N653FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
221 reports on file, 1995-12-20 – 2024-02-21.
Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 39,808 hrs · 21,651 cycles
RH ELEVATOR TOP SKIN BROKEN AT ER2 - ER5 INSTALLED THE REPAIR FLIES ON RH ELEVATOR TOP SKIN AT ER2 - ER5 PER A300-600F SRM55--21- 12-201 PARA.5.H & SRM51-77-12-201. MINOR REPAIR IAW FEDEX GMM 6-2-100 ENTERED BY ERROR. THIS REPAIR IS JUST A COSMETIC REPAIR PER A300-600F SRM55-21-12-201. MINOR REPAIR IAW FEDEX GMM 6-2-100
Part: WEB — CRACKED (FRM 47) · airframe 39,808 hrs · 21,651 cycles
MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: WEB — CRACKED (FRM 47) · airframe 39,808 hrs · 21,651 cycles
MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: FLOORBEAM — CRACKED (FRM 30) · airframe 39,808 hrs · 21,651 cycles
MDCC FLOOR CROSSBEAM FR30 CRACKED BETWEEN Y1456 - Y1959 COMPLIED WITH EA 6-5310 -T REPAIRED THE MDCC FLOOR CROSSBEAM FR30 CRACKED. REPAIR WITH MINOR DEVIATIONS. THIS REPAIR IS CAT. A REPAIR , MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: SEAT TRACK — WORN (FRM 63) · airframe 39,808 hrs · 21,651 cycles
MAIN DECK SEAT TRACK Y-2462 WORN AT FR63 REPAIRED THE WORN SEAT TRACK IN MAIN DECK Y-2462 AT FR63 PER A300-600F SRM53-10-16-201 PARA.4.THIS IS ACT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: WEB — CRACKED (FRM 47) · airframe 39,808 hrs · 21,651 cycles
MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: WEB — CRACKED (FRM 47) · airframe 39,808 hrs · 21,651 cycles
MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11,13,15,18,189,25 AND 26 AT STR. 2.6 / 2.7 / 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2- 100.SEE WRI 57-50/FOR WORK DETAILS.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
LH WNG CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11,13,15,18,189,25 AND 26 AT STR. 2.6 / 2.7 / 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57- 50/FOR WORK DETAILS.
Part: RIB — CRACKED (RT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
RT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB13 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 13 AND 21 AT STR. 2.7, RIBS 18 AT STR. 2.8 AND RIB 25 THRU 27 AT STR. 2.7 AND 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57-50/FOR WORK DETAILS.
Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 13 AND 21 AT STR. 2.7, RIBS 18 AT STR. 2.8 AND RIB 25 THRU 27 AT STR. 2.7 AND 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57-50/FOR WORK DETAILS.
Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
RH WING CENTER FLAP RIB UPPER FLANGE FOUND 6EA CRACKED AT RIB25,RIB26,RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25,26,27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 13 AND 21 AT STR. 2.7, RIBS 18 AT STR. 2.8 AND RIB 25 THRU 27 AT STR. 2.7 AND 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57-50/FOR WORK DETAILS.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11,13,15,18,189,25 AND 26 AT STR. 2.6 / 2.7 / 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2- 100.SEE WRI 57-50/FOR WORK DETAILS.
Part: RIB — CRACKED (RT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
RT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACKED AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 13 AND 21 AT STR. 2.7, RIBS 18 AT STR. 2.8 AND RIB 25 THRU 27 AT STR. 2.7 AND 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57-50/FOR WORK DETAILS.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 39,808 hrs · 21,651 cycles
LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11,13,15,18,189,25 AND 26 AT STR. 2.6 / 2.7 / 2.8 - ALT 575306-01-1A. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2- 100.SEE WRI 57-50/FOR WORK DETAILS.
Part: FLOORBEAM — CRACKED (FRM 59) · airframe 39,808 hrs · 21,651 cycles
MDCC FLOOR CROSSBEAM FR59 CRACKED BETWEEN Y-953 ~ Y-1456 REPAIRED THE CRACK IN THE MDCC FLOOR CROSSBEAM FR59 BETWEEN Y-953 ~ Y-1456 PER A300-600F SRM51-40-21 & SRM53-10-15-201 PARA.14. THE REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: CONTROL UNIT — FAILED (FUEL SYSTEM) · airframe 39,762 hrs · 21,632 cycles
ON INITIAL CLIMB OUT RECEIVED TRIM TANK AFT TRANSFER NOT AVAILABLE CAUTION. PASSING 8000 MSL, LEFT ECAM SHOWED AMBER XXX IN GW, CG, AND T. FUEL. RIGHT ECAM SHOWED AMBER XXX IN LEFT INNER AND LEFT OUTER FUEL TANKS, AS WELL AS TOTAL FUEL, GW, AND CG. THE OVERHEAD PANEL WAS ALSO BLANK FOR LEFT INNER AND LEFT OUTER TANKS AND TT. VERIFIED ALL CB WERE SET. FOUND THE PROBLEM TO BE A ELECTRICAL ISSUE WITH THE DC CONTACTOR. REF . WRI 24-40/7525 FOR INFO. WHEN THE AIRCRAFT IS ON APU AND ENGINE POWER WITHOUT THE FAULT ALL SYSTEMS FOR FUEL QTY OPERATE NORMAL. OK FOR SERVICE.
Part: COALESCER BAG — FAILED (N/A) · airframe 39,714 hrs · 21,603 cycles
DURING DESCENT WHEN THROTTLES REDUCED TO IDLE, STRONG BURST OF SMOKE SMELL AND SLIGHT HAZE IN THE COCKPIT. IMMEDIATELY CLEARED AND DID NOT REOCCUR. REMOVED AND REPLACED BOTH COALESCER BAGS IAW A300 AMM 21-51-16-03. ITEM CLOSED. GROUND RUN CARRIED OUT AS PER CHAPTER 6 OF JRH. NO SMOKE SMELL COULD BE DUPLICATED. NO PREVIOUS HISTORY. AIRCRAFT OK FOR SERVICE.
Earlier reports · 1995–2023 · 203 reports
2023
Part: TRANSMITTER — FAULTED (BRAKE PEDAL) · airframe 39,775 hrs · 21,640 cycles
ON LANDING ROLLOUT BRAKING WAS NOT AVAILABLE ON THE RIGHT SIDE FROM EITHER SEAT WITH THE BRAKES IN NORM/ON. SWITCHED BRAKES TO ALTN /ON AND BRAKING WAS RESTORED. PUMPED BRAKES IN NORMAL POSITION ON BOTH CAPT AND FO SIDE. NOTICED BRAKES WERE SLOW AND SPONGY IN MOVEMENT ON BOTH LT AND RT MAIN GEAR. ALSO, NOTICED NO ASSOCIATED BRAKE PRESSURE WHILE PUMPING THE BRAKES IN THE NORMAL POSITION. AFTER SWITCHING TO POSITION ALTERNATE, BRAKES AND BRAKE PRESSURE OPERATED NORMALLY ON BOTH SIDES. PERFORMED BITE CHECK OF THE BSCU PER ABOVE REFERANCE AND FOUND CODE (008) WHICH INDICATES THE BRAKE PEDAL POSITION TRANSMITTER UNIT 11GG. VERIFIED CODE WITH MOC. SUSPECT FAULTY BRAKE PEDAL POSITION TRANSMITTER UNIT 11GG. FURTHER T/S REQUIRED. FOUND DEBRIS IN FO'S BRAKE PEDAL TRANSMITTER CONNECTOR 11GG-A . CLEANED TRANSMITTER AND RECONNECTED. DID A BITE CHECK ON THE BSCU AND HAD NO CURRENT FAULTS. ALSO DID A PRESSURE CHECK ON THE R/H MAIN LANDING GEAR BRAKE SYSTEM IN NORMAL AND IN ALTERNATE. BOTH READ 2500 PSI. WITHIN LIMITS. ALL CHECKS GOOD. A/C OK FOR SERVICE. REFAMM 32-42-00-05
Part: BULB — FAILED (UNKNOWN) · airframe 39,597 hrs · 21,525 cycles
MDIS 653 33-50 6974 23OCT23 GSO FACT U ON 'A' CHECK, EMERG TEST BUTTON ON PANEL 25WL NOT ILLUMINATED. T/S PE ABOVE AMM, FOUND RED FAILURE LIGHT ON POWER SUPPULY UNIT 29WL. INSTALLED NEW BATTERY PER ABOVE AMM, NO RED OR GREEN LIGHT ON POWER UNIT TEST BUTTON. 25WL LIGHT STILL INOP. ORDERING NEW BATTERY & POWER SUPPLY UNIT. AMM: 33-51-00-05 IPC: 33-51-04-09 FOUND INOP EXIT SIGN BULBS AND RELAMPED BULBS IN LH AND RH EXIT DOOR SIGNS REF FDX A300 IPC 33-51-04-09. TESTED EMERGENCY LIGHTS REF A300 AMM 33-51-00-05-00. LIGHTS AND 25WL TEST SWITCH LIGHT OPS CHECK GOOD NUMEROUS TIMES. A/C OK FOR SERVICE.
