N137UP

Part: WINDOW — ARCED (ZONE 200) · airframe 28,360 hrs · 17,302 cycles

DURING DESCENT AT 8000 FT WINDOW ARCHING OBSERVED ON CAPTAIN€™S SIDE WINDSCREEN, AFTER FOLLOWING QRH PROCEDURE TO TURN OFF WINDOW HEAT CAPTAINS WINDSHIELD CRACKED AND EXPANDED ACROSS WINDSHIELD. ACCOMPLISHED RII ITEMS FOR R1 WINDOW INSTALL IAW AMM 56-11-11/401.

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 28,360 hrs · 17,302 cycles

DURING DESCENT AT 8000 FT WINDOW ARCHING OBSERVED ON CAPTAIN`S SIDE WINDSCREEN, AFTER FOLLOWING QRH PROCEDURE TO TURN OFF WINDOW HEAT CAPTAIN`S WINDSHIELD CRACKED AND EXPANDED ACROSS WINDSHIELD. REMOVED AND REPLACED CAPTAIN'S FORWARD WINDSHIELD, OPS CHECK GOOD, IAW AMM 56-11-11/0401. ACCOMPLISHED RII ITEMS FOR R1 WINDOW INSTALL IAW AMM 56-11-11/401.

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 27,907 hrs · 17,052 cycles

SLIDE LEVER WAS EXTREMELY DIFFICULT TO DISARM AFTER SHUTDOWN PRIOR TO OPENING DOOR. PERFORMED OPERATIONAL TEST OF THE MAIN DOOR SLIDE LEVER REF. AMM 25-61-21/401. OPS CHECK GOOD. NO DEFECTS NOTED. BACK PRESSURE CAUSED DUE TO GROUND AC CART WAS CONNECTED BEFORE OPENING MAIN DOOR. AIRCRAFT OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 27,556 hrs · 16,862 cycles

UPON ARRIVAL FLT CREW COULD NOT OPEN CABIN DOOR FROM INSIDE ADJUSTED GIRT AND GIRT BAR W/R/T MM 25-61-21. VERIFIED DOOR LOCK IND FUNCTIONS. GOOD FOR SERVICE AT THIS TIME.

Part: DAMPER — FAILED (NLG PITCH) · airframe 27,355 hrs · 16,745 cycles

LANDING GEAR RETRACTION FAULT UNABLE TO RETRACT.INSTALLED LOCKS ON MLG DOOR ACTUATORS IAW AMM 32-12-11/301 AND INSTALLED LOCKS ON NLG DOOR ACTUATORS IAW AMM 32-22-11/301.

Part: PIN — CORRODED (ZONE 600) · airframe 27,355 hrs · 16,744 cycles

FAULT: APG/ RH WING CENTER FLAP TRACK 3 PIN FLAP AND SLEEVE-LOCKING CORRODED REVIEWED

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 27,357 hrs · 16,747 cycles

FAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 27 AFT, AREAS CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776.

Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 27,357 hrs · 16,747 cycles

FAULT: LH CENTER FLAP CRACK FOUND IN RIB 13 AFT, AREA CIRCLED IN RED.ACCOMPLISHED REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3777.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 27,357 hrs · 16,747 cycles

FAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 26, AREA CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776

Part: FRAME — CRACKED · airframe 27,355 hrs · 16,745 cycles

CRACKS FOUND ON RH FR 47 HORIZONTAL JUNCTION HOLES F, B AND Q REVIEWEDROTO PERFORMED ON HOLE B. NO DEFECTS FOUND IAW NTM 51-10-01. T96525 T91779. COMPLIED WITH EO# 300-5710-27-A3775 PRELIM 1 STEP #2

Part: STRINGER — BENT (ZONE 100) · airframe 27,355 hrs · 16,744 cycles

R/H T.H.S COMP BETWEEN FRAME 86-87, STRINGER AT THE 7*CLOCK POSITION IS BENT. DOT 33-002. INSTALLED NEW PARTS AT FRAME 86-87, STRINGER AT THE 7*CLOCK POSITION IAW A300-600 SRM 51-40-21 WITH SEALANT P/N: 04-001-010P BACTH#: 0004318644 AND FASTENERS MS20426AD4-6 BACTH #:0004228197 AND P/N: DAN5-5-2 BACTH#: 004139128. AND OK TO RESTORE.

Part: FRAME — CRACKED (ZONE 100) · airframe 27,355 hrs · 16,744 cycles

CRACK FOUND ON LH FR47 HORIZONTAL JUNCTION HOLE S. ACCOMPLISH THE REPAIR PER EA 300-5710-27-A3774 REV. -.

Part: STRINGER — BENT (ZONE 100) · airframe 27,355 hrs · 16,744 cycles

R/H T.H.S COMP BETWEEN FRAME 86-87, STRINGER AT THE 8*CLOCK POSITION IS BENT. DOT 33-001. INSTALLED NEW PARTS AT FRAME 86-87, STRINGER AT THE 8*CLOCK POSITION IAW A300-600 SRM 51-40-21 WITH SEALANT P/N: 04-001-010P BACTH#: 0004318644 AND FASTENERS MS20426AD4-6 BACTH #:0004228197 AND P/N: DAN5-5-2 BACTH#: 004139128. AND OK TO RESTORE SURFACE.

Part: PLATE — CRACKED (ZONE 400) · airframe 27,355 hrs · 16,744 cycles

#2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER CRACKED-DOT 139/18-MR/139. NSTALLED PLATE AT #2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER IAW A300-600 SRM 51-40-21. FASTENER PN:NAS1200M4-7, BN:0004171072, PN:MS21060-3, BN:0004201914, PN:CCR264SS3-04, BN:0004331647.

Part: RIB — CRACKED (ZONE 400) · airframe 27,355 hrs · 16,744 cycles

FAULT-STR-Z400-#2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL CHANNEL CRACKED-DOT 139/21-MR/139. INSTALLED BLEED AIR PRECOOLER IAW AMM 36-11-15-0401. INSTALLED SPLICE BRACKET AT #2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL IAW SRM 51-40-21. REVIEWED

Part: BRACKET — BROKEN (ZONE 500) · airframe 27,355 hrs · 16,744 cycles

LH WING, CENTER FLAP, O/B EDGE HAS BRACKET BROKEN. DOT 103-62. REMOVERD AND REPLACE BRACKET AT L/H WING CENTER FLAP. FABRICATED BRACKET:P/N 2024-T3 0.32B BATCH 0004247650 P/N C3213-5-08 BATCH: 00044268033 IAW A300-600 SRM 51-40-21.

Part: BRACKET — CRACKED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

FR10 R/H SIDE HAS A CRACKED CEILING CORNER BRACKET. DOT 60-001. INSTALLED BRACKET IAW A300-600 SRM 51-40-21, HILOCK P/N: DAN5-6-4, BATCH # 0004128103.

Part: SKIN — GOUGED (ZONE 500) · airframe 27,355 hrs · 16,744 cycles

LH WING, LOWER SURFACE, NEAR STA 0,(ROOT), UNDER I/B FLAP, NEXT TO I/B FLAP TRACK HAS GOUGE. DOT 103-35. FABRICATED NEW SKIN, TOP STUB IAW A300 57-51-12. PN: 2024-T3 .050C, BN: 0004328497

Part: SKIN — DENTED (ZONE 600) · airframe 27,355 hrs · 16,744 cycles

R/H WING, AT O/B SLAT TIP, ON WING L/E SKIN WITH DENT. DOT 73-002. INSTALLED NEW PART SHOULD WING TIP ON RH WING WITH FASTENERS P/N# CR3212-4-2 BTCH#4349652, P/N# CR3212-6-7 BTCH#4262361, P/N# 04-001-0169 BTCH# 4263295 IAW A300-600 SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN DECK FLOOR PANEL 262DM IS BROKEN DOT CL 2. FABRICATED FLOOR PANEL 262DM USING PN: 5024N400001SS-G BATCH: 0004055277 PN: 04-001-0012 BATCH: 0004143182 PN: G2002B-3S BATCH: 0043483 PN: G2002B-3P BATCH: 000426239 IAW SREO-16407-REQ001. OSD: 1/27/2025

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN DECK FLOOR PANEL 251ZG IS BROKEN DOT CL 1. FABRICATED FLOOR PANEL 251ZG.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 27,355 hrs · 16,744 cycles

BASE FRAME FITTING FR46 LH HAS SUSPECTED CRACK. NO DOT. INSTALLED NEW REPAIR PARTS AT FR46 LH SHIM, DOUBLER AND STIFENER WITH HARDWARE INCLUDED IN THE KIT P/N#536177A44R00 BATCH N#4357712, HRDW P/N# EN6115V3X9, EN6115V3X10, EN6115V3X11 ASNA2528-3 IAW SRM 51-40-21.

