N665JB
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 462, SJU-BOS. FA'S REPORT THE ODOR OF A SWEET SMOKE IN THE AFT GALLEY DURING DECENT TILL LANDING. LAVS UNOCCUPIED AT THE TIME. ; ACCOMPLISHED INFO NOTICE 2017-T015M. VERIFIED NO ODOR PRESENT & NO RECENT HISTORY. DETERMINED TO BE MISC TYPE 10 TABLE 2 REF TSM 05-50-00. FLIGHT CREW DID NOT FILL OUT FORM. ACFT OK FOR CONT SERVICE.
FLT 1141 BDL-PBI, NR 4 F/A REPORTED ODOR FINAL APPROACH PILOT DID NOT EXPERIENCE ANY ODOR. ACCOMPLISHED INFO NOTICE 2017-T015M. VERIFIED ODOR NOT TO BE PRESENT AND NO HISTORY OF ODOR EVENTS. DETURMINED TO BE MISCELLANEOUS TYPE 10 PER TABLE 2.NO CORRECTIVE ACTION REQUIRED PER TSM 05-50-00-810-085B/TSM 05-50-00-810-085-D.AIRCRAFT IS OK FOR SERVICE.
FLT#369, BOS-FLL. 'LEVEL 2 ODOR EVENT DESCENDING THROUGH 20000FT. STRONG ODOR PRIMARILY FRONT CABIN AND COCKPIT. DIRTY SOCK. UTILIZED ODOR ISOLATION CHECKLIST. ODOR RETURNED AFTER 5 MINUTES AND LINGERED IN FRONT AND REAR OF AIRCRAFT FOR REMAINDER OF FLIGHT APPROXIMATELY 3 MINUTES. ALL CREW NOTICED. NO PAX COMPLAINTS; APPLIED TSM 05-50-00-810-085B , COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B`2 . IDENTIFIED ODOR COMING FROM APU BLEED SYSTEM . DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-085B /05-50-00-810-085. A/C OK FOR SERVICE.'
FLT#1098, MCO-LGA. 'OILY - CHEMICAL SMELL OBSERVED STARTING AT TOP OF DESCENT; C/W INFO NOTICE 2017-T015L. PERFORMED T/S IAW TSM 05-50-00-810-831-A. DETERMINED TO BE A TYPE 1 (APU). REF. TO LP 4238107, ITEM 2 FOR FINDINGS. APU REMAINS ON MEL. NO FURTHER DEFECTS NOTED. C/W LEVEL A DECONTAMINATION IAW AMM 21-00-00-615-802-A. NO ODORSS NOTED AT THIS TIME.'
FLT#436, STI-JFK. 'AT 10,000FEET ON DECENT AA STRONG DIRTY SOCKS SMELL WAS REPORTED BT THE FLIGHT ATTENDANTS IN THE FORWARD AND MID CABIN. THE ODOR WAS ALSO OBSERVED IN THE FLIGHT DECK. THE ODOR WAS FAINT IN THE FLIGHT DECK, APU WAS NOT ON; PERFORMED DETAILED VISUAL INSPECTION OF APU/COMPARTMENT, ENGINES 1 AND 2 PER INFO NOTICE 2017-T015-L. REPLACED BOTH RECIRCULATION FILTERS PER AMM 21-21-41. PERFORMED PACK BURN PER CABIN INFO NOTICE. NO ABNORMAL FINDINGS FOUND. ONLY RESIDUAL OIL IN THE APU. PER MCC REQUEST APU WILL REMAIN ON MEL. ALSO REQUEST APU COMPRESSOR WASH FROM BP. PREVIOUSLY ON MEL WILL REMAIN OPEN.'
