N298JB

Part: ACTUATOR — FAILED (OUTFLOW-VLV) · airframe 34,352 hrs · 22,403 cycles

FLT # 1126, FLL-RDU(AIR TURN BACK TO FLL). DOOR PAX FWRD OPEN MESSAGE AFTER TAKE OFF . PRESSURIZATION CLIMBED UNTIL WE LEVELED OFF AT 21000. MAXIMUM ALTITUDE DISPLAYED 7300 DIFF PRESS 6. NO OVERWEIGHT LANDING REQUIRED; PER AMM 52-72-20, REPLACED ROLL PIN TO SHAFT ROLLER DETECTOR AND CHECKED ADJUSTMENT TO FWD PAX DOOR CLOSED SENSOR. DOOR INDICATION NOW CHECKS NORMAL PER AMM 52-72-20. SEE LP #3261376-2 FOR OUTFLOW VALVE ACTUATOR REPLACEMENT. SEE LP #3261379-1 FOR CPCS CONTROLLER REPLACEMENT & PRESSURIZATION CHECK. ALL CHECKS NORMAL & A/C OK FOR SERVICE. AS PER TECH SUPPORT ADVISED TO REPLACED CPCS OUTFLOW VALVE. REMOVED AND REPLACED CPCS OUTFLOW VALVE ACTUATOR IAW AMM 21-31-03 OPS CHEK GOOD. REMOVED AND REPLACED CPCS CONTROLLER PER TECH SUPPORT GUIDANCE REF AMM 21-31-01. ALL OPS CHKS OK. CABIN PRESSURIZATION ACCOMPLISHED PER 21-31-00-720-802-A. NO ABNORMALITIES NOTED

Part: ACTUATOR VALVE — FAILED (CPCS-CTRL) · airframe 34,352 hrs · 22,403 cycles

FLT # 1126, FLL-RDU(AIR TURN BACK TO FLL). DOOR PAX FWRD OPEN MESSAGE AFTER TAKE OFF . PRESSURIZATION CLIMBED UNTIL WE LEVELED OFF AT 21000. MAXIMUM ALTITUDE DISPLAYED 7300 DIFF PRESS 6. NO OVERWEIGHT LANDING REQUIRED; PER AMM 52-72-20, REPLACED ROLL PIN TO SHAFT ROLLER DETECTOR AND CHECKED ADJUSTMENT TO FWD PAX DOOR CLOSED SENSOR. DOOR INDICATION NOW CHECKS NORMAL PER AMM 52-72-20. SEE LP #3261376-2 FOR OUTFLOW VALVE ACTUATOR REPLACEMENT. SEE LP #3261379-1 FOR CPCS CONTROLLER REPLACEMENT & PRESSURIZATION CHECK. ALL CHECKS NORMAL & A/C OK FOR SERVICE. AS PER TECH SUPPORT ADVISED TO REPLACED CPCS OUTFLOW VALVE. REMOVED AND REPLACED CPCS OUTFLOW VALVE ACTUATOR IAW AMM 21-31-03 OPS CHEK GOOD. REMOVED AND REPLACED CPCS CONTROLLER PER TECH SUPPORT GUIDANCE REF AMM 21-31-01. ALL OPS CHKS OK. CABIN PRESSURIZATION ACCOMPLISHED PER 21-31-00-720-802-A. NO ABNORMALITIES NOTED

Part: FLOOR SUPPORT — CORRODED (PASSENGER CABIN) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON PASSENGER CABIN FLOOR STRUCTURE WEB BETWEEN FRAMES 87-88 Y=240 TO Y=240 ; REF: TECHOPS MX W/O 1698 N/R 00510 REPLACED WEB PER EMB-190 SRM 51-42-01 PAR4 AND PAR6.

Part: REINFORCEMENT — DAMAGED (LT NACELLE) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION ON PYLON/LH PYLON/ IB AND OB UPPER SPARS BUSHING BORES/ IB UPPER SPAR REINFORCEMENT ATTACHING HOLE/ CORROSION/ SCRATCHES/ HOLE ELONGATION/ TEMPORARY REPAIR (E21-1100-01). CLASSIFIED AS MAJOR REPAIR

Part: FRAME — CORRODED (AFT CARGO) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: FR82 BETWEEN STR27-28R FRAME CLIP AFT CARGO COMPARTMENT ; REF TOMX NR 00275: R & R FRAME CLIP FR82 STR27-28R IAW SRM 51-41-02, 51-41-01, AND 51-43-01.