Part: BRACKET — CRACKED (ZONE 100) · airframe 27,355 hrs · 16,744 cycles

AVIONICS COMP. FLOORS, UNDER 121CF FLOOR PANEL, NEAR FR4, ELECTRICAL WIRE BRACKET SUPPORT IS BROKEN. DOT 103-01. INSTALLED NEW BRACKET UNDER PANEL 121CF NEAR FR4 IAW A300-600 SRM 51-40-21. JOB COMPLETE

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,381 hrs · 16,763 cycles

MAIN CABIN CLS ADAPTER FR61 Y0 RH HAS CORROSION NOTED. DOT 7628/09 INSTALLED CLS ADAPTER P/N A53275455200 ON FR61 RH Y0 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. REVIEWED

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR65 Y0 LH HAS CORROSION NOTED. DOT 7628/07 VERIFIED STEP #15, JOB COMPLETE.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR65 Y0 LH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 ON FR65 Y0 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92460-REQ1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN SEAT TRACK FR80 Y794.3 HAS CORROSION NOTED. DOT 7628/05. INSTALLED NEW SEAT TRACK SECTION FR80 WTH FAST P/N: HL70-8 BATCH: 4353581, P/N: NAS1097DD6 BATCH: 4244840 IAW A300-600 SRM 51-40-21. REVIEWED

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR66 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR63 Y0 RH HAS CORROSION NOTED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH UPS E0-92459-REQ1.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR63 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR60 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR60 Y0 RH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 ON FR60 Y0 RH IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92457-REQ1.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR61 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN SEATRACK FR80 Y794.3 HAS CORROSION NOTED.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,355 hrs · 16,744 cycles

MAIN CABIN CLS ADAPTER FR66 Y0 RH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT.

Part: WARNING LIGHT — ILLUMINATED (CABIN PRESSURE) · airframe 27,328 hrs · 16,731 cycles

AFTER SHUTDOWN WITH PACKS OFF, RED EXCESSIVE CABIN PRESSURE LIGHT ILLUMINATED ON CARGO DOOR CONTROL PANEL CHECKED FOR CONTINIUITY AND NORMAL OPERATION OF 13WN (L1 DOOR ESCAPE SLIDE MICRO SWITCH) AND 9WN (L1 DOOR MICRO SWITCH) BOTH SWITCHES CHECKED GOOD IAW ASM 52-73-00 SHEET 1, DID FIND 13WN TO BE STICKY WITH CPC ANTI-CORROSION COMPOUND. CLEANED 13WN MICRO SWITCH IAW ESPM 20-55-50. AWAITING OPS CHECK

Part: SLIDE — FAULTED (ZONE 800) · airframe 27,243 hrs · 16,687 cycles

SLIDE WARNING LIGHT DOES NOT ILLUMINATE WITH PRESS TO TEST PERFORMED ASPSU BITE TEST PER AMM 52-73-00/501, NO DISCREPANCIES NOTED, PERFORMED DOOR SLIDE WARNING LIGHT TEST PER AMM 52-73-00/401 AND OPERATION CHECKS GOOD , THIS CLEARS DMI,PLACARD REMOVED.

Part: CONTROLLER — FAULTED (PNEUMATIC SYS) · airframe 27,197 hrs · 16,666 cycles

**EMERGENCY DECLARED** DURING DESCENT, BLEED #2 FAULT, RAN ECAM / AOM PROCEDURE ACCOMPLISHED #2 ENG RUN, AND ACCOMPLISHED BITE TEST OF #2 PNEUMATIC PRESSURE CONTROLLER, BLEED VALVE OPS CHECKED GOOD AT THIS TIME AND NO FAULTS DISPLAYED IAW AMM 71-00-00 TABLE 501 TEST 3A AND AMM 36-11-00/501.

Part: ROD — BROKEN (ZONE 600) · airframe 27,175 hrs · 16,655 cycles

RH WING #1 SPOILER CONNECTING ROD BROKEN. INSTALLED/ADJUSTED RIGHT WING SPOILER #1 AND NEW CONNECTING ROD ASSY IAW AMM 27-61-54-401. OPS CHECK GOOD. COMPLIED WITH RII STEPS PER GMM 04.02.01.15.

Part: ROD — BROKEN (ZONE 600) · airframe 27,169 hrs · 16,652 cycles

RH WING #1 SPOILER CONNECTING ROD BROKEN REMOVED RIGHT WING #1 SPOILER IAW AMM 27-61-54-401. AWAITING PARTS.

Part: HYDRAULIC LINE — LEAKING · airframe 27,111 hrs · 16,617 cycles

LOST YELLOW HYD QUANTITY. ECAM YELLOW SYS LO PR. YELLOW LO PR LIGHT ON OVERHEAD FOLLOWED QRH/ECAM PROC DIVERTED BACK TO SDF. REPLACED THE YELLOW SYSTEM AILERON PRESSURE LINE REF AMM 20-23-11 AND EO A300-2910-60058-C. LEAKS CHECKS GOOD

Part: HYDRAULIC SYSTEM — LEAKING (ZONE 100) · airframe 27,106 hrs · 16,611 cycles

AIR TURN BACK, LOST YELLOW HYD QUANTITY. ECAM YELLOW SYS LO PR. YELLOW LO PR LIGHT ON OVERHEAD FOLLOWED QRH/ECAM PROC DIVERTED BACK TO SDF.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 26,257 hrs · 16,097 cycles

WHEN CLOSEING THE CARGO DOOR A PUNGENT SMELL STARTED BY THE CREW ENTRY DOOR. IT WAS HARD TO BREATHE WITHOUT COUGHING. SUSPECT HYD FLUID. OPEN

Part: UNKNOWN — ODOR (CABIN) · airframe 26,294 hrs · 16,119 cycles

WHEN CLOSEING THE CARGO DOOR A PUNGENT SMELL STARTED BY THE CREW ENTRY DOOR. IT WAS HARD TO BREATHE WITHOUT COUGHING. SUSPECT SKYDROL (HYD FLUID). ACCOMPLISHED REPAIR OF HYD TUBING AT MCD SELECTOR VALVE. REF AMM 20-23-11 PARA.5, H RYNGLOK REPAIR. OPERATED MCD SEVERAL CYCLES NO LEAKS NOTED. OKAY FOR SERVICE

Part: RELAY — UNKNOWN (UNKNOWN) · airframe 25,854 hrs · 15,838 cycles

*** ATB *** L/G RETRACTION INOP AFTER T/O LANDING GEAR LEVER WOULDN€™T MOVE TO THE UP POSITION.COMPLETED ECAM AND PERFORMED AN ATS, WHILE OPERATING IN SYSTEM 2 REPLACED NLG RELAY 14GB, AND MLG RELAYS 17GB AND 18GB IAW ESPM 20-46-50. PERFORMED GEAR SWING ION SYSTEM 2 IAW AMM 07-11-00, OPS CHECK GOOD.

