N146UP

Part: BATTERY — MALFUNCTIONED (ZONE 800) · airframe 26,073 hrs · 16,287 cycles

ESCAPE SLIDE LIGHTING BATTERY FUNCTIONAL CHECK FAILED CAPACITY CHECK R&R EMERGENCY EVACUATION SLIDE IAW AMM 25-61-21. SLIDE LIGHTING FUNCTIONAL TEST GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (ZONE 700) · airframe 25,765 hrs · 16,126 cycles

LANDING GEAR DID NOT RETRACT ON DEPARTURE. SWITCHED POSITION DET FROM SYSTEM 1 TO SYSTEM 2. LANDING GEAR RAISED NORMALLY. REPLACED LANDING GEAR CONTROL SWITCH REF AMM 32-31-11, OPS CHECK GOOD. REPLACEMENT PROX UNIT BAD FROM STOCK, ORDERED ANOTHER REPLACEMEN. C/W NORMAL GEAR EXTENSION AND RETRACTION IN REF TO AMM 32-31-00/501 OPS NORMAL

Part: DOOR — INOPERATIVE (FWD) · airframe 23,927 hrs · 15,047 cycles

FWD CABIN DOOR AUDIO WARNING INOPERATIVE. DEFERRED IAW MEL 52-73-01-2. M810723 ASSIGNED. NO DMPS. PLACARD INSTALLED.FOUND BROKEN WIRE ON WARNING HORN. REPLACED TERMINAL END AND INSTALLED ON WARNING HORN IAW ESPM 20-48-11-01 AND OPS CK IAW AMM 52-73-12 PB 0401. OPS CK GOOD. THIS CLEARS M810723. PLACARD REMOVED.

Part: OIL SYSTEM — LEAKING (APU) · airframe 23,217 hrs · 14,598 cycles

INSPECTION TYPE:N/AON APPROACH TURNED ENG & WING ANTI-ICE ON. SHORTLY AFTER HAD A FAINT SMELL IN COCKPIT. ON FINAL APPROACH NOTICED A FAINT VISIBLE SMOKE IN COCKPIT OVERHEAD LIGHT. SEEMED TO START TO DISSIPATE AFTER ANTI-ICE OFF.T/S C/O IAW TSM 21-20-00 PG 117. APU OIL LEAK FOUND AT OIL TEMP FITTING. LINE TORQUED IAW SPECIFIED VALUE PER A300-600 AMM 20-23-12 AND NO MORE LEAK PRESENT. ESC DUCT CLEANING PROC. C/O IAW AMM 21-51-00 PB 301. WATER SEPARATOR COALESCER BAGS REPLACED IAW AMM 21-51-16 PB 301. A/C OK TO CONTINUE SERV.

Part: NONE — NONE (CABIN) · airframe 22,379 hrs · 14,114 cycles

INSPECTION TYPE:N/AFUMES WITH OILY SMELL BEING DISCHARGED IN VENTILATION SYSTEM. BOTH PACK OPERATING FROM APU BLEED SMELL IN BOTH COCKPIT AND MAIN CARGO AREASREPLACED BOTH COALESCER BAGS REF AMM 21-51-16 KR #5601439 3-1-22 OPERATED LH ENG REF AMM 71-00-00 STARTED WITH HUFFER SMELL REMAINS KR #5601439 3-1-22. REPLACED BOTH COALESCER BAGS AGAIN IAW AMM 21-51-16 AND PERFORMED #1 AND #2 ENGINE GROUND RUN FOR OVER 30 MIN PER AMM 21-51-00-0301. SMELL

Part: UNKNOWN — ODOR (CABIN) · airframe 22,322 hrs · 14,083 cycles

INSPECTION TYPE:N/ASTRONG ODOR OF BREAD/ YEAST WETSOCKS FROM PACKS WHEN THROTTLES ADCANCED OUT OF IDLE THRUST FOR T/O ODOR REMAINED FOR ENTIRE FLIGHT.SUSPECT DE-ICD FLUID INGESTION LEADING TO UNSATISFACTORY CABIN AIR QUALITY PER A300 FIM 21-20-00 FIG. 210. RAN PACKS 1 AND 2 THRU FULL TEMP RANGE OVER 2 HRS ON APY REF AMM 21-51-00. OPS CKS GOOD, NO ODOR NOTED.

Part: STRAP — CRACKED (STRG 35RH) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CDURING CUSTOMER WALK THROUGH FOUND STIFFENER BETWEEN FR85 AND FR86 CRACKEDREMOVED AND REPLACED STIFFENER IAW SRM 51-40-21

Part: ENGINE — NONE (NONE) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR **REQUEST DMI TO COMPLY WITH EO 7100-53507 BETWEEN 10-20 FLIGHT CYCLES FOR RH ENGINE AFTER INSTALLATION.COMPLIED WITH EO-M-7100-53507COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760587

Part: ENGINE — NONE (NONE) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR**REQUEST DMI TO COMPLY WIT EO M-7100-53507 BETWENN 10 AND 20 FLIGHT CYCLES FOR LH ENG AFTER INSTALL. COMPLIED WITH EO M7100-53507 REF D760586COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760586

Part: BRACKET — BROKEN (#2 ENG) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.

Part: BRACKET — BROKEN (#2 ENG) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.

Part: FLAP — NONE (RT WING O/B FLAP) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300RT WING O/B FLAP O/B STATIC WICK BASE DIBONDED. AFTER FURTHER INVESTIGATION FOUND FLAP SKIN WITH CORROSION. MATERIAL REMOVED DOWN TO 0.043' (78%) WITH SOME CORROSION STILL REMAINING.ACCOMPLISHED DOUBLER SKIN REPAIRED PER EA #300-5754-27-A2710.

Part: WASHER — CRACKED (FR40R/HTENBOLT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 1 PER EA# A300-5710-81939-A , INSTALL ONLY.

Part: BUSHING — CRACKED (FR40R/H TENBOLT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IM MIDDLE HOLE.INSTALL BUSHING PER EA# A300-5710-81939-A, INSTALL ONLY.

Part: BRACKET — CRACKED (LOWER FUES) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300EXTERNAL LOWER FUSELAGE LH SIDE AR FR45 AFT AIRCON PANEL SUPPORT BRACKET CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: WASHER — CRACKED (FR40R/H TENBOLT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ROTO PROBE OF RH FR40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 2 PER EA# A300-5710-81939-A , INSTALL ONLY.

