N837UA
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES INC | Operator | 2025-02-02 – 2025-02-02 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2025-02-02 – 2025-02-02 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CABIN RE-CIRCULATION FILTERS NEEDS TO BE REPLACE WITHIN 2 DAYS REF LOG# 8508734 CABIN RE-CIRCULATION FILTERS TO BE REPLACEWITHIN 2 DAYMM 05-51-10-200-801-C1 NO ODOR OBSERVED OR ABLE TS REF AO BE IDENTIFIED BY MX. RECIRC FILTERS REQUIRE REPLACEMENT WITHIN 2 DAYS PER AMM 05-51-10-200-801-C1. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED. CONTROL: SOURCE DOCUMENT: TASK 05-51-1A: WITHIN 02 DAYS.HV U433304 REMOVED AND REPLACED RE-CIRC FILTERS PER AMM 21-20. OK FOR SVC TOMCQC REV PERFORMED
AFTER RAT FAN BLADE INSPECTION RED LIGHT ACTUATOR PRESSURE LGHT IS ILLUMINATED ON RAT CONTROL MODULE AFTER STOWING RAT ALSO RAT FAULT DISPLAYED ON UPPER ECAM WITH AMBER TRIANGLE DISPLAYED ON HYDRAULICS PAGE. REPLACED RAT ACTUATOR PRESURE SWITCH, LEAK CK OK OPS CK OK REF TSM 29-22-00-810-801-A, AMM 29-22-53-000-013-A, 29-22-53-400-013-A.
EMERGENCY LIGHTS AT SEAT 25C INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.
RAMP REPORT OF FUEL COUPLING CAP MISSING. RIGHT WING. INSTALLED FUEL CAP IAW AMM 28-25-41-400-005-A, SUB TASK 28-25-41-420-056-C, FROM STEP B2N TO B2Q,
FA REPORTS DOOR 2L PRESSURE GAUGE IN RED. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS.
PLEASE CHECK THE SLIDE PRESSURE GAUGE AT DOOR 2L AND REPLACE SLIDE IF THE NEEDLE IS IN AREA B CARRIED BY ELB ORIGINAL CYCLES LIMIT OF: 001 EXTENDED BY 001 NEW TIME REMAINING 001. REMOVED AND REPLACED DOOR 2 LEFT EVACUATION SLIDE REF 25-62-44. OPS CHECK SATISFACTORY. ACCOMPLISHED RII INSPECTION OF DOOR 2 LEFT EVACUATION SLIDE REPLACEMENT REF 25-62-44.
SEAT 23ABC EMERGENCY PATHWAY LIGHT FOUND INOP. REPLACED LENS COVER AND RECONNECTED EMERGENCY LIGHT AT SEAT 23ABC PER AIRBUS 319/320 AMM 33-51-19. OPS CHECK GOOD
FA REPORTS DOOR 2L SLIDE PRESSURE GUAGE IN RED. INDICATOR NEEDLE IS ONE NEEDLE WIDTH OVER THE GREEN BAND TO THE HIGH SIDE INTO THE RED ALLOWED TEMPERTURE CONDITIONS TO STABILIZE. PRESSURE INDICATION IS IN AREA A BAND. PER AMM TASK 25-62-00-210-001-A. OKAY FOR SERVICE.
L2 DOOR PRESSURE GAUGE SHOWS OVER PRESSURE SLIDE PRESSURE INDICATION FALLS WITHIN SERVICEABLE LIMITS. REF AMM 25-62-00-210- 001-A.
ENG 2 COMPRESSOR STALL A T CRZ ALT FL370 ENG 2 STALL ECAM ENG 2 EPR MODE FAULT CREW REPORTED MULTIPLE LOUD BANGS FOLLOWED BY STALL AND EPR MODE ECAM, ENGINE WAS REDUCED TO IDLE & RAN REMAINDER OF FLIGHT AT IDLE. CREW REPORTED ONE MORE LOUD BANG AFTER LANDING PRIOR TO ENGINE SHUTDOWN. NO EXCEEDANCES WERE RECORDED. ACCOMPLISHED BOROSCOPE INSPECTION OF THE HP COMPRESSOR & REMOVED AND REINSTALLED BOROSCOPE PLUGS ABCD IAW AMM 72-00-00-200-016B. EEC REPLACEMENT REF AMM 73-22-34 AND P5 LINE CHECK PER TSM 73-22-00-810-856-A. ACCOMPLISHED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00-710-013-C. OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE. BORO INSPECTED HPC STAGES 3,4,5,6&7 FOUND NO LIMITING DEFECTS.
ENG2 FAIL ON T/O ROLL. NO INDICATION NOTICED PRIOR TO FAILURE ENG 2 STALL WITH CFDS VSV MECH/BLD VLV/LPC2 REFERENCE TSM 71-00-00-810-809-A, ALSO SUGGEST MCD INSPECTION PER AMM 79-22-45-000-010-A TO DETERMINE ENGINE SERVICEABILITY. TOMC-MEREDITH FLAGGING SDR
DOOR 2 LEFT SLIDE DID NOT DEPLOY PROPERLY. REMOVED L2 SLIDE IAW AMM 25-62-44/401. INFO ONLY... PER FIRE DEPT, L2 SLIDE DID INFLATE AND 3 PASSENGERS WENT DOWN UNTIL IT DEFLATED AND FLIGHT ATTENDANT KEPT PEOPLE FROM USING IT.
HYD G RSVR OVHT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN . UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. FOLLOWED TSM TASK 29-11-00-810-802-A.AFTER ENG IDLE RUN/ TESTS NO MESSAGES FOUND ON UPPER OR LOWER ECAM , NO FAULT LIGHTS. NEXT STEP PER TSM 29-11-00-810-802-A. IS 4.D(1). ADD EMP:U238479 CORRECTION TO PREVIOUS UPDATE ORIGINAL FAULT WAS A RESERVOIR OVERHEAT , FOLLOWED TSM 29-10-00-810-807-A. AFTER ENG RUNS AND TESTS NO FAULTS NOTED NO MESSAGES DISPLAYED ON UPPER OR LOWER ECAM. PER TOMC REQUEST NEXT STEP IS TO REPLACE THE SDAC ADD EMP:U238479 REMOVED AND REPLACED SDAC 1 PRECAUTIONARY , REF AMM 31-55-34/401 CONFIG 00. SDAC GROUND SCAN PASSED. LEAK FOUND AFTER FURTHER INSPECTION . NO FURTHER DEFECTS NOTED AT THIS TIME.
