N329JB

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 31,128 hrs · 20,909 cycles

FLT#317, BOS-JFK. 'L2 DOOR WILL NOT OPN JAMMING ON UPPER LEFT SIDE; FOUND L2 DOOR ASSIST BOTTLE SAFETY PIN BENT PREVENTING CORRECT OPERATION OF DOOR. REMOVED PIN, INSPECTED DOOR, NO DAMAGE NOTED. OPS CHECKS GOOD, AMM; 25-65-00.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,700 hrs · 20,618 cycles

DURING HEAVY MAINTENANCE: DURING SERVICE CHECK FOUND AN EMERGENCY LIGHT AT L1 DOOR INOP; REF TOMX NRC 00039 WO 2157 EMERGENCY LIGHT POWER UNIT #2 WAS REPLACED PER EMB-190 AMM 33-50-01. OPS TEST GOOD.'

Part: ROLLER — LACK OF LUBE (RT OVERWING DOOR) · airframe 30,268 hrs · 20,307 cycles

FLT#1073, JFK-BNA. AIRCRAFT DIVERTED TO BOS. DOOR EMERGENCY RT OPEN EICAS MESSAGE IN FLIGHT. FOUND RT OVERWING EXIT DOOR NOT FULLY LATCHED. DETERMINED FWD LOCKING ROLLER STICKING AND NOT ENGAGING LOCKING MECHANISM. LUBRICATED FWD AND AFT LOCKING ROLLERS DOOR LOCKS AND OPERATED NORMALLY. OK FOR CONTINUED SERVICE IAW AMM 52-21-21.

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 29,986 hrs · 20,130 cycles

FLT # 1354, DCA-BOS. #1 ENGINE BLEED FAIL DURING CLIMB OUT.WAS RESET WITH QRH.BLEED 1 FAIL DURING DESCENT.REST WITH QRH.BOTH DURING ICE CONDITIONS.REPEAT WRITE UP; R+R'D ENG #1 FAN AIR VALVE IAW AMP 36-11-09- OPS AND LEAK CHECK GOOD MDDR CLEARED UPDATED MX-4 UPDATED AND REMOVED PLACARD

Part: ANTI-ICE SYSTEM — FAULTED · airframe 29,990 hrs · 20,133 cycles

FLT # 2041, CROSS BLEED FAIL IN FLIGHT COULD NOT RESET ENCOUNTERED ICING + SYSTEM COULD NOT FUNCTION W ONE BLEED AND NO BLEED ; PERFORMED OPS CHECK OF CROSS BLEED SYSTEM OPS CHECK GOOD REF FIM 36-10-00

Part: VALVE — FAILED (BLEED) · airframe 29,986 hrs · 20,130 cycles

FLT# 1354, DCA-BOS. #1 ENGINE BLEED FAIL DURING CLIMB OUT.WAS RESET WITH QRH.BLEED 1 FAIL DURING DESCENT.REST WITH QRH.BOTH DURING ICE CONDITIONS.REPEAT WRITE UP; R+R'D ENG #1 FAN AIR VALVE IAW AMP 36-11-09- OPS AND LEAK CHECK GOOD MDDR CLEARED UPDATED MX-4 UPDATED AND REMOVED PLACARD.

Part: STRINGER — CORRODED (FRAMES 74-75) · airframe 22,695 hrs · 15,222 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE STRINGER 22L BETWEEN FRAMES 74-75. THE REF.(5) SRM PROVIDES AN APPLICABLE SPLICE REPAIR, HOWEVER THE SPECIFIED REINFORCING ANGLE IS NOT AVAILABLE. EMBRAER WAS CONTACTED FOR REPAIR DISPOSITION, AND EMBRAER PROVIDED THE REF.(2) ETD CONSISTING OF ACCOMPLISHING REPAIR PER REF.(5) BUT USING ALTERNATE REINFORCING ANGLE MATERIAL. IN ADDITION, ALTERNATE FASTENER INSTALLATION FOR PRODUCTION WAS APPROVED BY BOTH REF.(1) AND REF.(3). AEROMAN ISSUED THE REF.(1) EA ACCOMPLISHING THIS REPAIR, AND THIS EC INCORPORATES THE REF.(1) EA WITHOUT DEVIATION; THIS REPAIR HAS BEEN APPROVED BY THE REF.(4) ANAC FORM. THIS REPAIR IS CLASSIFIED AS A MAJOR PERMANENT REPAIR.