Part: BUSHING — CRACKED (FR40R/H TENBOLT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EA3 A300-5710-81939-A,INSTALL ONLY.

Part: SHIM — NONE (FR 44L FRAME FIT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR44 LH SIDE HAS CRACK.REPAIRED PER EO A300-5310-46789-G APPENDIX J INSTALL ONLY.

Part: SUPPORT — CRACKED (FR36-37 MCD R/H) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300MDC RH FLOOR LEVEL ANGLE WEB SUPPORT BTW FR36 AND 37 CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: WEB — CRACKED (FR38-38.1 R/HMCD) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300MDC RH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR 38 AND 38.1 CRACKED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (MDC FR61-61) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CMDC LH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR 61 AND 62 CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21

Part: DOUBLER — CRACKED (FRFITTING 46 R/H) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR 46 R/H SIDE HAS CRACK.ACCOMPLISHED REPAIR PER EO# A300-5310-46789-G APPENDIX K. INSTALL ONLY

Part: NONE — CRACKED (MCD FR38.1-38.2) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CMDC RH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR38.1 AND 38.2 CRACKEDREMOVED AND REPLACED IAW SRM 51-42-21

Part: BUSHING — CRACKED (FR40R/HTENBOLT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EO# A300-5710-81939-A,INSTALL ONLY.

Part: FLOOR PANEL — NONE (MAIN CABIN) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CFWD L/H MAIN CABIN FLOOR 231MJ JUST INSIDE MAIN CARGO DOOR HAS BROKEN CORNER INSERT AS MARKEDCOMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CFWD MAIN CABIN L/H SIDE FLOOR PANEL 231PH JUST INSIDE MAIN CARGO DOOR HAS DAMAGE TO LOWER SURFACE AS MARKEDCOMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CMDCC FLOOR PANEL 232SG DAMAGED/CRACKEDCOMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CMDCC FLOOR PANEL 231NJ DAMAGED/CRACKEDCOMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:CMDCC FLOOR PANEL 231VG DELAMINATEDCOMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300PNL 231LG BROKEN.FABBED IAW SREO A300-5320-40552-B.

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300MDCC FLOOR PANEL 242RM HAS CORNER DAMAGECOMPLIED WITH SREO A300-5320-42722-F.

Part: SUPPORT PLATE — CORRODED (FR34 Y1959-Y2462) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300MAIN DECK SEATRACK ADAPTER SUPPORT PLATE CORRODED AT FR34 BTW Y1959 AND Y2462.REMOVED AND REPLACED IAW A300 SRM 51-40-21.

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300MAIN DECK FLOOR PANEL 241BJ LOWER SURFACE COVER DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300PNL 262 PF DAMAGED.FABBED IAW SREO A300-5320-40552-B.

Part: BRACKET — CRACKED (#3 SPOILER) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300RT WING BELOW #3 SPOILER I/B HINGE ARM,END RIB INTER-COSTAL WEB FWD BRACKET CRACKED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21.

Part: LONGERON — NONE (475AL #1 FAIRING) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ENG 1 ACCESS PANEL 475AL I/B MID ATTACHMENT PLATE WITH ENLONGATED HOLES MARKED WITH RED.REMOVE AND REPLACE P/N 221-0081-327 IAW SRM 51-42-21.

Part: BRACKET — CRACKED (#3 SPOILER) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300LT WING BELOW #3 SPOILER I/B HINGE ARM,END INTER-COSTAL WEB FWD BRACKET CRACKED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21.

Part: ADAPTER — NONE (FR 20-Y1959) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300AT FRAME 20-Y1959 HAS A EXFOLIATED CLS ADAPTER.WORKED PER EO A300-5310-81793-A AND ECD 229968.

Part: PLATE — CRACKED (MCD FR 76-77 RH) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300AFT CABIN RH SIDE PLATE BETWEEN FR76 TO FR77 CRACKED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21 AND 53-18-18.

Part: ADAPTER — NONE (FR 19-Y1959) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300AT FRAME 19- Y1959 HAS A EXFOLIATED CLS ADAPTER.WORKED PER EO A300-5310-81794-A AND RCD 229967.

Part: RIB — CRACKED (LT KRUGER RIB) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300LT WING KRUEGER BOX AREA END RIB CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT ANGLE — NONE (321AL/ANGLE) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300DORSAL PIN PANEL 321AL ATTACHMENT ANGLE ON TOP FUSELAG RH FWD SECTION HAS ENLONGATED HOLES.REMOVED AND REPLACED ANGLE IAW-SRM 51-40-21.

Part: SEAL DEPRESSOR — GOUGED (FWD CARGO DOOR) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO DOOR CUTOUT AT AFT EDGE SEAL DEPRESSOR HAS SEVERAL GOUGES AND DAMAGED AREAS LOCATED THE LENGTH OF AFT SEAL DEPRESSOR.REMOVED AND REPLACED 1EA IAW SRM 51-40-21,REMAINING 2EA BLENDED IAW SRM 53-10-18.

Part: NONE — CRACKED (#1 PYLON) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:C#1 PYLON FAIRING 413BL HAS CRACK LOC AT LOWER CUTOUT CORNERFABRICATED DOUBLER IAW SRM 54-21-51 FIG 205

Part: WEB — DEFORMED (FR85-86 LH) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300WEB ANGLE STIFFNER AT TAIL COMPT LH SIDE OF BILGE BETWEEN FR85-86 IS DEFORMED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300PNL 132QG DAMAGED.FABBED PER SREO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 132AH SIDES DAMAGED.COMPLIED WITH SREO A300-5320-42722-C.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 132QG SIDES DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 131SG EDGES DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300AFT CARGO FLOOR PANEL 151VF EDGES DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 132DE SIDES DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 131DE CRACKED AND SIDES DAMAGED.COMPLIED WITH SREO A300-5720-42722-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 131AH DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 131GE DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300PNL 132MG DAMAGED.FABBED PER SREO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 131MG DAMAGED AT EDGES.COMPLIED WITH SREO A300-5320-42722-F.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO FLOOR PANEL 132MG CRACKED AT 2 LOCATIONS.COMPLIED WITH SREO A300-5320-42722-F

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300AFT CARGO FLOOR PANEL 152KG EDGES DAMAGED.COMPLIED WITH SREO A300-5320-42722-F.