RH FR16 DOUBLE JOGGLE HOLES FOUND CRACKED, REQUIRING PARTIAL FRAME REPLACEMENT AT C CK IN BFM AS NOTED ON N/R''S 110289 &; 110293. 1, PART 1.2 REQUIRES DIP AS FOLLOWS; ACCOMPLISH INITIAL INSPS A ST REV OF ECRA5311-03281 ON/BEFORE ACFT REACHES 37002 TTL FC (FH ) THEREAFTER. T RH FR16 DOUBLE JOGGLE HOLE #C & #D PER PART 2 ITEM 2.1 OF LATE NOT RELEVANT) PERFORM REPEAT INSP EVERY 6000FC (FH NOT RELEVANT ACCOMPLISHED INTERIM REPAIRS IAW W/ ECRA5311-03281 & VTMAE EA319 -5311-13-A3682 AND AIRBUS RDAF AS NOTED WITHOUT DEVIATION PER 1. INSPECTIONS ACCOMPLISHED AT C CK IN BFM AS NOTED ON N/R''S 110289 & 110293.
(SUPPORT TASK) DURING ROTO TEST OF RH FRAME 16 HOLE 6 FOUND CRAC KED IN FRAME LAYER AT THE 3:00 POSITION. REPAIR BEFORE NEXT FLIG HT.() TRANSFERRED REPAIR INFORMATION AND DIP REQUIREMENTS TO LP''S 9509350, 9509474 & 9509861. THIS ITEM CAN BE CLEARED.
PDA 2 RH OB FLAP IB CUSHION SEAL AND PLATE MISSING FROM AIRCRAFT UPON ARRIVAL. 55SQ IN. UPDATED SDR INFORMATION.
HYD Y ENG2 PUMP LOPRESSURE PILOT SAID PARKING BRAKE INOP DUE TO LOW PRESS ,FOUND LARGE HYD LEAK UNDER ENG 2 ALSO GREEN SYST HYD AND YELLOW HYD LOW . 29-13-00-810-804-A UPON INSPECTION FOUND HYDRAULIC LINE TO THE HCU AT 12 O CLOCK R/R PER AMM 29-13-51-400-010-A REQUIRES LEAK CHECK AND OPS CHECK POS CRACKED UNDER FITTING. SEE ATTACHED ILLISTRATION. HCU DPI ROTABLE PARTS CHANGE WAS INDICATED - TT # 1039207 SN OFF 2592 NORMAL. PART ON ORDER AOG. STILL NEED TO PERFORM LOSS OF HYDRAULIC PRESSURE INSPECTION FOR ENGINE 2 PUMP TASK ADD EMP:U381306 IPC REFERENCE # 29-13-51 REPLACED #2 ENGINE HYD LINE 18-2911-3-0093. REPLACED #2 ENGINE SYSTEM PUMP AND PEFORMED IDLE LEAK CHECK OF #2 ENGINE HYD PUMP CASE DRAIN HYD FILTER REF AMM 29-13-43-610-010-A. REPLACED AND LINES. PERFORMED REQ''D OPS CHECKS REF AMM YELLOW SYSTEM LP FILTER REF AMM 29-13-44-610-001-A. REPLACED 29-13-00-710-002-A. ALL LEAK CHECKS GOOD. YELLOW SYSTEM HP FILTER REF AMM 29-13-45-610-001-A. RAN YELLOW PUMP, HYDRAULIC OFF 31-2914-9-9003 2592 ON 31-2914-9-9003 7327
CREW REPORTS HYD Y RSVR LO LVL MESSAGE. CREW FOLLOWED QRH 130.44 PTU SWITCHED OFF AND ENG 2 HYD PUMP SWITCHED OFF. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V928786 PLEASE CONTACT UA MAINTENANCE CONTROL BEFORE COMMENCING ANY PLEASE CONTACT UA MAINTENANCE CONTROL BEFORE COMMENCING ANY MAC RELATED WORK ORDER 000000003039298 AND PRTR WORK. NEED TECHNICIANS TO ACCOMPLISH LEAK CHECK OF YELLOW WORK. NEED TECHNICIANS TO ACCOMPLISH LEAK CHECK OF YELLOW DAVIS, STEWART (V928786)TROUBLESHOT HYD LEAK REF AMM 29-00-00. HYDRAULIC SYSTEM PER AMM29-00-99 HYDRAULIC SYSTEM PER AMM29-00-99 FOUND YELLOW HYD POWER ACCUM 3070GM LEAKING FROM UPPER FITTING ORING. REMOVED AND REPLACED ORING REF AMM 29-13-42. OPS AND LEAK CHK GOOD. HYD SYS SERVICED TO NORMAL LEVEL. DAVIS, STEWART (V928786)TROUBLESHOT HYD LEAK REF AMM 29-00-00. FOUND YELLOW HYD POWER ACCUM 3070GM LEAKING FROM UPPER FITTING ORING. REMOVED AND REPLACED ORING REF AMM 29-13-42. OPS AND LEAK CHK GOOD. HYD SYS SERVICED TO NORMAL LEVEL.
ABOUT/40 MINT AFTER T/OGOT G RSVR OVHT ECAM.WHEN OVHT OUT G ENG PUMP+ PTU ON GOT AIRFRM.FLIGHT CREW TURNED THE GREEN HYD ENG PUMP AND THE PTU BACK ON. AND GREEN HYD SYSTEM OVERHEAT DID NOT COME BACK ON. SEEMED SUSPICIOUS. WITH LEFT ENGINE RUNNING, PTU OPERATED AS WHEN PTU WAS TURNED ON FO SAID THAT THEY HEARD AND FELT A BUMP EXPECTED, 3000 PSI ON YELLOW SIDE WITH PTU AUTO. WITH YELLOW UNDER THE COCKPIT FLOOR. ALL HYD INDICATIONS WERE NORMAL, ELECTRIC ON, PTU TURNED OFF. GOT A 400 POUND INCREASE IN GREEN PRESSURE, TEMP AND QTY, PTU SHOWED OFF. PRESSURE BY SHUTING OFF GREEN LEAK MEASUREMENT VALVE. AFTER DISCUSSION WITH THE FLIGHT CREW. ALL HYD QTYS AND AFTER PTU AND ENGINE PUMPS WERE TURNED BACK ON THE FA REPORTED GREEN SYSTEM DOES NOT REACH FULL PRESSURE WHEN POWERED BY PTU PRESSURES WERE NORMAL BUT GREEN OVERHEAT CAME ON ABOUT 40 THAT THE PTU WAS RUNNING, INDICATION IN COCKPIT WAS THAT THE PTU AND YELLOW ELECTRIC PUMP..WHEN POWERED BY RIGHT ENGINE PUMP, MINUTES AFTER TAKEOFF. FOLLOWED QRH AND TURNED OFF ENG HYD WAS OFF. FLIGHT CREW TURNED OFF PTU AND FA CONFIRMED THAT PTU GREEN PRESSURE READ ZERO WITH PTU IN AUTO. AT ENGINE SHUT DOWN, PUMP AND PTU. AFTER 30 MINUTES THE GREEN OVERHEAT WENT OUT, ''BARKING'' HAD STOPPED. AGAIN, ALL PRESSURES AND QTYS ARE NORMAL GREEN PRESSURE CHANGED INSTANTLY FROM 0 TO 3000. THAT CHANGE REFERENCE LOG PAGE 8062895 AND 8062910 FOR CORRECTIVE ACTION. ADD EMP:U181398