2022
Part: VALVE — FAULTED (MLG) · airframe 38,495 hrs · 20,841 cycles
ON DEPARTURE WHEN RAISING THE GEAR WE GOT A LANDING GEAR RETRACTION FAULT. WE COMPLIED WITH THE QRH AND RETURN TO SDF FOR LANDING. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE. REMOVED AND REPLACED LANDING GEAR ELECTROVALVE 3GA IAW AMM 32-31-12-04, OPS & LEAK CHECKED GOOD. R & R LANDING GEAR NORMAL CONTROL SWITCH UNIT 2GA UP TO STEP D TEST REQUIRED IAW AMM 32-31-11-04. ALL OPS TESTS NORMAL.
Part: OVERHEAT LOOP — FAILED (ZONE 100) · airframe 38,362 hrs · 20,759 cycles
DURING CLIMBOUT, GOT AN ECAM MESSAGE GREEN RSVR OVHT . COMPLETED THE ECAM AND QRH, OVHT LIGHT INTERMITTENT. CONTINUED FLIGHT. DURING DESCENT, OVHT LIGHT EXTINGUISHED, DECIDED TO RESTORE SYS USING EDP. DECLARED AN EMERGENCY & LANDED WITHOUT ISSUES. IAW MM 29-33-00 INSPECTED CONNECTOR ON OVERHEAT SENSOR & WIGGLED WIRES & FOUND NO FAULTS. RSVR DID NOT APPEAR HOT TO TOUCH. INSPECTED CASE DRAIN FILTER DPI'S ON ENGINE #1 & #2, DID NOT FIND ANY TRIPPED. R & R NR 1 & 2 ENG CASE DRAIN FILTERS IAW MM 29-11-36-03-02. FOUND NO CONTAMINATION. R & R OVERHEAT DETECTOR IAW MM 29-33-12-04. GND OPS CHECKED GOOD IAW MM 29-33-00-05. RAN HYD FUNCTIONAL CHECKS IAW JRH. ALL CHECKED GOOD.
Part: CONTROL UNIT — FAILED (FLT CONTROLS) · airframe 38,019 hrs · 20,538 cycles
AT FL 310, THE AUTOPILOT AND AUTO THROTTLES KICKED OFF. LOST FMAS AND FCP FOR THE REMAINDER OF THE FLIGHT. THE FD WERE NOT WORKING EITHER. REMOVED AND REPLACED FLIGHT CONTROL UNIT (303CA) USING MM 22-15-12-04, PERFORMED AFS/LAND AND LIGHT DISPLAY ALL CHECKED GOOD.
2021
Part: SWITCH — UNKNOWN (ZONE 700) · airframe 37,513 hrs · 20,197 cycles
R1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL : 52-XX-XX CAT : C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE, INSPECTED LIMIT SWITCH 14WN CLEANED AND CHECKED SWITCH CLEARENECE OPS CHECKS GOOD. INSPECTED LIMIT SWITCH 14WN CLEANED AND CHECKED SWITCH CLEARENECE OPS CHECKS GOOD. . MFG P/N NSA932030-02, S/N NOT TRACKED. D) S/N NOT RECORDED TO DUE MOUNTING POSITION, (G UNKN, H) UNKN, I) UNKNOWN INSTALLATION DATE. ITEM CONDITION: ORIGINAL,
Part: SWITCH — UNKNOWN (ZONE 700) · airframe 37,513 hrs · 20,197 cycles
R1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL : 52-XX-XX CAT : C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE, INSPECTED LIMIT SWITCH 14WN CLEANED AND CHECKED SWITCH CLEARENECE OPS CHECKS GOOD. INSPECTED LIMIT SWITCH 14WN CLEANED AND CHECKED SWITCH CLEARENECE OPS CHECKS GOOD. . MFG P/N NSA932030-02, S/N NOT TRACKED. D) S/N NOT RECORDED TO DUE MOUNTING POSITION, (G UNKN, H) UNKN, I) UNKNOWN INSTALLATION DATE. ITEM CONDITION: ORIGINAL,
Part: SKIN — DAMAGED (FRM 57 S43L) · airframe 37,163 hrs · 19,974 cycles
SCRATCHES WERE FOUND AT FR57 10", S41L 0.2" AND FR57 13" TO FR57 18", S43L. ACCOMPLISHED EXTERNAL SKIN DOUBLER REPAIR I.A.W. A300-600F SRM 53-10-12-201 P.265~268 FIG207 SM4.THIS IS CAT B REPAIR I.A.W. A300-600F SRI 53-10-12-201 AND IIR 53-10-12- 2-001-00.
Part: DOUBLER — GOUGED (FRM 20A S38-41R) · airframe 37,163 hrs · 19,974 cycles
DURING PFM WORKCARD:E6-5100-7-5000 D7 PT1, FOUND GOUGE ON THE EXISTING REPAIR DOUBLER SURFACE AND SKIN CUTOUT EDGE AREA AT FR20A BETWEEN S-38R TO S-41R. GENERTAING FROM EO:E6-5100-7-5000 D7 PT1 & WO/NRC:00080535/N00132, ACCOMPLISHED THE WORK I.A.W. E.A:T6-5310-113285 B P3.
Part: FRAME — DAMAGED (FRM 47 S24R) · airframe 37,163 hrs · 19,974 cycles
1EA DAMAGE HOLE WAS FOUND AT FR47, S-24R, SPLICE FITTING, HOLE H AREA I.A.W. EO: 6-5310-7-50170 PART 6 FUSELAGE MAINFRAME - INSPECTION HOLE IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26 LH/RH, AIRBUS SB A300-53-6123( SEQ NO: 001066) PERFORM AND WORK ACCOMPLISHED.
Part: SKIN — DELAMINATED (RUDDER) · airframe 37,163 hrs · 19,974 cycles
1EA WATER TRAPPED AREA (50MMX50MM) WAS FOUND AT RH RUDDER T/E SCREW NEAR NO.37 FASTENER. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 22, FIG. 220, P. 286-294 AND SRI 55-71-12-201, IIR 55-41-12-2-005-00, 3E.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
THE #131NG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,163 hrs · 19,974 cycles
MAIN DECK COMPT FLOOR PANEL #241RJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
THE #132QG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
THE #131RG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
THE #131LG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
AFT CARGO COMPT FLOOR PANEL #151QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,163 hrs · 19,974 cycles
MAIN DECK COMPT FLOOR PANEL #251UH WAS FOUND EDGE DAMAGED.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,163 hrs · 19,974 cycles
THE #131SG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,163 hrs · 19,974 cycles
MAIN DECK COMPT FLOOR PANEL #241PH WAS FOUND INSERT DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
Part: RUDDER — DELAMINATED (ZONE 300) · airframe 37,163 hrs · 19,974 cycles
1EA WATER TRAPPED AREA (90MMX100MM) WAS FOUND AT RH RUDDER HOISTING POINT 2. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 25, FIG. 225A, P. 343-362 AND SRI 55-41-12-201, IIR 55-41-12-2-008-00, 3H.
Part: SERVO VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 36,994 hrs · 19,869 cycles
NR 2 BRAKE DID NOT RELEASE AFTER LANDING ROLLOUT. #2 TEMP REACHED MAX OF 370 DEGREES. PER MOCC THE #2 (13GG) SERVOVALVE IS REQUIRED TO BE CHANGED. REMOVED THE #2 (13GG) SERVOVALVE IAW AMM 32-42-48-04. INSTALLED THE #2 (13GG) SERVO VALVE DOWN TO AMM 32-42-48-04 STEP D (4). SERVO VALVE LEAK CHECK & OPS CHECKED GOOD IAW AMM 32-42-48-04. LT MLG NORMAL BRAKES BLED IAW AMM 32-42-00. LT MLG BRAKES. OK TO CONTINUE SERVICE.
