N292JB

Part: UNKNOWN — ODOR (CABIN) · airframe 36,062 hrs · 23,174 cycles

FLT #1366, CUN-TPA. CABIN ODOR REPORTED DURING CRUISE. REPORT ATTACHED; AFTER CUSTOMS CLEARED A/C WALK THRU CABIN NO ODOR PRESENT RNA PACKS FOR 15 MINS STILL NO ODOR PRESENT, POLED 4 CLEARERS PRESENT THEY ALL STATED NO UNUSUAL ODOR NOTICED. ECOR STATES BRIEF EVENT. LEVEL 1 REF FIM 21-20-00810-801A. NO DEFECTS NOTED. A/C OK FOR SVC.

Part: FILTER — ODOR (RECIRCULATION) · airframe 35,771 hrs · 22,989 cycles

FLT # 206, BNA-BOS. WE EXPERICENCED 4 SEPERATE ODOR EVENTS OF AN ACRID SMELL. DURING TAXI OUT IN BOS DURING CLIMB OUT OF BOS TAXI IN BNA AND CLIMBOUT OF BOS THEENTINSITY WAS MILD FOR ALL EVENTS DURATION FO ALL EVENTSWAS APPROXMILITY 2-3 MINUTES DETECTED ONLY ON FLIGHT DECK NO APPART SOURCE ; R&R BOTH RECIRC FILTERS IAW AMM 21-24-02. RAN BOTH ENGINES IAW FIM 21-20-00-810-801-A. COULDNT DUPLICATE SMELL. LOCKED OUT PACK 1 FLOW CONTROL VALVE IAW 21-51-00

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 35,544 hrs · 22,853 cycles

FLT 640, CLE-BOS. AFT MAIN DOOR EMERGENCY EXIT SIGN INOP ; FOUND WIRE BROKEN FROM SPLICE SP0904. TERMINATED NEW CONTACT SOCKET IAW SWPM 20-41-10 AND R/R ELPU #5 IAW AMM 33-50-01. OPS CHECK GOOD. A/C OK FOR SVC.

Part: WEB — CORRODED (FRMS 12-14) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FLOOR STRUCTURE SUPPORT WEB BETWEEN FR12 AND 14 BETWEEN Y=+35 TO Y=+47; (REF TOMX NR 00392) CORROSION BLEND-OUT WAS OUT OF LIMITS. R & R FLOOR STRUCTURE SUPPORT WEB FR12-14 Y=+35 - Y=+47 IAW SRM 51-41-02 PAR 4 & 6, 51-43-02 PAR 4, AND 51-43-04 PAR 5 FIG 2.

Part: SEAT TRACK — CORRODED (FRMS 60-73) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK FR60-73L OUTBD SIDE; (REF TOMX NR 00757) R & R SEAT TRACK FR60-73L OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03.

Part: SEAT TRACK — CORRODED (FRMS 35-42) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK FR35-42L OUTBD SIDE; (REF TOMX NR 00755) R & R SEAT TRACK FR35-42L OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03.

Part: SEAT TRACK — CORRODED (FRMS 74-84) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK OUTBOARD LH BTW FR74-84L; (REF TOMX NR 00758) R & R SEAT TRACK FR74-84L OUTBOARD IAW SRM 51-43-03.

Part: SEAT TRACK — CORRODED (FRMS 23-34) · airframe 35,419 hrs · 22,783 cycles

"DURING HEAVY MAINTENANCE, CORROSION ON LATERAL SEAT TRACK FROM FR 23 TO FRAME 34 RH OUTBD SIDE; BLENDED AREAS ON CROWN TEETH BTW FR 23 TO FR 34 ON RH LATERAL SEAT TRACK OUTBD SIDE MAX DEPTH .026"" THEREFORE IS OUT OF LIMITS PER EMB -190 SRM 53-21-10AD51 PAR 5 TABLE 103. RH LATERAL SEAT TRACK OUTBD SIDE FROM FRAME 23 TO FRAME 34 WAS REPLACED PER EMB -190 SRM 51-41-01 PAR 5 FIG 1 PAR 6 FIG2 . ALL WORK WAS ACCOMPLISHED ON TOMX NRS 00776 , 00750 AND 00625. CLASSIFIED AS MAJOR REPAIR."