REF L/P 7964207- AFT GALLEY DRAIN CLOGGED AND LEAKING. SPILL CLEANUP REQUIRED. CABIN FLOOR FRAME 62 THUR 66 (CTR AISLE ROW 32 TO AFT GALLEY). NO WATER IN AFT CARGO COMPT DETECTED. PLACED ON DIP. WITHIN 7 DAYS, ACCOMPLISH ECRA 2011-01000, GALLEY SPILL, SECTION 2.B, IN-DEPTH CLEANUP, IN THE APPROX AREA FROM APPROVED DIP PER ECRA 2011-01000 FOR IN DEPTH CLEANUP OF GALLEY TOMC-APPROVAL FROM SC1ELBYC COMMENT WATER SPILL REQUIRED TO CENTER ISLE AREA MAIN CABIN FLOOR FROM FRAME 62 THROUGH 66 (CENTER ISLE ROW 32 TO AFT GALLEY). WITHIN 7 DAYS, ACCOMPLISH EC/RA 2011-01000, GALLEY SPILL, SECTION 2.B., IN-DEPTH CLEANUP. ACCOMPLISHED IMMEDIATE CLEANUP OF WATER LEAK IN AFT GALLEY/CABIN TOMC APPROVED : QC REVIEWED RECORDS UPDATE.............VD AREA PER ECRA 2011-01000 REV AB TOMC APPROVED : QC REVIEWED T/A: 7 DAYS................VD/U353583
BRAKE SYS 1 FAULT, SYS RESET THEN FAULT CAME BACK LOCKED FOR FIX ITEM UNLOCKED FOR CLEARING ACTION. REMOVED AND REPLACED #1 BSCU PER AMM 32-42-34-400AND TESTED OK, LAND VERIFY PASSED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248627 SN OFF 5694 UNIT, BRAKE STE OFF 31-3242-9-0001 5694 ON 31-3242-9-0001 1719
(SDR) DOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW, HO LE B HAS A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED LH FR16 HOLE B DOUBLE JOGGLE IAW EC/RA 5311-02735. SEE DTA DIP #7806847 FOR INSPECTION REQUIREMENTS. EMP: V935774 WC: 0 018261 STA: ST ENG BFM
WHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19. REPAIRED RH KEEL BEAM FASTENER HOLE AND FITTING IAW EC/RA 5330-0 6891. EMP: V935774 WC: 0018386 STA: ST ENG BFM SFR# 1027500
WHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT) REPAIRED LH KEEL BEAM FASTENER HOLES AND FITTINGS IAW EC/RA 5330 -06891 EMP: V935774 WC: 0018385 STA: ST ENT BFM SFR# 1027501
WHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19.
WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. -06891 (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF WORK ACCOMPLISHED BY VTMAE EMPLOYEE V935774. WORK ACCOMPLISHED BY VTMAE EMPLOYEE V935774. EC/RA 5330-06891 ON OR BEFORE 7-JAN-2023. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06891 ON OR BEFORE 7-JAN-2023. PERFORMED INTERIM REPAIR RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE HOLES IN ACCORDANCE WITH EC/RA 5330 ADD EMP:V935774 OK TO TILL ON OR BEFORE 07-JAN-23 PER EC/RA 5330-06891 TOMC-APPROVAL FROM SC1ELBYC COMMENT CORRECTING WRONG REFERENCE IN PREVIOUS MX ACTIONS ENTERED, PERFORMED INTERIM REPAIR RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE HOLES IN ACCORDANCE WITH EC/RA 5330 -06891 (SEE FIGURE 1 - 17 OF EC/RA 5330-06891 FOR LOCATIONS). ADD EMP:V935774 QC REVIEWED INIT: SEE LP# 7832625 T/A: 07JAN23................VD/U353583
WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE LH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. 02712. (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF WORK ACCOMPLISHED BY VTMAE EMPLOYEE V935774. EC/RA 5330-06891 ON OR BEFORE 7-JAN-2023. EC/RA 5330-06891 ON OR BEFORE 7-JAN-2023. PERFORMED INTERIM REPAIR LH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE HOLES IN ACCORDANCE WITH EC/RA 5311 ADD EMP:V935774 OK TO DIP PER EC/RA 5330-06891 TILL ON OR BEFORE 07-JAN-23 TOMC-APPROVAL FROM SC1ELBYC COMMENT CORRECTING REFERENCE IN MAINTENANACE ACTION: QC REVIEWED RECORDS UPDATE...SP PERFORMED INTERIM REPAIR LH FUSELAGE KEEL BEAM MLG -06891 (SEE FIGURE 1 - 17 OF EC/RA 5330-06891 FOR LOCATIONS). WORK ACCOMPLISHED BY VTMAE EMPLOYEE V935774.
DOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW. HOLE B H AS A CRACK INDICATION. MUST BE REPAIRED BEFORE NEXT FLIGHT PER E A 5311-02442. WITH EC/RA 5311-02735. WORK ACCOMPLISHED BY VTMAE EMPLOYEE AIRCRAFT FLIGHT CYCLES, AND AT INTERVALS NOT TO EXCEED 4,800 PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02735. V935774. ON OR BEFORE THE ACCUMULATION OF 33,351 TOTAL FLIGHT CYCLES, THEREAFTER, PERFORM AN INSPECTION PERFORMED INTERIM REPAIR LH FRAME 16 DOUBLE JOGGLE HOLE B (LEADER HOLE) AND HOLE #A (ASSOCIATED HOLE) IN ACCORDANCE ADD EMP:V935774 OK TO DIP PER ECRA 5311-02735. ON OR BEFORE THE ACCUMULATION OF TOMC-APPROVAL FROM SC1ELBYC COMMENT 33,351 TOTAL AIRCRAFT FLIGHT CYCLES, AND AT INTERVALS NOT TO EXCEED 4,800 FLIGHT CYCLES, THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02735. QC QC REVIEWED.
WHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT)
RH FR16 DOORSTOP #7 HAS CRACK INDICATIONS. ACCOMPLISHED BY VTMAE EMPLOYEE V935774. ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 INTERVALS NOT TO EXCEED 15,500 FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT REF LP7795132: PERFORMED INTERIM REPAIR RH FR16 DOOR STOP #7 HOLE #1 AND #3 IN ACCORDANCE WITH EC/RA 5311-02712. WORK ADD EMP:V935774 DIP 53-DIP ITEM REJECTED FOR INFORMATION UPDATE. THE REPAIR OF RH FR16 DOORSTOP #7 CRACK IS CONSIDERED A PERMANENT REPAIR REF LP 7795132. ECRA DOES NOT LIST INTIATING A DTA DIP FOR FR16 DOORSTOP #7. THIS DTA DIP LP WAS CREATED IN ERROR.
DOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED L/H FR20 DOUBLE JOGGLE FASTENER HOLES IAW EC/RA 5311-02 726. SEE DTA DIP LP# 7802054 FOR INSPECTION REQUIREMENTS. EMP: V 935774 WC: 0018262 STA: ST ENG BFM
LH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 13,700 FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO PERFORMED INTERIM REPAIR TO LH FR16 #1 DOORSTOP FITTING IN ACCORDANCE WITH EC/RA 5311-02712 AND EA 5311-02164A, OP ADD EMP:V935774 OK TO DIP PER ECRA 5311-02712.ACCOMPLISH INSPECTION REQUIREMENTS TOMC-APPROVAL FROM SC1ELBYC COMMENT PER PART 2A OF LATEST REVISION OF EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 13,700 FLIGHT CYCLES THEREAFTER. Q/C REVIEWED. Q/C REVIEWED. INIT: 40,251 TAFC (INIT WILL AUTO ITO TO RIR-2701) RIR: 13,700 FC......CM U372988 RECORDS UPDATE......CM RECORDS UPDATE......CM RECORDS UPDATE.......CM
CRACK INDICATIONS NOTED AT LEFT FR36 PRESSURE PANEL HOLES #3 THRU #9. PER ECRA 5330-06903. WORK ACCOMPLISHED BY V935774 TOTAL AIRCRAFT FLIGHT CYCLES, OR 128,977 TOTAL PERFORM AN INSPECTION PER PART 2 OF THE LATEST REF LP 7800794. UPON THE ACCUMULATION OF 60,651 AIRCRAFT FLIGHT HOURS, WHICHEVER COMES FIRST, REVISION OF ECRA 5330-06903. INTERIM REPAIR FOR CRACK INDICATIONS LEFT FR36 PRESSURE PANEL HOLES #3 THRU #9 ACCOMPLISHED AS OK TO DIP PER ECRA 5330-06903. UPON THE ACCUMULATION OF 60,651 TOMC-APPROVAL FROM SC1ELBYC COMMENT TOTAL AIRCRAFT FLIGHT CYCLES, OR 128,977 TOTAL AIRCRAFT FLIGHT HOURS, WHICHEVER COMES FIRST, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5330-06903. REVIEWED RECORDS UPDATE.......CM QC REVIEWED T/A: 60,651TAFC OR 128,977 TAFH.....CM U372988
LH FRAME 20 DOUBLE JOGGLE HOLE "A" CRACKED 5311-02726. WORK ACCOMPLISHED BY VTMAE EMP V935774. ON OR CYCLES, AND AT INTERVALS NOT TO EXCEED 5,900 FLIGHT CYCLES, REVISION OF ECRA 5311-02726. BEFORE THE ACCUMULATION OF 35,451 TOTAL AIRCRAFT FLIGHT THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF THE LATEST PERFORMED INTERIM REPAIR TO LH FRAME 20 DOUBLE JOGGLE HOLE "A" AND ASSOCIATED HOLE #B IN ACCORDANCE WITH EC/RA ADD EMP:V935774 OK TO DIP PER ECRA 5311-02726. ON OR BEFORE THE ACCUMULATION OF TOMC-APPROVAL FROM SC1ELBYC COMMENT 35,451 TOTAL AIRCRAFT FLIGHT CYCLES, AND AT INTERVALS NOT TO EXCEED 5,900 FLIGHT CYCLES, THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02726. Q/C REVIEWED. Q/C REVIEWED. INIT: 35,451 TAFC (INIT WILL AUTO ITO TO RIR-2703) RIR: 5,900 FC........CM U372988 RECORDS UPDATE.....CM RECORDS UPDATE......C M
ROTO PROBE OF RH FR20 #7 DOOR STOP FITTING FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 15,500 FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO PERFORMED INTERIM REPAIR TO RH FR20 #7 DOORSTOP FITTING IN ACCORDANCE WITH EC/RA 5311-02712 AND EA 5311-02164A, OP ADD EMP:V935774 OK TO DIP PER ECRA 5311-02712.ACCOMPLISH INSPECTION REQUIREMENTS TOMC-APPROVAL FROM SC1ELBYC COMMENT PER PART 2B OF LATEST REVISION OF EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 42,051 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 15,500 FLIGHT CYCLES THEREAFTER. Q/C REVIEWED. Q/C REVIEWED. INIT: 42,051 TAFC (INIT WILL AUTO ITO TO RIR-2699) RIR:15,500 FC....CM U372988 RECORDS UPDATE......CM
DOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442.
LH FR35 ROTO PROBE AT STGR 30 FASTENER HOLES FOUND THE BOTTOM AF T HOLE CRACKED ACCOMPLISHED BY VTMAE EMP V935774 ON OR BEFORE JUNE 20, OF ECRA5310-07963 2022, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION PERFORMED INTERIM REPAIR TO LH FR35 STGR 30 FASTENER HOLES 1 AND 2 IN ACCORDANCE WITH EC/RA 5310-07963. WORK ADD EMP:V935774 OK TO DIP PER ECRA 5310-07963. ON OR BEFORE JUNE 20, 2022, TOMC-APPROVAL FROM SC1ELBYC COMMENT PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA / 5310-07963. REVIEWED QC REVIEWED T/A: 20JUN22................VD/U353583 RECORDS UPDATE............VD
R1 DOOR DAMPER FAILED OPS CHECK
TWO ADDTIONAL FASTENER HOLES WERE FOUND CRACKED AT FR36 PRESSURE PANEL O/B OF ALLOWABLE CUT-OUT AREA REPAIRED ADDITIONAL FASTENER HOLES FOUND CRACK AT FR36 PRESSURE PANEL IAW EC/RA 5330-01903. EMP: V935774 WC: 0018304 STA: ST ENG BFM SFR# 1027449
RH FR16 #7 DOOR STOP ROTO PROBE FOUND THAT THE TOP IB AND BOTTOM IB HOLES HAVE CRACK INDICATIONS REPAIRED RH FR16 #7 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017896 STA: ST ENG BFM SFR# 1027447
RH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION REPAIRED RH FR16 #1 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017897 STA: ST ENG BFM SFR# 0017897
FWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION. REMOVED FLOOR BEAM Y254 BETWEEN FR16 AND FR20 CORROSION AROUND T D5311281820401 IAW SRM 51-42-11. EMP: V933870 WC: 0018103 STA: S HE SELF-LOCKING CLIP NUT IS NOT PERMITTED IAW SRM 53-11-14-283-0 T ENG BFM SFR# 1027224 07 FIG 004 NOTE 3. L=1.399" W=1.0" D=0.039 ORIGINAL THICKNESS 0 .080" REMAINING THICKNESS 0.041" AND INSTALLED NEW BEAM P/N
CABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292 REMOVED CORROSION CABIN FLOOR STRUCTURE FR68 Y1292 BEAM IAW SRM BFM SFR# 1027223 51-74-00 BLENDED AREA MEASURES L=1.5" W=1.250" D=0.019" ORIGINAL THICKNESS 0/155" REMAINING THICKNESS 0.136" FOUND OUT OF LIMITS IAW SRM 53-41-15-283-002. EMP: V933870 WC: 0018128 STA: ST ENG
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765 REMOVED CORROSION ON CABIN STRUCTURE FLOOR BEAM Y765 AT FRAME 65 51-72-11-911 AND 51-42-11. EMP: V933866 WC: 0018116 STA: ST ENG IAW SRM 51-74-00. FRAME FOUND OUT OF LIMITS IAW SRM 53-00-14-28 BFM SFR# 1027204 3 ORIGINAL THICKNESS 0.100" REMIANING THICKNESS 0.60" D=0.040" L =2.250" W=1.500". REMOVED AND REPLACED STRUCTURE FRAME IAW SRM
FWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION.
CABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765
AFT CABIN, LH DOOR SILL FLANGE FR67-FR68 NUT PLATE HOLE IS ELONG ATED
FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/FR20 HAS CORROSION REMOVED CORROSION IAW SRM 51-74-00 CHECKED LMITS W=2" L=2.5" D=0 ENGINEERING BFM SFR# 1027118 .38" FOUND OUT OF LIMITS, RECEIVED NEW BEAM P/N D5311278220201, INSTALLED NEW BEAM FWD CABIN -Y1292 BETWEEN FR16/FR20 IAW SRM 51 -42-11. MAINTENANCE ACCOMPLISHED BY V933986 ON WC 0018102 AT ST
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 68 Y765 REMOVED CORROSION ON CABIN FLOOR STRUCTURE FRAME Y765 FR68 IAW S -11-911 AND 51-42-11. EMP: V933866 WC: 0018126 STA: ST ENG BFM S RM 51-74-00. FRAME FOUND OUT OF LIMITS. ORIGINAL THICKNESS 0.160 FR# 1027183 " REMAINING THICKNESS 0.110" D=0.050" L=2.250" W=1.500" IAW SRM 53-00-14-283. REMOVED AND REPLACED STRUCTURE FRAME IAW SRM 51-72
LH OVERWING EMERGENCY EXIT ESCAPE HATCH SHOWING CRACKS IN STRUCT URE, NEED NDT TO VERIFY CRACKS REMOVED AND REPLACED ANGLE L/H OVERWING EMERGENCY EXIT ESCAPE IA W SRM 51-42-11 AND SRM 51-72-11 EMP: V933870 WC: 0018149 STA: ST ENG BFM SFR# 1027184
LH ELEVATOR #6 HINGE FITTING, IB AND OB BUSHINGS ARE WORN ON INN TER DIAMETER (REMOVE AND REPLACE - SDR) REMOVED AND REPLACED #6 HINGE FITTING I/B AND O/B BUSHINGS IAW S RM 51-72-12-911-002 FIG 002 SHEET 01 AND CMM SUBTASK 55-21-15-41 0-012-A01. P/N D5598200120001 B/N 0003857626. EMP: V933868 WC: 0 018455 STA: ST ENGINEERING BFM SFR# 1027117
R2 DOOR SILL INBD FLANGE HAS CORROSION ON UPPER SURFACE AND AROU ND 2EA FASTENER HOLES AT FR68 REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-41-14-283-0 02 L=1.195" W=2" D=0.025" AND REPAIR AREA IAW SRM 53-41-14-300-0 01 FIG 1 SHEET 04 PRINCIPLE 7 REPAIR CAT. A. EMP: V934614 WC: 00 18426 STA: ST ENGINEERING BFM SFR# 1027119
R2 DOOR SILL INBD FLANGE HAS CORROSION ON UPPER SURFACE AND AROU ND 2EA FASTENER HOLES AT FR68
LH ELEVATOR #6 HINGE FITTING, IB AND OB BUSHINGS ARE WORN ON INN TER DIAMETER (REMOVE AND REPLACE - SDR)
FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/FR20 HAS CORROSION
CABIN FLOOR STRUCTURE FRAME DAMAGED BETWEEN FR66 AND FR68 Y1292
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 66 Y1292
CABIN FLOOR SRUCTURE FRAME HASW CORROSION AT FRAME 68 -Y254
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 70 -Y1732
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 68 -Y1292
FWD CABIN FLOOR BEAM -Y254 BETWEEN FR16/FR20 HAS CORROSION REMOVED CORROSION AT FLOOR BEAM -Y254 BETWEEN FR16/FR20 IAW SRM 0002586573 IAW SRM 51-42-11/001 SFR# 1026990. EMP: V935977 WC: 0 51-74-00, MEASURED FLOOR BEAM ORIGINAL T. 0.087" REAMING TO 0.37 018101 STA: ST ENGINEERING BFM " D: 0.050" L= 0.550" W: 0.260" FOUND OUT OF LIMITS IAW SRM 53-1 1-14-283-007, INSTALLED NEW FLOOR BEAM PN D5311146020201 BATCH#
ROTO PROBE OF LH FR16 #7 DOOR STOP FITTING FOUND THAT THE TOP I/ B AND BOTTOM I/B HOLES HAVE CRACK INDICATIONS. REPAIR BEFORE NEX T FLIGHT REPLACED INTERCOSTAL FITTING IAW SRM 51-72-11-911-001 AND SRM 51 -42-11/001. P/N D5311423620091 B/N: 0003867876. EMP: V933868 WC: 0017894 STA: ST ENGINEERING BFM
FWD CABIN FLOOR BEAM -Y254 BETWEEN FR16/FR20 HAS CORROSION REMOVED CORROSION AT FLOOR BEAM -Y254 BETWEEN FR16/FR20 IAW SRM 0002586573 IAW SRM 51-42-11/001 SFR# 1026990. EMP: V935977 WC: 0 51-74-00, MEASURED FLOOR BEAM ORIGINAL T. 0.087" REAMING TO 0.37 018101 STA: ST ENGINEERING BFM " D: 0.050" L= 0.550" W: 0.260" FOUND OUT OF LIMITS IAW SRM 53-1 1-14-283-007, INSTALLED NEW FLOOR BEAM PN D5311146020201 BATCH#
ABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 66 -Y765 REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 66 -Y765 IAW SR MPLISHED BY V936054 ON WC 0018120 AT ST ENGINEERING BFM M 51-74-00. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-14-283-002 FI G 001. REMOVED AND REPLACED NEW CABIN FLOOR STRUCTURE FRAME 66 - Y765 IAW SRM 51-42-11 AND SRM 51-72-11-911-002. MAINTENANCE ACCO
FWD CABIN, FLOOR BEAM -Y81 AT FR16 HAS CORROSION BLEND OUT CORROSION ON CABIN FLOOR BEAM Y-81 AT FR16 OAW A319 SR TENANCE ACCOMPLISHED BY V936035 ON WC 0018100 AT ST ENGINEERING M 51-74-00, FLOOR BEAM FOUND OUT LIMITS IAW SRM 53-11-14-283-007 BFM FIG 010, AND FIG 013, L: 2,5" W=2,0" D=0,038" REMOVED AND REPLA CED CABIN FLOOR BEAM IAW SRM 51-72-11-911 AND SRM 51-42-11. MAIN
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FR68 -Y765 REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 68 - Y765 IAW S RM 51-74-00 FOUND TO BE OUT OF LIMITS. REMOVED CABIN FLOOR STRUC TURE FRAME 68 - Y765 IAW SRM 51-42-11. INSTALLED NEW FLOOR BEAM IAW SRM 51-72-11. EMP: V936041 WC: 0018122 STA: ST ENGINEERING B FM
CABIN FLOOR STRUCTURE HAS CORROSION AT FR70 Y254 REMOVED AND REPLACED NEW CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-74-00, FOUND TO BE OUT OF LI MIT IAW SRM 53-00-14-283-002. FIG 001. EMP: V936054 W/C: 0018125 STA: ST ENGINEERING BFM
CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FR68 -Y765
CABIN FLOOR STRUCTURE HAS CORROSION AT FR70 Y254 REMOVED AND REPLACED NEW CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-74-00, FOUND TO BE OUT OF LI MIT IAW SRM 53-00-14-283-002. FIG 001. EMP: V936054 W/C: 0018125 STA: ST ENGINEERING BFM
AFTER T/O CREW HAD L/G UNLOCK MSG THEN FLAP LOCKED MSG FOLLOWED BY GREEN SYS OVERHEAT THEN HAD YELLOW SYS OVERHEAT AND FINALLY G EAR GRAVITY EXTEND.