Part: PANEL — CRACKED (#1 ENG I/B T/R) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300#1 ENG I/B T/R FAN DUCT LATCHES FWD CLOSING PANEL HAS CRACK.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT — CORRODED (CEILING SUPPORT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300FWD CARGO MIDDLE CEILING SUPPORT AT FR34 CORRODED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21.

Part: WEB — CRACKED (RH KRUGER COMPT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300RT WING KRUGER FLAP BOX COMPARTMENT REINFORCING WEB WITH CRACK.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SEAL — WORN (633AB) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300RT WING FLAP TRACK FAIRING 633AB I/B BULB SEAL WORN/TORN.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — BROKEN (POWERPLANT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ENG 2 T/R FWD CIRCUMFERENTIAL LATCH SUPPORT I/B BRACKET BROKEN.REMOVE AND REPLACE IAW SRM 51-40-21.

Part: BRACKET — DAMAGED (POWERPLANT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ENG 2 FAN COWL I/B FITTING SUPPORT BRACKET DAMAGED.REMOVE AND REPLACE IAW SRM 51-40-21.

Part: BRACKET — DAMAGED (POWERPLANT) · airframe 21,832 hrs · 13,825 cycles

INSPECTION TYPE:A300ENG 2 FAN COWL O/B FITTING SUPPORT BRACKET DAMAGED.REMOVE AND REPLACE IAW SRM 51-40-21.

Part: SEAT TRACK — CRACKED (FRMS 32-33) · airframe 21,586 hrs · 13,689 cycles

INSPECTION TYPE:N/AMAIN CARGO DECK SEAT TRACK DAMAGED BETWEEN FRAME 32 -33 AT Y=953SPLICED IN REPLACEMENT SECTION OF SEAT TRACK IAW EO A300-5310-81053-A

Part: A/C PACK — ODOR (NR 2) · airframe 20,765 hrs · 13,213 cycles

INSPECTION TYPE: N/A DIRTY SOCKS SMELL FROM PACK NR 2. PEFORMED OPERATION TEST OF PACK NR 2, REF AMM 21-11-00 PB 0001 STEP 3(2). RAN PACKS ORDER SMELL NO LONGER PRESENT.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 19,926 hrs · 12,734 cycles

EMERGENCY DECLARED. DURING CRUISE, YELLOW HYDRAULIC SYSTEM LEAKED TO RAT LEVEL. INSPECTED AND FOUND THE BLEEDER PLUG ON THE GY TRANSER UNIT TO HAVE A BLOWN SEAL CAUSING THE LEAK. REMOVED AND REPLACED THE DAMAGED O-RING AND INSTALLED THE BLEEDER PLUG IAW AMM 29-11-51-0401. NO FURTHER LEAKS. NO STARVATION IAW AMM 29-00-00-0301. SERVICED THE YELLOW HYD SYS IAW AMM 12-12-29.

Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 19,465 hrs · 12,441 cycles

INSPECTION TYPE:N/ABLACK BUTTON ON MAIN CABIN DOOR BROKEN, DOOR WILL NOT LATCH OPENLUBRICATED DOOR STAY MECHANISM, RELEASE BUTTON OPERATES NORMAL PER AMM 52-10-00-0001

Part: STICK SHAKER — FAULTY (COCKPIT) · airframe 19,231 hrs · 12,312 cycles

INSPECTION TYPE:N/AAIR TURN BACK - ON TAKE OFF ROLL THRU 10,000 FT AIRCRAFT HAD A SEVERE SHAKING IN YOKE AND RUDDER ALL ECAM INDICATIONS NORMALISOLATED TO CAPTAINS STICK SHAKER WHEN PULL CAPTAINS STICK SHAKER CB THE SHAKING GOES AWAY & WHEN RESET SHAKING COMES BACK MM 0558800 1-8-20/ REF ITEM #2 L/P 353197 R/R OF #1 FMC CK STICK SHACKES ON GROUND GROUND CK NORMAL IAW MM 31 53 34 OK FOR SERVICE EFF SOURCE REF IPC 31 53 08 03 FOR SERVICE

Part: THRUST REVERSER — INOPERATIVE (RIGHT) · airframe 18,929 hrs · 12,163 cycles

INSPECTION TYPE:N/AAFTER LANDING #2 THRUST REVERSER WOULD NOT STOWREMOVED AND REPLACED RT ENG I/B REVERSER PER AMM 71-13-03-0401. OPS CK NORMAL

Part: SWITCH — INOPERATIVE (ENTRY DOOR) · airframe 18,411 hrs · 11,855 cycles

INSPECTION TYPE:N/A DURING PREFLIGHT FOUND RED WARNING IN DOOR INOP. DEFERRED IAW MEL 52-73-01-1 PLACARD INSTALLED ENTERED IN DI LOG. **SUPPLEMENTAL SDR** REPLACED WARNING TEST SWITCH PER AMM 52-73-14-0401, WARNING LIGHT ASSY PER AMM 52-73-18-0401. & AUTONOMOUS STBY PWR SUPPLY PER AMM 52-73-18-0401. OPS CK GOOD. PLACARD REMOVED & ITEM CLEARED. IPC 52-11-11-23C/52-73-01-02A. THIS CLEARS M676338

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR23A HOLE 2, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.118 - 0.120 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATED 22-MAY-19.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C AFT CARGO DOOR LOWER SUPPORT BRACKET CRACKED @ FR 64A-65. REMOVED & REPLACED IAW SRM 51-40-21.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C #2 PYLON AFT LOWER FAIRING IB END CAP BRACKET ON PAN ASSY CRACKED AS MARKED. REMOVED AND REPLACED BRACKET ANGLE ASSY IAW SRM 51-40-21.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C AFT CARGO DOOR FORK FITTING FRAME 62 BOTTOM HOLE FWD SIDE SHOWS CRACK INDICATION IN SKIN LAYER AT THE 12'OCLOCK POSITION (MARKED). GENERATED RFTS #8, ACCOMPLISHED OPEN HOLE INSPECTION, REAR HOLE, ACCOMPLISHED OPEN HOLE ROTO PROBE CW, NO CRACK INDICATION NOTED.

