N748FD
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
PER CREW DEBRIEF, R1 DOOR SLIDE HANDLE HARD TO ARM/DISARM, DOOR OPENING/CLOSING AND LATCHING NOT AFFECTED, DOOR OPERATES NORMAL. RELEASED FOR SERVICE IAW MEL : 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 25-61-21-04-0 DURING GVI OF RT SLIDE FOUND SLIDER BOUND BY GIRT BAR FABRIC SLEEVE.RELEASED BINDING GIRT AND QUICK CHANGE BAR.DOOR SLIDE ARM/DISARM OPERATION CHECKS NORMAL.RETURNED RT DOOR TO OPERATION.
R1 DOOR SLIDE WOULD NOT DISARM . PBI RELEASED FOR SERVICE PER MEL : 52-11-01-01 CATEGORY C. CREW ENTRY DOOR ESCAPE SLIDE R1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." MEL: 52-11-01-001 OK FOR SERVICE. AMM: 12-22-52-00-01, AMM: 25-61-22-04-02, AMM: 52-10-00-03-01, FOUND GIRT PANEL PARTIALLY UNSNAPPED FROM ESCAPE SLIDE AND SAGGING DOWN. SECURED GIRT PANEL AS REQUIRED IAW AMM 25-61-22-04-02. CLEANED AND LUBED GIRT BAR AS REQUIRED IAW AMM 12-22-52-00-01. DOOR SLIDE ARMS AND DISARMS NORMALLY IAW AMM 52-10-00-03-01. OK FOR SERVICE.
R1 DOOR ASSIST BOTTLE REQUIRES DIAPHRAGM REPLACEMENT AND SERVICE PER AMM 52_10_14_03_10. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE DIAPHRAGM. SERVICED NITROGEN TO PLACARD ONBOARD. NO LEAK NOTED. CHECKS GOOD. OKAY FOR SERVICE.
FOUND ON SERVICE CHECK L 1 EMERGENCY OPERATION CYLINDER LOW PER SERVICE CHART. AMM: 52-10-14-03-10 SERVICED L 1 EMERGENCY OPERATION CYLINDER PER REF.
ON DEPARTURE, NR 1 ENG REV UNLOCK. RAN QRH, DECLARED EMERGENCY AND RETURNED TO ORF WITHOUT INCIDENT. AMM 78-31-35-04, AMM 78-32-11-05 IAW MOCC REQ (MTSI#78-31/9965) REPLACE ENG 1 SPLITTER GEARBOX. R & R ENG 1 SPLITTER GEARBOX. OPS CK OK. R & R SPLITTER AND PRSOV.
PRIOR TO PUSHBACK, WITH ALL DOORS CLOSED EXCEPT CREW ENTRANCE DOOR, RECEIVED AN ECAM ALERT FOR MAIN DECK CARGO SMOKE DETECTED MID & EXPERIENCED SMOKE IN COCKPIT FROM GASPERS. SMOKE ON SET RAPID & HIGHLY CONCENTRATED. SMOKE CLEARLY VISIBLE IN COCKPIT, APU BLEED AIR SELECTED OFF. FLIGHT CREW & LOAD CREW EXITED ACFT. APU HAD BEEN RUNNING FOR FIVE TO TEN MINS PRIOR TO SMOKE EVENT. AMM 21-51-00-03, OIL WETTING FOUND IN APU, APU WAS APROVED FOR R & R IAW W/C 4910000-00-00. OPS & LEAK CHKD GOOD. PERFORMED PACK BURN OUT, CHANGED COALESCER SOCKS IAW AMM 21-51-16-03-0. RAN BOTH ENGINES AGAIN AND RAN APU BLEED AIR FOR EXTENDED PERIOD OF TIME, NO SMOKE OR ODOR NOTED. ACFT OK FOR SERVICE.
EMPENNAGE - RH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER13) REPAIRED EMPENNAGE RH ELEVATOR UPPER L/E ER13 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6-5520-T0384490, TITEL: STABILIZERS - ELEVATORS - RH ELEVATOR UPPER SKIN REPAIR - RSC TRACKING. RSC TRACKING EA 6-5520- T0384490 WAS ISSUED AND COMPLETED. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 55209609 FOR WORL DETAILS
EMPENNAGE - LH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER2) REPAIRED EMPENNAGE LH ELEVATOR UPPER L/E ER2 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6-5520-T0384493, TITEL:STABILIZERS - ELEVATORS - LH ELEVATOR UPPER SKIN REPAIR - RSC TRACKING. RSC TRACKING EA 6-5520-T0384493 WAS ISSUED AND COMPLETED. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 55209606 FOR WORK DETAILS.
MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4EA FASTENER HOLES REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE PT1 BETWEEN FR22 AND FR25 4EA CRACKED FASTENER HOLES PER EA 6-5230-T0384376, MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 52309598 FOR WORK DETAILS.
LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)30MM*11MM, DEPTH: 1.60MM (2)150MM*15MM, DEPTH: 1.81MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKIN. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)40MM*16MM, DEPTH: 1.76MM (2)30MM*22MM, DEPTH: 1.83MM COMPLIED WITH EA 6-5750-T0384250 REPAIRED LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKIN. TITLE: WING - FLIGHT SURFACES - LH #4 SPOILER CENTER HINGE ARM OUTSIDE SURFACS DELAMINATION. THIS IS A CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 57509593 FOR WORK DETAILS.
RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: 50MM*15MM, DEPTH: 1.80MM COMPLIED WITH EA 6-5750-T0384249 REPAIRED RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE DELAMINATED SKIN. TITLE: WING - FLIGHT SURFACES - RH #3 SPOILER CENTER HINGE ARM AREA DELAMINATION. THIS IS A CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 57509594 FOR WORK DETAILS.
LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)30MM*18MM, DEPTH: 2.32MM (2) 82MM*39MM, DEPTH: 1.98MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR DELAMINATED SKIN. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT - UNDER FLOOR FR47 WEB CRACKED BETWEEN Y0 AND -Y450 REPAIRED THE MAIN DECK CARGO COMPARTMENT UNDER FLOOR FR47 CRACKED WEB BETWEEN Y0 AND -Y450 PER A300-600 SRM 53-15-15-201 PARA.5A. THIS IS A CAT B REPAIR. THE FIRST INSPECTION WAS 24000FC AFTER REPAIR EMBODIMENT AND THE SUBSEQUENT INSPECTION INTERVAL WAS 3000FC UNTIL 51000FC. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RIGHT FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPAIRED THE RH FWD PAX DOOR FRAME FR14C CRACKED SEGMENT PER SRM 51-40-21 AND DWG F52181297 ISSUE: K AND DWG F52181299 ISSUE: G. THIS IS A CAT A REPAIR AND RSC TRACKING EA 6-5210-T0384405 WAS ISSUED AND COMPLETED, TITLE: DOORS - PASSENGER/CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR - RSC TRACKING. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
CARGO DOOR / HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. THIS IS CATEGORY B REPAIR. FOLLOW-UP INSPECTION PER EO 6-5230- E0378588 B. MAJOR REPAIR IAW FEDEX GMM6-2-100.
NUMBER 1 OUTFLOW VALVE DEFERRED. AFTER TO #2 OUTFLOW STUCK FULL OPEN. COMPLIED WITH QRH REQUIRED MANUAL CONTROL TO OPEN ON TAXI IN. REMOVED AND REPALACED THE FWD OUTFLAW VALVE ASSY (202HM) I.A.W AMM 21-31-12-04 OPS CHECK PER AMM 21-31-00-5 OPS CHECK PASSED.
IN SYS 1 LANDING GEAR POSITION DETECTOR, TOOK OFF AND ATTEMPTED TO RAISE GEAR. UNABLE. WENT TO SYSTEM 2, GEAR CAME UP, BUT WE GOT MULTIPLE FAILURES. PITCH TRIM 1, ATS, CAPT PITOT OVERHEAT, FO PITOT OVERHEAT, STBY PITOT OVERHEAT, CAPT TAT HEAT FAILURE, CABIN PRESS REG 1., ADC 1. SWITCHED TO ADC SYSTEM 2, FD SYS 2. FO REMEMBER THE FCIF 24-00179 CONCERNING THIS ISSUE. DECLARED AN EMERGENCY. L/G POSITION DET SYSTEM 1 IS DRIVEN BY RELAY 90GB . REMOVED AND REPLACED RELAY 90GB PRECAUTIONARY. REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT 54GB GND FUNTIONAL CHECKS GOOD. ALL OTHER SYSTEMS THAT FAULTED A/T / ADS / PROBES OVERHEAT / CABIN PRESS REG / PITCH TRIM AND LANDING GEAR IND ALL GROUND CHECKS GOOD AT THIS TIME PER M/MS A/C OK FOR SERVICE.
ON MX PREFLIGHT: JUMPSEAT AREA EMERGENCY LIGHTS INOP. REPLACED EMERG. SUPPLY BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOOD. A/C OK FOR SERVICE.
