SRM 53-10-12 P.B. 201, FIG 208, SHEET 2 AND PARA 11, REV 20.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,902 hrs · 5,332 cycles

INSPECTION TYPE:3C, LT EXTERIOR FUSELAGE HAS DENT AT FR11 JUST FWD OF WASTE WATER CONNECTION BOX. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-12-12, CONFIG-1 FIG 202, PARA 5-8.

Part: SKIN — DAMAGED (BS 1812 S54R)

FUSELAGE SKIN DAMAGED STA 1812 S-54R. REPAIRED IAW A300-5330-43658-A.

Part: WIRE — BROKEN (NLG STEERING)

NORMAL APPROACH, LANDING AND TOUCHDOWN DURING ROLLOUT BETWEEN 60 TO 45 KTS NOSE WHEEL STEERING BECAME INCREASINGLY DIFFICULT TO CONTROL. FOUND BROKEN WIRE AT PIN A OF CONNECTOR 3GC A, REF AWM 32-51-01. REPINNED 3 GCA CONNECTOR IAW ESPM 20-48-53, PROCEDURES FOR NSA 938189 SOCKETS. OPS CKS OF STEERING GOOD IAW AMM 32-51-00-05.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FUSELAGE SKIN DAMAGED FR63 S-50L. REPAIRED PER EO A300-5330-35137-A.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FUSELAGE SKIN DAMAGED AT FRAME 64 JUST ABOVE STRINGER 46L. REPAIRED IAW EO A300-5330-34838. REFERENCE NRC 345572

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A 1 LIGHT OUT EMERGENCY GLARESHIELD CAPT SIDE. RELAMPED, OPS CHECK GOOD IAW IPC 33-12-01-04B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN CARGO DECK 262 AREA HAS FLOORBOARD 262GH WITH UPPER SKIN PUNCTURED. PERMANENTLY REPAIRED FLOOR PANEL IAW A300-600 SRM 35-10-20, TABLE 201 PARG 8A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN CARGO DECK FLOORBOARD 252 JF HAS PUNCTURE ON THE FWD I/B CORNER AT UPPER SKIN. PERMANENTLY REPAIRED FLOOR PANEL 252 JF IAW A399-600, SRM 53-10-20, TABLE 201 PARG 8A.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 231 XG IS CRACKED. FABRICATED REPLACEMENT MAIN CABIN FLOORBOARD 231 XG IAW IPXA EO A300-5320-16407-C APPX B.

Part: DOUBLER — DAMAGED (TE FLAP) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR REPAIR SURVEY SEQUENCE NUMBER 157-W3-01. EXT DOUBLER LEFT I/B FLAP UPPER SKIN BETWEEN RIBS 1C-3 STR 2.1-2.2 HAS GOUGE DAMAGE. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW SAA EA 300-5752-01-A0411 REV A AND IPXA EO A300-5750-32666-A.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN CARGO DECK FLOORBOARD 252UJ HAS I/B AFT CORNER CRACKED. FABBED FLOOR PANEL IAW EO A300-5320-16407-C APPX B.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 232 XG IS CRACKED. FABRICATED REPLACEMENT MAIN CABIN FLOORBOARD 232 XG IAW IPXA EO A300-5320-16407-C APPX B.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN DECK FLOORBOARD 242 LT IS CRACKED. FABRICATED REPLACEMENT MAIN DECK FLOORBOARD 242 LT IAW IPXA EO A300-5320-16407-C APPX B.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 5,855 hrs · 3,538 cycles

INSPECTION TYPE:5 YR MAIN DECK FLOORBOARD NR 261DM IS CRACKED. FABRICATED REPLACEMENT MAIN DECK FLOORBOARD IAW IPXA EO A300-5320-16407-C.

Part: HYDRAULIC SYSTEM — FAILED

LOSS OF GREEN HYDRAULIC SYSTEM.

Part: LIGHT — LOW (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS ARE DIM. CYCLED C/B U82 AS SVC CONTROL DMP 33-51-08, SYS CHECKS NORMAL IAW AMM 33-51-00-05.

Part: LIGHT — INOPERATIVE (COCKPIT)

FOUND CENTER INST PANEL LEFT EMERGENCY LIGHT INOP. RELAMPED. OPS CK GOOD.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 98 hrs · 59 cycles

43R INTERCOSTAL DAMAGED AT FRAME 57-58 RT. FABRICATED NEW INTERCOSTAL & INSTALLED IAW A300 SRM 51-26-00 AND PER SAMPLE IAW UPS GMM 5-9-2.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 98 hrs · 59 cycles

A/C SKIN DAMAGED BY GSE APPROX AT STRINGER 42R-54R AT FRAME 58. REPLACED STRINGERS 44R & 45R INTERCOSTAL 43R AND REPAIRED SKIN DAMAGED IAW REO-GO9854.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 98 hrs · 59 cycles

STRINGER 45R DAMAGE AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 98 hrs · 59 cycles

STRINGER 44R DAMAGED AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21.