N603JB
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 1471 LGA-FLL. STRONG PERSISTENT FUMES FROM 12,000 UNTIL LANDING. DIRTY SOCK SMELL. ATTEMPTED TO ISOLATE PACK 1 WAS UNSUCCESSFUL. SMELLED BY BOTH PILOTS. FA'S DID NOT SMELL IN THE CABIN. LEVEL II FUME EVENT; COMPLIED WITH INFO/ NOTICE 2017-T015. IDENTIFIED SOURCE AMBIENT AIR TYPE 10. INSP APU, WHEEL WELLS, LOWER FUSELAGE, TAIL SECTION. ALL FOUND IN CLAEN CONDITION. COMPLIED WITH LVL A ECS DECON. CABIN AIR QUALITY GOOD.
FLT 1471 LGA-FLL. STRONG PERSISTENT FUMES FROM 12,000 UNTIL LANDING. DIRTY SOCK ODOR. ATTEMPTED TO ISOLATE PACK 1 WAS UNSUCCESSFUL. SMELLED BY BOTH PILOTS. FA'S DID NOT ODOR IN THE CABIN. LEVEL II FUME EVENT; COMPLIED WITH INFO/ NOTICE 2017-T015. IDENTIFIED SOURCE AMBIENT AIR TYPE 10. INSP APU, WHEEL WELLS, LOWER FUSELAGE, TAIL SECTION. ALL FOUND IN CLEAN CONDITION. COMPLIED WITH LVL A ECS DECON. CABIN AIR QUALITY GOOD.
FLT 2252, SJU - SJU. LEVEL 1 ODOR EVENT, FWD GALLEY & ROWS 1 - 5. COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1. ISOLATED FAULT TO TYPE 10, POSIBLE SOURCE PASSENGER OR CREW HYGIENE , WIPE OUT SEATS COVERS FROM ROW 1 TO 5 FOLLOWED TSM 05-50-00-810-085-B AND AIRCRAFT IS OK FOR SERVICE.
FLT#2137. JFK-STI. (AN EMERGENCY WAS DECLARED) "GREEN HYD SYS LOW INFLIGHT. L/G GRAVITY EXTENDED" (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#1510, SDQ-JFK. 'ON DESCENT -CAB PR EXCESS CAB ALT -DOOR L AFT CABIN -DOOR R AFT CABIN; REF SUBSEQUENT L/P'S 9217, 9218 FOR T/S & R&R OF COMPONENTS, AFTER T/S AND PRECAUTIONARY R&R OF CPC1 SDAC 1 DIFFERENTIAL PRESS SQ. PERFORMED CABIN PRESSURIZATION TEST PER AMM 05-53-00-780-002-A01. NO ABNORMALITIES WERE NOTED, ALL ECAM INDICATIONS WERE NORMAL. THIS CLEARS THE ITEM ON FOR CONTINUED SVC.'
DURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON LH FUSELAGE SKIN AT FR 23 AND 1.5" ABOVE STGR 22; REF WO # 1283758 NR # 00230 DENT ON LH FUSELAGE SKIN AT FR23 AND 1.5" ABOVE ON STGR 22 WAS EVALUATED & FOUND OUT OF LIMITS I.A.W A320 S.- R.M. 53-11-11-283-012 FIG.006 (SHEET 1) REV.-148 FEB-01-2024. DENT LH FUSELAGE SKIN AT FR23 AND 1.5" ABOVE ON STGR 22 WAS REPAIRED I.A.W A320 S.R.M. 53-11-11-300-041 REV.- 148 FEB-01-2024. THIS REPAIR IS PERMANENT WITH CATEGORY B, INSPECTIONS REQUIRED AT 60,000FC/ 120,000FH FROM TIME OF REPAIR EMBODIMENT, WHICHEVER OCCURS FIRST I.A- .W. A320 SRI 53-11-11-205-037 REV.148 FEB-01--2024.FUR ASSIGNED FUR-A320-53-01328 ACFH 71435 ACFC 25499.