ON POSTFLIGHT, R1 DOOR ESCAPE SLIDE RELEASE WARNING LIGHT INOP, BUZZER OPERATES NORMALLY. RELEASED FOR SERVICE PER MEL : 52-XX-XX-XX CAT C EXP : AUG24 - R1__ CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP." R1 DOOR BUZZER OPERATES NORMAL, ITEM PLACED ON MEL. REMOVED AND REPLACED DOOR WARNING LIGHT IN REF TO AMM 52-73-11-04-01. OPS CHECK GOOD. A/C OK FOR SERVICE.
REJECTED TAKE OFF AT 40KTS FOR BLUE HYDRAULIC LOW ECAM CAUTION.
PERFORMED CAT III AUTOLAND WITH LOW BRAKES. DURING ROLLOUT PHASE, AIRCRAFT PULLED TO THE RIGHT WHEN AUTO BRAKES APPLIED. REQUIRED TO DISCONNECT AUTOPILOT AND RECENTER AIRCRAFT. WHEEL ECAM PAGE SHOWED RIGHT MAIN GEAR TEMPERATURE BETWEEN 450-500 DEGREES DEGREES. LEFT MAIN GEAR SHOWED READINGS AROUND 15 DEGREES DEGREES. SEEMED LIKE LEFT AUTOBRAKE SYSTEM DID NOT WORK AND THE RIGHT SIDE DID MOST/ALL OF THE BRAKING. PERFORMED BLEED STEPS ON THE BRAKE SYSTEM RESEVIOR (4300), TO THE DUAL ALTERNATE BRAKE DISTRIBUTION VALVE. FOUND AIR IN BOTH LEFT AND RIGHT SIDES OF THE DUAL ALTERNATE BRAKE DISTRIBUTION VALVE. BLED AND SERVICED RESERVOIR. PISTON IS NOW INSIDE OF SERVICEABLE BAND OF THE BRAKE SYSTEM RESEVIOR (4300), PERFORMED CHECK OF REMOVED AND REPLACED BRAKE AUTOMATIC SELECTOR. PERFORMED LEAK CHECK OF AUTOMATIC SELECTOR (1300). FOUND 2 EA. LEAKS. RESEALED 90' PRESS ELBOW AND RETORQUED RETURN B-NUT PER MM 32-42-13-04. AUTOMATIC SELECTOR LEAK CHECK NORMAL. REPLACED BRAKE SYSTEM CONTROL UNIT (29GG) MM 32-42-72-04. BITE TEST NORMAL-NO FAULTS. A/C OK FOR SERVICE PER MM 32-42-00-05.
1EA WATER TRAPPED AREA(140MM X 180MM) WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL T/E NO.26 SCREW. ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-21-12-201- 2, PARA.5F(REPAIR NO.6) PAGE.239-243, FIG.209(SHEET1-2) & SRI:55-21-12-201, IIR:55-21-12-2-001- 00, PARA.3A, TABLE.202, PAGE.203/204 "MAJOR REPAIR"
FUSELAGE SKIN FOUND 1EA DENT AT FR99 PLUS 5",S-4L PLUS 5" REPAIRED THE DAMAGE AREA WITH DOUBLER, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 53-19-12- 201, PARA.5, FIG.201, PAGE.204~208 "MAJOR REPAIR"
ON FINAL APPROACH ON RW 27, KMEM AT 3000 FT, GOT A SPOILER FAULT WITH #7 SPOILER SHOWING UP. DID ECAM & QRH PROCEDURE AND COULD NOT GET IT TO GO DOWN. DECLARED AN EMERGENCY AND LANDED ON RW 36C, BRAKES WERE NOT SHOWING HOT. TAXIED BACK TO THE RAMP. SPOILER SHOWED UP THE ENTIRE TIME, EVEN AFTER ENGINE SHUTDOWN. GAINED ACCESS TO 1790VC , DISCONNECTED PLUG 1790VCA. CLEANED SOCKETS OF RECP. AND PINS OF PLUG. CHECKED SOCKETS FOR PIN TENSION ,ALL CKED GOOD. CHECKED WIRING FROM RECEPTACLE TO HARNESS, ALL WIRING WAS GOOD. RECONNECTED PLUG TO RECEPTACLE. PERFORMED SEVERAL SPOILER INDICTION TEST. ALL TEST PASSED WITH GOOD INDICTION. IAW AMM 27-11-00-05-02, ESPM 20-55-50.
HI ENG OIL TEMP #1, GOT INITIAL ADVISORY AT CRUISE LEVELOFF 35,000; 168C. FOLLOWED QRH ADVISORY WHICH LED TO ENG OIL HI TEMP QRH PROCEDURE. TEMPERATURE PEAKED AT 176C, SHOWED 36C TO 40C HOTTER THAN #2 ENG DURING DESCENT AT FLIGHT IDLE. EMERGENCY DECLARED, DID NOT SHUTDOWN ENGINE. DRAINED OIL TANK AND VERIFIED QUANITY. REFILLED OIL TANK IAW A300 AMM 12-13-00-00. REMOVED AND REPLACED OIL TEMP SENSOR IAW AMM 79-32-11-04 DT582. CLEANED CANNON PLUG DT 597 FOR #3 BEARING TEMP .PERFORMED ENGINE RUNS AT POWER IN REF TO JRH CHAPTER 4 TEMPS STAYED AT 100 C. OK TO CONTINUE.
DURING THE EO NO: E 6-5710-E0342809 B P3 PARA. 5, FOUND THE HOLE "I" HAD BEEN ENLARGE ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE I REPAIR I.A.W. A300-600 EA NO: T6-5710-T0362021 P1, SEQ NO: 001077.
DURING EA NO: T 6-5710-T0307375 P2, FOUND HOLE "S" DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENERS HOLES CRACK REPAIR I.A.W. A300-600 EA NO: T6-5710- T0307375 A P3, SEQ NO: 001079.
PFM E.O. NACELLES /PYLONS INSP FOUND NO.2 PYLON O/B SIDE PNL AT RIB 8 HAS CRACK ALONG FRONT SCREW HOLE IAW WORK CARD SEQ 000960 INSPECTION OF PYLON SIDE PANELS AT RIB 8 AIRBUS SBA300-54- 6015 R03 & A310-54-2018 R03 E.O. 6-5450-7-5003 H PT4 SUBSTEP A. THRU D. ACCOMPLISHED REPAIR WORK
THE #241PH FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
THE #262XF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
THE #152GF FLOOR PANEL OF LOWER AFT CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
THE #132RF FLOOR PANEL OF LOWER FWD CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
THE #162HF FLOOR PANEL WAS FOUND SOFTEN & SERIOUS DAMAGED OVER HALF AREA FABRICATED THE FLOOR PNL I.A.W. FEDEX DWG. SRZ-25-005, REV. R AND SRZ25-011, REV. E.
THE #232RG FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
THE #232CF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
MAIN DECK SEAT TRACK CROWN AREA GOT A GOUGE AT FR 59,-Y450 PERFORM CUT OUT DAMAGE TRACK ( LENGTH 30.6") & REINFORCED REPAIR PART AND SPLICE U- SECTION WORK INSTUCTION I.A.W A300-600 SRM SUPPLEMENT 53-10-16-201, PARA 5 FG 202, P. 209-214
2EA DELAMINATIONS WERE FOUND. AREA 1 (80CM2) NEAR O/B HINGE ARM OF RH SPOILER 4. AREA 2 (82CM2) NEAR I/B HINGE ARM OF RH SPOILER 4. ACCOMPLISHED THE WORK: WING - FLIGHT SURFACES - RH 4# SPOILER LOWER SKKIN DELAMINATION NEAR CENTER HINGE ARM REPAIR I.A.W. A300-600 EA NO: 6-5750-T0361975.
M/D Y1456 SEAT TRACK CROWN GOUGE AT FR66 12.5" ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W. A300-600 SRM SUPPLEMENT 53-10-16-201, PARA. 5, FIG. 202, P. 209-214.
MAIN DECK FLOOR SEAT TRACK CROWN FOUND GOUGE BTWN FR26 16" AND FR26 18". ACCOMPLISHED THE FLOOR SEAT TRACK REPAIR I.A.W. A300-600 SRM 53-10-16-201, PARA. 10, FIG. 208 (SHEET 1) P. 243-248.
LH WING O/B FLAP L/E NOSE GOT A DENT AT RIB17 5". ACCOMPLISHED THE DENTED AREA REPAIR I.A.W. A300-600 SRM 57-50-00-201, PARA. 4H, P. 230- 234, FIG. 208. THIS IS CAT. B REPAIR I.A.W. A300-600 SRM 57-50-00-201, P. 202 AND SRI 57-50-00-201 IIR 57-50- 00-2- 001-00, PARA. 3.A, P. 201-204.
MDIS 748 52-70 3083 29JUN19 MEM FACT U WHILE TROUBLESHOOTING R1 DOOR, PERFOMED BITE TEST OF ASPSU REF AMM 52-73-00-05-01 AND FOUND TEST TO BE FAILING. SHOWS BAT 1 AND BAT 2 FAILURE. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: POS: ONL SRL: 002761 TAG NBR: G21412 ON MPN: 3214-90 CPN: 5210609 SRL: 0694 TAG NBR: 7371F5 REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 2 SRL: 128491 TAG NBR: G40821 ON MPN: AD-3214-30 CPN: 3310373 SRL: 61771 TAG NBR: H44581 REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 1 SRL: 82640 TAG NBR: 2230F8 ON MPN: AD-3214-30 CPN: 3310373 SRL: 54329 TAG NBR: 080F55 FACT 30JUN19 17:50 MEM U R & R APSCU AND ASSOC BAT 1 AND BAT 2 REF MM 52-73-18-04 OPS CK GOOD.