2019
Part: INDICATOR — FAILED (R1 DOOR) · airframe 35,224 hrs · 18,817 cycles
R1 DOOR WILL NOT ARM. . RELEASED FOR SERVICE PER MEL : 52-XX-XX CATEGORY : C EXPIRATION : MM-DD-YY "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR ( R1) _____ DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." VERIFIED DOOR 1 R IS PHYSICLLY ARMED. WHILE BUZZER 12WN. REPLACED TERMINAL REF. A300-600 AWM 52-73-01 AND ESPM 20-48-00 OPS CK GOOD. REF.52-73-14-04-02 AND 52-73-00-05-02 MEL CLEARED
Part: TACHOMETER — MALFUNCTIONED (NR 5 BRAKE) · airframe 35,039 hrs · 18,698 cycles
NR 5 BRAKE INDICATED ON DURING TAXI DRIFTED LEFT. THEN OFF, ATTEMPTED T/O AND HAD SAME INDICATION @80 KTS. CONDUCTED RTO AND RETURNED TO RAMP. TSI 2779 COMPLETED AND PROBLEM CORRECTED IN ASSOCIATED TSI ACTION IAW AMM 32-42-57-00, MAIN TACHOMETER REPLACED. ACFT TAXI CHECK TESTED GOOD. ACFT OK FOR SERVICE.
Part: BRACKET — CHAFED (FRAME 24) · airframe 34,307 hrs · 18,267 cycles
MCD FR24 CHAFFED BETWEEN S-12R AND S-13R REMOVED AND REPLACED 1EA BRACKET AND 1EA SPLICE AT FR24 RH SIDE ON MCD IAW SRM 51-40-21 MAJOR REPAIR
Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 34,307 hrs · 18,267 cycles
FLOOR PANEL 162CF WAS FOUND DAMAGED AFTER REMOVAL FOR FOM 162CF FABRICATED NEW PANEL IAW SRZ-25-005 AND TRAVELER T19/1395152 MAJOR REPAIR
Part: FLOOR PANEL — DELAMINATED (FRAMES 64-65) · airframe 34,307 hrs · 18,267 cycles
PANEL 162DF WAS FOUND DELAMINATED AFTER REMOVAL FOR FOM FABRICATED NEW PANEL 162DF IAW SRZ-25-005 AND TRAVELER T19/1395153 MAJOR REPAIR
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,307 hrs · 18,267 cycles
MAIN SEAT TRACK LBL 1456 WORN AND GOUGED FR57.1 TO FR60. UPON FURTHER INVESTIGATION SEAT TRACK FOUND TO BE CRACKED. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.
Part: ADAPTER — DAMAGED (FRAME 57.3) · airframe 34,307 hrs · 18,267 cycles
MCD ADAPTER FR 57.3 LT HAS DAMAGED LOBE FABRICATED NEW ADAPTER ON T19/1396201. REMOVED AND REPLACED MDCC ADAPTER AT FR57.3 LT IAW SRM 51-40-21, Y1456 TO Y1959 CLASSIFIED AS A CAT"A" MAJOR REPAIR.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 34,307 hrs · 18,267 cycles
MAIN CARGO DECK FR63 RT OUTBD Y-2462 SEAT TRACK LOBE MISSING. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.
Part: CLOSEOUT PANEL — DAMAGED (THRUST REVERSER) · airframe 34,307 hrs · 18,267 cycles
FOUND PANEL PULLED LOSE AND CRACKED ON LT ENGINE, I/B THRUST REVERSER AT APPROX THE 6 O'CLOCK POSITION. REMOVED DAMAGED PANEL ON NR 1 ENG THRUST REVERSER AT 6 O'CLOCK POS REF SRM 51-40-20. PART REPLACEMENT WAS ACCOMPLISHED ON EA 6-530-TO343829 PART 2 WRI 54301885 MRA PART 491B1313137-006, SKIN-LOWER CLOSEOUT.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 18,267 cycles
MAIN DECK BETWEEN FR69 AND FR72 Y-953 SEAT TRACK HAS CORROSION BLEND OUT AREA ON SEAT TRACK AT BETWEEN FR69 TO FR72 Y-953 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK BETWEEN FR69 TO FR72 Y- 953 IAW SRM 53-40-21 MAJOR REPAIR.
Part: SEAT TRACK — WORN (FRAME 78-80) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK FR78 Y0 SEAT TRACK SCALLOPS WORN. BLENDED OUT AREA ON SEAT TRACK SCALLOPS AT FR 78 "Y 0" FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. ACCOMPLISHED REPAIR AT FR 78 "Y 0" IAW SRM 51-40-21 CLASSIFIED AS A CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 34,307 hrs · 18,267 cycles
MDCC 241GF FLOOR PANEL BROKEN. FABRICATED FLOOR PNL 241 GF ON T19/1396619 IAW SRZ-25-005. INSTALLED ON WC 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 34,307 hrs · 18,267 cycles
MDCC 242HF FLOOR PANEL BROKEN. FABRICATED FLOOR PNL 242 HF ON T19/1396617 IAW SRZ-25-005. INSTALLED ON WC 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MDCC 241PJ FLOOR PANEL BROKEN FABRICATED FLOOR PNL 241PJ ON TR #T19/1394762 IAW SRZ-25-005. INSTALLED ON W/C 240- FL-FIT REPAIR CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT 251WH FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 251WH ON TRAVELER T19/1394769 IAW SRZ-25-005. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MDCC FLOOR PANEL 242AJ BROKEN FABRICATED FLOOR PLN 242AJ ON TR # T19/1394766 IAW SRZ 25-005. INSTALLED ON W/C 240- FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT 242XG FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242XG ON TRAVELER T19/1394765 IAW SRZ-25-005. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT 242RJ FLOOR PANEL BROKEN. FABRCIATED FLOOR PANEL 242RJ ON TRAVELER T19/1394767 IAW SRZ-25-005. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242VG BROKEN. FABRIATED FLOOR PANEL 242VG ON TRAVELER T19/1394764 IAW SRZ-25-005. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT 251YG FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 251YG ON TRAVELER T19/1394768 IAW SRZ-25-005. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 34,307 hrs · 18,267 cycles
MAIN DECK CARGO COMPARTMENT 241VJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241VJ ON TRAVELER T19/1394763 IAW SRZ-25-005. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR
2018
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN DECK PANEL Z-230 FLOOR PANEL 231TG MISSING EDGE FILLER AND IS CRUSHED FROM A CARGO LOCK. FABRICATED NEW FLOOR PANEL 231TG IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CABIN CARGO COMPARTMENT Z-231, FLOOR PANEL 231PG HAS MISSING EDGE FILLER AND DELAMINATED. FABRICATED NEW FLOOR PANEL 231PG IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CABIN CARGO COMPARTMENT Z-232, FLOOR PANEL 232VH HAS MISSING EDGE FILLER AND DELAMINATED. FABRICATED NEW FLOOR PANEL 232VH IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CABIN CARGO COMPARTMENT Z-231, FLOOR PANEL 231EF HAS MISSING EDGE FILLER AND DELAMINATED. FABRICATED NEW FLOOR PANEL 231EF IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CABIN CARGO COMPARTMENT Z-231, FLOOR PANEL 231DH HAS MISSING EDGE FILLER AND DELAMINATED. FABRICATED NEW FLOOR PANEL 231DH IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CARGO DECK Z-230, FLOOR PANEL 231GH IS CRUSHED AND DELAMINATED. FABRICATED NEW FLOOR PANEL 231GH IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — CRUSHED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CARGO DECK Z-230, FLOOR PANEL 231YG IS CRUSHED AND HAS PUNCTURE. FABRICATED NEW FLOOR PANEL 231YG IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CARGO DECK Z-230, FLOOR PANEL 232QG HAS A DELAMINATED CORNER. FABRICATED NEW FLOOR PANEL 232QG IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
MAIN CARGO DECK Z-230, FLOOR PANEL 231KG IS DELAMINATED. FABRICATED NEW FLOOR PANEL 231KG IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
COURIER AREA Z-220, FLOOR PANEL 221MF UPPER AFT CORNER IS DELAMINATED. FABRICATED NEW FLOOR PANEL 221MF IAW DWG SRZ 25-005 REV N AND GMM 07-01-1000.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,911 hrs · 18,040 cycles
COURIER AREA Z-220, FLOOR PANEL 222HF UPPER AFT CORNER IS DELAMINATED. FABRICATED NEW FLOOR PANEL 222HF IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.
Part: SEAT TRACK — BROKEN (CABIN) · airframe 32,899 hrs · 17,467 cycles
SEAT TRACK AT FRAME 65 BROKEN. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-10, AMM 53-10-23, AND AMM 25-58-00. OK FOR SERVICE.
2017
Part: COMPUTER — FAILED (NR 2 ENGINE) · airframe 32,687 hrs · 17,345 cycles
AFTER TAKEOFF, THE NR 2 ENGINE LOST POWER, ROLLED BACK. PARAMETERS NOT NOTED. PUSHED THROTTLE BACK UP AND REGAINED POWER. OPERATED NORMALLY. THIS ENGINE TOOK 2 START ATTEMPTS ON PUSHBACK. AUTO THROTTLES ENGAGED ENTIRE FLIGHT. REPLACED THE THRUST CONTROL COMPUTER IAW AMM 22-36-34-04-01 AND PERFORMED SUCCESSFUL AFS, LAND TEST IAW AMM 22-40-00-05. OPS CHECKED GOOD. NO DEFECTS NOTED.