DURING HEAVY MAINTENANCE: LH SIDE FR 66 AND STGR 14 AT UPPER HOLE OF GUSSET PLATE AND FRAME, WITH CRACK INDICATION; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00014) REF MEXICANA WO 1283758 NR # 00233 LH SIDE FR66 AND STGR 14 AT UPPER HOLE ON GUSSET PLATE AND FRAME WAS REPAIRED I.A.W A320 SRM 53-41-12-300-018 REV.148 FEB 01/2024. THIS REPAIR IS CATEGORY B; INSPECTION REQUIRED AT 8600FC/17200FH, INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT, INTERVAL 8600FC/17200FH INSPECTION METHOD ROTOTEST I.A.W. A320 SRI 53-41-12-205-019 TABLE 2 REV.148 FEB-01-2024.AC FH 71435 ACFC 25499 AT TIME OF FUR CREATION. FUR ASSIGNED FUR-A320-53-01329.
DURING HEAVY MAINTENANCE: LH FR68 DOOR STOP FITTING #1 WITH CRACK INDICATION; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00020) REF MRO WO# 1310910,1283- 758. N/R# 00255. LH FR68 DOOR STOP FITTING #1 WAS REPAIRED I.A.W. A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-010 REV.148 FEB 01/24. THIS REPAIR IS CATEGORY B, INSPECTION THRESHOLD 24 500FC FROM REPAIR EMBODIMENT, INSPECTION INTERVAL 10 700FC, INSPECTION METHOD HFEC I.A.W. A320 SRI 53-- 41-12-205-009 REV.148 FEB 01/24.
DURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON RH FUSELAGE SKIN BETWEEN FR2 AND FR3 AT 14" BELOW OF STGR RH SIDE; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00001) FUR CREATED # FUR-A320-53-01269, REF MEXICANA WO1310910, 1283758, NRC 00228, : DENT ON RH FUSELAGE SKIN AT FR3 AND 14" BELOW RH LATERAL STGR WAS REPAIRED I.A.W. S.R.M. 53-11-11-300-041 REV- .148 FEB-01-24. THIS REPAIR IS CATEGORY B, INSPECTIONS REQUIRED AT 60,000FC / 120,- 000FH FROM TIME OF REPAIR EMBODIMENT, WHICHEVER OCCURS FIRST I.A.W. S.R.M. 53-- 11-11-205-037 REV.148 FEB-01-24. ACC BY A04242 - AGUILAR RECAMIER, ALINE METZERI 09APR24. INSP BY A03131 VALDEZ ALVAREZ MAURICIO 30MAR24 ACC BY A04242 - AGUILAR RECAMIER, ALINE METZERI 09APR24. INSP BY A03131 VALDEZ ALVAREZ MAURICIO 30MAR24.
DURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON LH FUSELAGE SKIN AT FR23 AND 1.5" ABOVE STRG 22; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00004) REF MEXICANA WO 1310910, 1283758, NRC 00230. DENT ON LH FUSELAGE SKIN AT FR 23 AND 1.5" ABOVE ON STGR 22 WAS REPAIRED IAW A320-SRM 53-11-11-300-041. REV 148. REPAIR IS PERM CAT B. INSPECTION REQUIRED AT 60,000FC / 20,00FH FROM REPAIR EMBODIMENT WHICHEVER COMES FIRST IAW A320 SRI 53-11-11-205-037 REV 148 FUR A320-53-01295 ASSIGNED.
DURING HEAVY MAINTENANCE: INITIAL FINDING. CORROSION ON SEVERAL POINTS BETWEEN FR16 AND FR20 ON - Y30 AND -Y51.5; REF MEXICANA WO # 1283758 AND NR # 00236 BETWEEN FR16 AND FR20 ON SEAT TRACK Y1292 WAS REPLACED I.A.W. A320 SRM 51-72-11 REV 148 FEB/01/24.