Part: BEAM — CRACKED (FWD CARGO DOOR) · airframe 25,852 hrs · 15,836 cycles

INSPECTION TYPE:SVFR20A CRACKED AT BEAM 3REMOVED AND REPALCED FR20A IAW DWG A52370600,A52370610 AND A52370650

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 25,852 hrs · 15,836 cycles

INSPECTION TYPE:SV*MAJOR REPAIR* SKIN CRACKED ON C20A AT BEAM 3REPAIRED PER AIRBUS RDAF 81286150/03/2023#A AND UPS EO A300-5230-88313

Part: DOOR — CRACKED (FWD CARGO) · airframe 25,850 hrs · 15,835 cycles

INSPECTION TYPE:NA*SDR FILED OPEN* FOUND CRACK FWD LOWER CARGO DR LE BY DR LOCK HANDLE. ACCOMP A300-5230-88237-A FWD LOWER CRGO DR FWD EDGE DAMAGE AT FRAME 20A TO BEAM 3 FEF STEP 60A1 THRU 6 & TRANSFERRED ITEM TO DMI LOG REF D-812622 ASSIGNED FERRY PERMIT 9062 ISSUED VTO OPERATE A ONE TIME NON REVENUE FLIGHT TO KBFM IN AN UNPRESSURIZED CONDITION

Part: PIN — INOPERATIVE (DOOR) · airframe 25,500 hrs · 15,584 cycles

INSPECTION TYPE:NAPOST FLT.. - MAIN ENTRY DOOR SLIDE PIN HARD TO SEAT INTO DISARMED POINT.PLACED EMERGENCY CONTROL HANDLE IN DISARM POSITION AND INSTALLED SAFETY PIN WRT A300 AMM 52-10-00..

Part: CONTAINER — ODOR (LAVATORY TRASH) · airframe 25,192 hrs · 15,390 cycles

SHORLTY AFTER TAKEOFF , CREW SMELLED ACRID SMELL FROM PACKS. TRANIENT BUT STRONG.LAVATORY SVC'D BY AIR TO GROUND, MOLDY SMELL COMING FROM TRASH , CLEANED WITH ALCOHOL. RAN PACKS 1,2 AND 1&2 TOGETHER IAW AMM 21-51-14. COULD NOT REPLICATE ANY ACRID SMELL. ORIG SUBMISSION DATE: 1/18/2023

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 25,129 hrs · 15,352 cycles

EMERGENCY LIGHT, IS BURNED OUT IN THE DIM POSITION IN LAV. REMOVED & REPLACED DIM LAMP IN LAVATORY IN REFERENCE TO 33-51-21-0401.OPS CHECKED GOOD.

Part: ACCUMULATOR — INOPERATIVE (MLG BRAKE SYS) · airframe 24,998 hrs · 15,285 cycles

BRAKE ACCUMULATOR WILL NOT HOLD PRESSURE. BLEEDS DOWN SIGNIFICANTLY BELOW GREEN BANS MINUTES AFTER CHARGING WITH PARKING BRAKE APPLIED. PRESS CHRG WITHIN LIMITS PER AMM 32-45-00-501, DEFERRED PER MEL 32-42-08, M797134, DMP C/W PER MEL 32-42-08.TECH RECOMMENDS R&R SYS BRAKE ACCU PRESS TRANSMITTER IAW A300 AMM 32-74-22-401 LEAK AND OPS CK GOOD.

Part: WATER SEPARATOR — CONTAMINATED · airframe 24,852 hrs · 15,188 cycles

IMMEDIATELY AFTER TAKE OFF HAD "WET SOCK" SMELL IN COCKPIT. LASTED APPROX 30 SECONDS. PACK 1 OPERATING SE E PREV WRITE UP LOG PAGE 225135 ALSO SEE PREVIOUS LOG PAGE 225134 FOR #1 ENG"OIL WETTING EVIDENT IN INLET COWL COWL " AGAIN DURING DESUNABLE TO DUPLICATE "WET SOCK SMELL" ON GROUND. AD PRECUATIONAR SERVICED #1 PACK WATER SEPERATOR AS PER MM CHPTR 21-1-16. RAN PACK PACK FOR PERIOD OF TIME AS PER MM CHPTR 21-11-00 NO ISSUES NOTED. C/W CK NO 13 OIL LK CK. NO FURTHER ISSUES NOTED. OK TO CONT SERVICE REF A300 TSM 72-00-40

Part: A/C PACK — ODOR (NR 1) · airframe 24,839 hrs · 15,177 cycles

INSPECTION TYPE:N/ASTRONG WET SOCK SMELL ON DEPARTURE & ARRIVAL IN CLEAR AIR NO CLOUDS PACK #1 WAS IN USEPERFORMED OPERATIONAL CHECKOUT OF BOTH #1 AND #2 PACKS SEPERATELY WITH ENGINES RUNNING PER AMM 21-11-00. NO SMELL DETECTED OK FOR CONTINUED SERVICE

Part: LONGERON — ELONGATED (485 AL) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:1CPANEL 485AL HAS ELONGATED HOLES ALONG ENTIRE LENGTH OF THE PANEL ON THE I/B SIDE AS MARKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — CRACKED (RH WING FLAP) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:1CRH WING TRAILING FLAP, BETWEEN BOTH FLAPS AFT HAS BROKEN BRACKET.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: STRIP — CRACKED (#2 ENG) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:1C#2 ENG I/B PYLON LOWER ABOVE T/R ANTI CHAFE STRIP PLATE BROKENREMOVED AND REPLACED IAW SRM 51-40-21.

Part: STRIP — BROKEN (#2 ENG I/B T/R) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:1C#2 ENGINE I/B T/R UPPER T/E ANTI-CHAFFE STRIP PLATE BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: INTERCOSTAL — CRACKED (R/H WING) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:CRT WING BELOW #3 SPOILER I/B HINGE ARM END RIB INTER-COSTAL WEB CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: BRACKET — CRACKED (LH WING) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:CLH WING RIB 10 IS CRACKED LOWER I/B SIDE OF SPOILER #3REMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: BRACKET — CRACKED (#1 PYLON 475AL) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:C#1 PYLON AFT FAIRING 475AL FWD RIB C-ANGLE BRACKET CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: PANEL — CRACKED (#1 ENG) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:C#1 ENG PYLON AT RIB 3 FWD OF PRE-COOLER PANEL SUPPORT STRUCTURE CRACKEDREMOVED WELDED AND INSTALLED IAW SRM 51-40-21

Part: WEB — DAMAGED (#1 ENG I/B T/R) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:C#1 ENG I/B T/R COWL AT RIB 6 UPPER INNER EDGE PUNCTURED/DAMAGEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: BULKHEAD WEB — CRACKED (#1 ENG BULKHEAD) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:C#1 ENG NOSE COWL AFT BULKHEAD AT 9:00 POSITIO CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: WEB — DAMAGED (#1 ENG I/B T/R) · airframe 24,607 hrs · 15,037 cycles

INSPECTION TYPE:C#1 ENG O/B T/R COWL AT RIB 6 UPPER INNER EDGE PUNCTURED/DAMAGEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: WEB — CRACKED (L/H KRUGER FLAP) · airframe 24,606 hrs · 15,036 cycles

INSPECTION TYPE:CLH WING FWD SPAR WEB CRACED O/B OF KRUGER FLAP ACTUATORREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: STRING — CRACKED (L/H KRUGER FLAP) · airframe 24,606 hrs · 15,036 cycles

INSPECTION TYPE:CLH WING KRUGER FLAP AREA STIFFNER P/N A5724228420800 IS CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: ANGLE — CRACKED (L/H KRUGER FLAP) · airframe 24,606 hrs · 15,036 cycles

INSPECTION TYPE:CLH WING KRUGER FLAP AREA ANGLE P/N A572424207120200 IS CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: NONE — INOPERATIVE (CABIN) · airframe 24,416 hrs · 14,923 cycles

INSPECTION TYPE:NAREF;M781500 COURIER/SUPERNUMARARY AREA INTERIOR EMERGENCY LIGHT SYSTEM INOPR&R'D EMERGENCY POWER SUPPLY BATTERY (BATTERY FAULT DISPLAYED ON BITE TEST) IN REFERENCE TO AMM 33-51-14 OPS NORMAL AT THIS TIME. THIS CLEARS M781500. PLACARD REMOVED. EFF. SOURCE REF. 33-51-14-01.

Part: CONNECTOR — NOT SEATED (SLIDE WARNING) · airframe 21,527 hrs · 13,289 cycles

EVACUATION SLIDE RELEASE WARNING SYSTEM BUZZER VERY FAINT. REMOVED AND RESEATED THE ELECTRICAL CONNECTOR FROM ASPSU. OPS CHECKED DOOR WARNING SYSTEM WAS GOOD IAW AMM 52-73-00-0501.

