N649JB
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 | 2023-08-03 – 2023-08-03 | Operator named in NTSB report |
| JETBLUE AIRWAYS CORP | Operator | 2023-08-03 – 2023-08-03 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FLT#591, BOS-, "PACK 1 POSSIBLE OIL CONTAMINATION "DIRTY SOCK" ODOR IN COCKPIT WHEN PACK 1 IS ON; C/W INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, AMBIENT AIR, PERFORMED LEVEL DECON IRT AMM 21-00-00, PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085-D. A/C OK FOR SVC AT THIS TIME."
FLT#991, FLL-SJU. (AIRCRAFT DECLARED AN EMERGENCY INTO SJU) 'IN CRUISE AL FL 350- ECAM-CAB PR SYS 2 FAULT; REMOVED AND REPLACED CPC-2 REF AMM 21-31-34 OPS CHECK NORMAL.'
FLT#1885, BUF-MCO. 'DETECTED IN COCKPIT AND CABIN SELECTED PACK 1 OFF AND ODOR ABATED ODOR WAS MUSTY AND SMELLED OF MELTING CRAYONS; PERFORMED TROUBLESHOOTING FOUND ONE HEPA FILTER WITH OIL REPLACED BOTH HEPA FILTER AND PERFORMED DECONTAMINATION PER TSM 05-50-00 NO ODOR AT THIS TIME AND REQUESTED QC FOR ENG 1 INSPECTION ON CPC SECTION REF LOGPAGE 4315486 ITEM 2 NO EVIDENCE OF OIL FOUND A/C OK TO CONT SERVICE.'
FLT#2818, JFK-BOS. PERSISTENT LEVEL 1 PUNGENT ODOR TAXI OUT, TAKEOFF, CLIMB,DESCENT, TAXI IN.ENGINES STARTED ON APU. NO MOISTURE. FA'S DID NOT OBSERVE; COMPLIED WITH INFORMATION NOTICE 2017 -T015, SECTION A, ISOLATED FAULT TO TYPE 10, PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085D, A/C OK FOR SVC.
FLT#1793,JFK-SFO. 'DIRTY SOCK / MUSK SMELL IN COCKPIT AND MID CABIN ( APU SYSTEM ); REMOVED AND REPLACED COOLING FAN ASSY (8053KM) IAW AMM 49-52-51 OPS CHK AND LEAK CHK OK CLEANED RESIDUAL OIL FROM APU COMPARTMENT AND APU PLENUM SEAL IAW AMM 49-16-00 PERFORMED LEVEL A DECONTAMINATION OF ECS USING APU BLEED IAW AMM 21-00-00 NO SMELL NOTED THIS CLEARS THE MDDR MX-4 UPDATED PLACARD RMVD.'
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 68 LH SIDE, DOOR STOP FITTING 1 HOLE INBOARD LO WER. CRACK DIRECTION 10 OCLOCK ( VIEW LOOKING AFT; (RESOLVED ON W/O: 1292908 TASKCARD: NR-00019) REF AEROMAN NR 2024-168729 WO 2024 45/1 PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING 1 FR68 LH SIDE IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B. AREA 2 MUST BE INSPECTED AT 37900FC/FH NOT RELEVANT FROM TIME OF ADL/REPAIR EMBODIMENT, SUBSEQUENT INSPECTION AT INTERVAL OF:5300FC/FH NOT RELEVANT, INSPECTION METHOD: HFEC IAW A320 SRI 53-41-12-205-010 TABLE 006. TOOL USED NDT EQUIPMENT P/N:NORTEC 600D, S/N: 220272712, DUE DATE:NOV-28-2024, DIGITAL CALIPER P/N: 500-197-30 S/N:A23218442, DUE DATE:FEB-18-2025, MICROMETER P/N:293-344-30, S/N: 76020886, DUE DATE: FEB-25-2025, SMALL HOLE GAUGES P/N: 154-901, S/N: AE-412972, DUE DATE: SEP-23-2024, ULTRASONIC THICKNESS GAGE, P/N:45MG, S/N: 130066401, DUE DATE: OCT-05-2024 ACCOMPLISHED BY J. ARCHILA 8671320 FUR-A320-53-01266.