N680FE
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
EXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY.
EXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51-FR52,Y0~- Y450 REQUIRES EVALUATION FOR CONFORMITY.
EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45,Y1456 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53832020(ISSUE: J00), NO RECORD FOUND. EO: 6-5100-7- 5000 D07 PART1 WAS COMPLETED. THE REPAIR IS CATEGORY "A" AND CLASSIFIED AS MAJOR PER GMM6-2-100. MAJOR REPAIR IAW FEDEX GMM6-2-100.
EXISTING REPAIR ON MAIN DECK CROSSBEAM FR20,Y1959~Y2462 REQUIRES EVALUATION FOR CONFORMITY.
EXISTING REPAIR ON MAIN DECK CROSSBEAM FR38,Y0~Y953 REQUIRES EVALUATION FOR CONFORMITY.
EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,-Y1959 REQUIRES EVALUATION FOR CONFORMITY.
EXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 REQUIRES EVALUATION FOR CONFORMITY.
L1 DOOR EJECTOR BAG RELEASE CABLE/INFLATOR ACTUATING ARM CLIP HAD IMPROPER BREAKAWAY COPPER WIRE INSTALLED. INSTALLED CORRECT CAD PLATED BREAK AWAY WIRE MS20995CY AS PER CMM AND E.A. LISTED ABOVE FOR THE L1 DOOR SLIDE SERIAL NUMBER 0443TH EJECTOR BAG RELEASE CABLE. EA: 6-2560-F0386375 REV A PT1 EA: 9-2560-T0386431 CMM: 25-60-40 INSTALLED CORRECT CAD PLATED BREAK AWAY WIRE MS20995CY AS PER CMM AND E.A. LISTED ABOVE FOR THE L1 DOOR SLIDE SERIAL NUMBER 0443TH EJECTOR BAG RELEASE CABLE.
ON POSTFLIGHT INSPECTION FOUND EMERGENCY LIGHTING TEST INOP. REMOVED AND INSTALLED NEW POWER SUPPLY UNIT AS REQUIRED. OPS CHECKED GOOD.
CORROSION FOUND BETWEEN BUSHES 'D" AND "E" DURING RH RIB 5 INSPECTION COMPLIED WITH FED EX EA 6-571-T0316490 PT2 AND R57240425. MAJOR REPAIR. EA 6-5710- T0316490 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG RH. MPN A57240810214.
DISCREPANCY BETWEEN AIRSPEED ON CAPT & FO. AT CRUISE .02 MACH & ABOUT 8-10 KNOT DISCREPANCY AT FL 340. ALSO RECEIVED A MOMENTARY OVERSPEED WARNING AT FL 340 IN SMOOTH AIR, CAPT SHOWED .80 MACH & FO SHOWED .82. FO AIRSPEED SEEMS CLOSER TO STDBY AIRSPEED ON BOTH SIDES. AMM 34-11-15-06 DURING DEBRIEF CAPT REPORTS OVRSPD DURATION OF APROX 4 SECS, SUSPECTED ERROR WAS WITH CAPTS IND DUE TO FOS MATCHING STDBY. POST DEBRIEF INSPECTED PITOT PROBES & DISCOVERED FOREIGN MATERIAL JAMMED IN CAPTS PITOT PROBE. AMM 34-11-15-06 REMOVED FOD FROM CAPTS PITOT TUBE IAW AMM 34-11-15-06 INSPECTED FO & STDBY PROBE NO DEFECTS NOTED. INSTALLED CAPTS PITOT PROBE, ALL OPS &LEAK CHECKS GOOD.
DURING CLIMB RECEIVED FO PITOT HEAT FAULT. COMPLIED WITH ECAM. ENTERED ICING CONDITIONS. RECEIVED NI MODE 1 AND MODE 2 FAULT. UNRELIABLE AIRSPEED. DETERMINED DURING LEVEL FLIGHT THAT IT WAS ON THE FO S SIDE. DESCENDED TO GET OUT OF THE ICING CONDITIONS. LOST AUTOPILOTS, ATS AND YAW DAMPENER #2. WAS ABLE TO RECOVER AUTOPILOT #1 AND YAW DAMPER. ATS DID NOT RESET. C/W PROBE ICE PROTECTION ADJ/TEST CAPT. STBY PROBES HEAT AS REQUIRED WHILE F/O PROBE BARLEY WARM CHECKED PROBE CONNECTOR PLUG I.5 FULL TURN INSPECT FOR DAMAGE REINSTALLED PLUG AS REQUIRED OPS CHECK WAS GOOD. AS PER BITE TEST FOR 54GB HAD A FAULT CODE OF 01/28 . BAD BOX REMOVED AND REPLACED PROXIMITY ELECTRONIC UNIT AND BITE TESTED. ALL SYSTEMS NO FAULTS IAW AMM.
MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR AREA PER A300- 600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100
MAIN DECK FR47 Y953-Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y953-Y1456 UNDERFLOOR AREA PER A300- 600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100
MAIN DECK FR47 Y0-Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y0-Y450 UNDERFLOOR AREA PER A300-600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100
MDIS 680 27-50 1704 27FEB23 DEN OPEN U THE #7 TIRE THROWN TREAD AND DAMAGED THE R/H INBOARD FLAP. SEE ATTACHMENTS TIRE R&R ON WRI 34-42/1703 TIRE R&R'D DAMAGE WRI'S 53-30/1710, 1714 53-40/1708, 1709,1711 53-50/1706 1707,1712,
MDIS 680 33-50 0976 07MAY22 PIT OPEN U PER A-CHECK, EMERGENCY LIGHT OPS TEST FAILED BITE-CHECK. DUPLICATE SDR SEE 22-1140
MDIS 680 33-50 0976 07MAY22 PIT OPEN U PER A-CHECK, EMERGENCY LIGHT OPS TEST FAILED BITE-CHECK. FACT 10MAY22 23:37 TUL REPLACED BURNED OUT BULBS IN DOOR EXIT SIGNS, (3 IN THE R1 AND 2 L1 SIGN) AND PERFORMED OPS CHECKS IAW A300-600 AMM 33-51-00-05. OPS CHECK IS NORMAL. ALL OTHER BULBS ARE WORKING AT THIS TIME.
REMOVE LOBE DAMAGED SEAT TRACK (AT LS Y1995 TRACK) FROM SPLICE CENTER BETWEEN FR26/FR27 TO FR33/FR34 0000392279 : ORTEN, JONATHAN C - 30-AUG-2021 18:25 REPLACED SEAT TRACK SECTION REFERENCE A300-310 SRM 51-14-16---------- 0000638304 : LONEY, RANDOLPH C - 30-AUG-2021 18:27 .