FLT#1469, BUF-PBI. 'ADVISED BY INFLIGHT CREW AT GATE THAT DURING APPROACH,CREW EXPERIENCED FUME EVENT BELOW 10K. DESCRIBED THE SOURCE AS EMINATING FROM AFT CABIN AND MOVED FORWARD SYMPTOMS FROM CREW DESCRIBED AS EYE IRRITANT AND SLIGHT HEADACHES DUE TO OIL SMELL. APU WAS NOT ON; COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2, IDENTIFIED OIL ODOR PERFORMED DECONTAMINATION LEVEL A IAW TSM 05-50-00-810-831-A. REPLACED RECIRCULATION HEPA FILTERS IAW AMM 21-21-41. NO ODOR PRESENT.
FLT#1519, BOS-MIA. 'ODOR/FUMES TRANSIENT IN CLIMB. DISSIPATED PACK 1 SELECTOR OFF RETURNED WITH DELECTION OF PACK 1 IN DECENT BECAME LEVEL 2-3 WITH APU AND PACKS; C/W INFO NOTICE 2017-T015, SECTION B2 IDENTIFIED ODOR REPLACE RECIRCULATION FILTERS DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-085-B A/C OK FOR SVC MDDR CLEARED MX-4 UPDATED/PLACARD REMOVED.'
FLT#667, HPN-PBI.' ODOR REPORTED BY INFLIGHT NOTED AT 3;13 LOCAL THROUGHOUT CABIN MEDIUM INTENSITY DURATION 15 MINUTES CHEMICAL /DIRTY SOCK SMELL NOTED ON APPROACH NO NOTED PHYSIOLOGICAL EFFECTS EMITTED IN PSUS; COMPLIED WITH INFO NOTICE 2017-T015 SE3CTION B2 TSM 05-50-00-810-831-1 R/R HEPA FILTERS & CW ECS DECONTAMINATION IAW 21-00-00-615 ALL CKS NORMAL NO SMELL NOTED.'
FLT#2093, JFK-MIA. 'WET SOCK ODOR IN COCKPIT ON DESCENT ALSO ODOR IN CABIN; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, AMBIENT AIR ODOR, PER TSM 05-50-00-810-085-B AND -D. PERFORMED LEVEL 2 DECONTAMINATION. AIRCRAFT IS OK FOR SERVICE. MCC JI NOTIFIED.'
DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOC. AT LEVEL BTW RIB 7 TO RIB 8 ON RH WING; REF AEROMAN W/O 2023 363/1 N/R 2023-749626 EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOCATED AT LOWER BTW RIB 7 TO RIB 8 ON RH WING IAW A320 SRM 57-21-11-283-007 FIGURE 004 SHEET 1 THIS EVALUATION IS CATEGORY B AND INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AT 20.000 FC 40,000 FH AND SUB SEQUENT INSPECTION AT INTERVALS OF 9.000 FC 18.000 FH METHOD OF INSPECTION DETAIL VISUAL INSPECTION IAW SRI 57-21-11-205-007 TABLE 001 WORK DONE BY AEROMAN SAL ON W/O 2023 363/1 N/R 2023-749626 WORK ACCOMPLISHED BY AEROMAN TECH M.SHUL 8632015 AND RII C.BELTRAN 420 FUR-A320-57-01076.
DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE WEB LOC. BTW FR69/FR70 AT LEVEL STR23R AT AF T GALLEY AREA (1 EA) (CPCP RELATED, REFER TO MPD TASK 534195-01); REF AEROMAN WO 2023 363/1 NR 2023-749950 REMOVED AND REPLACED STRUCTURE WEB (FRAME SUPPORT) LOC. BTW FR69 TO FR70 AT LEVEL STRG23R AFT GALLEY AREA I.A.W. A320 SRM 51-42-11 AND DWG D53470100 WORK ACCOMPLISHED BY AEROMAN TECH 8632015 RII ACCOMPLISHED BY AEROMAN QC R MURILLO 222.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 843 CRACK L=0.365; REF: W/O 2023 363/1 N/R 2023-749593 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMENTS IAW A320 SRM 51-42-11 AND SRM 51-42-11.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. FR60 ON DOOR CUT OUT IN BULK CARGO COMPT; REF. AERO WO: 1256626 / 2023-749878 - PERFORMED PERM. REPAIR LOC. FR61 +0.064" ON LOWER SILL BULK CARGO COMPT. IAW A320 SRM 53-41-49-300-003 PROCEDURE 2A FIG 001 SHT 1 & SHT2 CAT.B. REPAIR AND REQUIRED INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60000FC /120000FH SUBSEQUENT INSP AT INTERVALS OF TBD. IAW SRI 53-41-49-205-003 TBL 001.FUR-A320-53-01118 ASSIGNED.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 844 CRACK L= 0.380 IN; REF: ARM W/O 2023 363/1 N/R 2023-749600 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMENTS IAW A320 SRM 51-42-11 SND SRM 51-42-11.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 834 CRACK L=0.300IN; REF: ARM W/O 2023 363/1 N/R 2023-749598 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-1144, R&R SEGMENTS IAW A320 SRM 51-42-11 AND SRM 51-42-11.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN BOTH FRAME SEGMENT (1) OF THE EMERGENCY EXIT HATCH DOOR 833 CRACK L=0.375 IN; REF: ARM W/O 2023 363/1 N/R 2023-749595 ACCOMPLISHED REINFORCEMENT DOOR STRUCTURE MODIFICATION IAW EC A320-52-11444, R&R SEGMENTS IAW A320 SRM 51-42-11 AND SRM 51-42-11.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 AT AFT GALLEY AREA (FR 68 LH STOP DOOR 1, INBOARD/ LOWER HOLE , DIRECTION OF CRACK IS 6 OCLOCK, LENGTH OF CRAC K IS: 0.118 INCHES APPROX); (RESOLVED ON W/O: 1256626 TASKCARD: NR-00011) REF: ARM W/O 2023 363/1 N/R 2023-749786 PERFORMED PERMANENT REPAIR ON FRAME 68 AT AFT GALLEY AREA (FR 68 LH STOP DOOR 1, INBOARD/ LOWER HOLE IAW A320 SRM 53-41-12-300-008 AND A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B AND INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 37900 FC (FH IS NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS 5300 FC (FH IS NOT RELEVANT), INSPECTION METHOD HFEC IAW A320 SRI 53-41-12-205-010 TABLE 006 AND FIGURE 001 (SHEET 9). FUR-A320-53-01119 ASSIGNED.
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 AT AFT GALLEY AREA FR 68 RH STOP DOOR 1 I/B LOWER HOLE CRACK INDICATION IS 5 O'CLOCK, NENGTH OF CRACK IS .127 INCHES; (RESOLVED ON W/O: 1256626 TASKCARD: NR-00009) REF: ARM W/O 2023 363/1 N/R 2023-749785 PERFORMED PERMANENT REPAIR ON FRAME 68 AT AFT GALLEY AREA (FR 68 RH STOP DOOR 1 INBOARD/ LOWER HOLE IAW A320 SRM 53-41-12-300-008 AND A320 SRM 53-41-12-300-011. THIS REPAIR IS CATEGORY B AND INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 37900 FC (FH IS NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS 5300 FC (FH IS NOT RELEVANT), INSPECTION METHOD HFEC IAW A320 SRI 53-41-12-205-010 TABLE 006 AND FIGURE 001 (SHEET 9). FUR-A320-53-01117 ASSIGNED.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. FR61 PLUS 9 INCHES ON DOOR CUT OUT IN BULK CARGO COMPARTMENT; REF.AERO W/O 1256621 / 2023-749879 - PERFORMED PERM REPAIR LOC. FR61 PLUS 9.510" ON LOWER SILL, BULK CARGO COMPT, IAW A320 SRM 53-41-49-300-003. PROCEDURE 2A FIG 001 SHT 1 & SHT2. THIS REPAIR IS CAT B & REQ'D INSP THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT 60000FC / 120000FH SUBSEQUENT INSP @ INTERVALS OF TBD, IAW A320 SRI 53-41-49-205-003 TBL 1. FUR-A320-53-01120 ASSIGNED.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC FR60 PLUS 11 INCHES ON DOOR CUTOUT IN BULK CARGO COMPARTMENT; REF: ARM W/O 2023 363/1 N/R 2023-749877 PERFORMED PERMANENT REPAIR LOC. FR 60 PLUS 10.908 INCHES ON LOWER SILL BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49-300-003 PROCEDURE 2A FIGURE 001 SHEET 1 AND SHEET 2. THIS REPAIR IS CATEGORY B 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 A320 SRI 53-41-49-205-003 TABLE 001. FUR -A320-53-01116 ASSIGNED.