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 68 LH SIDE DOOR STOP FITTING 1 HOLE INBOARD LOW ER CRACK DIRECTION 10 OCLOCK; (RESOLVED ON W/O: 1292908 TASKCARD: NR-00020) REF AEROMNA NR @)@$-168988 WO 2024 45/1 PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING 1 FR68 LH SIDE IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B. AREA 1 AND AREA 3 MUST BE INSPECTED AT 60000FC/FH NOT RELEVANT FROM TIME OF ADL/REPAIR EMBODIMENT, SUBSEQUENT INSPECTION AT INTERVAL OF: TBD, INSPECTION METHOD: TBD IAW A320 SRI 53-41-12-205-010 TABLE 006.(THIS TASK CARD IS GENERATED FOR TRACKING PURPOSES AREA 1 AND AREA 3 FUR-A320-53-01267.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR68 LH SIDE DOOR STOP FITTING 1 HOLE INBOARD LOWE R. CRACK DIRECTION 10 OCLOK (THIS TASK CARD IS GENERATED FOR TRACKING PURPOSES AREA 4); (RESOLVED ON W/O: 1292908 TASKCARD: NR-00021) REF AEROMAN NR 2024-168989 WO 2024 45/1 PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING 1 FR68 LH SIDE IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B. AREA 4 MUST BE INSPECTED AT 19700FC/FH NOT RELEVANT FROM TIME OF ADL/REPAIR EMBODIMENT, SUBSEQUENT INSPECTION AT INTERVAL OF:19700FC/FH NOT RELEVANT, INSPECTION METHOD: HFEC IAW A320 SRI 53-41-12-205-010 TABLE 006.(THIS TASK CARD IS GENERATED FOR TRACKING PURPOSES AREA 4) FUR-A320-53-01268.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL BTW FR 66 TO FR 68 AND AT LEVEL STR 23L AFT GALLE Y AREA (CPCP RELATED REFER TO THE MPD TASK 534195-01); REF AEROMAN NR 2024-168758 WO 2024 45/1REMOVED AND REPLACED LOWER SILL BTW FR66 TO FR68 AND AT LEVEL STR 23L AFT GALLEY AREA IAW A320 SRM 51-72-11, DWG D53480505 AND D53474250. THIS PART IS CONSIDERED PSE IAW 51-11-12. THIS REPAIR IS CATEGORY A NO REQUIRED FURTHER INSPECTION TOOL USED P/N 500-197-30 S/N A23218442 DUE DATE FEB/18/2025.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 68 RH SIDE, DOOR STOP FITTING 1 HOLE INBOARD LO WER. CRACK DIRECTION 6 O'CLOCK (VIEW LOOKING AFT); (RESOLVED ON W/O: 1292908 TASKCARD: NR-00022) REF AEROMAN NR 2024-168731 WO 2024 45/1 PERFORMED REPAIR ON FR68RH DOOR STOP FITTING 1 HOLE INBOARD LOWER IAW A320 SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B MUST BE INSPECTED AT 24,500FC/FH NOT RELEVANT FROM TIME OF ADL/REPAIR EMBODIMENT, SUBSEQUENT INSPECTION AT INTERVALS OF 10,700FC/FH NOT RELEVANT INSPECTION METHOD HFEC AND ROTOTEST IAW A320 SRI 53-41-12-205-009 TABLE 002. THIS PART IS CONSIDERED PSE IAW A320 SRM 51-11-12. TOOL USED EDDY CURRENT FLAW DETECTOR P/N NORTEC 600D; S/N 220272712 DUE DATE NOV/28/2024. DIGITAL CALIPER P/N 500-197-30 S/N A23218442 DUE DATE FEB/18/2025. SMALL HOLE GAUGES P/N 154-901; S/N AE-411360 DUE DATE FEB/11/2025. COMBINATION GAGE P/N CBG-12-2-N-1; S/N 2206025 DUE DATE NOV/30/2024. ULTRASONIC EQUIPMENT P/N 45MG; S/N 232017609; DUE DATE SEP/22/2024. ACCOMPLISHED BY AEROMAN TECH A. GUTIERREZ 8600815 RII BY J. PORTILLO QC 276 FUR-A320-53-01275.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (1) FWD LH DOOR EMERGENCY EXIT (833) CRACK LENGTH: 0.500 INCH; REF AEROMAN NR 2024-168774 WO 2024 45/1 REMOVED AND REPLACED FRAME SEGMENT (1) FWD ON DOOR EMERGENCY EXIT (833) IAW EC NO A320-52-1144 TASK CARD NO A320-52-1144-01.
