N602AE

Part: INVERTER — INOPERATIVE (EXTERIOR LIGHT) · airframe 49,777 hrs · 43,767 cycles

DISCREPANCY: INTERIOR REAR EXIT LOCATOR LIGHT INOPERABLE (EMERGENCY LIGHT). ACTION TAKEN: REMOVED HEADLINER PANEL IN REF TO AMM TASK 25-22-04-000-802-A. IN ORDER TO GET ACCESS TO EMERGENCY LIGHT INVERTERS. DISCONNECTED AND RECONNECTED NR 5 EMERGENCY LIGHT INVERTER AND TURNED ON EMERGENCY LIGHT AND FOUND ALL LIGHT TO BE WORKING CORRECTLY. REINSTALLED HEADLINER PANEL, IN REF TO AMM TASK 25-22-04-400-A. PERFORMED OPERATIONS CHECK 33-50-00-700-801-A. OPERATIONS CHECK GOOD. OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 49,145 hrs · 43,017 cycles

SPOILER FAILED MSG IN FLT WITH SPOILERS DOWN MSG CLEARED W/GEAR DOWN. MSG RETURNED WITH LANDING AND SPOILERS DEPLOYED. CMC MSG,S GND SPOILER ENG FAULT AND GROUND SPOILER WHL SPD CKT FAULT....FIX: R&RD SCU IAW EMB 145 AMM 27-63-02. OPS CHECK SAT. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 A/C PACK) · airframe 48,616 hrs · 42,420 cycles

PACK 1 OVRHEAT MESSAGE URING T/O ROLL.#2 PACK ON MEL....FIX: GROUND RAN A/C WITH BOTH ENGINES,OPS CK #1 PACK IAW EMB 145 21-51-00 OPS CK GOOD NO OBVIOUS DEFECTS NOTED,OK FOR SERVICE

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,557 hrs · 42,344 cycles

ROW 12 CEILING EMERGENCY EXI LIGHT INOP....FIX: R&RD #4 INVERTER IAW 33-50-11-000-801-A AND 33-50-11-400-801-A. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (SEAT 12) · airframe 48,469 hrs · 42,250 cycles

EMERGENCY CEILING LIGHT BY SEAT 12 WILL NOT TURN ON....FIX: REMOVED CEILING PNL AT ROW 12INSTALLED NEW LIGHT, REINSTALLED CEILING PNL IAW AMM33-50-15. OPS CHECK GOOD. OK FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,259 hrs · 42,017 cycles

NDIS 602 33-50 0024580 14SEP19 SBY CLOSE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 6 & 7 IS INOP. FACT 14SEP19 14:42 SBY. R&R EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 6 & 7 IAW AMM 33-50-12. P/N ON LIGHT STRIP 1013194 P/N OFF LIGHT STRIP 1013194.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,778 hrs · 36,218 cycles

AFT PORTION OF OVER-WING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE....FIX:FOUND BROKEN WIRE W200-8508-20,CRIMPED NEW CONTACT AND CONNECTOR IAW 20-21-00. INSTALLED PANEL OPS CHECK GOOD

Part: FAN — FAILED (RECIRCULATION) · airframe 47,306 hrs · 40,910 cycles

PDIS 602 05-50 1874192 11FEB19 PGV CLOSE ELECTRICAL SMELL/ODOR COMING FROM FLIGHT DECK CAPTAINS SIDE. FACT 11FEB19 00:30 PGV INSP SMELL IN FLT DECK FOUND NO OBVIOUS DEFECTS AT SUSPECT AREA OF FWD GLARESHILED. INSPECTED SUSPECT AREA PER FIM 21-20-00-810-801-A AND PERFORMED GROUND RUN W CREW W NO NOTED DEFECTS. PDIS 602 21-25 1874193 11FEB19 PGV ASSGN DURING T/S OF SMELL IN FLIGHT DECK. FOUND RECIRC FAN 2 FAIL MSG ON CMC. MX P/C C/B CABIN RECIRC PER MEL MX PROCEDURE. MEL 11FEB19 15:52 PGV C04214 21-4-1 RECIRC FANS ELCTRO MECH STANDBY INST DFRL 13FEB19 08:46 SBY CCN 1210078

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 47,276 hrs · 40,874 cycles

PDIS 602 30-10 1874141 06FEB19 SYR CLOSE ICE COND-A/ICE MESSAGE APPEARED DURING TAKEOFF ROLL. MSG EXTINGUISHED FACT 06FEB19 16:56 SYR PERFORMED ELECTRICAL RESET. OPS CHECKED A/ICE SYS IA W AMM 30-00-00-700-803-A OPS CHECK NORMAL OK FOR SER

Part: TERMINAL — NOT SEATED (EMERGENCY LIGHT) · airframe 47,210 hrs · 40,796 cycles

DISCREPANCY: EMERGENCY FLOOR LIGHTS ROW 2 AND 3 INOP. CORRECTIVE ACTION: RESEATED TERMINAL ENDS ON EMERG. FLOOR LIGHT ROW 2, RESECURED LIGHT STRIP WITH RETAINED HARDWARE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,116 hrs · 40,684 cycles

DIS 602 33-51 0018450 31DEC18 SBY CLOSE LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. FACT 31DEC18 10:52 SBY R&R BOTH LT AND RT OVER WING EMERGENCY EXIT LIGHT LAMPS IAW AMM 33-50-10, NO FIX R&R NR 3 BATTERY AND POWER SUPPLY IAW AMM 33-50-04-04, PART INSTALLED/REMOVED BULB 1317 PART INSTALLED/REMOVED BATT & POWER SUPPLY 1330408 PART INSTALLED S/N C06887 PART REMOVED S/N 24491.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 47,056 hrs · 40,614 cycles

MDIS 602 33-51 1978093 16DEC18 CLT ASSGN EMERGENCY LIGHT AT AFT GALLEY WALL HAS BROKEN WIRE A T SPLICE. 26390 00 DS HISTORY: . DFRL 16DEC18 13:40 CLT INSTALLED TEMP SPLICE AT LT ON AFT GALLEY WALL. OP S CK GOOD. PLACED ON 100 FH DMT. DNAA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,053 hrs · 40,609 cycles

MDIS 602 33-51 1978082 15DEC18 CLT CLOSE L/H AND R/H EXTERIOR OVERWING EMERGENCY LIGHTS INOP FACT 16DEC18 11:56 CLT R\R EMERGENCY BATTERY PACK AT ROW 15A OPS CHECK GOOD , OK FOR SERVICE. CLEAR MEL.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 46,739 hrs · 40,244 cycles

AT 400 FEET AGL AT TAKEOFF YD FAILED AND RUD SYS 1/2 INOP CAUTION MSG PRESENTED. RAN QRH WHEN RUD SYS 2 DESELECTED RUD SYS 1 CAME BACK ON LINE. YD RE-ENGAGE AND IT STAYED ONLINE. T/S IN REF TO FIM 27-22-00-810-804-A FOUND RUD SYS 2 PRESS SW FAIL. R&R RUD SYSTEM 2 PRESSURE SWITCH IN REF TO AMM 27-23-04. OP CK AND LK CK GOOD OK FOR SERVICE.

