N661JB
Registered owner: JETBLUE AIRWAYS CORP, NY (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
FLT 772, CUN-BOS. DOOR SLIDES R2 SHOWS DISARMED IN FLIGHT THIS A REPEAT WRITE UP A FL 370 7 PSI DOOR SHOWED ARMED AFTER LANDING ; R & R R2 DOOR PROXIMITY SWITCH, PERFORMED OPS CHKD ON GORUND, FOUND WORKING GOOD AT THIS TIME. IAW AMM 52-73-11
FLT 8582, SAL-FLL. DOOR SLIDE R2 INDICATION SHOWS ARMED ON THE GROUND, BUT AS SOON AS CAB PRESS REACHES 6.0, IT SHOWS DISARMED (6.0 PSI); REMOVED & REPLACED R2 ESCAPE SLIDE RAFT PACK ASSY IN REF. AMM 25-62-44, OPS CHK GOOD. AS PRECAUTIONARY, PRESSURIZED A/C IN REF. AMM 321-31-00 TO VERIFY THE ARMED SLIDE INDICATION, DOOR REMAINS ARMED AS NORMAL. A/C OK FOR CON'T SVC.
DURING HEAVY MAINTENANCE, DOES NOT PASS TEST OF EMERGENCY LIGHT EPSU LH AT PASSENGER CABIN ; REF AEROMAN WO# 2026-267/1 NR 2026-305064 REMOVED AND REPLACED BULB IAW AMM 33-51-15-000-001-A. AND AMM 33-51-15-400-001-A. AND PERFOMED OPERATIONAL TEST EMERGENCY LIGHT IAW AMM 33-51-00-710-001-A. TEST IS OK (JOB CARD 335100-06-1-JB)
DURING HEAVY MAINTENANCE, DOOR SLIDE "R2" INDICATION SHOWS ARMED ON THE GROUND, BUT AS SOON AS CAB PRESS REACHES 6.0, IT SHOWS DISARMED (6.0 PSI); REMOVED & REPLACED R2 ESCAPE SLIDE RAFT PACK ASSY IN REF. AMM 25-62-44, OPS CHK GOOD. AS PRECAUTIONARY, PRESSURIZED A/C IN REF. AMM 321-31-00 TO VERIFY THE ARMED SLIDE INDICATION, DOOR REMAINS ARMED AS NORMAL. A/C OK FOR CON'T SVC.
FLT#655. SYR-MCO. GOING THROUGH 6500 WE HAD FUMES EVENT IDLE THRUST APU OFF SMELLED LIKE DIRTY SOX/MUSTY ODOR; C/W INFO NOTICE 2017-T015M PERFORMED LEVEL A APU ODOR INSPECTION PER AMM TASK 49-00-00-200-812-A NO LEAKS FOUND ISILATED FAULT TO TYPE 10 AMBIENT AIR DURING FLIGHT PER AMM TSM 05-50-00-810-085B/TSM 05-50-00-810-085-D A/C OK FOR SVC.
FLT # 62 PBI- MCO. " AT CRUISE FA+PAX SMELLED BURNING/SMOKE NOTHING VISIBLE LOCATION WAS AROUND ROW 16-20 FA WERE NOT ABLE TO LOCATE SOURCE ALL ELECTRICAL PAGE INDICATIONS NORMAL DISSIPATED AFTER APPROCH 15-20 MIN.; COMPLIED WITH INFO NOTICE 2017-T015 STEP 1 ISOLATED FAULT TO TYPE 10 CABIN ITEMS PER TSM 05-50-00-810-085 AIRCRAFT OK TO CONT SRV."
FLT#887, JFK-SXM. "STRONG ODOR DIRTY SOCK SMELL ON APPROACH AT 7500 FEET; C/W INFO NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10 ODOR ENVIRONMENTAL. NO 30-DAY HISTORY. PERF LEVEL A ECS DECON IAW TSM 05-50-00-810-085-B. A.C OK FOR SVC. MCC LEO NOTIFIED."