Part: FITTING — GOUGED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG MCD FR 47 SPLICE FITTING AT STR 24-26L SIDE HAS GOUGES. REPAIRED SPLICE FITTING GOUGES IAW EA 300-5710-27-A2458.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG RT WW BULKHEAD PANEL HAS SEAL FLANGE EXFOLIATED AND CRACKED. REMOVED AND REPLACED PART IAW SRM 51-40-21.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG OB TR AFT UPPER CORNER DAMAGED. REPAIR PER EO A300-7830-50286-C.

Part: BUSHING — MISSING (RT MLG WW) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG RT WW BULKHEAD PANEL (1) BUSHING MISSING AT HINGE. REMOVED & REPLACED HINGE FITTING IAW SRM 51-40-21.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG OB TR AFT UPPER CORNER DAMAGED. REPAIRED PER EO A300-7830-50286-C.

Part: LONGERON — WORN (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG NR 2 PYLON FAIRING RT UPPER CENTER LONGERON HAS WORN HOLES. REMOVED & REPLACED IAW SRM 51-40-21.

Part: CARGO TRACK — CORRODED (MAIN CARGO) · airframe 21,525 hrs · 13,287 cycles

MCD TIE DOWN HAD CORROSION AROUND TRACK O CROSSBEAM. REMOVED CORROSION (OUT OF LIMITS). REMOVED AND REPLACED ADAPTERTRACK IAW EO A300-5310-76843-A.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C, FWD CARGO FLOOR PANEL 132FE DAMAGED, FABRICATED A NEW FLOOR PANEL IAW SREO A300-5320-40552-B, AND A300-5320-76594-B.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C, INBD THRUST REVERSER TOP AFT BRACKET WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-21.

Part: CARGO TRACK — CORRODED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C, MAIN CARGO TRACK CORRODED NEXT TO TRACK 0 CROSSBEAM 27. REMOVED AND REPLACED SECTION ADAPTER IAW SRM 51-40-21.

Part: BRACKET — BROKEN (NR 1 NOSE COWL) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG NR 1 ENGINE NOSE COWL LOWER LT SIDE BRACKET BROKEN. REMOVED AND REPLACED NR 1 ENG NOSE COWL LT SIDE BRACKET IAW AMM 71-11-00-0401.

Part: STRIP — CORRODED (LT MLG WW) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG LT W/W FWD CENTER BULKHEAD PANEL CLOSEOUT STRIP CORRODED. REMOVED AND REPLACED CLOSEOUT STRIP IAW SRM 51-40-21.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG FLOORDBOARD 252LM DAMGED. FABBED PNL 252LM FROM 5024N400001SS-G BAT 3546253 PER SREO A300-5320-40552-B.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C RT WING TOP HAS POSSIBLE CRACK ON PANEL FWD OF SPOILER NR 5 AND LOOSE FASTENERS. REPAIRED SKIN PANEL IAW SRM 57-51-12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT CARGO COMPARTMENT CEILING PANEL SUPPORT STRUCTURE FR57 CENT SECTION CORRODED. REPLACED IAW SRM 51-40-21.

Part: BRACKET — BROKEN (THRUST REVERSER) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG NR 2 ENG O/B T/R BIFURCATION LATCH BAND RETAINING BRACKET BROKEN. REPLACED IAW SRM 51-41-21.

Part: STRUCTURE — CHAFED (RT MLG WW) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG RT W/W FWD BULKHEAD PANEL, 1EA CHAFED AREA ON FLANGE. REPLACED FLANGE EXTRUSION IAW SRM 51-40-21.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C NR 2 PYLON O/B SIDE ABOVE T/R PLATE CRACKED. REPLACED IAW SRM 51-40-21.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C NR 2 PYLON O/B SIDE ABOVE T/R PLATE CRACKED. REPLACED IAW SRM 51-40-21.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C NR 2 PYLON O/B SIDE ABOVE T/R PLATE CRACKED. REPLACED IAW SRM 51-40-21.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C NR 2 PYLON O/B SIDE ABOVE T/R PLATE CRACKED. REPLACED IAW SRM 51-40-21.

Part: DEFLECTOR — BROKEN (TE FLAP) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C RT WING CENTER FLAP O/B SIDE WATER DEFLECTOR BROKEN. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: DEFLECTOR — MISSING (TE FLAP) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C LT CNT FLAP O/B SIDE WATER DEFLECTOR MISSING. REPLACED IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C FWD PIT FLOOR PANEL 132DE IS DAMAGED. FABBED NEW PANEL IAW EO A300-5320-16407-E AND A300-5320-76594-B.

Part: CHANNEL — CORRODED (LT MLG WW) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C LT W/W FWD BULKHEAD PANEL HAS CORROSION WITH FLANGE LIFTING AT ATTACH AREA. REMOVED AND REPLACED CHANNEL IAW 51-40-23.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT PIT FLOOR PANEL 151VF MISSING EDGE SECTION. FABBED PANEL IAW EO A300-5320-76594-A AND EO A300-5320-16407-E.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT CARGO PBH TRACK -Y953 HAS 2 ANGLES CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: LONGERON — DAMAGED (PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C PYLON NR 1 LOWER AFT FAIRING 475AL UPPER EDGE 4EA FASTERNER HOLES ELONGATED. REMOVED AND INSTALLED NEW LONGERON IAW SRM 51-40-21.

Part: TIE DOWN — CORRODED (MCD) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C MCD TRACK TIE DOWN HAS CORROSION AROUND BET TRACKS Y1456/Y1959 CROSS BEAM 25. REMOVED CORROSION IAW SRM 53-10-16 FIG 101.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT CARGO COMP ABOVE PBH TRACK -Y5919 HAS ANGLE SUPPORT CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT CARGO PBH TRACK Y953 HAS ANGLE CRACKED. REMOVED AND REPLACED NEW BRACKET IAW SRM 51-40-21.

Part: PIN — WORN (NR 2 FAN COWL) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C NR 2 ENGINE I/B ALIGNMENT PIN AND RECEIVER WORN. REMOVED AND REPLACED ALIGNMENT PIN AND RECEIVER.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 AFT PIT FLOOR PNL 152NG HAS MISSING EDGE FILLER. FABBED FLOOR PANEL IAW EO A3005320-76594-A AND EO A300-53220-16407-E.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 FWD PIT FLOOR PANEL 132PG IS BROKEN. FABBED PANEL IAW EO A300-5320-76594 AND EO A300-5320-16407-E.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 MCD SUPPORT FLOOR STRUCTURE CRACKED BET-Y 450 AND -Y953 CROSSBEAM 51. REMOVED AND INSTALLED CROSSBEAM IAW EO A300-5310-75878-B.

Part: FLOOR PANEL — DELAMINATED (BULK CARGO) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C BULK PIT FLOOR PANEL 161MF IS DELAMINATED. FABBED FLOOR PANEL IAW EO A300-5320-16407-E AND EO A300-5320-76594-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 FWD PIT FLOOR PANEL IS DELAMINATED ON LOWER SKIN. FABBED PANEL IAW EO A300-5320-76594-A AND A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C AFT PIT FLOOR 152UF LOWER SKIN IS DAMAGED. FABBED PNL IAW EO A300-5320-10407 AND EO A300-5320-76594.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 AFT CARGO FLOOR PANEL 151LG HAS MISSING EDGE FILLER AND LOWER SKIN DAMAGE. FABBED PANEL IAW EO A300-5320-16407-E AND A300-5320-76594-A.