Part: SEAT TRACK — CORRODED (FRMS 43-59) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK FR43-59R OUTBOARD SIDE; (REF TOMX NR 00752) R & R SEAT TRACK FR43-59R OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03.

Part: SEAT TRACK — CORRODED (FRMS 23-34) · airframe 35,419 hrs · 22,783 cycles

"DURING HEAVY MAINTENANCE, SEVERAL CORROSION ON LH CENTRAL LONGITUDINAL SEAT TRACK BTW FR 23 AND FR 34 AT CABIN PAX; BLENDED AREAS ON CROWN TEETH BTW FR 23 TO FR 34 ON LH CENTER SEAT TRACK MAX DEPTH .029"" THEREFORE IS OUT OF LIMITS PER EMB -190 SRM 53-21-10AD51 PAR 5 TABLE 103 LH SEAT TRACK FROM FRAME 23 TO FRAME 34 WAS REPLACED PER EMB -190 SRM 51-43-03 PAR 5 AND 6FIG 1 AND SRM 51-43-04 PAR 4 AND 5 FIG 1 . ALL WORK WAS ACCOMPLISHED ON TOMX NRS 294 AND 760. CLASSIFIED AS MAJOR REPAIR."

Part: WEB — CORRODED (FRMS 17-19) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FLOOR STRUCTURE SUPPORT WEB BETWEEN FR17 AND 19 Y=+49; (REF TOMX NR 00393) R & R FLOOR STRUCUTRE SUPPORT WEB FR17-19 AND Y=+49 IAW SRM 51-41-02 PAR 4 & 6, AND SRM 51-43-02 PAR 4 & PAR 5 FIG 2.

Part: SEAT TRACK — CORRODED (FRMS 23-34) · airframe 35,419 hrs · 22,783 cycles

"DURING HEAVY MAINTENANCE, CORROSION: SEAT TRACK FR23-34L OUTBD SIDE; BLENDED AREAS ON CROWN TEETH BTW FR 23 TO FR 34 ON LH LATERAL SEAT TRACK OUTBD SIDE MAX DEPTH .028"" THEREFORE IS OUT OF LIMITS PER EMB -190 SRM 53-21-10AD51 PAR 5 TABLE 103. LH LATERAL SEAT TRACK OUTBD SIDE FROM FRAME 23 TO FRAME 34 WAS REPLACED PER EMB -190 SRM 51-41-01 PAR 5 FIG 1 PAR 6 FIG2 AND SRM 51-43-03. ALL WORK WAS ACCOMPLISHED ON TOMX NRS 00777 , 00754 AND 00624. REF TOMX NR 00777,00754 AND 00624 R &R SEAT TRACK FR 23L-34L OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03. CLASSIFIED AS MAJOR REPAIR."

Part: HINGE FITTING — CRACKED (RUDDER) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CRACK ON HINGE FITTING OF UPER PCU AT RUDDER IN REFERENCE TO TC E190-27-22-01-214-801; (REF TOMX W/O 1614 N/R 00465) R & R RUDDER SURFACE PER EMB-190 AMM 27-21-05-000-801-A AND AMM 27-21-05-400-801-A

Part: SEAT TRACK — CORRODED (FRMS 23-34) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, SEVERAL CORROSION ON RH CENTRAL LONGITUDINAL SEAT TRACK BTW FRAME 23 AND FR 34; SEAT TRACK FROM FR 23 TO FR 34 RH INBD SIDE WAS REPLACED PER EMB -190 SRM 51-43-03 PAR 5 AND 6 FIG 1 AND SRM 51-43-04 PAR 4 AND 5 FIG 1 . ALL WORK ACCOMPLISHED ON TOMX NRS 00293 AND 00759. CLASSIFIED AS MAJOR REPAIR.

Part: WEB — CORRODED (FRM 16) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FLOOR STRUCTURE SUPPORT WEB BETWEEN Y+-13 AND FR16; (REF TOMX NR 00390) FLOOR STRUCTURE SUPPORT WEB Y=-13 AND FR16 WAS REPLACED PER EMB 190 SRM 51-12-01 PAR. 6 AND 51-10-03 PAR. 4A AND SRM 53-10-10 AD/56 PAR 5 TABLE 101, SRM 51-42-02 PAR.4 AND 6 FIG 2.