FOUND SEVERAL SEAT MOUNT EMERGENCY LIGHTS AND L2 DOOR 2L LT INOP DURING A SERVICE CHECK. REPLACED BATTERY AT RIGHT OVERWING AREA, CHKS GOOD. REPLACED THE 13WL POWER SUPPLY AFT LT, CHECKED GOOD. REPLACED THE LAMPS AT SEATS 25, 26, 29, 30, 34 AND DOOR 2L, EMERGENCY LIGHTS CHECKED GOOD.
EMERGENCY EXIT ON DOOR PAGE FOR LEFT SIDE AIRCRAFT ON AND OFF. ACP CONTINUITY CHECK OF WIRING IAW AWM 31-54-45 &52-73-06. ALL CHECKED GOOD. FOUND PROXIMITY SENSOR 2WN1 LOOSE INTERNALLY, REPLACED THE PROXIMITY SENSOR IAW AMM 52-73-11-400-004-C AND OPS CHECKED GOOD IAW GMM 9 25 05
EMER EXIT LIGHTS FLICKERING ON AND OFF WITH SWITCH IN ARM POSITION. RESET EMERGENCY POWER SUPPLY PER AMM 33-51-00, OPS CKS NORMAL AT THE GATE.
EMERGENCY EXIT LIGHTS FLICKERING ON AND OFF WITH SWICH IN ARM POSITION AGAIN. FOUND CIDS SYSTEM LOCKED UP AND WAS UNABLE TO GET EMERGENCY LIGHT TEST TO OPERATE. RESET CIDS SYSTEM. AFTER RESET, OPERATION RETURNED TO NORMAL.
DURING CLIMBOUT, THE LEFT WING EMERGENCY EXIT ECAM DISPLAYED FOR 10 MINS. ADJUSTED THE CLEARANCE ON LT OVERWING EXIT HANDLE COVER PROXIMITY SWITCH. IAW AMM 52-71-13. LIGHT EXTINGUISHED OK.
CABIN EMERGENCY LIGHTS OPS CHECK SHOWS AN EPSU EXT LOAD EMER R FAULT. FOUND THE AFT OVERWING EMERGENCY LIGHT ASSY 62WL BAD, REPLACED THE LIGHT ASSY, EMERGENCY LIGHT OPS TESTED OK IAW AMM TK33-51-00-710- 001-A.
EMERGENCY CABIN CIDS TEST, FOUND EPSU COM AFT LT MESSAGE, REMOVED AND REPLACED EPSU 13WL AND BATTERY PACK IAW MM 33-51-38. OPS CHECKED GOOD.
LEFT EMER EXIT DOOR OPEN ECAM OUT OF 6500, WARNING OUT PASSING FL290. PRESS NORMAL PERFORMED TSM 52-21-00-810-806-A, FOUND DOOR MONITORING SYSTEM OPS CKED GOOD.
OVERHEAD EMER EXIT LIGHTS ARE FLICKERING ON AND OFF IN THE REAR OF CABIN RESET CIDS. LIGHTS WORKING NORMAL.
EMERGENCY BATT TEST FAIL FAULTS EXTERIOR LOAD AFT LEFT. AFT SLIDES BAD, CAUSING EXTERIOR LIGHTS FAULT ON EPSU (AFT). BOTH LT AND RT AFT DOOR SLIDES REMOVED AND REPLACED IAW AMM 25-62-44.
APSU UNIT FWD LT UNIT FAULT DURING TEST REPLACE POWER SUPPLY AND BATTERY PACK LOCATED AT DOOR 1L. PASSED TEST.
EMERGENCY EXIT LIGHT POWER SUPPLY FAILED SELF TEST. REPLACED EMERGENCY EXIT POWER SUPPLY AT DR 1L IAW AMM.
EPSU EXT LOAD, EMER RT FAULT ON EMER LIGHT TEST. REPLACED EMER POWER SUPPLY & BATTERY IAW MM 33-51-38-401 & MM 33-51-38-402 & RELAMPED AFT ASSEMBLY FWD BULB ON OVERWING LIGHT. OPERATIONS NORMAL.
EMERGENCY LIGHTS FAIL MSG FOUND DURING 2 SVC CHECK. MSG READS, EPSU EXT LOAD RT. REPLACED EPSU & BATTERY FOR 12WL, NO HELP. REPLACED ALL FOUR LAMPS AT LIGHTS 60WL & 62WL. OPERATIONS CHECKED GOOD IAW AMM 33-51-15-400-0.
EMERGENCY LIGHTS FAILED TEST IAW NR 2 SERVICE. FOUND OVERWING EMER SLIDE LIGHT INOPERATIVE. RELAMPED IAW MM 33-51-15 EMER LIGHT TEST DID NOT PASS.
FLIGHT DIVERTED DUE TO LOSS OF YELLOW HYDS. SERVICED HYDS TO FULL LEVEL.
SEAT ROW 28 ABC OXYGEN DOOR WILL NOT RESET AFTER DROP TEST. REPLACED ACTUATOR ON CONTAINER & OPERATIONS TESTED IAW AMM 35-23-00. OPERATIONS CHECKED GOOD.
SEAT ROW 28ABC OXYGEN DOOR WILL NOT RESET AFTER DROP TEST, REQUIRES O2 BOX REPLACEMENT. SEAT ROW 28ABC INOPERATIVE. PSU PANEL SECURED CLOSED.
ECAM ON TO SCREEN DIM & HARD TO READ. ABORT AT 60KTS. PFR HAS NO A & T ISSUE, CHECKED ALL FADEC LLR & EIU. NO FAULT NOTED. RESET FMGC 1 & 2 PRECAUTIONARY. PERFORMED NORMAL AFS & LAND TEST IAW MM 22-97-00. ACFT RETAINS CAT III STATUS.