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. BTW FR66/FR68 AT LEVEL STR23R AFT GALLEY ARE A (1 EA) (CPCP RELATED, REFER TO MPD TASK 534195-01); PERFORMED PERMANENT REPAIR LOC. LOWER SILL AT LEVEL STR23R BTW FR 67 TO FR 68 AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001 PROCEDURE 2.A THIS REPAIR IS CATEGORY A AND NOT FURTHER INSPECTION REQUIRED.
FLT#573, EWR-TPA. 'AFT EMER. LIGHT BATTERY (13WL) FAILED EMER. LIGHT TEST; REMOVED AND REPLACED AFT EMER. LIGHT BATTERY (13WL) IAW AMM 33-51-38. THE OPS CHECK IS GOOD. A/C OK FOR SERVICE.'
FLT#884, MCO-JFK. 'EMERGENCY EXIT LIGHTS ARE ON IN THE ARMED POSITION. CYCLING LIGHTS OFF AND BACK TO ARM DID NOT FIX THE LIGHTS; REMOVED AND REPLACED EMERGENCY LIGHT SWITCH 4WL IAW ESPM 20-45-21. OPS CHECK GOOD REF AMM 33-51-00.'
FLT #1134, SJU-MCO. DURING EMER LT TEST REQUIRED BY R1 SLIDE R&R TEST FAILED W/ FWD ESPU L FAIL T/S IAW TSM 33-51-00-810-808-A FOUND L1 DOOR SLIDE LIGHTS CAUSING FAULT; R&R FWD LH DOOR SLIDE REFERENCE AMM 25-62-44-400-007-A OPS CHKS GOOD REFERENCE AMM 25-62-44-710-061-A & 33-51-00-710-001
FLT 2427, EWR-MCO. ALL PAX ECTRIC OUTLETS INOP FAILURE ASSOCIATED WITH BURNING RUBBER SMELL IN CABIN. POSSIBLY ORIG. NEAR ROW 5; FOUND OUTLET AT 5F BROKEN. R & R OUTLET AT 5F PER AMM 44-22-43 OPS CK GOOD. ACCOMPLISHED ELEC. INSP OF IFE SYST. IN ROW 5 AREA PER ESPM 20-52-10. CKS OK ALL OUTLET UNITS CK OK.
DURING HEAVY MAINTENANCE, REF EC A5109057-01. A320 AGING AIRCRAFT PROGRAM FCBS REPAIR SURVEY AND IDENTIFICATION WING SLATS. EXISTING REPAIRS SLAT 1 SKIN ON LH WING; REF AEROMAN NR 2019-329064. EVALUATED REPAIR PER SRM 57-40-00-300-007 FIG 001 SHEET 7 AND SHEET 9. REPAIR DOES NOT MEET CURRENT SRM. REMPAIR WAS REMOVED AND RE- ACCOMPLISHED PER SRM 57-40-00-900-033 FIG 001 SHEET 2 AND AIRBUS MSG 806935801006. NO ADDITIONAL ACTION REQUIRED AS THIS IS A REPAIR "A" CATEGORY.
DURING HEAVY MAINTENANCE, REF EC A5109057-18, EXISTING REPAIR SLAT 3 EXTERNAL SKIN ON RH WING; REF AEROMAN NE 2019-329067, EVALUATED EXISTING REPAIR ON SLAT 3 EXTERNAL SKIN ON RH WING AND FOUND OUT OF LIMITS NOT MEETING SRM REQUIREMENTS SRM A320-57-40-00-300-006. REMOVED REPAIR AND REPLACED WITH NEW REPAIR IAW EA 57-0495-19 AND SRM 57-40-00-300-025. JETBLUE EC A19-851-01 ACCOMPLISHED. THIS REPAIR IS CLASSIFIED AS MAJOR.
