N3104J
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
Maintenance disclosures
DURING HEAVY MAINTENANCE, AC26-396-03 REAR FUSELAGE, FR 67 & STR 32L. GROUND DAMAGE. TIME LIMITED REPAIR (CONSIDERED MAJOR REPAIR)
FLT#1675, FLL-KIN. AIRCRAFT PERFORMED AN AIR TURN-BACK TO FLL. LEFT WING ANTI ICE FAIL EICAS WHEN CONDUCTING TEST ABOVE 10K FEET. AIR RETURN FLL. DID NOT LAND OVER WEIGHT; REMOVED AND REPLACED WING ANTI-ICE VALVE IAW AMP J30-12-01 LEAK AND OPS OK REQUIRES FUNCTION TEST SEE LOG 4335418 ITEM 1(ACCOMPLISHED GROUND TEST OF L/H WING ANTI-ICE AS PER REF AMP J30-12-00-01AAA-320A-A. NO FAULTS NOTED ON EICAS. A/C OK FOR SERVICE).
FLT#713, BOS-DFW. (AIRCRAFT DIVERTED TO BUF) .' WING A/ICE FAIL EICAS; REMOVED AND REPLACED R/H WAI VALVE PER AMP BD500A-J30-12-01-01AAA-720A-A.'
DURING HEAVY MAINTENANCE: FCCD STRICKER UNDER SCUFF PLATE FOUND (X2) PLACES OF CORROSION AROUND ATTACHMENT HOLES; REF TO AVIANOR WO A49144 NR 1024, FCCD FWD AND AFT LOWER CORNER STRICKERS CORROSION PERMANENT REPAIR CARRIED OUT IAW AC24-1262-01 AND IAW GREO 500-53-21-101 REV D AND REO 500-53-21-970.
DURING HEAVY MAINTENANCE: FUSELAGE / MID FUSELAGE / REAR BARREL / LOWER SKIN FR 57-58 AND STGR 36L / CORROSION - TIME LIMITED REPAIR; REFERENCES: /1/ AIRBUS CANADA REO 500-53-51-200 /2/ AVIANOR DAMAGE REPORT A49144-1096 /3/ ASRP BD500-A-J53-61-01-04AAB-661A-A /4/ AIRBUS CANADA SNIEO C00001300-S033. DESCRIPTION: DURING THE CURRENT (10/2024) C1 CHECK FOR A/C N3104J (MSN 55150) AT YMX, CORROSION WAS FOUND ON THE REAR BARREL LOWER SKIN BETWEEN FR57-58 AND STGR36L (PN: C01733918-017). SEE REF/2/, DAMAGE REPORT. THE DAMAGE WAS REVIEWED AGAINST THE REF/3/, ASRP AND NO LIMITS WERE FOUND. THEREFORE, AIRBUS CANADA WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS CANADA PROVIDED THE REF/1/, REO WITH INSTRUCTIONS TO REMOVE THE DAMAGE BY CUTTING AWAY THE CORROSION AND INSTALLING A DOUBLER AND TIPLER TO REINFORCE THE AREA, AND PERFORM REF /4/ SNIEO. AIRBUS APPROVED THIS REPAIR PER THE REF /1/ REO AS TIME-LIMITED, PENDING FURTHER DTA DUE IN 12 MONTHS. THIS EC AC24-1349-01 IS ISSUED TO ACCOMPLISH THE TIME-LIMITED REPAIR PER THE REF /1/ REO. EC AC24-1349-02 PROVIDES A PLACEHOLDER ISSUED TO TRACK THE 12-MONTH LIMITATION FOR THE DTA. SUBSTANTIATION: THIS TIME LIMITED REPAIR HAS BEEN APPROVED VIA REF/1/, REO AND IS CLASSIFIED AS MAJOR. (E/C: AC24-1349-01)
DURING HEAVY MAINTENANCE: WINGS / RH WING / FIXED LE SKIN / SLAT TRACK #6 CUTOUT / CRACK - PERMANENT REPAIR; REFERENCES:/1/ AIRBUS GREO-500-57-41-025 REV C /2/ AVIANOR NON-ROUTINE TASK CARD A49144-1079 /3/ MX-244. DESCRIPTION: DURING CURRENT C1 CHECK (10/2024) ON N3104J (MSN: 55150) @ YMX, DURING INSPECTION PHASE AVIANOR REPORTED TWO CRACK DAMAGES ON THE RH WING FIXED LE SKIN @ THE SLAT TRACK #6 CUTOUT. SEE REF /2/, NRC, FOR FULL DETAILS. CRACKS DIMENSION ARE AS FOLLOWS: 1. CRACK #1: L=0.063â 2. CRACK #2: L=0.056â. AVIANOR EVALUATED THE DAMAGE PER REF /1/, GREO AND FOUND THAT THE CRACK DAMAGE WAS WITHIN LIMITS TO UTILIZE THE METHODS OF THE GREO. THIS GREO AUTHORIZES THE PERMANENT REPAIR CONSISTING OF A DAMAGE CUT-OUT, NDT INSPECTION (LPI OR HFEC), DOUBLER AND FILLER FABRICATION AND INSTALLATION, REAPPLICATION