Part: CONTROL UNIT — INOPERATIVE (FLIGHT) · airframe 32,573 hrs · 17,276 cycles
AT ENGINE START, ATS SYSTEM ADVANCED UNCOMMANDED AT THE TIME OF A NR 2 ENGINE ROLLBACK. N2 ATTAINED APPROXIMATELY 87% BEFORE THROTTLES WERE MANUALLY RETARDED. REMOVED AND REPLACED FCU IAW 22-15-XX PERFORMED AFS/LANDS TEST IAW 22-00-XX ,22-40-XX, ALL TESTS PASSED WITHOUT FURTHER OCCURRENCES, REMOVED AND REPLACED SDAC IAW 31-55-XX, ECAM BITE TEST SHOWED SDAC FAULT. SDAC TEST CHECKED GOOD. REMOVED AND REPLACED THRUST CONTROL COMPUTER IAW 22-36-34-04-01 PERFORMED AFS TEST REF 20-40-00-5 AND ALL PASSED WITH NO FURTHER OCCURRENCES, PLACED ACFT COCKPIT CONFIGURATION TO THAT OF FLIGHT CREW PRIOR TO ENG START, PER FLIGHT CREW AUTOTHROTTLE WAS ARMED, RAN NR 2 ENG REF A300 JRH NO FAULTS OCCURRED DURING START, NR 2 ENG RESPONDED NORMALLY, WITH NR 2 ENGINE ROLL BACK AFTER START, PROCEEDED WITH NR 1 ENGINE START TO MIMIC FLIGHT CREW ACTIONS. NR 1 ENG STARTED NORMALLY AND NR 2 ENGINE REMAINED IN GROUND IDLE CONFIGURATION. CYCLED ATS SWITCH TO ARM AND DISARM SEVERAL TIMES NON COMMANDED RESPONSES OCCURRED, NR 1 AND NR 2 ENG SHUTDOWN WAS NORMAL. AFS TESTED GOOD REF 20-40-00-5. ACFT OK TO CONTINUE.
2016
Part: SMOKE DETECTOR — DIRTY (MAIN DECK CARGO) · airframe 31,521 hrs · 16,630 cycles
CARGO FIRE LOOP FAULT DURING TAXI OUT. COMPLIED WITH QRH. SMOKE LIGHT ILLUMINATED. SHUTDOWN ACFT. RAN EVACUATION CHECKLIST. FIRE DEPARTMENT DETECTED NO HOTSPOTS WITH IR. NO ODOR IN COURIER COMPARTMENT. ENGINE RESTART FOR RETURN TO RAMP. THEN RECEIVED A MID 1 LOOP A FAULT. NO SMOKE LIGHT ASSOCIATED. RETURNED TO RAMP. REMOVED AND INSPECTED THE SMOKE DETECTORS. NO EVIDENCE OF DAMAGE OR CONTAMINATION. INSPECTED AIR TUBES FOR SECURITY AND GOOD AIRFLOW. INSPECTED AIR INLET FILTERS. NO OILY FILM FOUND ON ANY OF THE FILTERS OR LINES. FOUND DEBRIS FROM DUST AND LINT ON FILTERS. CLEANED DEBRIS FROM THE FILTERS IAW AMM 26-19-13-06. PERFORMED OPS TEST OF MAIN DECK CARGO SMOKE DETECTION SYS IAW AMM 26-19-00-5.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 31,195 hrs · 16,440 cycles
LEFT INBD AFT FLAP LOWER SURFACE HAS A DENT AT RIB 17. REPAIRED THE FLAP SKIN IAW SRM 57-50-00.
Part: SEAT TRACK — GOUGED (FRAMES 25-26) · airframe 31,195 hrs · 16,440 cycles
GOUGES ON SEAT TRACK SCALLOPS IN MID CARGO COMPT FRAMES 25 TO 26 Y2456. REPAIRED SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201 CAT "A" MAJOR REPAIR
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005
Part: FLOOR PANEL — CRACKED (FWD CABIN) · airframe 31,195 hrs · 16,440 cycles
FWD CABIN FLOOR PANEL 232YG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: SEAT TRACK — CORRODED (FRAMES 73-76) · airframe 31,195 hrs · 16,440 cycles
AFT CABIN BETWEEN FRAMES 73 AND 76 SEAT TRACK Y450 HAD SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 53-10-16. FOUND OUT OF LIMITS FIG 102. REMOVED DAMAGED SECTON OF SEAT TRACK IAW SRM 53-10-16. FABRICATED A NEW SECTION IAW SRM 53-10-16. LOCATED AND DRILLED IAW SRM 53-10-16 AND SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED IAW SRM 53-10-16 AND SRM 51-40-21. MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 31,195 hrs · 16,440 cycles
FWD CARGO FLOOR PANEL 131LG DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 31,195 hrs · 16,440 cycles
FWD CARGO FLOOR PANEL 131KG HAS HOLE AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 31,195 hrs · 16,440 cycles
BULK CARGO FLOOR PANEL 161HF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 231UG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 252UH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: SEAT TRACK — CORRODED (FRAME 50) · airframe 31,195 hrs · 16,440 cycles
SEAT TRACK CORRODED FRAME 50 LBL 60. BLENDED AREA IAW SRM 51-73-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 251BF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 31,195 hrs · 16,440 cycles
MAIN DECK FLOOR PANEL 232TG IS BROKEN AT AFT EDGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 231NG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241BF BROKEN. FABRICATED A NEW FLOOR PANEL8 IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 242RG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241XJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 242BF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ25-005, CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241VG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — DEBONDED (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241TH DEBONDED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 242XJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241AJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 251VF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 31,195 hrs · 16,440 cycles
MAIN CABIN FLOOR PANEL 241DF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — CRACKED (FRAME 54) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 152PF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 58-60) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151XF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 58-60) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 152WF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 56-57) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151TF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 56-57) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151SF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 11-14) · airframe 31,195 hrs · 16,440 cycles
COURIER FLOOR PANEL 221LF HAS AN EIGHT INCH CRACK ON BOTTOM SIDE OF THE PANEL. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.
Part: FLOOR PANEL — CRACKED (FRAMES 57-58) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151UF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FRAMES 11-14) · airframe 31,195 hrs · 16,440 cycles
COURIER FLOOR PANEL 221MF DENTED, PUNCTURED, AND DAMAGED INSERTS. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.
Part: FLOOR PANEL — CRACKED (FRAMES 58-60) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151WF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 57-58) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 152UF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAMES 57-58) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151VF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FRAME 54) · airframe 31,195 hrs · 16,440 cycles
AFT CARGO FLOOR PANEL 151MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FRAMES 15-19) · airframe 31,195 hrs · 16,440 cycles
COURIER FLOOR PANEL 221GF HAS MULTIPLE PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.
Part: INDICATION SYS — MALFUNCTIONED (R1 DOOR) · airframe 31,014 hrs · 16,322 cycles
R1 DOOR WOULD NOT ARM, NO SLIDE INDICATION ON ECAM. RELEASED FOR SERVICE IAW MEL 52-30-04, CATEGORY C, EXPIRATION 28JUN16, MEL 52-30-04, ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. DEFERRED IAW MEL 52-30-04. DESCRIPTION IS PUT IN WORK, R/I 18JUN16 13:54. PREMATURE REMOVAL/INSTALLATION. OFF MPN: AD-3214-30, POS: 2, SRL: 58254, TAG: 2743E4 ON MPN: AD-3214-30, CPN: 3310373, SRL: 51625, TAG: 0213C0 FACT 18JUN16, UNABLE TO DUPLICATE AT MDT. AS PRECAUTION, R & R BATTERY ON ASPSU IAW MM 52-73-18-04. TESTED IAW MM 52-73-00-05-02. OPS CHECK GOOD. CLEARS MEL ITEM.
Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 30,727 hrs · 16,157 cycles
YELLOW HYD PUMP LOW PRESS. WHEN ACFT RETURNED TO GATE ALL HYD INDICATIONS WERE NORMAL & THE HYD QUANTITIES WERE AT NORMAL LEVELS. PERFORMED A GND ENG RUN TO SEE IF THE FAULT WOULD RETURN. AFTER ENG START & OPERATION OF THE FLIGHT CONTROLS, THE FAULT RETURNED. THEY GOT A YELLOW PUMP LOW PRESS & YELLOW SYS LOW PRESS ECAM MSG ALONG WITH AN OVERHEAD ENG YELLOW PUMP, LO PR LIGHT, A YELLOW SYS SERVO CTL, LO PR, LIGHT AS WELL AS A SPOILER FAULTS FOR THE YELLOW SYS. AFTER ENG SHUTDOWN WE FOUND THE OVERHEAD YELLOW ENG PUMP, LO PR, LIGHT WAS NOT ILLUMINATED WITH NO PRESS ON SYS. R & R NR 2 ENG DRIVEN YELLOW SYS HYD PUMP IAW MM 29-11-32-04-02. OK FOR SERVICE IAW MM 29-11-32-04-02.
