N165UP

Part: SELECTOR VALVE — INOPERATIVE (ZONE 700) · airframe 25,504 hrs · 15,181 cycles

DURING CRUISE, NOTICED SLOW DEPLETION OF GREEN SYSTEM HYDRAULIC RESERVOIR. SHORTLY THEREAFTER, RECIEVED €ŒGREEN RSVR LO LEVEL€? ECAM MESSAGE. RAN ECAM ITEMS AND QRH / AOM ASSOCIATED CHECKLISTS. ENGAGED. FOUND LANDING GEAR SELECTOR VALVE 3GA LEAKING BEYOND LIMITS, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE 3GA IAW AMM 32-31-12/401 ON BARCODE T3F18E007661D. OPS AND LEAK CHECK GOOD.

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 24,952 hrs · 14,913 cycles

EMERGENCY EXIT LIGHTS WILL NOT DISARM OPERATED AND TESTED SUPERNUMERARY AREA EMERGENCY LIGHTS REF AMM 33-51-00/501 LIGHTS GO ON/OFF AS COMMANDED

Part: TRIM PANEL — UNSECURE (ZONE 800) · airframe 24,560 hrs · 14,714 cycles

TOP TRIM PANEL ON CREW ACCESS DOOR IS NOT SECURE AND NEEDS TIGHTENING TIGHTED AND INSTALLED TOP TRIM PANEL MOUNTING HARDWARE IAW AMM 25-23-41. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — FAULTED (EMERGENCY LIGHTS) · airframe 24,435 hrs · 14,642 cycles

EMERGENCY EXIT LIGHT SWITCH WOULD NOT DISARM LIGHTS AFTER LANDING RECYCLED EMER LIGHT CHARGER C/B, CKS OK IAW MM 33-51-00-715-001 NO HISTORY LAST 10 DAYS, SYS OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 24,398 hrs · 14,615 cycles

MAIN CABIN DOOR ASSIST BOTTLE PRESSURE READS 900. SERVICED ASSIST BOTTLE IAW AMM 52-10-14.

Part: RIB — CRACKED (ZONE 400) · airframe 24,190 hrs · 14,512 cycles

PANEL 423AL HAS A CRACK (BETWEEN 3" TO 4" LONG) DOT 129-001 (GE-129) INSTALLED RIB AT PYLON #2 WITH EXISTING FASTENERS IAW A300-600 SRM 51-40-21.

Part: STRINGER — CRACKED (ZONE 600) · airframe 24,190 hrs · 14,512 cycles

STR R/H I/B AILERON P/N A57661001179 HAS A GOUGE WITH A CRACK IN IT ON FITTING. COMPLIED WITH EO-91570-REQ1 AND VTMAE FINAL EA 300-5761-27-A3701 REV -. REVIEWED

Part: ARM — DETERIORATED (ZONE 800) · airframe 24,190 hrs · 14,512 cycles

CREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPLIED CIC IAW EO-2780-REQ001. PN 04-002-0153 BATCH 0004291043. REVIEWED

Part: DOOR — DETERIORATED (ZONE 800) · airframe 24,190 hrs · 14,512 cycles

*SDR FILED OPEN* FAULT: APG-Z800 CREW ENTRY DOOR, DOOR ARM W/CIC DETERIORATED; NO DOT. JR-117. APPROVED

Part: SUPPORT — CRACKED (ZONE 100) · airframe 24,190 hrs · 14,512 cycles

R/H MCD FOOR DAWG BONE SUPPORT BETWEEN FR 38.1-38.2 AT -Y2462 IS CRACKED. 33-026. INSTALLED DAWG BONE AT MDC BETWEEN FR38.1 AND FR38.2 -Y2462 USING FASTENERS P/N HL10VF6-8, BATCH 0004288775 AND P/N HL70-6, BATCH 0004305623, IAW A300-600 SRM 51-40-21.

Part: WEB — BROKEN (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

BTW FR 79 AND 80, L/H NEXT TO SEAT TRACK Y2462, WEB BROKEN. DOT 73-038 (MOYA-73). INSTALLED NEW WEB AT FR79 TO FR 80 IAW A300 SRM 51-40-21 PN#5398111320051 BATCH#0003652288.

Part: WEB — DAMAGED (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

MCC, BTW FR 76 AND 77, R/H NEXT TO SEAT TRACK Y-2462, WEB BROKEN. DOT 73-040 (MOYA-73). INSTALLED NEW WEB WITH EXISTING FASTENERS AND RIVETS P/N MS20426AD5-8, BATCH 0004289284 AND MS20426AD6-15, BATCH 0004225945 IAW A300-600 SRM 51-40-21.

Part: TRACK — BROKEN (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

R/H MCD FLOORPANEL 242KF C-TRACK AT FR 34 IS BROKEN. 33-022. INSTALLED ADAPTER IAW A300-600 SRM 51-40-21.

Part: WEB — BROKEN (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

BTW FR 79 AND 80, R/H NEXT TO SEAT TRACK Y-2462, WEB BROKEN. DOT 73-039 (MOYA-73). INSTALLED NEW WEB AT FR79 TO FR80 IAW 300 SRM 51-40-21 PN 4263193 BN#02-013-8 PN#4319064 BN#PG-W2K4Q PAINT CUP 02-012-176.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

BTW FR 38.1, AND 38.2, L/H AFTER SEAT TRACK 2462, BONE SUPPORT BROKEN. DOT 73-036 (MOYA-73). INSTALLED NEW BONE SUPPORT AT FR38.1 TO FR38.2 IAW A300 SRM 51-40-21 PN 5378103821400 BN 0004062096.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

MAIN DECK. SEAT TRACK AT FR37 BTW Y2462/Y1959 BROKEN. INSTALLED ADAPTER AT MAIN DECK SEAT TRACK AT FR 37 IAW 51-41-21 PN B5377413620490 BN 0004312613.