1 EA CORROSION INDICATION WAS FOUND ON THE HOLE "N" OF RH FRAME 47. ACCOMPLISHED THE TASK I.A.W A300-600F EA WORK CARD NO:T6-5710-T0362495 P1, SEQ NO:001066
RH WING L/E KRUEGER BOX O/B SIDE RIB NEAR PNEUMATIC DUCT AREA GOT A GOUGE REINFORCED WITH A REPAIR ANGLE I.A.W A300-600F EA WORK CARD NO: T6-5710-T0362830 P1, SEQ NO:001065
1EA CRACK INDICATION WAS FOUND ON THE HOLE "J" OF FR47,STR24L-STR25L. THE CRACK INDICATION IS OVER 100%FSH. ACCOMPLISHED THE WORK:FR47,STR24L-STR25L HOLE ''J'' GOUGE REPAIR - THIS EA DEVIATES FROM EO 6-5310-7-5017 (AIRBUS SERVICE BULLETIN ) I.A.W. A300-600F EA NO: T6-5310 - T0344789 B P3, SEQ NO: 001056.
THE #242EF FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
THE #242GJ FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
1EA CRACK INDICATION WAS FOUND ON THE HOLE "N" OF FR47 SPLICE FITTING BETWEEN STR24&26,LH. THE CRACK INDICATION IS OVER 100%FSH. ACCOMPLISHED THE WORK CARD:INSPECTION HOLES IN FUSELAGE FRAME47 SPLICE FITTING BETWEEN STR24&26,LH/RH, AIRBUS SB A300-53-6123 I.A.W A300-600F WORK CARD NO:E6-5310- 7- 5017 O PT5 SEQ O:001045
THE #241WH FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
THE #241AK FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
THE #151VF LOOR PANEL OF LOWER AFT CARGO COMPARTMENT WAS FOUND EDGE 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.
THE #151XF LOOR PANEL OF LOWER AFT CARGO COMPARTMENT WAS FOUND EDGE 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.
THE #132NG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND EDGE 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.
THE #132MG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND EDGE 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.
THE #231CF FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
THE #242NH FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
1EA CRACK (12MM) WAS FOUND AT R/H WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK: RH CENTER FLAP CRACK IN UPPER FLANGE OF RIB 27 AT STRINGERS 2.8 - ALI 575306-01(FAA AD 2019-21-01) I.A.W. A300-600 EA NO: 6-5750-T0362465 P1 SEQ NO: 001055.
NO 1 PYLON AFT FAIRING SUPPORT WEB GOT CHAFING AT RIB 19 O/B ACCOMPLISHED LH PYLON AFT FAIRING SPAR AT RIB 19 OUTBOARD FLANGE WEAR DAMAGE REPAIR INSTRUCTION I.A.W EA: #6-5450-T0362605 P1, SEQ NO: 001050
2EA DELAMINATIONS WERE FOUND. AREA 1 (20CM2) IS NEAR I/B HINGE ARM OF RH SPOILER 4 LOWER SKIN. AREA 2 (17.5CM2) IS NEAR O/B HINGE ARM OF RH SPOILER 4 LOWER SKIN. ACCOMPLISHED RH #4 SPOILER LOWER SKIN DELAMINATION REPLACEMENT OF REINFORCEMENT PLIES NEAR CENTER HINGE ARM WORK INSTRUCTION IAW EA NO: 6-6750- T0362608 P1.
RH WING #2 SPOILER O/B EDGE FWD SECTION WORN ACCOMPLISHED THE TASK I.A.W A300-600F EA WORK CARD NO: T6-5750-T0362676 P1 ,SEQ NO:001059.
#1 ENG LH CORE COWL INNER LAST FRAME WAS FOUND CRACK ACCOMPLISHED THE HAT FRAME REPAIR I.A.W. GOODRICH GE CF6-80C2 A5F CMM 71-13-31 REPAIR NO.1, P. 6001-6003.
SEAT TRACK ADAPTER AT 3L ID C840 HAS LOBE DAMAGE, RESTRAINT REMOVED, SEE WRI 25-50/8938. NO OTHER DAMAGE NOTED. INSTALLED SEAT TRACK ADAPTER REF DWG A53781936.
SEAT TRACK ADAPTER AT 3L ID C840 HAS LOBE DAMAGE, RESTRAINT REMOVED, SEE WRI 25-50/8938. NO OTHER DAMAGE NOTED.
ON APPROACH, LT SIDE BRAKE PRESURE GAGE READS 500 LBS. RIGHT SIDE 0 LBS. DECLARED EMERGENCY IN CASE LT BRAKE WAS STICKING. LT YELLOW SYSTEM BRAKE PRESURE INDICATOR. PARKING BRAKE ACCUM LOW, WHILE ATEMPTING TO SERVICE FLUID WAS COMING OUT OF SERVICE PORT. FOUND LOW PRESSURE AT YELLOW SYS BRAKE ACCUMULATOR INDICATOR. OPENED SERVICE VALVE, FOUND HYDRAULIC FLUID ON NITROGEN SIDE OF ACCUMULATOR. R&R UPPER & LOWER YELLOW BRAKE SYS ACCUMULATOERS IAW AMM 32-44-11-04 AND PERFORMED SAT OPS CHK & LEAK CHK. PERFORMED ALT BRAKING W/ANTISKID SERVICING IAW AMM 32-43-00-03-0. REQUIRES FURTHER TROUBLESHOOTING PER MOCC. PER MOCC NORMAL BRAKING. ADJUSTMENT/TEST PERFORMED AND OPS CK NORMAL PER AMM 32-42-00-05.
MCD ADAPTER FR58 L/H DAMAGED. REMOVED AND INSTALLED NEW ADAPTER IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
MCD FLOOR ADAPTER FR59 LT DAMAGED. REMOVED AND INSTALLED NEW ADAPTER FR59 IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
FLOOR PANEL 231PG FWD PIT IS DAMAGED. REPAIRED BY FABBED FLOOR PANEL 132PG ON T19/1388837 IAW SRZ-25-005, CAT A AND MAJOR REPAIR.
(DOT 38-23) MDC SEAT TRACK CORRODED FR 60 TO FR 61 -Y450. REMOVED DAMAGE SECTION FROM SEAT TRACK -Y450 AT FRAME 58-61.10 RT SIDE ON MDC, FABRICATED REPAIR SEAT TRACK SPLICE PER SRM 51-10-16, INSTALLED REPAIR SEAT TRACK SPLICE AT SEAT TRACK -Y450 FROM FRAME 58-61.10 RT SIDE IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
MCD FLOOR PANEL 251NH BROKEN. FABBED FLOOR PANEL 251NH ON TR#19/1390031 IAW SRZ 25-005 REV P INSTALLED ON W/C 250- FL-FIT, REPAIR CAT A AND MAJOR REPAIR.