Part: SEAT TRACK — CORRODED (FRMS 74-84) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK FR74-84R OUTBD SIDE; (REF TOMX NR 00753) R & R SEAT TRACK FR74-84R OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, EMERGENCY LIGHT ON LH SIDE OVERWING EMERGENCY EVACUATION INOP; (REF TOMX 1614 N/R 00205) R & R ELPU IAW EMB-190 AMM 33-50-01-400-801-A OPS CHECKS GOOD

Part: SEAT TRACK — CORRODED (FRMS 43-59) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION: SEAT TRACK FR43-59L OUTBOARD SIDE; (REF TOMX NR 00756) R & R SEAT TRACK FR43-59L OUTBD SIDE IAW SRM 51-41-01 AND 51-43-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON ACCESS PANEL 351GL AT FWD LH & RH SIDE; (REF TOMX NR 00030) REPAIRED PANEL IAW SRM 53-03-64/REPAIR 51P.

Part: SEAT TRACK — CORRODED (FRMS 35-42) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON SEAT TRACK FR35-42R OUTBD SIDE; (REF TOMX NR 00751) R & R SEAT TRACK FR35-42R OUTBOARD IAW SRM 51-41-01 AND 51-43-03.

Part: PLATE — CORRODED (FRM 100 S29L) · corrosion level 2 · airframe 35,419 hrs · 22,783 cycles

"DURING HEAVY MAINTENANCE, CORROSION ON PLATE OF REAR FUSELAGE AT FR 100; UT ON AREA WAS PERFORMED AND FOUND WITH FOLLOWING DIMENSION NOMINAL THICKNESS .063 AND MINIMUM REMAINING THICKNESS .015"" THEREFORE IS OUT OF LIMITS AND WILL BE REPLACED PER EMB -190SRM 51-75-16 PAR 6 PLATE OF REAR FUSELAGE AT FR 100 WAS REPLACED PER EMB -190 SRM 51-41-02,51-42-01, 51-43-01.AND SRM 51-41-01 ALL WORK ACCOMPLISHED UNDER TOMX NR 00524"

Part: FLOOR SUPPORT — CORRODED (FRMS 84-85) · airframe 35,419 hrs · 22,783 cycles

DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT FR84-85 & Y= +12(W2 AREA); (REF TOMX NR 00353) REPAIRED FLOOR STRUCTURE SUPPORT FR84-85 Y=+12 IAW SRM 53-23-10/REPAIR 54P.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 34,602 hrs · 22,278 cycles

FLT 712, ROC-BOS. R2 EMERGENCY EXIT DOOR SIGN WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT POWER UNIT, IAW AMM 33-50-01. OPERATIONS CHECK GOOD AT THIS TIME.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 34,367 hrs · 22,092 cycles

DURING RTS, NOTED EMERGENCY LIGHT SYSTEM TEST FAILS EMER LT BATT (FWD L) FAULT CODE 33500002UT1; R & R FWD LT EMERG. LIGHT POWER UNIT OPS CK GOOD IAW MM 33-50-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,328 hrs · 21,390 cycles

FT # 1011, BOS-ORD. RETURNED TO FIELD. DURING FLT STRONG ODOR OF EXHAUST IN COCKPIT AND FWD PORTION OF GALLEY AND CABIN; REF TROUBLESHOOTING TAB FOR WORK PERFORMED FOR THIS DEFECT ITEM. RAN BLEEDS WITH APU FOR 40 MINUTES WITH NO ODOR. THEN WITH #1 ENG , NO ODOR. #2 BLEED ON MEL. CABIN FILTERS REPLACED IAW AMM 21-42-02. REF AMM 21-24-02, 21-51-00, 71-00-01. MCC REQUESTED CLEARING MDDR 406203 TAT #2. R & R TAT #2 PROBE, SEE DEFECT 2642184 ITEM #2. AIRCRAFT OK FOR SERVICE. AMM REFERENCES 21-24-02, 21-51-00, 71-00-01.