Part: PROCESSOR — MALFUNCTIONED (TCAS) · airframe 46,587 hrs · 40,067 cycles

ATC REPORTS BOTH TRANSPONDERS FAIL INFLIGHT -WILL NOT IDENT-. R&R TCAS PROCESSOR IAW AMM 34-43-01. OPS CHECK IAW AMM 34-43-00 REQUIRES FUNCTIONAL CHECK.

Part: DOOR — MISSING (APU BAY) · airframe 46,262 hrs · 39,695 cycles

RIGHT AFT FUSELAGE IS MISSING APU ACCESS DOOR AFTER FLIGHT.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 45,954 hrs · 39,350 cycles

DURING FLIGHT, NOTICED A RAPID DEPETION OF THE NR 1 HYD SYSTEM QUANTITY WITH AN EICAS MESSAGE. R & R GROUND SPOILER ACTUATOR IAW AMM 27-62-01-400-801-A. REPLENISHED TH EHYDRAULIC SYSTEM.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 45,918 hrs · 39,305 cycles

NR 2 HIGH STAGE VALVE FAILURE DURING TAKE OFF AT ABOUT 20 KNOTS. R&R NR 2 HIGH STAGE VALVE IAW AMM 36-11-02. OPS GOOD AT THIS TIME. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 45,887 hrs · 39,272 cycles

SEAT 12A EXIT SIGN INOPERATIVE. CLEANED CONNECTORS AND SECURED IAW AMM 33-50-14-0001/400-801-A. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 45,832 hrs · 39,202 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED THE LIGHT WIRES IAW 20-21-00.

Part: LIGHT — UNKNOWN (SEAT 1A) · airframe 48,769 hrs · 39,136 cycles

FLOOR EMERGENCY LIGHT STRIP, SEAT 1A INOPERATIVE. PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHT. OPS CHECKED NORMAL. OK FOR SERVICE. E.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,126 hrs · 38,444 cycles

LEFT AFT INTERIOR OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. R & R THE INVERTER IAW AMM 33-50-11-000/400-801A. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 45,030 hrs · 38,352 cycles

EMERGENCY LIGHT AT ROW 12A, AFT WINDOW DOES NOT ILLUMINATE. REMOVED THE EMERGENCY LIGHT. CLEANED THE CONTACTORS, AND INSTALLED THE LIGHT. OK FOR SERVICE. OPS CHECKED SATISFACTORY IAW AMM 33-50-14-000/400-801A.

Part: RELAY — INOPERATIVE (NR 3 PITOT) · airframe 44,446 hrs · 37,735 cycles

PITOT NR 3 INOPERATIVE CAUTION EICAS MESSAGE. R & R THE RELAYS K0058 & K0060 IAW TASK 30-31-00-810-803-A. OPS GOOD.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 44,052 hrs · 37,296 cycles

CARGO DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.

Part: STRINGER — CHAFED (FRAMES 52-53) · airframe 44,052 hrs · 37,296 cycles

STRINGER 19R BETWEEN FRAMES 52-53 CHAFED. REPAIRED THE STRINGER IAW SRM 53-24-02.

Part: FRAME — BROKEN (FRM 10) · airframe 44,052 hrs · 37,296 cycles

FRAME 10 UNDER COPILOTS WINDOW IS BROKEN. REMOVE AND REPLACED THE FRAME IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 44,052 hrs · 37,296 cycles

CARGO DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT — CORRODED · airframe 44,052 hrs · 37,296 cycles

TOILET WASTE VALVE SUPPORT IS CORRODED. PERFORMED PERMANENT REPAIR INSTALLED DOUBLER IAW ERS-EM-53MR-2471.

Part: SUPPORT — CORRODED · airframe 44,052 hrs · 37,296 cycles

TOILET WASTE VALVE SUPPORT IS CORRODED. REPAIRED THE SUPPORT AND INSTALLED A DOUBLER IAW ERS-EM-53MR-2471.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 44,052 hrs · 37,296 cycles

FRAME 65 SHEAR TIE CORRODED. INSTALLED A REPAIR IAW SRM 53-31-04.

Part: FRAME — CORRODED (FRM 25) · airframe 44,052 hrs · 37,296 cycles

FRAME 25 UPPER FLANGE CRACKED BETWEEN STRINGERS 15 - 16R. REPAIRED THE FRAME IAW SRM 53-00-04 AND ERS-EM-53MR-2472.

Part: FRAME — CORRODED (FRM 65) · airframe 44,052 hrs · 37,296 cycles

FRAME 65 CORRODED UNDER FWD LOWER CARGO DOOR STRIKER PLATE. REPAIRED THE FRAME IAW ERS-EM-53MR-2466

Part: YOKE — CRACKED (RT ENGINE) · airframe 44,052 hrs · 37,296 cycles

RIGHT ENGINE PYLON FWD LOWER YOKE CRACKED. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386

Part: FRAME — CRACKED (FRM 25) · airframe 44,052 hrs · 37,296 cycles

FRAME 25 UPPER FLANGE CRACKED BETWEEN 15R AND 16R. REPAIRED THE FRAME IAW ERS-EM-53MR-2472.