Part: FLOOR PANEL — BROKEN (BULK CARGO) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:C BULK CARGO FLOOR 162MF HAS BROKEN CORNER. FABBED FLOOR PANEL IAW EO A300-5320-76594-A AND EO A300-5320-16407-E.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 WHEEL WELL FLOOR PANEL DELAM/OIL SOAKED. FABBED NEW PNL IAW EO A300-5320-57698-A & SREO A300-5320-16407-E.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 251FJ DAMAGED. FABBED 251FJ FROM 502N40000155-G BAT NR 3546255 PR SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 231SG DAMAGED. FABBED 231SG FROM 5024N40000155-G BAT NR 3546253 IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 31NJ DAMAGED. FABBED PNL 231NJ FROM 5024N40000155-G BAT 3546253 IAW SREO 5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 FLOORBOARD 242DQ DAMAGED. REPAIRED FLOORBOARD 242DQ PER SREO A300-5320-42722-F.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 251XG DAMAGED. FABBED PNL 251XG FROM 524N40000155-G BAT NR 3546253 IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 232SG DAMAGED. FABBED NEW PNL 232SG FROM 5024N40000155-G BAT NR 3546253 IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE SEG FLOORBOARD 231LH DAMAGED. FABBED PANEL 231LH PN B5327072800000 FROM 5024N40000155-G BAT NR 3546253 IAW SREO A300-5320-40522-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 FLOORBOARD 241BJ DAMAGED. REPAIR FLOORBOARD 241BJ PER SREO A300-5320-42722-F.

Part: SKIN — CORRODED (NR 1 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:SEG 1 PYLON O/B ON LOWER WING SURFACE HAS BARE METAL AND PITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-10. IN LIMITS SRM 57-20-12

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 MCD SUPPORT STRUCTURE CRACKED BET TRACKS-Y450 AND -Y953 CROSS BEAM 48. INSTALLED NEW CROSS BEAM IAW EO A300-5310-75878-B.

Part: FLOORBOARD — DAMAGED (MCD) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE A300 FLOORBOARD 251CN DAMAGED. FABBED PNL 251CN FROM 5024N400001SS-G BAT 3546253 PER SREO A300-5320-40552-B.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE A300 MCD SUPPORT FLOOR STRUCTURE CRACKED BETWEEN -Y450 AND -Y953 CROSS BEAM 50. INSTALLED NEW CORROSION IAW EO A300-5310-75878-B.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE A300 MCD FLOOR STRUCTURE CRACKED BETWEEN TRACKS-Y450 AND -Y953 CROSSBEAM 49. INSTALLED NEW CROSSBEAM IAW EO A300-5310-75878-B.

Part: BRACKET — DAMAGED (LE SLAT) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 NR 3 SLAT NR 10 TRACK CLOSE PANEL HAS DAMAGE. REPLACED BRACKET ON TASK CARD 574402-01-1-522.

Part: SUPPORT FRAME — BROKEN (FUSELAGE) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 E AND E BAY FLOOR LT SIDE BELOW PANEL 121TF 1 CLAMP SUPPORT FRAME BROKEN. REMOVED OLD SUPPORT AND INSTALLED NEW SUPPORT FRAME PN A9242628900001 IAW SRM 51-40-21.

Part: WEB — CRACKED (NR 1 NOSE COWL) · airframe 21,525 hrs · 13,287 cycles

NR 1 ENGINE NOSE COWL AFT 49306-A BACK AT NINE O'CLOCK POSITION CRACKED AROUND STATIC TUBE. NEW WEB AND SPLICE PLATE LOWER ANGLE IAW SRM 51-40-21 AND PW SRM 54-10-00 FIG 201 REPAIR 14

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE A300 AFT PIT FLOOR PANEL 152SF HAS BROKEN CORNER. FABBED PANEL IAW SREO A300-5320-76594-A AND EO A300-5320-16407-E.

Part: STRUCTURE — DAMAGED (NR 2 PYLON) · airframe 21,525 hrs · 13,287 cycles

INSPECTION TYPE:A300 NR 2 PYLON AFT FIXED FAIRING LT HAS ELONGATED HOLES. REMOVED AND REPLACED T CHORD IAW SRM 51-40-44.

Part: HANDLE — DEFECTIVE (L1 DOOR) · airframe 20,348 hrs · 12,598 cycles

INSPECTION TYPE:N/A L1 ENTRY DOOR WILL NOT CLOSE WITH EXTERIOR HANDLE OPERATES FINE FROM INSIDE. DEFERED PER MEL 52-11-01-5 DMP C/W USED CONTROL NO M676813 DMP 52-11-01-5 C/W. **SUPPLEMENTAL SDR** R/R L1 EXTERIOR DOOR HANDLE ASSY. OPS CK GOOD IAW MM 52-11-21-0401. THIS CLEARS M676813.

Part: HANDLE — LACK OF LUBE (CREW ENTRY) · airframe 19,475 hrs · 12,109 cycles

CREW ENTRY DOOR CAN NOT BE LOCKED FROM OUTSIDE. LUBRICATED THE OUTSIDE DOOR HANDLE MECHANISM, OPS CHECKED GOOD IAW MM 52-00-00-060.

Part: HANDLE — BINDING (L1 DOOR) · airframe 18,316 hrs · 11,441 cycles

MAIN ENTRY DOOR IS VERY HARD TO CLOSE USING THE OUTSIDE HANDLE. THE INSIDE HANDLE OPERATES NORMALLY. LUBRICATED OUTSIDE DOOR HANDLE MECHANISM DOOR OPERATING NORMALLY AT THIS TIME IAW AMM 52-00-00 0601

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 18,016 hrs · 11,302 cycles

FUSELAGE SKIN DENT AFT OF FR 85 BETWEEN S44L AND 45. REPAIRED DENTS IAW SRM 53-10-12 FIG 210 SHT 1 AND 2.

Part: LIGHT — INOPERATIVE (DOOR) · airframe 17,835 hrs · 11,191 cycles

DOOR ARM DISARM LIGHT INOPERATIVE, BUZZER & HORN GOOD. RESET LIGHT ASSY FROM AUTONOMOUS BATTERY SOURCE. PERFORMED ADJUSTMENT AND TEST IAW AMM 52-73-00, BLOCK 503. OPERATED NORMALLY.

Part: SKIN — DAMAGED (TE FLAP) · airframe 17,767 hrs · 11,144 cycles

TWO DENTS, RT INBD FLAP UPPER SURFACE 49 INCHES FROM INBD EDGE, AND 12 INCHES FROM FWD EDGE OF UPPER SKIN. SECOND DENT IS 57 INCHES FROM INBD EDGE AND 14 INCHES FROM FWD EDGE OF UPPER SKIN. REPAIRED IAW EO A300-5750-65321-B.

Part: SMOKE DETECTOR — FALSE INDICATION (E/E BAY) · airframe 16,537 hrs · 10,367 cycles

AFTER TAKEOFF, RECEIVED AN AVIONICS SMOKE MASTER CAUTION. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. R & R 13WA SMOKE DETECTOR IAW AMM 26-15-12. ACCOMPLISHED ADJUSTMENT AND TEST IAW 26-15-00. CHECKED GOOD.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, RT WING FUEL ACCESS ANGLE 642EB IS LEAKING. R & R PANEL IAW MM 28-11-22.

Part: ATTACH ANGLE — DAMAGED (NR 1 NACELLE) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, ATTACH ANGLES HOLE ELONGATED. REMOVED DAMAGED ANGLE AND REPLACE WITH NEW.

Part: SHEAR TIE — DAMAGED (NR 1 NACELLE) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE :5YR, ATTACH ANGLE CRACKED. R & R ATTACH ANGLE.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, WIRE BUNDLE STANDOFF BRACKET BROKEN AND CRACKED. R & R BRACKET.

Part: BRACKET — CRACKED (AFT CARGO BLKHD) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, AFT CARGO BULKHEAD ANGLE BRACKET CRACKED. REMOVED DAMAGE ANGLE BRACKET AND REPLACED WITH NEW.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, LOWER ANGLE CRACKED, R & R DAMAGED ANGLE.

Part: BRACKET — CRACKED (AFT CARGO BLKHD) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, ANGLE CRACKED, REMOVED DAMAGED ANGLE AND REPLACED WITH NEW.

Part: FLOOR PANEL — PUNCTURED (FRAME 31) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FRAME 31, LBL 103 HAS A PUNCTURE IN FLOOR PANEL. REPAIRED FLOOR PANEL IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FRAME NR 31, LBL 115 HAS A PUNCTURE IN FLOOR PANEL. REPAIRED FLOOR PANEL IAW SREO A300-5320-42721-F.