Part: WEB — CORRODED (FWD CARGO DOOR) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FWD WEB OF LOWER BEAM @ FWD CARGO COMPARTMENT DOOR CUTOUT ; REF TOMX NR 00480: R & R DAMAGED DOUBLER AT FWD CARGO COMPARTMENT DOOR CUTOUT IAW SRM 51-41-02 AND SRM 51-43-04.

Part: WEB — CORRODED (PAX CABIN) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION: WEB @ PASSENGER CABIN FLOOR STRUCTURE FR15-16 Y=1200. ; REF TOMX NR 00516: R & R WEB @ PAX CABIN FLOOR STRUCTURE BETWEEN FR15-16 Y=1200 IAW SRM 51-41-01 PAR4, 51-43-02 PAR4, AND 51-41-02 PAR 6.

Part: SHEAR TIE — CORRODED · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION: SHEAR CLIP FR87 STR27-28R ; REF TOMX NR 00421: R & R SHEAR CLIP FR87 STR27-28R IAW SRM 51-41-02 AND 51-43-01.

Part: FRAME — CORRODED (AFT CARGO) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FRAME CLIP OF FRAME 85 BTW STGR 27R AND STGR 28R AT AFT CARGO COMPARTMENT ; REF: TECHOPS MX W/O 1698 N/R 00277 REPLACED PER EMB 190 SRM 51-41-02

Part: FRAME — CORRODED (PASSENGER CABIN) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON BEAM AT PASSENGER CABIN FLOOR FRAME 16 AND FRAME 19 Y=300 ; REF: TECHOPS MX W/O 1698 N/R 00457 REPAIRED PER EMB 190 SRM 53-10-10 REPAIR 51

Part: SHEAR TIE — CORRODED · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION: SHEAR CLIP FR88 STR27-28R ; REF TOMX NR 00420: R & R SHEAR CLIP FR88 STR27-28R IAW SRM 51-43-03, 51-41-02, AND 51-41-01.

Part: BRACKET — CORRODED · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: BRACKETS (2EA) AT FUSELAGE INTERNAL STRUCTURE FR86-87 STR27-28R ; REF TOMX NR 00593: R & R BRACKETS (2EA) AT FUSELAGE INTERNAL STRUCTURE BETWEEN FR86-87 STR27-28R IAW SRM 51-41-01 PAR 4, 51-41-02 PAR 4, 51-41-01 PAR 6, AND 51-41-02 PAR 6.

Part: DOUBLER — CORRODED (WASTE BOX) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION: INNER DOUBLER OF WASTE BOX @ FR88-89 STR28R ; REF TOMX 00426: REPAIRED INNER DOUBLER OF WASTE BOX @ FUSELAGE INTERNAL STRUCTURE BETWEEN FR88-89 STR28R IAW SRM 53-23-60/REPAIR 51P.

Part: FRAME — CORRODED (AFT CARGO) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FRAME CLIP OF FRAME 86 BTW STGR 27R AND STGR 28R AT CARGO COMPARTMENT ; REF: TECHOPS MX W/O 1698 N/R 00278 REPLACED PER EMB 190 SRM 51-41-02

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: WEB @ PASSENGER CABIN FLOOR STRUCTURE FR17-19 Y=1200 ; REF TOMX NR 00460: WEB @ PAX CABIN FLOOR STRUCTURE BETWEEN FR17-19 Y=1200 REPLACED IAW SRM 51-41-02 PAR 4 & 6.

Part: WEB — CORRODED (AFT CARGO) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FRAME CLIP OF FRAME 81 BTW STGR 27R AND STGR 28R AT AFT CARGO COMPARTMENT ; REF: TECHOPS MX W/O 1698 N/R 00274 REPLACED PER EMB 190 SRM 51-41-02

Part: SLAT TRACK — CRACKED (LEFT NR 5 SLAT) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CRACK: LH WING L.E. SLAT TRACK #5 CUTOUT ; REF. TOMX NR 00206: R & R FIXED LEADING EDGE BTW RIB12 TO RIB17 @ LH WING IAW SRM 51-41-02 AND SRM 51-43-02.