Part: POWER SUPPLY — MALFUNCTIONED (L1 DOOR) · airframe 30,711 hrs · 16,150 cycles
L1 ESCAPE SLIDE LIGHTS WILL NOT ILLUMINATE WHEN PRESS TO TEST BUTTON IS ENGAGED. BUZZERS ARE OK. RELEASED FOR SERVICE IAW MEL 52-73-01-01 CATEGORY C, EXPIRATION 10 APR 16 MEL 52-73-01-01. R1 & L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYS LIGHTS INOPERATIVE. R1 & L1 ENTRY DOOR ESCAPE SLIDE WARNING SYS LIGHTS INOPERATIVE. PULLED AND RESET AUTONOMOUS STANDBY POWER SUPPLY UNIT C/B PERFORMED BITE TEST PER 52-73-00 BITE CK PASSES, CHECKED L1 & R1 DOOR SLIDE WARNING LIGHTS OPS CKS GOOD CLEARED DEFERRAL. A/C OK FOR SERVICE.
Part: GENERATOR — FAULTED (NR 2) · airframe 30,533 hrs · 16,056 cycles
TAKEOFF ABORTED AT 80 KIAS DUE TO GENERATOR NR 2 FAULT. GEN 2 RESET NORMALLY IAW QRH. PER CREW DEBRIEF NR 2 GENERATOR RESET WITHOUT ANY FURTHER ISSUES, NO FURTHER ISSUES DURING FLIGHT, ACFT OK TO CONTINUE.
2015
Part: RIB — CORRODED (RT WING) · airframe 293 hrs · 15,422 cycles
OPEN R MOD TYPE T MOD NR 6-5710-T0316275 REV NR PS P1 WINGS, BASIC WING STRUCTURE, TERMINATING ACTION OF RIB 5 FWD LUG RT COMPLY WITH EA 6-5710-T0316275 REV NR POS P1. COMPLIED WITH EA 6-5710-T0316275 P1 WINGS BASIC WING STRUCTURE & TERMINATING ACTION OF RIB 5 FWD LUG RT.
2014
Part: LUG — CORRODED (LT WING) · corrosion level 2 · airframe 28,779 hrs · 15,079 cycles
LEFT RIB 5 MLG LUG FWD HAS CORROSION IN BORE, FWD & AFT FACE. REPAIRED IAW DWG R57240425 REV D & COMPLIED WITH EA 6-5710-T0311784 REV A PART 5.
Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 28,715 hrs · 15,039 cycles
DURING CRUISE ALTITUDE 35000, LT MAIN CARGO DOOR UNLOCK INDICATION CAME ON NO DISCERNABLE CHANGE IN CABIN PRESSURE, LIGHT REMAINED ON UNTIL 200 FL. DURING TROUBLESHOOTING WITH MAIN CARGO DOOR CLOSED & LOCKED FOUND DOOR WARNING SWITCH 49WS ADJUSTMENT AT MINIMAL CONTACT AT LOCKED POSITION. USED SHIMS, MULTIMETER & ACFT INDICATIONS, ADJUSTED 49WS SWITCH IAW AMM. OPS CHECKED NUMEROUS TIMES WITH NO FAULTS.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
ACFT COMPARTMENT FRAME 45, STRINGER 37 RT FRAME BASE FITTING FOUND CRACK 0.44 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5. THE JOB WAS ACCOMPLISHD, MAJOR REPAIR IAW FEDEX GMM 6-2-100
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
ACFT COMPARTMENT FRAME 46, STRINGER 37 RT FRAME BASE FITTING FOUND CRACK 0.48 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5. THE JOB WAS ACCOMPLISHD. MAJOR REPAIR IAW FEDEX GMM 6-2-100
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
ACFT COMPARTMENT FRAME 46, STRINGER 37 LT FRAME BASE FITTING FOUND CRACK 0.43 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5 , THE JOB WAS ACCOMPLISHD, MAJOR REPAIR IAW FEDEX GMM 6-2-100
Part: SPLICE — CRACKED (ZONE 100) · airframe 28,541 hrs · 14,930 cycles
JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT FRAME 44. FOUND TWO CRACK SIGNALS. REPAIRD IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
Part: SPLICE — CRACKED (ZONE 100) · airframe 28,541 hrs · 14,930 cycles
JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT 7 INCHES IN FRONT OF FRAME 44 STIFFENER LOCATION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE T FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE C FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE S FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0307901 P1 EA TITLE, WINGS BASIC WING STRUCTURE AD2005-23-08--CRACK HOLES AT FRAME 47-SB57-6086 EMBODIMENT. REPAIRED THE FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE S. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE G FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: SPAR — CRACKED (WING) · airframe 28,541 hrs · 14,930 cycles
FUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.
Part: FRAME — CRACKED (ZONE 100) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — CRACKED (ZONE 100) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — CRACKED (ZONE 100) · airframe 28,541 hrs · 14,930 cycles
FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
Part: COMPUTER — FAULTED (SLAT SYSTEM) · airframe 28,146 hrs · 14,733 cycles
AT TAKEOFF CAPTAIN RECEIVED A FLASHING, SPD LIM, WARNING ON PFD NEXT TO SPEED TAPE. ALL SPEED LIMIT INFO WAS LOST ON CAPTAIN'S PFD. UPON RETRACTING SLATS, RECEIVED SLATS SYS 1 FAULT. CYCLED SLATS IAW QRH BUT FAULT REMAINED, REPEAT WU. SFCC NR 1 FAULTED, SFCC NR 2 FAULTED. LT RETRACT SWITCH ALSO CHECKED SLAT TORQUE LIMITERS, NEITHER TRIPPED. WILL CONTINUE TO TROUBLE SHOT. FOUND NR 2 SFCC UNIT FAULTED. R & R NR 2 DUE TO FAULT & NR 1 SFCC PRECAUTIONARY IAW AMM A300 27-51-18. OPERATIONS CHECKED GOOD. .
2012
Part: POWER SUPPLY — INOPERATIVE (ESCAPE SLIDE) · airframe 26,667 hrs · 13,914 cycles
ON PREFLIGHT, FOUND R1 ESCAPE SLIDE WARNING LIGHT INOPERATIVE. REMOVED AND REPLACED AUTONOMOUS AS PER AMM 52-73-18-04, SLIDE CHECKED GOOD.
Part: SPRING — BROKEN (UPLOCK HOOK) · airframe 26,574 hrs · 13,869 cycles
DURING GEAR RETRACTION THREE GEAR UP & LOCKED INDICATIONS, BUT UNSAFE NOSE GEAR DOOR SYS 1 AND 2. COMPLIED WITH QRH GEAR DOWN AND LOCKED, NOSE DOOR REMAINED AMBER. AIR TURNBACK WITH UNEVENTFUL LANDING AND ROLLOUT. FOUND BOTH SPRINGS FROM LT UPLOCK HOOK BROKEN. ON RT UPLOCK HOOK ALSO ONE SPRING BROKEN.
Part: UPLOCK — FAILED (NLG DOOR) · airframe 26,574 hrs · 13,868 cycles
DURING GEAR RETRACTION, THREE GEAR UP & LOCKED INDICATIONS. UNSAFE NLG DOOR SYS 1 AND 2. COMPLIED WITH QRH GEAR DOWN AND LOCKED, NOSE DOOR REMAINED AMBER. RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING AND ROLLOUT. INSTALLED LT NLG DOOR UPLOCK ASSEMBLY IAW MM 32-31-14-04.
2011
Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 25,454 hrs · 13,222 cycles
LT WING INBD T/E FLAP LOWER SURFACE AT RIB 12, REAR SPAR, MISREPAIRED. CARRIED OUT REPAIR IAW EA 6-5750-155851.
Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 25,454 hrs · 13,222 cycles
LEFT WING INBD T/E FLAP LOWER SURFACE AT RIB 17 REAR SPAR, MISREPAIRED. CARRIED OUT REPAIR IAW EA 6-5750-155851.
