N192JB

Part: ENGINE — FAILED (RIGHT) · airframe 44,080 hrs · 28,552 cycles

FLT 1882, IAH-JFK. RIGHT ENGINE FAILED WITH WEIGHT ON WHEELS UPON TOUCHDOWN RT ITT WAS ALSO EXCEEDENCE, ITEM C/W PER WO #1226080 EC E22-1068-01.

Part: NONE — NONE · airframe 42,966 hrs · 27,732 cycles

FLT#1237, BOS-DTW. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO BOS) ' HUD SYS 2 FAIL APPRX 45 MIN INTO FL CYAN HYD 2 LOW QTY AT 16%PRSSR AT 2900 PST OUR PRD OF 5 MIN HYD 2 QTY DROPPED TO TO 0%. PRSSR STDY AT 2900 FOR 5 MIN THEN DRP TO 2500 SLOWLY SOON APT SUDDEN DROP TO PSI; FOUND PYLON LINE ON #2 SIDE HAD PINHOLE CAUSING SYSTEM FLUID LOSS. REPLACED DAMAGED PRESSURE LINE PN:190-05170-406 BY TUBING REPAIR UNDER AMM 20-10-03-300-801-A. SEE ITEM #3387281-2 (#2 PYLON HYD LINE, CLAMPS, AND STANDOFF INSTALLED AND LEAKED CHECKED IAW AMM 29-13-00) FOR INSTALLATION OF STANDOFF, CLAMPS, AND LEAK CHECK.' (SUPPLEMENTAL ADDED TO DESCRIPTION AND DATE).

Part: LIGHT — INOPERATIVE · airframe 42,795 hrs · 27,627 cycles

FLT#2224, MCO-DCA. 'LH MID EXTERNAL EMERGENCY LIGHT INOP. (EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT).' (SUPPLEMENTAL TO FOLLOW)

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,449 hrs · 25,363 cycles

DURING HEAVY MAINTENANCE, CRACK STR 9L FR73 UPPER FUSELAGE; REF AEROMAN NR 2020-125482: R & R STR 9L FR73 UPPER FUSELAGE IAW SRM 51-40-08 AND DWG #190-67977-803.

Part: SKIN — DENTED (TAILCONE) · airframe 39,449 hrs · 25,363 cycles

DURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN ON TAIL CONE 1"" AFT TO LH LOWER PANEL; REF AEROMAN NR 2020-125440 ACCOMPLISHED REPAIR OF THE BULGE AND CORROSION DAMAGES ON LH & RH SKINS OF THE TAIL CONE ASSY (P/N 170-98035-415 S/N 0132001) IAW AEROMAN EA 53-0276-20 REV. 0 (COVER, PART 1 & 2), 53-0277-20 (COVER, PART 1 & 2), ETD2020-190-0

Part: RIB — CRACKED (RT WING) · airframe 39,449 hrs · 25,363 cycles

DURING HEAVY MAINTENANCE, CRACK LEADING EDGE AT LEVEL RIB 17 INTERNAL AREA RH WING (1EA); ACCOMPLISHED REPAIR IAW AEROMAN NR 2020-109092, AEROMAN EA 57-0257-20 REV 0, EMBRAER ETD 2020-190-008623-A, AND JETBLUE EC 20-300-01.

Part: BEAM — CRACKED (FUSELAGE) · airframe 39,449 hrs · 25,363 cycles

DURING HEAVY MAINTENANCE, AEROMAN REPORTED TWO CRACKS FOUND ON THE LH LONGITUDINAL BEAM (P/N 190-22014-001) AT FR49 LEVEL IN THE CENTER FUSELAGE II. SEE REF /1/ EA FOR DETAILS. THE DAMAGES WERE FOUND TO BE OUTSIDE OF THE SCOPE OF SRM. AEROMAN PROPOSED TO PERFORM THE REPAIR CUT OUT REPAIR PER PREVIOUSLY APPROVED REF /3/ ETD. EMBRAER PROVIDED REF /2/ ETD WITH REPAIR INSTRUCTIONS CONSIST OF TRIMMING OUT THE CRACKED BEAM SECTION, FABRICATE AND INSTALL A REPAIR ANGLE AND FILLER AND RESTORE SURFACE PROTECTION PER SRM. THIS EC E20-288-01 ACCOMPLISHES PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH REF /2/ ETD WITHOUT DEVIATION; THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /2/ ETD & REF /4/ ANAC FORM AND IS CLASSIFIED AS MAJOR.