MCD FLOOR PANEL 231VG BROKEN. FABBED FLOOR PANEL 231VG ON TR# 19/1390024 IAW SRZ 25-005 REV P, INSTALLED ON W/C E6-5321-E0339394B P6, REPAIR CAT A, MAJOR REPAIR.
FLOOR PANEL 131QG FWD PIT IS DAMAGED. REPAIRED BY FABBED FLOOR PANEL 131QG ON T19/1388841 IAW SRZ-25-005, CAT A AND MAJOR REPAIR.
MDCC BET FR59 ANF FR60 AT Y "0" SEAT TRACK HAS NICKS, GOUGES AND SCRATCHES. 91-053 REMOVED DAMAGE SECTION FROM SEAT TRACK Y 0 AT FRAME 58-50 LT SIDE ON MDCC AND FABRICATED REPAIR SEAT TRACK SPLICES PER SRM SRM 51-10-16, INSTALLED REPAIR SEAT TRACK SPLICES FROM FRAME 58-60 AT SEAT TRACK Y 0 IN MDCC IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
MCD ADAPTER FR 57.3 LT DAMAGED. REMOVED AND REPLACED MDCC ADAPTER FR 57.3 LT IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
MCD FLOOR PANEL 251RG BROKEN. FABBED FLOOR PANEL 251RG ON T19/1388406 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 261AH BROKEN. FABBED FLOOR PANEL 261AH ON T19/1388407 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241NJ BROKEN. FABBED FLOOR PANEL 241NJ ON T19/1388518 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 252TH BROKEN. FABBED FLOOR PANEL 242BH ON T19/1388517 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241KJ BROKEN. FABBED FLOOR PANEL 241KJ ON T19/1388409 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241RJ BROKEN. FABRICATED FLOOR PANEL 241RJ ON T19/1388408 IAW SRZ-25-005. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241VJ BROKEN. FABBED FLOOR PANEL 241VJ ON T19/1388410 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 262TF BROKEN. FABBED FLOOR PANEL 262 TF ON T19/1388404 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241DK BROKEN. FABBED FLOOR PANEL 241DK ON T19/1388405 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241MJ BROKEN. FABBED FLOOR PANEL 241MJ ON T19/1388519 IAW SRZ-25-005 REV. P REPAIR CLASSIFIED AS A CAT "A" MAJOR REPAIR.
MCD FLOOR PANEL 241SF BROKEN. FABBED FLOOR PANEL 241SF ON TR#T19/1388520 IAW SRZ-25-005 REV P. PANEL INSTALLED ON W/C 240-FL-FIT, REPAIR CAT A AND MAJOR REPAIR.
COURIER AREA FLOOR PANEL 221QF DELAMINATED FABRICATED FLOOR PANEL 221QF ON T19/1388833 IAW DWG SRZ25-05 CLASSIFIED AS A CAT "A" MAJOR REPAIR.
COURIER FLOOR PANEL 222QF DELAMINATED AND GOUGED FABRICATED COURIER FLOOR PANEL 222QF ON 19/1388826 IAW DWG SRZ-25-005 CLASSIFED AS A CAT "A" MAJOR REPAIR.
COURIER FLOOR PANEL 221LF DELAMINATED FABRICATED COURIER FLOOR PANEL 221LF ON 19/1388821 IAW DWG SRZ-25-005 CLASSIFED AS A CAT "A" MAJOR REPAIR.
MDIS 680 53-21 7368 24OCT18 MEM OPEN U SEAT TRACK LUG DAMAGE IN MAIN DECK CARGO COMPT 4LEFT. FACT 22NOV18 18:41 LAX TERMINATING ACTION ACCOMPLISHED FOR SRD-25-008 AT 28,057:19 HOUR(S), 15,629 CYCLE(S) INSTALLED DAMAGED SEAT TRACK ADAPTER. AT STA. 4L (C38) PER SRM 53-16-15-001-3 INSTALLED FLOOR PANEL 241PF AT STA. 4L. PER AMM 53-10-23-04. INSTALLED ANCRA P/N 86182 CARGO HANDELING SYSTEM AT STA. 4L PER AMM: 25_58_07_02_02. OK FOR SERVICE.
ON GRND A/C LIGHTNING STRIKE. ALL SYSTEMS INOP, APU NOT AVAILABLE, EXT POWER NOT AVAILABLE. AIRPLANE NEEDS INSPECTION PRIOR TO FLIGHT. MULTIPLE SYSTEM FAILURE. LIGHTNING STRIKE INSPECTION PER AMM 05-51-18-00. 52KA SWITCH BODY SWAPPED WITH 52KD SWITCH BODY IAW ESPM 20-45-11 AND DIODE MODULE 87VD R&R. MFA TEST PERFORMED IAW AMM 33-17-00-05, ALL TEST GOOD. STAND-BY PITOT PROBE 42DA R&R IAW AMM 34-11-15-04, TEST OK. TCC R&R IAW AMM 22-36-34-04-01, AFS/LAND TEST C/O IAW AMM 22-40-00-05, LAND ENGAGE OK. R&R GPCU PER AMM 24-41-11-04, TEST OK. MDC SMOKE DETECTION CONTROL UNIT AFT 50WU3 R&R IAW AMM 26-19-34-04, TEST OK. APU ECB R&R IAW AMM 49-61-11-04, TESTED SERVICEABLE. ALL AFFECTED SYSTEMS TESTED OK.
NO AIRSPEED F/O PFD 21C WIND 250/7. FOUND F/O PITOT TUBE BLOCKED BY PIECE OF PAPER, REMOVED BLOCKAGE. R&R PRECAUTIONARY ADC NR 2 PER AMM 34-11-34-04. ADC NR 2 BITE TEST OK.
CAPTAINâS SIDE WINDSHIELD SHATTERED DURING CRUISE AT FL 310. FOLLOWED QRH LANDED WITHOUT INCIDENT. THE WINDSHEILD WAS REPLACED IAW MM 56-11-11-04 AND CHECKED GOOD.