FLT#38, SJO-FLL. 'EMERGENCY LIGHT EPSU WONT BITE TEST; REMOVED AND REPLACED DEU UNIT B FIN 300RH1 REF AMM 23-73-48. OPS CHECK GOOD. TEST OF EMERGENCY LITS'S OK REF AMM 33-51-00.'
FLT#38, SJO-FLL. 'EMERGENCY LTS INOP IN MID CABIN + RH OVER WING DOOR; REMOVED AND REPLACED MID R/H EMERGENCY PSU BATTERY REF AMM 35-51-38.'
FLT#729, BQN-MCO. 'FO & I EXPERIENCED DIRTY SOCK SMELL ( ODOR) AFTER PROLONGED IDLE DESCENT. ( PACKS ); PERFORMED INFO NOTICE 2017-T015 STEP B2 INSPECT APU COMPARTMENT WITH BLACK LIGHT TOOL INSPECT ENGINE 1 & 2 FOR OIL LEAKS, REPLACED FILTHER AS NECESSARY PER TSM 05-50-00-810-831 PERFORMED ALL AMM, IPC & GMM POLICIES & PROCEDURES MDDR CLEARED NO ODOR DETECTED MX-4 UPDATED PLACARD REMOVED.'
FLT#533, BDL-TPA. 'DIRTY SOCK SMELL UPON DECENT W/ SINGLE PACK ON ENGINE BLEEDS. APU BLEED AT GATE ALSO SMELLED; LEVEL "A" ODOR EVENT CLASSIFIED TYPE 1. MOST POSSIBLE CAUSE IS THE APU. ACCOMPLISHED DECONTAMINATION OF ECS IAW AMM 21-00-00-615-802A. COUPLED WITH INFO NOTICE 2017-T015-J, SECTION B2. DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER (TEMPORARY) AMM 21-00-00-615-802A. A/C OK FOR SERVICE.'
FLT#TPA-HPN. (AIRCRAFT DIVERETED TO JFK) 'A/C DIVERTED DUE TO FCU BEING LOCKED UP; REMOVED AND REPLACED FCU IAW AMM 22-81-12. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.'
FLT#2129, JFK-RSW. ' ODOR IN REAR OF AIRCRAFT MUSTY SMELL TURNED OFF PACK 2 AND IT SMELL DISSIPATED. ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#471, LGA-FLL. 'FUME EVENT AT 6000 FT LEVEL OFF PACKS 1 AND 2 ON. PROMINENT IN FLIGHT DECK FDW AND AFT GALLEYS; PLEASE REFER TO CORRECTIVE ACTIONS AND INSPECTIONS ACCOMPLISHED ON L/P 3867592 ITEMS 1 (W/O 1299560 SERVICE CHECK, APU WASH, APU COMP CLEANING, ECS DECON ACCOMPLISHED) AND 2 INFO NOTICE 2017-T015-J COMPLIED WITH.'
FLT#2625, RDU-FLL. 'LEVEL 2 FUME EVENT, STRONG PERSISTENT MAGIC MARKER SMELL FROM TOD UNTIL 8000, SUSPECT PACK 1; REF TSM 05-50-810-831-A, FOUND TO BE AN AMBIENT ODOR WHICH OCCURRED DURING FLIGHT PHASES WITH CHANGES IN HUMIDITY. DEBRIEFED CABIN CREW, NO FINDING OF ODOR NOTICED. FOUND TO BE TYPE 10 ODOR EVENT.'
