N294JB

Part: SKIN PANEL — CRACKED (RT WING) · airframe 33,853 hrs · 21,779 cycles

DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 10; (REF AEROMAN NR 2020-164211) PERFORMED PERMANENT REPAIR IAW SRM 57-10-01 REPAIR 54P ITEM #9 FIG. 201 SHEET 6 TABLE 202. THIS REPAIR IS CAT ""A"" & NO FURTHER ACTION REQUIRED.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 33,853 hrs · 21,779 cycles

DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 4; (REF AEROMAN NR 164208) ACCOMPLISHED REPAIR IAW AEROMAN EA57-0355-20 REV. O (COVER & PARTS 1-3), EMBRAER ETD 2020-190-0151501, AND JETBLUE EC NO. E20-443-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,379 hrs · 19,391 cycles

FLT 1887, ORH-MCO. LEVEL 1 TRANSIENT ODOR FLIGHT DECK ONLY, DURING LEVEL OFF AT 6,000FT N1 APPROX 33% LASTED APPROX 30 SEC. BURNING SMELL AND FO HAD MINOR EYE IRRITATION; C/W FIM TASK 21-20-00-810-801-A. NO ABNORMAL SMOKE/SMELL IN COCKPIT OR CABIN. RAN BOTH PACKS INDIVIDUALLY WITH ENGS & APU BLEEDS. NO ODOR NOTED PER FIM TASK PAGE 13 BLOCK 7 "TRANSITORY CONDITION OF THE AIR CONDITIONING PACK(S) OR OTHER COMPONENTS" OK FOR SVC.

Part: DOOR SILL — DAMAGED (FUSELAGE) · airframe 28,496 hrs · 17,928 cycles

DURING HEAVY MAINTENANCE, AN ELONGATED HOLE WAS DISCOVERED. REFER TO EC E18-425-01. FUSELAGE / CENTER FUSELAGE II / FLOOR STRUCTURE SILL FR42-43 & STR 17R / ELONGATED HOLE - PERMANENT REPAIR; THIS PERMANENT REPAIR IS APPROVED PER REF /2/ ETD AS CATEGORY A AND CLASSIFIED AS “MAJOR”

Part: WIRE HARNESS — DEFECTIVE (R1 DOOR) · airframe 25,791 hrs · 15,968 cycles

THE FLIGHT CREW REPORTED VIA ARINC THAT THEY WERE GETTING AN INTERMITTENT AURAL WARNING IN FLIGHT. THE R1 DOOR INDICATION WAS ON MEL AND THE WARNINGS THAT THE DOOR IS OPEN IS INTERMITTENTLY ACTIVATING. THE CREW REPORTED THAT THE AURAL WARNINGS WERE A DISTRACTION TO THEM. DUE TO THOSE WARNINGS, THEY WERE MISSING SOME ATC RADIO CALLS. AS A RESULT OF THES AURAL WARNINGS, THE CAPTAIN WAS OF THE OPINION THAT IT WAS A SAFETY OF FLIGHT ISSUE. THE CREW RETURNED TO DEPARTURE. FOUND THE R1 DOOR ELECTRICAL HARNESS AT FAULT. R & R THE R1 DOOR ELECTRICAL HARNESS IAW AMM 52-72-21. OPS CHECKED GOOD.

Part: GIRT BAR — DIRTY (L1 DOOR SLIDE) · airframe 24,643 hrs · 15,222 cycles

L1 DOOR IS UNABLE TO BE DISARMED AFTER LANDING. HANDLES ARE FROZEN IN DOWN POSITION. REMOVED AND INSTALLED THE DOOR EVACUATION SLIDE IAW AMM 52-11-40. FOUND DEBRIS ON DOOR FLOOR FITTING. CLEANED DEBRIS IAW AMM 52-11-00. PERFORMED OPS CHECK. OPS CHECK PASSED.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP, LOCATED, DRILLED, AND TREATED NEW CLIP. INSTALLED AND TOPCOATED NEW CLIP.

Part: STRINGER — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

CORROSION, STR 21L HAS CORROSION FRAME 89-90. COMPLIED WITH E15-1067-01 BY CUTTING OUT DAMAGED STR SECTION, FABRICATING NEW STR SECTION, HFEC, INSTALLED NEW STRINGER SECTION, AND RESTORING TOPCOAT.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

SHEAR CLIP CORRODED AT FRAME 87 BETWEEN STR 26L AND STR 27L. REMOVED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IN COMPLIANCE WITH E15-1085-01. INSTALLED FABRICATED SHEAR CLIP. RESTORED TOPCOAT.