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 33 AND BTW STR 43L AND STR 43R IN FWD CARGO COMPARTMENT (CPCP RELATED REFER TO THE MPD TASK 532180-01); REF AEROMAN NR 2024-168823 WO 2024 45/1 REMOVED AND REPLACED SHEAR TIE LOC. FR33 BTW STR43L AND STR43R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DWG D53231375. THIS PART IS CONSIDERED PSE IAW A320 SRM 51-11-12. FORM MX220 COMPLETED. DONE BY J. MARTINEZ 8602115 RII BY QC 360.
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 31 BTW STR 42R AND STR 43R IN FWD CA RGO COMPARTMENT (CPCP RELATED REFER TOTHE MPD TASK 532180-01); REF AEROMAN NR 2024-168828 WO 2024 45/1 REMOVED AND REPLACED SHEAR TIE LOC. AT FR31 BTW STR 42R AND STR43R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DGW D53232542. THIS PART IS CONSIDERED PSE IAW A320 SRM 51-11-12. FORM MX220 COMPLETED TOOL USED CALIPER P/N 500-752-20 S/N B20317422 DUE DATE SEP/21/2024 ELECTRONIC GAUGE P/N 547-257A, S/N 000400 DUE DATE MAR/13/2024. ACCOMPLISHED BY AEROMAN TECH 8653118 RII BY QC 420.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON AFT FRAME SEGMENT (1) AFT RH DOOR EMERGENCY EXIT (844) CRACK LENGTH: 0.4375 INCH; REF AEROMAN NR 2024-168772 WO 2024 45/1 REMOVED AND REPLACED FRAME SEGMENT (1) AFT RH DOOR EMERGENCY EXIT (844) IAW EC A320-52-1144 TASK CARD NO A320-52-1144-04.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON BOTH FRAME SEGMENTS (1), FWD RH EMERGENCY EX IT DOOR (843) CRACK LENGTH: 0.812 INCH; REF AEROMAN NR 2024-168773 WO 2024 45/1 REMOVED AND REPLACED FRAME SEGMENT (1) FWD RH EMERGENCY EXIT DOOR (843) IAW EC A320-52-114 TASK CARD A320-52-1144-02.
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR. 43R AND STR 44 IN FWD CA RGO COMPARTMENT; REF AEROMAN NR 2024-168821 WO 2024 45/1 REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR43R TO STR44 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-72-11-911-001. DWG D53232542. THIS PART IS CONSIDERED PSE IAW A320 SRM 51-11-12. TOOL USED CALIPER P/N 500-752-20. S/N B20317422 DUE DATE SEP/21/2024. FORM MX220 COMPLETED. DONE BY J. MARTINEZ 8602115.
DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / RH TOP SKIN BTWN FR 41-42 & BTWN BEAM -Y1292 - RIB 1 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION ON TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR 41 TO FR 42 AND BTW -Y1292 TO -Y1732 PASSENGER CABIN; REF AEROMANM NR 2023-168921 WO 2024 45/1 PERFORMED PERMANENT REPAIR LOC.TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR41 TO FR42 ON STIFF 17, BTW -Y1292 TO -Y1732 IAW EA 57-0087-24 PART 1. REVISION 0. EC NO A24-481-01. THIS REPAIR IS CATEGORY A. NO REQUIRED FURTHER INSPECTION. THIS REPAIR IS CONSIDERED PSE IAW A320 SRM 51-11-12. TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B16144234 DUE DATE MAR/27/2024. MICROMETER P/N 293-344-30 S/N 71736459 DUE DATE DEC/29/2024. SMALL HOLE GAUGE P/N 154-901 S/N AE-403297 DUE DATE AUG/06/2024. ULTRASONIC THICKNESS GAGE P/N 45MG S/N 232019809 DUE DATE SEP/22/2024. EDDY CURRENT EQUIPMENT P/N NORTEC 600D, S/N 210138503 DUE DATE JUL/21/2024. RADIUS GAUGE P/N S167C S/N ARE-29044. DUE DATE AUG/01/2024. DONE BY J. MARTINEZ 8602115.