Part: FLOOR SUPPORT — CORRODED (WEB) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: PAX CABIN FLOOR WEB FR87-88 Y=300 - Y=1000 ; REF TOMX NR 00419: R & R PAX CABIN FLOOR WEB @ FR87-88 Y=300 - Y=1000 IAW SRM 51-42-01, 51-42-02, AND 51-43-03.

Part: SLAT TRACK — CRACKED (RH WING) · airframe 33,846 hrs · 22,060 cycles

DURING HEAVY MAINTENANCE, CRACK: RH WING L.E. SLAT TRACK #5 CUTOUT ; REF TOMX NR 00060: RH WING FIXED LEADING EDGE SLAT TRACK #5 CUTOUT WAS REPAIRED IAW SRM 57-49-01/REPAIR 51P.

Part: FRAME — CORRODED · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: FR83 BETWEEN STR27-28R FRAME CLIP AFT CARGO COMPARTMENT ; REF TOMX NR 00276: R & R FRAME CLIP FR83 STR27-28R IAW SRM 51-41-01, 51-41-02, AND 51-43-02.

Part: SKIN — DENTED · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, FUSELAGE/ CENTER FUSELAGE III/ LOWER SKIN BTWN FR 83-84 & STGR 23L-24L/ DENT- PERMANENT REPAIR. CLASSIFIED AS MAJOR REPAIR

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: SHEAR CLIP AFT CARGO INTERNAL STRUCTURE FR75 BETWEEN STR 29R-29L ; REF TOMX NR 00558: R & R SHEAR CLIP @ AFT CARGO FR75 STR29R-29L IAW SRM 51-41-01 AND 51-41-02.

Part: ATTACH FITTING — CORRODED (LH PYLON) · airframe 33,846 hrs · 22,061 cycles

DURING HEAVY MAINTENANCE, CORROSION: AFTER BUSHING REMOVAL - FOUND CORROSION AT HOUSING OF INBD/OUTBD AFT FITTING IN LH PYLON ; REF TOMX NR 00548: HOUSING OF INBD/OUTBD AFT FITTING IN LH PYLON WAS REPAIRED IAW ETI - 190-21-817 REV 6, ETD-2021-190-031064 REV B. AND JETBLUE EC E21-1100-01.

Part: LIGHT — NO TEST (LT OVERWING) · airframe 32,535 hrs · 21,305 cycles

FLT 756, TPA-DCA. WHEN PERFORMING TASK CARD E190-33-50-25-710-801 FOUND FWD LT EXT EMERGENCY LIGHT INOPERABLE (EXTERNAL EMERGENCY-OPERATIONS NOT CONDUCTED AT NIGHT). R & R FWD LT OVER WING EMERGENC LIGHT ASSEMBLY, IAW AMM 33-50-25. OPERATIONS CHECK GOOD. MX4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.

Part: SENSOR — FAILED (LE SLAT) · airframe 29,878 hrs · 19,449 cycles

FLT 832, LGA-BOS. EMERGENCY DECLARED. SLAT FAIL ON APPROACH. COMPLIED WITH QRH PROCEDURES; CHECKED LEFT WING OUTBOARD SLAT SKEW SENSOR WIRING PER WM 27-83-53. CHECKS GOOD. R & R BOTH OUTBOARD SLAT SKEW SENSORS IAW AMM 27-83-01. OP CHECKS GOOD.

Part: SENSOR — FAILED (LE SLAT) · airframe 29,878 hrs · 19,449 cycles

FLT 832, LGA-BOS. EMERGENCY DECLARED. SLAT FAIL ON APPROACH. COMPLIED WITH QRH PROCEDURES; CHECKED LEFT WING OUTBOARD SLAT SKEW SENSOR WIRING PER WM 27-83-53. CHECKS GOOD. R & R BOTH OUTBOARD SLAT SKEW SENSORS IAW AMM 27-83-01. OP CHECKS GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 25,855 hrs · 16,531 cycles

DURING HEAVY MAINTENANCE, THE LEFT WING CRACKED ON THE LOWER SKIN, THE SKIN WAS REPAIRED IAW ETD2018-190-001572, SRM 57-10-01, REP 54, REV 36 AND E18-014-01.