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1CAFT CARGO DOOR FORK FITTINGS FRAME 60A 2ND HOLE FROM TOP FWD SIDE SHOW A CRACK INDICATION IN SKIN LAYER AT THE 9 O'CLOCK POSITIONACCOMPLISHED HAECO REO-G22051 AND UPS EO A300-5230-72784A

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C AFT CARGO COMPARTMENT FWD BULKHEAD UPPER SUPPORT BRACKET FR54 @ LBL 77 CRACKED. REMOVED AND REPLACED NEW UPPER SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FR38.2 RBL60 BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FR38.2 LBL22 BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FR38.2 @ RBL22 CRACKED BRACKET. REMOVED AND REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FR38.2 @ RBL22.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FR38.2 @ RBL41 BRACKET CRACKED. REMOVED AND REPLACED FWD CARGO AFT BULKHEAD UPPER FRAME SUPPORT 38.2 @ RBL41.

Part: RETAINER — DEFORMED (APU CUTOUT) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C APU COMPARTMENT,DOOR CUTOUT,AFT EDGE, MIDDLE SEAL RETAINER DAMAGEDREMOVED AND REPLACED DAMATGED RETAINER PER A300-600 SRM 51-40-21

Part: SKIN — DEFORMED (TAILCONE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1CAPU COMPARTMENT. TAIL CONE, AFT EDGE OF APU CUTOUT DAMAGED / GOUGEDREPAIRED PER UPS EO NO: A300-5330-72788-A

Part: STRAP — CRACKED (FUSELAGE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C TAIL SECTION INTERNAL STRUCTURAL INTERCOSTAL IS DEFORMED BETWEEN FRAME 86-87 RT JUST ABOVE FLOOR LEVEL. REMOVED AND REPLACED STRAP IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (NR 2 ENGINE) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C #2 ENG LOWER "V" BAND LATCHING SUPPORT BRACKET CRACKED. REMOVED AND REPLACED LATCHING SUPPORT IAW P AND W SRM 54-04-01.

Part: LOUVER — CRACKED (NR 1 PYLON) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C #1 PYLON PANEL 413BL 2EA LOUVERS ARE CRACKED LHS AS MARKED. REPAIRED #1 PYLON 413BL LOUVERS IAW SRM 54-52-51.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C PARTS RACK: #1 PYLON AFT LOWER FAIRING IB AND OB END CAP BRACKETS AT LOWER PAN ASSY CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-21.

Part: VENT — CRACKED (NR 1 PYLON) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C #1 PYLON PANEL 413BL LOUVER VENT CRACKED RHS AS MARKED. REPAIRED #1 PYLON PANEL 413BL LOUVER RHS IAW SRM 54-52-51.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE:1C PARTS RACK: #1 PYLON AFT LOWER FAIRING IB AND OB END CAP BRACKETS AT LOWER PAN ASSY CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-21.

Part: SUPPORT STRAP — CRACKED (MAIN CABIN) · airframe 18,286 hrs · 11,787 cycles

INSPECTION TYPE: 1C, MAIN CABIN CEILING PNL SUPPORT STRAP IS CRACKED AND BENTREMOVED AND REPLACED SUPPORT STRAP PER A300-600 SRM 51-40-21 & AIRBUS DWG A25576098 ISSUE B

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,281 hrs · 11,784 cycles

INSPECTION TYPE:OTHAFT CARGO COMPARTMENT; FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR-54 @ LBL-36 CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,281 hrs · 11,784 cycles

INSPECTION TYPE:OTH AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR-54 @ LBL-40 CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,281 hrs · 11,784 cycles

INSPECTION TYPE:1C AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 @ RBL 36 CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 17,269 hrs · 11,238 cycles

LOWER LAV LIGHT INOP. RELAMPED GROUND CHECKED GOOD REF MM 33-51-21.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 16,974 hrs · 11,086 cycles

FUSLAGE SKIN DAMAGE AT FR18 BETWEEN STR 32R & 33R. REF EO A300-5330-67871-B PERMANENT REPAIR. INSTALLED REPAIR DOUBLER. REPAIR COMPLIED WITH REF EO A300-5330-67871-B.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,789 hrs · 10,981 cycles

EMERGENCY LIGHT IN THE LAVATORY, BULBS WERE OUT. REPLACED THE BULBS IAW AMM 33-51-21.

Part: FWC — CRAZED (PRESS IND) · airframe 16,767 hrs · 10,969 cycles

INCREASE AT FL 320, 3 HOURS INTO FLT CHECKED ECAM SUNOPTICS AND FOUND ALL 3 HYD PRESSURES LOW. BLUE = 1500, GRN = 1500, YELLOW =1600. PRESSURES - 100. DVERTED. ON LDG, PRESSURE BLUE & GRN = 2850, YELLOW 300 PSI. RESET SDAC & CYCLED-TROUBLESHOT PER ASM 29-32-00 DETERMINED 1WV FAULTING FOR PRESS IND FWC DID NOT FLAG ANY OTHER INDICATIONS. REMOVE AND REPLACED SDAC PER AMM 31-55-22 / 401 OPS CKS OK PER AMM 31-51-00 / 501. IPC 31-55-08-02, ITEM OIOC.

Part: SWITCH — INOPERATIVE (CONTROL HANDLE) · airframe 16,675 hrs · 10,914 cycles

AFTER TAKEOFF, THE LANDING GEAR HANDLE STUCK IN THE CENTER OR DOWN POSITION. COULD NOT RAISE THE HANDLE TO THE UP POSITION. GEAR REMAINED DOWN AND LOCKED. REPLACED THE LANDING GEAR CONTROL SWITCH UNIT IAW MM 32-31-11-0401, CHECKED OK.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 15,603 hrs · 10,234 cycles

RIGHT ELEVATOR UPPER SURFACE HAS TRAPPED WATER INDICATION. REPAIRED THE ELEVATOR SURFACE IAW SRM 55-21-12.

Part: ATTACH ANGLE — CRACKED (FRAME 79) · airframe 15,603 hrs · 10,234 cycles

MAIN CABIN SEAT TRACK ATTACH ANGLE AT FRAME 79, Y-1580 IS CRACKED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-40-21.