RT SIDE ENTRY DOOR, IN FLIGHT, MAKING LOUD SQUEAL AND HAS A FLASHING RED LIGHT. INDICATIONS WERE NORMAL WHEN ARMED ON THE GRD. COCKPIT INDICATIONS NORMAL. DURING FLIGHT. CORRECTED ITSELF AFTER LANDING WITH NO PRESSURIZATION IN CABIN AREA. TROUBLESHOT REF TSM 52-73-00 FOUND A CHAFED WIRE FOR WARNING LIGHT RUBBING AGAINST THE SLIDE ARM\DISARM PIN BRACKET. REPLACED THE CONTACT REF ESPM 20-48-20. ALSO REPLACED THE TEST SWITCH 40WN REF MM 52-73-14-04-01 AND TSM 52-73-00. REPLACED 40WN [E0064-83-5-0] P/B TEST SWITCH. PRESSURIZED A/C REF MM 05-53-00 AND ALSO REF MM 52-73-00-05 NO NOISE, NO LIGHTS, AND NO LEAKS FOUND A/C OK FOR SERVICE.
AFTER FLIGHT, JUMPSEATER REPORTED THAT RIGHT CREW ENTERY DOOR (R1) WAS BEEPING AND PRESSURE LIGHT WAS ON ABOVE 10,000 FEET. THERE WERE NO INDICATIONS IN THE COCKPIT. ADJUST R1 DOOR LIMIT SWITCH 10WN REF. MM 52-73-13-05-01 FIGURE 501. OPS CHECKED GOOD, RETURN A/C TO SERVICE.
FLOOR PANEL P/N A5398408500600 IS CRUSHED ON THE INBOARD SIDE OF TOP PANEL AND MISSING A SECTION OF PANEL. FABRICATED NEW FLOOR PANEL PER DWG SRZ-25-005 REV P
REJECTED TAKE-OFF TO STAGNATED AIRSPEED @ 100 KIAS BOTH CAPT AND F\O AIRSPEED INDICATORS. PERFORMED RTO CHECK LIST. NO BRAKE FANS INSTALLED ON THIS AIRCRAFT, TAXI BACK TO GATE 823 WITH HOT BRAKES, MOST TEMPS ON BRAKES WERE ABOVE 440 ON RIGHT ECAM. TROUBLESHOT PER TSM 34-10-00 FIG. 112. PERFORMED AIR DATA SYSTEM FUNCTIONAL TEST REFERENCE AMM 34-10-00-05, PITOT HEATER TEST REFERENCE AMM 30-31-00-05 AND AIR DATA SYSTEM FLUSHING REFERENCE AMM 34-10-00-03. NO DEFECTS NOTED AT THIS TIME, ALL CHECKS GOOD. RAN AIRSPEED AND STANDBY AIRSPEED UP AND DOWN MULTIPLE TIMES, VARYING THE SPEED OF ACCELERATION AND DECELERATION IN AN ATTEMPT TO CATCH INDICATION HANGING UP. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY AND NO HISTORY NOTED. OK FOR SERVICE.
ON GEAR EXTENSION GEAR DID NOT COME DOWN RECYCLEED GEAR 3 REDS PROC "MAIN GEAR EXT"ACCOMPLISHED PER QRH. POS DET 1& 2. GOT TOWED TO RAMP. HYD SYST NORMAL IN FLIGHT AFTER BLOCK IN GREEN SYST OFF SCALE HIGH. RESET MANUAL GEAR EXTENSION TO NORMAL POSITION IAW AMM 32-33-00-00-0 AND HYD QTY RETURMED TO NORMAL AFTER CLOSING LANDING GEAR DOORS IAW AMM 32-33-00-00-0. RELEASED FOR SERVICE PER MEL : 32-30-01-B "MEL 32-30-01-B: LANDING GEAR RETRACTION SYSTEM - INOP. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE." NO OVIOUS FAULT FOUND, TRANSFER TO MEL 32-30-01-B, AS REQUESTED BY MOCC, A/C OK FOR SERVICE. REMOVED AND REPLACED 3GA LANDING GEAR SELECTOR VALVE REF AMM 32-31-12-04, LEAK CHECK GOOD. PERFORMED OPS CHECK REF AMM 32-31-12-6 AND NORMAL EXTENSION/RETRACTION TEST REF AMM 32-31-00-05. PERFORMED OPS CHECKS OF LANDING GEAR NORMAL CONTROL MICROSWITCH (GEAR HANDLE) REF 32-31-11-04 AND ALL CHECKS GOOD. P/N OF NEW SELECTOR VALVE- A25199-0-3, S/N H0232 P/N OF OLD SELECTOR VALVE- A25199-0-3, S/N M412.
LEFT MAIN GEAR TOOK AN EXTRA 20 SECONDS TO COME DOWN WE ALMOST HAD TO GO AROUND. REMOVED AND CHECKED LEFT MAIN GEAR VALVE AND GEAR DOOR RESTRICTOR VALVES. FOUND DIRT IN GEAR RESTRICTOR VALVE. REPLACED GEAR RESTRICTOR PER AMM 32-31-57-04 AND GEAR DOOR RESTRICTOR VALVES PER AMM 32-31-58-04. LEAK CHECK AND GEAR SWING GOOD. GEAR RESTRICTOR VALVE PN 7310SE010500. GEAR DOOR RESTRICTOR VALVE PN 7306SE010200.
RT WING CENTER FLAP RIB 26 HAS TWO CRACKS AT TOP SKIN ATTACHMENT, 6TH FASTENER AND 12TH FASTENER FWD OF REAR SPAR. REPAIRED 2 CRACKS BETWEEN STR 2.7 AND 2.8 IAW SRM 57-50-00, FIG 201, SEE RSC TRACKING EA 6-5750-T0343180 PT1, WRI 57502376. REPAIR IS CLASSIFIED AS CAT "A" AND MAJOR REPAIR.
TAIL COMPARTMENT BETWEEN FRAMES 86 AND 87, STRINGER 23R, WEB AND STRAP ARE BENT. FABRICATED THE WEB AND STRAP IAW SRM 53-19-18, AND SRM 51-31-00. REMOVED AND REPLACED THE WEB AND STRAP IAW SRM 51-40-21. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 252XG WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 242KF WAS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 231HG BROKEN. FABRICATED FLOOR PANEL 231HG IAW SRZ-25-005 ON T18/1373260. INSTALLED ON WORK CARD E-6-5321-E0339394 A PT4. REPAIR CAT "A" MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 252JK BROKEN. FABRICATED FLOOR PANEL 252JK IAW SRZ-25-005 ON T18/1373252. INSTALLED ON WORK CARD 250-FL-FIT. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 242XJ BROKEN. FABRICATED FLOOR PANEL 242XJ IAW SRZ-25-005 ON T18/1373258. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 242WJ BROKEN. FABRICATED FLOOR PANEL 242WJ IAW SRZ-25-005 ON T18/1373250. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 252WG BROKEN. FABRICATED FLOOR PANEL 252WG IAW SRZ-25-005 ON T18/1373244. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 252UH BROKEN. FABRICATED FLOOR PANEL 252UH IAW SRZ-25-005 ON T18/1373247. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 241LK HAS DAMAGED CORNER SECTION. FABRICATED FLOOR PANEL 241LK ON T18/1372165 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 252XK BROKEN. FABRICATED FLOOR PANEL 242XK ON T18/1372105 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
CABIN FLOOR PANEL 241HK HAS BROKEN CORNER. FABRICATED FLOOR PANEL 241HK ON T18/1372172 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 251XF BROKEN. FABRICATED FLOOR PANEL 241XF ON T18/1372104 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 251SK BROKEN. FABRICATED FLOOR PANEL 241SK ON T18/1372103 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
COURIER FLOOR PANEL 221PF DELAMINATED. FLOOR PANEL 221PF FABRICATED ON T18/1371843. CLASSIFIED AS A CAT "A" MAJOR REPAIR IAW SRZ-25-005.
DURING CLIMB OUT FROM KMEM, ENG 1 LOOP B FAULTED. PER FLT CREW THE ENG 1 B LOOP FAULT LIGHT FLICKERED ON AND OFF MULTIPLE TIMES THEN WOULD FAULT AND GO OUT AGAIN. THEN FAULTED AND STAYED FAULTED. THE LOOP TESTED GOOD ON THE GROUND AND WOULD NOT FAULT. PERFORMED VISUAL CHECK OF ALL NR 1 ENGINE B FIRE LOOPS. SHOOK ALL WIRE HARNESSES FOR FIRE LOOPS CHECKED CONNECTIONS. NO FAULTS NOTED INTERMITTENT OR LATCHED. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL UNIT. REF AMM 26-12-11-04. PERFORMED 5 FIRE LOOP TESTS ON NR 1 ENGINE. OPS TESTS GOOD AT THIS TIME.
