N273JB

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,222 hrs · 27,526 cycles

FLT#8428, BTV-JFK. ' FUME EVENT-STRONG DIRTY SOCK ODOR ON TAKEOFF AND LANDING/TAXI IN; PERFORMED FIM TASK FIM 21-20-00-810-801-A AND 21-20-00-810-803-A BOTH PACKS OPERATED USING ENGINE AND APU BLEED NO EVIDENCE OF ODOR FOUND AIRCRAFT CONSIDERED SERVICEABLE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,123 hrs · 27,453 cycles

FLT#2555, BOS-DCA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' “CABIN/COCKPIT ODOR – DIRTY SOCK / VOMIT (STRONG) FROM A/C ECS VENTS FIRST NOTICE DURING T/O ROLL (HIGH SPEED) PERSISTED THROUGH CLIMB. ODOR PRESENT IN COCKPIT, FWD + AFT CABIN. ALSO FAINT TO MODERATE OIL/BURNING OIL ODOR DURING CLIMB- UNKNOWN DURATION. SOCK/VOMIT ODOR STILL PRESENT ON GROUND AFTER LANDING AT IDLE POWER”; REF FIM 21-20-00-810-805-A NO ODORS DETECTED. NO HISTORY. OK FOR SVC. NOTE- #1 ENG WATER WASH PERFORMED REF PREVIOUS LP. SUSPECT THAT WAS THE CAUSE AND IS NORMAL.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,983 hrs · 27,335 cycles

FLT#2587, JFK-DCA. 'RH WING MIDDLE EXTERNAL EMERGENCY LIGHT INOP; REMOVED AND REPLACED #4 ELPU IAW E190 AMM 33-50-01. OPS CHECK GOOD. AIRCRAFT OK FOR CONTINUED SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,793 hrs · 27,163 cycles

FLT#8492, ACK-JFK. 'L1 DOOR PNEUMATIC ASSIST BOTTLE DEACTIVATED; RE-ACTIVATED / RE-PINNED L1 DOOR ASSIST BOTTLE IAW AMM 52-00-23. OPS CHECK GOOD.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,663 hrs · 27,062 cycles

FLT#1338, JFK-MVY. 'L1 DOOR WILL NOT LATCH AND ARM; FOUND GRIT BAN NOT ATTACHED TO L1 DOOR BRACKET. ATTACHED GRIT BAR PER AMM 52-11-41-400-O1. OPERATED FWD PASSENGER DOOR ARM AND DISARM PER AMM 52 -11 -00.'