Part: ATTACH BRACKET — CRACKED (NR 2 PYLON) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, ATTACH BRACKET CRACKED, REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH NEW PER SRM 51-40-21.

Part: ANGLE — CRACKED (FRAME 80-82) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CABIN ANGLE AT FRAME 80/82, RT -Y1137.1 IS CRACKED R & R ANGLE IAW SRM 51-40-21.

Part: ANGLE — CRACKED (FRAMES 80-82) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CABIN ANGLE AT FRAMES 80 - 82, LT Y1137.1 IS CRACKED. REPLACED ANGLE IAW SRM 51-40-21.

Part: ADAPTER — CRACKED (FRAME 19) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:1C2C, MAIN CABIN FRAME 19 RT SEAT TRACK ADAPTER CRACKED. R & R IAW SRM 51-40-21.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, ANGLE CRACKED, REMOVED UNSERVICEABLE ANGLE AND REPLACED WITH NEW IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, FWD CARGO FLOOR PANEL 131RG HAS MISSING HONEYCOMB AROUND A FASTENER BOTTOM SIDE. REPAIRED IAW EO A300-5320-42721-F.

Part: WEB — DENTED (BULK CARGO) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:1-3C, LEFT VERTICAL WEB DENTED, REPLACED WEB.

Part: SHEAR TIE — CRACKED (FRAME 79) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CABIN SHEAR PLATE LOCATED AT FRAME 79, STGR-26L IS CRACKED. REPLACE SHEAR PLATE WITH ANGLE BRACKET, PN A53979871200 IAW EO A300-5310-58168-A.

Part: SKIN — DELAMINATED (SPOILER) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, UPPER SKIN OF SPOILER HAS 2 INDICATIONS OF DELAMINATION. REPAIRED 2 AREAS OF DELAMINATION IAW SRM 57-72-11, 12.C.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CARGO FLOORBAORD 231LG HAS EDGE DAMAGED. REPAIRED FLOORBOARD IAW A300-5320-42721-F.

Part: PANEL — CORRODED (FRAME 47) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:1-C3, CENTER WING UPPER PANEL CORRODED BETWEEN BEAM 4 LT TO 6 LT AT FRAME 47. REMOVED CORROSION AND REPLACED FASTENERS WITH NEW OVERSIZED IAW EO A300-5710-58628-A.

Part: PANEL — CORRODED (FRAME 47) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:1-C3, CENTER WING UPPER PANEL CORRODED BETWEEN BEAM 5 RT & BEAM 6 RT AT FRAME 47. REMOVED CORROSION AND REPLACED FASTENERS WITH NEW OVERSIZED IAW EO A300-5710-58629-A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:1C,2C, MAIN CARGO FLOORBOARD 231QJ HAS EDGE DAMAGE. REPAIRED THE FLOORBOARD IAW EO A300-5320-42721-F.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CABIN FLOOR PANEL 231NF HAS CRACKED CORNER. REPAIRED IAW EO A300-5320-42721-F.

Part: ADAPTER — CRACKED (FRAME 32) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, MAIN CABIN SEAT TRACK ADAPTER CRACKED AT FRAME 32 BETWEEN Y1959 AND Y2462. R & R IAW DWG B53774136 & SRM 51-40-21.

Part: ADAPTER — CRACKED (FRAME 38) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, MAIN CABIN SEAT TRACK ADAPTER CRACKED AT FRAME 38.1 BETWEEN Y1959 AND Y2462. R & R IAW DWG A53774136 AND SRM 51-40-21.

Part: ADAPTER — CRACKED (FRAME 38) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, MAIN CABIN SEAT TRACK ADAPTER CRACKED AT FR 38.1 BETWEEN Y1959 AND Y2462. R & R IAW DWG A53774136 AND SRM 51-40-21.

Part: ADAPTER — CRACKED (FRAME 37) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE:5YR, MAIN CABIN SEAT TRACK ADAPTER FR37 LT IS CRACKED. REPLACED SEAT TRACK ADAPTER IAW SRM 51-40-21.

Part: PANEL — CHAFED (LT WING) · airframe 15,396 hrs · 9,626 cycles

INSPECTION TYPE: 5YR, LEFT WING PANEL NR 512-LB CHAFED ON TOP SIDE. REPLACED THE PANEL.

Part: PANEL — CRACKED (LT PYLON) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE:5YR, PANEL 413CL CRACKED, RIB REPAIRED / FABRICATED REPAIR DOUBLER IAW SRM 54-52-51.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE:5YR, MAIN CABIN FLOORBEAM FRAME 79, Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-58454-A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE:5YR, PUNCTURES IN FLOORBOARD REPAIRED IAW SRM 51-77-10.

Part: ROLLER TRACK — CORRODED (FWD CARGO) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE: 5YR, FORWARD CARGO BAY FLOOR, SCREW CORRODED IN ROLLER TRAY FR27, LBL 55. OUT OF SRM LIMITS. R & R SCREW AND NUT IAW SRM 51-40-21.

Part: PANEL — CRACKED (LT PYLON) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE: 5YR, PANEL 424CR CRACKED, RIB REPAIRED. FABRICATED DOUBLER IAW SRM 54-52-51.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE:5YR, PUNCTURE IN FLOORBOARD. REPAIRED IAW EO: A300-5320-42722-E.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,395 hrs · 9,624 cycles

INSPECTION TYPE:5YR, MAIN CABIN FLOORBEAM RT FRAME 79 -Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-58454-A.

Part: O-RING — WORN (HYD SYSTEM)

EMERGENCY DECLARED - ECAM WARNING, BLUE SYSTEM LOW LEVEL, HYD QTY GAUAGES CONFIRMED LOW QUANTITY IN BLUE SYS. COMPLETED STEPS IN ECAM AND QRH PROCEDURES. VISUALLY INSPECTED AND FOUND BLUE HYD SYS SERVO CONTROL MANIFOLD NO NON RETURN VALVE LEAKING FROM THE EXTRACTOR PLUG. R & R NON-RETURN VALVE EXTRACTOR PLUG O-RING, IAW AMM 29-12-34-0401. SERVICED RESERVOIR, BLEEDING EFFICIENCY CHECK OK AND LEAK CHECK OK.

Part: LAMP — INOPERATIVE (LAVATORY)

DURING MX INSPECTION, LAVATORY AUX/MIRROR LIGHT FOUND TO BE INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21-401. OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,101 hrs · 8,114 cycles

INSPECTION TYPE:1C, LT FUSELAGE SKIN IS CREASED BETWEEN S3-4L, 6.5 INCHES FWD FR 54.1 ACCOMPLISHED REPAIR IAW EO A300-5330-50571-A, PARA 6A.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,101 hrs · 8,114 cycles

INSPECTION TYPE:1C, LT FUSELAGE SKIN HAS A DENT AT FR 30 S28L. ACCOMPLISHED REPAIR IAW SRM 53-10-12, FIG 210.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 12,404 hrs · 7,636 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 222DG HAS LOWER SKIN TORN AND DELAMINATED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,404 hrs · 7,636 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD NR 231TG UPPER AND LOWER SKIN IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 231TG IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,404 hrs · 7,636 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD NR 231RG HAS UPPER SKIN PUNCTURED AND LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42722-B, PARA 6A AND EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,404 hrs · 7,636 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231MJ HAS UPPER SKIN PUNCTURED AND LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN DAMAGED AT FR67 S1R - S2R. REPAIRED IAW EO A300-5330-42289-B.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR)

L1 DOOR ESCAPE SLIDE FELL THEN DEPLOYED. REPLACED EMERGENCY EVACUATION SLIDE. REF MM 25-61-21-04.

Part: SKIN — DAMAGED (FUSELAGE)

LIGHTNING STRIKE FRM 67 BETWEEN STR 1 AND 2 RT. ACCOMPLISHED INTERIM REPAIR IAW EO A300-5330-42289-A.