Part: SHEAR TIE — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STR 19L. REMOVED CORRODED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IAW TASK CARD NR E15-1076-01. INSTALLED FABRICATED SHEAR CLIP.

Part: STRINGER — CORRODED (FRAME 90-91) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

STR 23L CORRODED AROUND FASTENERS AT FRAME 90-91 AS MARKED. BLENDED CORROSION , HFEC, NO DEFECTS NOTED, FABRICATED L-ANGLE DOUBLER, INSTALLED DOUBLER, ALODINED, PRIMED AND TOP-COATED.

Part: STRINGER — CORRODED (FRAME 91) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

CORROSION ON STRINGER 23L AT FRAME 91. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, R & R STRINGER.

Part: SHEAR TIE — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

SHEAR CLIP CORRODED AT FRAME 85 BETWEEN STR 27L AND STR 28L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP, HFEC FABBED SHEAR CLIP, ALODINED, PRIMED, TOPCOATED AND INSTALLED NEW SHEAR CLIP.

Part: SHEAR TIE — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

LT SHEAR CLIP CORRODED AT FRAME 89 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP. LOCATED, DRILLED, AND TREATED NEW SHEAR CLIP. INSTALLED AND TOP-COATED NEW SHEAR CLIP.

Part: STRINGER — CORRODED (FRAME 91) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

STR 19L CORRODED AT FRAME 91. R & R CORRODED STRINGER JUNCTION. RESTORED TOPCOAT.

Part: SHEAR TIE — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STRINGER 19L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP IAW JB EA E15-1076-01, INSTALLED NEW FABRICATED SHEAR CLIP.

Part: STRINGER — CORRODED (FRAME 88) · corrosion level 2 · airframe 21,473 hrs · 13,016 cycles

STR 17L CORRODED, 14" AFT OF FRAME 88. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIRED DOUBLER. COMPLIED WITH E15-1067-01.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 21,220 hrs · 12,826 cycles

DURING MAINTENANCE WHILE PERFORMING EMERGENCY, BATTERY PACKS FAILED TEST. R & R IAW AMM 33-50-01.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 21,220 hrs · 12,826 cycles

DURING MAINTENANCE WHILE PERFORMING EMERGENCY, LIGHT POWER UNITS FAILED TEST. R & R BATTERY PACK IAW AMM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,220 hrs · 12,826 cycles

DURING MAINTENANCE, WHILE PERFORMING EMERGENCY. POWER UNITS FUNCTIONAL TEST FAILED. R & R BATTERY PACK & FUNCTION TEST IAW AMM 33-50-01.

Part: ACM — FAILED · airframe 21,085 hrs · 12,725 cycles

RETURNED TO DEPARTURE SHORTLY AFTER TAKEOFF, LAVATORY SMOKE INDICATION, R & R ACM IAW AMM 21-51-05, OPS AND LEAK CHECKED GOOD.

Part: ACM — CONTAMINATED (NR 2) · airframe 20,669 hrs · 12,458 cycles

RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500 AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF COFFEE GRINDS IN NR 2 PACK ACM ASSEMBLY. R & R NR 2 ACM IAW MM 21-51-05, NO LEAKS NOTED, OPS CHECKS GOOD ADDITIONAL COMPONENT CHANGE IAW MCC R/R DUAL HEAT EXCHANGER IAW MM 2-51-04. OPS CHECKS GOOD.

Part: HEAT EXCHANGER — CONTAMINATED (NR 2) · airframe 20,669 hrs · 12,458 cycles

RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF COFFEE GRINDS IN NR 2 PACK ACM ASSY. R & R NR 2 ACM IAW MM 21-51-05 NO LEAKS NOTED. OPS CHECKS GOOD, ADDITIONAL COMPONENT CHANGE IAW MCC R & R DUAL HEAT EXCHANGER IAW MM 2-51-04. OPS CHECKS GOOD.