AFTER TAKEOFF, RECEIVED GREEN HYDRAULIC LOW PRESSURE ON THE NR 1 GREEN PUMP. AUTO BRAKE FAILED AND A LANDING GEAR MESSAGE ILLUMINATED. THE GREEN HYDRAULIC SYSTEM INDICATOR BEGAN DECLINING. DECLARED AN EMERGENCY AND RETURNED FOR LANDING. THE GREEN HYDRAULIC DECREASED TO THE TOP OF THE YELLOW BAND. ONCE ON FINAL, AND GEAR DOWN THE GREEN HYDRAULIC SYSTEM LEVEL INCREASED TO BELOW THE TOP HAT. INSPECTED ACFT FOR HYD LEAKS, NO LEAKS FOUND. RAN BOTH ENGINES IAW JRH, NO FAULTS FOUND, NR 1 ENGINE GREEN PUMP OPS NORMAL AND NR 2 ENGINE GREEN PUMP OPS NORMAL. NO AUTO BRAKE OR LANDING GEAR FAULTS SHOWN. GREEN HYD SYS AT NORMAL LEVEL. MAINT PANEL SHOWS ALL OPEN FOR ALL ENGINE DRIVEN PUMPS, RAN BIT TEST OF BSCU, NO FAULTS FOUND IAW MM 32-42-00-05. ACFT OK FOR SERVICE.
AT 400 FT AFL, ON APPROACH, LOST THE GREEN HYD SYSTEM. REMOVED AND REPLACED RIGID HYD LINE ON THE RT MLG IAW MM 29-00-00-04, LEAK CHECKED NORMAL.
SEAT TRACK FRAMES 54 TO 54.2 OUT OF LIMITS. REPAIRED THE SEAT TRACK IAW SRM 53-15-16 FIG 201.
AFT CARGO BAY FLOOR PANEL 152UF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005.
LEFT CENTER TE FLAPS UPPER SURFACE HAD FOUR GOUGES APPROX 0.45 EACH. SMOOTHED AND BLENDED GOUGES, REMOVED DAMAGE. FABRICATED REPAIR AND INSTALLED IAW SRM 57-50-00. MAJOR REPAIR
LEFT NR 5 DUMMY SEAT TRACK FRAME 54 TO 54.2 OUT OF LIMITS. REPAIRED LT 5 DUMMY SEAT TRACK FRAME 54 TO FRAME 54.2 IAW SRM 53-15-16, FIG 201. FABRICATED INSERT ON T16/1225696 IAW SRM 53-15-16. MACHINED DUMMY TRACK ON T16/1225679 IAW SRM 53-15-16. MAJOR REPAIR.
FWD CARGO FLOOR PANEL 131QG BROKEN AND DAMAGED. THE FLOOR PANEL WAS FABRICATED.
AFT CARGO FLOOR PANEL 151QF CRACKED. THE FLOOR PANEL WAS FABRICATED.
RIGHT NR 4 SEAT TRACK FRAMES 54 TO 54.2 OUT OF LIMITS. REMOVED, REPAIRED, AND RE-INSTALLED THE SEAT TRACK IAW SRM 51- 40-21, AND SRM 53-15-16 FIG. 201. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 241ZJ CRACKED. FABRICATED A NEW FLOOR PANEL. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 262AH HAS CRACK. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
BULK CARGO FLOOR PANEL 161GF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR
RT NR 5 DUMMY SEAT TRACK FRAMES 54 TO 54.2 OUT OF LIMITS. REMOVED AND REPLACED THE DUMMY TRACK IAW SRM 51-40-21. REPAIRED IAW SRM 53-15-16 FIG 201. MAJOR REPAIR.
RIGHT NR 3 DUMMY SEAT TRACK FRAMES 54 TO 54.2 OUT OF LIMITS. REMOVED AND RE-INSTALLED THE SEAT TRACK IAW SRM 51-40-21.
MAIN CABIN FLOOR PANEL 232AH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DRAWING SRZ-25-005 REV M. MAJOR REPAIR.
MAIN CABIN CARGO FLOOR PANEL 242AJ HAS DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
AGING REPAIR ASSESSMENT: RIGHT HORIZONTAL STABILIZER L/E PANEL 341AB FOUND HOLE ELONGATED. COMPLY WITH ATTACHMENT-B OF EO 6-5100-7-5000, PART 1. COMPLIED WITH ATTACHMENT-B OF EO 6-5100-7-5000 P1 INSPECTION OF REPAIR, DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA EA 6-5510-150443. THE REPAIR IS CLASSIFIED AS A MAJOR CATEGORY-A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIRED.
MAIN DECK FLOOR PANEL 242DF DAMAGED FABRICATED FLOOR PANEL 242DF ON T16/1225111 IAW SRZ 25-005. MAJOR REPAIR.
DELAMINATION, CRACK ON FLOOR PANEL 242AK IN MD CARGO COMPARTMENT FRAME 47, RT SIDE, DOT 139-010. FABRICATED PANEL 242AK ON T16/1225628 IAW SRZ 25-005. MAJOR REPAIR.
NR 1 ENGINE FORWARD PYRAMID MOUNT INBD AFT HOLE HAS A SIGN OF CORROSION AND HAS GOUGE ON TOP 91-097. REMOVED CORROSION IAW SRM 51-74-10 & GOUGE IAW SRM 51-73-10. BORE DIAMETER AFTER REMOVAL IS 0.964", FOUND TO BE WITHIN REPAIRABLE LIMITS IAW SRM 54-51-81, FIG 202, CAD PLATED AREA IAW SRM 54-51-81 FIG 104 AND SRM 51-21-10. FABRICATED BUSHING ON T16/1226376. INSTALLED BUSHING IAW SRM 54-51-81. CLASSIFIED AS MAJOR CAT-B, REPAIR SRI 54-51-81-2-001-00.
FORWARD CARGO FLOOR PANEL 131KG BROKEN DAMAGED. PANEL RACK, FABRICATED FLOOR PANEL 131KG ON T16/1225127 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.
FWD CARGO FLOOR PANEL 132KG BROKEN, DAMAGED. PANEL RACK, FABRICATED FLOOR PANEL 132KG ON T16/1225128 IAW SRZ 25-005, CAT-A. MAJOR REPAIR.
AFT CARGO FLOOR PANEL 152PF CRACKED. FABRICATED FLOOR PANEL 152PF ON T16/1225224 IAW SRZ 25-005, CAT A. MAJOR REPAIR.
AFT CARGO FLOOR PANEL 152RF CRACKED. FABRICATED FLOOR PANEL 152RF ON T16/1225120 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.
FORWARD CARGO FLOOR PANEL 132SG BROKEN, DAMAGED. FABRICATED FLOOR PANEL 132SG ON T16/1225126 IAW SRZ 25-005 CAT-A. MAJOR REPAIR.