Part: ACTUATOR — FAULTED (RT WING SLATS)

EMERGENCY DECLARED - ON SLAT EXTENSION RECEIVED SLATS SYS 1 & 2 FAULT, RAN CHECK LIST. APPLIED ALL ADDITIVES. FOLLOWED QRH THROUGH TOUCHDOWN. T/S DISCREPANCY IAW TSM 27-80-02. ISOLATED TO RT WING SLAT NR 5 ACTUATOR. SERVICED NR 5 JACKSCREW IAW AMM CH 12-13-27 AND 12-22-27. SYS OPERATES NORMAL IAW AMM 27-80-00.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, REPAIR SURVEY SEQUENCE NR137-W3-05 DOES NOT CORRELATE TO SRM AT LT INBD FLAP LWR SKIN, RIB 22A TO 20D STR 2.6 TO STR 2.7. ACCOMPLISHED REPAIR ON LT INBD FLAP LWR SKIN IAW EO A300-5750-40510-A AND STA EA 300-5750-01-A2792 IR.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL NR 251LJ IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR PANEL NR 251LJ IAW EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — PEELING (MAIN CARGO BAY) · airframe 10,515 hrs · 12,387 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOOR PANEL 252DF IS PEELING AT LOWER SURFACE. REPAIRED MAIN CARGO FLOOR PANEL 252DF IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 10,515 hrs · 12,387 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOOR PANEL 252LM IS CRACKED AT LOWER SURFACE. REPAIRED MAIN CARGO FLOOR PANEL 252LM IAW EO A300-5320-38221-B, PARA 6 A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 10,515 hrs · 12,387 cycles

INSP TYPE:10YR, MAIN CARGO FLOOR PANEL 252DN IS PUNCTURED AT LOWER SURFACE. REPAIRED MAIN CARGO FLOOR PANEL 252DN IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 10,515 hrs · 12,387 cycles

INSP TYPE:10YR, MAIN CARGO FLOOR PANEL 251UJ IS PEELED AND PUNCTURED AT UPPER AND LOWER SURFACE. REPAIRED MAIN CARGO FLOOR PANEL 251UJ PER EO A300-5320-38221-B, PARA 6 A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 251CN IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251CN IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD 252YH IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 252YH IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:5YR, MAIN CABIN FLOOR PANEL NR 252YJ IS CRACKED AN PEELING AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252YJ IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251YJ HAS A TEMPORARY REPAIR AT UPPER SURFACE AND 4 EA CRACKS. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251YJ IAW EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOOR PANEL NR 251VJ IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CARGO FLOOR PANEL NR 251VJ IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 10,515 hrs · 12,387 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOOR PANEL 261AM IS CRACKED AT BOTTOM SURFACE. REPAIRED MAIN CARGO FLOOR PANEL 261AM IAW EO A300-5320-38221-B, PARA 6A.

Part: FRAME — DAMAGED (CARGO DECK) · airframe 10,515 hrs · 6,480 cycles

INSP TYPE:10YR, ABOVE MAIN CARGO DECK FLOOR FRAME 32 RT SIDE HAS 6 SCREWS PROTRUDING THROUGH FRAME AND 3 SCREWS PROTRUDING INTO FRAME. ACCOMPLISHED REPAIR AT MAIN DECK FLOOR FRAME 32 STR 13R TO STR 31R IAW SRM 53-10-13, FIG 203.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, LT WING CTR FLAP UPPER SKIN HAS REPAIR DOUBLER GOUGED. REPAIRED LT WING CTR FLAP UPPER SKIN IAW STA-SA, EA 300-5750-A2759, REV I/R AND UPS EO A300-5750-40453-A.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, LT CTR FLAP L/E BETWEEN FLAP TRACKS 3 AND 4 RIB 12 AND 16 HAS A EXTERNAL REPAIR DOUBLER THAT DOES NOT CORRELATE TO THE SRM REPAIR SURVEY ACCOMPLISHED REPAIR ON LT CTR FLAP L/E RIB 12 AND RIB 16 IAW SRM 57-50-00 PARA 4H FIG 208.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK FR 80, Y1137.1 IN MAIN CABIN ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK FR8 Y1137.1 IAW SRM 53-10-16, P.B 201 PARA 4, FIG 201

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK FRAME 80,CTR LINE Y0 IN MAIN CABIN. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK FRAME 80,CTR LINE Y0 IAW SRM 53-10-16 PB 201, PARA 4, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK FR 80 Y1137 IN MAIN CABIN ACOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 80 Y1137 IAW SRM 53-10-16 P B201 PARA 4A, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK, FR80 Y 450 IN MAIN CABIN. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR80 Y450 IAW SRM 53-10-16, P.B201 PARA 4, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK FR80 Y794 IN MAIN CABIN ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 80 Y794 IAW SRM 53-10-16 P.B 201 PARA.4A, FIG 201.

Part: WING — DENTED (RIGHT) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, RT ASA HAS A DENT IN OTBD LOWER CORNER. ACCOMPLISHED REPAIR ON RT ASA OTBD LOWER CORNER IAW EO A300-5750-40464-A.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131SG IS CRACKED. REPAIRED FWD CARGO FLOOR PANEL 131SG IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, NUMEROUS DENTS ON BULK CARGO FLOORBOARD NR 161LF. FABRICATED BULK CARGO FLOORBOARD NR 161LF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DAMAGED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, EDGE DAMAGE ON AFT CARGO FLOORBOARD NR 152SF. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 152SF IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — GOUGED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 152UF IS GOUGED AND DELAMINATED. FABRICATED NEW NEW AFT CARGO FLOOR PANEL 152UF IAW EO A300-5320-16407-E, APPENDIX A/C.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CRACKED BOTTOM ON AFT CARGO FLOOR PANEL 152QF. REPAIRED AFT CARGO FLOOR PANEL 152QF IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, EXISTING REPAIR LOOSE, DENTS ON BULK CARGO FLOORBOARD NR 162HF. FABRICATED BULK CARGO FLOORBOARD NR 162HF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 152TF IS CRACKED. REPAIRED AFT CARGO FLOOR PANEL 152TF IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, NUMEROUS DENTS, HOLES ON BULK CARGO FLOORBOARD NR 161HF. FABRICATED BULK CARGO FLOORBOARD NR 161HF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CRACKED BOTTOM AND DELAMINATED AFT CARGO FLOOR PANEL 151QF. REPAIRED AFT CARGO FLOOR PANEL 151QF IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, NUMEROUS DENTS ON BULK CARGO FLOORBOARD NR 161MF. FABRICATED BULK CARGO FLOORBOARD NR161MF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CRACKED BOTTOM ON AFT CARGO FLOORBOARD NR 151SF. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 151SF IAW EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, CRACKED BOTTOM OF AFT CARGO FLOOR PANEL 151NG. REPAIRED AFT CARGO FLOOR PANEL 151NG IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, FWD CARGO COMPT FLOOR PANEL 131MG IS CRACKED. FWD CARGO COMPT FLOOR PANEL 131MG IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, NUMEROUS DENTS, HOLES AND PUNCTURES ON BULK CARGO FLOORBOARD NR161GF. FABRICATED BULK CARGO FLOORBOARD NR161GF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 10,515 hrs · 6,480 cycles

INSPECTION TYPE:10YR, NUMEROUS PUNCTURES AND DENTS ON BULK CARGO FLOORBOARD NR 161JF. FABRICATED BULK CARGO FLOORBOARD NR 161JF IAW EO A300-5320-16407-E, APPENDIX D.

Part: SKIN — DAMAGED (RT WING TE FLAP)

RT WING INBD FLAP LOWER SURFACE DAMAGED. REPAIRED IAW EO A300-5750-36683-B.

Part: POWER SUPPLY — INOPERATIVE (ESCAPE SLIDE)

EVAC SLIDE LIGHT INOP. BITE TESTED THE AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN). UNIT FAILED, REMOVED AND REPLACED UNIT, REF MM 52-73-18-04. OPS OK. EVAC SLIDE WARNING LIGHT OPS OK. THIS CLEARS M410281.

Part: SLIDE — LOW PRESSURE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE PRESSURE LOW. REMOVED EMERGENCY ESCAPE SLIDE PER MM 25-61-21-04, OK TO INSTALL SLIDE ASSY. INSTALLED ESCAPE SLIDE IAW MM 25-61-21-04. OPS CHECK OK.