FLT#1130, FLL-CHS. ' (L) REAR DOOR OPEN ON ECAM AT ABOUT 2500 FEET MSL PRESSURE SHOWED VS- ALONG WITH VS OF A/C ON FINAL APPROACH; ACCOMPLISHED INSP ON AFT LH DOOR SEAL INSP SEAL FOUND TO BE OK REMOVED DEBRIS AND CLEANED SEAL REF AMM 52-13-11. ACCOMPLISHED CABIN PRESSURIZATION TEST IAW AMM 05-53-00-780-001-A. NO DEFECTS OR LEAKS NOTED NO ECAM DOOR MSG IAW TSM 52-13-00, MCC NOTIFIED.'
FLT#2085, BDL-MIA. 'DURING DESCENT THROUGH 10,000 FT A MODERATE CHEMICAL ODOR WAS NOTICED ODOR WAS TRANSIENT & GONE AFTER LANDING ( APU BLEED AIR SUPPLY SYSTEM); BP PERFORMED APU COMPRESSOR WASH AS PER TC A320-49-20-00-100-004 ON WO 1234163.
FLT#1447, HPN-TPA. 'INFLIGHT REPORTS STRONG "MAGIC MARKER SMELL" IN FWD GALLEY FAINT IN AFT GALLEY ON FINAL LASTED ABOUT 5-10 MINUTES; "COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10,(A),1, C PER TSM 05-50-00-810-085-B TSM 05-00-00-810-085-D AIRCRAFT IS OK FOR SERVICE.'
DURING HEAVY MAINTENANCE, (REF A320-52-1145-02) CRACK INDICATION ON EMERGENCY EXIT DOOR 843 AFT SEGMENT IN PASSENGER CABIN; (REF AEROMAN WO 2021-10/1, NE # 2021-55913) ACCOMPLISHED MODIFICATION RE-INFORCE DOOR STRUCTURE ON EMERGENCY EXIT 843 IAW SRM 51-42-11 AND EC A320-52-1144-02
DURING HEAVY MAINTENANCE, (REF A320-52-1145-03) CRACK INDICATION ON EMERGENCY EXIT DOOR 834 FWD AND AFT SEGMENT IN PASSENGER CABIN; (REF AEROMAN WO 2021-10/1, NR # 2021-55855) ACCOMPLISHED MODIFICATION RE-INFORCE DOOR STRUCTURE ON EMERGENCY EXIT 834 IAW SRM 51-42-11 AND EC A320-52-1144-03.
DURING HEAVY MAINTENANCE, (REF A320-52-1145-01) CRACK INDICATION ON EMERGENCY EXIR DOOR 833 AFT SEGMENT IN PASSENGER CABIN; (REF AEROMAN WO 2021-10/1, NR # 2021-5591) ACCOMPLISHED MODIFICATION REINFORCE DOOR STRUCTURE ON EMERGENCY EXIT 833 IAW SRM 51-42-11 AND EC A320-52-1144-01.
FT # 1818, POS-JFK. RH EPSU BATTERY FALED BITE TEST; R & R RH EPSU BATTERY IAW AMM 33-51-38 OPS CHECK GOOD.
DURING HEAVY MAINTENANCE, WAS FOUND WITH CORROSION DAMAGE ON THE RT WING TOP SKIN PANEL 2 UPPER SURFACE ALONG THE REAR SPAR AND TRAILING EDGE OVERHANG RIBS 10-12 & 16-17. THE DAMAGE WAS OUTSIDE THE LIMITS OF REF /5/ SRM REPAIR. CONTACT VIA REF /4/ DOSSIER AND WAS PROVIDED WITH REF /2/ RDAS & REF /3/ TD WHICH PROVIDES REPAIR INSTRUCTION TO BLEND OUT THE CORROSION DAMAGE AND INSTALL A REPAIR PLATE. THIS REPAIR IS TEMPORARY AND PENDING 6 MONTH DTA ANALYSIS. ISSUED REF /1/ EA TO ACCOMPLISH THE REPAIR AS PER REF /3/ TD WITHOUT DEVIATION. EC A19-299-01 ACCOMPLISHES THE REPAIR AS PER REF /1/ EA WITHOUT DEVIATION. EC A19-299-02 TRACKS THE 6 MONTH DTA; THIS TEMPORARY REPAIR HAS BEEN APPROVED BY REF /2/ RDAS AND IS CLASSIFIED AS MAJOR.