AFT CARGO FLOOR PANEL 151WF CRACKED. FABRICATED FLOOR PANEL 151WF ON T16/1225119 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.
AFT CARGO FLOOR PANEL 152WF CRACKED. FABRICATED FLOOR PANEL 152WF ON T16/1225384 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.
AFT CARGO FLOOR PANEL 151PF CRACKED. FABRICATED FLOOR PANEL 151PF ON T16/1225376 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.
AFT CARGO FLOOR PANEL 151MF CRACKED. FABRICATED FLOOR PANEL 151MF ON T16/1225374 IAW SRZ 25-005, CAT-A MAJOR REPAIR.
AFT CARGO FLOOR PANEL 152VF CRACKED. FABRICATED FLOOR PANEL 152VF ON T16/1225401 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.
MDCC FLOOR PANEL 241TH PUNCTURED, CRACKED 91-078. FABRICATED PANEL 241TH ON T16/1225470 IAW SRZ-25-005. MAJOR REPAIR.
COURIER FLOOR PANEL 221GF DENTED WITH CRACKED IN MULTIPLE AREAS. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.
COURIER FLOOR PANEL 222NF DELAMINATED AND HAS A DAMAGED INSERT. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.
MAIN CARGO FLOOR PANEL 251GF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
MAIN CARGO DECK PANEL 242QH DAMAGED. FABRICATED FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 242KF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 251BF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005.
MAIN CARGO DECK FLOOR PANEL 252RG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
MAIN CARGO DECK FLOOR PANEL 252XF HAS DELAMINATION ON BOTTOM. FABRICATED A NEW FLOOR PANEL. MAJOR REPAIR.
MAIN CARGO DECK PANEL 241NJ HAS CRACK. FABRICATED A NEW FLOOR FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
MAIN CABIN FLOOR PANEL 232WG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DRAWING SRZ-25-005 REV M. MAJOR REPAIR.
MAIN DECK CARGO FLOOR PANEL 252NH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.
WHEN FLYING ILS 26L, AT 3000 MSL & ON INTERCEPT HEADING TO FINAL, WHILE SLOWING FROM 170 KIAS TO 160, FLAPS STUCK AT 15. RECYCLED HANDLE & FLAPS STAYED STUCK AT 15. SLATS WORKED NORMALLY, LANDED WITH FLAPS 15. CHECKED FLAP TORQUE INDICATORS, NOT SET. CHECKED SFCC'S, BOTH SHOWED SFCC FAILURE ON 1 & 2. RESET SFCC'S, CYCLED FLAPS WITH NO FAULTS IAW AMM 27-51-00-05. SUSPECT TRANSIENT CAUSED BOTH SFCC FAULTS. OK FOR SERVICE.
RIGHT MLG FWD LUG HAS CORROSION ON FWD FACE & IN BORE. COMPLIED WITH EA 6-5710-T0316490 REV NO POS P1. WINGS, BASIC WING STRUCTURE CORROSION REPAIR OF RIB 5 FWD LUG. MAJOR REPAIR.
LEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & BOTH FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0313802 WINGS BASIC WING STRUCTURE TERMINATING ACTION OF MLG SUPPORT RIB 5 FWD LUG LT. MAJOR REPAIR.
ONE CRACK 5/8 INCH, WAS FOUND AT FRAME 12A RT FITTING AREA. R & R FITTING IAW EO 6-5340-7-5002 PT8. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
FOUND FRAME 12A RT FITTING CRACKED 5/8 INCH. R & R FITTING IAW EO 6-5340-7- 5002 PT 7.
FORWARD MAIN DECK UTILITY AREA FOUND ONE ATTACHED ANGLE CRACKED. CUT OUT DAMAGED ATTACH ANGLE. FABRICATED REPLACEMENT SECTION OF ANGLE AND REPAIR SPLICE ANGLE. INSTALLED REPAIR WET WITH SEALANT IAW EA 6-5310-T0308363. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LOWER FUSELAGE EXTERNAL SKIN SCRATCHED, LOCATION BETWEEN FRAME 66 & 67 FROM STRING 49 RT TO 52 RT. DURING PRELIMINARY INSPECTION WAS FOUND, BLEND OUT THE SCRATCHED ARE & MEASURE THE MAX DEPTH 0.036"X2.7"X1.7" DXLXW OVER ALLOWABLE LIMIT IAW AB6F SRM 53-17-12 & 53-10-12 DIAGRAM 101. DRILL OUT AFFECTED FASTENERS & CUT OUT THE DAMAGE SKIN LXW=2.7"X1.75". COMPLIED WITH AB6F SRM 53-10-12 PARAGRAPH 11. FABRICATED THE DOUBLER & INSTALL THE DOUBLER WITH RIVETS BY SEALANTS. COMPLIED WITH IIR 53-10-12-2-002-00 TABLE 205C.
ON CLIMBOUT, RECEIVED ECAM ADV FOR PACK 2 AT 95 DEGREES & CLIMBING. PACK NR 2 MODE SELECTED TO MAN AND MODUALATED VALVE POSITION TO KEEP PACK FROM OVERHEATING. COULD NOT GET COCKPIT TEMP BELOW 96 DEGREES AND RISING. R & R FAN BYPASS CHECK VALVE IAW AMM 21-61-00. RAN ENGINE IAW JRH WITH NO DEFECTS IN CABIN TEMP NOTED. OPS CHECKED GOOD.
LANDING GEAR AIR GROUND POSITION DISAGREE AT ROTATION, SWITCHED TO POSITION NR 2. CREW DEBRIEF INDICATES THAT FAULT WAS ECAM ALERT - FLT/GND DISAG. FURTHER DEBRIEF INDICATES THAT FAULT CLEARED WHEN L/G POS NR 2 WAS SELECTED.
MAIN DECK FLOOR PANEL 242MF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 241PF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
BULK CARGO COMPARTMENT FLOOR PANEL 162EF LOWER SURFACE FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-35 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-011 REVISION E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
CARGO BAY FLOOR PANEL 162HF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-35 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-011 REVISION E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 241JF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
COCKPIT FLOOR PANEL NR 211HF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-21 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SR30-53-005. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL NR 242KF FOUND DELAMINATED. MAIN DECK FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REV. 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 114.
RIGHT HORIZ STABILIZER L/E PANEL NR 341AB FOUND HOLE ELONGATED. REPAIRED IAW EA 6-5510-150443 PART1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 114.