Part: FRAME — CORRODED (FRM 65) · airframe 44,052 hrs · 37,296 cycles

FRAME 65 CORRODED UNDER FWD LOWER CARGO DOOR STRIKER PLATE. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM 53-31-04 ITEM 4E AND ERS-EM-53MR-2466

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 44,052 hrs · 37,296 cycles

SERVICE DOOR CUTOUT AFT FRAME IS CORRODED BEHIND LOWER PLASTIC GUIDE. REPAIRED IAW ERS-EM-53MR-2479

Part: YOKE — CRACKED (RT ENGINE) · airframe 44,052 hrs · 37,296 cycles

RIGHT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 44,052 hrs · 37,296 cycles

LEFT NR 7 AND 9 EMERGENCY LIGHT STRIPS HAD BROKEN WIRES. REPLACED THE LIGHT STRIPS IAW AMM 33-50-12

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,052 hrs · 37,296 cycles

NR 4 EMERGENCY LIGHT BATTERY IS DEAD. R & R THE BATTERY IAW AMM 33-50-04.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 43,898 hrs · 37,145 cycles

AUTO PRESSURIZATION SYSTEM FAILED ELEVATION DIGITS DISSAPEARED AND CABIN ALTITUDE RAPIDLY DESCENDED TO DASHES ON CABIN ALTITUDE. AUTO PRESSURE DEFERRED PER MEL 21-17 SECTION 4 M PROCEDUES C/W. REMOVED AND REPLACED MANUAL PRESSURE CONTROL RECEPTACLE IAW EMB MM 21-31-02 OPS CHECK GOOD IAW MM 21-30-00 PERFORMED OPC PRESURUZATION CONTROL IN AUTO/MANUAL MODE IAW AMM 21-31-00.OPC GOOD MEL 21-17 RESTORED.OUTFLOW VALVE SECTION 4 PROCEDURE REACTIVATED.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 43,556 hrs · 36,813 cycles

NR 1 ENGINE N1 ROLL BACK UNCOMMANDED 90-60% FOR A FEW SECONDS, CAUTION YAW TO LEFT N2 RECOVERED 5 SECONDS LATER AT FL 320. LANDED NORMALLY. NO WEATHER, NO EXTEME WINDS, DIVERTED AND LANDED NORMALLY. PERFORMED FDR DOWNLOAD IAW W/C 31-700-05. R & R FADEC 1A IAW AMM 73-22-01. FADEC INSPECTION GOOD AND NO FURTHER FAULTS FOUND.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,422 hrs · 36,677 cycles

MAIN DOOR EXIT LIGHT INOPERATIVE. R & R MAIN DOOR EXIT LIGHT BULB IAW 33-50-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,696 hrs · 35,984 cycles

LEFT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LT OVERWING EXTERIOR EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,143 hrs · 35,520 cycles

LEFT AFT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LT AFT OVERWING EXTERIOR EMER LIGHT IAW AMM 33-50-10. TESTED SATISFACTORY.

Part: PIN — BROKEN (NLG PROX SWITCH) · airframe 41,796 hrs · 35,229 cycles

DURING FLIGHT, GOT LANDING & AIR GND FAIL 4 TIMES DURING CRUISE & DECENT. ALSO 2 TIMES ENG 1 - 2 REV DISAGREE. BOTH INTERMITTENT. DECLARED EMER LANDED WITHOUT FURTHER INCIDENT. FOUND PIN A BROKEN ON NOSE GEAR AIR & GND PROX SWITCH, R & R;. OPERATIONS CHECKED GOOD IAW AMM CH 32-63-02. CMC MSGS E-2 & E-1 REV AIR GND LOG FAIL. 4X LG AIR & GND PROX SWITCH FAIL. 4X AIR & GND LGEU FAIL.

Part: WIRE — DAMAGED (CABIN) · airframe 41,501 hrs · 34,929 cycles

CENTER AISLE FLOOR PROXIMITY LIGHT STRIP AT SEAT 18A, WIRES DAMAGED. R & R CTR AISLE PROXIMITY LIGHT STRIP AT SEAT 18A IAW AMM 33-50-12.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,501 hrs · 34,929 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R AFT CABIN EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 41,398 hrs · 34,843 cycles

PTRIM MAIN INOPERATIVE ON EICAS, AFTER TAKEOFF, DURING CLIMB OUT AT ABOUT 3000 FT. TRANSFERRED TO NRWC 602-DFW-02484. RESET HORIZONTAL STAB SYS & PERFORMED OPERATIONAL CHECK OF HORIZONTAL STABILIZER IAW AMM 27-40-00. OPERATIONS CHECKED GOOD AT THIS TIME. R & R THE HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 41,329 hrs · 34,781 cycles

PTRIM MAIN INOPERATIVE, MSG ON EICAS IN FLIGHT, AT APPROX 2500 MSL. FLIGHT CONTROL FELT JAMMED, OCCURRED ON TAKEOFF CLIMB OUT. TRANSFERRED TO NRWC 602-DFW-02455. R & R HORIZONTAL STAB ACTUATOR IAW AMM 27-40-02. NO DEFECTS NOTED. REFERENCE NRWC 602-DFW-02455

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 40,822 hrs · 34,299 cycles

AFTER TAKEOFF, PTRIM MAIN INOPERATIVE. PERFORMED PITCH TRIM OPERATIONAL TEST IAW AMM 27-40-00. OPERATIONS CHECKED OK.

Part: CLAMP — FAILED (BLEED AIR SYS) · airframe 40,158 hrs · 33,711 cycles

DURING PNEUMATIC ICE TEST IN AIR BLD 2 LEAK WITH ASSOCIATED LOUD BANG HEARD IN COCKPIT & IN CABIN. FOUND RT BLEED DUCT JOINT 9 SEPARATED. INSTALLED NEW O RINGS & CLAMP IAW AMM 36-11-00. LEAK & OPERATIONS CHECKED GOOD IAW AMM 36-00-00.

Part: FRAME — NICKED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

CARGO BAY RT FRAME 68 HAS A NICK NEAR STRINGER 11R. COMPLIED WITH REPAIR FOR THE RT FRAME 68 NICK IAW ERS-EM-53MR-928.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

UPPER FRAME 78 RT SIDE VERTICAL STAB HAS 1 RIVET WITH SKIN CRACK. UPPER FRAME 77 RT SIDE VERTICAL STAB HAS 1 RIVET WITH SKIN CRACK. UPPER FRAME 78 SKIN CRACK REPAIRED AS REQUIRED IAW ERS -EM-5300-898 & UPPER FRAME 77 SKIN CRACK REPAIRED AS REQUIRED IAW ERS-EM-5300-898.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

UPPER FRAME 77 LT SIDE OF VERTICAL STAB HAS TWO RIVETS WITH SKIN CRACKS. UPPER FRAME 78 LT SIDE VERTICAL STAB HAS ONE RIVET WITH SKIN CRACK. REPAIRED SKIN AT FRAME 77 TWO EACH RIVETS HOLES IAW ERS EM-5300-912 & FABRICATED ONE EACH REPAIR BUSHING FOR UPPER FRAME 78 IAW ERS-EM-5300-911.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 39,734 hrs · 33,246 cycles

DWMS NRWC E417504 STRINGER 19 R BETWEEN FRAME 52 - 53 DAMAGED. REPAIRED IAW ERS EM 53MR 895.