Part: ATTACH ANGLE — CRACKED (FRAME 79) · airframe 15,603 hrs · 10,234 cycles

CABIN SEAT TRACK ATTACH ANGLE A FRAME 79, Y1580 IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-21

Part: FLOORBEAM — CORRODED (FRAME 65) · airframe 15,603 hrs · 10,234 cycles

AFT CARGO DOOR SILL, FRAME 65, STRINGER 44R, CORRODED ON THE END OF THE FLOORBEAM. REMOVED AND REPLACED THE FLOORBEAM, SUPPORT FITTING IAW SRM 51-40-21

Part: FLOORBEAM — CRACKED (FRAMES 79) · airframe 15,603 hrs · 10,234 cycles

MAIN CABIN FLOORBEAM AT FRAME 79, Y-1580 IS CRACKED. REPAIRED IAW EO A300-5310-64233-A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,603 hrs · 10,234 cycles

MAIN CABIN FLOORBEAM AT FRAME 79, Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-64233-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,397 hrs · 10,099 cycles

EMER LIGHT FOR LAV IS BURNT OUT REMOVED AND REPLACED BULB PER MIM 33-51-00 OPS CHECK GOOD. ESR: IPC 33-51-21-02

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 14,962 hrs · 9,855 cycles

INSPECTION TYPE: 1C2C, NR 1 PYLON 412DR PLATE FITTING CRACKED. REMOVED AND REPLACED THE PLATE IAW SRM 51-40-21

Part: ATTACH ANGLE — CRACKED (AFT CARGO) · airframe 14,962 hrs · 9,855 cycles

INSPECTION TYPE: 1C, & 2C, AFT CARGO FWD BULK HEAD PANEL UPPER ATTACH ANGLE CRACKED BL 0. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-21.

Part: ATTACH ANGLE — CRACKED (AFT CARGO) · airframe 14,962 hrs · 9,855 cycles

INSPECTION TYPE: 1C, & 2C, AFT CARGO FWD BULKHEAD PANEL UPPER ATTACH ANGLE CRACKED AT RBL 40. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: JACKSCREW — FAILED (RT TE FLAP) · airframe 14,843 hrs · 9,767 cycles

DURING APPROACH FLAPS SYS 1 FAULT FLAPS SYS 2 FAULT. FLAPS STUCK. C/W ON APP SLATS FULLY EXTENDED. FLAPS STUCK AT 15. REMOVED RT SIDE NR 1 FLAP JACKSCREW IAW AMM 27-54-21 PB 0401. INSTALLED NR 1 FLAP JACKSCREW IAW AMM 27-54-21 PB 0401. OPS CHECKED NORMAL.

Part: FLAP — FAULTED (WING) · airframe 14,777 hrs · 9,726 cycles

CORNER FLAP SYS 1, FLAP SYS 2, FAULT. FLAPS STUCK, 15/15. PERFORMED BITE ON SFCC 1 AND 2 AND GOT A KRUGER RT EXTEND SW MESSAGE. TROUBLESHOT IAW TSM 27-80-12,102. OPS CHECKED NORMAL. COULDN’T FIND ANY WIRING PROBLEMS AND COULD NOT DUPLICATE ORIGINAL WRITE UP ON THE GROUND. NO CURRENT HISTORY. SYS OK FOR SERVICE.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 14,270 hrs · 9,392 cycles

MAIN CARGO DECK FLOORBOARD DAMAGE AT POSITION 10L. FABRICATED A NEW FLOORBOARD IAW EO A300-5320-40552-B AND EO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD FLOOR PANEL POS 10R DAMAGED. FABRICATED NEW PANEL IAW EO A300-5320-16407-E.

Part: WINDSHIELD — FAILED (COCKPIT)

ON CLIMB F/O NOTED WINDSHIELD ARCING FOLLOWED SHORTLY BY WINDOW HEAT WARNING ON ECAM FOLLOWED BY F/O WINDSCREEN OUTER PANEL SHATTERING. R & R RT FRONT WINDSHIELD IAW AMM 56-11-11-0401. OPS CHECKED GOOD IAW 30-42-00-501, REF IPC 56-11-01-018.

Part: FIRE LOOP — LOOSE (NR 2 NACELLE)

AFTER TAKEOFF, BOTH CREW NOTICED A "DIFFERENT" SOUND FROM ENGINES. ACFT SOUNDED LIKE MAY HAVE HAD A COMPRESSOR STALL BUT WE HAD NORM ENG INDICATIONS. AT 200' RECEIVED AN ENGINE FIRE LIGHT ON ENG NR 2. AFTER ABOUT 15-20 SEC. WARNING WENT OUT AND RECEIVED AN ENG 2 LOOP A FAULT. ELECTED TO DIVERT, ABOUT 5 MINUTES, RECEIVED A LOOP B FAULT ON ENG 2. PERFORMED VISUAL INSPECTION IAW FIM AND SENT DOWNLOAD DATA TO ENGINEERING. NO ABNORMAL OPERATION OF ENGINE FOUND. TIGHTENED B LOOP, REPLACED A LOOP AND REPLACED FDCU. OPS CHECKED GOOD.

Part: LATCH — UNSECURE (F/O WINDOW)