EMERGENCY EXIT SIGN AT THE L1 DOOR, MOUNTED ON THE AFT WALL OF LAVATORY. FOUND THE LAMPS BURNED OUT. REPLACED THE LAMPS IAW AMM 33-51-16. OPS CHECKED OK.
CABIN EMERGENCY LIGHT TEST FAILED. R & R THE EMERGENCY LIGHT BATTERIES 12WL AND 13WL IAW AMM 33-51-38. SYSTEM OPS CHECKED GOOD.
CABIN EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHT BATTERIES 12WL AND 13WL IAW AMM 33-51-38. SYSTEM OPS CHECKED GOOD.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, + Y 765, FRAME 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y1162.5, FRAME 67. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWGSD534-72780, AND D534-72089.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y 765, FRAMES 66 TO 67. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y 765, FRAMES 66 TO 67. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CORROSION FLOOR BEAM -Y 1162.5 AT FR 67 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y 1162.5 AND FASTENERS AT FR 67 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472780 AND D53472089.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CORROSION LOWER SILL AT FR66 STR 23R AT AFT GALLEY AREA. REPLACED LOWER SILL BTW FR 66 TO FR 68 STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, + Y512, FRAME 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472815.
FWD EMERGENCY EXIT SIGNS DO NOT ILLUMINATE WHEN TESTED. R & R THE FWD RT EPSU IAW AMM 33-51-38. CHECKED NORMAL.
FWD EMERGENCY EXIT SIGNS DO NOT ILLUMINATE WHEN TESTED. R & R THE FWD RT EPSU IAW AMM 33-51-38. ALL CHECKED NORMAL.
EMERGENCY LIGHTS FAILED TO TEST. R & R THE BATTERY PACK AT 11WL LEFT. CHECKED OK IAW AMM 33-51-38.
CREW & PAX REPORTED AN ELECTRICAL BURNING ODOR, ORIGINATED BETWEEN 10000FT AND LANDING GEAR EXTENSION AND PRESISTED THROUGH ENGINE SHUTDOWN AND APU START ODOR CONCENTRATED IN AFT OF AIRCRAFT. PERFORMED TSM 05-50-00-810-831 ISOLATED CAUSE OF ODOR TO TYPE 9 ELECTRICAL BURNING ODOR. ACCOMPLISHED INSPECTION FOR ELECTRICAL BURNING ODOR IAW TSM 24-00-00-810-823-A. NO DEFECTS NOTED.
DIVERTED DUE TO NR 2 CENTER TANK PUMP, NR 2 FAULT. R & R CONTACTOR FOR THE CENTER TANK NR 2 PUMP IAW ESPM 20-46-50. OPS TESTED GOOD IAW AMM 28-21-51-710-052-A.
ON CLIMBOUT, ENGINE 1 COMPRESSOR VANE ON ECAM. FOLLOWED QRH. IN CLIMB EPR FLEX EGT NR 1 100 DEGREES HIGHER THAN ENGINE 2. NR 1 ENGINE N2 PERCENT 86.6 AND ON NR 2, 84.4. R & R ENGINE NR 1. ALL OPS CHECK FOUND OK. NOTE: ON APPROACH INTO PBI PILOT DECLARED AN EMERGENCY.
DURING HEAVY MAINTENANCE CHECK, RT OVERWING SLIDE MANUAL RELEASE FAILED CHECK. ADJUSTED HORN END OF CONDUIT HOUSING TO TOP OF HATCH BRACKET INNER RELEASE CABLE IAW AMM 25-62-43. PULL TEST CHECKED OK.
FLT 6491 ON HEAVY MAINTENANCE CHECK FOUND LEFT OVERWING SLIDE RELEASE CABLE FAILED OPS CHECK. REPLACED CABLE AS PER TASK CARD A320-53-1227-01.