FLT#2157, LGA-DEN. (AIRCRAFT DIVERTED TO JFK) 'EPR FAULT ENG 2 ( EPR CONTROL MODES ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE AT LEVEL STR. 22R IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING Ã1 CRACK DIRECTION 8 AND 12 O CLOCK; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00012 ) REF AEROMAN NR 2023-393765 WO 2023 228/1 PERFORMED REPAIR ON FRAME 68 RH SIDE AT LEVEL STR. 22R IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING # 1 AFT GALLEY AREA I.A.W A320 SRM 53-41-12-300-010. THIS REPAIR IS CLASSIFIED AS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT AT 24,500 FC/ FH NOT RELEVANT); SUBSEQUENT INSPECTION AT INTERVALS OF 10,700 FC/ FH NOT RELEVANT; INSPECTION METHOD: HFEC AND ROTOTEST IAW A320 SRI 53-41-12-205-009, TABLE 002. TOOL USED: DIGITAL CALIPER P/N 500-197-30 S/N A21043178 DUE DATE FEB-13-2024; SMALL HOLE GAUGE P/N 154-901 S/N AE- 412979 DUE DATE JUL-15-2023; EDDY CURRENT EQUIPMENT, P/N: NORTEC 600D, S/N: 210138003, DUE DATE: MAR-27-2024; EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE DATE: MAR-12-2024; MICROMETER P/N: 293-831-30, S/N: 71150743, DUE DATE: NOV-17-2023; ULTRASONIC THICKNESS GAGE PN: 45MG SN: 130064101 DUE DATE: OCT 12 2023. DONE BY C. PEREZ 8606212 FUR-A320-53-00808.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 LH SIDE AT LEVEL STR. 22L IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING Ã 1 CRACK DIRECTION 12 AND 5 O'CLOCK AFT GALLEY AREA; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00013 ) REF AEROMAN NR 2023-393766 WO 2023 228/1 PERFORMED REPAIR ON FRAME 68 LH SIDE AT LEVEL STR. 22L IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING # 1 AFT GALLEY AREA I.A.W A320 53-41-12-300-010. THIS REPAIR IS CLASSIFIED AS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT AT 24,500 FC/ FH NOT RELEVANT); SUBSEQUENT INSPECTION AT INTERVALS OF 10,700 FC/ FH NOT RELEVANT; INSPECTION METHOD: HFEC AND ROTOTEST IAW A320 SRI 53-41-12-205-009, TABLE 002. TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N: A21043178 DUE DATE FEB-13-2024, TOOL USED SMALL HOLE GAUGE P/N 154-901 S/N AE-412979 DUE DATE JUL-15-2023. EDDY CURRENT EQUIPMENT, P/N: NORTEC 600D, S/N: 210138003, DUE DATE:MAR-27-2024.EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE DATE: MAR-12-2024 DONE BY C. PEREZ 8606212 FUR-A320-53-00809.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC BTW FR 66 TO FR 68 AT LEVEL STR23L AT AFT GALLEY AREA (REPAIR AREA)CPCP RELATED ITEMS MPD RELATED TASK 534195/01; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00023 ) REF AEROMAN WO 2023-22/1, WO 2023-393831; PERFORMED REPAIR LOC. LOWER SILL BTW FR66 TO FR68 AT LEVEL STR23L AT AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001. TOOL USED CALIPER P/N: 500-193-30 S/N 0039250 DUE DATE MAR/27/2024.
DURING HEAVY MAINTENANCE: CRACK SHEAR PLATE LOC BTW FR69 TO FR 70 AT LEVEL STRG 23L AT AFT GALLEY AREA; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00019 ) REF AEROMAN WO 2023-228/1, NR 2023-393830; REMOVED AND REPLACED SHEAR PLATE LOC. BTW FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53474180.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 FWD AND AFT FRAME SEGMENT IN PASSENGER CABIN (2 EA); REF AEROMAN NR 2023-393688 WO 2023-228/1 ACCOMPLISHED EC # A320-52-1144, DOORS/ EMERGENCY EXIT/ OVERWING EMERGENCY EXIT HATCH (FWD RH EEH) FRAME/ REINFORCE DOOR STRUCTURE- MODIFICATION.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR 844 FWD AND AFT FRAME SEGMENT 1 IN PASSENGER CABIN (2 EA); REF AEROMAN NR 2023-383690 WO 2023 228/1 ACCOMPLISHED EC # A320-52-1144, DOORS/ EMERGENCY EXIT/ OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME/ REINFORCE DOOR STRUCTURE- MODIFICATION. DONE BY C. PEREZ 8606212.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 ON AFT FRAME SEGMENT IN PASSENGER CABIN (1 EA); REF AEROMAN NR 2023-393687 WO 2023 228/1 ACCOMPLISHED EC # A320-52-1144, DOORS/ EMERGENCY EXIT/ OVERWING EMERGENCY EXIT HATCH (AFT LH EEH) FRAME/ REINFORCE DOOR STRUCTURE- MODIFICATION.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 ON AFT FRAME SEGMENT IN PASSENGER CABIN (1 EA); REF AEROMAN NR 2023-393689 WO 2023 228/1 ACCOMPLISHED EC # A320-52-1144, DOORS/ EMERGENCY EXIT/ OVERWING EMERGENCY EXIT HATCH (AFT LH EEH) FRAME/ REINFORCE DOOR STRUCTURE- MODIFICATION.