DURING HEAVY MAINTENANCE: CORROSION RETRACTION ACTUATOR ATTACHMENT BRACKET ON LH MLG. (CPCP RELATED); "REF AEROMAN NR 2024-168957 WO 2024 45/1 REPAIRED BORE, LOWER AND UPPER FACES OF RETRACTION ACTUATOR ANCHORAGE FITTING LH MLG IAW A320 SRM 57-26-13-300-008. MEASURES AFTER REWORK: BORE 105.700 MM LUG THICKNESS 35.80 MM REPAIR CATEGORY C: THE LIFE LIMIT".(CONSIDERED A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 CROSSBEAM AREA LH SIDE HOLE H2 FWD GALLEY AREA; AEROMAN REPAIRED DISCREPANCY ON W/O 2024 45/1 N/R 2024-168729 BY J. MATTINEZ 8602115 AND QC318.
FLT#8358, BOG-FLL. 'DIRTY SOCKS ODOR ON DESCENT; ACCOMPLISHED INFOR NOTICE 2017-T015J PERFORMED A LEVEL C DECONTAMINATION USING ENGINE 1 AND 2 BLEED IAW TSM 05-50-00-810-831-A AND AMM 21-00-00 NO ODOR FOUND AFTER THE DECONTAMINATION PROCEDURE APU REQUIRED FURTHER T/S ON MDDR 576559. A/C IS OK FOR SVC.'
FLT#2604, SDQ-EWR. (AIRCRAFT DIVERTED TO JFK) 'IN CRUISE- ECAM HYD RES G LO LVL INDICATED TOP OF AMBER BOX; REMOVED AND REPLACED GREEN HYDRO PRESS SWITCH FIN 1151GU OPS CHECK GOOD.'
FLT#348, SLC-BOS. 'CHEMICAL SMELL LIKE DEICING FLUID ON DESCENT PASSING THROUGH 13,000 UNTIL LANDING; COMPLIED WITH INFO NOTICE 2107-T015 SECTION A ISOLATED TO TYPE 10, (A) 1, C, PER TSM 05-50-00-810-085-B AIRCRAFT IS OK FOR SERVICE.'
FLT#1233, MCO-SJU. (AIRCRAFT PERFORMED AN AIR TURN BACK) ' ON TAKEOFF, TOGA, ENG #2. AFTER ROTATION ON INITIAL CLIMBOUT ENGINE #2 "CYCLED AT LEAST 3 TIMES W/ EPR FLUXING. MOMENTARY "ENG 2 STALL" AFTER THRUSTERS BROUGHT BACK TO CLIMB, ENG RECOVERED TO NORMAL OPS; REMOVED AND REPLACED THERMOSTAT SELONOID IAW AMM 36-11-55. PERFORMED ENGINE RUN IAW AMM 71-00-00. SYS OPS CHECK NORMAL. NO COMP STALL.'
FLT#18, FLL-JAX. 'DUAL GEN FAIL ON SHORT FINAL RAT EXTENDED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#2752, SJU-TPA. ' EMERG LIGHT BATTERY 11WL FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY 11WL IAW AMM 33-51-38.'
FLT # 2693, JFK-MIA. DURING APPROACH AT 1500FT THE INFLIGHT CREW CALLED AND ADVISED OF A DIRTY SOCK SMELL VERY STRONG FROM THE EMERGENCY EXIT ROW REARWARD ; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10 PER TSM 05-50-00-810-085B/TSM 05-50-00-810-085D. AIRCRAFT IS OK FOR SERVICE
DURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT ON FUSELAGE WHEN THE DOOR IS FULLY OPENED AND L OCKED DUE TO SWELLING AT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA ( 1 EA); R & R NEW ESCAPE SLIDE DOOR 841 IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A.
DURING HEAVY MAINTENANCE, EMERGENCY POWER UNIT EPSU 11WL IN PASSENGER CABIN DOES NOT PASS TEST; REF AEROMAN N/R 2019-363259 - THE VISUAL INSPECTION OF THE WIRING OF THE TERMINAL BLOCK 7225VT-6 FOUND WIRE 3351-1780 IMPROPERLY CONNECTED AND WIRE 3351-1780 WAS CONNECTED PROPERLY ON POSITION "C" I.A.W AWM 33-51-07 SHEET 01 AND PERFORMED OPERATIONAL TEST I.A.W AMM 33-51-00-710-001, TEST IS OK.
