N535JB
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JETBLUE AIRWAYS CORPORATION (YENA) | Operator | 2010-04-05 – 2010-04-05 | Operator named in NTSB report |
| JETBLUE AIRWAYS CORP | Operator | 2010-04-05 – 2010-04-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FLT 655, SYR-MCO. "DESCENDING INTO MCO THROUGH 3800FT POWER IDLE LEVEL 1 FUMES ODOR DIRTY SOX. DISSIPATED AROUND 2500 FT. APU WASH & BLACK LIGHT COMPLETED NO LEAKS OR ODOR AT THE MOMENT. THIS CLEARS MDDR MX4 UPDATED PLACARD REMOVED.
FLT#769, BOS-FLL. 'POSSIBLE FUME EVENT. SMELL WAS STRONGER IN THE BACK.SMELL LIGHT BURNING; "COMPLIED WITH INFORMATION NOTICE 2017-T015K, SECTION B2. IDENTIFIED ODOR AS RESIDUAL (NO ACTIVE LEAKS) DECONTAMINATION LEVEL "B" WAS ACCOMPLISHED PER TSM: 05-50-00-810-831-A. AIRCRAFT IS OK FOR SERVICE." DUE TO HISTORY: R/R RECIRC FILTERS IAW AMM: 21-21-41.'
FLT#1111, JFK-CUR. 'AFT CABIN SMELL DEVELOPED AS F/A WERE DOING CABIN PREPARATION PRIOR TO LANDING SMELL BECAME STRONGER AFTER LANDING AND CONTINUED UNTIL PACK 2 TURNED OFF AT GATE; C/W INFO NOTICE 2017-T015 SEC A ISOLATED FAULT TO TYPE 10 ENVIRONMENTAL PER TSM 05-50-00-810-085B INSPECTED APU COMPARTMENT WITH NO LEAKS NOTED RAM BOTH ENGINES WITH ASSIST OF FLIGHT CREW NO ODOR PRESENT WITH ENGINE OR APU BLEED A/C OK FOR SERVICE MCC LEO NOTIFIED.'
FLT#933, BDL-TPA. 'BELOW FL 190, FA REPORTED BURN RUBBER SMELL FROM FORWARD GALLEY VENT 8,000' FAINT ODOR/FUME ( APU SYSTEM ); PERFORMED AOTHER GVI & PACK BURN. COULD NOT DUPLICATE ODOR. NO OTHER FAULTS/DEFECTS NOTED. THIS CLEARS MDDR. MX-4 UPDATED. PLACARD REMOVED.
FLT#420, ATL-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK), 'ON APPROACH WHEN FLAPS 2 WERE SELECTED, ECAM FLT CONTROL FLAPS LOCKED-ALIGNMENT FAULT - SLATS OPERATED NORMALLY - FLAPS STUCK BETWEEN 0 AND 1; REF LP 3551343 -2 (PERFORMED CHECK OF R/H FLAP DRIVE SYSTEM IAW AMM 27-54-00-220-007-A. CHECK OKAY) & LP 3551344-1 (REMOVED AND REPLACED RH INTERCONNECTING STRUT IAW AMM 27-51-44. INCLUDING RIG AND FULL OPS CHECK. ALL FAULTS CLEARED. FLAP OPERATING NORMALLY.). ALL FAULTS CLEARED. OPS CHECK GOOD.'
FLT#218, JFK-BOS. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK) ' FLAPS LOCKED AT FLAP 2 SLATS AT 2 FLAPS LESS THAN 1 COMPLIED W/ QRH LAND CONF-3.' (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION WITH ADDITIONAL INFORMATION TO FOLLOW)
FLT#218, JFK-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK) ' FLAPS LOCKED AT FLAP 2 SLATS AT 2 FLAPS LESS THAN 1 COMPLIED W/ QRH LAND CONF-3.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHEM ENT INTERNAL AREA FROM UPPER TENSION BOLT LH SIDE, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGTH IS 0.135 INCH, IN COCKPIT (1 EA); ALL WORK ACCMPLISHED ON AE WO 2023-279/1 NR 2023-590628 ACCOMPLISHED THE REPAIR OF THE CRACKS FOUND AT THE WINDSHIELD FRAME CENTER POST UPPER FASTENERS LH AND RH COMMON AREA AND THE MIRROR FITTING REPAIR IAW REF /1/ AEM EA 53-0360-23 REV 0 (COVER PART 1AND PART 2) JB EC A23-1068-01.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL DOOR IN BULK CARGO COMPARTMENT; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00005 ) REF AEROMAN WO 2023 279/1 WCC 2023-590586 PERFORMED REPAIR LOWER SILL DOOR IN BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49-300-003 AND REQUIRED INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60000 FC/ 120000 FH SUBSEQUENT INSPECTION AT INTERVALS OF TBD FC/ TBD FH INSPECTION METHOD TBD IAW SRI 53-41-49-205-003 TABLE 001. WORK ACCOMPLISHED BY AEROMAN TECH 8632015 RII: QC220. FUR-A320-53-00960 ASSIGNED.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.68 AND STR. 8L INTERNAL STRUCTURE CRACK L ENGTH: 0.410 INCH APPROX; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00023 ) REF AEROMAN W/O 2023 279/1 WCC 2023-590638 PERFORMED REPAIR LOCATED ON FR 68 AND STGR 8 LH SIDE INTERNAL STRUCTURE IAW A320 SRM 53-41-12-300-012 FIGURE 003 (SHEET 1) THIS REPAIR IS CATEGORY B AND THE INSPECTION THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT AT 57700FC, SUBSEQUENT INSPECTION AT INTERVALS OF 2600FC AND METHOD INSPECTION IS HFEC WITH REMOVED PART IAW NTM 51-10-08 AND A320 SRI 53-41-12-205-014, TABLE 001 AND FIGURE 001. FUR-A320-53-00979 CREATED.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 14 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590793 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8640408 RII: QC265.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC.RIB 11 PLUS 3 INCHES TRAILING EDGE (OVERH ANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590791 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII: QC360.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 11 PLUS 20 INCHES TRAILING EDGE (OVER HANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590792 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01 . WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII:QC360.
DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOC RIB 7 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590805 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII:QC318.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA FROM UPPER TENSION BOLT RH SIDE, CRACK DIRECTION IS 10 OCLOCK, CRACK LENGTH IS 0.105 INCH, IN COCKPIT (1 EA); ALL WORK ACCOMPLISHED ON AE WO # 2023-279/1 NR # 2023-590631 ACCOMPLISHED THE REPAIR OF THE CRACKS FOUND AT THE WINDSHIELD FRAME CENTER POST UPPER FASTENERS LH AND RH COMMON AREA AND THE MIRROR FITTING REPAIR IAW REF /1/ AEM EA 53-0360-23 REV 0 (COVER PART 1 AND PART 2) AND JB EC A23-1068-01.
DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON CENTER WING BOX FR41 TO FR42 ON LH SID E IN PASSENGER CABIN; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00028 ) ALL WORK ACCOMPLISHED ON AE WO # 2023 279/1 NR # 2023-590664 ACCOMPLISHED THE REPAIR OF THE CORROSION FOUND AT THE CENTER WING BOX-LH TOP SKIN BTWN FR 41-42 AT BEAM Y1292 IAW AEM EA 57-0376-23 REV 0 (COVER, PART 1) AND AIRBUS RDAF 81292115/003/2023#A JB EC A23-1070-01.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 14 PLUS 16 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590795 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII: QC318.
DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST UPPER FASTENERS LH & RH AREA / CRACKS - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / LH TOP SKIN BTWN FR 41-42 AT BEAM Y1292. CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / REAR SPAR - TE OVERHANG / WX3494-WX4490 AND RIBS 9-18 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 15 PLUS 17 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590797 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8640408 RII: QC265.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 16 PLUS 20 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/11 WCC 2023-590799 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8640408 RII: QC265.
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 17 PLUS 16 INCHES TRAILING EGDE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590801 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII: QC318.
DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOC RIB 7 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590805 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TRAILING EDGE OVERHANG UPPER AND LOWER SURFACE IN ACCORDANCE WITH SAL EA# 57-0370-23 COVER AND P1-P8 AND AIRBUS RDAF # 81076849/038/2023 ISSUE A AND EC# A23-1153-01. WORK ACCOMPLISHED BY AEROMAN TECH 8613413 RII: QC318.
DURING HEAVY MAINTENANCE: CORROSION ELEVATOR TIP OUTBOARD RIB ON RH HORIZONTAL STABILIZER (CPCP RELATED REFER TO THE MPD TASK: 552006-01); (RESOLVED ON W/O: 1264003 TASKCARD: NR-00021 ) REF AEROMAN W/O 2023 279/1 WCC 2023-590516 REMOVED AND REPLACED TIP ELEVATOR OUTBOARD RIB 10 LOCATED IN INTERNAL SURFACE ON RH HORIZONTAL STABILIZER IAW A320 SRM 55-21-12-300-002 AND A320 SRM 51-72-11, DWG D55281545. WORK ACCOMPLISHED BY AEROMAN TECH 8609718 RII: QC318. MX220 COMPLETED.
DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON CENTER WING BOX FR41 TO FR42 ON LH SID E IN PASSENGER CABIN; ALL WORK ACCOMPLISHED ON AE WO # 2023 279/1 NR # 2023-590664 ACCOMPLISHED THE REPAIR OF THE CORROSION FOUND AT THE CENTER WING BOX-LH TOP SKIN BTWN FR 41-42 AT BEAM Y1292 IAW AEM EA 57-0376-23 REV 0 (COVER, PART 1) AND AIRBUS RDAF 81292115/003/2023#A JB EC A23-1070-01. (CONSIDERED AS A MAJOR REPAIR)
FLT#17, JAX - FLL. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JAX) ' SHUT DOWN #2 ENGINE IN FLIGHT DUE TO HEAVY SURGING EVEN AT IDLE; C/W TSM 71-00-00 AND FOUND VSV ACT AT FAULT. VSV ACT REPLACED IAW 75-32-41. ACCOMPLISHED #2 ENG VSV LUVE PER AMM 75-32-42. BSIHPC ACCOMPLISHED. NO FAULTS FOUND. PERFORMED IDLE LEAK CHECKS & HIGH POWER ASSURANCE TEST PER AMM 71-00-00. ALL CHECKS GOOD AT THIS TIME & NO LEAKS.'