DURING PREFLIGHT, F/O DISCOVERED WINDOW NOT LATCHING PROPERLY. FOUND EMERGENCY ACCESS LATCH ON OUTSIDE OF AIRCRAFT NOT CLOSED PROPERLY. CLOSED LATCH. WINDOW CLOSED AND LOCKED NORMALLY.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241BQ IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK AT BS 953 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 241LJ DELAMINATED. REPAIRED IAW EO NR A300-5320-42721-B, PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK AT FR62 AND STA -Y953 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 251WG CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241RM IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241VM IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231GH IS CRACKED ON LOWER SKIN. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231HG HAS A HOLE IN THE LOWER SKIN ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 222BG PUNCTURED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 232NJ HAS A PUNCTURE AND DELAMINATION AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231SG IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 3241TM IS BROKEN AT CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231MJ HAS FOUR CORRODED INSERTS. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 231LG PUNCTURED AND INSERTS CORRODED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231QH CORNER IS BROKEN OFF. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242TN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 231PH PUNCTURED AND CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252LG IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FLOOR PANEL 262FM CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251GJ IS DELAMINATED AT LOWER SKIN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242VM IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252ZJ IS DELAMINATED AT LOWER SKIN. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252YM IS CRACKED AT UPPER CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252GF IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 261SF HAS DAMAGED EDGE SEALING. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 261GH HAS DAMAGED INSERTS. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251LG HAS DAMAGED INSERTS. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 261AM CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 261FM CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242UM IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242LJ HAS A MISSING INSERT. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241SK IS CRACKED AT LOWER SURFACE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241NN IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251XJ HAS A CRACK AT LOWER SURFACE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD NR 242UK LOWER SURFACE IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252ZG LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-4272-B, PARA 6A.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 242PK DELAMINATED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242NK IS CRACKED AT LOWER SURFACE FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241PM IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241SH IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241YK IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241AJ IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232BH IS DELAMINATED AT LOWER SKIN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FLOORBOARD 242EK CRACKED AT MDC. PERMANENTLY REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 242RH IS CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251JF HAS A CRACK ON LOWER SKIN. ACCOMPLISHED REPAIR IAW EO A300-5320-4272-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSP TYPE:10YR, MAIN CABIN FLOORBOARD NR 251VJ HAS A CRACK ON LOWER SKIN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 242GF IS DEBONDED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241RH IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242KF HAS EDGE DAMAGE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241TK IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241BF LOWER SKIN IS DAMAGED IN TWO PLACES. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242SK IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241NK IS CRACKED AT TWO PLACES ON LOWER SKIN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252LM HAS A CRACK ON LOWER SKIN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 242ZG LOWER FACE SHEET IS DAMAGED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241KF IS CRACKED AT LOWER SURFACE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B APPENDIX B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 242YG CORNER IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251FJ IS CRACKED AT EDGE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 252QG HAS A PUNCTURE AT LOWER SKIN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231XG HAS A PIECE BROKEN OFF AND LOWER SKIN DAMAGED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252KJ HAS A PUNCTURE AND A CRACK ON LOWER SKIN. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252FM LOWER SKIN IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 221EG LOWER SURFACE IS CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232UG LOWER SURFACE IS PUNCTURED IN 2 PLACES. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232XG LOWER FACE SHEET IS DAMAGED. ACCOMPLISHED REPAIR ON FLOOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251BN IS DELAMINATED AT UPPER AND LOWER SKIN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR FRAME 12A RT FITTING IS CRACKED. R & R FRAME FITTING IAW EO A300-5310-23539-C, APPENDIX E.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FWD CARGO FLOORBOARD 132FE IS BROKEN ON CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOOR PANEL — CRACKED (COURIER AREA) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, COURIER FLOOR PANEL 221WF CRACKED. REPAIRED IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FWD CARGO FLOORBOARD 132SG IS BROKEN ON THE CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, BULK CARGO FLOORBOARD 161KF HAS DAMAGED FASTENER HOLE. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, BULK CARGO FLOORBOARD 161GF HAS DAMAGED INSERT. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152SF IS CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PAR 6A.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, AFT CARGO FLOORBOARD 151QF IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK AT FR 80 IS CORRODED. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80 STA Y794.3. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, AFT CARGO FLOORBOARD 151SF IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-532042721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (AFT CARGO BAY) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, AFT CARGO FLOORBOARD 152KG IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80 Y794 ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80, STA 1137.1. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — DENTED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 161HF IS DENTED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80 STA Y0. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80 STA-Y1137.1. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR80, STAY450. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, AFT CARGO FLOORBOARD 151UF IS CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR AFT CARGO FLOORBOARD 152VF IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FWD CARGO FLOORBOARD 131MG IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 131SG IS BROKEN ON CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOOR SUPPORT TEE UPPER AND LOWER SURFACE HAS CORROSION AROUND FASTENERS HOLES, BELOW FLOOR PANEL 221FF FR12A TO FR 17 STA Y1959. R & R MAIN CABIN FLOOR SUPPORT TEE STA Y1959 FROM FR12A TO FR 17.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FUSELAGE SKIN LIGHTNING STRIKE AT FR57.1 BETWEEN S2L AND 3L. ACCOMPLISHED REPAIR ON FUSELAGE SKIN IAW SRM 53-10-12, FIG 208.

Part: SKIN — DENTED (EMPENNAGE) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, DENT AT EMPENNAGE 6 INCHES AFT OF FR 98 AT UPPER LT SIDE. ACCOMPLISHED REPAIR ON SKIN IAW SRM 53-19-12, PARA 6, FIG 202.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FUSELAGE SKIN HAS A LIGHTNING STRIKE AT FR54.2 BETWEEN STRG 2L AND 3L. ACCOMPLISHED REPAIR ON FUSELAGE SKIN IAW SRM 53-10-12, FIG 208.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, FUSELAGE SKIN HAS A LIGHTNING STRIKE. ACCOMPLISHED REPAIR ON FUSELAGE SKIN IAW SRM 53-10-12, FIG 208.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251DF IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,109 hrs · 7,244 cycles

INSPECTION TYPE:10YR, FLOOR PANEL 242TN CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN AND JACK POINT FITTING AT FR 85 BETWEEN STG R 44L AND STG R 44R IS DAMAGED. REPAIRED IAW EO A300-5330-46026-A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,161 hrs · 6,652 cycles

INSPECTION TYPE:4C, LT WING CENTER FLAP UPPER SKIN BETWEEN RIBS 21 AND 23, STRINGERS 2.6 AND 2.7, EXISTING REPAIR DOUBLER IS GOUGED. REPAIRED LT WING CTR FLAP UPPER SKIN BETWEEN RIBS 21 AND 23, STRINGERS 2.6 AND 2.7 IAW STA-SA EA 300-5750-01-A3596-I/R AND EO A300-5750-45074-A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,161 hrs · 6,652 cycles

INSPECTION TYPE:4C, LT WING CTR FLAP REPAIR DOUBLER IS GOUGED BETWEEN RIB 13 AND RIB 15 STR 2.6 AND STGR 2.8. ACCOMPLISHED REPAIR ON LT WING CTR FLAP BETWEEN RIB 13 AND RIB 15, STGR 2.6 AND STR 2.8 IAW EO A300-5750-45089-A, PARA 6A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,161 hrs · 6,652 cycles

INSPECTION TYPE:4C, LT INBD FLAP NOSE AND UPPER SKIN FWD OF STGR 2.2 AND BETWEEN RIBS 3 AND 4 HAS 10 EA GOUGES. REPAIRED LT INBD FLAP NOSE AND UPPER SKIN FWD OF STR 2.2 AND BETWEEN RIBS 3 AND 4 HAS 10 EA GOUGES IAW EO A300-5750- 45129-A AND STA-SA EA 300-5750-01-A3592-I/R.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 10,161 hrs · 6,652 cycles

INSPECTION TYPE:4C, RT WING OTBD FLAP BULLNOSE SKIN IS CHAFED BETWEEN RIB 1 AND RIB 2. ACCOMPLISHED REPAIR IAW EO A300-5750-45028-A PARA 6A.