Part: LOOP — OUT OF POSITION · airframe 15,066 hrs · 8,917 cycles

ACFT DIVERTED DUE TO BLEED 2 LEAK EICAS MESSAGE DURING CLIMB OUT. RUN QRH PROCEDURES AND MESSAGE EXTINGUISHED. PERFORMED FIM TASK 36-21-00-810-803-A, FOLLOW CH 1 SHORT CONDITION AT 1630 FOUND ODS LOOP INSULATION POSITIONED IMPROPERLY. REPOSITIONED INSULATION IAW AMM 36-21-42. CH 2 OVERHEAT COND AT 1802 PERFORMED EC NO E13-515-01 DUE TO DAMAGED PRECOOLER SEAL ON RT ENGINE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,333 hrs · 8,412 cycles

FLT 1706 SDQ-MCO, AFTER LANDING THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO CAPT WINDSCREEN CRACKED AND CAUGHT ON FIRE. REMOVED AND REPLACED CAPT'S SIDE LEFT WINDSHIELD PER EMB AMM TASK 56-11-00. NO OTHER DAMAGED NOTED AROUND WINDSHIELD AREA OK TO CONTINUE.

Part: PRESSURE SENSOR — FAILED (BLEED AIR SYS) · airframe 13,292 hrs · 7,843 cycles

FLT 663 SYR-MCO, AIRCRAFT DIVERTED TO IAD DUE TO NR 1 ENGINE BLEED OVER PRESSURE MESSAGE AT 129 PSI. UNABLE TO RESET PER THE QRH. REFERENCE FIM 36-14-00-810-804-A, REMOVED AND REPLACED LEFT BLEED PRESSURE SENSOR REF AMM 36-14-02. BLEED FAIL CLEARED.

Part: ELECTRICAL BOX — DEFECTIVE (CABIN) · airframe 10,739 hrs · 6,255 cycles

FLT 1258 IAD-BOS, WHILE AIRCRAFT WAS SLOWING AND BEING VECTORED ON APPROACH, THE FLIGHT ATTENDANTS CALLED TO SAY A BURNING SMELL LIKE BURNING RUBBER WAS AROUND ROW 23. THERE WAS NO SMOKE OR FIRE JUST SMELL. IT DISSIPATED AFTER ABOUT 3-4 MINUTES. PERFORMED INSPECTION AND FOUND SMELL TO BE COMING FROM XEB AT ROW 23AB PER AMM 21-20-00-810-801-A. REMOVED AND REPLACED XEB AT SEAT 23AB. INSPECTED ALL XEB'S AND XEB CONNECTORS THROUGHOUT THE CABIN NO DEFECTS OR SMOKE SMELL FOUND.

Part: POWER UNIT — FAILED (CABIN) · airframe 10,308 hrs · 6,007 cycles

FLT 1712 SDQ-MCO, ON GROUND MAINTENANCE CHECK FOUND FWD LT DOOR EMERGENCY EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED POWER UNIT IAW AMM 33-50-01. OPS CHECK GOOD.

Part: SHUTOFF VALVE — STUCK (BLEED AIR SYS) · airframe 9,147 hrs · 5,296 cycles

FLT 335 IAD-MCO, UPON DEP AT 1500 AGL - REQ'D BLEED 1 OVERPRESS EICAS WHILE RUNNING QRH. BLEED 2 IS FLUCTUATING FROM 2-98 PSI WITH BLEED 1 ALREADY ON MEL, ELECTED TO RETURN TO AIRPORT. NO OTHER EICAS MESSAGES REC'D. INSPECTED AND FOUND NR 1 NAPRSOV STUCK IN THE OPEN POSITION. REMOVED AND REPLACED NR 1 NAPRSOV IAW 36-11-03. PERFORMED HIGH POWER RUN, PERFORMED OPS CHECK OF BOTH BLEED SYSTEM IAW 36-11-00. OPS CHECK GOOD NO DEFECTS NOTED. NR 1 AND NR 2 BLEED SYSTEM OPERATING NORMAL. MDDR 118416 CLOSED.