Part: RIB — CRACKED (ZONE 400) · airframe 24,190 hrs · 14,512 cycles

PYLON #1 UPPER AREA PRESSURE RELIEF DOOR AFT BOLT SIDE HAS 2 POINTS WITH CRACKS 34-023. INSTALLED RIB AT PYLON #1 IAW A300-600 SRM 51-40-21 USING EXSISTING FASTENERS.

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 24,190 hrs · 14,512 cycles

RIGHT WING CENTER FLAP, LEADING EDGE. DENTED FOWARD OF CENTER UPPER SKIN SLING ATTACH POINT. INSTALLED 02 EA BUTTSTRAPS AND DOUBLER TO RH CENTER FLAP LEADING EDGE SKIN. WITH RIVETS P/N: MS20426DD4-5. BATCH: 4196486. P/N: NAS1739E4-3. BATCH: 4302252 AND SEALANT 870 B1/2 P/N: 04-001-0109. BATCH: 4304380. IAW A300-600 SRM 57-50-00, PAGE 233.

Part: FLOORBEAM — BENT (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

MAIN DECK-FR 48 CROSSBEAM BENT -Y450 TO -Y953-DOT 109-097-VWV. REMOVED AND REPLACED ON MAIN CABIN DECK FR 48 CROSSBEAM IAW A 300-600 SRM 51-40-21.NO FURTHER ACTION REQUIRED.

Part: INLET — CRACKED (NR 2 ENGINE) · airframe 24,190 hrs · 14,512 cycles

ENG# 1 INLET COWL T/E AREA AT POSITION 9 O'CLOCK HAS SURFACE CRACKED. DOT 34-003. INSTALLED NEW WEB REPAIR AND SPLICE IAW PRATT & WHITNEY SRM 54-10-00. PN: CR3213-6-06, BN: 0004304591, PN: CR3213-6-04, BN: 0004282032. INSTALLED LINE AND COVER IAW A300 AMM 73-24-06/401. T86780, T89028.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,190 hrs · 14,512 cycles

PANEL 147CZ HAS (1EA) CRACK TO EDGE AT ATTACH HOLE-DOT 109-076-VWV. REPLACED 147CZ WITH NEW PANEL P/N A2551030700600 BATCH 0004327949 IAW A300-600 AMM 25-72-41/401. NO FURTHER ACTION REQUIRED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 24,190 hrs · 14,512 cycles

AFT CARGO FWD BULKHEAT FR 54 L/H MID FOUND TWO CRACKED FLOOR SUPPORT BARCKETS. DOT 60-008 AND 60-009. INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN :0004085927.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 24,190 hrs · 14,512 cycles

AFT CARGO-FR54 CTR B/H PANEL SUPPORT (A5341076521700) AT Y0 CRACKED-DOT 109-009-VWV. INSTALLED NEW SUPPORT BRACKET AT AFT CARGO COMPARTMENT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN 0004085927.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 24,190 hrs · 14,512 cycles

AFT CARGO-FR54 L/H B/H PANEL SUPPORT (A5341076522200) AT Y1959 CRACKED-DOT 109-010-VWV. INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21 PN EN6001D6-10 BN 00040855927.

Part: BRACKET — DETERIORATED (ZONE 100) · airframe 24,190 hrs · 14,512 cycles

FUSELAGE LOWER, AFTER ADAPTER SAFETY STAY HAS BRACKET DETERIORATED DOT 108-08. INSTALLED 02 EA ANGLES WITH 04 EA RIVETS P/N: HL12VF6-4. BATCH: 4115479 WITH 04 EA COLLARS P/N:HL70-6, BATCH: 4305623. AND SEALANT P/N: PR1422 B2. BATCH: 4305492. IAW A300-600 SRM 51-40-21.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 24,182 hrs · 14,507 cycles

EMERGENCY EXIT LIGHTS IN DISARM POSITION NOT WORKING. EMERGENCY LIGHTS IN SUPERNUMERARY AREA ON. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHT SWITCH IAW AMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 23,746 hrs · 14,234 cycles

OPEN, OPERATIONAL CHECK OF INTERIOR EMERGENCY LIGHTS FAILED THE AUTOMATIC ACTIVATION IN EVENT OF DC POWER FAILURE CHECK

Part: RELAY — FAULTED (EMERGENCY LIGHTS) · airframe 23,746 hrs · 14,234 cycles

OPERATIONAL CHECK OF INTERIOR EMERGENCY LIGHTS FAILED THE AUTOMATIC ACTIVATION IN EVENT OF DC POWER FAILURE CHECK T/S PER A300 AWM 33-51-03 SUSPECT 490VU MAINTENANCE PANEL 233LT RLY DIM. R&R RELAY IAW ESPM 20-46-50-01. PERFORMED OPS TEST OF EMERGENCY LIGHTING AUTO ACTIVATION IN EVENT OF DC POWER FAIL IAW AMM 33-51-00/501. OPS NORMAL