MAIN DECK SEAT TRACK AT FRAME 54 TO FRAME 54.2 LT NR 5 FOUND DIMENSION "B". GAP VALUE EXCEEDED LIMITS. REPAIRED IAW SRM 53-15-16 FIGURE 201 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 241LK FOUND BROKEN. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 251XG FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 241QH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL NR 241QH FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 251VF FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 241GF FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED AS PER DWG SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 241BF FOUND DELAMINATED. MAIN DECK FLOOR PANEL R & R IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 231YG FOUND DELAMINATED. MAIN DECK FLOOR PANEL 231YG FOUND DELAMINATION. FLOOR PANEL R & R IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 242SF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK SEAT TRACK AT FRAME 54 - 54.2, LEFT NR 3 FOUND CRACKED AT CROWN AREA. DAMAGED SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 241GJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 242BF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 242UJ FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 242QJ FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 242ZJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 232YG FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23, REV 52.2. NEW FLOOR PANEL 232YG FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 242GF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 241WH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 241AJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 241TH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CABIN FLOOR PANEL 242RG FOUND DAMAGED. FLOOR PANEL R & R IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 242EK FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
CABIN FLOOR PANEL 242VG FOUND DAMAGED. FLOOR PANEL R & R IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
AFT CARGO BAY FLOOR PANEL NR 151TF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-33 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.
MAIN DECK FLOOR PANEL 252PH FOUND DELAMINATED. R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132QG FOUND DAMAGED. R & R IAW AMM 53-10-29, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO COMPARTMENT FLOOR PANEL 131SG FOUND DAMAGED. R & R IAW AMM 53-10-29, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132SG FOUND DAMAGED. R & R IAW AMM 53-10-29, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR PANEL 252VF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL 252GF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK FLOOR PANEL NR 252UH FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV. J. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.
AFT CARGO BAY FLOOR PANEL NR 152TF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-33 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REV. J. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.
AFT CARGO BAY FLOOR PANEL NR 152QF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-33 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.
FORWARD CARGO BAY FLOOR PANEL NR 131LG FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-29 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ -25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.
FORWARD CARGO BAY FLOOR PANEL NR 132RG FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-29 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
FORWARD CARGO BAY FLOOR PANEL NR 131PG FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-29 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
FORWARD CARGO COMPARTMENT FLOOR PANEL NR 132MG FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-29 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
AFT CARGO BAY FLOOR PANEL NR 151XF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-33 REV.52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ -25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.
MAIN DECK SEAT TRACK AT FR54/FR54.2 LT NR 6 FOUND "A" GAP VALUE AS 0.08 INCH. REWORKED PER SRM 53-15-16 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK SEAT TRACK AT FR38.2/FR40 LT NR 5 FOUND "A" GAP VALUE AS 0.06 INCH. REPAIRED PER SRM 53-15-16 FIGURE 201 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.
MAIN DECK SEAT TRACK AT FR38.2 - 40 RT NR 2 FOUND "A" GAP VALUE AS 0.06 INCH. REPAIRED IAW SRM 53-15-16 FIGURE 201 REVISION 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.
MAIN DECK SEAT TRACK AT ABOUT FR15A -Y953 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-10, REV 21. MATERIAL REMOVED 0.071", ORIGINAL MATERIAL THICKNESS 0.120", MATERIAL REMAIN 0.049" AND FOUND OUT OF LIMITS IAW SRM 53-10-16, FIG 102, REV 21. SEAT TRACK, R & R IAW SRM 51-40-21, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOOR SUPPORT STRUCTURE AT ABOUT FR12, Y730 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-10, REV 21. MATERIAL REMOVED 0.057", ORIGINAL MATERIAL THICKNESS 0.071", MATERIAL REMAIN 0.014" AND FOUND OUT OF LIMITS IAW SRM 53-10-16, FIG 102, REV 21. FLOOR SUPPORT R & R IAW SRM 51-40-21, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK AT FRAME 47, S13L, FOUND GOUGED. REPAIRED IAW EA 6-5310-150436. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.
MAIN DECK AT FRAME 47 S13R FOUND GOUGED. REPAIRED IAW EA 6-5310-150437. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOORBEAM AT FR 31, RBL 27 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, FIG 211, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK FLOORBEAM AT FR 58, RBL 27, FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, FIG 211, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
ON TAKEOFF ROLL, NR 1 ENGINE NEVER WENT PAST 80 PERCENT. RTO WAS AT 80KTS. OMA R BITE CHECK FADEC, REF TSM, NO FAULTS NOTED. INSPECTED BURNER BYPASS LINE, NO LEAKS NOTED. INSPECTED AND CHANGED FUEL FILTER REF MM. R & R FUEL PUMP AND HMU. LEAK CHECK GOOD. RAN ENGINES IAW ALL PARAMETERS NORMAL - NO LEAKS FOUND. PREFORMED POWER ASSURANCE RUN.
DURING CLIMB OUT AT ABOUT FL270 ECAM GAVE US A ENG 2 OVERLIMIT FOLLOWED BY VIBRATION BAD ENOUGH AND ENG WINDING DOWN THAT WE HAD TO SHUT ENG DOWN, FOLLOWED QRH PROCEDURE FOR ENG FAIL. FOUND PIECES IN TAILPIPE. SUSPECT DAMAGED ENGINE. THE ENGINE IS APPROVED FOR REMOVAL.
RT WING SKIN LWR SURFACE; PYLON AFT FAIRING SUPPORT IS CRACKED BETWEEN RIB 7 AND RIB 8. REMOVED HYD LINES AND FITTINGS IAW AMM 54-54-00-4. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21, PARA 7. REINSTALLED HYD LINES AND FITTINGS IAW AMM 54-54-00-4 (TWS8312A AND T83421). LEAK CHECK GOOD AFTER ENGINE RUN IAW AMM 71-00-00-5.
LT WING BOTTOM SKIN LWR SURFACE; PYLON AFT FAIRING SUPPORT BRACKET IS CRACKED AROUND THE FASTENER BETWEEN RIBS 7 AND 8. REMOVED HYD LINES AND UNIONS IAW AMM 20-23-12-0 AND AMM 54- 54-00-4. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21, PARA 7 AND SRM 51-72-10, PG 2. REINSTALLED HYD LINES AND UNIONS IAW AMM 20- 23-12-0 AND AMM 54-54-00-4. LEAK CHECK GOOD AFTER ENGINE RUN IAW AMM 71-00-00-5. (E7739C AND T8342D).
NR 2 PYLON "Y" DUCT HEAT SHIELD IS CRACKED AT THE LR FLANGE. REMOVED AND INSTALLED HEAT SHIELD IAW SRM 51-40-21. MATERIAL ID 2024-T3 IAW SRM 51-70-10; PG 102. ALODINED AMD PRIMED DOUBLER IAW SRM 51-40-2; PARA 6. STOPPED DRILLED IAW SRM 51-70-10; PG 102.