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR TRAILING EDGE TOP SKIN, LOWER SURFACE, OVERHANG. BT W RIB7 TO RIB8 ON RH WING (REFER TO THE MPD TASK: 572178-01); PERFORMED REPAIR ON RH WING TOP SKIN BOTTOM SURFACE TRAILING EDGE BTW RIB 7 TO RIB 8 IN ACCORDANCE WITH EA NO. 57-0218-22 AND EC NO. A22-578-01, THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT THRESHOLD (OR INSPECTION STAR POINT) 60000FC/120000FH WITH INTERVALS TBD AND METHOD OF INSPECTION TBD I.A.W. RDAF 81076843/003/2022 ISSUE A TOOL USED DIGITAL CALIPER P/N: 500-147-20 S/N: 12141490 DUE DATE: FEB-02-2023. TOOL USED EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023. TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; DUE DATE: JAN-26-2023. TOOL USED MICROMETER P/N: 293-340-30 ,S/N: 63324500; DUE DATE : SEP-24-2022. TOOL USED FLAP SPEED P/N: FPK-PRO-104, S/N: PRO-3344, DUE DATE: MAY-06-2023. COMPLETED MX-220 FORM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1. NRC: 2022 - 327776 TECH: J. MARTINEZ 8618012. INSP: E. LOPEZ AE 244 QC.
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. ON TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB7 TO RIB8 ON LH WING; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 7 ON LH WING I.A.W. EC NO. A22-604-01 AND EA NO. 57-0204-22, PART 1, PART 5, AND PART 12, EA# 57-0357-55 COVER REV. 0 AND RDAF NO. 81076198/142/2022#A THIS REPAIR IS CATEGORY A AND NOT FURTHER INSPECTION IS REQUIRED TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 CALIPER: P/N: 500-752-20 S/N: B16101293; DUE DATE: SEP-16-2022 EDDY CURRENT FLAW DETECTOR P/N: NORTEC600D, S/N: 190023010, DUE DATE: FEB-14-2023 THICKNESS GAGE: P/N 45MG, S/N: 130060401, DUE DATE: JAN-26-2023, MICROMETER P/N: 293-340-30, S/N: 63324500; DUE DATE: SEP-24-2022, TOOL USED P/N: FPK-PRO-107, S/N: PRO-3344, DUE DATE: MAY-06-2023. COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC; 2022 - 327720TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 7 ON LH WING I.A.W. EC NO. A22-604-01 AND EA NO. 57-0204-22, PART 1, PART 5, AND PART 12, EA# 57-0357-55 COVER REV. 0 AND RDAF NO. 81076198/142/2022#A THIS REPAIR IS CATEGORY A AND NOT FURTHER INSPECTION IS REQUIRED TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 CALIPER: P/N: 500-752-20 S/N: B16101293; DUE DATE: SEP-16-2022 EDDY CURRENT FLAW DETECTOR P/N: NORTEC600D, S/N: 190023010, DUE DATE: FEB-14-2023 THICKNESS GAGE: P/N 45MG, S/N: 130060401, DUE DATE: JAN-26-2023, MICROMETER P/N: 293-340-30, S/N: 63324500; DUE DATE: SEP-24-2022, TOOL USED P/N: FPK-PRO-107, S/N: PRO-3344, DUE DATE: MAY-06-2023. COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC; 2022 - 327720 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB10 T O RIB11 ON LH WING. REFER TO THE MPD TASK 572178-01; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG BTW RIB 10 TO RIB 11 ON LH WING I.A.W. EC NO. A22-605-01 AND EA NO. 57-0204-22, PART 1,2,7,8,10,11,12 ,EA# 57-0358-22 COVER REV. 0 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED FOR TOP SKIN PANEL2 UPPER SURFACE AT THE REAR SPAR AT THRESHOLD (OR INSPECTION START POINT) 10000FC/20000FH INTERVAL 10000FC/20000FH METHOD SDI,DET EXTERNAL , FOR REAR SPAR TOP FLANGE AT THRESHOLD (OR INSPECTION START POINT) 33100FC/66200FH. INTERVAL: TBD METHOD: TBD I.A.W. RDAF NO. 81076198/141/2022#A TOOL USED CALIPER P/N: 500-464, S/N: B17030932, DUE DATE: NOV-29-2022; TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200048001, DUE DATE: MAR-30-2023; TOOL USED ULTRASONIC EQUIPMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN-26-2023; TOOL USED MICROMETER P/N: 293-340-30, S/N: A18229497, DUE DATE: SEP-21-2022; TOOL USED TORQUE P/N: QD1R200A, S/N: 0821901619, DUE DATE: AUG-13-2022 COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN: W/O:2022 76/1 NRC: 2022 - 327724 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG BTW RIB 10 TO RIB 11 ON LH WING I.A.W. EC NO. A22-605-01 AND EA NO. 57-0204-22, PART 1,2,7,8,10,11,12 ,EA# 57-0358-22 COVER REV. 0 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED FOR TOP SKIN PANEL2 UPPER SURFACE AT THE REAR SPAR AT THRESHOLD (OR INSPECTION START POINT) 10000FC/20000FH INTERVAL 10000FC/20000FH METHOD SDI,DET EXTERNAL , FOR REAR SPAR TOP FLANGE AT THRESHOLD (OR INSPECTION START POINT) 33100FC/66200FH. INTERVAL: TBD METHOD: TBD I.A.W. RDAF NO. 81076198/141/2022#A TOOL USED CALIPER P/N: 500-464, S/N: B17030932, DUE DATE: NOV-29-2022; TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200048001, DUE DATE: MAR-30-2023; TOOL USED ULTRASONIC EQUIPMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN-26-2023; TOOL USED MICROMETER P/N: 293-340-30, S/N: A18229497, DUE DATE: SEP-21-2022; TOOL USED TORQUE P/N: QD1R200A, S/N: 0821901619, DUE DATE: AUG-13-2022 COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN: W/O:2022 76/1 NRC: 2022 - 327724 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION LOCATED ON RIB 11 PLUS 3 INCH TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE LH WING. REFER TO THE MPD TASK 572178-01; REWORKED AFFECTED AREA LOC. ON RIB 11 PLUS 3IN AT TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE AT LH WING I.A.W. A320 SRM 51-74-00-001 THEN EVALUATED THE REWORKED AREA AND FOUND WITHIN LIMITS I.A.W.N A320 SRM 57-21-11-283-007 TABLE 002, THIS ALLOWABLE DAMAGE IS CATEGORY B AND MUST BE INSPECTED AT INTERVALS OF 20000FC/40000FH INSPECTION THRESHOLD FROM EMBODIMENT OF REPAIR WITH SUBSEQUENT INSPECTION AT INTERVALS OF 9000FC/18000FH AND METHOD OF INSPECTION DVI I.A.W. SRI 57-21-11-205-006. TOOL USED CALIPER P/N: 500-752-20, S/N: B21038234, DUE DATE: SEP-16-2022; TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D, S/N: 190023010, DUE DATE: FEB-14-2023; TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG, S/N: 130066701, DUE DATE: APR-08-2023. COMPLETED MX-200 FORM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC: 2022 - 327847 TECH: J. MARTINEZ 8618012 INSP: INSP. D. LUNA.
DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 13 AND 15 - TIME-LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR TRAILING EDGE TOP SKIN, LOWER SURFACE, OVERHANG BT W RIB8 TO RIB9 ON RH WING (REFER TO THE MPD TASK: 572178-01.); PERFORMED REPAIR ON RH WING TOP SKIN BOTTOM SURFACE TRAILING EDGE BTW RIB 8 TO RIB 9 I.A.W EA NO. 57-0218-22 AND EC NO. A22-578-01, THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT THRESHOLD (OR INSPECTION STAR POINT) 60000FC/120000FH WITH INTERVALS TBD AND METHOD OF INSPECTION TBD I.A.W. RDAF 81076843/003/2022 TOOL USED DIGITAL CALIPER P/N: 500-147-20 S/N: 12141490, DUE DATE: FEB-02-2023. TOOL USED EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023; TOOL USED ULTRASONIC THICKNESS GAUGE; P/N: 45MG, S/N: 130060401, DUE DATE: JAN-26-2023; TOOL USED MICROMETER P/N: 293-340-30, S/N: 63324500; DUE DATE: SEP-24-2022; TOOL USED FLAP SPEED P/N: FPK-PRO-104, S/N: PRO-3344, DUE DATE: MAY-06-2023. COMPLETED MX-220 FORM BY CPCP PROGRAM ACCOMPLISHED AEROMAN W/O:2022 76/1. NRC: 2022 - 327780 TECH: M. MARMOL 8613913 INSP: J. MORENO AE 215 QC.
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB8 TO RIB9 ON LH WING; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 8 PLUS 4 INCH ON LH WING I.A.W. EC NO. A22-604-01 AND EA NO. 57-0204-22, PART 1, PART 5, AND PART 12, EA# 57-0357-55 COVER AND RDAF NO. 81076198/142/2022#A THIS REPAIR IS CATEGORY A AND NOT FURTHER INSPECTION IS REQUIRED TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 CALIPER: P/N: 500-752-20 S/N: B16101293; DUE DATE: SEP-16-2022 EDDY CURRENT FLAW DETECTOR P/N: NORTEC600D, S/N: 190023010, DUE DATE: FEB-14-2023 THICKNESS GAGE: P/N 45MG, S/N: 130060401, DUE DATE: JAN-26-2023, MICROMETER P/N: 293-340-30, S/N: 63324500; DUE DATE: SEP-24-2022, TOOL USED P/N: FPK-PRO-107, S/N: PRO-3344, DUE DATE: MAY-06-2023 COMPLETED MX -220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC: 2022 - 327721 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO.
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB14 T O RIB15 ON LH WING REFER TO THE MPD TASK 572179-01; PERFORMED INTERIM REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 14 ON LH WING I.A.W. EC NO. A22-606-01, AND EA NO. 57-0204-22, PART 1 TO PART 12, WITH NO REPAIR CATEGORY, SOLUTION LIFE, OR LIMITATION. 6 MONTHS I.A.W. RDAF NO. 81076198/004/2022#A TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 CALIPER, P/N:500-752-20 S/N: B21038259 DUE DATE: AUG -10-2022. EDDY CURRENT EQUIPMENT PN: NORTEC500D, SN: N500X1693P030456 DUE DATE: JAN 26 2023. ULTRASONIC EQUIPMENT PN: 45MG, SN: 130060401, DUE DATE: JAN 26 2023. ULTRASONIC THICKNESS INSTRUMENT P/N 45MG S/N 130066701 DUE DATE APR-08-2023. DIGITAL CALIPER :P/N: 500-197-30 S/N: A18229497 DUE DATE : SEP-21-2022 MICROMETER P/N : 293-340-30 ,S/N : 63324500; DUE DATE : SEP-24-2022 ULTRASONIC THICKNESS INSTRUMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN 26 2023. FLAP SPEED P/N FPK-PRO-104, S/N PRO-3446, DUE DATE JAN-12-2023 COMPLETED MAX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC: 2022 - 327730 TECH: S. MURCIA 8672520 INSP: INSP. S. ASCENCIO PERFORMED INTERIM REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 14 ON LH WING I.A.W. EC NO. A22-606-01, AND EA NO. 57-0204-22, PART 1 TO PART 12, WITH NO REPAIR CATEGORY, SOLUTION LIFE, OR LIMITATION. 