Part: CONTACT — BROKEN (SLIDE LIGHT) · airframe 23,406 hrs · 14,039 cycles

CREW ENTERANCE DOOR SLIDE LIGHT OUT OF MOUNTING BRACKET FOUND WIRE 5273-1099 BROKEN AT CONTACT 2 OF THE SLIDE LIGHT ASSEMBLY 7WN. REPINNED, REF ESPM 20-48-21 AND AWM 52-73-05. OP CHECKS GOOD, REF AMM 52-73-11. DEFERRAL CLEARED. PLACARD REMOVED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,328 hrs · 13,994 cycles

DOOR SLIDE ARMING LEVER RED LIGHT INOPERATIVE RESEATED CONNECTOR ON THE AUTONOMOUS PWR SUPPLY UNIT 70WN REF AMM 52-73-18 & OPS CHECKED OK IAW AMM 52-73-00. WARNING LIGHT 7WN TESTS OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,222 hrs · 13,935 cycles

DOOR ACTUATOR PRESSURE IS LOW SERVICED DOOR DAMPER WITH HIGH PRESSURE DRY NITROGEN PER AMM 52-10-14. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,162 hrs · 13,904 cycles

DURING PREFLIGHT FOUND WHAT APPEARS TO BE A CRACK RUNNING ACROSS THE CENTER OF F/O WINDSCREEN. REMOVED F/O WINDSHIELD UP TO STEPS 1.C.(6) PER AM 56-11-11. COMPLETED INSTALL OF F/O WINDSHIELD IAW AMM 56-11-11

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,073 hrs · 13,857 cycles

LOWER VERTICAL STAB LEADING EDGE PANEL HAS SUSPECTED EROSION DAMAGE ON BOTTOM TWO THIRDS OF PANEL AS VIEWED FROM GROUND LEVEL. REMOVED AND REPLACED LOWER VERTICAL STAB LEADING EDGE PANEL 322AL IAW A300 AMM 55-32-11-401

Part: DAMPER — INOPERATIVE (CABIN) · airframe 22,423 hrs · 13,465 cycles

INSPECTION TYPE:NACREW ENTRY DOOR DAMPER / EMERGENCY OPERATION CYLINDER PRESSURE LOW.CYLINDER SERVICED WITH NITROGEN REF: A300 AMM 52-10-14-0301. NO LEAKS/DEFECTS.

Part: CONTROL SWITCH — FAULTED (MLG) · airframe 22,128 hrs · 13,295 cycles

ATB, CONTINUOUS GEAR OVERSPEED WARNING DUE TO DOWN ARROW ON GEAR AIR TURNED BACK TO RFD, FLSE GEAR DWN INDICTION AT ALT VRIFID THRU ATS RPLCD L/G CTOL MICROSWTCH UNIT (2GA) A300MM 32-31-11-401 OPS CK NRML RPLCD FAULTY FWC2 IPC 32-31-12-10. MM 31-51-00 ECAM SYS ADJ/TEST DRING TST FND FWC2 W/ INTERM VFE 175, RPLCD FWC2 REF MM 31-53-34 OPS CK NORMAL PERF ADJ/TEST AGN VFE 175 P/N 35-OB5-3008-320 S/N OFF 222 ON 0B5002036 IPC 31-53-08-02B

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,487 hrs · 12,949 cycles

INSPECTION TYPE:N/AEMER EXIT LT ON OVHD NOT ILLUMINATED WHEN DISARMED LGIHT DOES NOT TESTEMER EXIT LT ON OVHD OPS CHECK GOOD IAW AMM 33 14 00

Part: POWER SUPPLY — UNSERVICEABLE (L-1 DOOR) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:SEGDOES NOT ILLUMINATE RESIDUAL PRESSURE WARNING LIGHTREMOVED AND REPLACED ASPSU IAW AMM 52-73-18-401

Part: ANGLE — BROKEN (RH KRUEGER FLAP2) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:CRH WING KRUEGER FLAP ZONE LH SIDE PANEL SUPPERT IS BROKENFAB REMOVED AND REPLACED ANGLE IAW SRM 57-41-11 AND SRM 51-40-21

Part: SHEAR PLATE — CRACKED (LH STR 44L FR 65) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:CLH SIDE STR 44 AT FR65 WEB IS CRACKED AT UPPER AFT CORNERFAB REMOVED AND REPLACED WE (SHEAR PLATE) IAW SRM 53-17-8 AND SRM 51-40-21

Part: STIFFENER — CRACKED (APU TAIL CONE) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:SEGCRACK IN APU TAIL COMPARTMENT AT FRAM 101 APP. 3 O'CLOCK POSITION LOOKING FORWARD.ACCOMPLISHED REPAIR PER FINAL EA 300-5319-27-A2874 AND FINAL UPS EO A300-5320-83201-A

Part: ANGLE — CRACKED (RH KRUEGER) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:A300RH WING KRUEGER FLAP ZONE SUPPORT BRACKET (ANGLE) IS CRACKEDFABRICATED,REMOVED AND REPLACED ANGLE IAW SRM 57-41-11 AND SRM 51-31-00 TABLE 4

Part: ANGLE — CRACKED (RH KRUEGER) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:A300RH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21

Part: ANGLE — CRACKED (LH KRUEGER) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:A300LH WING KREUGER FLAP MIDDLE ZONE WEB IS CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21