Part: YOKE — CRACKED (LT ENGINE) · airframe 39,735 hrs · 33,246 cycles

LT ENG FWD YOKE CRACKED IN LOWER FWD RADIUS. REPAIR OF LT ENG FWD LOWER YOKE WAS COMPLETED IAW ERS-EM-54MR-268.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

RIGHT OMEGA BEAM ATTACH ANGLE CRACKED BETWEEN FRAMES 47 - 48. R & R DAMAGED RT OMEGA BEAM ATTACH ANGLE IAW SRM 53-23-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

LEFT OMEGA BEAM AT FRAME 54 CROSS MEMBER FOUND TO BE CORRODED. REPAIRED LT OMEGA BEAM AT FRAME 54 IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

CENTER OMEGA BEAM HAS EVIDENCE OF CORROSION AT FRAME 58. REPAIRED CTR OMEGA BEAM IAW EO EM-53 R-1518 PART B.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

CABIN RT OTBD SIDE SUPPORT FOR THE CTR OMEGA BETWEEN FRAMES 45 - 46 HAS EVIDENCE OF CORROSION. FOUND TO BE CRACKED. R & R CORRODED RT OTBD SIDE SUPPORT FOR THE CTR OMEGA BEAM IAW SRM 53-23-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

LEFT OMEGA BEAM HAS EVIDENCE OF CORROSION AT FRAME 49. COMPLIED WITH REPAIR IAW ERS-EM-53MR?925.

Part: SPAR — CRACKED (LT WING) · airframe 39,735 hrs · 33,246 cycles

LEFT WING SPAR NR 3 CRACKED WHERE WIRE BUNDLE PASSES THRU SPAR, JUST INBD OF THE GND SPOILER ACTUATOR. COMPLIED WITH SPAR 3 REPAIR IAW ERS-EM-57MR-325.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

FUSELAGE EXTERIOR SKIN HAS A 1 1/8 INCH CRACK BY THE AFT UPPER CORNER OF CAPTAINS DV WINDOW CUT OUT. COMPLIED WITH REPAIR EXTERIOR SKIN AFT UPPER CORNER CAPTAIN'S DV WINDOWS CUT OUT IAW ERS-EM-53MR-872.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,735 hrs · 33,246 cycles

LEFT OMEGA BEAM AT CROSS MEMBER NEAR FRAME 38 IS CORRODED. LEFT OMEGA BEAM AT FRAME 38 REPAIRED IAW SRM 53-00-10.

Part: ROLLER — DIRTY (CABI DOOR) · airframe 39,440 hrs · 32,917 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE & OPEN. CLEANED & LUBED DOOR ROLLERS NO DEFECT NOTED IAW AMM 53-21-02.

Part: HANDLE — LACK OF LUBE (PARKING BRAKE) · airframe 39,426 hrs · 32,897 cycles

PARKING BRAKE STICKING & BINDING UNABLE TO ENGAGE FULLY AT TIMES. LUBED PARKING BRAKE HANDLE IAW AMM 32-44-10. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: UPLOCK — FAILED (RT MLG) · airframe 39,342 hrs · 32,817 cycles

DURING TAKEOFF, ON GEAR RETRACTION A LOUD NOISE STARTED FROM THE FRONT OF THE ACFT. FEW SECONDS LATER ON EICAS GEAR INDICATION OF THE RT MAIN GEAR CYCLED BETWEEN UP INDICATION & TRANSIT INDICATION CONTINUOUSLY. CAUTION MSG DAU 1 WARN MISCOMP APPEARED ON EICAS, IT WILL STAY ON FOR A FEW SECONDS & THEN CLEAR ITSELF, COMING BACK EVERY 30 SECONDS. ALL ALERTS & MSGS WENT AWAY. R & R RT MLG UPLOCK BOX IAW AMM 32-33-10. GEAR NOW OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 39,137 hrs · 32,662 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,923 hrs · 32,503 cycles

HAIL FWD FUSELAGE I HAS TWO DENTS 27 & 33, OUT OF LIMITS PN L 120-41320-055. TWO DENTS 27 & 33 FWD FUSELAGE I PN L 120-41320-055 ARE ACCEPTED AS IS IAW ERS-5300-549.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL RT ELEVATOR INBD LE HAS TWO DENTS 201 & 202, OUT OF LIMITS ON SKIN PANEL PENDING DISPOSITION. DENTS 201 & 202 ON RT ELEVATOR INBD LE HAS BEEN FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5500-117.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 38,923 hrs · 32,503 cycles

HAIL REAR FUSELAGE I HAS ONE DENT NR 2, OUT OF LIMITS ON SKIN PANEL, PENDING DISPOSITION PN 145-22228-005. DENT NR 2 REAR FUSELAGE I ON SKIN PANEL IS ACCEPTED AS IS IAW ERS-5300-549.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,923 hrs · 32,503 cycles

HAIL REWORK OR REPAIR 2 DENTS, DENTS 381 & 317 ON CTR FUSELAGE II. THE OTHER 5 DENTS 325. 326. 329. 336 & 339 ARE OUT OF LIMITS PENDING DISPOSITION PN 145-33761-003. REWORKED DENTS 381 & 317 TO WITHIN LIMITS IAW EO EM-5100-064 PART C & DENTS 325, 326, 329, 336 & 339 WERE ACCEPTED AS IS IAW ERS-EM-5300-549.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL LT ELEVATOR INBD LE HAS ONE DENT, NR 1 OUT OF LIMITS, PENDING DISPOSITION. DENT NR 1 ON LT ELEVATOR LE HAS BEEN ACCEPTED AS IS IAW ERS-EM-5500-117.