Part: HANDLE — INOPERATIVE (L1 DOOR SLIDE)

L1 DOOR EMERGENCY EXIT SLIDE HANDLE WILL NOT MOVE TO ARMED POSITION M464722. REMOVED EMERGENCY SLIDE COVER ON MAIN ENTRY DOOR. REMOVED ESCAPE SLIDE IAW MM 25-61-21-04. CLEANED AND LUBED GIRT BAR, FITTINGS, AND FLOOR FITTINGS. REINSTALLED ESCAPE SLIDE IAW 25-61-21-04. OPS CK GOOD. THIS CLEARS M464722. PLACARD REMOVED.

Part: HANDLE — BINDING (L1 DOOR SLIDE)

L1 DOOR EMERGENCY EXIT SLIDE HANDLE WILL NOT MOVE TO ARMED POSITION M464722. DEFERRED IAW MEL.

Part: FITTING — DIRTY (GIRT BAR)

CABIN DOOR SLIDE DISARMING LEVER FELT UNUSUAL WHEN DISARMING SLIDE. FOUND AND CLEANED DEBRIS AT AFT GIRT BAR FITTING. OPERATED ARM SLIDE HANDLE, OPS CK NORMAL IAW MM 52-10-30-06.

Part: A/C PACK — FAULTED (COCKPIT)

DIVERSION - PACK NR1 & PACK NR2 FAULT ON BOTH WHILE CLIMBING TO FL 350. STOP CLIMB, LANDED. T/S IAW AMM 36-11-00-05 - ALL CHECKS NORMAL. RUN BOTH PACKS FOR 3 HRS. OPS CHECK GOOD. REPLACED ENG NR1 & NR2. START SELECTOR RELAY AS PRECAUTIONARY. ALL OPS CHECK GOOD. OK FOR SERVICE.

Part: SLIDE — LOW PRESSURE (EXIT DOOR)

ON PREFLIGHT, FOUND ESCAPE SLIDE PRESSURE IN RED AREA. TRANSFER TO M423412 IAW MEL 52-11-01-3. PLACARD INSTALLED. DOOR VERIFIED CLOSED AND LOCKED. REMOVED AND REPLACED CREW ESCAPE SLIDE. OPS CHECK GOOD. OK FOR SERVICE. PLACARD REMOVED.

Part: SKIN — PUNCTURED (AILERON)

INSPECTION TYPE:N/A .375 INCH PUNCTURE BOTTOM SKIN OF T/E WEDGE. REPAIRED PER EO A300-5750-35403-B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO COMPARTMENT PANEL 242LJ REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED MAIN CARGO FLOOR PANEL 242LJ PER EO A300-5320-16407-C APPENDIX B.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C REPAIR SURVEY SEQ 146-W3-01 ON LEFT WING CENTER FLAP UPPER SKIN DOUBLER REPAIR IS GOUGED. FABBED AND INSTALLED REPAIR DOUBLER IAW EO A300-5750-34432-A AND SAA EA 300-5753-01-A1929.

Part: SKIN — CHAFED (TE FLAP) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C LT WING CENTER FLAP UPPER SKIN CHAFED, APP 24 INCHES ABOVE RUB STRIP NR 4 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW EO A300-5750-34429-A AND SAA EA 300-5753-01-A1939.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO COMPARTMENT PANEL 251EN REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 251EN PER EO A300-5320-16407-C APPENDIX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CABIN COMPARTMENT FLOOR PANEL 252DF REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER UPS EO A300-5320-16407-C. FABRICATED MAIN CABIN FLOOR PANEL 252DF PER EO A300-5320-16407-C APPENDIX B.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C MAIN CARGO FLOORBOARD 252JF REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3C MAIN CARGO FLOORBOARD 222DG REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C MAIN CARGO FLOOR PANEL 241HF REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C MAIN CABIN FLOOR PANEL 242LT REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO DECK FLOOR PANEL 232SG REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407C. FABRICATED MAIN CARGO DECK FLOORBOARD 232SG PER EO A300-5320-16407 -C APPENDIX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO FLOOR PANEL 242EF REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED MAIN DECK FLOOR PANEL 242EF PER EO A300-5320-16407-C APPENDIX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO COMPARTMENT FLOOR PANEL 251ZF REQUIRES EVALUATION FOR SRM REPAIR PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 251ZF PER EO A300-5320-16407-C APPENDIX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C MAIN CARGO FLOOR PANEL 231QJ REQUIRES EVALUATION FOR REPAIR OR REPLACEMENT. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: SKIN — CORRODED (TE FLAP) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3/C LT WING O/B FLAP, O/B STATIC WICK BASE CORRODED BETWEEN BASE AND FLAP SKIN. FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO A300-5750-34431-A AND A SAA EA 300-5753-01-A1937.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CABIN FLOOR PANEL 241NK REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 241NK PER EO A300-5320-16407-C APPENDIX B.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3C MAIN CARGO FLOORBOARD 231NJ REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER UPS EO A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C UPPER DECK CARGO BAY FLOOR PANEL 261GH REQUIRES EVALUATION FOR SRM OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED MAIN DECK FLOOR PANEL 261GH PER EO A300-5320-16407-C APPENDIX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CARGO COMP FLOOR PANEL 241UK REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 241UK PER EO A300-5320-16407-C APPENDIX B.

Part: FLOORBOARD — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C MAIN CABIN FLOORBOARD 251ZG REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT. FABRICATED FLOORBOARD 251ZG PER EO A300-5320-16407-C APPENDIX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3C MAIN CARGO DECK FLOOR PANEL 262PF REQUIRES EVALUATION FOR SRM REPAIR OR REPLACEMENT PER UPS EO A300-5320-16407-C. FABRICATED FLOOR PANEL 262PF PER UPS EO A-300-5320-16407-C APP B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C AFT CARGO COMPARTMENT FLOOR PANEL 151UF REQUIRES REPLACEMENT PER EO A300-5320-16407-C. FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 151UF PER EO A300-5320-16407-C APPENDIX C.