Part: FITTING — BROKEN (LH WING KRUEGER) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:SEGLH WING KRUEGER FLAP MIDDLE ZONE HAS METAL PLATE BROKENFABRICATED AND REPLACED PLATE PER SRM 57-41-12 FIG 3 SECTION B-B

Part: NONE — BROKEN (E/E COMP 121YF) · airframe 21,163 hrs · 12,744 cycles

INSPECTION TYPE:SEGE/E COMP FLOOR PANEL 121YF BROKENREPAIR IAW SREO A300-5320-42722F

Part: SKIN — DAMAGED (TE FLAP) · airframe 20,371 hrs · 12,314 cycles

DAMAGE TO THE UPPER SKIN OF THE FLAP REQUIRES REPAIR. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO A300-5750-81573-B

Part: SLIDE — INOPERATIVE (PAX DOOR) · airframe 20,268 hrs · 12,260 cycles

SLIDE ARMING LEVER WILL NOT MOVE CANNOT ARM EMERG ESCAPE SLIDE. DEF PER MEL 52-11-01-2-3. SLIDE ARMING LEVER WILL NOT MOVE CANNOT ARM EMERG ESCAPE SLIDE. DEF PER MEL 52-11-01-2-3DMP REVERSED REMOVED GIRT BAR FROM FLAP. REORIENTED GIRT BAR IAW AMM 25-61-21.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 18,923 hrs · 11,498 cycles

INSPECTION TYPE: NA EMERGENCY LIGHTS POWER SUPPLY FAULTING ON BITE TEST. REPLACED POWER SUPPLY, PER AMM 33-50-00-0001.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:A300 EXFOILATED CORROSION ORIGINAL MATERIAL .098 AFTER REWORK .038. REMOVED AND REPLACED BRACKET.

Part: WARNING LIGHT — INOPERATIVE (L1 DOOR) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEGRED ESCAPE SLIDE WARNING LIGHT INOPREMOVED AND REPLACED ESCAPE SLIDE WARNING LIGHT

Part: INTERCOSTAL — CRACKED (HORIZONTAL STAB) · airframe 17,303 hrs · 10,574 cycles

INSIDE HORIZONTAL STABILIZER COMPARTMENT BETWEEN C85-C86 HAD A CRACKED INTERCOASTAL, AFT OF THS DOOR. REMOVED AND REPLACED.

Part: CEILING PANEL — DAMAGED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG 132NC CEILING PANEL DAMAGED. FABBED 132NC PER EO# A300-5320-73929-P2.

Part: CEILING PANEL — DAMAGED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG 132LC CEILING PANEL DAMAGED. FABBED PANEL 132LC PER EO A300-73929-P2.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG AFT CARGO COMPARTMENT FLOOR PANEL 151QF LWR SKIN CRACKED. FABBED PANEL 151QF FROM 4522-377001CB-8 BATCH# 3356860 PER EO A300-5320-73928-RA.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FWD CARGO COMPT FLOOR PANEL 131AH SKIN CRACKED. FABBED PNL 131AH FROM 4522-374001CB-8 BATCH# 3356860 PER EO# A300-5320-73928-RA.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG AFT CARGO COMPARTMENT FLOOR PANEL 151UF LWR SKIN CRACKED. FABBED PANEL 151UF FROM 4522-374001CB-8 BATCH# 3356860.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FWD CARGO COMPARTMENT FLOOR PANEL 131BH LWR SKIN CRACKED. FABBED PANEL 131BH FROM 4522-374001CB-8 BATCH# 3356860 PER EO# A300-5320-23928-RA.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG AFT CARGO COMPARTMENT FLOOR PANEL 151NG LWR SKIN CRACKED. FABBED 151NG FROM 4522-37001CB-8 BATCH# 3356860 PER EO#A300-5320-73928-AA.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FWD CARGO COMPARTMENT FLOOR PANEL 132MG LWR SKIN CRACKED. FABBED PANEL 132MG FROM 4522-374001CB-8 BATCH# 3356860 PER EO# A300-5320-73928-RA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG AFT PIT TO FR58 AT STRINGER 50R, UNDER FLOOR HYDRAULIC LINE SUPPORT P/N A9358423220000 IS BROKEN AND CRACKED. REMOVED AND REPLACED LINE SUPPORT IAW SRM 51-40-21.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG LT WING TE, O/B LWR INTERCOSTAL, CRACKED ABOVE FLAP TRACK. REMOVED & REPLACED IAW SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG MCD FL PNL 252FJ, P/NB5327076800100 IS BROKEN. FABBED PNL 252FJ FROM 5024N40000155-G BATCH#3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C MCD FL PNL 252RG, P/N B5327083000100 CORNER BROKEN. FABBED PNL 252RG FROM 5024N400001SS-G BATCH 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PANEL 242EN, PN-B5327084600300 HAS DAMAGED INSERT HOLE; INSERT MISSING. FABBED PANEL 242EN FROM 5024N40000155-G, BATCH# PER SREO A300-5320-40532-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL P#B5327073400100 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 232NJ FROM 5024N40000155-G BATCH#3525521 PER SREA A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C MCD FL PNL 221FG, P/N B5327086400200 IS DAMAGED. FABBED PNL 221FG FROM 5024N400001SS-G BATCH 3525521PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C MCD FL PNL 2522G, P/N B532707750010. FABBED PNL 2522G FROM 5024N40001SS-G BATCH # 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C MCD FLOOR PANEL, P/N B5327086300200 IS DAMAGED ON LOWER SURFACE (PANEL ROCK). FABBED PNL 221BG FROM 5024N400001SS-G BATCH # 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C MCD FLOOR PANEL 222BG, P/N B5327086300200 IS DAMAGED ON LOWER SURFACE ( PANEL ROCK). FABBED PNL 222BG FROM 5024N400001SS-G BATCH #3525521 PER A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL P#B5327073300200 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 231QH FROM 5024N40000155-G BATCH#3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG MCD FL PNL 232WG, P/N5327074600400 IS DAMAGED. FOBBED PNL 232WG FROM 5024N40000155-G BATCH# 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PANEL B5327053300000 IS DAMAGED IN MULTIPLE AREAS. FABBED PANEL 152UF FROM 4522-374001CB-8 BATCH 3356860 PER EO# A300-5320-73928-RA.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C FLOOR PANEL P# 135327075200000 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 242CF FROM 5024N400001SS-G BATCH #3525321 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL# B5327074700400 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 231BH FROM 5024N40000155-G BATCH #3525521 PER SREO A300-5320-40552-B.