BRAKE SYS 1 FAULT ON ENG 2 SHUTDOWN WITH MOMENTARY LOSS OF BRAKING. REPLACED BRAKE PEDAL TRANSMITTER. NO FAULTS ON BSCU BITES IAW AMM 32-42-47.
NOSE LANDING LIGHT LENS IS CRACKED. SYMM REPORTS SCREW HEAD IS STRIPPED. R & R NOSE LANDING LIGHT, OPERATIONS CHECKED GOOD. SCREW HEAD IS STRIPPED NEEDS SERVICE BULLETIN REQ UPGRADE CF944.
UNABLE TO OPEN ENG 1 START VLV DURING NORMAL START ATTEMPT NR N2 ROTATION. REPLACED NR 1 ENG START VLV & STARTER, OPERATIONS CHECKED NORMAL.
EMERGENCY LIGHTS TEST FROM CIDS INDICATES 33-51-38, EPSU EXTERIOR EMERGENCY RT. BITE TEST OF OVERWING 12 WL, EPSU INDICATES EXTERIOR LIGHT FAULT. REPLACED AFT FWD OVERWING SLIDE LIGHT IAW AMM 33-51-14. FWD ATTN PANEL CHECKED GOOD ALONG WITH EPSU AT RT OVERWING.
ROW 8 ABC MASKS FELL ON LANDING. INSTALLED PASSENGER OXYGEN SYSTEM. OPS CHECKED GOOD
EMER LIGHT TEST GIVES EPSU LT MESSAGE. REPLACED BATTERY IAW MM.
EEL TEST FAILED NR 2 SV, "MESSAGE EPSU BATTERY AFT". REPLACED BATTERY AFT UNIT IAW AMM. TESTS GOOD. PN AD-3214-30.
ELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL REPLACED RIGHT BLUE SYSTEM ELEVATOR SERVO CONTROL ACTUATOR SERVO VALVE. PERFORMED SERVO VALVE SYSTEM TEST NO FAULTS FOUND AT THIS TIME.
F-CTL ELAC 1 PITCH FAULT PROG TEXT: - ITEM ROLLED FORWARD. (COMPLIED WITH MEL) RPR- :T/S FAULT TO ELAC 1. REMOVED AND REPLACED ELAC 1, OPS CHECK GOOD. CAT THREE PERFORMED, SEE SEQ 2692006.
FLOOR TRIM BY 29F IS TORN. FLOOR TRIM HAS BEEN REMOVED, OKAY TO CONTINUE. PARTS: 110-3219 (ABS5310-01 - PROFILE) LOB: N
RIGHT WINDOW DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE. F/O'S SLIDING WINDOW HEAT INOP. DF STICKER APPLIED. MEL C-W. REPLACED RIGHT SLIDING WINDOW.
WATER GUSHING FROM BELLY OF ACFT. SUSPECT RUPTURED WATER LINE. TROUBLESHOOTING FOUND RUPTURED WATER LINE IN CABIN FLOOR AT ROW 12ABC AND 20ABC. REPLACED WATER LINE REF AMM 20-23-38-300-002-A. PRESSURE CHECKED LINE AND NO LEAKS FOUND.
G RSVR LO LEVEL DISPLAYED ON UPPER ECAM SCREEN - HYD. FOUND CHECK VALVE ON PTU MANIFOLD BROKEN. LOCATED IN LEFT WW. VALVE REMOVED. WIRING TEST CHECKED OK. CHANGED CONNECTOR AT 15HHA PER MM. GROUND TESTED GOOD.
EMERGENCY EXIT LIGHTING RED LENSE ON FWD EDGE OF 1ST CLASS CLOSET FELL OFF. BROKEN OFF. :ACP INTERIM REPAIR WITH CLEAR TAPE LIGHT OP CHECK GOOD. LIGHT ASSY CLIP IS WEAK. ^22AUG LGA RCF-T :IPC REF 33-51-18-05 RED LENS CAP 07912-3.
RIGHT WINDOW DISPLAYED ON UPPER ECAM SCREEN. REPLACED RIGHT SLIDING WINDOW PANEL PER MM. RIGHT WINDOW MESSAGE ON UPPER ECAM STILL PRESENT.
LAVATORY AND CARGO DETECTION FAULT DISPLAYED ON UPPER ECAM SCREEN, SMOKE. REPLACED AFT CARGO DETECTOR 5WH PER AMM, OPS NORMAL.
STRONG ODOR IN AFT GALLEY OF BURNING ELECTRICS, WHEN POWER CUT. FOUND AFT LAVATORY OCCUPIED LIGHT ASSY SHORTED OUT. REPLACED SIGN ASSY AND LENS. OP'S CHECKED GOOD, NO BURNING ODOR.
CRACK ON INBOARD ENG 1 COWL. MAINT TEXT: REV SLEEVE HAS A PANEL SEPARATION, WITH A RIVET HEAD STICKING OUT 1-8". ANEL SEPARATION IS BETWEEN TS5,TS8,TS10. SEPARATION MEASURES 2 & 12-32"LONG. LOCATION IS 9 AND 34" DOWN FROM PYLON AND 19 AND 3-8" FWD OF THE AFT EDGE OF SLEEVE. ALL MEASUREMENTS REF SRM 54-30-00, PG 208, FIG 201. NO CRACKS FOUND AT THIS TIME. BLISTER FAIRING ATTACH FASTNERS LOOSE ALLOWING FILLET SEAL TO SEPARATE. REPLACED LOOSE FASTENERS AS REQUIRED. MT54-0014A. RESEALED AS NEEDED.
SEATS 10 ABC MASKS DROPPED ON LANDING. CHECKD O2 GENERATOR, PIN IN PLACE AND NOT ACTIVATED. REPACKED MASKS AND CLOSE DOOR. CHECKED LATCH FOR DEFECTS. PLACE TAPE OVER MODULE TO SECURE DOOR.
CREW REPORT: LIGHTNING STRIKE. NOT SURE OF ACTUAL LOCATION. SAMC TEXT: CONTACT SAMC, INSPECT PER MM 05-51-18 (FAXED) LEFT WINGTIP FENCE, DAMAGED BY LIGHTNING IN "NO DAMAGE" AREA, REMOVE PER AMM AND CDL PER 57BA. COMPLETED LIGHTNING STRIKE INSPECTION PER AMM. FOUND DAMAGE TO LEFT WING TIP FENCE WHICH REQUIRED IT'S REMOVAL. FENCE REMOVED PER AMM AND CDL'D PER 57BA, WILL REQ PCN (110-2006) FENCE PER OPBLM. SAMC REMARKS: WING TOP COVERED WITH TAPE TO REQ TAPE CHECK BEFORE EVERY DEPARTURE UNTIL THE FENCE IS REPLACED. PARTS: 110-2006 D5735120000200Z-U1 WINGTIP.
CREW O2 OVERPRESSURE DISK ON OUTSIDE OF ACFT IS WHITE INSTEAD OF GREEN. CLEANED RESIDUE FROM DISK.
LEFT EPSU BATTERY FAULT DISPLAYED DURING EMERGENCY LIGHTS TEST. REPLACED BATTERY AT LEFT EPSU. EMERGENCY LIGHT TEST SATISFACTORY.