DURING HEAVY MAINTENANCE: CRACK SHEAR PLATE LOC. BTW FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA; REF AEROMAN NR 2023-393830 WO 2023 228/1 REMOVED AND REPLACED SHEAR PLATE LOC. BTW FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53474180.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL BTW FR60 AND FR62 IN BULK CARGO COMPARTMENT (CPCP RELATED REFER TO MPD TASK 534107-01); REF AEROMAN WO 202-228/1, NR 2023-393838; PERFORMED REPAIR ON LOWER SILL BTW FR60 AND FR62 IN BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49-300-003 THIS REPAIR IS CLASSIFIED AS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL REPAIR EMBODIMENT AT 60,000 FC/ 120,000 FH; SUBSEQUENT INSPECTION AT INTERVALS OF TBD FC/ TBD FH INSPECTION METHOD TBD IAW A320 SRI 53-41-49-205-003, TABLE 001. TOOL USED DIGITAL CALIPER: P/N 500-197-30 S/N A21043178 DUE DATE FEB-13-2024. TOOL USED: EDDY CURRENT EQUIPMENT, P/N: NORTEC 600D, S/N: 210138203, DUE DATE: JUN-09-2024. ULTRASONIC EQUIPMENT USED P/N:45MG, S/N: 221860711 AND DU DATE: NOV-07-2023.FUR-A320-53-00814 ASSIGNED. (CONSIDERED AS A MAJOR REPAIR)
FLT#1015, EWR-PUJ. 'ODOR EVENT. AT 10000FT FLIGHT IDLE VMC, NO DEICING. PAX COVERED MOUTH AND NOSE, FA SMELL DIRTY SOCKS, FO ASKED IF I HAD AN UPSET STOMACH. ( PACKS ); COMPLIED WITH INFORMATION NOTICE 2017-T015J, SECTION A, ISOLATED TO TYPE 10, (A), 1, C PER TSM 05-50-60-810-085-B/TSM 05-50-00-810-085-D. THE AIRCRAFT IS OK FOR SERVICE. ALSO PERFORMED LEVEL A DECONTAMINATION CHECK AS PER AMM 21-00-00-615-802-A. MX-4 UPDATED. PLACARD REMOVED. MDDR CLEARED.'
FLT#2433, DCA-PBI. 'DIRTY SOCK ODOR REPORTED FROM CABIN CREW DURING DESCENT. THE ODOR WAS MILD AND TRANSIENT IN NATURE. ODOR ONLY NOTICED IN THE AFT GALLEY WITH PACKS ON/APU OFF; ACCOMPLISHED INFO NOTICE 2017-T015J SECTION A. ISOLATED FAULT TO TYPE 10 PER TSM 05-50-810-831A. NO ODOR IS PRESENT. NO HISTORY. A/C OK FOR SERVICE.'