AFT MAIN PAX CABIN FLOOR SUPPORT Y1292, FRAMES 66-68 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-11.
AFT MAIN PASSENGER CABIN, FLOORBEAM AT FRAME 68, HAS CORROSION. R & R FLOORBEAM AT FRAME 68, IAW SRM 51-72-11.
AFT MAIN PAX CABIN FLOORBEAM AT FRAME 66 CORRODED. R & R CORRODED FLOORBEAM IAW SRM 51-42-11, 51-72-11.
AFT MAIN PAX CABIN FLOOR SUPPORT FRAMES 68 - 69, CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-11.
AFT MAIN PAX CABIN FLOOR SUPPORT Y1292 FRAMES 66 - 68 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-11.
AFT MAIN PAX CABIN FLOOR SUPPORT Y1292 BET FRAMES 64 - 66 CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-72-11, 53-00-14.
AFT MAIN PAX CABIN FLOOR SUPPORT Y1732 AT FR 66 - 68 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11.
AFT MAIN PASSENGER CABIN FLOOR SUPPORT Y1232, FRAME 66 CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.
AFT MAIN PAX CABIN FLOOR SUPPORT Y1292, FRAMES 68 - 69 CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.
VISUAL INSPECTION L2 DOOR CUTOUT UNDERNEATH SCUFF PLATE TOP EDGE FOUND CORRODED. R & R L2 DOOR CUTOUT DOOR SILL IAW SRM 51-74-00, 51-44-11, 51-72-11.
MAINTENANCE REPORTED L2 DOOR SLIDE LOW PRESSURE. R & R SLIDE ASSY AT L2 DOOR IAW AMM 25-62-44.
FOUL ODOR FROM PACKS DURING ALL PHASES OF FLIGHT. WORST, DURING GROUND OPS AND DESCENT, APU SYSTEM. UPON INVESTIGATION, FOUND EVIDENCE OF APU GEN OIL LEAK INTO THE INLET DUCT. R & R APU GENERATOR IAW AMM 24-23-51, OPS AND LEAK CHECKED NORMAL.
DURING MAINTENANCE CHECK, FOUND LT EMERGENCY LIGHT BATTERY FAILED. REPLACED BATTERY IAW AMM 33-51-38. OPS CHECKED NORMAL.
FOD: FOREIGN OBJECT (TAPE MEASURER) EJECTED FROM EVACUATION SLIDE/RAFT FWD P/N D30664-309 S/N A9631 WHEN FLAT FIRED AS FUNCTIONAL TEST.
FLT 654 SJU-TPA, DURING MAINTENANCE EMERGENCY LIGHTS TEST SHOWS EPSU 12 WL FAILED. EPSU SELF-TEST SHOWS BATTERY FAULT. REPLACED BATTERY AND RE-TEST GOOD.
FLT 523 MCO-TPA, ON HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT AT FWD F/A'S STATION INOPERATIVE. REMOVED AND REPLACED EPSU IAW A320 AMM 33-51-38. OPS CHECK GOOD.
FLT 6415 JFK-LCQ ON GROUND FOR MAINTENANCE, REF NR 440011-32615 LT OVERWING EMERGENCY ESCAPE SLIDE CABLE FAILS TO TRAVEL REQUIRED DISTANCE & DOES NOT RETURN TO EXTENDED POSITION. SERVICED LT OVERWING ESCAPE SLIDE CABLE IAW AMM 25-62-00-03. OPS CHECK GOOD IAW 52-21-00.
FLT 6415 JFK-LCQ ON GROUND FOR MAINTENANCE, REF NR 440011-32616 RT OVERWING EMERGENCY ESCAPE SLIDE CABLE FAILS TO TRAVEL REQUIRED DISTANCE AND DOES NOT RETURN TO EXTENDED POSITION. SERVICED RT OVERWING ESCAPE SLIDE CABLE IAW AMM 25-62-00-03. OPS CHECKS GOOD IAW AMM 52-21-00.