Part: ACM — FAILED (RIGHT) · airframe 9,113 hrs · 5,278 cycles

FLT 1791, AIR TURNBACK & EMERGENCY DECLARED - AFTER TAKEOFF CLIMBING THROUGH 500 FT, RECEIVED "LAV SMOKE" MESSAGE & ALARM. AFT F/A REPORTED SMOKE STARTED IN FWD CABIN THEN AFT THEN MID. SMOKE WAS COMING IN THROUGH SIDEWALL VENTS. SMOKE DISSIPATED ON DESCENT, "LAV SMOKE" MESSAGE & ALARM CONTINUOUS THROUGH FLT. F/A REPORTED OIL ODOR ASSOCIATED WITH SMOKE. PERFORMED TSM TASK 21-20-00-810-801A AND FOUND NO DEFECTS IN CABIN. INSPECTED NR 1 AND NR 2 PACK IAW 21-51-05 AND FOUND NR 2 HEAT EXCHANGER CONTAMINATED. PERFORMED ENG PNEUMATIC BLEED CHECK IAW AMM 36-11-00 AND FOUND STRONG ODOR COMING FROM PACK NR 2 WITH ENG BLEEDS OR APU BLEED. PLACED PACK NR 2 ON MDDR 118101 IAW MEL 21-51-00 COND NR 1.

Part: SLIDE — FAILED (L1 DOOR) · airframe 8,503 hrs · 4,884 cycles

PRIOR TO DEPARTURE WITH L1 DOOR CLOSED, THE F/A REPORTED L1 DOOR SLIDE TOUGH TO ARM. TECH HAD TO REMOVE THE SLIDE IN ORDER TO OPEN DOOR. REPLACED L1 DOOR SLIDE ASSY IAW 25-65-01. OPS CHECKED GOOD.

Part: ACM — FAILED (NR 2) · airframe 6,696 hrs · 3,802 cycles

FLT 578 FLL-HPN, AIR RETURN TO FLL DUE TO SMOKE AND FUMES IN CABIN, FUMES IN FLT DECK ON DEPARTURE. COCKPIT, CABIN SMOKE/FUMES QRH COMPLETED THRU BLEEDS OFF. SMOKE DISSIPATED MOSTLY AFTER RECIRC FAN TURNED OFF. PAX REPORTED A SQUEAL BEFORE SMOKE AND FUMES UNDER ROWS 8 AND SCREECH. (AIR CONDITIONING PACKS-SINGLE). REMOVED AND REPLACED NR 2 ACM IAW 21-51-05. OPS CHECK NORMAL.

Part: ELECTRICAL BOX — MALFUNCTIONED (CABIN) · airframe 6,282 hrs · 3,551 cycles

FLT 1263 BOS-AUS, INFLIGHT AT FL 340, THE F/A NR 1 REPORTED ELEC SMELL AT ROW 13. CREW DEPOWERED ALL 3 IFE/CSS SWITCHES AND SMELL ABATED AFTER FEW MINUTES. PERFORMED ELECTRIC ODOR SYSTEM INTEGRITY AND FOUND 11AB XEB WITH ODOR. REMOVED AND REPLACED 11AB XEB, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 5,799 hrs · 3,250 cycles

FLT 612 JAX-JFK A/C DECLARED EMERGENCY ON LANDING. REF LOG PAGE 643107 ITEM 1 (DUE TO HYD 2 ELEC PUMP SECURED TO OFF POSITION). QRH WERE CONSULTED AND CALL FOR NON NORMAL LANDING CONFIGURATION. THE CREW DEPLOYED LG MANUALLY ON LANDING. PERFORMED L/G FREE FALL COND INSP/CHECK PER AMM 5-50-14-200-001A INSP OF MAIN L/G PER 32-10-00-200-801-A/600 NLG PER 32-20-00-200-801-A/600 GOOD, NO FAULTS NOTED OK FOR SVC.

Part: PRESSURE SWITCH — FAILED (HYDRAULIC SYS) · airframe 5,799 hrs · 3,250 cycles

FLT 612 JAX - JFK A/C DECLARED EMERGENCY ON LANDING. SHORTLY AFTER T/O RECEIVED HYD 2 HI TEMP EICAS. SECURED HYD 2 ELEC PUMP AND SYNOPTIC PAGE SHOWED HYD 2 SHUT OFF VALVE CLOSED AND ENGINE HYD PUMP OFF. TEMP PEAKED AT 110C AND COOLED FINE AFTER SECURING PUMP. AS PER FIM TASK 29-31-00-810-812A, REMOVED AND REPLACED NR 2 HYD SYS EDP PRESS SWITCH REF 29-31-03. OPS CHECK GOOD.