FLT#670, SJC-JFK. 'AIRCRAFT HAS A "DIRTY SMELL" SMELL. TURNED APU BLEED OFF SEEMED TO GET A LITTLE LESS SMELL; REF INFO NOTICE 2017-T015I. FOUND APU TO BE THE CAUSE OF THE ODOR. APU IS LEAKING INTERNALLY. FOUND OIL WITHIN THE CENTER DRAIN TUBE & DRAIN MASS. PERFORMED LEVEL A DECON IAW AMM 21-00-00. R/R RECIRCULATION FILTERS IAW AMM 21-21-41. AND PERFORMED ANOTHER DECON IAW AMM 21-00-00. ODOR NO LONGER PERSISTS. A/C OK FOR SERVICE.'
FLT#1910, BOS-JFK. 'PER TASK CARD NO. A320-33-51-00-710-003 BATTERY CAPACITY CHECK, REMOVE BATTERY AT FIN 13WL.; REMOVED & REPLACED BATTERY PACK AT FIN LOCATION 13WL, OPS TEST OK. IAW AMM 33-51-38.'
FLT#1910, BOS-JFK. 'PER TASK CARD NO. A320-33-51-00-710-003 BATTERY CAPACITY CHECK, REMOVE BATTERY AT FIN 11WL.; REMOVED & REPLACED BATTERY PACK AT FIN LOCATION 11WL, OPS TEST OK. IAW AMM 33-51-38.'
FLT#1910, BOS-JFK. 'PER TASK CARD NO. A320-33-51-00-710-003 BATTERY CAPACITY CHECK, REMOVE BATTERY AT FIN 10WL.; REMOVED & REPLACED BATTERY PACK AT FIN LOCATION 10WL, OPS TEST OK. IAW AMM 33-51-38.'
FLT#1910, BOS-JFK. 'DURING T/C A320-33-51-00-710-003 CHECK OF THE BATTERY CAPCITY FOUND L1 DOOR SLIDE FAULTING.; REMOVED AND REPLACED L1 DOOR SLIDE. ALL REQUIRED TEST CHECKS GOOD. NO FAULTS NOTED. REF AMM 25-62-44.'
FLT#1910, BOS-JFK. 'PER TASK CARD NO. A320-33-51-00-710-003 BATTERY CAPACITY CHECK, REMOVE BATTERY AT FIN 12WL.; REMOVED & REPLACED BATTERY PACK AT FIN LOCATION 12WL, OPS TEST OK. IAW AMM 33-51-38.'
FLT 226, TPA-JFK (AIR RETURNED BACK TO TPA).SEE PREVIOUS WRITEUP ABOUT NOSE UP- FORWARD PRESSURE REQUIRED (DEFECT : 3245934) DURING CLIMB SIGNIFICANT NOSE-DOWN PRESSURE REQUIRED AT VARYING PRESSURES. WHEN TURNING OFF A/P PLANE LURCHED NOSE UP. PROBLEM OBSERVED FROM VARYING SPEEDS IN CLIMB. DURING APPROACH ISSUE WAS MINIMAL.; R & R ELAC 2 IAW TSM 27-30-00-810-853-A
FLT 533, BDL-TPA. A/C REQUIRES UNUSUAL AMOUNT OF FORWARD SIDESTICK PRESSURE DURING CLIMB & CRUISE UP TO FL280. RELEASING SIDESTICK PRESSURE CAUSES A/C TO TRIM UP. NOTED ON BOTH L & R SIDESTICKS; PERFORMED AMM TASKS 27-96-00-710-007-A AILERON DAMPING CHECK & TASK 27-96-00-710-008-A ELEVATOR DAMPING CHECK. TEST OK ON BOTH TASKS. A/C OK FOR CONTINUED SERVICE.
DURING HEAVY MIANTENANCE, (REF. AEROMAN N/R 2021-393852) CORROSION STRINGER 39R BTW FR31 TO FR32 IN FWD CARGO COMPARTMENT; (PER AEROMAN N/R 2021-393852) R & R STRINGER 39R LOC. BTW FR30 TO FR35 IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-72-11 DRAWING D53231962.
FLT 1348, EMERGENCY LIGHT POWER SUPPLY FAIL TEST UNIT FAULT; R & R LH EMERGENCY LIGHT POWER SUPPLY UNIT REF AMM 33-51-38 BITE CHECK GOOD."