AFT CARGO DOOR CUTOUT ; THE AFT SEAL DEPRESSOR IS CRACKED AT FRAME 65. REMOVED AFT DOOR CUTOUT, AFT SEAL DEPRESSOR AT FRAME 65 AND REPLACED IAW SRM 51-40-21; PARA 5. REMOVED AND INSTALLED PANEL 162 IAW AMM 25-56-11-2. FABBED SEAL DEPRESSOR ON NR N00530.
INBD RAIL ON THE BATTERY RACK IS CRACKED AT THE CTR SUPPORT. REMOVED SUPPORT TUBE IAW SRM 51-72-10; PARA 5 AND 6. LOCATED; DRILLED AND DEBURRED NEW TUBE IAW SRM 51-72-10; PARA 5 AND 6 AND SRM 51-40-44.; PARA 2. INSTALLED TUBE IAW SRM 51-72-10; PARA 5 AND 6 AND SRM 51-40-44.; PARA 2.
RT WING T/E ATTACH ANGLE HAS A GOUGE ON THE OTBD END; LWR SURFACE UNDER PANEL 572 PB. CHECKED DAMAGE AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-51-11; FIG 102; ORIGINAL THICKNESS IS 0.048; REMAINING THICKNESS IS 0.015. CUT OUT DAMAGE IN REF SRM 57-51-11; FIG 207. FABRICATED REPAIR ANGLE AND FILLER IN REF TO SRM 57-51-11; FIG 207. ALODINED ; PRIMED AND PAINTED IN REF AMM 51-23-10-0. INSTALLED THE REPAIR IN REF TO SRM 57-51-11; FIG 207.
AVIONICS COMPARTMENT; THE BATTERY RACK CTR SUPPORT IS CRACKED AT THE INBD RAIL. REMOVED AND REPLACED CRACKED SUPPORT TUBE IAW SRM 51-72-10 AND 51-40-44. REINSTALLED SHIP'S BATTERY IN REF TO AMM 24-31-11-4. PERFORMED GOOD OPS CHECK IN REF TO AMM 34- 31-00; BLOCK 501. INSTALLED NEW O-RING ON FRONT VENT DUCT COUPLING IN REF TO AMM 24-31-11-4.
MAIN CABIN SEAT TRACK SCALLOP IS WORN AT BS 3710 - BS 3715; LBL Y45 - LBL Y45. BLENDED DAMAGED AREA. MINIMUM ALLOWABLE MATERIAL .26. REMAINING MATERIAL .245 AND BEYOND ALLOWABLE LIMITS IAW SRM 53-10-16, FIG 102. REMOVED FLOOR PANELS 251 LG;PG; BF;GF;NH AND PH IAW AMM 53-10-25-4. REMOVED SECTION OF SEAT TRACK FROM FR 57.05 TO FR 58 IAW SRM 53-10-16. LOCATED AND DRILLED HOLES IN NEW SEAT TRACK SECTION PN A53274005000053, PO NR 662246.1 AND SPLICES PN A5327049020000, PO NR 661818.4. INSTALLED NEW SECTION OF SEAT TRACK AND SPLIVES IAW SRM 53-10-16. INSTALLED FLOOR PANELS 251 LG;PG;BF;GF;NH AND PH IAW AMM 53-10-25-4.
MAIN CABIN ADAPTER TRACK IS WORN AT FS 2029; RBL-Y 700 TO -Y 900. REMOVED ADAPTER CHECKED AND EVALUATED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; PG 105. REPLACED WITH A NEW ADAPTER IAW SRM 51-40-12 AND SRM 51-72-10; PG 1; PARA 4-6.
MAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS PUNCTURED AND CRUSHED FROM FRAME 51 TO FRAME 54. REMOVED DAMAGED FLOOR PANEL 242 EK. FABRICATED NEW FLOOR PANEL 242 EK, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.
MAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 4140 - BS 4120; LBL Y 440 - LBL Y 440. CHECKED DAMAGED SCALLOP 0.170 REMAINING. SCALLOP WORN BEYOND MINIMUM ALLOWABLE LIMITS OF 0.260 IAW SRM 53-10-16, PG 105. REMOVED SEAT TRACK SECTION IAW SRM 53-10-156, PG 204. REINSTALLED FLOORBOARDS 251 VFP; WG AND TH IAW AMM 53-10-23-4.
MAIN CABIN SEAT TRACK IS GOUGED AT BS 4360 - BS 4360; LBL Y 1400 - LBL Y 1410. CHECKED GOUGED AREA, SCALLOP WORN BEYOND MINIMUM ALLOWABLE LIMIT OF .26. .21 REMAINING OUT OF LIMITS IAW SRM 53-10-16; PG 105. REMOVED FLOOR PANELS (251AH; BH;YG AND XG) FOR ACCESS IAW AMM 53-10-23-4. REMOVED DAMAGED SEAT TRACK AND DRILLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM ; FIG 201; PGS 204; 207 AND 208. INSTALLED NEW SEAT TRACK AND SPLICES IAW SRM 53-10-16; FIG 201. INSTALLED FLOOR PANELS (251 AH; BH; YG AND XG) IAW AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 SF IS PUNCTURED AND CRUSHED FROM FRAME 38.2 TO FRAME 40. REMOVED PANEL 242 SF AMM 53-10-23-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV "H". PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL REF AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 MF IS PUNCTURED AND CRUSHED FROM FRAME 37 TO FRAME 38.2. REMOVED PANEL 242 MF REF AMM 53-10-23-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV "H". PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 GF IS PUNCTURED AND CRUSHED FROM FRAME 34 TO FRAME 37. REMOVED PANEL (242 GF) AMM 53-10-23-4. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 BF IS PUNCTURED AND CRUSHED FROM FRAME 31 TO FRAME 34. REMOVED PANEL 242 BF REF AMM 53-10-23-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV "H". PART MARKED PANEL IAW GMM 7-0-1000. INSTALLED PANEL REF AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 232 YG IS PUNCTURED AND CRUSHED FROM FRAME 28 TO FRAME 30. REMOVED PANEL (232 YG) AMM 53-10-23-4. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 TH IS PUNCTURED AND CRUSHED FROM FRAME 40 TO FRAME 43. FABRICATED NEW FLOOR PANEL 241TH IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 QJ IS PUNCTURED AND CRUSHED FROM FRAME 40 TO FRAME 43. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 242 UJ IS PUNCTURED AND CRUSHED FROM FRAME 43 TO FRAME 47. REMOVED DAMAGED FLOOR PANEL 242 UJ. FABRICATED NEW FLOOR PANEL 242 UJ, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.