OF CIC AND FINISH, AERODYNAMIC CHECKS, THEN A CYCLING OF THE SLATS TO ENSURE NO FOULING. AVIANOR ACCOMPLISHED THIS REPAIR WITHOUT DEVIATION, AS REPORTED ON NRC, REF /2/. EC AC24-1257-01 IS ISSUED TO ACCOMPLISH THE PERMANENT REPAIR PER REF /1/. SUBSTANTIATION: THIS PERMANENT REPAIR IS APPROVED PER REF /1/, GREO AND IS CLASSIFIED AS MINOR IAW REF /3/ MX-244 GUIDELINES. **REV 01**REFERENCES: /4/ AIRBUS GREO-500-57-41-025 REV E. EC/TC ARE REVISED TO INCLUDE THE LATEST REVISION OF THE REF /4/ GREO. WORK WAS ACCOMPLISHED AT AVIANOR TO REF /4/. NO OTHER CHANGES. ***REV 02*** ON 10/21/2024, AVIANOR REACHED OUT TO REPORT THAT THE REPAIR CLASSIFICATION PER THIS EC WAS INACCURATELY CLASSIFIED AS MINOR WHEREAS IT SHOULD BE MAJOR. UPON REVIEW, THIS EC IS BEING REVISED TO CORRECT THE REPAIR CLASSIFICATION TO MAJOR AS THE AFFECTED AREA IS IDENTIFIED AS PSE AS PER A220 ASRP BD500-A-J51-00-00-01AAA-030A-A, TABLE 23, ITEM 24 FIGURE 22. NO OTHER CHANGES EXIST. (E/C: AC24-1257-01)
DURING HEAVY MAINTENANCE: FCCD SKIN AROUND UNDERNEATH SCUFF PLATE FOUND (X9) PLACES OF CORROSION AROUND ATTACHMENT HOLES OF LOWER SCUFF PLATE; REF TO AVIANOR WO 49144 NR 1025, FCCD SKIN AROUND UNDERNEATH SCUFF PLATE TEMPORARY REPAIR CARRIED OUT I.A.W AC24-1251-01 AND I.A.W REO 500-53-21-100 REV E, DETAIL VISUAL INSPECTION TO BE CARRIED OUT AT INTERVALS NOT TO EXCEED 1000 FH AND THIS TEMPORARY REPAIR IS VALID FOR 10000 FH FROM TIME OF INCORPORATION OF REO.
DURING HEAVY MAINTENANCE: FCCD SILL UNDER SCUFF PLATE FOUND (X5) PLACES OF CORROSION AROUND ATTACHMENT HOLES; REF TO AVIANOR WO 49144 NR 1023, FCCD SILL UNDERNEATH SCUFF PLATE TEMPORARY REPAIR CARRIED OUT I.A.W AC24-1249-01 AND I.A.W REO 500-53-21-099 REV E, DETAIL VISUAL INSECTION AT INTERVALS NOT TO EXCEED 2000 F/H AND THIS TEMPORARY REPAIR IS VALID FOR 10000 F/H FROM THE TIME OF INCORPORATION OF THIS REO.
FLT#592, TPA-BOS. 'DURING SCHEDULED L1 DOOR SLIDE SYSTEM DEPLOYMENT TEST DOOR SLIDE FAILED TO EXTEND FULLY TEST THERE BY FAILED; L1 DOOR SLIDE CHANGED UNDER WO 1340135.'
FLT#451, BOS-MCO. 'DURING INSP OF LH EMER EXIT DOOR ACCIDENTLY BLEW EMER SLIDE; REMOVED AND REPLACED L/H OVER WING SLIDE PER AMP BD500-A-J25-63-02-01AAA-720A-A.'
FLT#1220, MIA-BOS. 'WING SLIDE EICAS CAUTION IN FLIGHT. EICAS AND INFLIGHT DID NOT NOTE ANY ABNORMALITIES ON LEFT WING. INFO 52 WING SLIDE-L OVER SLIDE INOP; REMOVED AND REPLACED LH OVERWING EMER EXIT DOOR SLIDE IAW AMP 25-63-02. NO DEFECTS NOTED.'
FLT#8384, MCO-JFK. (AIRCRAFT DID AN AIR TURN BACK TO MCO) 'DIRTY SOCK SMELL, VERY STRONG AFTER T.O. UPTO FL330 WOULD NOT GO AWAY, BOTH PILOT ON OXY TILL DOOR OPEN; FOUND SOURCE OF ODOR WHEN #1 PACK IS IN OPERATION. NORMAL - NO SMELL FROM PACK 2. PERFORMED ENG 1 -2 BORO INSP REF LOGPAGES 3867870 (BORESCOPE INSP. ACCOMPLISHED ON RH ENG. HPC 1 THRU 8 IAW PW MANUAL CH 72-35-00-00A-312A NO OIL STAINS OR OIL PUDDLING FOUND DURING BORESCOPE INSP.) AND 3867872 (CH ENG LPC1, LPC2 AND LPC 3 BOROSCOPE INSP. ACCOMPLISHED IAW PW MANUAL 72-31-00-00A*312A FOUNDOIL STAIN ON LPC 2 WEEP HS). ENG WASH OF #1 ENGINE PERFORMED , POWER ASSURANCE TEST OF ENG 1-2 NORMAL. AIRCRAFT OK FOR SVC. REF FIM BD500-A-J21-22-00-00AAA-423A-A.'