Part: BUSHING — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FAILED NON REMOVAL GAP CHECK. FABRICATED REPAIR BUSHING IAW SRM 53-15-16.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL P#B5327074200000 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 231BG FROM 5024N40000155-G BATCH# 3525531 PER SREA A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL P#B5327086600200 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 221CG FROM 5024N40000155-G BATCH 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PANEL B5327053100000 IS DAMAGED IN MULTIPLE AREAS. FABBED FLOOR PANEL 152QF FROM 4522-374001CB-8 BATCH# 3356860 PER EO A 300-5320-73928 RA.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PANEL B5327053300000, IS DAMAGED IN MULTIPLE AREAS. FABBED FLOOR PANEL FROM 4522-374001CB-8 BATCH# 3356860 PER EO# A300-5320-73928-RA.

Part: NOT REPORTED — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:A300 FAILED NON REMOVAL GAP CHECK. FAB REPAIR BUSHING IAW SRM 53-15-16.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL, P#B5327075300100 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 242LJ FROM 502N40000155-G BATCH# 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNL P#B5327074900000 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 231XG FROM 5024N40000155-G BATCH #3525321 PER SREO A300-5320-40552-B.

Part: BUSHING — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:A300 FAILED NON REMOVAL GAP CHECK. FABRICATED REPAIR BUSHINGS IAW SRM 53-15-16.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C FLOOR PANEL P# B53227075600000 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 241LH FROM 5024N400001SS-G BATCH 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C FLOOR PANEL P#1353270740500100 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 232SG FROMN5024N00001SS-G BATCH # 3525521 PER SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:C FLOOR PNL P# B5327075600100 IS DAMAGED IN MULTIPLE AREAS. FABBED PNL 242LH FROM 5024N400001SS-G BATCH # 3525521 PER SREO A300-5320-40552-B.

Part: BUSHING — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FAILED NON REMOVAL GAP CHECK. FABRICATED REPAIR BUSHING IAW SRM 53-15-16.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FLOOR PNLY P#B5327085100000 IS DAMAGED IN MULTIPLE AREAS. FOBBED PNL 241LN FROM 5024N40000155-G BATCH# 3525521 PER SREO A300-5320-40552-B.

Part: BUSHING — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FAILED NON REMVAL GAP CHECK. FABRICATED REPAIR BUSHING IAW SRM 53-15-16.

Part: BUSHING — OUT OF LIMITS (CABIN) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG FAILED NON REMOVAL GAP CHECK. FABRICATED REPAIR BUSHINGS IAW SRM 53-15-16.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:A300 MCD RT SHEAR PLATE BETWEEN FR 79 AND FR80- Y2127.6 CRACKED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-40-21.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:A300 MCD FLOOR LT SHEAR PLATE BETWEEN FR79 AND FR 80 Y2127.6 CRACKED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-40-21.

Part: CEILING PANEL — DAMAGED (CARGO BAY) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEGQAFT CARGO DOOR CUTOUT FWD SIDE CEILING PANEL BENT AT THE EDGE AND SCRATCHESFABBED CEILING PANEL PER EO# A300-5320-739329-P1

Part: INTERCOSTAL — CRACKED (SPOILER) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEG INTERCOASTAL CRACKED. FABRICATED NEW INTERCOASTAL IAW SRM.

Part: SKIN — GOUGED (LE SLAT) · airframe 17,303 hrs · 10,574 cycles

INSPECTION TYPE:SEGL/WING #2 SLAT INBD. TRAILING EDGE IS GOUGED, LWR SKINREPAIRED PER SRM 57-43-11, PAR 4.B. FIG 202

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR) · airframe 16,370 hrs · 10,038 cycles

INSPECTION TYPE:N/A CABIN MAIN ENTRANCE DOOR OPENING PRESSURE LOW. SERVICED MAIN ENTRY DOOR DAMP EMERGENCY CYLINDER PER AMM 52 10 14.

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR) · airframe 15,837 hrs · 9,736 cycles

CREW ENTRY DOOR OPENING PRESSURE LOW. SERVICEC EMERGENCY OPERATION CYLINDER IAW AMM 52-10-14-0301.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,831 hrs · 9,732 cycles

INSPECTION TYPE:SEG FWD PIT FLOOR PANEL PART# B5327052800000 IS DAMAGED. FABBED PANEL 131MG FROM 4522-374001CB-8, BATCH 3356860 PER EO# A300-5320-73928-AA.