Part: SKIN — CRACKED (LT WING) · airframe 27,537 hrs · 17,247 cycles

DURING HEAVY MAINTENANCE OF THE LT WING, FOUND 2 CRACKS ON LOWER SKIN, SPAR 11, RIB 10. DAMAGE MEASURES 1.880" IN LENGTH. ACCOMPLISHED A REPAIR IAW EC E17-1000-01.

Part: SLIDE — DAMAGED (R2 DOOR) · airframe 27,271 hrs · 17,058 cycles

R2 DOOR SLIDE HAS COME UNSTICHED AND PARTIALY UNRAVELED. R & R THE DOOR SLIDE ASSEMBLY IAW AMM 25-65-01. CHECKED GOOD.

Part: ENGINE — STALLED (NR 2) · airframe 24,830 hrs · 15,323 cycles

DURING CLIMB, THE CREW REPORTED THE NR 2 ENGINE HAD A COMPRESSOR STALL. THE ENGINE WAS SHUT DOWN IAW THE QRH. THE CREW DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. PERFORMED A VISUAL INSPECTION OF THE RT ENGINE. NO DAMAGE NOTED PERFORMED AMM TASK 72-00-00-810-321 AND 72-00-00-200-003. VIBRATIONS VERIFIED TO BE WITHIN LIMITS IAW ENGINE SHUTDOWN THRU CMC INTEROGATION.

Part: BEAM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,728 hrs · 13,134 cycles

AFT PAX DOOR LOWER BEAM HAS CORROSION AT AFT GIRT BAR FLOOR FITTING R & R AFT PAX DOOR LOWER BEAM, SRM 51-41-01; 51-41-02; 51-43-03.

Part: BEAM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,728 hrs · 13,134 cycles

AFT PAX DOOR LOWER BEAM HAS CORROSION AT FWD GIRT BAR FLOOR FITTING R & R FWD PASSENGER DOOR LOWER BEAM SRM 51-41-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,865 hrs · 8,671 cycles

ON MX CHECK, FOUND RT AFT EMERGENCY LIGHT INOP, EXTERIOR. R & R RT AFT EMERGENCY LIGHT REF AMM 33-50-25. OPS CHECK GOOD.

Part: FLOAT VALVE — FAILED (LT WING) · airframe 14,091 hrs · 8,196 cycles

FLT 253, DECLARED EMERGENCY AND RETURNED TO DEPARTURE DUE TO FUEL IMBALANCE MESSAGE. LEFT WING ABOUT 900 LBS MORE THAN RIGHT, FOLLOWED QRH. TOTAL FUEL IN FMS WAS LARGER THAN FUEL ON EICAS. 2000 LBS DIFFERENCE. FOLLOWED QRH, FUEL WAS OBSERVED COMING OUT OF RIGHT WING. REMOVED & REPLACED RT VENT FLOAT VALVE IAW AMM 28-12-05-400-801A. OPS CHECKED GOOD IAW AMM 28-12-05-710-801A.

Part: FADEC — FAILED (NR 1 ENGINE) · airframe 13,531 hrs · 7,876 cycles

FLT 117 JFK-MSY, CREW DECLARED EMERGENCY DUE TO TLA COMP FAIL FOLLOWED SHORTLY AFTER BY ENGINE 1 FAIL. FOLLOWED BY NORMAL SINGLE ENGINE LANDING AT MSY. NO ABNORMAL SIGNS PRIOR TO ENGINE FLAMEOUT ENGINE WINDMILLED THROUGHOUT LANDING ROLL AUTO AND MANUAL RELIGHT WERE UNSUCCESSFUL. REMOVED AND REPLACED NR 1 ENGINE FADEC REF AMM 73-21-01-04 OPS CHECK GOOD. PERFORMED SUCCESSFUL HIGH POWER ASSURANCE RUN PER EMM 72-00-00-760-118. OK FOR CONTINUED SERVICE AT THIS TIME.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 12,802 hrs · 7,400 cycles

FLT 1052 PIT-JFK, CREW DECLARED EMERGENCY DUE TO HYD 1 EDP FAIL HYD 1 LOW QTY. FOUND NR 1 ENGINE PYLON HYDRAULIC LINE LEAKING THROUGH PIN HOLE FROM CLAMP VIBRATION. PERFORMED PERMASWAGE REPAIR IAW AMM 20-10-03. REMOVED AND REPLACED NR 1 ENG EDP IAW AMM 29-11-01. LEAK CHECK OF EDP AND REPAIR GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 12,111 hrs · 6,952 cycles

FLT 35 JFK-PBI, DURING THE WEEKLY CHECK MAINTENANCE FOUND LEFT FORWARD EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT POWER SUPPLY UNIT IAM AMM 33-50-01-04, OPS NORMAL.