Part: BRACKET — CHAFED (NR 2 NACELLE) · airframe 25,454 hrs · 13,222 cycles
CASE DRAIN LINE LOOSE AND CHAFING AT NR 2 PYLON AFT END AT LOWER WING SKIN FEED THRU HOLE (AFT WING JACK PAD POINT). REPAIR ACCOMPLISHED IAW EA 6-5410-155854. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FRAME 28 RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FRAME 29, RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FRAME 30, RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: SPLICE — DENTED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK CARGO RT FRAME 22 AT L8-9R BRACKET SPLICE FOUND DENTED. DENTED BRACKET REMOVED AS PER SRM 51-40-21 REVISION 21. FABRICATED AS PER DWG A5377090321000 ISSUE "E" AND INSTALLED AS PER SRM 51-40-21 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: SPLICE — DENTED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK CARGO RT FR 23 AT L8-9 BRACKET SPLICE FOUND DENTED. DENTED BRACKET SPLICE REMOVED AS PER SRM 51-40-21 REVISION 21. FABRICATED AS PER DRAWING A5377090320800 ISSUE "E" AND INSTALLED AS PER SRM 51-40-21 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FITTING — DAMAGED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
FOUND EXTERNAL COUPLING DAMAGED. CARRIED OUT REPAIR IAW EA 6-5310-155852, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: CROSSBEAM — MISREPAIRED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
CROSSBEAM MISREPAIRED AT FRAME 66 APPROX Y=960. REPAIRED IAW SRM 53-10-15, FIG 211, REV 21 AND EO E6-5100-7-5000D PT1.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132LG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132SG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 131PG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132NG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: SKIN — CRACKED (RT WING) · airframe 25,454 hrs · 13,222 cycles
RIGHT WING L/E PANEL NR 613AB CUT-OUT FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 53-15-63, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 4.5 INCHES FROM FRAME 1 AND 10.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT IAW SRM 51-40-41 REVISION 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH A LIGHTNING STRIKE APPROX.4.5 INCHES FROM FRAME 1 AND 10.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT IAW SRM 51-40-41, REVISION 2. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 1.75 INCHES FROM FRAME 1 AND 10.0 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT ON FASTENER HOLE IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE FROM FRAME 1 AND 9.0 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE. REPAIR CARRIED OUT IAW SRM 51-40-41 REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: SKIN — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
LOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 2.75 INCHES FROM FRAME 0 AND 8.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 25,454 hrs · 13,222 cycles
AFT CARGO BAY FLOOR PANEL NR 152XF FOUND DAMAGED. R & R IAW AMM 53-10-33-04, REV 52.1. FLOOR PANEL FABRICATED IAW DG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 25,454 hrs · 13,222 cycles
AFT CARGO BAY FLOOR PANEL NR 152WF FOUND DAMAGED. R & R IAW AMM 53-10-33-04 REV 52.1. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,454 hrs · 13,222 cycles
CARGO BAY FLOOR PANEL NR 162EF FOUND LOWER SURFACE CORRODED. R & R IAW AMM 53-10-35-04, REV 52.1. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 5 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.020IN). REPAIR CARRIED OUT IAW 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 113.
Part: ATTACH FITTING — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 2 LT AT FR 54 TO FR 54.2. FOUND WORN AND OUT OF GAP VALUE (0.031INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
FOUND AT MAIN DECK FLOORBEAM AT FR 30 APPROX - Y = 700 CRACKED. CARRIED OUT REPAIR IAW EA NR 6-5310-155850 & EO E6-5100-7-5000D-PT1 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.
Part: ATTACH FITTING — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 3 RT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.022IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG 201 REV.21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 3 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.019IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: ATTACH FITTING — WORN (SEAT TRACK) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACH FITTING NR 5 LT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.023IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FR 32, LBL 67 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, FIG 212, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: ATTACH FITTING — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 5 RT AT FR 38.2 TO FR 40. FOUND WORN AND OUT OF GAP VALUE (0.022 INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FR 67, LBL 63 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG 211 REV 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FRAME — DAMAGED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
AFTER THE REMOVAL OF REPAIR SPLICE AT FRAME 23 L8-9, FOUND UNDERLYING STRUCTURE DAMAGE. DAMAGED FRAME REMOVED IAW SRM 51-40-21, REV 21. FABRICATED IAW DWG A53770911200 ISSUE B AND INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSFIED MAJOR IAW GMM 6-2-100, REV 113.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 6 RT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.032IN). REPAIR CARRIED OUT IAW 53-15-16 FIG 201, REV 21 REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 2 RT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.026IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
FOUND AT MAIN DECK FLOORBEAM AT FR 28 APPROX - Y= 700 CRACKED. CARRIED OUT REPAIR IAW EA 6-5310-155850& EO 6-5100-7-5000D-PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK CARGO TRACK CROWN AREA AT FR66, Y = 17.5 FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-16, FIG 201, REV 21 BETWEEN FRAME 65.6 TO FRAME 67.5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
FOUND MAIN DECK FLOORBEAM AT FRAME 29 APPROX Y=700 CRACKED. CARRIED OUT REPAIR IAW EA 6-5310-155850 & EO E6-5100-7-5000D-PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 4 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.027IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: ATTACH FITTING — WORN (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 2, RT AT FR 38.2 TO FR 40 FOUND WORN AND OUT OF GAP VALUE (0.020 INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
MAIN DECK FLOORBEAM AT FR64, RBL 65 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG.211 REV21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: ATTACH FITTING — WORN (SEAT TRACK) · airframe 25,454 hrs · 13,222 cycles
SEAT AND DUMMY TRACK ATTACH FITTING NR 6 LT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.020IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG. 201 REV. 21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.
Part: FRAME — DAMAGED (ZONE 200) · airframe 25,454 hrs · 13,222 cycles
AFTER THE REMOVAL OF REPAIR SPLICE AT RT FRAME 22 L8-9, FOUND UNDERLYING STRUCTURAL DAMAGE. DAMAGED FRAME REMOVED IAW SRM 51-40-21, REV 21. FABRICATED IAW DWG A5377169420300, ISSUE B AND INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSFIED MAJOR IAW GMM 6-2-100 REV 113.
Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 25,454 hrs · 13,222 cycles
LEFT INBD FLAP, 5 INCHES FROM INBD EDGE FOUND LOWER SURFACE DRAIN HOLE ELONGATED. CARRIED OUT REPAIR IAW EA NR 6- 5750-155851, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
Part: BATTERY — DISCHARGED (SLIDE LIGHT) · airframe 25,358 hrs · 13,173 cycles
R1 DOOR NO ECAM SLIDE LIGHT WHEN DOOR IS ARMED. R & R ASPSU BATTERY'S 1 AND 2 REF AMM 52-73-18-04. SYS TEST'S GOOD. ACFT OK FOR SERVICE. R & R ASPSU BATTERY'S 1 AND 2 REF AMM 52-73-18-04. SYS TEST'S GOOD. ACFT OK FOR SERVICE. FINAL CLOSED.
Part: CYLINDER — GOUGED (LT MLG) · airframe 25,240 hrs · 13,097 cycles
LT MLG ACTUATING CYLINDER GOUGED ON UPPER BODY. REMOVED LT MLG ACTUATING CYLINDER AND INSTALLED SERVICEABLE CYLINDER PN C23129004-4 ON 32T0007.
Part: LIGHT — NO TEST (CABIN) · airframe 25,175 hrs · 13,068 cycles
DURING SERVICE CHECK EMERGENCY LIGHTS DID NOT TEST PROPERLY FROM SWITCH AT DOOR 1L. RED LIGHT ON POWER SUPPLY UNIT ILLUMINATED WHEN TEST BUTTON PUSHED. COMPLIED WITH EPSU OPS CHECK IAW MM 33-50-00-00. OPS CHECKED OK. NO FAULTS NOTED. GREEN LIGHT ILLUMINATED AND RED LIGHT STAYED OUT. OK FOR SERVICE.
Part: TIRE — FAILED (MLG) · airframe 24,989 hrs · 12,976 cycles
NR 4 TIRE BLEW ON LANDING, REPLACED TIRE.
Part: COALESCER BAG — ODOR · airframe 24,813 hrs · 12,881 cycles
AFTER LANDING AT APPROX 60KTS, GOT A SMOKE INDICATIONS IN THE EQUIPMENT BAY FOLLOWED BY MAIN DECK SMOKE INDICATIONS. THERE WAS SMOKE IN THE COCKPIT. R & R NR 1 AND NR 2 PACK COALESCER SOCKS IAW MM 21-51-16-03. R & R AVIONICS COOLING FILTER IAW MM 21-21-16-04.
2009
Part: WEB — CRACKED (NR 1 SLAT) · airframe 22,540 hrs · 11,648 cycles
RT WING NR 1 SLAT VERTICAL WEB AT RIB 24 HAS A 0.30 INCH CRACK. REMOVED DAMAGED VERTICAL WEB, FABRICATED REPLACEMENT WEB AND INSTALLED ON NR 1 SLAT RIB 24 IAW DWG A57863063 AND A300-600 SRM 57-42-11 AND SRM 51-72-10.