Part: SLIDE — NO TEST (L1 DOOR) · airframe 41,603 hrs · 27,016 cycles

FLT#1484, RDU-BOS. 'L1 SLIDE REMOVED FOR EC;25-65-01-002-FLH S/N EF1050; INSTALLED L1 DOOR SLIDE REF AMM 25-65-01 NOTE SN/ EF1050 FAILED OPS TEST.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: CORROSION IN FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1; (RESOLVED ON W/O: 1216530 TASKCARD: NR-00002 ) ALL WORK ACCOMPLISHED ON TOMEX NRC 00149, FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1, IT IS CLASSIFIED AS NON-REPAIRABLE THEREFORE WAS REPLACED PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-10-02, SRM 51-41-01, SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: [CPCP FINDING] CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH AT FLOOR STRUCTURE W2; ALL WORK ACCOMPLISHED ON TOMEX NRC # 00094: CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH WAS REMOVED AND EVALUATED, THEREFORE IS OUT LIMITS. THE FLOOR BEAM WAS REPLACED PER EMB190 SRM 51-41-01, SRM 51-42-01, AND SRM 51-43-03. NO SPECIFIC OR ADDITIONAL INSPECTION REQUIREMENTS. (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: [CPCP FINDING] CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH AT FLOOR STRUCTURE W2; (RESOLVED ON W/O: 1216530 TASKCARD: NR-00001 ) ALL WORK ACCOMPLISHED ON TOMEX NRC # 00094: CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH WAS REMOVED AND EVALUATED, THEREFORE IS OUT LIMITS. FLOOR BEAM WAS REPLACED PER EMB190 SRM 51-41-01, SRM 51-42-01 AND SRM 51-43-03. NO SPECIFIC OR ADDITIONAL INSPECTION REQUIREMENTS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: REF TOMX W/O 2195 NR 00310. CRACK SUSPECT IN INBOARD FITTING SPAR AT RH PYLON; REF TOMX W/O 2195 NR 00310. INBOARD FITTING SPAR AT RH PYLON WAS REPLACED PER EMB-190 S.R.M. 51-43-03 AND S.R.M. 51-43-04.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: ELPU #1 & #3 INOPERATIVE; REF TO TOMX WO 2195 NR 00385, REMOVED ELPU #1 PN 3400-22-10 SN 001913 AND ELPU #3 PN 3400-22-10 SN 001895 AND REPLACED WITH ELPU #1 PN 3400-22-10 SN 015432 AND ELPU #3 PN 3400-22-10 SN 001910 PER EMB190 AMM 33-50-01-000-801-A WITH SATISFACTORY TEST.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: CRACK ON LH WING FIXED LEADING EDGE SLAT #5 CUTOUT; REF TOMX W/O 2195 NR 00025. REMOVED AND REPLACED SKIN PANEL PER EMB SRM 51-41-02 AND SRM 51-43-04.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTW STGR 28R - 27R / CORROSION -TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,972 hrs · 26,534 cycles

DURING HEAVY MAINTENANCE: CORROSION IN FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1; ALL WORK ACCOMPLISHED ON TOMEX NRC 00149, FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1, IT IS CLASSIFIED AS NON-REPAIRABLE THEREFORE WAS REPLACED PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-10-02, SRM 51-41-01, SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04. (CONSIDERED AS A MAJOR REPAIR)

Part: LIGHT — FAILED (EMER-BATT-AFT-RH) · airframe 38,646 hrs · 24,898 cycles

FLT#968, PBI-HPN. 'REAR EMERGENCY LIGHT INOP; REPLACED CABIN EMER LIGHT ASSY FWD OF AFT GALLEY IAW AMM 33-50-13. OPS CHECK FAIL. NO FIX. REMOVED AND REPLACED ELPU # 5 IAW AMM 33-50-01. OPS CHK OK. NO DEFECTS WERE NOTED. ALL CABIN EMER LIGHTS ARE OPERATIONAL. OK FOR SERVICE.'

Part: NONE — NONE · airframe 38,550 hrs · 24,845 cycles

FLT#2094, NAS-FLL. ' L-1 DOOR ASSIST BOTTLE NOT HOLDING PRESSURE.; FOUND L1 DOOR, DOOR ASSIST DIAPHRAGM DAMAGED. REMOVED AND REPLACED L1 DOOR DIAPHRAGM IAW AMM: 52-11-53. LEAK CHECK GOOD.'

Part: SLIDE — DEPLOYED (L1-SLIDE) · airframe 38,195 hrs · 24,622 cycles

FLT # 1576, KIN-FLL. REF W/O 1158783 L1 DOOR SLIDE R& R ASSIGNED. ACCOMP CONTROL SLIDE DEPLOYMENT DUE UNABLE TO INSTALL SAFETY PIN; CONTROL SLIDE DEPLOYMENT ACCOMP PER GMM 6.24.3 NO FAULTS DIAPHRAGM REPLACED PER AMM 52-41-53 SERVICED AND LEAK CHK GOOD.