6 MONTHS I.A.W. RDAF NO. 81076198/004/2022#A TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 CALIPER, P/N:500-752-20 S/N: B21038259 DUE DATE: AUG -10-2022. EDDY CURRENT EQUIPMENT PN: NORTEC500D, SN: N500X1693P030456 DUE DATE: JAN 26 2023. ULTRASONIC EQUIPMENT PN: 45MG, SN: 130060401, DUE DATE: JAN 26 2023. ULTRASONIC THICKNESS INSTRUMENT P/N 45MG S/N 130066701 DUE DATE APR-08-2023. DIGITAL CALIPER :P/N: 500-197-30 S/N: A18229497 DUE DATE : SEP-21-2022 MICROMETER P/N : 293-340-30 ,S/N : 63324500; DUE DATE : SEP-24-2022 ULTRASONIC THICKNESS INSTRUMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN 26 2023. FLAP SPEED P/N FPK-PRO-104, S/N PRO-3446, DUE DATE JAN-12-2023 COMPLETED MAX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC: 2022 - 327730 TECH: S. MURCIA 8672520 INSP: INSP. S. ASCENCIO (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB13 TO RIB14 ON LH WING REFER TO THE MPD TASK 572179-01; B17030932, DUE DATE NOV-29-2022 ULTRASONIC PHASED ARRAY P/N: OMNI-MX; S/N: OMNI-102103; DUE DATE: JUL-30-2022. CALIPER P/N: 700-113-10; S/N: 0002956; DUE DATE: NOV-05-2022. DIGITAL CALIPER P/N: 500-197-30 S/N: B20189511 DUE DATE SEP-16-2022. DIGITAL CALIPER P/N 700-113-10; S/N 0013356; DUE DATE SEP-30-2022. PRECISION RADIUS GAUGE P/N S167C; S/N AE-35946; DUE DATE FEB-11-2023 TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A18135095, DUE DATE: FEB-12-2023 DIGITAL CALIPER P/N: 500-197-30 S/N: A21143429, DUE DATE: OCT-11-2022. TORQUE 1/4 P/N: QD1R200A; S/N: 0821901612; DUE DATE: AUG-13-2022.COMPLETED MAX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1 NRC:2022 - 327729 TECH: S. MURCIA 8672520 INSP: INSP. S. ASCENCIO PERFORMED INTERIM REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 14 ON LH WING I.A.W. EC NO. A22-606-01, AND EA NO. 57-0204-22, PART 1 TO PART 12, WITH NO REPAIR CATEGORY, SOLUTION LIFE, OR LIMITATION. 6 MONTHS I.A.W. RDAF NO. 81076198/004/2022#A, TOOL USED CALIPER P/N 500-464, S/N B17030932, DUE DATE NOV-29-2022 ULTRASONIC PHASED ARRAY P/N: OMNI-MX; S/N: OMNI-102103; DUE DATE: JUL-30-2022. CALIPER P/N: 700-113-10; S/N: 0002956; DUE DATE: NOV-05-2022. DIGITAL CALIPER P/N: 500-197-30 S/N: B20189511 DUE DATE SEP-16-2022. DIGITAL CALIPER P/N 700-113-10; S/N 0013356; DUE DATE SEP-30-2022. PRECISION RADIUS GAUGE P/N S167C; S/N AE-35946; DUE DATE FEB-11-2023 TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A18135095, DUE DATE: FEB-12-2023 DIGITAL CALIPER P/N: 500-197-30 S/N: A21143429, DUE DATE: OCT-11-2022. TORQUE 1/4 P/N: QD1R200A; S/N: 0821901612; DUE DATE: AUG-13 2022. COMPLETED MAX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN W/O:2022 76/1, NRC:2022 - 327729 TECH: S. MURCIA, 8672520. INSP: INSP. S. ASCENCIO. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 9 AND 11 - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
FLT#1496, CUN-FLL. ' DESCENDING THROUGH 12,000' FUME EVENT BEGAN, AND BOTH PILOTS DETECTED A MUSTY DIRTY SOCK SMELL. TURNED OFF PACK 1 AS PER ODOR ISOLATION PCDR, MOSTLY CLEARED BY 6,000'; ACCOMPLISHED INSPECTION OF APU AREA. NO FUEL / OLIS LEAK WAS NOTED AT THIS TIME. COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ( A ) ISOLATED FAULT TO TYPE 10 ( A ) , 1 C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE .'
FLT 379, DCA-FLL. VERY FAINT BURNING SMELL FROM FORWARD GALLEY BY COFFEE MAKER DURING DESCENT. DISSIPATED AFTER LANDING COFFEE MAKER WAS ON (MX-270 ATTACHED). ( COFFEE MAKERS ) ; INSP FOUND FWD COFFEE MAKER 106 HEATING PLATE BURNT OUT CAUSING ODOR PLACED ON NEF N25-30-01A MDDR# 326988-2 MX-4 UPDATED AND PLACARD INSTALLED. (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT# 2204, SJU-JFK.MCDU #1 FAILED ASSOCIATEDELECTRICAL ODOR PULLED BREAKER B1 & B2 AS PRECAUTION NO ECAM WARNING MCDU SIMPLY WENT BLANK ; R/R CAPT'S MCDU IAW AMM 22-82-12.PERFORMED OPERATIONAL TEST PER AMM TASK 22-70-00-710-00-A.OPS CHECKS OKAY AT THIS TIME, THIS CLERAS MDDR 438169 MX-4 UPDATED PLACRD REMVED.
DURING HEAVY MAINTENANCE, IMPROPERLY PACKED SLIDE RAFT AT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA; (REF. AERO N/R 2021-134049 W/O: 2021 70/1 -) R & R EMERGENCY EVACUATION ESCAPE SLIDE RAFT DOOR 832 IAW AMM 25-62-44-400-007-A. SUPPLEMENTAL INFORMATION TO FOLLOW.