Part: SKIN — CRACKED (LT WING) · airframe 25,855 hrs · 16,531 cycles

DURING BRIDGE CHECK AT YRQ, FOUND 0.740" LONG CRACK ON THE REF 2 LT WING MAIN BOX LOWER SKIN AT SPAR II & RIB 11. THE CRACK WAS REMOVED AS PER SRM PART II 51-10-03 BUT IS OUTSIDE THE LIMITS OF REF 3 REPAIR. CONTACTED MANFACTURER FOR FURTHER DISPOSITION AND WAS PROVIDED WITH REF 1 ETD. REF 1 ETD PROVIDED APPROVAL TO ACCOMPLISH REF 3 SRM REPAIR WITH A 12 MONTH DTA. EC E18-014-01 ACCOMPLISHED THE TEMPORARY REPAIR AS PER REF 1 ETD WITHOUT DEVIATION. PER REF 5 ALLOWED THE TEMPORARY REPAIR THAT WAS PREVIOUSLY ACCOMPLISHED TO REMAIN AS PERMANENT WITH NO ADDITIONAL INSPECTIONS REQUIRED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,333 hrs · 14,079 cycles

FLT 1044 CHS-DCA, DURING MAINTENANCE, TECHNICIAN DISCOVERED THE AFT RT DOOR EXIT LIGHT TO BE INOPERATIVE. REMOVE AND REPLACE AFT EMERGENCY BATTERY AS PER AMM 33-50-01. PERFORMED OPS CHECK. OPS CHECK PASSED.

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,751 hrs · 12,275 cycles

REF EAMS NR H4803/00485, SHEAR CLIP ON FRAME 84 BETWEEN STR 27R AND STR 28R CORRODED PN170-66017-002. REF EAMS NR H4803/00485, REPLACED SHEAR CLIP IAW SRM 51-41-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,751 hrs · 12,275 cycles

LEFT EXTERNAL EMERGENCY LIGHT ON PANEL 1932AL WILL NOT ILLUMINATE DURING OPS CHECK. REF W/O H4803- 00773, R & R EMERGENCY BATTERY PACK NR 4 AND PERFORMED OPS CHECK REF E-190 AMM 33-50-01.

Part: FLOORBEAM — CORRODED (FRAME 80) · corrosion level 2 · airframe 19,751 hrs · 12,275 cycles

FLOOR SUPPORT BRACKET FRAME 80 BETWEEN STR 27R AND 28R CORRODED PN 170-87229-001. REF EAMS NR H4802/00482, REPLACED FLOOR SUPPORT IAW SRM 51-41-01.

Part: FLOORBEAM — CORRODED (FRAME 80) · corrosion level 2 · airframe 19,751 hrs · 12,275 cycles

FLOOR SUPPORT BRACKET ON FRAME 80 BETWEEN STR 27R AND 28R CORRODED. REF EAMS NR H4803-00482. R & R BRACKET WITH NEW AND APPLIED FINISH REF SRM 51-41-01, 51-41-02, 51-23-06.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 19,751 hrs · 12,275 cycles

SHEAR CLIP ON FRAME 83 BETWEEN STR 27R AND 28R CORROSION, PN 170-66868-001. REF EAMS NR H4803/00484, REPLACED SHEAR CLIP IAW SRM 51-41-01.

Part: CONTROL MODULE — FAILED (BRAKE SYS) · airframe 18,722 hrs · 11,552 cycles

RECEIVED BRAKE LEFT FAULT MESSAGE DURING LANDING GEAR EXTENSION. PERFORMED GO-ROUND. RECEIVED BRAKE RT FAULT MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH NR 2 BRAKING WAS NORMAL. REPLACED BCM NR 2, OPS TEST, OK IAW 32-41-7.

Part: SHUTOFF VALVE — FAILED (RT MLG) · airframe 18,722 hrs · 11,552 cycles

RECEIVED BRAKE LEFT FAULT MESSAGE DURING LANDING GEAR EXTENSION. PERFORMED GO-ROUND. RECEIVED BRAKE RT FAULT MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH NR 2 BRAKING WAS NORMAL. REPLACED NR 2 BRAKE SHUTOFF VALVE IAW MM 32-41-00, NO DEFECTS.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 16,409 hrs · 10,069 cycles

DURING MAINTENANCE, R2 DOOR LOWER EMERGENCY LIGHT WAS INOPERATIVE AT POWER UNIT NR 6. R & R POWER UNIT IAW AMM 33-50-01, OPS CHECKED GOOD.