Part: SKIN PANEL — DENTED (RT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL RT ELEVATOR TIP INBD LE HAS ONE DENT NR 29, OUT OF LIMITS ON SKIN PANEL PENDING DISPOSITION PN 45-30807-004. DENT NR 29 ON RT ELEVATOR TIP INBD LE HAS BEEN ACCEPTED AS IS IAW ERS-EM-5500-117.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,923 hrs · 32,503 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE 1. R & R RT CTR FUSELAGE 1 IAW SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,923 hrs · 32,503 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE 1. R & R LT CTR FUSELAGE 1 IAW SRM 51-40-02.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 38,923 hrs · 32,503 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACED LT STABILIZER SKIN. R & R LT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR SKIN TIP. R & R RT ELEVATOR SKIN TIP IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 38,923 hrs · 32,503 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE RT STABILIZER SKIN. R & R RT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,923 hrs · 32,503 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02 & ETN-EM-55-073, ERS-EM-5500-109.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 38,705 hrs · 32,311 cycles

MAIN DOOR HANDLE GRIP BROKEN. INSTALLED NEW MAIN DOOR ASSIST HANDLE IAW AMM 25-23-04.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 38,547 hrs · 32,193 cycles

ACFT MAIN ENTRY DOOR HARD TO OPEN, HANDLE HARD TO MOVE FULLY UP. LUBED MAIN DOOR IAW AMM 52-18-00.

Part: PITOT SYSTEM — CONTAMINATED · airframe 38,423 hrs · 32,085 cycles

ON DECENT IN IMC CONDITIONS, FIRST OFFICER'S IAS BECAME INVALID, DROPPING TO APPROX 140 KTS, CAPTAIN'S & STBY WERE NORMAL. AFTER FURTHER DECENT FIRST OFFICER'S IAS STARED WORKING NORMALLY & CAPTAIN'S IAS BECAME UNRELIABLE DROPPING TO APPROX THE BOTTOM OF THE SCALE. AFTER A FEW MINUTES & FURTHER DECENT ALL IAS INDICATIONS RETURNED TO NORMAL. DRAINED FAIR AMOUNT WATER FROM CAPTAIN`S SIDE, LOTS OF WATER FROM FIRST OFFICER`S SIDE VIA QUICK DISCONNECTS. DID DUAL PITOT STATIC SYS LEAK CHECKS IAW AMM 34-13-00, ALL CHECKS WERE GOOD. BOTH ADC'S OPS CHECKED GOOD IAW 34-15-00. BOTH ADC'S & PITOT STATIC SYS ARE RVSM ELIGIBLE .

Part: PANEL — CRACKED (COCKPIT) · airframe 38,364 hrs · 32,039 cycles

PILOT SIDE CEILING PANEL CRACKED. REPAIRED CRACKS IAW ETN GN-20-023R3.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 38,363 hrs · 32,038 cycles

PRESS LEAK, RUSHING AIR, AT TOP WINDOW AREA ON CAPTAIN`S SIDE. REPAIRED DAMAGE IN ACCORDANCE WITH AEA EO EM-5300-2232 AND ERS-EM-5300-326.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 38,294 hrs · 31,991 cycles

CAPTAIN'S FLASHLIGHT WILL NOT ILLUMINATE. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 38,136 hrs · 31,866 cycles

FORWARD FLIGHT ATTENDANT`S FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53 AUTH 020570-C. COMPLIED WITH THE MEL PROCEDURES.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 37,717 hrs · 31,526 cycles

FLIGHT 3135 NR 1 HYD QTY LOW. 1 HYD QTY AMBER INDICATION AOM 1 PRQC COMPLETE. RETURNED TO DFW & DECLARED EMERGENCY & LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN-EM-29-023, SEE ITEM NR 3 & 4 OF THIS PAGE & ITEM NR 1 AML PG 3414476 FOR FINAL CORRECTIVE ACTION. INSTALLED NEW HYD LINE IAW EMB AMM 20-10-03. LEAK CHECKED GOOD IAW AMM 27-23-04 & OPERATIONS CHECKED GOOD IAW EMB AMM 27-23-00.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 37,639 hrs · 31,464 cycles

AFT CABIN EMERGENCY FLASHLIGHT DIM. R & R AFT CABIN EMERGENCY FLASHLIGHT IAW 145 AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (ENTRY DOOR) · airframe 37,521 hrs · 31,361 cycles

MAIN ENTRY DOOR HARD TO OPEN. C/A SERVICED MAIN CABIN DOOR ROLLERS IAW EMB 145 AMM 53-21-02. NO FURTHER DEFECTS NOTED.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 37,082 hrs · 31,019 cycles

MAIN CABIN ENTRY DOOR IS HARD TO OPEN. F/O FOUND IT HARD TO OPEN ALSO. PERFORMED LUBRICATION ON ROLLERS AND ACTUATING AND LOCKING MECHANISM ON MAIN DOOR IAW AMM 52-11-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,075 hrs · 31,013 cycles

FLASHLIGHT CRADLE ABOVE F/A SEAT IS BROKEN. R & R FLASHLIGHT ASSEMBLY ABOVE F/A SEAT IAW AMM 33-50-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,670 hrs · 30,682 cycles

MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,323 hrs · 30,400 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE MAIN CABIN DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 36,296 hrs · 30,375 cycles

THE CREW REPORTED, THE LT SIDE EMERGENCY LIGHT WAS UP-SIDE DOWN. THE ACFT WAS REMOVED FROM SERVICE. REPOSITIONED LT SIDE EMERGENCY LIGHT ASSY IAW AMM 33-50-15. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 35,939 hrs · 30,076 cycles

ON FLIGHT 3324 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS ON MAIN CABIN DOOR IAW AMM 53-21-02. THE OPERATIONAL CHECKS WERE GOOD AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — FAULTY (CABIN DOOR) · airframe 35,911 hrs · 30,054 cycles