DURING HEAVY MAINTENANCE, INOP EPSU 12WL; (REF. AERO N/R 2021-134069 W/O : 2021 70/1) R & R EPSU (12WL) IAW AMM 33-51-38-400-001-A AND PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK
DURING HEAVY MAINTENANCE, DISCHARGED BATTERY OF EPSU 13WL; (REF. AERO N/R 2021-134068 W/O:2021 70/1) R & R BATTERY OF EPSU (13WL) I.A.W A.M.M 33-51-38-400-001 AND PERFORMED BITE TEST I.A.W A.M.M 33-51-00-710-001. TEST IS OK.
DURING HEAVY MAINTENANCE, R2 DOOR ESCAPE SLIDE CANNOT BE PINNED SAFELY DUE TO ROTATED REGULATOR; (REF. AERO N/R 2021-133886 W/O: 2021 70/1) R & R EMERGENCY EVACUATION ESCAPE SLIDE RAFT DOOR 842 IAW AMM 25-62-44-400-803-A. SUPPLEMENTAL INFORMATION TO FOLLOW.
DURING HEAVY MAINTENANCE, INOP EPSU 12WL; (REF. AERO N/R 2021-134069 W/O : 2021 70/1) R & R EPSU (12WL) IAW AMM 33-51-38-400-001-A AND PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK
FLT 225, JFK-TPA. EMERGENCY LIGHT BATTERY ON EPSU 11WL AND 13WL FAILED TEST. R & R EMER LIGHT BATTERY ON EPSU 11WL AND 13WL REF AMM 33-51-38. OPS CHKS OK.
FLT 225, JFK-TPA. DURING WEEKLY (EMER LIGHT TEST ) FOUND FWD R1 DOOR ESCAPE SLIDE LIGHTING FAULTED (ESCAPE SLIDE LIGHTING). PERFORMED AN OPS CHECK IA AMM 25-62-44-710-064A. OPS CHECK OK AS WELL AS AMM 33-51-00-710-001-A OPS CHECK OK. MDDR CLEAR MS-4 UPDATED PLACARD REMOVED.
FLT 225, JFK-TPA. EMERGENCY LIGHT BATTERY ON EPSU 11WL AND 13WL FAILED TEST. R & R EMER LIGHT BATTERY ON EPSU 11WL AND 13 WL REF AMM 33-51-38. OPS CHKS OK.
FLT 1348, SJU-DCA. RED OVERWING EXIT EMERGENCY SEAT MARKER LIGHTS INOP; R & R EMERGENCY LIGHT POWER SUPPLY 12WL REF AMM 33-51-38. OPS CHECK GOOD.
FLT 2128, MCO-EWR. CIDS PANEL INDICATING RED DUAL LGTS ON THE INDICATION CAUTION BUTTON; FOUND AFT L SLIDE BOTTLE EMPTY (SLIDE NOT BLOWN). R & R AFT L SLIDE BOTTLE 7506MM PER AMM 25-62-46 OPS CK GOOD. OKAY FOR SERVICE.
EMERGENCY LIGHT LENS MISSING. INSTALLED THE LENS IAW AMM 25-65-00.
FWD LT EPSU UNIT FAULT WHEN PERFORMING EMERGENCY LIGHT TEST. R & R THE EPSU IAW AMM 33-51-38.
R2 DOOR TOP EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT ASSY OPS CHECKED GOOD IAW AMM 33-51-13.
FT # 170, FLL-BOS. RED INCANDESCENT EMERGENCY ESCAPE PATH LIGHT MOUNTED ON 9D IS INOP; R & R EMERGENCY LIGHT ASSY ON SEAT 9D I.A.W M.M 33-51-19. OPS CHECK OK.
L1 DOOR EMERGENCY LIGHT NOT ILLUMINTATED AND L1 DOOR SILL LIGHT ILLUMINTAED AT ALL TIMES. R2 DOOR EMERGENCY SIGN LIGHT NOT ILLUMINTAED AND R2 DOOR SILL LIGHT ILLUMINATED AT ALL TIMES. FOUND WIRING FOR L1 DOOR MISWIRED. CORRECTED EMERGENCY LIGHT AND EMERGENCY SIGN PER ASM 33-51-00 LIGHTING OPS CK GOOD. FOUND WIRING FOR R2 DOOR MISWIRED. CORRETED EMERGENCY LIGHTS AND EMERGENCY SIGN PER ASM 33-51-00 LIGHTING OPS CK GOOD.
DURING HEAVY MAINTENANCE, EMERGENCY LIGHTS AT SEAT ROWS 9 -11 LT & RT FAILED TO TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY 12WL. OPS CHECKED GOOD IAW AMM 33-51-38.
DURING HEAVY MAINTENANCE, FOUND THE RT ELEVATOR NR 2 HINGE ARM STRAP CRACKED. REMOVED AND REPLACED THE STRAP ASSY IAW SRM 51-44-11.
DURING HEAVY MAINTENANCE, FOUND THE RT WING NR 3 SLAT DENTED AT BULLNOSE OTBD END. REPAIRED THE SLAT IAW SRM 57-44-21-300-005.
DURING INSTALLATION FWD LEFT SLIDE ON TASK CARD A320-25-62-44-400-803A. SLIDE BECAME UNRAVELED. DEEMING IT UNSERVICEABLE.IAW AMM 25-62-01. REPLACED THE LT FWD ESCAPE SLIDE ASSY IAW AMM 25-62-41.