Part: SKIN — DAMAGED (LT WING TE) · airframe 22,695 hrs · 15,222 cycles

DURING HEAVY MAINTENANCE, DISCOVERED CRACK RIB 9 WING MAIN BOX TO RIB 10 EXTERNAL SKIN TRAILING EDGE ON LH WING (1 EA); REF. AERO N/R 2019-41038. PERFORMED PERMANENT REPAIR LOC. BTW RIB 9 TO RIB 10 EXTERNAL LOWER SKIN TRAILING EDGE ON LH WING I.A.W E190 SRM 57-10-01. REPAIR 54.

Part: ACCESS PANEL — CORRODED · airframe 22,695 hrs · 15,222 cycles

DURING HEAVY MAINTENANCE, WAS REPORTED WITH CORROSION DAMAGE AFFECTING THE TAIL COND FORWARD ACCESS PANEL 351GL (PN 190-17325-401) AT FORWARD EDGE (SEE REF /1/ EA FOR DETAILS). THE DAMAGE IS OUT OF SRM SCOPE AND EMBRAER WAS CONTACTED FOR GUIDANCE. EMBRAER PROVIDED REF /2/ ETD CONSISTING OF TRIMMING OUT THE DAMAGED AREA, PERFORMING NDT INSPECTIONS, FABRICATING AND INSTALLING A FILLER AND A REPAIR DOUBLER. THIS REPAIR DOES NOT ADVERSELY AFFECT A FATIGUE CRITICAL STRUCTURE AND DOES NOT REPRESENT AN AIRWORTHINESS LIMITATION. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY; EMBRAER APPROVED THIS REPAIR PER REF /3/ ANAC FORM AND IS CLASSIFIED AS MAJOR.

Part: ENGINE — CONTAMINATED · airframe 18,760 hrs · 12,379 cycles

STRONG PUNGENT AND NOXIOUS ODOR EXPERIENCED BY FLIGHT CREW DURING TAKEOFF AND CLIMBOUT. EXPERIENCED STRONG ODORS IN FWD.GALLEY THROUGH MID CABIN. CONFIRMED ODOR PRESENCE AT ROW 14 BRIEFLY. NO VISIBLE HAZE OR SMOKE PRESENT IN COCKPIT OR CABIN. ODORS GRADUALLY DISAPPATED AS AIRCRAFT CLIMBED. NOT PRESENT AFTER 10,000 FT. TAKEOFF WAS PERFORMED T/O 1 ECS ON FLEX 47,N1 87%.APU OFF. AFT GALLEY DID NOT HAVE ODOR PRESENT. THE ABNORMAL ODOR OCCURED AFTER ENGINE COMPRESSOR WASH IAW FIM 21-20-00-810-803-A. ACFT OKAY TO CONTINUE. NO DEFECTS OR ODOR NOTED.

Part: BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FWD SERVICE DOOR LOWER BEAM SEVEN INCHES AFT OF FRAME 16, RBL 49.5. R & R THE BEAM IAW SRM 51-34-04.

Part: BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FWD SERVICE DOOR LOWER BEAM 9.75 INCHES AFT OF FRAME 16 RBL 49.5. R & R THE BEAM IAW SRM 51-43-04.

Part: FLOORBEAM — CORRODED (FRAME 75) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 75 FROM CENTERLINE TO STRINGER 29R. R & R THE FLOORBEAM IAW IAW SRM 51-40-01.