Part: DUCT — CONTAMINATED (BLEED SYSTEM) · airframe 22,305 hrs · 11,526 cycles
SMOKE IN COCKPIT ON GROUND AFTER AIR COND PACK TURNED ON. ACFT RELEASED FOR SERVICE PER MEL/CDL: 49-10-01. SMOKE WAS NOTED DURING FIRST PACK OPERATION FOLLOWING COMPRESSOR WASH OF THE NR 2 ENGINE, SUSPECT WATER FROM WASH IN BLEED DUCT. OPERATED APU PER JRH 3-2 WITH NO FAULTS NOTED.
Part: UNKNOWN — ODOR (CABIN) · airframe 21,949 hrs · 11,323 cycles
ON FINAL 1500' AGL, MASTER CAUTION EQUIP BAY SMOKE INDICATION. DECLARED EMERGENCY RAN ECAM & LANDED. INDICATION WENT AWAY SHORTLY INTO PROCEDURE & NO SMOKE SEEN OR SMELLED. INSPECTED E/E BAY & NO EVIDENCE OF SMOKE OR FUMES. 12WA REPLACED. FOUND NO EVIDENCE OF MOISTURE FROM OVERHEAD IN E/E BAY. AFTER ENG RUN, NOTICED STRONG OIL ODOR IN CABIN & COCKPIT, CHANGED COALESCER SOCKS PER MM 21-51-16-3. RAN ENGINES PER JRH AGAIN & ODOR CLEARED. ODOR PRESENT AGAIN AFTER APU BLEED OPENED. CLOSED APU BLEED & CONTINUED ENG RUN TO CLEAR DUCTS. AVIONICS SMOKE DETECTOR REPLACED, RAN ENGS WITH PACKS ON FOR APPROX. 20 MIN. NO SMOKE ALERTS OR ODOR . OK FOR SERVICE.
2007
Part: SPAR — CRACKED (LT WING) · airframe 19,854 hrs · 10,212 cycles
A 1.5 INCH CRACK EXIST AT LT WING REAR SPAR BETWEEN RIBS 8/9 ACCESS PROVISIONS THROUGH PNL 575FB REF 57-00-00-6 ZONE 500. INSTALLED S/B NR A300-57-6064 DOUBLERS AT RIB NR 9 AFT OF REAR SPAR (REINFORCEMENT DOUBLERS) COMPLIED WITH EA 6-5730-110509.
Part: SKIN — CRACKED (ZONE 600) · airframe 19,854 hrs · 10,212 cycles
RT WING LOWER SKIN CRACKED AT T/E ACCESS PANEL 675FB CUTOUT. FORWARD O/B CORNER AREA TOTAL CRACKED LENGTH 1.25 APPROX REF A300-600 SRM 51-10-00. COMPLIED WITH EA 6-5730-110509 REF SB'S A300-600 57-6064 AND 57-6029 DWG R57340199, SMALL REPAIR PLATE.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,854 hrs · 10,212 cycles
SEAT TRACK 2R AT FR 78 AND FR75 HAS 1 SQ IN OF CORROSION EACH ZONE 260 REF A300-600 SRM 51-10-00. REMOVED CORRODED FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 201. INSTALLED NEW REPAIR SECTION OF SEAT TRACK AND SPLICE IAW A300-600 SRM 53-10-16 FIG 201.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
MDCC AT FR22 BETWEEN STG 9R AND 8R HAS 1 EA GOUGE APPROX 1" ZONE 230 REF A300-600 SRM 51-10-00. REMOVED DAMAGE FRAME SPLICE PER A300-600 SRM 51-40-21. CUT OUT CRACKED FRAME INNER FLANGE AND INSTALLED REPAIR SPLICE PER FEDEX EA 6-5310-110521.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
LATE FIND FLOORBEAM FR 30 BETWEEN SEAT TRACK NR 2L AND 3L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT DAMAGED SECTION OF FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRAICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A300-600 FREIGHTER SRM 53-10-15. ALODINED ALL PARTS IAW A300 SRM 51-21-10. PRIMED ALL PARTS IAW A300 SRM 51-75-10. TOPCOATED REPAIR IAW A300 SRM 51-75-10.
Part: FRAME — GOUGED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
MDCC AT FR 22 BETWEEN STG 17R AND STG 9R HAS 7 GOUGES APPROX 4" ZONE 230 REF A300-600 SRM 51-10-00. BLENDED 7 GOUGES FR 22 BETWEEN STR 7 AND 17R IAW A300-600 SRM 51-73-10 1EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.063 A=.046 L=.017. FABRICATED AND INSTALLED FRAME REPAIR IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202. ALODINED IAW A300 SRM 51-21-10. PRIMED AREA IAW A300 SRM 51-75-10.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
FUSELAGE MAIN DECK SEAT TRACK 5L I/B FLANG PANEL LANDING HAS WEAK AROUND 7 EA FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300-600 SRM 51-10-00. BLENDED 7 AREAS AT LT 5L FR47-51 IAW A300-600 SRM 51-73-10. AFTER REWORK ALL 7 AREAS WERE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW A300-600 SRM 51-72-10, 51-40-21 AND DWG A538-12915.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
FUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 7 FASTENER HOLES BETWEEN FRAMES 43-47. REF A300-600 SRM 51-10-00 TOTAL AREA GOUGED 7 INCH APPROX BY 0.010 DEEP. BLENDED GOUGES IAW A300-600 SRM 51-73-10. SEAT TRACK OUT OF LIMITS IAW A300-600 SRM 53-10-16. FABRICATED NEW SEAT TRACK IAW AIRBUS DWG A53832020. ALODINED NEW SEAT TRACK IAW A300 SRM 51-21-10. PRIMED TRACK IAW A300 SRM 51-75-10. TOP COATED TRACK IAW A300 SRM 51-75-10. INSTALLED TRACK IAW A300 SRM 51-72-10.
Part: FRAME — DENTED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
FWD CARGO DOOR CUT-OUT STRUCTURE FR 20 HAS INCOMING CONDITION IMPACT DENT ON FRAME W/APPROX SIZE 4-IN LONG BY 2-IN WIDTH BY 0.25 DEPTH. (REF A300-600 AMM 53-13-11-6) SRM 53-10-13. CUT OUT DAMAGED SECTION AND DRILLED UP, REPAIR SECTION AND INSTALLED IAW FEDEX DRAWING SR30-53-001.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
FLOORBEAM FRAME 31 BETWEEN SEAT TRACKS NR L4 AND NR 5L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT CRACKED SECTION OF FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A 300-600 FREIGHTER SRM 53-10-15. ALODINED FLOORBEAM, REPAIR ANGLE AND FILLER IAW A300-SRM 51-21-10. PRIMED ALL PARTS IAW A300 SRM 51-75-10. TOPCOATED REPAIR IAW A300 SRM 51-75-10.
Part: ANGLE — GOUGED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
MDCC AT FR 24 BETWEEN STG 11R AND 15R HAS 4 EA GOUGES APPROX 4 " ZONE 230 REF A300- 600 SRM 51-10-00. BLENDED GOUGES (4EA) FR 24 BETWEEN STR 11R AND 15R IAW A300 SRM 51-73-10 1 EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.63 A=0.50 L= .013. FABRICATED REPAIR ANGLE IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202. ALODINED REPAIR IAW A300 SRM 51-21-10. PRIMED REPAIR IAW A300 SRM 51-75-10. INSTALLED REPAIR IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,854 hrs · 10,212 cycles
FWD CARGO COMPT CEILING, CABIN FLOORBEAM C-27 HAS A CRACK ON FWD FACE VERTICAL FORMED SECTION, BETWEEN RT SEAT TRACK 2-3 WITH APPROX 0.25 IN LONG REF A300-600 SRM 51-10-10. CLEAN OUT CRACK IN FLOORBEAM IAW A300-600 SRM 53-10-15. FAB`D REPAIR ANGLE AND FILLER IAW A300-600 SRM 51-10-15. ALODINE PARTS IAW A300-600 SRM 51-53-00. PRIME IAW A300-600 SRM 51-23-00. TOPCOAT IAW A300-600 SRM 51-23-00. INSTALLED REPAIR PART IAW A300-600 SRM 51-10-15 FIG 212.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,854 hrs · 10,212 cycles
COURIER AREA FR 16A- FR 18 SEAT TRACK 3L 20 SQ IN CORROSION REF A300-600 AMM 53-12-00-6 ZONE 230. REMOVED CORROSION ON L3 SEAT TRACK. WENT OUT OF LIMITS IAW A300-600 SRM 53-10-16. REPAIR SEAT TRACK IAW A300-600 SRM 53-12-16. PRIMED AND TREATED PARTS IAW A300-600 SRM 51-75-10. INSTALLED REPAIR IAW A300-600 SRM 53-12-16 FIG 201.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 19,854 hrs · 10,212 cycles
FUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 6 FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300-600 SRM 51-10-00 TOTAL AREA GOUGED 6 INCHES APPROX. BY .010 DEEP. BLENDED DAMAGE PER A300-600 SRM 51-73-10 AND FOUND TO BE OUT OF LIMITS PER A300-600 SRM 53-10-16 PB 101. REMOVED DAMAGED SEAT TRACK SECTION PER A300-600 SRM 51-72-10. FABRICATED NEW SEAT TRACK SECTION PER A300-600 SRM 53-15-16 AND DRAWING A53812915. ALODINED, PRIMED AND TOP COATED SEAT TRACK SECTION PER A300-600 SRM 51-21-10 AND 51-75-10. INSTALLED SEAT TRACK SECTION ASSY PER A300-600 SRM 51-72-10.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,854 hrs · 10,212 cycles
MDCC SEAT TRACK L5 FR 19-FR 24 18 SQ IN CORROSION INBOARD FLANGE IN AND AROUND FASTENER HOLES REF A300-600 AMM 53-13-11-6 ZONE 230. CLEAN CORROSION IAW A300-600 SRM 51-74-10. CHECK LIMITS PER A300-600 SRM 53-10-16 OUT OF LIMITS. FAB REPAIR PART PER A300-600 SRM 53-10-16 FIG 202. ALODINE, PRIME, AND TOPCOAT PARTS PER A300-600 SRM 51-35-00 AND 51-21-10. INSTALLED REPAIR IAW A300-600 SRM 53-10-16 FIG 202.