DURING BLOCK IN, NOTICED THE RIGHT CABIN DOOR SLIDE SHOWED DISARMED EVEN THOUGH THE LEVER WAS IN ARMED POSITION. PERFORMED OPS TEST OF THE R1 DOOR SLIDE ECAM MESSAGE IAW MM 52-73-13-05-09, OPS TESTED NORMAL.
WITH STAB TRIM SET AT 2.5 DEGREES THE TAKE OFF CONFIGURAION TEST FAILED WHEN CHECKED ON TAXI OUT. WE CONFIRMED THE TRIM WAS CORRECT AND WAS SET ACCORDING TO APS. ECAM HAD INDICATED OUT OF TO RANGE AS REASON FOR FAILURE. WE RESET TRIM SETTING, VERIFIED THE IDEX WAS IN THE GREEN BAMD. A SECOND TO CONFIG TEST WAS SATISFACTORY. ON TO ROLL AT APPROX 100 KTS RECIEVED TO WARNING HORN W/NO ECAM INDICATION. ABORTED TAKE OFF AT APPROX 100 KTS AND 330,000 LBS. PERFORMED ADJUSTMENT OF MECHANICAL CONTROL OF THS REF A300-600 MM 27-40-00- 5AND 27-41-00-05 THRU STEPS 1. D (D) AND CHECKED CONTROL CABLES REF PARAGRAPH (2) A-E. ALL RIG PINS REMOVED AND TURNBUCKLES SAFTIED AT FRAME 20
R1 DOOR INDICATED UNLOCKED WHILE CLIMBING THROUGH APPROX 4000 FEET. PRESSURIZATION INDICATED NORMAL. FOUND THE DOOR CONTROL HANDLE NOT FULLY IN LOCKED POSITION AND LOUD SQUEAL COMING FROM AROUND THE DOOR FRAME. PUSHED DOOR HANDLE DOWN IAW QRH AND DOOR INDICATED LOCKED AND SQUEAL CEASED. NORMAL INDICATION FOR REMAINDER OF FLIGHT. L1 DOOR INTERIOR CONTROL HANDLE LATCH ASSY FOUND CONDUIT FROM DOOR PRESSURE LIGHT ROUTED OVER THE LATCH ASSY, NOT ALLOWING POSITIVE LATCHING, SPRING AND PLUNGER WERE CONTAMINATED WITH DIRT AND GREASE NOT ALLOWING PROPER EXTENSION AND RETRACTION OF SPRING ASSY TO ALLOW LATCH TO ENGAGE. CLEANED AND LUBRICATED ALL COMPONENTS. SATISFACTORY DOOR OPERATION AND LATCH ASSY AFTER REROUTING CONDUIT AND CLEANING. FOUND BROKEN STRAIN RELIEF ON ELECTRICAL CONNECTOR IAW WRI 52-70 / 0654. R1 INTERIOR PANELS STILL NEED TO BE INSTALLED IAW AMM 52-10-20-05-01. PREFORMED OPS CHECK OF R1 DOOR PRESSURE WARNING LIGHT, CHECKED GOOD IAW AMM 52-73-15-04-01, NO ADJUSTMENTS MADE. INSTALLED DOOR LINER IAW AMM 52-73-00-05-01.
RIGHT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10 FOUND CRACK. COMPLIED WITH EA 6-5450-T0324904 PT 1. REPAIRED RT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10. THIS REPAIR WAS CATEGORY C. REPAIR LIFE LIMITATION 6 MONTHS. LIFE LIMITATION MAYBE FURTHER EXTENDED AFTER DETAILED ANALYSIS. MAJOR REPAIR IAW GMM 6-2-100.
RIGHT PYLON RIB 18-19, AFT FAIRING UPPER SPAR CRACKED AT OTBD SIDE, APPROX 3.0 INCHES IN LENGTH.
LEFT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10 FOUND CRACK. COMPLIED WITH EA 6-5450-T0324873 PT 1, REPAIRED LT PYLON LOWER SPAR CENTER STIFFENER. THIS REPAIR WAS CATEGORY C. REPAIR LIFE LIMITATION 6 MONTHS. LIFE LIMITATION MAY BE FURTHER EXTENDED AFTER DETAILED ANALYSIS. MAJOR REPAIR IAW GMM 6-2-100.
CENTER MAIN DECK UNDER FLOOR, FRAME 47, BETWEEN Y953 & Y1456, VERTICAL WEB CRACKED. REPLACED THE VERTICAL WEB, CTR MAIN DECK UNDER FLOOR IAW SRM 51-40-21. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CENTER MAIN DECK UNDER FLOOR FRAME 47, BETWEEN Y-953 & Y-1456, VERTICAL WEB CRACKED. REPAIRED THE VERTICAL WEB IAW SRM 53-15-15 FIG 201 SHEET 2. THE REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100. THE FIRST INSPECTION THRESHOLD WAS 24000 FC AFTER REPAIR EMBODIMENT, THE REPETITIVE INSPECTION INTERVAL WAS 3000 FC & THE INSPECTION METHOD WAS DETAILED VISUAL IAW SRI 53-15-15-2-001-00.
MAIN DECK CARGO COMPARTMENT, FRAME 11 - 13A, Y730, FLOOR SUPPORT CORRODED. REPLACED THE MDCC FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR WAS CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, FRAME 11 - 13A, Y953, FLOOR SUPPORT CORRODED. REPLACED THE MDCC FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR WAS CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.
BULK CARGO COMPARTMENT, FRAME 66 - 69, Y805, FLOOR SUPPORT CORRODED. REPLACED THE BULK CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-40-21. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.
BULK CARGO COMPARTMENT, FRAME 66 - 69, Y140, FLOOR SUPPORT CORRODED. REPLACED THE BULK CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-40-21. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.
AFT CARGO COMPARTMENT FRAME 63, BETWEEN Y805 & Y1470, FLOOR CROSSBEAM CORRODED. REPAIRED THE TOP CAP OF FLOOR CROSSBEAM IAW SRM 53-10-15 FIGURE 207. THIS REPAIR WAS CATEGORY A. MAJOR REPAIR IAW MM 6-2-100.
AFTER LANDING, BRAKE TEMPS APPEARED TO BE CLIMBING NORMALLY, NO BRAKES FANS. AFTER TAXING FOR A WHILE MOST BRAKE TEMPS WERE BELOW 200 DEGREES, ONE ON THE LT SIDE CLIMBED TO MAX 280 DEGREES. NR 3 BRAKE KEPT CLIMBING., RT SIDE BRAKES WHERE NOT USED AFTER 285 DEGREES, NR 3 KEPT CLIMBING NOTIFIED OPERATIONS, NOTIFIED FIRE DEPARTMENT & MX. PULLED INTO PARKING AREA WITH NR 3 BRAKE CLIMBING ABOVE 600 DEGREES, MAXED AT 700 DEGREES. FIRE TRUCKS ARRIVED & FIRE INDICATED OUT. REMOVED AND REPLACED NR 3 BRAKE IAW AMM 32-42-27 . REMOVED AND REPLACED NR 3 TIRE IAW AMM 12-37-32. COMPLIED WITH AFTER BRAKE OVERHEAT INSPECTION . REMOVED AND REPLACED NR 3 MLG WHEEL TACHOMETER.
AFTER LANDING ON 15R & CLEARING RUNWAY, BRAKE TEMPS APPEARED TO BE CLIMBING NORMALLY, NO BRAKES FANS, AFTER TAXING FOR A WHILE MOST BRAKE TEMPS WERE BELOW 200 DEGREES. ONE ON THE LT SIDE CLIMBED TO MAX 280 DEGREES. NR 3 BRAKE KEPT CLIMBING. RT SIDE BRAKES WHERE NOT USED AFTER 285 DEGREES, NR 3 KEPT CLIMBING, NOTIFIED OPERATIONS, FIRE DEPARTMENT & MX. PULLED INTO PARKING AREA WITH NR 3 BRAKE CLIMBING ABOVE 600 DEGREES, MAXED AT 700 DEGREES. FIRE TRUCKS ARRIVED, FIRE INDICATED PUT OUT. R & R NR 3 BRAKE IAW AMM CH 32-42-27. R & R NR 3 TIRE IAW AMM12-37-32. COMPLIED WITH AFTER BRAKE OVERHEAT INSPECTION. R & R NR 3 MLG WHEEL TACHOMETER.
WE HAD A VIOLENT BANG WITH THE GEAR WARNING ON THE RT MAIN GEAR DOOR WITH OVERSPEED WARNING, NO OTHER INDICATIONS. NORMAL GEAR EXTENSION AT LANDING ON TOUCHDOWN WE COULD FEEL THE RUMBLE OF POSSIBLE TIRE FAIL. QRH FOR GEAR DOOR WAS COMPLETED. DOOR WAS INSTALLED & ALL DISCREPANCIES ACCOMPLISHED. ACFT OK FOR SERVICE.