ON FLIGHT 2964 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD UPPER ROLLER ON PASSENGER DOOR FRAME IAW EMB 145 AMM 53-21-02. PERFORMED OPERATIONAL CHECK IAW EMB 145 AMM 52-10-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND RIGHT WING RIB 5 TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIB 5 IAW EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND FUSELAGE SKIN HAS 3 CRACKS AT FRAME 75 STRINGER 1 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 75 AT STRINGER 1L IAW EO EM-53MR-2099. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRUNNION — CRACKED (LT WING) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND THE LEFT MAIN LANDING GEAR TRUNNION HAS A DEFECT/CRACK ON OUTBOARD LOWER GEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR TRUNNION IAW EO EM57MR-678R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 35,872 hrs · 30,023 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING SKIN AT SPOILER HINGE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT WING SKIN CRACK AT SPOILER HINGE POINT IAW EM-57MR-661. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND THE FUSELAGE BELLY SKIN CORRODED BETWEEN FRAMES 13 AND 14, STRINGERS 20 LEFT AND 21 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE BELLY BETWEEN FRAMES 13 AND 14 & STRINGERS 20 LEFT AND 21 LEFT IAW EO EM 53MR-2101. LEVEL OF CORROSION NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,872 hrs · 30,023 cycles

DURING MAINTENANCE INSPECTION FOUND STRINGER 21 RIGHT BETWEEN FRAMES 12 AND 13 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COMPLETED IAW EO EM-53MR-2109. LEVEL OF CORROSION NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE FITTING — GOUGED (LT AILERON) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND LEFT AILERON HINGE FITTING NR 2 TO BE GOUGED ON INBOARD BUSHING SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING ASSEMBLY IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 35,872 hrs · 30,023 cycles

DURING HMBV INSPECTION FOUND ADDITIONAL DAMAGE TO THE LEFT WING SKIN AND SPAR 3 DURING REMOVAL OF DOUBLERS AT CENTER GROUND SPOILER ATTACH POINT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT WING SKIN AND SPAR 3 AT CENTER GROUND SPOILER HINGE POINT IAW EO EM 57MR-680 AND ETA 5700-714. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 35,932 hrs · 30,070 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 1 EMERGENCY LIGHTSTRIP HAD DAMAGED WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE LEFT NR 1 EMERGENCY LIGHTSTRIP IAW EMB145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — MISINSTALLED (FLASHLIGHT) · airframe 35,932 hrs · 30,070 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN FLASHLIGHT CHARGER BASE INOPERABLE, IT DID NOT RECHARGE THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. EVALUATED THE FLASHLIGHT CHARGER BASE AND FOUND NOT TO BE INSTALLED IAW AMM. REMOVED AND REINSTALLED CHARGER BASE. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-16-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 35,869 hrs · 30,020 cycles

DURING HMBV INSPECTION FOUND RIGHT WING RIB 5 TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIGHT HAND RIB 5 AS REQUIRED. IAW EO EM-57MR-595R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,869 hrs · 30,020 cycles

FUSELAGE SKIN UNDERNEATH TCAS II ANTENNA BETWEEN FRAMES 10 AND 11 CORRODED. REPAIRED IAW EO EM-53MR-2109.

Part: SKIN — CRACKED (RT WING) · airframe 35,869 hrs · 30,020 cycles

RT WING SKIN AT SPOILER HINGE CRACKED. REPAIRED IAW EO EM-57MR-661.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,869 hrs · 30,020 cycles

FUSELAGE BELLY SKIN CORRODED BETWEEN FRAMES 13 AND 14, STRINGERS 20 AND 21L. REPAIRED SKIN IAW EO-EM-53MR-2101.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,869 hrs · 30,020 cycles

STRINGER 21R BETWEEN FRAMES 12 AND 13 CORRODED. REPAIRED IAW EO EM-53MR-2109.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,869 hrs · 30,020 cycles

STRINGER 21R CORRODED BETWEEN FRAMES 10 AND 11. COMPLETED SPLICE OF STRINGER IAW EO EM-53MR-2109.

Part: SKIN — CRACKED (RT WING) · airframe 35,869 hrs · 30,020 cycles

RT WING SKIN AT SPOILER HINGE CRACKED. REPAIRED IAW EO EM-57MR-661.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 35,490 hrs · 29,739 cycles

ON FLIGHT 3295 THE CREW REPORTED DIFFICULTY OPENING THE MAIN DOOR. IT APPEARED TO CATCH ON THE TOP OF THE LEFT SIDE FACING OUTWARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED FRAME DOOR ROLLERS REF EMB-145 AMM 53-21-02 AND THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — CORRODED (BLEED AIR SYS) · airframe 35,485 hrs · 29,735 cycles

DURING MAINTENANCE INSPECTION FOUND THE HIGH STAGE VALVE PRESSURE SWITCH PINS VERY CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 2 ENGINE HIGH STAGE PRESSURE SWITCH AS PER AMM 36-11-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 35,450 hrs · 29,695 cycles

FOR FLIGHT 2972 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR SEAL IAW EMB-145 AMM 52-11-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DEFECTIVE (CABIN DOOR) · airframe 35,441 hrs · 29,685 cycles

ON FLIGHT 3312 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ROLLER "UPPER" IAW EMB 145 AMM 53-21-02. PERFORMED OPS CHECK IAW EMB 145 AMM 52-10-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,057 hrs · 29,363 cycles

DURING B INSPECTION FOUND THE AFT EMERGENCY LIGHTS ABOVE WINGS BOTH SIDES INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 & 4 EMERGENCY BATTERY AND POWER SUPPLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FADEC — UNSERVICEABLE (RIGHT) · airframe 34,473 hrs · 28,880 cycles

DURING FLIGHT 2822, CREW REPORTED NR 2 ENGINE N1 SURGING IN CRUISE FLIGHT. AFTER LANDING EICAS MESSAGE WAS E1/E2 SHORT DISP/ E2 NO DISP. THE AIRCRAFT WAS REMOVE FROM SERVICE. TROUBLESHOT, REMOVED AND REPLACED RIGHT 2B FADEC IAW EMB 145 AMM 73-22-01. OPS CHECK GOOD ON GROUND IAW EMB 145 AMM 73-22-01. THE AIRCRAFT RETURN TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 34,117 hrs · 28,613 cycles

WHILE PERFORMING INSPECTION IAW MX WC 57-200-34, FOUND A 5" CRACK AT LT WING RIB NR 5, NEXT TO FWD LARGE LIGHTNING HOLE. COMPLIED WITH AEA EO EM-57MR-574.