MAIN CABIN FLOORBOARD 241 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.
MAIN CABIN FLOORBOARD 242 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. LOCATED FASTENER HOLES AND PREPED EDGE FOR POTTING IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000.
MAIN CABIN FLOORBOARD 242 ZJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.
MAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 PH IS PUNCTURED AND CRUSHED FROM FRAME 58 TO FRAME 60. DAMAGED FLOOR PANEL 252 PH REMOVED. NEW PANEL 252 PH FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".
MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL (252 UH) REMOVED. NEW PANEL (252 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".
MAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL REMOVED. NEW PANEL (251 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".
MAIN CABIN SEAT TRACK SCALLOP IS BROKEN BETWEEN FR 63 AND FR 64; RT BUTTLINE 37 INCHES FROM CTR. REMOVED DAMAGED AREA REF SRM 71-73-10, PARA F. MATERIAL LOSS ALLOWED 0.016. MATERIAL REMOVED 0.155; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; PG 105. INSTALLED REPAIR SECTION OF SEAT TRACK IAW 53-10-16; 204-208. APPLIED CIC IN THE AREA IAW AMM 51-22-0-0. REINSTALLED FLOORBOARDS 252 XG AND VF IAW AMM 53-10-25-4.
UNABLE TO RETRACT GEAR IN EITHER SYS 1 OR SYS 2. PERFOMED BIT CHECK ON PROX BOX, GOT CODES P1, P2, 90, BL. REMOVED CLEANED AND LUBED BOGIE BEAM PIVOT PIN AND REINSTALLED. REPLACED PITCH DAMPNER. PERFORMED MLG SWING, OPS CHECKS NORMAL ALL INDICATIONS NORMAL. REF MM 32-11-15 AND 32-11-14.
LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. TRIED SYS 1 AND SYS 2. SERVICED BOTH LANDING GEAR PITCH DAMPERS FOUND WITH LOW PRESSURE AND REPLACED LANDING GEAR PROX BOX AS PRECAUTION.
APPROX 1 HOUR OF FLIGHT NR 1 OIL QUANTITY STARTED TO DECREASE. ALL OTHER INDICATIONS NORMAL. AFTER APPROX 2 HOURS OF FLIGHT THE OIL PRESSURE STARTED TO FLUCTUATE PLUS OR MINUS 15 PSI. PER QRH THIS COULD BE ABNORMAL, DIVERTED TO KDEN. ENGINE NR 1 LEFT AT IDLE, NO SHUTDOWN. NO EMERGENCY DECLARED. OIL LEAKING FROM NR 1 STARTER DRIVE PAD AS PER AMM 71-70-00-6-05 CAPPED STARTER DRIVE PAD DRAIN AND STOWED CLOSED AND SECURED COWLING AS PER AMM 71-13-00. A/C LIMITED TO 10 CYCLES. REMOVED AND REPLACED STARTER DRIVE PAD CARBON AND MAGNETIC SEAL REF A300-600 MM 72-65-00-8-05. REINSTALLED STARTER REF A300 MM 80-13-01-4-05.
ON TAXI OUT, NR 1 AFT SMOKE FAULT LIGHT ILLUMINATED. TURNED OFF PER PROCEDURE. ON TAKEOFF, AFT SMOKE LIGHT ILLUMINATED. NR 2 MID SMOKE LIGHT ILLUMINATED ON LANDING ROLL. CONFIMED BOTH MID 2 AND AFT ON MX PANEL AND CONTROL UNITS ARE HARD FAULTS. REMOVED AND REPLACED 5 DETECTORS, AND BOTH COALESCER BAGS. SYSTEM CHECKS GOOD.
REJECTED TAKEOFF - AIRCRAFT NI WENT TO MAX POWER (TOGA) THOUGH FLEX POWER SELECTED ENT BY: 097576 RPT BY: 097023 THIS ITEM WAS CLEARED WITH THE R&R OF THE T.C.C. PER A-300-600 M/M 22-36-34-4-01, AND OPS CHECK OF THE AUTOTHROTTLE SYSTEM PER A-300-600 M/M 22-30-00-5 -01. SEE PREVIOUS UPDATE FOR ORIGINAL SIGNOFF OF THE DEFERAL AND THE PART CHANGED.
WITH POWER SET ON TAKEOFF NR 2 ENGINE N2 ANALOG INDICATION SHOWED APPROXIMATELY 20 LESS THAN THE DIGITAL INDICATION. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 ENG N2 GAUGE PER AIRBUS M/M 77-12-21-4, OPS CHECKED PER ENG RUN PER JRH. NORMAL INDICATIONS FOLLOWED.
T/O PLUS 1 HR, DURING DESCENT TO FL240, GOT ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY. GAGE AND ECAM SCHEMATIC SHOWED QUANTITY AT THE RED DOT LEVEL. TURNED OFF GREEN PUMPS, MANUALLY EXTENDED THE GEAR, UTILIZED THE ALTERNATE BRAKE SYSTEM AND LANDED AT MSY. AFTER GEAR WAS MANUALLY LOWERED, QUANTITY SHOWED JUST BELOW TOP HAT. PERFORMED A VISUAL INSPECTION OF THE A/C TO DETERMINE IF ANY EVIDENCE OF HYDRAULIC FLUID LEAKAGE IS PRESENT, NONE FOUND. SERVICED GREEN SYSTEM RESERVOIR PER MM 12-12-29-0. RESTORED LANDING GEAR SYSTEM TO NORMAL CONDITION AFTER LANDING GEAR FREEFALL PER MM 32-33-00-2. RAN ENGINES 1 & 2 PER JRH AND OPERATED ALL FLIGHT CONTROLS THROUGH THE FULL RANGE OF MOTION.
DURING CLIMBOUT FLAPS WOULD NOT RETRACT. R&R NR 1 & 2 SFCC PER MM 27-51-18.4.
AFTER T/O GEAR DOOR IND UNSAFE SYS 1 & 2 FWD AND OVERHEAD PANEL, LOWERED GEAR IND SAFE, NOSE DOOR STILL SHOW UNSAFE.
NR 1 ENG AGENT NR 2 DISCHARGE LIGHT CAME ON IN FLT. REMOVED AND REPLACED NR 1 ENG OVERHEAD FIRE SHUTOFF PNL. RECHECK GOOD. OPS CK PER A300 AMM 26-12-20-4.