Part: HINGE FITTING — MISALIGNED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, (E/C E22-045-01) FUSELAGE / REAR FUSELAGE / H. STABILIZER HINGE / FR 100 / RH FITTING / MISALIGNMENT - TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)

Part: SHEAR TIE — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, W.O 1094103 NR 00006 CORROSION ON SHEAR CLIP BTW STGR 28LH/ STGR 29LH OVER FR76 AT AFT CARGO COMPARTMENT; CORROSION FOUND TO BE OUT OD LIMITS IAW SRM 51-12-01 REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02 51-41-01 REFERENCE TECHOPSMX NR 00105 FOR WORK ACCOMPLISHED TECH 201635713 RII INSPECTOR 200002656

Part: HINGE FITTING — WORN · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, (E/C E22-044-01) FUSELAGE / REAR FUSELAGE / H. STABILIZER HINGE / FR 100 / LH FITTING / WEAR - TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)

Part: LUG — WORN · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, WEAR WAS FOUND ON BORE OF LH LUG (AFT LOOKING FWD) OF CENTRAL FITTING OF LH REAR FUSELAGE TO THS FITTING ASSY; REF TOMX NR 00150: BORE OF LH LUG (AFT LOCKING FWD) OF CENTRAL FITTING OF LH REAR FUSELAGE TO HORIZONTAL STABILIZER FITTING ASSY WAS REWORKED WITH JB EC E22-044-01, ETI-190-22-503-REV 4, AND EMBRAER ETD2022-190-000513.

Part: STRINGER — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, (E/C E22-008-02) FUSELAGE/ CENTER FUSELAGE III / STRINGERS 28LH AND 29 RH / FR 76-77 CORROSION/ PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)

Part: SHEAR TIE — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, CORROSION ON INTERNAL STRUCTURE SHEAR CLIP AT WASTE CUT OUT FR88 BTW STGR 25R/28R, CENTER FUSELAGE III; CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-01, REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02. REFERENCE TECHOPSMX NR 00070 FOR WORK ACCOMPLISHED TECH 201635713 RII INSPECTOR 200002656

Part: SHEAR TIE — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, W/O 1094103 NR 00002 CORROSION ON SHEAR CLIP BTW STGR 29RH STGR 28RH OVER FR75 AT AFT CARGO COMPARTMENT; CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16 REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02 REFERENCE TECHOPSMX NR 00103 FOR WORK ACCOMPLISHED TECH 201635713 RII 200002656

Part: NONE — NONE · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, EXCESSIVE PLAY IN THS: RH HINGE FITTING SPHERICAL BEARING LOOSE AND CORRODED. THS OUT OF ALIGNMENT; REF TOMX NR 00148: MISALIGNMENT ON RH FRAME 100 REAR FUSELAGE TO HORIZONTAL STABILIZER FITTING ASSY WAS CORRECTED WITH EC E22-045-01 AND ETI-190-22-502-REV, AND EMBRAER ETD2022-190-000485

Part: SHEAR TIE — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, W.O 1094103 NR 00005 CORROSION ON SHEAR CLIP BTW STGR 29RH/ STGR 28RH OVER FR76 AT AFT CARGO COMPARTMENT; CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-01 REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02 51-41-01 REFERENCE TECHOPSMX NR 00100 FRO WORK ACCOMPLISHED TECH 201635713 RII INSPECTOR 200002656

Part: SHEAR TIE — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, W.O 1094103 NR 00004 CORROSION ON SHEAR CLIP BTW STGR 27LH / STGR 28 LH OVER FR76 AT AFT CARGO COMPARTMENT; CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-01 REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02 REFERENCE TECHOPSMX NR 00102 FOR WORK ACCOMPLISHED TECH 201635713 RII INSPECTOR 200002656

Part: RIB — CRACKED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, CRACK ON FIXED LEADING EDGE RIB #17 AT LH WING; REF: TOMX W/O 1788 N/R -00068 REPLACED RIB PEER EMB190 SRM 51-41-02, 51-43-04, AND SRM 51-43-03