LEFT MLG RIB 5 FITTING FWD LUG HAS CORROSION IN BORE, FWD FACE & AFT FACE. COMPLIED WITH EA 6-5710-T0310821 P1 BASIC WINGS STRUCTURE LT & RT RIB 5 CORROSION.
RIGHT RIB 5 MLG FITTING HAS CORROSION IN BORE AT FWD LUG. COMPLIED WITH EA 6-5710-T0310821 P2 BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.
LEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
LEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
RIGHT FUSELAGE TO CENTERR WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
RIGHT FUSELAGE TO CENTER WING BOX FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
MAIN DECK FRAME 47, STRINGER 24 - 26 RT N HOLE FOUND CRACKED. REPAIRED, MAJOR REPAIR IAW 6-2-100.
LEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
LEFT FUSELAGE TO CENTER WING BOX ATTACH ANGLE AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
CRACK FOUND IN CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.
CRACK FOUND IN THE CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.
CRACK FOUND IN THE LT CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.
GREEN HYD QTY DECREASED DURING FLIGHT UNTIL LOW QTY ECAM WARNING. DECLARED EMERGENCY, FOLLOWED QRH MANUAL GEAR EXTENTION HYD FAILURE REQ TOW IN. PRESS REMAINED NORMAL UNTIL QTY LOW INDICATION, VERY SLOW QTY LOSS ABOUT 2 HRS INTO FLIGHT WHEN INDICATION OCCURRED. CREW REPORTED PRESS WAS GOOD. FOUND GREEN RESERVOIR FULL AT MECHANICAL GAUGE. PRESSURIZED SYS, NO LEAKS FOUND. R & R GREEN RESERVOIR HYD QTY TRANSMITTER. SERVICED GREEN SYS CHECKS NORMAL IAW MM29-31-11-04.. DUE TO MANUAL EXTENSION IN FLIGHT PERFORMED RESTORATION OF SYS TO NORMAL AFTER FREEFALL EXTENSION IAW MM 32-33-00-02, OK FOR SERVICE.
DURING CLIMB, RECEIVED A PARTIAL POWER LOSS. ALL INSTRUMENTS ON F/O'S SIDE. RT ECAM, RT FMS AND RT IDC 900 WERE LOST. FOUND TR2 FAULTED ON MAINT PANEL. R & R TR2 (2PU) IAW MM 24-32-11-04. OPS TEST NORMAL IAW MM 24-32-00-05. OK FOR SERVICE.
IMMEDIATELY AFTER TAKEOFF, ECAM YELLOW LOW PRESSURE. LOW YELLOW QUANITY. FOUND LT AILERON YELLOW SYS SERVO CONTROL HYD LINE RUPTURED. R & R HYD LINE, (PN A27142012), REF MM 27-14-12-04. SERVICED YELLOW HYD SYS IAW MM 12-12-29-0. LEAK CK GOOD. ENGINE PUMP REPLACED AND FILTERS CHECKED DUE TO CREW UNSURE OF ACTUAL TIME PUMP ONLINE WITH LOW FLUID. FINAL CLOSED
LT WING ALL SPEED AILERON LOWER SURFACE T/E HAS 2 EA DENTS WITH DELAMINATION 10 IN FROM OFF CENTER T/E DEFECTS MEASURE 1.5 X 1.0 X 0.003 AND 1.0 X 1.5 X 0.002. REPAIRED LT WING AILERON LOWER T/E SURFACE BY CUTTING OUT DAMAGE AND APPLYING FILLER AND DOUBLER IAW SRM 57-77-12 (4C).
SEAT TRACK GOUGED BETWEEN FR 48 AND 49. BLENDED GOUGE, FOUND TO BE OUT OF LIMITS IAW 51-73-10. REMOVED DAMAGED SECTION AND INSTALLED SEAT TRACK REPAIR IAW SRM 51-10-16.
LT ELEVATOR TOP SKIN APPROX 14 FT FROM ELEVATOR TIP AND 9.5 IN. FROM T/E HAS A PUNCTURED IN COMPOSITES 1.0 IN. X .50 IN REPAIRED 1 EA PUNCTURED ON ELEVATOR TIP OTBD T/E USING CARBON FIBER AND RESIN IAW SRM 55-21-12, PARA 5A. RESTORED SURFACE PROTECTION IAW SRM 51-75-10, PARA 3. REF EA 6-5520-156051.
AFT CARGO COMPARTMENT STRINGER 56R CORRODED LOCATED BETWEEN FRAME 57.2 THRU FRAME 57.3. FOUND OUT OF LIMITS IAW SRM 51-73-11. REPAIRED STRINGER IAW SRM 53-10-14, FIG 201E, SHEET 1, PAGE 215/216.
FWD CARGO DOOR EXTERIOR SKIN DENTED APPROX L=0.7X W"=0.5" BETWEEN FR 21A AND FR 22 AT BEAM 3. FWD CARGO DOOR EXTERIOR SKIN DENTED, SKIN REPAIRED IAW SRM 52-30-00, FIG 203. COMPLIED WITH EA6-5230-156053.
LT WING INBD FLAP INBD L/E RIB HAS A 1" X 1" X .102" DENT REPAIRED LT WING INBD FLAP INBD L/E DENT IAW WITH SRM 57-50 00, PG 231-234, FIG 208.
FLOOR PANEL 241LK BROKE IN 2 PIECES. FABRICATED REPLACEMENT FLOOR PANEL 241LK IAW DWG SRZ25-005, REV J.
R-1 DOOR FWD UPPER CORNER INNER SKIN HAS WEAR MARK. BLENDED OUT. DAMAGE FOUND TO BE OUT OF LIMIT IAW SRM 52-11-00, TABLE 101. ORIGINAL MATERIAL THICKNESS .039, MATERIAL LOSS ,006. REMOVED SEAL RETAINER FOR ACCESS OF REPAIR IAW SRM 51-40-21. CUT-OUT DAMAGE IAW SRM 52-11-00, FIG 208. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 52-11-00, FIG 208. LOCATED AND DRILLED HOLES ON DOUBLER AND FILLER IAW SRM 51-40-44. NDT CHEKED FOR CRACK ON CUT OUT. NO CRACK FOUND. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 51-40-21 AND IAW SRM 52-11-00, FIG 208 & INSTALLED DOOR RETAINER SEAL. COMPLIED WITH E.A. 6-5210-156052
LT WING LOWER INBD SURFACE PICKUP ANGLE AFT OF REAR SPAR RIB 1 HAS 15" AREA OF CHAFING AT HYD SERVICING PANEL. R & R ANGLE (STAMPING) IAW SRM 51-40-21, PARA 5.
AFT CARGO DOOR BULB SEAL DEPRESSOR FOR DOOR CUTOUT HAS NICKS AND GOUGES OVER ENTIRE SURFACE ALONG FWD AND AFT EDGES. R & R 6EA SEALING SECTIONS ON AFT CARGO DOOR CUTOUT.
SEAT TRACK R-5 HAS GOUGED SCALLOPS AT 2 EA PLACES BETWEEN FR63R AND FR64R. SMOOTHED AND BLENDED 2 EA GOUGES IN SEAT TRACK BETWEEN FR 63R AND FR 64R IAW SRM 51-73-10, PARA 5, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 51-40-20 AND 53-10-16.
FLOOR SUPPORT CORRODED BETWEEN FR 14A TO FR 16, BUTTLINE -Y1959, AT BOTTOM SIDE AROUND FASTENER HOLES. TEE CORRODED WITH 100 PERCENT LOSS, R & R TEE IAW SRM 51-72-10.
FLOOR PANEL 262 ZF IS BROKEN IN HALF AND CRACKS FABRICATED REPLACEMENT FLOOR PANEL 262 ZF IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.
CABIN SEAT TRACK 4R, FRAME 74 9 INCHS, 2 EACH GOUGES ON SCALLOP TOP ON EACH SIDE 1/4" BY 1/4" WITH METAL RAISED UP .100" SMOOTHED AND BLENDED CABIN SEAT TRACK 4R, FR. 74 9" IAW A300-600 SRM 53-17-16 P101 PARA 3, FOUND TO BE OUT OF LIMITS ORG. .655" MATERIAL LOSS .444" IAW SRM53-10-16, P103, CUT OUT DAMAGED AREA ON TRACK IAW SRM53-10-16 TAB 01 P5, FAB SEAT TRACK FROM 60-22457/7075-T6-54 P.O. 11-102657 IAW SRM 53-10-16, REPROTECTED SEAT TRACK AND SPLICES IAW SRM 51-75-10, INSTALLED SEAT TRACK IAW SRM53-10-16, P209-214, APPLIED CIC TO NEW SEAT TRACK AND SPLICES IAW AMM 51-22-00, P2 FRAME 73 TO FRAME 74 10".
FLOORBEAM IN CARGO BAY AT FRAME 67 AND 6 INCHES LT OF CTR AREA, CORRODED 2 SQ IN. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-74-10, AREA IS OUT OF LIMITS IAW SRM 53-10-15, FIG 100 SH2. 100 PERCENT MAT LOSS, 2"X 2 X .125. R & R WITH NEW FLOORBEAM IAW SRM 51-72-10 PARA 5A & 6A. REPROTECTED FLOORBEAM & FASTENER IAW SRM 51-75-10, PG 206.