Part: FLOORBEAM — CORRODED (FRAME 75) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 75 STR 29L-29R. R & R THE FLOORBEAM IAW SRM 51-40-01.

Part: BEAM — CORRODED (FRAME 77) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO CUTOUT LOWER BEAM AT FR 77 + 6 RBL 17. R & R THE BEAM IAW SRM 51-40-01, 51-41-02, AND 51-43-03.

Part: FLOORBEAM — CORRODED (FRAME 77) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 77. R & R THE FLOORBEAM IAW AMM 51-41-02.

Part: BEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FWD SERVICE DOOR LOWER BEAM 2.5 INCHES AFT OF FRAME 14 RBL 49.5. R & R THE BEAM IAW SRM 51-43-04.

Part: BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 16,030 hrs · 10,426 cycles

DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FWD SERVICE DOOR LOWER BEAM CORRODED 11.75 INCHES AFT OF FRAME 16 RBL 51. R & R OF FWD LOWER BEAM IAW SRM 51-43-04.

Part: ACM — FAILED (NR 2) · airframe 15,532 hrs · 10,051 cycles

FLT 1131, AIR TURN BACK, EMERGENCY DECLARED. CREW EXPERIENCED A BURNING PLASTIC ODOR IN THE CABIN. PAX REPORTED THERE WAS POP ON THE RT SIDE OF THE ACFT RIGHT BEFORE THE ODOR AND SMOKE. PAX ALSO REPORTED THAT GRAY PEBBLES WERE SHOOTING OUT OF THE OVERHEAD VENTS AT THE SAME TIME AS WELL. ODOR WAS REPORTED AS EMITTING FROM THE GASPER VENTS. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. DURING INSPECTION, NR 2 ACM WAS FOUND BURNED OUT. R & R ACM. PERFORMED OPS CHECK. OPS CHECK PASSED.

Part: BATTERY — FAILED (EMREGENCY LIGHTS) · airframe 14,413 hrs · 9,314 cycles

FWD RT EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT POWER UNIT NR 1 IAW AMM 33-50-01. OPS CHECK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 14,413 hrs · 9,314 cycles

FWD RT EMERGENCY LIGHTS INOPERATIVE.; R & R EMERGENCY, LIGHT POWER UNIT NR 1 IAW AMM 33-50-01. OPS CHECK GOOD.

Part: FAN — FAILED · airframe 14,402 hrs · 9,308 cycles

REMOTE CB. TRIP, FAN EBAY 1 MID, ODOR OF ELECTRICAL ISSUES FOR 20 MIN OF FLIGHT; MID EBAY FAN 1 C/B POPPED, REPLACED MID EBAY FAN 1 IAW AMM 21-26-04, PERFORMED BITE CHECK THROUGH CMC CHECKS GOOD.

Part: ACM — FAILED (NR 2) · airframe 9,375 hrs · 5,936 cycles

DURING DESCENT, BURNING ODOR FILLED CABIN FOLLOWED BY A PACK 2 FAIL MESSAGE. ODOR IMPROVED ONCE PACK 2 WAS OFF. PERFORMED AMM TASK 21-20-00-810-801-A, FOUND NR 2 A/C PACK AT FAULT. R & R NR 2 ACM DUE TO A BROKEN BLADE IAW AMM 21-51-05.