Part: RIB — CRACKED (LT WING) · airframe 34,117 hrs · 28,613 cycles

FOUND A 5 INCH CRACK AT LT WING RIB NR 5 NEXT TO FWD LARGE LIGHTNING HOLE. COMPLIED WITH AEA EO EM-57MR-574. MAJOR REPAIR

Part: SENSOR — INOPERATIVE (TEMP) · airframe 33,610 hrs · 28,206 cycles

FLIGHT 2864, THE CREW REPORTED AFTER STARTING APU & WAITING 3 MINUTES SELECTED PACK 1 & 2 ON THEY NOTICED A BURNING ODOR THROUGHOUT AIRCRAFT. FOUND COCKPIT TEMPERATURE CONTROL INOPERATIVE. REMOVED AND REPLACED THE COCKPIT AMBIENT TEMPERATURE SENSOR IAW EMB AMM 21-60-02. THE OPERATIONAL CHECK WAS GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,426 hrs · 27,356 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — LOOSE (COCKPIT) · airframe 32,385 hrs · 27,332 cycles

ON FLIGHT 3374 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER DOES NOT SECURE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,008 hrs · 27,036 cycles

ON FLIGHT 3516 THE CREW REPORTED AN OIL SMELL COMING FROM PACKS IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE GROUND RUN IAW AMM CHPT 71=00=01 AND OPERATIONAL CHECK OF AIR DISTRIBUTION IAW AMM 21-10-00. NO OIL SMELL OR HAZE NOTED DURING GROUND RUN. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELBOW — DAMAGED (HYDRAULIC SYS) · airframe 31,484 hrs · 26,616 cycles

ON FLIGHT 4105 DURING CRUISE THE CREW REPORTED A LOW HYDRAULIC QUANTITY. THE CREW NOTICED A SIGNIFICANT DROP IN HYDRAULIC QUANTITY DURING FLIGHT. THE CREW ELECTED TO DIVERT TO CVG WITH QUANTITY ALMOST AT ZERO. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED HYDRAULIC TUBE ELBOW PN 145-33601-433. THE LEAK AND PRESSURE CHECK WAS GOOD IAW EMB AMM 20-10-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (LT MLG ACTUATOR) · airframe 31,460 hrs · 26,596 cycles

ON FLIGHT 3526 THE CREW REPORTED THAT AFTER TAKEOFF THE HYDRAULIC SYSTEM 1 FAILED. THE HYDRAULIC PRESSURE INDICATION DID NOT FALL. THE CREW ELECTED TO DIVERT TO PNS AND LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED O-RING ON VALVE BODY ASSEMBLY ON THE LEFT MAIN GEAR ACTUATOR IAW ELEB CMM 32-33-08. NO LEAKS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 31,205 hrs · 26,383 cycles

DURING MANTENANCE BASE VISIT FOUND FRAME 69 HAS MIS-DRILLED HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 69 IAW EO EM-53MR-1255. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,205 hrs · 26,383 cycles

DURING MANTENANCE BASE VISIT FOUND SCRATCHES AND DENTS ON THE RIGHT CENTER FUSELAGE THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AREA WITH SKIN DOUBLER IAW EO EM-53MR-1527. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (NLG WW) · airframe 31,205 hrs · 26,383 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE VERTICAL RIB IN NOSE LANDING GEAR WHEEL WELL ABOVE THE DRAG BRACE CRACKED IN THE LOWER LEFT CORNER (WHEN LOOKING AFT). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW VERTICAL RIB IN THE NOSE LANDING GEAR WELL IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN) · airframe 30,833 hrs · 26,110 cycles

ON FLIGHT 4196 THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR OZONE SMELL FROM GASPER VENT AND OVER SEAT 1A. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND SEAT 4A CEILING LIGHT HARNESS ASSEMBLY RECEPTACLE BURNT. REMOVED AND REPLACED THE HARNESS ASSEMBLY AND THE LAMP IAW EMB 145 AMM 33-21-06. THE OPERATIONAL CHECK WAS GOOD NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — DEFECTIVE (BLEED AIR SYS) · airframe 30,824 hrs · 26,101 cycles

ON FLIGHT 3967 THE CREW REPORTED, RECEIVED NR 1 BLEED LEAK MESSAGE ON EICAS IN CLIMBOUT AT APPROX 5000". FOLLOWED AOM NR 1 CHECKLIST WITH NR 1 BLEED OFF MESSAGE REMAINED AFTER 3 MINUTES. TURNED NR 2 BLEED OFF MESSAGE WENT OUT AFTER APPROXIMATELY 4 MINUTES WITH NR 1 BLEED BACK ON. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE T- TUBE LOCATED BETWEEN JOINTS 17 AND 19 ON NR 1 BLEED SYSTEM IAW M/M 36-11-09. THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 29,323 hrs · 24,934 cycles

DURING MAINTENANCE BASE VISIT FOUND CORROSION ON SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGER 21 LEFT AND 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGER 21 LEFT AND 21 RIGHT IAW EO EM-5300-1620 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 29,137 hrs · 24,771 cycles

ON FLIGHT 4319 DURING THE APPROACH THE CREW REPORTED, RECEIVED A BRAKE DEGRADED MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CONTROL VALVE IAW EMB145 AMM 32-41-06. ALSO BLED THE BRAKES IAW 32-40-00, COMPLYING WITH A FUNCTIONAL CHECK IAW 32-41-00. THE OPERATIONAL CHECK WAS GOOD. ALSO MAINTENANCE INSPECTED THE FUEL QUANTITY INDICATION HARNESS IAW 28-41-00-200-801. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,023 hrs · 24,685 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN ON THE AFT GALLEY TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE EMERGENCY EXIT MARKER IAW EMBRAER AMM 33-50-13 AND REPLACED THE INVERTER FOR THE EMERGENCY EXIT MARKER. THE OPERATIONAL CHECK WAS GOOD IAW EMBRAER AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,679 hrs · 24,412 cycles

DURING MAINTENANCE BASE VISIT FOUND DENT DAMAGE TO THE RIGHT REDUCED VERTICAL SEPARATION MINIMUM AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE DENT DAMAGE TO THE RIGHT REDUCED VERTICAL SEPARATION MINIMUM AREA IAW EO EM 53-MR-1527. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 28,164 hrs · 23,965 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CABIN EMERGENCY FLASHLIGHT TO BE WORKING INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

ON FLIGHT 3609, DURING A ROUTINE MAINTENANCE CHECK, FOUND THAT THE FORWARD CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. CLEANED THE ELECTRICAL CONNECTORS OF THE LIGHT, OPS CK GOOD IAW SWPM 20-50-00, 33-50-15 AND 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,189 hrs · 21,165 cycles