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE) · airframe 11,342 hrs · 6,482 cycles

FLT 1739 JAX-SJU, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO MCO DUE TO EICAS ENGINE 1 FUEL LO PRESS ILLUMINATED ON CLIMB THROUGH 20000. REPLACED NR 1 ENGINE FUEL LOW PRESS SWITCH PER 73-31-01/401. OPS AND LEAK CHECK NORMAL.

Part: LOOP — MALFUNCTIONED (DETECTION SYS) · airframe 9,244 hrs · 5,234 cycles

FLT 746 SJU-MCO, AIRCRAFT DIVERTED TO PBI DUE TO BLEED 2 EICAS MESSAGE. CREW FOLLOWED QRH AND ON DESCENT AT 18,000 FEET THE LIGHT EXTINGUISHED. THE LIGHT CAME BACK AND INTERMITTENT AT 10,000 FEET AND BELOW. ON TROUBLESHOOTING FOUND CHANNEL 1 PYLON LOOP FAULTING. THE TECHNICIAN REMOVED AND REPLACED RT PYLON LEAK DETECTOR LOOP A IAW AMM 36-21-02. OPS AND LEAK CHECK OK. HIGH POWER RUN WAS ACCOMPLISHED AND FOUND OK.

Part: ACM — FAILED (NR 2) · airframe 9,096 hrs · 5,155 cycles

FLT 131 BUF-JFK, BURNT SMELL FROM AFT CABIN ON APPROACH, TURNED OFF NR 2 PACK AND TV AS PRECAUTION. PERFORMED FIM TASK 21-70-00-810-801A FOUND NR 2 PACK ACM TO BE AT FAULT. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW 21-51-05. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,227 hrs · 4,102 cycles

FLT 401 BOS-MSY, DIVERTED TO IAD - FUMES BY ROW 2 DESCRIBE AS "BURING IRON" SMELL, RULED OUT LAPTOP / BATTERIES / PED'S. TURNED OFF TV'S AND DIVERTED TO IAD, FUMES SEEMED TO STOP. PERFORMED A VISUAL INSPECTION ON THE PASSENGER CABIN & E&E BAYS. NO SIGNS OF BURNING ODOR, ACFT OK TO CONTINUE SERVICE IRW FIM 21-20-00810-801A.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 5,418 hrs · 3,050 cycles

FLT JB 1245 BOS-CLT "SLAT FAIL" CAS MESSAGE ON APPROACH TO CLT WHEN SELECTING FLAPS. RAN QRH PROCEDURES FLAPS/SLATS OPERATED NORMALLY, LANDED UNEVENTFULLY. CLT MX RESET SLAT SYS PER AMM FIM 27-50-00-810-803A, FAULT CLEARED, OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 03/24/2010 FLT JB916 ORD-JFK "SLAT FAIL" ON APPROACH TO JFK, PERFORMED QRH PROCEDURE OPERATED NORMAL AFTER QRH LANDED UNEVENTFUL. JFK MX INTERROGATED CMC FOUND FAULT CODE 27811021ACE TROUBLESHOT IAW AMM FIM TASK 27-81-00-810-802A FOUND RT WING SLAT ACTUATOR NR 7 TORQUE LIMITER TRIPPED. REMOVED AND REPLACED RT NR 7 SLAT ACTUATOR IAW AMM 27-81-01, OPS CHECK NORMAL, OK FOR SERVICE.

Part: MODULE — FAILED · airframe 4,300 hrs · 2,421 cycles

FLT 658 - MCO-ROC DIVERTED TO IAD DUE TO AVNX MAU 3A FAIL EICAS MESSAGE IN FLIGHT. AIRCRAFT LANDED SAFELY. MX REMOVED AND REPLACED NIC-PROC 5 MODULE IN MAU 3A PER AMM 31-41-04. OPS CHECK NORMAL, OK FOR SERVICE.