FT 861, BOS-SJU. FUME/ODOR (SOCK ODOR) REPORTED BY CABIN CREW DURING DESCENT OUT OF 15000' ENG BLEED USED (APU OFF). C/W INFORMATION NOTICE 2017 SECTION A. A/C OK FOR SERVICE. RVR PACK 1 & 2 NO ODOR DETECTED PERFORMED EXTERIOR INSPECTION NO DEFECTS FOUND AS PER AMM 05-15-14.
FLT 788, SXM-JFK. EMERGENCY LIGHT INOP IN A/C. MULTILE CABIN LGHTS INOP. INSPECTED CABIN EMERGENCY LIGHTS UNITS AND FOUND ALL CABIN EMERGENCY BATTERIES AT FAULT. REMOVED AND REPLACED ALL CABIN BATTERIES REF AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. NO DEFECTS TO REPORT. SUPPLEMENTAL INFORMATION TO FOLLOW.
FLT 788, SXM-JFK. EMERGENCY LIGHT INOP IN A/C. INSPECTED CABIN EMERGENCY LIGHTS UNITS AND FOUND ALL CABIN EMERGENCY BATTERIES AT FAULT. REMOVED AND REPLACED ALL CABIN BATTERIES REF AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. NO DEFECTS TO REPORT. SUPPLEMENTAL INFORMATION TO FOLLOW.
FLT 788, SXM-JFK. EMERGENCY LIGHT INOP IN A/C. INSPECTED CABIN EMERGENCY LIGHTS UNITS AND FOUND ALL CABIN EMERGENCY BATTERIES AT FAULT. REMOVED AND REPLACED ALL CABIN BATTERIES REF AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. NO DEFECTS TO REPORT. SUPPLEMENTAL INFORMATION TO FOLLOW.
FLT 788 SXM-JFK. EMERGENCY LIGHT INOP IN A/C. INSPECTED CABIN EMERGENCY LIGHTS UNITS AND FOUND ALL CABIN EMERGENCY BATTERIES AT FAULT. REMOVED AND REPLACED ALL CABIN BATTERIES REF AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. NO DEFECTS TO REPORT. SUPPLEMENTAL INFORMATION TO FOLLOW.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SUPPORT, FRAME 61 + 9 AND 62, STRINGER 38R, IN THE BULK CARGO BAY. PERFORMED REPAIRS ON THE LOWER SUPPORT IAW SRM 53-41-49-300-003, FIG 001, AND EA 53-0033-18.
DURING C6 CHECK ON AIRCRAFT AT (SAL) DATED 03/18, CORROSION WAS FOUND ON THE BULK CARGO DOOR SILL BTWN FR61-62 & STR 37-38R AT THE AFT FUSELAGE. SEE REF /1/ EA FOR MORE DETAILS. CONTACTED FOR REPAIR DISPOSITION. PROVIDED REF /2/ RDAS WITH REPAIR INSTRUCTIONS PER REF /3/ SRM TASK WHICH CONSISTS OF CUT OUT DAMAGE AREA, INSTALL REPAIR DOUBLERS AND RESTORE SURFACE PROTECTION. THIS REPAIR IS APPROVED PER REF /2/ RDAS AS A TIME LIMITED REPAIR PENDING DTA, FOR PERMANENT REPAIR DISPOSITION, DUE WITHIN 6 MONTHS. THIS EC A18-177-01 ACCOMPLISHES TIME LIMITED REPAIR PER REF /1/ EA & REF /2/ RDAS WITHOUT DEVIATIONS. EC A18-177-02 IS ISSUED AS PLACEHOLDER FOR PERMANENT REPAIR, PENDING DTA IN 6 MONTHS; THIS TIME LIMITED REPAIR, PENDING DTA WITHIN 6 MONTHS, IS APPROVED PER REF /2/ RDAS AND CLASSIFIED AS MAJORâ
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + Y765, AT FRAME 16 + 2. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-42-11, DRAWING D53112812, AND SRM 51-72-11.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, +Y765 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, DRAWING D53112812, SRM 51-72-11.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SUPPORT, FRAMES 61 + 9 AND 62, STRINGER 38R IN THE BULK CARGO BAY. PERFORMED REPAIRS IAW SRM 53-41-49-300-003, FIG 001, AND EA 53-0033-18.
STRONG ACRID ODOR APPARENT DURING DESCENT AT 1100 FT, BOTH PILOTS OBSERVED ODOR BUT CABIN DID NOT. PERFORMED AN OPS CHECK IAW AMM 12-33-21. NO ODORS NOTED. AIRCRAFT IS OK FOR SERVICE.