FLT 817 JFK-SDQ, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO MCO DUE TO DURING CRUISE AT FLT FL350 RECEIVED ECAM "F/CTL ALTN LAW" (PROT LOST). T/S CFDS POST FLIGHT, FOUND ELAC NR 1 FAULTED. REMOVED AND REPLACED ELAC NR 1 PER AMM 27-93-34-04. OPS CHECK OK.
FLT 182 SAN-JFK ON MAINTENANCE CHECK, LEFT OVERWING EMERGENCY LIGHT FLICKERING AND TICKING SOUND FROM BEHIND PANEL NUMEROUS EMERGENCY LIGHT OUT. REMOVED AND REPLACED EPSU AT LEFT OVERWING ROW 11, ITEM CLEARED OPS CHECK OK PER AMM 33-51-38-04.
FLT JB510 FLL - EWR IN EWR EMERGENCY LIGHT EPSU EXT LOAD FAULT AFT LEFT DURING EMERGENCY LIGHT TEST. EWR MAINTENANCE INSTALLED CONNECTOR ON R2 DOOR SLIDE RAFT IAW 25-62-44. IAW AMM 33-51-00 EMERGENCY LIGHT PASSED NO FAULTS PRESENT. OK FOR SERVICE.
FLT JB833 JFK-STI ON APPROACH INTO STI CREW RECEIVED FLIGHT/CONTROL STABILIZER JAM AND F/CTL ELAC 2 PITCH FAULT AND AUTO PILOT DISCONNECTED. CREW MANUALLY TRIM STABILIZER AND LANDED IN DIRECT LAW SUCCESSFULLY. MX REMOVED AND REPLACED THE ACTUATOR IAW AMM 27-44-55 OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
FLT 481 BOS-LGB LTV ALL INOP DUE TO BURNING SMELL. DURING FLIGHT STRONG ELECTRICAL ODOR COMING FROM ROW 18 AND 19 AREA. TURNED ENTIRE LIVE TV OFF AND SMELL SUBSIDED. PERFORMED INSPECTION OF LIVE TV SYSTEM PER TSM 23-39-00-810-801. RAN SYSTEM FOR ONE HOUR WITH NO INDICATIONS OF ANY ODOR. REMOVED AND REPLACED XEB AT 18E AS PRECAUTIONARY PER TSM 23-39-00-810-801. OPS CHECK NORMAL PER AMM 23-39-00.
FLT 233, SLC-LGB, AFTER TAKEOFF ACFT SUFFERED A L&R AIL FAULT WITH ACFT ONLY ABLE TO FLY IN ALTERNATE LAW. PER PFR MSGS ELAC AIL ORDER DISAGREE & ELAC 2 AIL ORDER DISAGREE WERE FOUND. PER TSM 27-93-00-810-949 STEP 4A. ELAC (2CE1) NEEDS REPLACING. PERFORMED TSM 34-13-00-810-967. NO PRESENCE OF WATER WAS FOUND ON ANY OF THE ADIRS OR ADIRS AREA. REMOVED AND REPLACED ELAC 1 (2CE1) IAW 27-93-34-04. OPS TEST NORMAL THIS TIME. NO FAULTS FOUND. (S)
FLT 59, JFK-MCO, ATB TO JFK, ON TAKEOFF LANDING GEAR NOT UPLOCKED INDICATION & ECAM GEAR. GEAR FAILED TO RECYCLE. GEAR INDICATIONS NORMAL IN DOWN LOCKED POSITION. FOUND SAFETY VALVE AT FAULT. REMOVED AND REPLACED SAFETY VALVE IAW 32-31-00-810-856. ACCOMPLISHED NORMAL ALT GEAR OPERATION IAW 32-31-16-720-050, ALL FOUND NORMAL. A/C OK FOR SERVICE.