2006
Part: PITOT TUBE — FAILED · airframe 18,947 hrs · 9,702 cycles
RTO NO F/O AIRSPEED ON PFD. A/C RETURNED TO BLOCKS DUE TO NO AIRSPEED INDICATION ON F/O'S PFD. BLEW OUT PITOT TUBE FOR F/O AIRSPEED PER MM 34-11-15-6, NO DEFECTS NOTED. USED PITOT TESTER TO VERIFIY SPEED TAPE ON FO,S PFD OPERATED NORMALLY PER MM 34-11-15-6. REMOVED AND REPLACED F/O'S PITOT TUBE AND PERFORMED LEAK CHECK, AMM 34- 11-15-4. OPS CKS NORMAL. ALSO, SWAPPED NR 1 AND NR 2 AIR DATA COMPUTERS AS PRECAUTION. A/C OK FOR SERVICE.
2005
Part: BATTERY — FAILED (CABIN) · airframe 16,530 hrs · 8,456 cycles
EMERGENCY LIGHT POWER SUPPLY FAILED TEST PER 33-51-14 (NR#N0060, W/O NR 28630). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-14 TEST OF EMERGENCY LIGHTS GOOD IAW MM 33-51-14 (NR#N0060, W/O#28630)
Part: ACOUSTIC PANEL — DENTED (NR 1 INTAKE) · airframe 16,530 hrs · 8,456 cycles
COMPLY WITH EA 6-7110-55485 POWER PLANT-INLET COWL NR 1 ENGINE ACOUSTIC PANEL DENT REPAIR. REPAIRED AREA PER EA 6-7110-55485.
Part: SHROUD — CRACKED (ZONE 500) · airframe 16,530 hrs · 8,456 cycles
PYLON NR 1 SHROUD/PAN, UNDER THE ENGINE BLEED AIR DUCT, IS CRACKED. VIEWED THRU ACCESS PANEL 413EL. REMOVED CRACKED SHROUD, FAB NEW SHROUD ON TR T5/517007 301-25 .025SS BATCH 0000887337, INSTALLED SHROUD IAW SRM 51-4-21.
Part: CONTROL PANEL — MALFUNCTIONED (SPOILERS) · airframe 16,386 hrs · 8,374 cycles
WHEN SPEED BRAKES WERE DEPLOYED, ALL SPOILERS DEPLOYED EXCEPT NR 6 AND NR 7 ON THE RIGHT WING THIS CAUSED A WING ROCK THAT IN TURNED CAUSED THE PLANE TO START A 10 DEGREE BANK. FOUND LT NR 5 SPOILER ONLY ATTACHED AT ACT CONNECTION. REPLACED SPOILER PANEL, DAMAGE TO WING AT NR 5 SPOILER PERFORMED A THOROUGH VISUAL INSPECTION OF REAR SPA DEFERRED UNTIL COMPLIANCE WITH E.A. 6-5730-87052 ON LT NR 5 SPOILER, AND EA 6-5750-87053 ON RT NR 5 SPOILER. REPAIRED DAMAGE TO WING SKIN INBD/OTBD OF NR 5 LT IAW
Part: IDG — FAILED (NR 2 GENERATOR) · airframe 16,119 hrs · 8,218 cycles
ON INITIAL T/O ROLL NR 2 GEN FAULTED. T/O WAS REJECTED AT 70 KTS ESTIMATED. GENERATOR WAS RESET, VOLTS AND FREQS APPEARED NORMAL. SECOND T/O WAS ATTEMPTED GENERATOR FAILED AGAIN ON INITIAL T/O ROLL, IDG 2 FAULT LIGHT WAS FLUCUATING ON AND OFF. RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 10JAN05.
2004
Part: THRUST REVERSER — MALFUNCTIONED (NR 1 ENGINE) · airframe 16,050 hrs · 8,183 cycles
ON TAKEOFF RWY 6 KBDL- NR 1 ENGINE REV PRESSURIZED LIGHT CAME ON AT 70 KNOTS, ENGINE N1 APPROX 75 PERCENT. REJECTED TAKEOFF AT 72 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 31DEC04 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE AND PRESSURE SWITCH ASSY ACCORDING TO AMM78-31-06-2-F. T 29DEC04 05:38 SEAR WITH REF TO: A300-600 AMM 78-30-00-5 (GE-CF680C2A5F) NR 1 ENGINE THRUST-REVERSER RETURNED TO SERVICE. COMPLIED WITH AMM INSPECTION & OPERATING OUTLINE. NO REPEAT OF DISCREPANCY. CHECKS OK. MEL PLACARD REMOVED.
1998
Part: DETECTOR — FAILED (E/E COMPT)
AVIONICS SMOKE ECAM AND CRG AT 1500 FT AFTER T/O. NO ODOR WITH SNIFFER OR SMOKE IN COCKPIT. WARNING CONTINUED, DECLARED EMERGENCY AND RETURNED FOR LANDING. NOT OVERWEIGHT. NOTICED SLIGHT ELECTRICAL SMELL IN CABIN AFTER SHUTDOWN. FOUND SMOKE DETECTOR FAILED. REMOVED AND REPLACED 11WA DETECTOR PER MM 26-15-12-4, OPS TEST GOOD. NO HINT OF SMOKE IN AVIONICS COMPARTMENT, OK FOR SERVICE.
1996
Part: PANEL — MISSING (NR 1 PYLON)
LT WING I/B FLAP FAIRING I/B SIDE DAMAGED. PANEL 416AR TORN LOOSE FROM NR 1 ENG PYLON. PANEL EXITED A/C AND STRUCK TO LT WING I/B FLAP FAIRING. REPLACED MISSING PYLON PANEL, RELEASED FLAP FAIRING PER CDL 27-1. REMOVED MOVEABLE FLAP TRACK FAIRINGS FROM LT NR 2 FLAP TRACK PER MM 27-50-21 AND 57-20-35. REMOVED FAIRING SIDE LOAD STAY PER 27-50-23. INSPECTED ALL AREAS AFT, NO OTHER DAMAGE FOUND.
1995
Part: NR 1 FIRE SQUIB — MALFUNCTIONED (NR 2 ENGINE)
NR 2 ENGINE FIRE LIGHT, ECAM AND BELL ON LANDING AT EWR. AFTER PHASE I ITEMS COMPLETED, FIRE LIGHT CAME ON AGAIN IN HANDLE. DISCHARGED AGENT AND SECURED ENG. REMOVED AND REPLACED NR 2 ENGINE, NR 1 FIRE EXTINGUISHER BOTTLE PER MM 26-21-15, AFTER NR 1 FIRE BOTTLE REMOVED AND REPLACED, NR 1 AND NR 2 SQUIB W/N TEST. REMOVED AND REPLACED ENGINE S/O MODULE, NR 2 SQUIB TEST GOOD, NR 1 SQUIB DOES NOT TEST. REMOVED AND REPLACED NR 1 SQUIB, NR 2 FIRE DETECTION AND PROTECTION CHECKS GOOD AS PER MM. REF TO WRI 72-00/844 FOR ENGINE FIRE INSPECTION.