FLIGHT ATTENDANT SMELLED A DIRTY SOCK ODOR AFTER APU BLEED AIR TURNED ON. THE ODOR WAS DETECTED RIGHT AFTER TAKEOFF AND 1:36 HOURS INTO FLIGHT, DESCENDING +20 UGH 200 HP. BLEED VALVE OPEN, DIRTY SOCKS ODOR REPEATED 230-190. CONTINUED DURING FINAL APPROACH PHASE. PERFORMED INFO NOTICE 2017-T015B, AND ISOLATED THE ODOR TO APU. PERFORMED TSM 49-00-81-810-874-A. FOUND AN OIL LEAK FROM THE OIL COOLING FAN AND CONTAMINATION OF COOLING FAN DISCHARGE DUCTING. REMOVED AND REPLACED THE COOLING FAN ASSY IAW AMM 49-52-51, AND CLEANED DUCTING, OPS & LEAK CHECKED OK. R & R THE NR 1 & 2 PACK CONDENSERS IAW AMM 21-52-32. OPS NORMAL. R & R NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. OPS NORMAL.
FLIGHT ATTENDANT SMELLED A DIRTY SOCK ODOR AFTER APU BLEED AIR TURNED ON. THE ODOR WAS DETECTED RIGHT AFTER TAKEOFF AND 1:36 HOURS INTO FLIGHT, DESCENDING +20 UGH 200 HP. BLEED VALVE OPEN, DIRTY SOCKS ODOR REPEATED 230-190. CONTINUED DURING FINAL APPROACH PHASE. PERFORMED INFO NOTICE 2017-T015B, AND ISOLATED THE ODOR TO APU. PERFORMED TSM 49-00-81-810-874-A. FOUND AN OIL LEAK FROM THE OIL COOLING FAN AND CONTAMINATION OF COOLING FAN DISCHARGE DUCTING. REMOVED AND REPLACED THE COOLING FAN ASSY IAW AMM 49-52-51, AND CLEANED DUCTING, OPS & LEAK CHECKED OK. R & R THE NR 1 & 2 PACK CONDENSERS IAW AMM 21-52-32. OPS NORMAL. R & R NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. OPS NORMAL.
FLIGHT ATTENDANT SMELLED A DIRTY SOCK ODOR AFTER APU BLEED AIR TURNED ON. THE ODOR WAS DETECTED RIGHT AFTER TAKEOFF AND 1:36 HOURS INTO FLIGHT, DESCENDING +20 UGH 200 HP. BLEED VALVE OPEN, DIRTY SOCKS ODOR REPEATED 230-190. CONTINUED DURING FINAL APPROACH PHASE. PERFORMED INFO NOTICE 2017-T015B, AND ISOLATED THE ODOR TO APU. PERFORMED TSM 49-00-81-810-874-A. FOUND AN OIL LEAK FROM THE OIL COOLING FAN AND CONTAMINATION OF COOLING FAN DISCHARGE DUCTING. REMOVED AND REPLACED THE COOLING FAN ASSY IAW AMM 49-52-51, AND CLEANED DUCTING, OPS & LEAK CHECKED OK. R & R THE NR 1 & 2 PACK CONDENSERS IAW AMM 21-52-32. OPS NORMAL. R & R NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. OPS NORMAL.
FLIGHT ATTENDANT SMELLED A DIRTY SOCK ODOR AFTER APU BLEED AIR TURNED ON. THE ODOR WAS DETECTED RIGHT AFTER TAKEOFF AND 1:36 HOURS INTO FLIGHT, DESCENDING +20 UGH 200 HP. BLEED VALVE OPEN, DIRTY SOCKS ODOR REPEATED 230-190. CONTINUED DURING FINAL APPROACH PHASE. PERFORMED INFO NOTICE 2017-T015B, AND ISOLATED THE ODOR TO APU. PERFORMED TSM 49-00-81-810-874-A. FOUND AN OIL LEAK FROM THE OIL COOLING FAN AND CONTAMINATION OF COOLING FAN DISCHARGE DUCTING. REMOVED AND REPLACED THE COOLING FAN ASSY IAW AMM 49-52-51, AND CLEANED DUCTING, OPS & LEAK CHECKED OK. R & R THE NR 1 & 2 PACK CONDENSERS IAW AMM 21-52-32. OPS NORMAL. R & R NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. OPS NORMAL.