Part: ACM — FAILED (AC BAY) · airframe 38,262 hrs · 24,519 cycles

FLT 1137, BOS-DTW. SMOKE REPORTED IN CABIN DURING FLIGHT BY INFLIGHT. FIRST NOTICE IN MID CABIN AND OBSERVED TO BE ELECTRICAL SMELL. AFTER DURING QRH AND DUMPING PRESSURIZATION SMOKE CLEARED AND DID NOT RETURN; PERFORMED FIM TASK 21-20-00-810-801-A FOUND SMOKE TO BE CAUSED BY THE # 2 ACM FAILURE. COMPLETED INSPECTION WITH NO OTHER FINDINGS. SEE DEFECT # 2671815 # 2 ACM FAIL. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: SKIN — CORRODED (FRAMES 97-98) · corrosion level 2 · airframe 32,409 hrs · 20,393 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATION FRAMEA 97 TO 98, STRINGERS 29L TO 29R ON LOWER FUSELAGE SKIN. PERFORMED A REPAIR IAW EA 53-0373-17 PART 1 AND EC E17-701-01.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 30,994 hrs · 19,412 cycles

FLT 400, MSY-BOS. THE L1 DOOR WOULD NOT DISARM. LEVER WAS STUCK, REMOVED DEBRIS FROM GIRT BAR AND PERFORMED OPS CHECK OF DOOR ARMING. CHECKS PASSED. OK FOR CONTINUED SERVICE.

Part: CONTROL PANEL — FAILED (PITCH TRIM) · airframe 30,942 hrs · 19,384 cycles

WHILE CLIMBING THROUGH 28000 TO 34000, FLIGHT CREW RECEIVED A PITCH TRIM FAIL AND A PITCH TRIM BACK UP FAIL ON EICAS. EMERGENCY DECLARED. IAW FIM 27-43-00-810-809A, R & R TRIM CONTROL PANEL. ALL CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,868 hrs · 17,302 cycles

FOUND LT SIDE OVER DOOR LOWER LT EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY LIGHT POWER UNIT FORWARD CENTER FUSELAGE IAW AMM 33-50-01. OPS CHECK NORMAL.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 27,803 hrs · 17,270 cycles

AFTER BLOCKING IN AT GATE, THE L1 DOOR WAS WAS UNABLE TO BE DISARMED, THE HANDLE WOULD NOT MOVE. MAINTENANCE ENTERED VIA L2 DOOR. WHILE L1 DOOR WAS OPENED BY MAINTENANCE, THE SLIDE DROPPED FROM ITS ENCLOSURE AND JAMMED AGAINST JETWAY. INSTALLED L1 DOOR EMERGENCY EVACUATION SLIDE ASSY. OPS CK GOOD.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE, FOUND AFT CARGO BAY-LOWER SKIN PANEL, FRAME 76 SHEAR TIE 28L AND 28R HAS CORROSION. R & R SHEAR TIE AT FRAME 76, STRINGER 28L REF SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE FOUND AFT CARGO BAY-LOWER SKIN PANEL FRAME 76 SHEAR TIE S28L AND 28R HAS COROSION. R & R SHEAR TIEAND FRAME 76, STR 28R IAW SRM 51-41-12.

Part: SEAT TRACK — CORRODED (FRAMES 13-24) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE FOUND FORWARD FLOOR STRUCTURE RT SEAT TRACK FRAME 13-FRAME 14 AND FRAME 19-FRAME 20 HAS CORROSION. REMOVED OLD DOUBLER, ACCOMPLISHED DVI OF SEAT TRACK. FABRICATED NEW DOUBLER, DRILLED, COUNTERSUNK, TREATED AND PRIMED, AND INSTALLED NEW DOUBLER IAW E15-426-01. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SEAT TRACK — GOUGED (FRAMES 82-83) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE FOUND RT SIDEWALL SEAT TRACK HAS GOUGE BETWEEN FRAME 82-83. DURING EVALUATION FOUND CORROSION TO BE OUT OF LIMITS, R & R LT LATERAL SEAT TRACK BEAM IAW SRM 51-40-02, 51-41-01, 51-43-01 & 51-43-04.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE AFT CARGO BAY-LOWER SKIN PANEL, FRAME 76, SHEAR TIE S28L AND 28R HAS CORROSION. R & R SHEAR TIE AT FRAME 76, STR 28R IAW SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 75) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE AFT CARGO BAY-LOWER SKIN PANEL FRAME 75, SHEAR TIE 28L AND 28R HAS CORROSION. INSTALLED NEW SHEAR TIE AT FRAME 75, STR 75R IAW SRM 51-21-01 AND 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE FOUND AFT CARGO BAY-LOWER SKIN PANEL FRAME 77 SHEAR TIE S28L HAS CORROSION. R & R SHEAR TIE AT FRAME 77, STRINGER 28L REF SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 75) · corrosion level 2 · airframe 26,013 hrs · 16,021 cycles