Part: I/O MODULE — FAILED (NR 2) · airframe 5,082 hrs · 3,171 cycles

FLT 6128 MCO-BOS, AIR TURNBACK TO MCO DUE TO ANTI ICE WING 2 LEAK MSG AT 410 IN NON ICING CONDTITONS. FOLLOWED QRH MESSAGE EXTINGUISHES. MSG RETURNED 30 MIN LATER. FOLLOWED QRH WITH BLEED 2 AND X BLEED OUT MSG CONTINUE INTERMITTENTLY. FOLLOWED TSM 30-11-00-810-823A. REMOVED AND REPLACED CUSTOM I/O MODULE 2 IAW 31-41-07. PERFORMED OPS TEST OF WING ANTI ICE SYSTEM PER 30-11-00, OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (RT WING) · airframe 5,082 hrs · 3,171 cycles

FLT 6128 MCO-BOS, AIR TURNBACK TO MCO DUE TO ANTI ICE WING 2 LEAK MSG AT 410 IN NON ICING CONDTITONS. FOLLOWED QRH MESSAGE EXTINGUISHES. MSG RETURNED 30 MIN LATER. FOLLOWED QRH WITH BLEED 2 AND X BLEED OUT MSG CONTINUE INTERMITTENTLY. FOUND BUTTERFLY ON VALVE WITH GAPS. REMOVED AND REPLACED RIGHT WING SLAT ANTI ICE VALVE IAW 30-11-01. PERFORMED OPS TEST GOOD, NO LEAKS NOTED.

Part: WIRE HARNESS — DEFECTIVE (ANTI-ICE SYSTEM) · airframe 5,078 hrs · 3,169 cycles

FLT 522 MCO-EWR, AIRCRAFT DIVERTED TO CLT DUE TO ANTI ICE WING 2 LEAK EICAS MESSAGE CAME ON AT FL370. NON ICING CONDITIONS SHUT OFF WING ICE DETECT BUTTON PER QRH MESSAGE EXTINGUISHED AND THEN RETURNED. SHUT BLEED 2 AND X BLEED PER QRH. MESSAGE RETURNED AND EXTINGUISHED. REMOVED AND REPLACED W611 HARNESS & TEMP SENSOR FOR NR 2 RIGHT SLAT OUTBOARD IAW AMM 30-11-02.

Part: FAN — FAILED (CARGO BAY) · airframe 4,806 hrs · 3,010 cycles

FLT 1242 CLT-BOS, DURING FINAL APPROACH TV'S WENT BLANK. F/A'S NOTICED SMELL OF ELECTRICAL BURNING IN CABIN OF AIRCRAFT. REPLACED AFT CARGO RACK VENT FAN IAW AMM 21-28-00. OPS CHECK OK.

Part: FADEC — FAILED (NR 2 ENGINE) · airframe 4,806 hrs · 3,010 cycles

FLT 1242 CLT-BOS, CREW DECLARED EMERGENCY AND AIR RETURN TO CLT DUE TO NR 2 ENGINE FAILED AT 16000FT. REIGNITED APPROX 20 SECONDS LATER WITH NO EICAS MESSAGES. THE NR 2 ENGINE FADEC WAS REMOVED AND REPLACED PER AMM 73-00-00-800-812. PERFORMED GROUND POWER ASSURANCE CHECK PER ENG MANUAL CF34-10E ESM 72-00-00 TESTING 03, NO FAULTS FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 1,408 hrs · 881 cycles

FLT JB1259 BOS-IAD, DURING MAINTENANCE EMERGENCY LIGHT ON CEILING, FORWARD OF OVERWING EXIT FAILED TO ILLUMINATE DURING NORMAL MAINTENANCE TEST. REMOVED AND REPLACED BATTERY PACK/CHARGER OVER FWD LT DOOR. OPS CHECK OF EMERGENCY LIGHTS GOOD PER AMM 33-50-01.

Part: POWER UNIT — FAILED (COCKPIT) · airframe 1,137 hrs · 707 cycles

FLT 560, MCO-HPN, ON PREFLIGHT AT HPN, CREW FOUND COCKPIT CENTER OVERHEAD OVAL LENS INTERIOR EMERGENCY LIGHT NOT ILLUMINATED WHEN ON. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT (ELPU) IAW AMM 33-50-01. SYSTEM OPS CHECK OK AT THIS TIME.