FLT#551, BOS-MCO. 'DIRTY SOCK SMELL REPORTEDBY THE F1 DESCENDING THRU 14000; TSM INSPECTION ACCOMPLISHED ON LOG PAGE 3867863 ITEM 1 PER TSM BD500-A-J21-22-00-00-AAA-423A-A. NO CONTAMINATION FOUND BY STEP 3.2 AND PER TSM NO FURTHER MXREQUIRED. RAN BOTH ENGINES FOR 30 MINS. NO SMELL/ODOR A/C OK FOR CONTINUED SVC.'
FLT#2229, BOS-MKE. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) 'R COWL A/ICE FAIL ON EICAS. RAN ECL.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#2364, MCI-BOS. 'RH OWEE SLIDE SAFETY PIN HOLE WAS OBSTRUCTED, CONTROLLED SLIDE DEPLOYMENT PERFORMED IAW GMM; RH OVERWING SLIDE REMOVED IAW AMP 25-63-02. SLIDE WAS BEING REMOVED TO ACCOMPLISH WORK REGARDING MDDR 521167.'
FLT#835, BOS-MSP. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' 36 R BLEED FAIL IN CLIMBING THENFL330. R PASS REG SOV INOP COMPLIED WITH ECL- DESCENT 300; THE OMS RECORDED R ENG PRSOV AS THE POSSIBLE CAUSE. REMOVED AND REPLACED R ENG PROV PER AMP 36-11-01. OPS CHECK W/ENG RUN IS STILL REQUIRED. SEE L/P 3764547 ITEM,1 (OPS CHECK OF R ENG BLEED PRSOV WAS SUCCESSFUL. A/C OK AT THIS TIME).
FLT#2186, PIT-BOS. 'DEPARTING PIT WITH A CLEARANCE TO CLIMB AND MAINTAIN 5000', PASSING BETWEEN 4000' AND 4300', THE FO NOTICED THE FMA INDICATE RETARD WITH THE THRUST LEVERS COMING BACK TO IDLE. THE AUTOTHROTTLES WERE DISCONNECTED AND THE A/C WAS LEVELED OFF AT 5000'. THE FCP XFR WAS SET ON THE FO'S SIDE AT THE TIME. WE TRANSFERRED THE FCP TO THE CAPT SIDE; FOUND RA 2 (FWD) CONNECTOR LOOSE RESECURED COAXIAL CABLE PER AMP 34-44-05.'
FLT#207, BOS-BNA. ' ON VECTORS FOR APPROACH TO ZOL BNA. LEVEL AT 3000FT, AP & AT ENGAGED SPEED SELECTED TO MAN 180 KTS. UNCOMMANDED (RETARD) ANNUNCIATED IN THE AUTOTHROTTLE ACTIVE IMA DISPLAY. SPEED OBSERVED AT 150KTS AND RAPIDLY DECELERATING. THE A/P & AT WERE DISCONNECTED AND THE AIRCRAFT WAS RECOVERED AND LANDED ON A NORMAL FLIGHT PATH; ITEM HAS NO HISTORY AND IS CONSIDERED A NUISANCE CASE PER AIRBUS ISI A220-ISI-22-30-001. A/C OK FOR CONT SRV. MCC JUAN NOTIFIED.'
FLT#1235, BOS-MSP. (AIRCRAFT DIVERTED TO BUF) ' WHILE AT F360 AT FAULT. SLAT FAULT, FD INTERMITTENT, AP UNCOMMANDED ROLL TO THE LEFT. TCAS FAIL. ADDITIONAL MESSAGES INTERMITTENT; RR ADSP2 PER AMP TASK BD500-A-J34-11-01-01AAA-520A-A. OPS CHECK GOOD.'
FLT#207, BOS-BNA. (AIRCRAFT DIVERTED TO PHL AND DECLARED AN EMERGENCY) ' FO WINDSHIELD CRACKED AT FL 360. EMERGENCY DECLARED. ECL COMPLETED. LANDING UNEVENTFUL; REMOVED AND REPLACED FO WINDSHIELD IAW AMP TASK BD500-A-J56-11-01-01AAA-520A-A. PERFORMED OPS CHECK OF TEMP CONTROLLER. OPS CHECK GOOD IAW AMP TASK BD500-J-J30-41-06-01AAA-320A-A AND CABIN PRESS CHECK GOOD IAW AMP TASK BD500--A-J21-31-00-01AAA-364B-A. ' (SUPPLEMENTAL INFORMATION ADDED)