SEAT TRACK NR 4 LT HAS 2 GOUGES UP CROWN BETWEEN FR 60-61. SMOOTHED & BLENDED GOUGED AREAS IAW SRM 53-17-16, PG 101, PARA 103. ORIGINAL MATERIAL .655 HOLE DIA NOW 1.0. REMOVED .345" FOUND TO BE OUT OF LIMITS REMOVED SEAT TRACK IAW SRM 53-10-16, ALODINED, PRIMED AND PAINTED IAW 51-21-10 & 51-75-10. INSTALLED SEAT TRACK & SPLICES IAW SRM 53-10-16. CIC SEAT TRACK AND SPLICES IAW AMM 53-10-16.
NR 1 PYLON OTBD VERTICAL STIFFENER ON FWD FACE OF RIB 20 HAS GOUGE L.3 X D.1. R & R NR1 PYLON OTBD VERTICAL STIFFENER ON FWD FACE OF RIB 20 WITH NEW PART IAW SRM 51-41-21, PG 22 AND PARA 13.
MAIN DECK CARGO TRACK NR 2 LT CORRODED AT FR 18, 12" UP SIDE. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 103. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. REPROTECTED FASTENERS IAW SRM 51-75-10. APPLIED CIC TO SEAT TRACK IAW 51-72-10.
MAIN DECK CARGO NR 3 LEFT SEAT TRACK HAS SPOTS OF CORROSION FROM FR 15B TO 19. FOUND TO BE OUT LIMITS IAW SRM 53-10-16. REMOVED & REPLACED SEAT TRACK IAW SRM 51-72-10 PARA 5A REPROTECTED FASTNERS IAW SRM 51-75-10 APPLIED CIC IAW AMM 51-75-10-8.
FWD CARGO FLOOR PANEL 132QF DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J.
FWD AREA FLOORBOARD 221PF CRACKED LT SIDE 22 IN. APPROX ALSO 2 EA LONG SCRATCHES UP SKIN REF AMM 53-10-15-06 FABRICATED REPLACEMENT FLOORBOARD 221PF IAW DWG SRZ25-005 REV J, MAJOR REPAIR IAW GMM 6-2-100.
FLOORBOARD 151CF HAS 4 DISCREPANCY 1.AND2. GOUGES AT END CORNERS OF BOARD.3. CORNER OF BOARD BY SCREW HOLE IS BROKEN 4. SIDE OF FLOORBOARD HAS FILLING COMING OUT FABRICATED REPLACEMENT PANEL 151CF IAW DWG SRZ25-005 REVJ IDENTIFIED REPLACEMENT FLOORBOARD IAW GMM7-0-1001
FLOORBOARD 151GF HAS 5 DISCREPANCY 1. CORNER HAS FILLING COMING OUT. FASTENER HOLE ON BOTTOM SIDE HAS FILLING BREAKING OFF. CORNER IS BROKEN, HAS 2" CUT INBD. GOUGE ON END OF BOARD. FABRICATED REPLACEMENT FLOORBOARD 151GF IAW DWG SRZ25-005 REV J, IDENTIFIED REPLACEMENT FLOORBOARD IAW GMM7-0-1001 MAJOR REPAIR IAW GMM6-2-100.
FWD MACC FLOORBOARD 231KG BROKEN AT LOWER SURFACE APPROX W=4"X2=4" REF AMM 53-10-16-06 FABBED FLOORBOARD 231KG IAW DWG SRZ25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.
MLG W/W FLOOR PANEL 147EF WET AND DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL 147EF MLG WHEEL WELL IAW DWG SRZ 25-005, REV J.
SEAT TRACK NR 2 RT CORRODED AT FR 16. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK IAW SRM 51-72-10.
RT WING NR 2 FLAP TRACK CARRIAGE AFT OTBD YOKE ROLLER DAMAGED. R & R NR 2 FLAP TRACK CARRIAGE AFT OTBD YOKE ROLLER IAW AMM 20-21-12.
SEAT TRACK NR 5 LT Y1959 BETWEEN FRAMES 59 TO 60 MISREPAIRED. R & R COMPLETE SEAT TRACK ASSY FROM FR 58 TO 62 IAW SRM 51-72-10, PG 1 TO 3 AND DWG A53274786.
FLOORBOARD 252DH HAS A CRACK ALL ACROSS BOTTOM SIDE 12" LONG AMM 53-10-16-06 FABRICATED REPLACEMENT PANEL 252DH IAW DWG SRZ25-005 REV J, MAJOR REPAIR IAW GMM 6-2-100.
FWD CARGO BAY STRINGER 46R CORRODED AT FR 38.2 PLUS 10. REPAIRED STRINGER IAW SRM 53-10-14 FIG 201 PGS 205/206.
FLOORBOARD 162EF METAL SKIN DISBONDED AND 1 EA INSERT PULLED THRU FABRICATED NEW FLOORBOARD IAW DWG SRZ-25-005 AND SRZ-25-011.
FLOORBOARD 151FF HAS SEVERAL CRACKS AND DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.
FLOORBOARD 147CF OIL SOAKED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ-25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.
FLOOR PANEL 151HF HAS AN 18" CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 22-005, REV J.
FLOOR PANEL 162DF CRUSHED AND DELAMINATED ON UPPER SURFACE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
FLOOR PANEL 131RF HAS 8 SQ INCHES OF DELAMINATION AND CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
FLOOR PANEL 143DF IS OIL SOAKED 25 PERCENT OF PANEL. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
FLOOR PANEL 131JG HAS 3EA DELAMINATED CORNERS AND 1EA CRACK 1" LONG AND 4 SQ IN OF DELAMINATION ON UPPER SURFACE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
FLOOR PANEL 132JG HAS 2 CRACKS 8" AND 10" FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.
FLOORBOARD 143CF IS OIL SOAKED AROUND EDGES, FABRICATED FLOORBOARD IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.
FLOORBOARD 151LF HAS DELAMINATED CORNER AND EDGE OF PANEL 6" FABRICATED FLOORBOARD IAW DWG SRZ 25-005 MAJOR REPAIR IAW GMM 6-2-100.
FLOORBOARD 132HG HAS 2 FT OF DELAMATION ON EDGE. FARICATED REPLACEMENT FLOORBOARD IAW SRZ-25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.
FLOOR PANEL 131ZF SEVERAL CRACKS AND DAMAGE ON PANEL FLOOR BOARD 131 ZF. FABRICATED NEW FLOOR PANEL IAW DWG SR25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.
FLOOR PANEL 131HG HAS EDGE DAMAGE AND SEVERAL CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.
FLOOR PANEL 132ZF CRACKED IN HALF, FABRICATED REPLACEMENT FLOOR PANEL 132 ZF IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.
FLOOR PANEL 132RF HAS DELAMINATED EDGE 8FT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J IDENTIFIED. MAJOR REPAIR IAW GMM 6-2-100.
FLOOR PANEL 251YG HAS 2 EA CRACKS AT CLS CUT OUT 4" AND 1". FABRICATED REPLACEMENT FLOOR PANEL IAW SR25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.
FLOORBOARD 151BF HAS 12" OF EDGE DELAMINATION. FABRICATED REPLACEMENT FLOORBOARD 151BF IAW DWG SRZ 25-005 REV J MAJOR REPAIR IAW GMM 6-2-100
AFT CARGO COMPARTMENT FLOORBEAM TEE CORRODED UNDERNEATH 1R ROLLER TRACK AT FR 62R. REPLACED TEE IAW SRM 51-40-24.
FWD CARGO COMPARTMENT CUT-OUT AFT SIDE FR 26 GOUGED AT EDGE BETWEEN STR 36 R- 37R, BLENDED AND SMOOTHED GOUGE AT FWD CARGO COMPARTMENT CUT-OUT BETWEEN STR 36R AND 37R AT FR 26R IAW SRM 51-73-10, MECHANICALLY MEASURE MAT LOSS ON EDGE .020" FOUND TO BE WITHIN LIMIT IAW SRM 53-13-12, TOP COATED BLENDED AREA IAW SRM 51-75-10.
T/O MEM HOT BRAKES AFTER LANDING CLT BRAKE TEMPS EXCEEDED 600 (MAX TEMP 630). ACFT STOPPED OUTSIDE GATE AND CHECK BY FIRE CREW. TIRE NR 7 & 8 HOTEST WITH 1 FLAT. R & R NR7 AND NR8 TIRE IAW MM 12-37-32-0. R & R NR8 BRAKE IAW MM 32-42-27-4. BLEED NR7 AND NR8 BRAKES IAW 32-42-00 AND 32-43-00.C/W BRAKE OVERTEMP INSP IAW 05-51-16-00.