FLT 1459. BDL-FLL. DIVERTED TO JFK NO EMERGENCY LANDING REQUESTED. âPASSING FL230 TO FL340 ENGINE 1 STALLED. ECAM DISAPPEARED SO WE COULDNâT RUN IT. ENGINE AT IDLE ECAM STAYED BLANKEDâ. A NORMAL LANDING. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE AND A DFDR DOWNLOAD HAS BEEN ACCOMPLISHED. R & R NR 1 ENGINE IAW T/C A320 71-00-20-000-040. OPS NORMAL OK FOR CONT SVC.
FT # 950, GND-JFK. RETURNED TO FIELD. THE A/C LANDED WITHOUT INCIDENT WITH THE #1 ENGINE SHUT DOWN. ENGINE #1 FAILED AT 400 FEET ON TAKEOFF, LOUD BANG. ENG ROLLED BACK NO FIRE ASSOCIATED; (REF WO 1039192 ON LP 2496877 ITEM 1) R & R #1 ENGINE LEAK AND OPS CHECK NORMAL REF 71-00-00.
R ROW 9 DEF EMERGENCY LIGHT INOPERATIVE. R & R ROW 9 DEF EMERGENCY LIGHT WIRE HARNESS IAW AMM 32-51-11. OPS CHECKED GOOD.
FLT 1031, BOS-HOU. CABIN ODOR ( PACKS - SINGLE (SPEEDBRAKES OK) (N503-N665) ); REF WO#1007031 TASK CARD A2117101-02 DECONTAMINATION OF ECS PERFORMED DECONTAMINATION PER TASK CARD. OPS CHECK OK FOR FLT SERVICE AT THIS TIME MCC NOTIFIED MX-4 UPDATED PLACARD REMOVED DISPATCH NOTIFIED 85067.
FLT 22, PBI-BOS. DIRTY SOCKS SMELL OB SENSED BY IN FLIGHT THROUGH 10000 FEET TO 5000 ON THE DESCENT; PERFORMED ECP DECON PER 21-00-00 AND INFO NOTICE 2017 T015E INSTRUCTIONS PROVIDED. A/C OK FOR SERVICE.
FLT 6131, SLC-LGB. FOUND R1 SLIDE FAULTING. EPSU 10WL SLIDE REQ REPLACEMENT. SLIDE PIN INSTALLED; R & R R1 ESCAPE SLIDE PER AMM 26-62-44 OPS CHECK GOOD. REMOVED ESCAPE SLIDE PINNED & STOWED.
FLT 6131, SLC-LGB. DURING TEST OF EMERGENCY LIGHTS FOUND FWD EMERGENCY LIGHTS INOP; REMOVED AND REPLACED FWD EPSU (1OWL) BATTERY. OPS TEST GOOD PER 33-51-00.
FT # 871, HALF OF THE CABIN EMERGENCY LIGHTS ARE OUT. STARTING FROM FWD GALLEY TO ROW 10. PERFORMED OPS TEST OF EPSUS PER AMM 33-51-00-740-801. TROUBLESHOT PER TSM 33-51-00-810-802-A. R & R BATTERY OF EPSU 12WL (FWD). PER AMM 33-51-38. OPS/BITE TEST OF EPSU NORMAL. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.
FLT 391, BOS-TPA. DURING WALK AROUND FOUND INTER-GRANULAR CORROSION AT RT REAR FUSELAGE AT LAV EXHAUST; REF NR 440510-38011-REPAIRED IAW SRM 53-41-11-300-004 AND EC A18-475-01. THIS REPAIR HAS BEEN APPROVED PER THE REF/4/ RDAS. PER THE MAJOR/ MINOR CLASSIFICATION THIS REPAIR IS AS A âMAJORâ
ODOR REPORTED BY F/A'S IN REAR OF ACFT DURING CRUISE FL 330. ACCOMPLISHED DECONTAMINATION OF THE ENVIROMENTAL CONTROL SYSTEM. R & R RECIRCULATION FILTERS. RAN BOTH ENGINES. NO ODORS IN CABIN. OK FOR SERVICE.