DURING HEAVY MAINTENANCE FOUND AFT CARGO BAY-LOWER SKIN PANEL FRAME 75 SHEAR TIE 28L AND 28R HAS CORROSION. R & R SHEAR TIE AT FRAME 75, STR 28L IAW SRM 51-21-01 AND 51-41-01.

Part: FILTER — UNKNOWN (HYD SYSTEM) · airframe 21,793 hrs · 13,377 cycles

AIR RETURN, LANDING GEAR WOULD NOT COME UP. R & R NR 2 HYD SYS FILTER ELEMENTS & CASE DRAIN FILTER ELEMENT IAW AMM 29-11-07 & 29-11-05. LEAK CHECK GOOD. PERFORMED GEAR SWING 10 TIMES IAW AMM 32-33-00. OPS CHECK GOOD. RAN ENGINE & EDP PRESSURE GOOD. OK FOR SERVICE.

Part: CIRCUIT CARD — FAILED (EMERGENCY LIGHTS) · airframe 20,957 hrs · 12,800 cycles

ON MX CHECK, FOUND EMERGENCY LIGHTS FROM OVERWING EXIT AFT, FLASH SPURIOUSLY WHEN ACFT IS POWERED DOWN OR PUT ON GROUND SERVICE BUSS. R & R GENERAL I/O CARD MAU 2, MOD 9 IAW AMM 31-41-06. OPS CHECK SATISFACTORY.

Part: CIRCUIT CARD — FAILED (NR 1 MAU) · airframe 20,267 hrs · 12,381 cycles

FLT 114 MSY-JFK, CREW DECLARED AN EMERGENCY DUE TO AVNX MAU 1A FAIL ON DESCENT THRU FL 280. MULTIPLE ASSOCIATED EICAS MESSAGES FAIL MESSAGE CLEARED ON FINAL TO LAND. ACCOMPLISHED FIM TASK 45-45-00-810-939-A00. REMOVED AND REPLACED MAU 1 NIC1 PER AMM 31-41-04 OPS CHECK OK, OK FOR SERVICE.

Part: WIRE HARNESS — SHORTED (LE SLAT) · airframe 19,958 hrs · 12,191 cycles

FLT 571 HPN-PBI, AIRCRAFT DIVERTED TO JFK DUE TO SLATS WOULD NOT RETRACT AFTER TAKEOFF. ON TROUBLESHOOTING FOUND SKEW SENSOR HARNESS P0893 SHORTED TO SHIELDING AT PINS 1 AND 2. NEED TO REPLACE SKEW SENSOR HARNESS P0893 LEFT WING SKEW SENSOR BETWEEN SLATS 3/4. REMOVED AND REPLACED LEFT HARNESS P0893 IAW AMM 27-83-07. OPS CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,613 hrs · 11,370 cycles

FLT 131 BUF-JFK, ON GROUND MAINTENANCE CHECK FOUND R2 EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY BATTERY ELPU IAW EMB AMM 33-50-01. OPS CHECK OK.

Part: PRINTER — MALFUNCTIONED (COCKPIT) · airframe 17,912 hrs · 10,912 cycles

FLT 1216 BUF-BOS, SMOKE CAME OUT OF PRINTER IN FLIGHT. APPEARED TO BE JAMMED PAPER SMOLDERING. PERFORMED INSPECTION IAW FIM TASK 21-20-00-810-801-A. POSITIVELY IDENTIFIED SOURCE OF SMOKE/BURNING COMING FROM INTERNAL PRINTER COMPONENT. REMOVED AND REPLACED PRINTER IAW AMM 23-24-01-04. OPS CHECK NORMAL.