CHECKED FUEL GAUGES. 2900 NR SPLIT BETWEEN LT INNER AND RT INNER (4.42 L VS 1.9 R) DIFFERENCE INCREASED RAPIDLY TO 2800 NR WITHIN 2 MINUTES. DECLARED EMERGENCY FOR POSSIBLE FUEL LEAK AND DIVERTED. OPEN XFEED TO MAINTAIN FUEL BALANCE. TOTAL BURN IN 35 MINUTES OF FLIGHT WAS 10,600 LBS. TANK COMP AND PROBE CAP/RESISTANCE READINGS WITHIN LIMITS. REPLACED FUEL QTY COMPUTER PER MOCC REQUEST AND PERF A SUCCESSFUL OPS TEST PER MM 28-42-38. THE FUEL QTY COMPUTER IS QUALIFIED FOR FURTHER SERVICE.
ON GEAR RETRACTION, HAD LANDING GEAR NOT UP AND LOCKED INDICATION ON FWD PANEL AND OVERHEAD PANEL. RETURNED TO DEPARTURE AND LANDED. FOUND UNIVERSAL BINDING AND UPLOCK FREE FALL RETURN SPRING TENSION WEAK. REMOVED AND REPLACED RT MAIN GEAR UPLOCK ACTUATOR AND FREE FALL UNIVERSAL SHAFT IAW MM 32-31-44-4 AND OPS CHECKED IAW MM 32-33-00-5 AND 32-31-00-5 LEAK CHECK GOOD. FINAL CLOSED
AFTER TAKEOFF, RT MLG DOOR LIGHT REMAINED ON. PUT MLG DOWN, RETURNED TO PIT. RELEASED FOR SERVICE IAW MEL: 32-61-01-C CATEGORY: B EXPIRATION: 28APR10 "MEL 32-61-01-C: RT MLG DOOR INDICATORS SYS NR 1 - INOP." TESTED RT MLG DOOR IAW MM 21-31-00-5 GROUND OPENING TEST. CK GOOD. INSPECTED DOOR & SWITCHES CHECK GOOD. NO BUFFETING NOTED BY CREW, NO UPPER INDICATIONS NOTED BY CREW, NO 99 DAY HISTORY. INSTALLED RT DOOR SEQUENCE VALVE IAW 32-31-37-4 LEAK TEST GOOD FOR VALVE AND RESTRICTOR, RT LG DOOR STILL WILL NOT STAY LATCHED WHEN HYD OFF REF WRI 32-30-3231 ITEM IS NOW BEING WORKED UNDER THIS WRI DUE TO SECOND AIR TURN BACK AND RT MLG REPEAT WRITE-UP. AWAITING TDR RESULTS.
DURING ACFT POLISH OF LOWER FUSELAGE BELLY FOUND 1 EA DENT WITH FILLER BELOW FWD CARGO ENTRY DOOR BETWEEN FR 23 AND FR 24,R/H STRINGER 43 AND 44. AFTER REMOVAL OF DENT FILLER DENT MEASURED OUT OF LIMITS IAW A300 -600 FRIEGHTER SRM 53-13-12,FIG 103. CUT OUT DAMAGED AND INSTALLED EXTERNAL SKIN REPAIR DOUBLER AT FWD LOWER CARGO DOOR ENTRY BETWEEN FR 23 AND FR 24 AND STRINGERS 43 AND 44 IAW A300-600 FRIEGHTER SRM 53-10-12,FIG 210,PAGE 307/308 AND REF SRI 53-10-12-2-004-00.
ECAM GAVE BLUE HYD RES LOW QTY. FOLLOWED ECAM AND TURNED OFF BLUE HYD PUMP. CHECKED QRH RED TABS MISC SECTION FOR GUIDANCE. CONT TO KLAX. A/C DIVERTED FROM SNA TO LAX. FOUND BLUE SYSTEM SERVO CONTROL PRESSURE SWITCH 17CB O-RING PINCHED/LEAKING. REMOVED AND REPLACED O-RING PER M/M 27-14-18-4. OPS AND LEAK CHECK GOOD. SERVICED BLUE SYSTEM RESERVOIR PER M/M 12-12-29.
LEFT ECAM INDICATED GREEN SYS HYD RESVR LO LEVEL ON DESCENT. GREEN SYS HYD OVERHEAD PANEL GAUGE INDICATED BOTTOM OF YELLOW ARC. RT ECAM HYD POINTER INDICATED BOTTOM OF YELLOW ARC. AFTER COMPLETING HYD RSVR LO LEVEL PROC AND L/G GRAVITY EXT PROC, GREEN SYS QUANTITY RETURNED TO NORMAL. SERVICED GREEN SYSTEM HYDRAULICS PER FEDEX A300-600 M/M 12-12-29-0. PRESSURIZED SYSTEM NO LEAKS NOTED. RAN ENGINES PER FEDEX A300 JRH CHAP 5. DURING RUN EXERCISED ALL FLT CONTROLS NO LEAKS FOUND, HYD QTY AND PRESS OPS CHECKED GOOD. RESTORED LANDING GEAR TO NORMAL OPERATING CONDITION PER A300-600 M/M 32-33-00-5 AND EA 6-3231-71640.
EDGE MARGIN TO SHORT FOR TEMPORARY REPAIR ON RIB 5 IAW DR 426 REPAIR PERFORMED BY INSTALLATION ADDITIONAL FASTENER IAW EA 6-5710-108975 AND RAS/BAE/1004080/2006 A.
MISDRILLED HOLE AT FRAME 13A DURING ACCOMPLISHMENT OF DR 179. REPAIR PERFORMED BY REAM UP AND COLD WORKING IAW EA 6-5312-106395 A AND RAS/AS/010/2007 ISS. C
CRACKS IN SEALING ANGLE AND AFT SPLICE, RT, FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-5002 PART 4 REPAIR PERFORMED BY SEALING ANGLE REPLACEMENT IAW DRAWING R571-50404, APPROVED BY EO 5-5710-7-5002.
FOUND CORROSION FINDING ON RT WING OUTER SHROUD BOX RIB 25-29 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS. A.
CRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5710-7-3305 REV C1, SB A300-57-6050 REV 3-AD 2005-23-08 REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW EA 6-5710-106435 AND RAS/049856/032/2007 ISS. A
CRACK AND BEND ON LT SIDE OF THE CENTER SPAR REINFORCING ANGLE REPAIR PERFORMED BY TRIM OUT IAW EA 6-5511-106378 AND RAS/CASA/5355/2007 ISS A.
FOUND CORROSION FINDINGS ON RT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS.A.
CORROSION SPOTS ON OUTER SHROUD BOX AND TOP SKIN REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. A
CORROSION AND CRACK FINDINGS DURING SEALING ANGLE INSTALLATION- EO 6-5710-7-5002- SB A300-57-6033 REV 1- SBA300-57-6027 REV 6- AD 98-18-02 AND AD 2006-07-07 REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106433 AND RAS/BAE/1004205/2007 ISS. A.
DAMAGE ON SPOILER NR 4 LT REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY EA 6-5770-106440 REV A AND RAS/DABRE/7007420/2007 ISS. A
CORROSION AND CRACK FINDINGS IN HOLES DURING SEALING ANGLES INSTALLATION-EO 6-5710-7-5002-SB A300-57-6033 REV 01-SB A300-57-6-27 REV 6- AD98-18-02 AND AD 2006-07-07. REPAIR PERFORMED BY REAM UP AND SEALING ANGLE REPLACEMENT IAW EA 6-5720-106433 AND RAS/BAE/1004205/2007 ISS.A
CRACK WAS FOUND ON MLG RIB 5 RT WING INTERIM REPAIR PERFORMED IAW, DRAWING R572-40265 AND APPROVED BY EA 6-5710-108975 AND RAS/BAE/1004080/2006 ISS.A
CORROSION SPOTS ON LT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. A.
CORROSION ON AFT BEAM (RIB 8) OF PYLON NR 1, REPAIR WAS PERFORMED BY OVERSIZING IAW EA 6-5451-106439 AND RAS/050001/005/2007 ISS.A
FUSELAGE NOSE SECTION, CORROSION ON FWD PAX DOOR FRAME AREA C14 UPPER CORNER LT, GUSSET A536-11511-204. REPAIR PERFORMED BY REPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.B.
FUSELAGE NOSE SECTION-CORROSION ON FWD PAX DOOR FRAME AREA, RT LOWER CORNER, GUSSET A536-11517-205 REPAIR PERFORMED BY REPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.B
CRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017-SB A300-53-6123 REV 2-AD2004-20-14, ON SPLICE FITTING C47 LT REPAIR WAS PERFORMED BY REPLACEMENT OF SPLICE FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS /033769/043/2004 ISS.A
CRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017, SB A300-53-6123 REV 2, AD2004-20-14, SPLICE FITTING C47 RT REPAIR PERFORMED BY REPLACEMENT OF FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS/033769/043/2004 ISS.A,
OLD TOOLING MARK ON COVER PLATE AT DOOR NR 4 RT. REPAIR PERFORMED BY REWORK AND HFEC INSPECTION IAW EA6-5318-106393 AND RAS/DAHAM/4021668/2006 ISSUE "A".
FOUND CORROSION ON RUDDER HINGE FITTINGS NR 5, NR 6 AND NR7 (A554-71605-200, A554-71606-200, A554-71617-000) CORROSION REWORK AND HFEC INSPECTION IAW EA 6-5546-106387, APPROVED BY RAS/DAHAM/4021625/2006 ISSUE "B".