FLIGHT ATTENDANT SMELLED A DIRTY SOCK ODOR AFTER APU BLEED AIR TURNED ON. THE ODOR WAS DETECTED RIGHT AFTER TAKEOFF AND 1:36 HOURS INTO FLIGHT, DESCENDING +20 UGH 200 HP. BLEED VALVE OPEN, DIRTY SOCKS ODOR REPEATED 230-190. CONTINUED DURING FINAL APPROACH PHASE. PERFORMED INFO NOTICE 2017-T015B, AND ISOLATED THE ODOR TO APU. PERFORMED TSM 49-00-81-810-874-A. FOUND AN OIL LEAK FROM THE OIL COOLING FAN AND CONTAMINATION OF COOLING FAN DISCHARGE DUCTING. REMOVED AND REPLACED THE COOLING FAN ASSY IAW AMM 49-52-51, AND CLEANED DUCTING, OPS & LEAK CHECKED OK. R & R THE NR 1 & 2 PACK CONDENSERS IAW AMM 21-52-32. OPS NORMAL. R & R NR 1 & 2 PACK OZONE FILTERS IAW AMM 21-51-41. OPS NORMAL.
DIVERTED, AT DEPARTURE ALL HYDRAULIC SYS INDICATED FULL. WHILE ENROUTE HYD G RESERVOIR INDICATES APPROX 1/8 ABOVE AMBER, LOW INDICATION. QTY REDUCTION WAS APPROXIMATELY 1 MM PER 10 MINUTE INTERVALS. RECOVERED TO 3 MM BELOW FULL AT SHUTDOWN; SERVICED GREEN SYSTEM HYDRAULICS IAW AMM 12-12-29. RAN ALL GREEN SYSTEM USERS INCLUDING FLT CTRLS, BRAKE SYS AND GEAR DOORS WITH NO LEAKS FOUND. CONFIRMED GREEN HYDRAULIC QTY INDICATION IN THE FLIGHT DECK AND RESERVOIR QUANTITY READ THE SAME. ALL IAW AMM 29-11-00.
DURING MAINTENANCE, EMERGENCY LIGHT WAS TESTED AND FAILED TEST. R & R BATTERY PACK AT FORWARD 10WL AND AFT 13WL IAW AMM 33-51-38. PERFORMED SECOND TEST. LIGHT PASSED.
DURING MAINTENANCE, EMERGENCY LIGHT WAS TESTED AND FAILED TEST. R & R BATTERY PACK AT FORWARD, 10WL AND AFT, 13WL IAW AMM 33-51-38. PERFORMED SECOND TEST. LIGHT PASSED.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT Y765 AFT OF FRAME 67+3". REMOVED AND REPLACED THE FLOOR SUPPORT.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT Y1292 AFT OF FRAME 67+5. REMOVED AND REPLACED THE FLOOR SUPPORT.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM Y765 AT FR 68. REMOVED AND REPLACED THE FLOORBEAM.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM Y503 AT FRAME 16 AT LAV MOUNT. R & R THE FLOORBEAM.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON RT SHEAR WEB FRAMES 69-70 AT STR 23R. R & R THE SHEAR WEB.
FLT 171 JFK-SMF, FLIGHT CREW REPORTED ELECTRICAL SMELL IN AFT COFFEE POT AREA. REMOVED POWER AND PULLED 3 CB'S AND SMELL DISSIPATED. ACCOMPLISHED TSM 24-00-00-810-823-A, FOUND COFFEEMAKER INOP. REMOVED AND REPLACED NR 1 AFT COFFEEMAKER IAW A320MM 25-35-15. OPS CHECK OK.
FLT NR 718, SJU-JFK, ENROUTE AT FL360 FA'S SMELLED A BURNING RUBBER SMELL BETWEEN ROWS 11-16 NEAR TOP OF AC. SMELL WAS EVIDENT FOR APPROX 15 MINUTES, THEN DISSIPATED. INSPECTED CABIN FOUND THAT PASSENGER ITEMS BLOCKING LIVE TV BOX UNDER ROW 12 PRODUCED EXCESSIVE HEAT AS SOURCE OF SMELL. ALL VISUAL CHECK OK AT THIS TIME.