Part: FRAME — GOUGED (FUSELAGE)

GOUGE AT RT FUSELAGE FRAME 57.2 BELOW STR 36R. REPAIRED IAW EOA300-5330-33509-A.

Part: LIGHT — INOPERATIVE (LAVATORY)

INSPECTION TYPE:N/A LAV AUX LIGHT OUT. RELAMPED AND OPS CHECKED GOOD.

Part: BUTTON — LACK OF LUBE (EVAC SLIDE)

INSPECTION TYPE:N/A EMERGENCY SLIDE TEST BUTTON SOMETIMES STICKS IN TEST. LUBRICATED SWITCH. OPS OK SEVERAL TIMES PER M/M 52-73-00-00.

Part: SHUTOFF VALVE — MALFUNCTIONED (THRUST REVERSER)

INSPECTION TYPE:N/A ATB - NR 1 ENG REVERSER UNLOCK LIGHT ILLUMINATED. REMOVED & REPLACED THRUST REVERSER PRSOV FOR TSM 78-31-40 BLOCK 22 PER AMM 78-31-05-04. PERFORMED OPS CHECK PER AMM 78-32-11-05. NR 1 ENG REVERSER SYSTEM HAS NO DEFECTS NOTED.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE)

CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT AFTER DEPARTURE. NR1 & NR2 AUTOMATIC CABIN PRESSURE CONTROLLERS INOPERATIVE. CREW SWITCHED TO MANUAL. MANUAL SYSTEM UNABLE TO CONTROL CABIN PRESSURE. NR1 AUTO PRESS SYS DEFERRED IAW MEL. REPLACED FWD OUTFLOW VALVE PER MM 21-31-12-04. PLACARD REMOVED. D382069 CLEARED.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,705 hrs · 4,846 cycles

INSPECTION TYPE:3C MCD FLOOR PANEL NR 251WJ HAS A LARGE FIELD REPAIR WITH A LARGE DENT. REMOVED FIELD REPAIR AND REPAIRED FLOOR PANEL NR 251WJ IAW A300-600 SRM 53-10-20 FIG 203.

Part: SKIN — CHAFED (T/E FLAP) · airframe 7,705 hrs · 4,846 cycles

INSPECTION TYPE:3C LEFT WING CENTER FLAP UPPER SKIN MID SECTION HAS 6 CHAFE MARKS. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00 FIG 206, 51-40-21 AND EO M-5100-19814-D.

Part: SKIN — GOUGED (T/E FLAP) · airframe 7,705 hrs · 4,846 cycles

INSPECTION TYPE:3C LEFT I/B FLAP UPPER SKIN MID SECTION 6 INCH LONG GOUGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00.

Part: SKIN — CHAFED (T/E FLAP) · airframe 7,705 hrs · 4,846 cycles

INSPECTION TYPE:3C LEFT I/B FLAP UPPER L/E SKIN CHAFED 8 INCH HORIZONTALLY. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00.

Part: ESCAPE ROPE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A CAPT ESCAPE ROPE IS FALLING OUT OF STORAGE SPOT. RESECURED AS REQUIRED.

Part: WARNING LIGHT — INOPERATIVE (EVACUATION SLIDE)

INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT SYSTEM INOP. REMOVED AND REPLACED ESCAPE SLIDE INDICATION LIGHT, NO HELP. RESET CONNECTOR ON ASPSU. OPS CHECKED GOOD IAW 52-23-11-4. DEFERRAL CLEARED, PLACARD REMOVED.

Part: CONNECTOR — LOOSE (DOOR SLIDE)

CREW ENTRY DOOR SLIDE ARMED LIGHT INOP. AURAL WARNING OK. RESET CONNECTOR AND PSU. OPS GOOD PER AMM 52-73-11-4.

Part: SLIDE — INOPERATIVE (COCKPIT)

EVAC SLIDE SYSTEM WARNING LIGHT INOP. DEFERRED M319607 ISSUED. CLEANED TEST SW 39WN. CKS GOOD PER AMM 52-73-14-4.

Part: INTERCOSTAL — BUCKLED (BS 5647) · airframe 5,103 hrs · 3,105 cycles

INSPECTION TYPE:5 YR TAIL SECTION FS 95 STA 5647 RT AFT OF DOOR 312AR INTERCOSTAL BUCKLED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-00.

Part: INTERCOSTAL — BUCKLED (FR 84-86) · airframe 5,103 hrs · 3,105 cycles

TAIL SECTION BOTTOM INTERCOSTAL BUCKLED BTWN FS 84 AND FS 86. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-00.

Part: INTERCOSTAL — CRACKED (FR 79 LT) · airframe 5,103 hrs · 3,105 cycles

MAIN CABIN INTERCOSTAL AT FS 79 LT FLOOR LEVEL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-21.

Part: INTERCOSTAL — CRACKED (FR 79 RT) · airframe 5,103 hrs · 3,105 cycles

MAIN CABIN INTERCOSTAL A FRAME 79 RT FLOOR LEVEL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-21.

Part: FRAME — DAMAGED (FR 52 LT) · airframe 5,103 hrs · 3,105 cycles

INSPECTION TYPE:2C MAIN CARGO COMPARTMENT FLOOR FRAME 52 BTWN FLOOR PNL 242EK AND 242ZJ FRAME DAMAGED PN 99589. REMOVED AND REPLACED FRAME IAW SRM 51-40-00.

Part: DOUBLER — CRACKED (RT K FLAP BOX) · airframe 5,103 hrs · 3,105 cycles

INSPECTION TYPE:C2 RT WING KRUEGER FLAP BOX AREA CURVED DOUBLER HAS CRACK APPROX 1". REMOVED AND REPLACED DOUBLER IAW SRM 51-40-00.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 5,103 hrs · 3,105 cycles

5YR N2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED RT AND LT MEMBER SECTIONS IAW SRM 51-40-00.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 5,103 hrs · 3,105 cycles

INSPECTION TYPE:5YR NR 2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-00.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 5,103 hrs · 3,105 cycles

NR 1 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED 2 PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 5,103 hrs · 3,105 cycles

NR 1 ENG AFT LWR PYLON LWR SECTION IS CRACKED FWD, AFT THROUGH PRESS LINE MOUNT HOLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-21.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 5,103 hrs · 3,105 cycles

NR 1 AFT LWR PYLON MEMBER SECTION IS CRACKED 2 EA PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061.

Part: SWITCH — STUCK (ESCAPE SLIDE)

AT DEPARTURE ENTRY DOOR SLIDE WARNING HORN & LT SOUNDED. RECONNECTED CONNECTOR ON ASPSU. RESET SLIDE TEST SWITCH ON DOOR HANDLE SLIDE. OPS CHECK NORMAL IAW AMM CH 25.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:AS TOILET EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT.

Part: SLIDE — MALFUNCTIONED (PAX DOOR)

INSPECTION TYPE:N/A MAIN CABIN DOOR SLIDE INOPERABLE REF UPS03641656 VOIDED BECAUSE TAIL NUMBER SHLD HAD BEEN N137UP INSTEAD OF N320UP. INSTALLED DUAL ESCAPE SLIDE TO DOOR PER Z831 PER MM 25-61-21-4, CLEARS M272188.

Part: BOTTLE — DISCHARGED (MAIN ENTRY DOOR)

INSPECTION TYPE:N/A MAIN ENTRY DOOR DAMPNER/EMERGENCY OPERATION CYLINDER NITROGEN BOTTLE READS 0 PSI. REPLACED DIAPHRAM 10 SHEAR PIN 15 AND O-RINGS 7-8-9 AND RESERVICED MAIN ENTRY DOOR DAMPNER AND EMERGENCY OPERATING CYL PER 52-10-14-3.

Part: LIGHT — WILL NOT TEST (PAX DOOR)

INSPECTION TYPE:N/A EVAC SLIDE LIGHTS IN MAIN CABIN DOOR WILL NOT TEST. PERFORMED ADJUSTMENT TEST IAW MM 52-23-00 PG 501, NO FAULTS NOTED.