Part: STRINGER — CORRODED · airframe 38,185 hrs · 24,617 cycles

DURING HEAVY MAINTENANCE, (E/C E22-008-01) FUSELAGE/ CENTER FUSELAGE III / STRINGERS 28LH AND 29 RH / FR 76-77 CORROSION/ TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)

Part: SKIN — DAMAGED · airframe 37,756 hrs · 24,332 cycles

DURING HMV, EA E21-1098-01 FUSELAGE/ FWD FUSELAGE/ SKIN AT FR6, S-21R-EXISTING TEMPORARY REPAIR/ TEMPORARY REPAIR (MAJOR REPAIR).

Part: LIFE RAFT — UNWANTED DEPLOY (GALLEY) · airframe 35,412 hrs · 22,812 cycles

FT # 1637, SJU-SDQ. DURING SECURITY CHECK #2 LIFE RAFT IN FORWARD GALLEY DEPLOYED INTO THE FORWARD CABIN( LIFE RAFT ); LIFE RAFT PLACED ON MEL PER 25-66-01 CAT D MDDR# 411480 PER MCC CRIS - MX-4 UPDATED PLACARD INSTALLED. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 32,893 hrs · 20,989 cycles

FLT 112, ORD-BOS. L1 DOOR REQUIRED (MANUAL) DEPLOYMENT REQUIRED DUE TO (UNCOMMANDED) UNPACKING; R & R L1 SLIDE PACK ASSEMBLY IAW AMM 25-65-01/400. OK TO CONTINUE. OP CHK OF ARM/DISARM AND DOOR CLOSING MECHANISM GOOD.

Part: ACM — FAILED (AC BAY) · airframe 26,063 hrs · 16,027 cycles

FLIGHT CREW AND CUSTOMERS REPORTED STRONG SULFUR SMOKE ODOR WITH VISIBLE SMOKE MID CABIN. FLIGHT CREW SHUTOFF THE LTV SYS UPON RECEIVING THE REPORT. A PACK 2 FAIL THEN OCCURED AND CREW DESELECTED THE PACK. THE ODOR AND SMOKE DISSIPATED QUICKLY AFTER THE LTV AND PACK WERE SELECTED OFF. THE ODOR & SMOKE GRADUALLY DIMINISHED. FOUND NR 2 ACM FAILED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 25,683 hrs · 15,761 cycles

ACFT LANDED WITH THE NOSE GEAR NOT FULLY EXTENDED. THE NOSE GEAR MADE A VERY ABNORMAL SOUND. INDICATIONS DID NOT SHOW THE NOSE GEAR DOWN AND LOCKED. THE NOSE COLLAPSED UPON LANDING ONTO THE NOSE OF THE PLANE. PASSENGERS AND CREW EXITED THE ACFT WITH NO REPORTED INJURIES. ACFT IS UNDER INVESTIGATION, SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: CONTROL MODULE — MALFUNCTIONED (NLG STEERING) · airframe 22,428 hrs · 13,649 cycles

ACFT EXECUTED AN EMERGENCY LANDING DUE TO STEERING FAIL EICAS WHEN GEAR EXTENDED. NOSE WHEEL STEERING INOPERATIVE ON LANDING. ACCOMPLISHED RESET OF STEERING CONTROL MODULE IAW FIM TASK 32-53-00-810-818. ALL FAULTS CLEARED AND OPS TEST OF NWS ACCOMPLISHED AND CHECKS NORMAL. ACFT OK TO CONTINUE.