Part: POWER SUPPLY — FAILED (DOOR) · airframe 15,670 hrs · 9,637 cycles

ASPSU WILL NOT PASS BITE TEST WRT AMM 52-73-00-0501. REPLACED ASPSU WRT 52-73-18-0401 NO HELP 0557453 07-27-18. PERFORMED ASPSU BITE TEST IAW AMM 52-73-00-05001. ALL CHECKS GOOD TEST IS NORMAL ALL REMAINING STEPS COMPLETED ESR: 52-73-18-01-001A

Part: DOOR — UNKNOWN · airframe 14,823 hrs · 9,152 cycles

INSPECTION TYPE:N/AONE FLIGHT CREW ENTRY DOOR WILL NOT CLOSE FROM OUTSIDECYCLED DOOR PERFORMED OPS CK OF DOOR PER A300 MM 52-10-00 OPS CK NORMAL

Part: DETECTOR — INOPERATIVE (MLG) · airframe 13,929 hrs · 8,611 cycles

ON GEAR RETRACTION, HAD THE ATS TRIP OFF EITH UNSUCCESSFUL RESET. SHORTLY THEREAFTER PITCH TRIM NR 1 FAILED. SHORTLY AFTER THAT CABIN PRESSURE FAILED. NOTED ACARS DID NOT SHOW OFF OR ON TIMES. ACARS NEVER LEFT GROUND. PERFORMED PROXIMITY DETECTOR UNIT BITE IAW TSM 32-61-00, BOX LIGHT ON WITH FAULT ID CODES 23,24. REPLACED PROXIMITY DETECTOR UNIT 54GB IAW MM 32-31-71-04. OPS TESTED GOOD ON GROUND.

Part: SKIN — CRACKED (LEFT WING) · airframe 13,701 hrs · 8,466 cycles

INSPECTION TYPE: 1C, LEFT WING FORWARD WING ROOT PANEL CUTOUT 513AB, CRACKED AT FWD OTBD CORNER. REPAIRED IAW SRM 53-15-63 PARAGRAPH 5A FIG 201.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 13,522 hrs · 8,357 cycles

AT FL360, RECEIVED A FWD CARGO DOOR NOT CLOSED INDICATION WITH A 300-500 FPM CABIN CLIMB RATE. RAN CHECKLIST TO EQUALIZE PRESSURE AND STARTED DESCENT BELOW 10000. ABOUT FL230 IN DESCENT THE DOOR WARNING LIGHT EXTINGUISHED. EMERGENCY DECLARED. INSPECTED FWD LWR CARGO DOOR, DOOR SEAL AND SEAL DEPRESSOR IAW AMM 52-31-11, NO DAMAGE WAS FOUND. MESSAGE DETERMINED TO BE INDICATION PROBLEM. R & R FIN 16 WS SWITCH IAW AMM 52-71-11-0401. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

FWD ENTRY DOOR EMERGENCY OPERATION CYLINDER PRESSURE IS LOW . SERVICED THE NITROGEN BOTTLE TO PRESSURE IAW AMM 52-10-14.

Part: LIGHT — UNKNOWN (SWITCH)

DURING SHUTDOWN, DISARM LIGHT DID NOT COME ON WITH SWITCH IN DISARM. SYSTEM OPS CKS GOOD IAW MM 33-51-00-0501.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DURING SHUTDOWN, EMERGENCY EXIT LIGHT DOES NOT SHOW DISARMED, BULB CHECKED OK. REPLACED THE BULBS IN THE LIGHT SWITCH IAW ESPM 20-45-11. SYS OPS CHECKED NORMAL IAW MM 33-50-00.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN FLOORBOARD 231LG HAS LOWER SKIN CRACKED. REPAIRED THE FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN FLOORBOARD 231PH LOWER SKIN IS CRACKED. REPAIRED THE FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN FLOORBOARD 252QG HAS MISSING EDGE FILLER. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: SEAT TRACK — CORRODED (FRAME 71) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT 7.5 IN AFT OF FRAME 71, BL 0. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,892 hrs · 6,720 cycles

LEFT WING INBD FLAP UPPER SURFACE FWD PANEL HAS DENT AND GOUGE. LT WING INBD FLAP UPPER SURFACE FWD PANEL BETWEEN RIBS 16-17 AND STRINGERS 2.1-2.2 IAW EA 300-5754-01-A5609-I/R AND EO 5750-55681-A.

Part: FLOORBOARD — DAMAGED (BULK CARGO) · airframe 10,892 hrs · 6,720 cycles

BULK CARGO FLOORBOARD 162HF HAS ONE MISSING INSERT. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 10,892 hrs · 6,720 cycles

RT INBD FLAP UPPER SKIN REPAIR DOUBLER CHAFED BETWEEN RIB 12 AND RIB 17, STGR 2.2 AND 2.3. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 12 AND RIB 17 STR 2.2 AND 2.3 IAW SRM 57-50-00, PARA 4E, FIG 205.