TORSION BOX COVER PLATE MARKS AT EMERGENCY EXIT DOOR RT. REWORK WAS PERFORMED BY BLEND OUT, HFEC INSPECTION AND FLAP PEENING IAW EA 6-5316-106394 AND RAS/DATLS/0003542/2006 ISSUE "A".
CORROSION ON FUSELAGE UPPER SKIN PANEL C78-85, P4RH AND P7 LT REPAIR WAS PERFORMED BY REWORK IN SMOOTH CONTOUR AND FLAP PEENING IAW EA 6-5319-106398 AND RAS/DAHAM/4021681/2006 ISS. B
REPAIR DEFORMATION AND TOOL MARKS ON C74 OUTER FLANGE AT P26 LT AND RT REPAIR WAS PERFORMED BY REWORK TO SMOOTH CONTOUR ON THE OUTER FLANGE IAW EA 6-5318-106420 AND RAS/DATLS/0003545/2007 ISS. A
OLD GRINDING MARK AT INTERNAL DOUBLER, C70-71, P48-49 LHS REPAIR WAS PERFORMED BY BLEND OUT THE DAMAGE IAW EA 6-5317-106396 AND RAS/DAHAM/ 4021674/2006 ISS. A.
CRACK FINDINGS IN ANGLE (HOLE 11, 13, 42, 45, 160, 180, 191, ALL LT SIDE) DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, SB A300-57-6050 REV.03, AD 2005-23-08 REPAIR WAS PERFORMED BY REAM OUT, OVERSIZING AND COLD WORKING IAW EA 6-5710-106435 AND RAS/049856/032/2007 ISS. A
CORROSION ON SILL BEAM C59-63A, RT REPAIR WAS PERFORMED BY CUT OUT AT C60 AND C63 IAW SRM 53-17-18 AND REWORK AT SILL BEAM EDGE IAW EA 6-5317-106399 AND RAS/DAHAM/4021663/2006 ISS. A
PYLON SUPPORT BRACKET AND BOTTOM WING SKIN (LT WING), ELONGATED HOLES REPAIR WAS PERFORMED IAW DRAWING R571-50532 REV A, APPROVED BY EA 6-5720-106407 AND RAS/BAE/1004134/2007 ISS A.
BOTTOM SKIN REWORK CAUSED BY CORROSION AT RIB 8, P19, RT OUTER WING REPAIR WAS PERFORMED IAW EA 6-5721-106402 AND RAS/BAE/1004132/2007 ISS A (BLEND OUT CORROSION, FASTENER REPLACEMENT.
LT WING TIP, CORROSION UNDER ONE STATIC DISCHARGER AND CRACK ON NAVIGATION LIGHT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5730-106400 AND RAS/FOK/004/2007 ISSUE "A".
FOLDING NOSE LT INTERNAL RIB CRACKED. REPAIR WAS PERFORMED IAW EA 6-5710-106358 AND SB A300-57-6067.
ELONGATED HOLES IN PYLON SUPPORT BRACKET AND BOTTOM SKIN, RT WING. REPAIR PERFORMED IAW AI-INSTRUCTION: R571-50532 ISSUE "A" AND EA 6-5720-106407.
FOUND CORROSION ON CROSSBEAMS C56 AND C58. PARTS REPLACED IAW SRM 71-52-10.
SOME PARTS IN KRUEGER FLAP AREA AT FWD FAIRING HEAVY CORRODED, PARTS REPLACED IAW SRM 57-45-11, KEEL BEAM PN A535-10215-201, BRACKET A535-10219-201 AND FITTING A535-10561-201.
FOUND CLIP AT FRAME 22 AD HEAVY CORRODED. NEW PART INSTALLED IAW SRM 51-72-10.
FOUND CORROSION INSIDE OF FORK ON RUDDER HINGE FITTING NR 5, NR 6 AND NR 7. REPAIR WAS PERFORMED IAW EA 6-5546-106387 INCLUDES REPAIR REF.: TD/K4/S1/21625/2006/A AND IS APPROVED BY RAS/DAHAM/4021625/2008 ISS B.
CORROSION AT ATTACHMENT HOLES ON SILL BEAM BETWEEN C25 AND 25A AT FWD CARGO DOOR. REPAIR WAS PERFORMED IAW TD/K7/S1/07372/2006 ISS A AND EA 6-5313-106401 AND IS APPROVED BY RAS/DABRE/7007372/2006 ISS A.
FOUND CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR WAS PERFORMED IAW SRM 53-13-13, FIG 204, SHEET 1, 2.
FOUND CORROSION AROUND TWO FASTENERS BETWEEN RIB 7-8 AT STRINGER 19 ON RT WING BOTTOM SKIN. REPAIR WAS PERFORMED IAW EA 6-5721-106402, APPROVED BY RAS/BAE/1004132/2007.
FOUND CORROSION ON CROSSBEAM C67 RT. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 207.
FOUND CORROSION ON FLOOR SUPPORT STRUCTURE IN SEC 12. THE AFFECTED PARTS ARE SHOWN IN SRM 53-12-15 FIG.19, SHEET 3: ITEM 190,200 AND 275. REPAIR WAS PERFORMED IAW SRM 53-12-15, FIG 207 (ITEM 190 / 200) AND BY REPLACE A NEW PART IAW SRM 51-72-10 (ITEM 275).
OLD GRINDING MARK BETWEEN C70-71, P48-49 LT. REPAIR WAS PERFORMED IAW TD/K4/S1/21674/2006 ISS A, APPROVED BY RAS/DAHAM/4021674/2006 ISS A.
FOUND CORROSION AT C54, TRACK 5, LT AND RT REPAIR WAS PERFORMED IAW EA 6-5315-106393 AND RAS/049222/.008/2006 ISS A, LT INSTALL FITTING P/N A538-13311, RT INSTALL COUNTRSINK BUSH.
FOUND CORROSION ON SKIN PANEL BETWEEN C77-87, P3-6 RT AND C78-86, P3-6 LT. REPAIR PERFORMED BY REMOVE CORROSION IAW SRM51-74-10, SRM 53-19-12/FIG 1.
TWO OVERSIZED AND DAMAGED HOLES ON THE END OF THE LONGITUDINAL BEAM AT THE LOWER SIDE ON BULK CARGO DOOR NEAR TO C67 BETWEEN STRINGER P`45 / P`47 RT. REPAIR WAS PERFORMED BY REPLACE A NEW BEAM (A539-73100-200-51) IAW SRM 51-72-10, FIG 8, SHEET 8.
CORRODED BRACKET UNDER PRESSURE MEMBRANE AT TRACK 5 LT C54. CORRODED HOLE AFTER COUNTERSINK OF PRESSURE MEMBRANE AT TRACK 5 RT, C54. REPAIR WAS PERFORMED BY INSTALLING FITTING P/N A538-13311-201-EF ON LHS AND INSTALLING A COUNTERSUNK BUSH IN THE AFFECTED HOLE ON RHS WITH REINSTALLING NOMINAL FASTENER. REPAIR IS APPROVED BY RAS 049222/008/2006 ISSUE A AND EA 6-5315-106392.
OLD REPAIR ON LT INBOARD FLAP ON TOP SKIN CLOSE TO TRACK 2 RIB 7. REPAIR WAS PERFORMED IAW RAS/FOK/064/2003 ISSUE B.
OLD REPAIR ON TOP CAP BEAM AT C62 LT. REPAIR WAS RENEWED IAW SRM 53-10-15, FIG 207.
OLD REPAIR ON RT INBOARD FLAP AT LOWER AND UPPER SKIN BETWEEN RIB 12/14 TRAILING EDGE (PATCH REPAIR). REPAIR WAS PERFORMED IAW RAS/FOK/060/2003 ISSUE A.
OLD REPAIR ON LT/RT OUTBOARD WING TIP UNDERNEATH STATIC DISCHARGER. REPAIR WAS PERFORMED IAW RAS/FOK/247/2000 ISSUE B.
OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE AT C89, P39-42. REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 215.
OLD DENT REPAIR ON FWD CARGO DOOR SURROUNDING PANEL, C23, P 44 RT DAMAGE ARE ACCEPTABLE IAW RAS/DABRE/00688/ 2000 ISS.B
FWD RIGHT PAX DOOR FAIL/SAFE RING CORRODED IN FWD UPPER CORNER. REPAIR WAS PERFORMED IAW RAS/AS/103/2003 (REWORK OF CORROSION, INSTALLATION OF NEW FASTENERS).
OLD FLUSH REPAIR DOUBLER ON FUSELAGE AT C76/77, P26/27 LT. REPAIR WAS PERFORMED IAW RAS-DA/HAM 1207/96 ISSUE B AND IS APPROVED BY EA 6-5318-106345.
CORRODED CROSS BEAM AT C57.2 LT / AD AND C61 RT/AD. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 208 AT CROSSBEAM 57.2 AND IAW SRM 53-10-15, FIG 207 AT CROSSBEAM C61.
CORROSION ON STRINGER P56 LT BETWEEN C70 AND C71. REPAIR ON STRINGER P56 LT WAS PERFORMED IAW SRM 53-10-14, FIG 201.