Part: DOUBLER — CORRODED (FRAME 88) · airframe 21,250 hrs · 12,932 cycles

DURING HEAVY SERVICE, WASTE BOX DOUBLER AT FRAME 88, NEAR STR 28R HAS CORROSION AT SHEAR CLIP AREA. ACCOMPLISHED DVI OF THE CORRODED AREA TO ENSURE NO ADDITIONAL DAMAGE EXISTS. REAMED THE HOLE TO THE MINIMUM DIAMETER WITHIN H7 TOLERANCE UNTIL ALL CORROSION REMOVED. PERFORMED HFEC INSPECTION OF REAMED HOLE IAW E190, PART 1, 51-00-00-916-801 TO VERIFY NO CRACKS EXISTS. MANUFACTURED A SPECIAL BUSHING IAW E190, SRM 51-10-07, CASE 02. COMPLIED WITH E14-536-01, SRM 53-23-01, FIG 35, ITEM 20 AND NR H4350/1667. RETURN ACFT TO NORMAL CONFIGURATION.

Part: FLOORBEAM — CORRODED (FRAME 17) · airframe 21,250 hrs · 12,932 cycles

DURING HEAVY MAINTENANCE, FOUND FLOORBEAM CORRODED AT FRAME 17 BETWEEN LBL 12 AND RBL 12. BLENDED OUT THE CORROSION IAW SRM 51-10-03 PART 11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 16,393 hrs · 9,864 cycles

FLT 6425 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN CORROSION ON FR 17 CROSS BEAM. REPAIRED BY BLENDING CORROSION, HFEC INSP, MACHINED TWO L SHAPED ANGLES, REPOSITIONED FLOOR STRUCTURE BRACKET AS REQUIRED, FILL LOW AREAS WITH HYSOL, BLEND SMOOTH AFTER CURE AS PER EA E13-014-01.

Part: ENTERTAIN SYS — ODOR (CABIN) · airframe 6,621 hrs · 3,865 cycles

FLT 34 JFK ROC ON TAKE OFF CLIMBING TO 1500 FT FA NR 2 REPORTED A "BURNED PLASTIC ODOR" VERY STRONG IN THE BACK. A LITTLE IN FRONT OF CABIN AND NO SMELL IN COCKPIT NO SMOKE WAS REPORTED.GOING TO 14000 FT ODOR DISSIPATED ON DESCENT FA NR 2 SAID ODOR CAME BACK A LITTLE BUT NOT AS MUCH AS ON TAKE OFF. NO EICAS MSG OR LTV ISSUES ASSOCIATED WITH ODOR. ACCOMPLISHED FIM TASK 21-00-00-810-801-0A FOUND NO DEFECTS. OPERATED PNEU SYS USING APU BLEED NO DEFECTS NOTED. OPERATED COFFEEMAKER SYS CHECKS OK NO DEFECTS NOTED. ACCOMPLISHED FIM TASK 75-30-00-810-801A FOUND NO DEFECTS ON AFT GALLEY AREA. ACCOMPLISHED GEN VISUAL INSPECTION OF AFT LAV AND AFT AVIONICS COMPARTMENTS NO SIGNS OF ELECTRIC BURNING OR PLASTIC BURNING NOTED. ITEM IS STILL OPEN LTV SYSTEM IS DEACTIVATED DUE TO PLASTIC BURNED ODOR, OPS CHECK GOOD PER LTV AMM 44-20-10.

Part: FADEC — FAILED (NR 2 ENG) · airframe 6,172 hrs · 3,588 cycles

FLT 581, HPN-PBI, DURING DESCENT WITH THRUST LEVERS AT IDLE APPROX 11,000 FT, GOT A ELEV THR COMP FAIL. COMPLIED WITH THE QRH BUT MSG REMAINED STILL DESCENDING THROUGH APPROX 9,000 FT. GOT AN ENG 2 FAIL MSG (THRUST AT IDLE), COMPLIED WITH QRH AND WERE ABLE TO RELIGHT ENG. ENGINE REMAINED OPERABLE THROUGHOUT LANDING (NORMAL/0) AND TO GATE. ACCOMPLISHED ESM 72-00-00. FAULT ISOLATION 008, REMOVED AND REPLACED NR 2 ENGINE FADEC IAW CF34-10E EMM 73-00-00-800-812. ALL OPS OK.