PER CALLOUT SW2311. FIRST CLASS COAT CLOSET LOWER AFT CORNER HAS DAMAGE THAT HAS BEEN TAPED AND NOT DOCUMENTED. DAMAGE IS TAPED PER SW2311. CLOSET ASSY PART NUMBER 101744-101. SER # 005. LM INFO: PLEASE ID SOURCE OF PART NUMBER. IPC OR PART DATA PLATE? ALSO PLS EVALUATE PANES FOR REPAIRABILITY & UPDATE.
NR 1 ENG INBOARD T-R SLEEVE HAS SEVERAL LOOSE RIVETS AFT UPPER T-R ASSY (OUTER SHEETMETAL). REPLACED LOOSE RIVETS PER SRM, REPAIR NR 48, FIG 202.
PORTABLE OXYGEN BOTTLE MASK DEFECTIVE - OXYGEN. O2 MASK MISSING OR USED ROW 24ABC. MASK APPEARS TO BE USED, OXY BOTTLE CONSIDERED INOP PER MEL. RPL'D O2 MASK. BOTTLE WAS NORMAL.
THREE SERVICE EMERGENCY LIGHT TEST GIVES 2 FAULTS. EPSU INTERNAL AND EXTERNAL LIGHT FAULTS AT AFT L. FOUND WIRES PULLED AND SHORTED BELOW AFT ROW LT SEATS. RECONNECTED, TESTS OK.
ENG 1 FLAMEOUT TAIL PIPE DURING SHUT DOWN AS REPORTED BY OBSERVER. INSPECTED INLET, EXHAUST AND TAIL SECTION OF ENG 1, NO DAMAGE FOUND. WITH CREW ASSIST RAN ENGINE, SHUTDOWN NORMAL.
EXTERNAL FUSELAGE IS GOUGED AT FRAME 34 AT STR 43R DUE TO LONG FUSE FILLET FAIRING ATTACH SCREW. MAJOR REPAIR ACCOMPLISHED: DAMAGE REPAIRED IAW SRM, FIG 224. AREA HFEC INSPECTED, NO CRACKS NOTED. DOUBLER INSTALLED IAW SRM. REPAIR REQUIRES INSPECTION AT DEFINED INTERVALS.
20 EACH LIGHTNING STRIKES ON LT FWD FUSELAGE AFT OF BS 3500, FRAME 1, SUB ZONE 120. BURNISHED BURN AREAS. REMOVED BURNED RIVETS. REPLACED RIVETS AND LOCK FASTENERS WET PRIMED AND PAINTED AREA. HAD HFEC DONE ON HOLES. NO DEFECTS NOTED.
3 EACH LIGHTNING STRIKES ON LT FWD FUSELAGE BELOW CAPT'S FIXED NR 1 AND SLIDING WINDOW AT BS 2540, SUB ZONE 210. INSTALLED 3 EA CHERRY MAX RIVETS WET. PERFORMED HFEC ON EXISTING FASTNER HOLES. NO DEFECTS NOTED.
DOOR 1L SLIDE ARM LIGHT INTERMITTENT. ACFT WAS ON GROUND AND CABIN WAS UNPRESSURIZED WHEN DEFECT WAS NOTED. REPLACED DOOR 1L PROX SW 13WV1. ALL CHKS NORMAL.
ENG 2 OIL QUANTITY FLUCTUATIONS. FLIGHT DIVERTED. OIL TANK CHECKED FULL, NO OIL ADDED. REPLACED THE TRANSMITTER, OPS CHECKED OKAY.
RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. FOUND 1 LAMP OUT ON RT OVERWING PATHWAY, REPLACED LAMP. ALSO HAD L EPSU COMM, REPLACED LT EPSU (P/N 3214-54-10) AND BATTERY FOUND PUSHED BACK PIN ON RT EPSU, RESET PIN AND PERFORMED SUCCESSFUL EMERGENCY LIGHT TEST.
PITOT HEAT & AUTO PILOT PROBLEMS. FLIGHT DIVERTED.
EEL LIGHT AT SEAT 23ABC INOP. *S/D* SECURED CONNECTOR. OPS CHECK GOOD.
AIRBUS RAFT DOOR BROKEN HOSE. UNKNOWN DAMAGE. REPLACED HOSE.
F/O O2 MASK GREEN HOSE FRAYED. SWAPPED WITH 1ST OBS POSTION AND LATER REPLACED ASSY.
CAPTAIN'S O2 MASK LEAKING DURING TEST. UNKNOWN O2 LEAK. REPLACED CAPT O2 MASK. OPS CHECKED OK.
FUSELAGE SKIN AT FRAME 64 AND FRAME 65 AND STRINGER 23L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED AT DEN.
DENT FOUND RUNNING IN A VERTICAL DIRECTION APPROX 3 FT FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED AT DEN.
ON APPROACH ELECTRICAL ODOR. GALLEY CABIN OFF, VIDEO PLAYER OFF. ODOR DISSIPATED. [SUP 06-01-07] INSPECTED FORWARD AND AFT EE COMPARTMENTS AND FORWARD GALLEY WITH NO DEFECTS NOTED. RAN BOTH AC PACKS WITH NO NOTICABLE ODOR DETECTED.
STA 12267, STR 42 RIVET HAS LIGHTNING DAMAGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA & INSTALLED DOUBLER REPAIR.
EMERGENCY LIGHT TEST FAILS -EPSU BATTERY EMER L-. REPLACED BATTERY.
LEFT EPSU POWER SUPPLY MSG WHEN ACCOMPLISHING 3SVC.
RTF DUE TO NR 2 PACK ECAM FAULT MSG AND NR 1 PACK ALREADY DEFERRED. NR 2 PACK OVERHEAT WAS REPORTED WITH NR 1 PACK ALREADY DEFERRED. NR 2 PACK FAULT DISPLAYED ON THE UPPER ECAM SCREEN. REMOVED AND REPLACED NR 2 ACM (MR21552), 11HM1, PER MM-21-52-21. OP-CHECK AND LEAK CHECK WAS GOOD. FOLLOWING REPLACEMENT OF ACM, TWO DAYS LATER, THE DIFFERENTIAL PRESSURE SENSOR 9HB (PCN 565-2246) WAS REPLACED PER MM 21-51-11. OP-CHECK GOOD, NO MESSAGES OR FAULTS.
FLIGHT DIVERTED DUE TO STALL WARNING AND MASTER CAUTION LIGHTS. SUPPLEMENTAL DATA UPDATE THE SPURIOUS STALL WARNING WAS CAUSED BY A FAULTY FLIGHT WARNING COMPUTER (FWC) AND WAS CORRECTED BY REPLACING NR 1 FWC.
LOST CAPTAIN'S AIRSPEED TAPE INDICATION ON ROTATION. REPLACED AIR DATA INERTIAL REFERENCE UNIT NR 1. BUILT IN TEST EQUIPMENT CHECKED GOOD.