Part: FLOORBOARD — DAMAGED (BULK CARGO) · airframe 10,892 hrs · 6,720 cycles

BULK CARGO FLOORBOARD 161LF HAS TWO MISSING INSERTS. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — CRACKED (BULK CARGO) · airframe 10,892 hrs · 6,720 cycles

BULK CARGO FLOORBOARD 161KF IS CRACKED. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — CRACKED (BULK CARGO) · airframe 10,892 hrs · 6,720 cycles

BULK CARGO FLOORBOARD 162MF IS CRACKED. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D

Part: FLOORBOARD — DAMAGED (BULK CARGO) · airframe 10,892 hrs · 6,720 cycles

BULK CARGO FLOORBOARD 161MF HAS TWO MISSING INSERTS. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN SEAT TRACK IS CORRODED FRAMES 80-82, Y450. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 10,892 hrs · 6,720 cycles

FLOORBEAM AT FRAME 79 Y1580 CRACKED. REPAIRED IAW EA 300-5310-01-A5575-IR AND EO A300-5310-55488-A.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN SEAT TRACK IS CORRODED FRAMES 80-82, Y794.3. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 10,892 hrs · 6,720 cycles

FLOORBEAM AT FRAME 79 -Y1580 CRACKED. REPAIRED FLOORBEAM IAW EA 300-5310-01-A5575-IR AND EO A300-5310-55488-A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 10,892 hrs · 6,720 cycles

MAIN CABIN SEAT TRACK IS CORRODED AT FRAMES 80 - 82 Y0. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: TURBINE — FOD (NR 2 ENGINE)

SHORTLY AFTER TAKEOFF CREW SHUTDOWN NR 2 ENGINE DUE TO COMPRESSOR STALL. EMERGENCY DECLARED. PERFORMED BOROSCOPE IAW FIM 72-00-40 FIG 122, SHEET 4 BLK 7. FOUND 5TH STAGE BURNER CAN DETERIORATION. SECOND STAGE TURBINE DAMAGE. REPLACED NR 2 ENGINE. LEAK AND OPS CHECKED GOOD PER TC 710001-P1-1-400.

Part: SENSOR — OUT OF RIG (MLG)

ON DEPARTURE, GEAR WOULD NOT RAISE IN SYS 1, SWITCHED TO SYS 2 & RAISED GEAR NORMALLY. FOUND AND REPLACED MAIN TORQUE LINK SENSOR 64 GB OUT OF RIG IAW MM 320-00-00 0401. REF IPC 32-31-73-02A ITEM 020B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 231SG IS DELAMINATED AT LOWER SKIN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DENTED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, BULK CARGO FLOORBOARD 161LF HAS A DENT AT CENTER EDGE. FABRICATED BULK CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — BROKEN (CARGO BAY) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, BULK CARGO FLOORBOARD 161MF HAS INSERT BROKEN OUT AT FWD EDGE. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 231NG LWR SKIN IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 222EG UPPER SKIN IS TORN. FABRICATED FLOORBOARD IAW EO A300-5320-45567-A, APPENDIX B.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 221EG LOWER SKIN IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 222NG LWR SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOORBOARD 231MJ IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: SKIN — CHAFED (NR 1 SLAT) · airframe 8,568 hrs · 5,222 cycles

INSPECTION TYPE:3C, RT NR 1 SLAT LOWER SURFACE SKIN PREVIOUS REPAIR IS CHAFED INBD OF FOLDING NOSE. REPAIRED RT NR 1 SLAT LOWER SKIN BETWEEN RIB 20 AND 21A IAW EA 300-5750-01-A3962-A AND EO A300-5750-47458-B.

Part: MODULE — INOPERATIVE (FIRE CONTROL)

NR 2 ENG, NO FIRE DETECTION (A LOOP FAILURE, ACFT DEPARATED WITH MEL 26-12-01-1, NR 2 ENGINE FIRE DETECTION SYS B LOOP INOP. DEF NR 427111, CLEANED AND SECURE C/P'S DH3 AND DH4 AT R SIDE ENG CORE FIRE SENSING LOOPS. CLEANED AND SECURED C/P'S D4989P (1) D4953P OF ENG NR 2 PYL R&R E2 ENG FIRE CONTROL MODULE IAW MM 26-12-20-04. RAN & TAXIED ACFT FOR 50 MIN UP TO T/O RUN ALL IND NORMAL. THIS CLEARS 427111. PLACARD REMOVED.

Part: SLIDE — UNWANTED DEPLOY (PAX DOOR)

MAIN CABIN DOOR SLIDE DEPLOYED. INSTALLED NEW EMERGENCY DUAL ESCAPE SLIDE REF AMM 25-61-21-04. RESERVICED FWD DOOR DAMPER & EMERGENCY OPER CYL REF AMM 52-10- 14-03. PLACARD REMOVED AND M421869 CLEARED IN LOGBOOK.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

EVAC SLIDE LIGHT WARNING INOP, BUZZER OK.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231LJ PAIN MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOORPANEL IAW UPS EO A300-5320-16407-D, APPX. B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231VG PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 252DF IS BROKEN AT AFT EDGE. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOOR PANEL — DAMAGED (MAIN DECK 231PJ) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 PJ PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMANTION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 252WJ IS DELAMINATED AT AFT CORNER. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231KJ PAINT IS MISSING IN SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABRICATED FLOORBOARD IAW EO A300-5320-16407-D APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 261CM IS BROKEN AT AFT CORNER. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOOR PANEL — DAMAGED (MAIN DECK 231QG) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 QG PAINT MISSING SEVERAL A AREAS WITH SMALL AREAS OF DELAMINATION, FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK 231QJ) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 QJ PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.B

Part: FLOOR PANEL — DAMAGED (MAIN DECK 231GH) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 GH PAINT MISSING SEVERAL AR AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B

Part: FLOOR PANEL — DAMAGED (MAIN DECK 231RH) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 RT PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE: 5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 231HG PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOORPANEL IAW EO A300-5320-16407-D, APPX B.