FLAPS LOCKED, ALIGNMENT FAULT ECAM DURING CONFIGURATION FOR APPROACH. PERFORMED RIGGING OF FLAP DRIVE MOTORS NR 2,3,4 RT WING, PERFORMED ADJUSTMENT OF BOTH LT & RT FLAP INTERCONNECT STRUTS. PERFORMED ADJUSTMENT OF RT APPU TO ZERO IAW AMM 27-51-00-820-001-A. ADJUSTED STRUT INTERCONNECT IAW MM 27-51-44-941-063-A. R & R IPPU IAW AMM 27-55-11. ADJUSTED FLAP TRACK NR 3, RT WING IAW AMM 27-54-00-820-053-A. RIG CHECKED OK.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON NUMEROUS PLACES FROM FRAME 69 - 70, STRINGER 23L LOCATED AFT CORNER BEHIND L2 DOOR. REMOVED CORROSION AND VERIFIED BEYOND LIMITS. REMOVED AND REPLACED IAW SRM 53-41-17, FIG 001.
DURING HEAVY MAINTENANCE, THE FWD & AFT CABIN EMERGENCY LIGHT ZONES FAILED TO FUNCTION DURING A CONTROL PANEL TEST. R & R THE EPSU BATTERIES 10WL AND 13WL IAW AMM 33-51-38. OPS CHECKED GOOD.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL FRAME 68, STRINGER 23R. REMOVED THE CORROSION AND VERIFIED BEYOND LIMITS. REPAIRED THE AREA IAW SRM 53-41-14-300-001.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT AFT SHEAR WEB FROM FRAMES 69 - 70 AFT OF R2 DOOR. REMOVED CORROSION AND VERIFIED BEYOND LIMITS. REMOVED AND REPLACED IAW SRM 53-41-17, FIG 001.
DURING HEAVY MAINTENANCE, FWD & AFT CABIN EMERGENCY LIGHT ZONES FAILED TO LIGHT DURING CONTROL PANEL TEST. R & R EPSU BATTERIES 10WL AND 13WL IAW AMM 33-51-38. OPS CHECKED GOOD.
FLT 6464, LCQ-FLL. ON APPROACH SELECTING FLAPS 2 ECAM MESSAGE F/CTL FLAPS LOCKED ALIGNMENT FAULT. DURING FLAPS OPERATION FOUND HANDLE STICKING IN NR 2 POSITION; ACCOMPLISHED ZONAL INSP OF RT WING FLAP DRIVES TORQUE TUBES CANOES AND AFT FLAP WELLS WITH A GVI IAW AMM 27-54-00, NO DEFECTS NOTED AFTER INSP. REMOVED AND REPLACED FLAP/SLAT CONTROL LEVER IAW AMM 27-51-43. NO DEFECTS NOTED.
DIRTY SOCK ODOR DESCENDING THROUGH 9000 FT, BOTH PACKS ON. ODOR DISIPATED BY 4000 FT. ACCOMPLISHED ENGINE WASH ON THE NR 1 ENGINE. TROUBLESHOOT IAW TSM 05-50-00-810-831-A, R & R THE NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. PB 401.
DIRTY SOCK ODOR WHILE DESCENDING THROUGH 9000 FT, BOTH PACKS ON. ODOR DISIPATED BY 4000 FT. ACCOMPLISHED ENGINE WASH ON NR 1 ENGINE. TROUBLESHOT IAW TSM 05-50-00-810-831-A, R & R THE NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. PB 401.
DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT EMERGENCY LIGHTS WERE OUT AT ROWS 25, 21, 17, AND 3. EMERGENCY EXIT SIGN ABOVE THE R2 DOOR WAS INOPERATIVE. EMERGENCY EXIT SIGN ABOVE THE L2 WAS INOPERATIVE. R2 SIDEWALL EMERGENCY LIGHT WAS INOPERATIVE.REPLACED THE LAMPS AT ROWS 25, 21, 17, AND 3 IAW AMM 33-51-18. REPLACED THE LAMPS AT THE R2 DOOR SIGN. FOUND EMERGENCY POWER SUPPLY UNIT TO BE FAULTY DURING TROUBLESHOOTING. R & R THE EPSU IAW AMM 33-51-38, OPS CHECKED GOOD.