EMERGENCY LIGHTS FAILED TO TEST. R & R THE BATTERY IAW AMM 33-51-38.
EMERGENCY LIGHTS FAILED TO TEST. R & R THE BATTERY IAW AMM 33-51-38.
VERY STRONG ODOR OBSERVED FROM AIR CONDITIONING SYSTEM, DURING DESCENT BELOW 15000 FEET UNTIL LANDING. ODOR IS SIMILAR TO SWEATY SOCKS. R & R BOTH RECIRCULATING FILTERS IAW AMM 21-21-14. PERFORMED CHECK. CHECK PASSED. NO FURTHER ODORS NOTED.
R1 DOOR SILL FORWARD GIRT BAR ATTACHMENT HAS CORROSION AT ALL 4 EA HOLES. REMOVED CORROSION AT ALL 4 EA HOLES ON R1 DOOR SILL FORWARD GIRT BAR ATTACHMENT.
AFT CABIN RT FLOORBEAM -1292 TRIPLE BEAM HAS CORROSION FRAME 68-FRAME 69, STR 23R. R & R AFT CABIN RT FLOORBEAM -1292 TRIPLE BEAM FROM FRAME 68-FRAME 69, STR 23R.
AFT CABIN RT FLOORBEAM -1292, TRIPLE BEAM HAS CORROSION FRAME 66-FRAME 68, STR 23R. R & R AFT CABIN RT FLOORBEAM -1292 TRIPLE BEAM FROM FRAME 66-FRAME 68, STR 23R.
AFT CABIN LEFT FLOORBEAM HAS CORROSION AT 4" FORWARD OF FRAME 70, 765. R & R AFT CABIN LT FLOORBEAM 765 FROM FRAME 65-FRAME 70.
L1 DOOR SILL AFT GIRT BAR ATTACHMENT HAS CORROSION AT ALL 4 HOLES. REMOVED CORROSION AT ALL 4 EA HOLES ON L1 DOOR SILL AFT GIRT BAR ATTACHMENT.
L1 DOOR SILL FORWARD GIRT BAR FITTING ATTACHMENT HAS CORROSION AT FORWARD AND AFT OTBD HOLES. REMOVED CORROSION AT FORWARD AND AFT OTBD HOLES ON L1 DOOR SILL FORWARD GIRT BAR FITTING ATTACHMENT.
R1 DOOR SILL AFT GIRT BAR ATTACHMENT HAS CORROSION AT AFT INBD HOLES. REMOVED CORROSION AT AFT INBD HOLES ON R1 DOOR SILL AFT GIRT BAR ATTACHMENT.
AFT CABIN LT FLOORBEAM 1292, TRIPLE BEAM HAS CORROSION FRAME 66-68, STR 23L. R & R AFT CABIN LT FLOORBEAM 1292, TRIPLE BEAM FR66-68, STR23L.
AFT CABIN LT FLOORBEAM 1292 TRIPLE BEAM HAS CORROSION AT FRAME 64-66, STR 23L. R & R AFT CABIN LT FLOORBEAM 1292 TRIPLE BEAM AT FRAME 64-66, STR 23L.
AFT CABIN FLOOR STRUCTURE RT SHEAR PLATE SUPPORT HAS CORROSION AT LOWER SURFACE FR70. REMOVED OLD SHEAR PLATE AFT CABIN RT, FOUND TO BE OUT OF LIMITS, FABRICATED NEW SHEAR PLATE.
AFT CABIN LT FLOORBEAM 1292, TRIPLE BEAM HAS CORROSION AT FRAME 68-69, STR 23L. R & R AFT CABIN LT FLOORBEAM 1292, TRIPLE BEAM FROM FRAME 68-69, STR23L.
AFT CABIN FLOOR STRUCTURE LT SHEAR PLATE SUPPORT HAS CORROSION AT LOWER SURFACE FRAME 70. R & R AFT CABIN FLOOR STRUCTURE LT SHEAR PLATE SUPPORT.
DURING MAINTENANCE FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 9DEF INOPERATIVE. FOUND WIRING PULLED FROM CONNECTORS AT LIGHT ASSY, REPLACED TERMINALS IAW ESPM 20-48-14 AND RECONNECTED. PERFORMED OPS TEST OF EMERGENCY LIGHT SYS IAW AMM 33-51-00. ALL OPS NORMAL.
RETURNED TO DEPARTURE, DUE TO DC BUSS 1 ECAM FAULT INTERMITTENT. R & R NR 1 SDAC IAW AMM 31-55-34. OPS CHECK GOOD. PERFORMED A HIGH POWER ASSURANCE TEST IAW AMM 71-00-710-013.
AIR RETURN DUE TO ENG 1 BLEED LEAK. ACCOMPLISHED TSM 36-22-00-810-803-A. FOUND THERMOSTAT SOLENOID 10HA1 LEAKING. R & R THE SOLENOID IAW AMM 36-11-55. LEAK AND OPS CHECKED NORMAL.
FOUND A DRILL START ON STRINGER 2L, SIX INCHES FORWARD OF FRAME 51. REMOVED STRINGER BETWEEN FRAME 50 AND 53. PERFORMED STRINGER REPAIR IAW A14-606-01, ER14-04271 AND SRM 53-00-13.
DURING A HEAVY MAINTENANCE CHECK, FOUND LT FUSELAGE SIDE BOX BEAM FLANGE AT STRINGER 15L FRAME 43, CRACKED, VERIFIED. CUT OUT DAMAGE. HFEC INSP ACCOMPLISHED. INSTALLED PRESSURE PLATE AND NEW FITTINGS. ALL WORK ACCOMPLISHED IAW SB A320-53-1251/EC A320-53-1251-01.