Part: SLAT — OUT OF RIG (WING) · airframe 15,888 hrs · 9,674 cycles

FLT 1199 JFK-ACK, AIR RETURN DUE TO SLAT FAIL ON RETRACT, RESET UNSATISFACTORY. FOUND ALL SLATS ON LT WING AND RT WING OUT OF RIG. MECHANICALLY RIGGED ALL SLATS ON LT AND RT WING IAW AMM 27-80-00-820-801-A. PERFORMED ELECTRONIC RIGGING OF ALL SLATS IAW AMM 27-80-00-820-802-A. SLAT RESOLVERS AND SKEW SENSORS WITHIN RIG LIMITS. OPS CHECK AND RIG CHECK OK.

Part: ENGINE — VIBRATION (NR 2) · airframe 15,447 hrs · 9,409 cycles

FLT 660 MCO-SYR, AIR RETURN TO MCO DUE TO NR 2 ENGINE WITH HIGH LP VIBRATION DURING T/O AND CLIMB. ENGINE NR 2 VIBRATION AMBER BOXED 4.1 ON LP. VIBRATION DECREASED ON LOW ALTITUDE LEVEL AND CAME BACK ON DURING CLIMB. T/S PER EMM 72-00-00 AND PERFORMED ENG VIBRATION TEST. ALL N1 VIB PARAMETERS WITHIN LIMITS. INTERROGATED CMC, NO PREVIOUS ABNORMAL FLIGHT NOTED. ALL VIBRATION PLOT INDICATION NORMAL. NO PREVIOUS EXCEEDANCES NOTED. A/C OK FOR CONT SVC. ENG HIGH POWER TEST PERFORMED REF EMM 72-00-00. MAX N1 REACHED 93.2. MAX LP VIBE 0.4 MAX HP 0.6. ALSO PERF VISUAL INSP OF SPINNER. NO DISCREPANCY NOTED.

Part: POWER UNIT — SHORTED (CABIN) · airframe 14,923 hrs · 9,083 cycles

FLT 6202 RDU-JFK EMERGENCY LIGHT ROW 13 AND AFT CAME ON WITH EMERGENCY LIGHT SWITCH IN OFF AND EXTERNAL POWER REMOVED. ACCOMPLISHED FIM TASK PER 33-50-00-810-812-A AND FOUND NR 4 EMERGENCY POWER UNIT TO BE FAULTING (SHORTING). REMOVED AND REPLACED UNIT PER AMM 33-50-01. ACCOMPLISHED TEST OF UNIT 33-50-01, OPS CHECK OK.

Part: ROD — BROKEN (TE FLAP) · airframe 13,837 hrs · 8,468 cycles

FLT 435 BOS-MCO, CREW REPORTED IN LEVEL FLIGHT A/C BANKED 5-10 DEGREES WITH AUTO PILOT ENGAGED. ON FLIGHT CONTROL PAGE LEFT OUTER AILERON INDICATES UP AND RIGHT OUTER AILERON DOWN. TRIM ROLL AND YAW CENTERED TRIM BALL CENTERED. THRUST ON BOTH ENGINES SYMMETRICAL. FOUND LOWER ROD ON LEFT INBOARD FLAP MECHANISM 1 BROKEN. REMOVED AND REPLACED LOWER ROD ON FLAP MECHANISM 1&2 REF AMM 57-54-30. OPS CHECK OK.

Part: INSERT — DAMAGED (BLEED AIR SYS) · airframe 11,542 hrs · 7,070 cycles

FLT JB463 BOS-RSW DIVERTED TO JFK BLEED 1 LEAK CLIMBED THRU FL290 RAN QRH AND BLEED 1 LEAK WENT OUT, SEVERAL MINUTES , BLEED 1 LEAK ILLUMINATED AGAIN, DUMPED PRESSURIZATION PER QRH. PERFORMED FIM TASK 36-21-00-810-801A AND FOUND ODS LOOP 3 LEFT WING HAS DAMAGED / MISSING CERAMIC INSERT. REPLACED INSERT AS PER CMM FENWAL 26-14-53. OPS CHECK NORMAL AS PER MM 45-45-00-970-805-A/200.