Part: POWER UNIT — FAILED (CABIN) · airframe 12,312 hrs · 7,395 cycles

FLT 1276 CHS-JFK, ON GROUND MAINTENANCE CHECK FOUND LEFT AFT PAX SERVICE DOOR EMERGENCY EXIT INDICATOR SIGN OUT. REMOVED AND REPLACED AFT LEFT EMERGENCY LIGHT POWER UNIT PER AMM 33-50-01. OPS CHECK GOOD.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 9,094 hrs · 5,446 cycles

FLT 681, AFT INBOARD COFFEEMAKER SMOKING. INSPECTION COMPLETED PER FIM 21-00-00-810-801A.

Part: MODULE — FAILED (NR 3) · airframe 8,825 hrs · 5,300 cycles

FLT 1968 AUS-JFK, IN DESCENT EICAS MESSAGE AVNX MAU 2A FAILED, CREW PERFORMED QRH PROCEDURE, LANDED NORMALLY AND TOWED INTO THE GATE. REMOVED AND REPLACED NIC PROC MOD 3 (MAU 2-NIC 1) AND PERFORMED TARGET LOAD NO FAULTS NOTED SYS OPS NORMAL.

Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 7,383 hrs · 4,410 cycles

FLT 698 FLL-DCA DIVERTED TO IAD, ON GEAR EXTENSION INTO DCA RECEIVED BRAKE LT AND RT FAULT. AFTER GO AROUND COMPLETED THE QRH PROCEDURE AND MADE A LANDING AT IAD. BRAKE RT FAULT WENT AWAY ON SHORT FINAL, AND THEN RETURNED THEN WENT AWAY AGAIN ON TAXI. THERE WAS A NOTICEABLE GROANING SOUND FROM THE BRAKE ON TAXI IN, THAT WAS NOT PRESENT ON DEPARTURE. REMOVED AND REPLACED I/B SHUT-OFF VALVE IAW AMM 32-41-03. OPS CHECK AND LEAK CHECK OK. ACCOMPLISHED TAXI CHECK. NO ABNORMALITIES NOTED. A/C OK FOR CONTINUED SERVICE.

Part: VALVE — FAILED (NR 1 BLEED) · airframe 4,813 hrs · 2,841 cycles

FLT 1296, BLEED NR 1 FAIL WITH COINCIDING BURNING SMELL. TURNED NR 1 BLEED OFF. REMOVED AND REPLACED HIGH STAGE BLEED VALVE PER AMM 36-11-01. T/S BURNING SMELL PER FIM TASK 21-20-00-810-A. NO ABNORMAL SMOKE /SMELL NOTED.

Part: PROBE — FAULTY (TAT) · airframe 2,400 hrs · 1,422 cycles

FLT 915 BOS-JFK AOA 1 CAUTION MESSAGE AND SMELL OF SLIGHT BURNING PLASTIC, TURNED RECIRC FAN OFF SMELL DISAPPEARED. REG LOG PAGE 688966 AND 688967, REMOVED AND REPLACED NR 1 TAT PROBE AND CONNECTOR AS PER AMM 34-15-02 AND SPWM 20-21-20.

Part: DUCT — DAMAGED (AC BAY) · airframe 2,304 hrs · 1,367 cycles

FLT JB337 IAD-MCO UPON REACHING CRUISE ALTITUDE FL 360, CABIN ALTITUDE CONTINUED TO INCREASE INITIATED DESCENT TO FL 320 AN CABIN ALTITUDE DESCENDED TO NORMAL RANGE. MAX CABIN ALTITUDE NOTED WAS 8900 FT. MX TROUBLESHOT TO RT PACK OUTLET DUCT DAMAGE ON FLANGE AREA FOR RAM AIR EMERGENCY CHECK VALVE. REMOVED AND REPLACED RT PACK OUTLET DUCT IAW AMM 21-51-21, OPS AND LEAK CHECK PERFORMED PRESSURIZATION CHECK PER AMM 21-31-00, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRICAL BOX — FAILED (ENTERTAIN SYS) · airframe 1,454 hrs · 829 cycles

FLT 1402 SFO-AUS HARSH ODOR REPORTED IN AFT CABIN WITH PACK 1 AND PACK 2 AND A HAZY SMOKE. WHILE T/S ODOR EVENT NOTED POSSIBLE SMELL FROM LTV XEB AT 23CD. OPS CHECK ON PACK 1 AND 2 OK IAW AMM 21-00-00. REMOVED AND REPLACED 23 XEB AND PERFORMED LTV MM 44-20-10, SYS OK.