DURING CLIMB, TEMPORARY ELECTRICAL ODOR WAS NOTICED IN COCKPIT AND CABIN. PERFORMED ELECTRICAL BURN ODOR INSPECTION IAW TSM 24-00-00-810-823A, FOUND CABIN NR 1 RECIRCULATION FAN CIRCUIT BREAKER X18 TRIPPED. REMOVED & INSTALLED A NEW RECIRCULATION FAN ASSY IAW AMM 21-21-51-400-001-A. REMOVED & INSTALLED A NEW 10HG LT FAN FAULT RELAY AS PRECAUTION IAW WDM 21-21-01 & 21-21-02. OPS CHECKED NORMAL.
FLT 11 JFK-FLL, MAINTENANCE FOUND EMERGENCY EXIT MARKER LIGHT AT SEAT 9DEF FOUND INOP. RE-ATTACHED CONNECTOR AS REQUIRED. OPS CHECK NORMAL PER AMM 33-51-00.
FLT 415 BOS-SAN, FLIGHT ATTENDANT OBSERVED ELECTRICAL BURNING SMELL FROM ONE COFEE POT IN REAR GALLEY. REMOVED AND REPLACED NR 1 AFT COFFEEMAKER AS REQUIRED.
FLT 180 PHX-JFK, CREW QUICKLY DONNED OXYGEN MASKS AND REQUESTED AN EXPEDITED DESCENT DUE TO PRESSURIZATION PROBLEMS. CABIN V/S FLUX BETWEEN +- 1700 FT/MIN ABOVE FL 300. BOTH PACK FLOWS WERE HIGH WITH RIGHT PACK FLUX BETWEEN HIGH AND LOW SLOWLY BLEED PSI AND OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE IAW MM 21-51-51. OPS AND LEAK CHECK OK.
FLT 836 STI-JFK, STRONG INTERMITTENT ODOR ON CLIMBOUT (HORRID, RUBBER ODOR) INFLIGHT DECK AND FWD GALLEY, DISAPPEARED AFTER RACK POWER TO OFF. COMPLIED WITH TSM 23-39-00-810-801 "ELECTRICAL ODOR OR FUMES IN THE CABIN DUE TO LIVE TV SYSTEM" NO FAULTS FOUND. NO ODOR NOTICED. ALSO PERFORMED TSM 24-00-00-810-823, TSM 26-15-00-810-804, NO FAULTS FOUND. PERFORMED BITE TEST OF DU'S PER 31-63-22 NO FAULTS NOTED.
FLT 826 SDQ-JFK, CEILING AND AFT MOUNTED EXIT SIGNS FLICKERING LAST 30 MINUTES OF FLIGHT AND EMERGENCY FLOOR LIGHTING. AS PER TSM 33-51-00-810-819 CHANGED RELAY 8WL PER TROUBLESHOOTING PARA 4, A. OPS CHECK GOOD OF EMERGENCY LIGHTING SYSTEM. NO FURTHER FAULTS NOTED AT THIS TIME. OK FOR CONT SERVICE. OPS CHECK GOOD AS PER AMM REF 33-51-00-710-001.
FLT 700 - SJU-JFK - LTV TURNED OFF DUE TO A BURNING PLASTIC SMELL AROUND ROW 2 OR 3. SMELL WENT AWAY SHORTLY AFTER TV'S TURNED OFF. C/W TSM TASK 23-39-00-810-801. NO VISUAL OR SMELL OF BURNING PLASTIC XEB AT 2ABC SEEMED TO BE OPERATING AT A HIGHER TEMP THAN OTHER XEB'S. AS A PRECAUTION, REMOVED AND REPLACED XEB AT 2ABC IAW LTV MM 44-20-17. OPS CHECK GOOD.
FLT 640, SFO-JFK, DIVERTED TO LGB, ENG 1 AND ENG 2 BLEED FAULTS DURING TAKEOFF DEPARTURE PHASE, ENG 2 BLEED FAULT OCCURRED FIRST. REPLACED NR 2 ENG THERMOSTAT FIN7170HM2. LEAK CHECK GOOD. REF AMM 36-11-06. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE THERMOSTAT FOR TROUBLESHOOTING IAW 36-11-43-04 71770HM1. LEAK CHECK OK. (S)
FLT 718, SJU-JFK, BETWEEN 20:00 TO 23:00 Z, CUSTOMER COMPLAINED INFLIGHT, CONFIRMED ODOR BURNING, FROM ROW 10 FORWARD, LIVE TV WAS DEACTIVATED AND ODOR DISSIPATED. PERFORMED TSM 23-39-00-810-801, TASK 4.C, REPORT OF ELECTRICAL ODOR THROUGHOUT CABIN ALSO INSPECTED ALL LIVE TV COMPONENTS AND CABLES FROM ROW 12 TO ROW 1 ABC AND DEF, NO DEFECTS NOTED INSPECTION LIMITED TO CABIN ONLY NOT BEHIND SIDEWALLS. PERFORMED TSM TASK 24-00-00-810-823. NO ABNORMALITIES FOUND IN CABIN OR GALLEYS. NO ODOR EVIDENT THROUGHOUT CABIN. OK TO CONTINUE.
CABIN CREW REPORTED BURNING SMELL IN VICINITY OF ROWS 21-22 DEF. LIVE TV TURNED OFF, SMELL DISSIPATED. PERFORMED TSM 23-39-00-810-801. REMOVED AND REPLACED SEB 22E. OPS GOOD. NO SMELLS NOTED.