Part: PROBE — FAULTY (ADS) · airframe 11,506 hrs · 7,045 cycles

FLT JB242 LGB-OAK AIR TURNBACK TO LGB DUE TO WHILE AT CLIMB THRU 9000 FT ADS 2 HEATER FAIL, ADS 3 HEATER FAIL, ADS 4 HEATER FAIL EICAS MESSAGES APPEARED. CREW ACCOMPLISHED QRH PROCEDURES AND RETURNED TO THE FIELD AND LANDED SAFELY. LGB MX PERFORMED TROUBLESHOOTING IAW TSM 30-31-00-810-804/805, NO FAULTS NOTED. PERFORMED FHDB DOWNLOAD ANALYSIS SHOWS ADS PROBE NR 3 CHANNEL A TRIPPING. REMOVED AND REPLACED NR 3 ADS PROBE PER AMM 34-13-01 ACCOMPLISHED PITOT STATIC/AOA SENSOR HEATING ADJUST/TEST IAW AMM 30-31-00-710-801-A. OPS CHECK NORMAL, NO FAULTS NOTED ON EICAS. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 7,877 hrs · 4,959 cycles

JFK-PIT, STRONG UNKNOWN FUMES IN COCKPIT AND CABIN DURING INITIAL CLIMB. COMPLETED CABIN /SMOKE FUMES QRH AND RETURNED TO JFK. FUMES DISSIPATED INFLIGHT PRIOR TO LANDING. ACCOMPLISHED FIM TASK 21-20-00-810-801-A SMOKE AND /OR ABNORMAL SMELL IN PASSENGER CABIN AND/OR ABNORMAL SELL IN PASSENGER CABIN AND/OR COCKPIT. FOUND FOUL SMELL DURING ENGINE NR 1 OPERATION DUE TO ENGINE NR 1 BIRD INGESTION. ENGINE WAS BORESCOPED AND CLEANED, NO ABNORMALITIES NOTED. PERFORMED ELECTRICAL ODOR INSPECTION PER LTV MM 44-20-10. NO ABNORMALITIES NOTED. LTV OPS NORMAL.

Part: UPLOCK ACTUATOR — FAILED (RT MLG) · airframe 6,436 hrs · 4,152 cycles

FLT 4152, IAD-BOS, UPON LANDING GEAR EXTENSION, BRK CONTROL FAULT LG LEVER DISAG, RIGHT MAIN LANDING GEAR DISPLAYED UNSAFE INDICATION. ALL INDICATIONS RETURNED TO NORMAL WITHIN 1 MINUTE. CYCLED GEARS MANY TIMES AND COULD NOT DUPLICATE FAULT, AS PRECAUTIONARY REMOVED AND REPLACED RT MLG UPLOCK ACT ASSY WITH 2 EACH NEW SENSORS ALREADY INSTALLED PER MM 32-31-03. ALSO LUBED MLG UPLOCK ROLLER ASSY PER CMM 32-11-14 MLG SHOCK STRUT PER EMBRAER TECH SUPPORT ENGINEER. OPS CHECKED MANY TIMES, NO FAULTS FOUND. A/C OK FOR CONTINUED SERVICE PER EMBRAER I/C 2008-190/02336A.

Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 6,044 hrs · 3,919 cycles

FLT 610, JAX-JFK, ON FINAL APPROACH, LANDING GEAR LIGHT DISAGREE RIGHT MAIN DID NOT INDICATE DN/LOCKED. "LG LEVER DISAG". QRH CHECK LIST AND LDG ABNORMAL EXTENSION CHECK LIST COMPLIED WITH. RT MAIN GEAR DID THEN SHOW GREEN DOWN/LOCKED. MANUAL RELEASE LEVER DEPLOYED GEAR. NOT OVERRIDE. REPLACED RT MAIN LANDING GEAR UPLOCK BOX PER AMM 32-31-03 AND PERFORMED AN OPERATIONAL TEST OF THE LANDING GEAR SYSTEM PER AMM 32-33-00-710-801A/500. OPS CHECK OK.

Part: WIRE HARNESS — SHORTED (RT SLAT) · airframe 2,106 hrs · 1,407 cycles

SLAT FAILED AT 0 DURING CLIMB OUT AT 5500 FT WITH SLAT/FLAPS AT 0/0. ACCOMPLISHED ELECTRICAL CK OF THE OB SLAT SKEW SENSOR AND WIRE HARNESS. IAW FIM 27-83-00-810-814-A. REPLACED FAULTED RT WIRE HARNESS (W612) IAW M/M 27-83-07 FOR SLATS 3/4 SKEW SENSOR. OPERATION CKS NORMAL. FAIL MSG CLEARED.