UPON WEEKLY CHECK FOUND AFT EMERGENCY BATTERY INOPERATIVE. R & R EMERGENCY BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHT POWER SUPPLY TO FAIL TEST. R & R BATTERY PACK IAW AMM 33-51-00, OPS CHECKED GOOD.
FLT 651 TPA-SJU, INFLIGHT CREW REPORTS FWD LAVATORY HOT WATER HEATER EXTREMELY HOT, SMOKING IN FLIGHT. TURNED OFF HEATER AND ALL INDICATIONS FIXED. PERFORMED TSM 24-00-00-810-823 FOR ELECTRICAL BURNING SMELL IN CABIN. INSPECTED LAVATORY. FOUND WATER HEATER AT FAULT. HEATER PLACED ON NEF N25-40-01 MDDR 164244. NOTE: SUPPLEMENTAL INFO WILL BE FILED AFTER HEATER REPLACEMENT.
FLT 1206 RSW-HPN (A/C DIVERTED TO MCO) HYD GLOW LEVEL ECAM AT CRUISE FOLLOWED BY LOW PRESSURE. FOLLOWED ECAM AND QRH PROCEDURES NORMAL DESCENT, MANUAL GEAR EXTENSION, NORMAL LANDING. L/G SYSTEM BACK TO NORM MODE OK REF MM 32-00-00-02 CHECK PERFORMED. REF LOG PAGE 647497 ITEM 1 & L/P 647498 ITEM 2. PYLON HYDRAULIC PRESSURE PIPE REMOVED AND REPLACED & LEAKED CHECKED OK IAW AMM REF 29-11-49-04. RII REQUIREMENTS ACCOMPLISHED ON REFERENCE LOG PAGES. A/C OK FOR SERVICE.
FLT 134 RSW-JFK - SMALL UNCOMMANDED RUDDER MOVEMENT FELT ON RUDDER PEDAL DURING TAKEOFF ROLL. MX REPLACED CENTERING ROD SPRING PER AMM 27-21-48, ALSO PERFORMED RUDDER TRAVEL AND RETURN CHECK. ACCOMPLISHED AFS AND CAT III TEST IAW 22-97-00 AND RUDDER ARTIFICIAL FEEL LOAD TEST IAW 27-23-00-710-001 PEDAL MOVEMENTS SMOOTH AND TRIM NORMAL. A/C OK FOR SERVICE.
FLT 766, BQN-MCO, GREEN HYDRAULIC FLUID DEPLETED IN FLIGHT. GEAR MANUALLY EXTENDED. FLUID LOSS ECAM OCCURRED DURING DESCENT INTO MCO. APPROXIMATELY BELOW 30,000 FT ENGINES AT IDLE. REMOVED CASE DRAIN LINE (HYDRAULIC) FROM NR 1 ENGINE PYLON AND DISCONNECTED HYDRAULIC PRESSURE LINE FROM NR 1 ENGINE PYLON. REF IPC 29-11-06-02D ITEM 240 AND 220. HYDRAULIC CASE DRAIN LINE FOUND BROKEN AT CLAMP. INSTALLED CASE DRAIN LINE REF IPC 29-11-06-02D ITEM 240 & 220 AND TORQUED REF AMM 20-00-00. LEAK CHECK OK. RETORQUED HYD PRESS LINE IAW AMM 20-00-00. OPS CHECK OK.
OPS TEST OF EMERGENCY LIGHTS BY TEST BUTTON ON PROGRAM & TEST PANEL INOP. REMOVED & REPLACED PROGRAMMING & TEST PANEL IAW AMM 23-73-18-04, OPS TEST NORMAL, OK FOR SERVICE.