Part: FLOOR PANEL — UNKNOWN (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:3C BULK CARGO COMPARTMENT AFT FLOOR PANEL 161JF REQUIRES REPLACEMENT PER UPS EO-A300-5320-16407-C. FABRICATED BULK CARGO COMPARTMENT AFT FLOOR PANEL 161JF PER EO A300-5320-16407-C APP D.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:C/3 BULK CARGO COMPARTMENT FLOOR PANEL 161GF REQUIRES REPLACEMENT PER EO A300-5320-16407-C. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX D.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C BULK CARGO COMPARTMENT FLOOR PANEL 162HF REQUIRES REPLACEMENT PER EO A300-5320-16407-C. FABRICATED BULK CARGO COMPARTMENT FLOOR PANEL 162HF PER EO A300-5320-16407-C APPENDIX D.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C AFT PIT FLOOR PANEL 161LF AT FR 66 REQUIRES REPLACEMENT PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 161LF PER EO A300-5320-16407-C APPENDIX D.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 7,497 hrs · 5,008 cycles

INSPECTION TYPE:1C AFT CARGO COMPARTMENT FLOOR PANEL 152KG REQUIRES REPAIR PER SRM OR REPLACEMENT PER EO A300-5320-16407-C. FABRICATED FLOOR PANEL 152KG PER EO A300-5320-16407-C APP C.

Part: UNKNOWN — ODOR (COCKPIT)

STRONG CLEANING SOLVENT TYPE ODOR DETECTABLE ONLY FROM COPILOT'S SIDE OF C/P IN AIR AND ON GROUND. NO ODOR DETECTED IN AVIONICS BAY. POTENTIAL HEALTH SIDE AFFECTS DUE TO EXPOSURE OF SAID UNKNOWN ODOR. UNLOADED AIRCRAFT. RAN PACKS AND ENGINES. INSPECTED ALL CARGO COMPARTMENTS AND AVIONICS BAY NO ODOR DETECTED AT THIS TIME. OK FOR SERVICE.

Part: WARNING LIGHT — INOPERATIVE (EVAC SLIDE)

INSPECTION TYPE:N/A EVAC SLIDE WARNING LIGHT INOP. DEFERRED PER MEL 52-73-01-1. M 355534 PLACARD INSTALLED. RESET PLUG ON ASPSU. PERFORMED BITE TEST OF FASPSU PER 52-73-00-05, OPS CHECK NORMAL. PLACARD REMOVED.

Part: BRAKE — MALFUNCTIONED (MLG)

UPON ARRIVAL, NOTED SMOKE, SPARKS AND SMALL FLAME COMING FROM #4 BRAKE FAN OUTLET W/BRAKE FANS RUNNING. FLAME EXTINGUISHED. FURTHER EVALUATION NOTED MOLTEN METAL LODGED IN THE WHEEL HALF. A/C FERRIED & OOS IN AHM. INSTALLED & REPAIRED RH MLG BOGIE. ALL SYSTEMS CHK GOOD. THIS CLEARS D339118

Part: LAMP — NO TEST (EMERGENCY LIGHT)

EMERGENCY LIGHTS WON'T TEST PROPERLY. RELAMPED 3 BULBS OVER FWD ENTRY DOOR EXIT IT MODULE, TESTED IAW A300-600 AMM 33-51-00-05, NO DEFECTS NOTED. RELAMPED W/SERVICEABLE BULBS.

Part: WARNING BUZZER — INOPERATIVE (ESCAPE SLIDE)

FOUND EMERGENCY EVAC SLIDE, WHEN ARMED, BUZZER IS INOP. PLACED ON DEFERRAL M-332178 PER MEL 52-73-01-2 PLACARD INSTALLED. R&R ESCAPE SLIDE LIMIT SWITCH 13WN IAW A300-AMM 52-73-13-04 AND 52-73-13-05 AND OPS CH'D OK. THIS CLEARS M332178. PLACARD REMOVED.

Part: LIGHT — NO TEST (CABIN)

SUPERNUMERARY EMERGENCY LIGHT TEST FUNCTION AT MAIN ENTRY DOOR INOP. VERIFIED COURIER COMPARTMENT INTERIOR EMERG LIGHT SYSTEM OPERATIVE. DEFERRED "TEST" FUNCTION AT COURIER STATION PER MEL 33-51-05-2.

Part: LAMP — INOPERATIVE (LAVATORY LIGHT)

FOUND LAVATORY AUXILIARY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD. REF M/M 33-51-00-5

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER ENTRY DOOR DIMLY ILLUMINATED. REPLACED 3 BULBS IN EMERGENCY EXIT LIGHT. CHECKS NORMAL.

Part: SCREW — WRONG PART (COCKPIT)

ACCESS FOR EMERGENCY EXIT BELOW COCKPIT HAS FLATHEAD SCREW INSTALLED INSTEAD OF WINGNUT. CREW CAN NOT ACCESS. REMOVED AND REPLACED QUICK RELEASE AND LOCKING PIN PER IPC 53-11-27- 01A

Part: WARNING SYSTEM — INOPERATIVE (ESCAPE SLIDE)

FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE WARNING BUZZER INOP DURING REST, IN ARM POSITION, LIGHT OPERATES NORMAL. PLACED ESCAPE SLIDE BUZZER ON DEFERRAL M-321840 PER MEL 52-73-01-2. PLACARD INSTALLED.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

LAV EMERGENCY EXIT LIGHT INOP, RELAMPED.

Part: WARNING SYSTEM — INOPERATIVE (PAX DOOR SLIDE)

BUZZER DOES NOT SOUND DURING TESTING ENTRY DOOR EMERGENCY ESCAPE SLIDE PLACED BUZZER ON DEF M306464 PER MEL 52-73-01-2 PLACARD INSTALLED. R&R EMER ESCAPE SLIDE TEST SWITCH 39WN. POS CK NORMAL IAW MM 25-61-21-4 THIS CLEARS M306464

Part: WARNING LIGHT — WILL NOT TEST (SLIDE)

SLIDE SYSTEM WARNING LIGHT WILL NOT PRESS TO TEST. LIGHT OP. PERFORMED TEST OF EVACUATION WARNING SYS ON MAIN ENTRY DOOR, OPS CK GOOD. ITEM CLEARED M299091

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY)

BULK CARGO COMP SMOKE LIGHT COMES ON INTERMITTENTLY FOR 2 - 5 SECONDS DURING GROUND OPS, TAXI AND IN-FLIGHT. SYSTEM CHECKED OK IAW TSM 26-16-00.