Part: FLOORBOARD — CRACKED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 232LF IS BROKEN. ACCOMPLISHED REPAIR IAW SRM 53 10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 232WG IS DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231XG IS DELAMINATED AT AFT CORNER. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 252DN AFT CORNER EDGE BROKEN. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-D, APPX. B

Part: FLOORBOARD — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 241BF RT LOWER SIDE BROKEN. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — GOUGED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 241LJ LOWER RT SIDE GOUGED. ACCOMPLISHED REPAIR IAW SRM 53 10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231SG IS BROKEN. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 251KJ AFT CORNER BROKEN. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-D, APPX. B

Part: FLOORBOARD — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 251ZF FWD EDGE IS BROKEN. ACCOMPLISHED REPAIR IAW SRM 53 10-20 PARA 8.B FIG 203.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 262RF IS DELAMINATED AT AFT CORNER. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 241SN FWD EDGE BROKEN. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-D, APPX B.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 252FM AFT CORNER EDGE BROKEN. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-D, APPX B.

Part: SKIN — MISREPAIRED (LE FLAP) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, REPAIR SURVEY SEQ NR 165-W3-01 EXISTIG FLUSH REPAIR AT INBD FLAP OTBD BULLNOSE DOES NOT CORRELATE WITH SRM 57-50-00 FIG 208. REPAIRED IAW EO A300-5750-36980-A AND SAA EA 300-5753-01-A2198 IS SUE IR.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, RT INBD FLAP UPPER SKIN GOUGED IN SEVERAL PLACES APPROX 24 INCHES FWD OF RUB STRIP AN INBD OF NR 2 FLAP TRACK. REPAIRED IAW SRM 57-50-00, FIG. 205,

Part: FLOOR PANEL — DAMAGED (BULK CARGO 162HF) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, AFT BULK CARGO RT FLOOR PANEL 162HF REQUIRES REPLACEMENT IAW EO NR A300-5100-35883-A, APPX.B. FABBED FLOOR PANEL IAE EO A300-5320-16407-D, APPX D.

Part: FLOOR PANEL — DAMAGED (BULK CARGO 161JF) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5YR, AFT BULK CARGO CTR FLOOR PANEL 161JF REQUIRES REPLACEMENT IAW EO A300-5100-35883-A APPX B. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.D

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,881 hrs · 3,612 cycles

INSPECTION TYPE:5 YR, AFT BULK CARGO LT FLOOR PANEL 161 HF REQUIRES REPLACEMENT IAW EO A300-5100-35883-A. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. D

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

INSPECTION TYPE:N/A ECAM STATUS MSG DISPLAYED "EXIT ON" WITH EMERGENCY EXIT LIGHT ON, EMERGENCY EXIT LIGHT SWITCH IN THE ARM/DISARM OR ON (NORMAL ON) POSITION EMERGENCY EXIT LIGHT "BLINKS" WHEN SWITCH IS MOVED FROM DISARM TO ARM POSITION ON THE SWITCH. NO FAULT HISTORY 90 DAYS. ACCOMPLISHED EMERGENCY LIGHTING ADJUST TEST REF MM 33-51-00-05, NO FAULTS FOUND EMERGENCY LIGHT SYSTEM CHECKED GOOD.

Part: CONTROL MODULE — FAULTY (LANDING GEAR)

INSPECTION TYPE:N/A ON TAKEOFF LANDING GEAR WOULD NOT GO UP PAST NEUTRAL. LEVER PUT BACK DOWN; GEAR DOWN 3 GREEN ALL NORMAL. DEFERRED IAW MEL 32-30-01. DMI 364010 REMOVED AND REPLACED LANDING GEAR CONTROL MODULE PER MM 32-31-11-04 PARA 2. PERFORMED OPS CHECK IAW MM 32-31-11-04 AND 32-00-00-05. ALL OPS NORMAL. DEFERRAL CLEARED, PLACARD REMOVED.

Part: SWITCH — MALFUNCTIONED (ESCAPE SLIDE)

INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE DIFFERENTIAL PRESSURE WARNING HORN SOUNDS IN FLIGHT W/SLIDE ARMED, RED WARNING LIGHT ILLUMINATED. DEFERRED DOOR SLIDE PER MEL 52-11-01-3 DMP ACCOMPLISHED. PER CONVERSATION WITH CREW DETERMINED BUZZER AND WARNING LIGHT WERE FOR THE SLIDE ARMING NOT DIFFERENTIAL PRESSURE. REMOVED AND REPLACED SWITCH 9WN IAW MM 52-73-13-04 AND PERFORMED ADJ & TEST IAW 52-73-13-05. CHECKS OK. THIS CLEARS M 360383. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (LAVATORY)

INSPECTION TYPE:N/A EMERGENCY AUX WALL MOUNTED MIRROR LIGHT IN LAVATORY INOP. RELAMPED WITH A SERVICEABLE LAMP IAW A-300-600 AMM 33-51-21-4.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY)

INSPECTION TYPE:N/A AFT BULK CARGO COMPARTMENT PIT FOUND FLOOR PANEL PUNCTURED. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-10-20.