DURING A IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITION THE NEW SILL AND DRILLED, REMOVED TO CLEAN AND TREAT NEW PART. REPAIR DONE IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 22,189 hrs · 21,165 cycles

DURING A IMBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGE SILL AND CLEANED THE AREA. POSITIONED NEW SILL AND DRILLED, CLEANED AND TREATED PARTS AND INSTALLED. REPAIR DONE IAW SRM 51-20-01,03, 51-40-02, 04 AND 06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,189 hrs · 21,165 cycles

DURING A MBV INSPECTION THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION BY BLENDING AND PERFORMED NDT INSP CLEANED, ALODINED AND PRIMED THE REWORKED AREA. FILLED IN BLENDED AREA. FABRICATED A DOUBLER. REPAIR DONE IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: PROFILE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 22,189 hrs · 21,165 cycles

DURING AN IMBV INSPECTION, THE MAIN DOOR LOWER PROFILE WAS FOUND TO BE CORRODED AROUND THE AFT SCREW HOLE. REMOVED CORROSION BY BLENDING, PERFORMED NDT INSPECTION, NO CRACK NOTED. FABRICATED A DOUBLER. DRILLED, CLEANED, ALODINED AND PRIMED DOUBLER AND BLENDED AREAS. REPAIR DONE IAW ETN-EM-52-041 DATED 12/31/08. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (ENGINE)

ABI - FLT 9305 - RETURN TO FIELD ABI, SMOKE IN LAVATORY, EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED O-RING AND ZERO CARBON SEAL ON RT ENGINE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB GST 3664/01 PARA 1 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 29. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, AND SHIMS. REPAIR DONE IAW EMB GST-3354/01, EMB 145 (SRM145/1142 CHAPTER 53 REV 15) 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: BRACKET — CRACKED (RT WING)

DURING INSPECTION, FOUND RIGHT WING TIP LOWER ATTACHMENT BRACKET CRACKED. REMOVED CRACK BY CUT OUT. FABRICATED A DOUBLER ANGLE AND A FILLER. REPAIR DONE IAW EMB GST 3691/01 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM (PREV REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREV REPAIR). FABRICATED A DOUBLER ANGLE AND FILLER. WORK DONE IAW EMB 145 (SRM-145/1142 CHAPTER 53 REV 15) 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM BETWEEN FRAMES 21 AND 23. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3679/01 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM GOING UNDER CENTER AISLE SUPPORT AT FRAME 58. REMOVED CORROSION BY CUT OUT. FABRICATED A REPAIR FILLER AND SHIMS. REPAIR DONE IAW EMB GST-3679/01 PARA 3B AND STANDARD SRM PRACTICES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, FOUND CORROSION WAS FOUND ON THE GALLEY CENTER FLOOR SUPPORT, OMEGA SHAPE THAT SUPPORTS THE RIGHT INBOARD SEAT TRACK. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. REPAIR DONE IAW EMB GST-3686/01/, PARA 1 EMB145 SRM'S 51-20-03, 51-21-04, 51-40-02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER FLOORBEAM CORRODED. REMOVED AND INSTALLED SERVICEABLE GALLEY CENTER BEAM IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. CENTER BEAM GUSSET CORRODED IS GALLEY AREA. INSTALLED SERVICEABLE GUSSET IAW EMB145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. SERVICE DOOR AFT SILL CORRODED. INSTALLED SERVICEABLE SILL IAW EMB145 SRM 51-40-02. (M)

Part: CHARGER — INOPERATIVE (CABIN)

ORD - FLT 4198 - EMERGENCY LIGHT OVER 12AC INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY CHARGE CHASIS ASSEMBLY IAW EMB145 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (NR 2)

GSP - FLT 4168 - AFTER STARTING TWO ENGINE, WITH ENGINE PARAMETERS STABLE. ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. CREW HAD NO WARNINGS PRIOR TO SHUT DOWN. (M)

Part: BATTERY — INOPERATIVE (CABIN) · airframe 3,820 hrs · 4,120 cycles

MGM - FLT 3703 - FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 1 FORWARD CABIN EMERGENCY BATTERY. OPS CHECK GOOD. (X)

Part: BOTTLE — DISCHARGED (CARGO BAY)

ORD - FLT 4125 - CARGO SMOKE LIGHT CAME ON IN FLIGHT. DISCHARGED BOTH FIRE BOTTLES AND RETURNED TO FIELD. AIRCRAFT HAD NORMAL LANDING. INSPECTED SYSTEM AND PERFORMED OPS CHECKS. FOUND BLEED DUCT LINE LOOSE IN LEFT SIDE OF CARGO BAY. CORRECTED AND PERFORMED OPS CHECK OF SYSTEM IAW AMM 36-11-09. REMOVED AND REPLACED BOTH FIRE BOTTLES IN CARGO BAY. OPS CHECK GOOD IAW AMM 26-15-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — FALSE INDICATION (BAGGAGE COMPT)

XNA - FLT 3603 - DURING APROACH, THE CARGO SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS IAW EMB-145 AMM 26-15-00. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (BAGG COMPT)

DSM - FLT 4017 - ON APPROACH BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. DECLARED EMERGENCY. LANDED SAFELY. DETERMINED TO BE A FALSE WARNING. DEFERRED BAGGAGE SMOKE WARNING SYSTEM. PERFORMED OPERATIONAL CHECK OF BAGGAGE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. MEL ITEM RESTORED ON 3-18-99. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (E/E COMPT)

MKE - FLT 4300 - ON CLIMB-OUT, HAD BAGGAGE SMOKE DETECTION WARNING. DISCHARGED NR 1 FIRE EXTINGUISHER. DECLARED EMERGENCY. LANDED SAFELY. DETERMINED TO BE A FALSE WARNING. SYSTEM DEFERRED PER MEL 26-13 AND 26-15. DURING THE WEEKEND OF 3/5-7, A RELAY WAS REPLACED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CLE - FLT 4337 - BAGGAGE COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED FIRE EXTINGUISHERS. EVENT WAS DETERMINED TO BE A FALSE WARNING. DEFERRED BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM FOR FLIGHT BACK TO ORD WHERE THE SMOKE DETECTOR AND FIRE EXTINGUISHERS WERE REMOVED AND REPLACED. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — LOOSE (CARGO BAY)

MKE - FLT 4300 - CARGO SMOKE INDICATION ILLUMINATED ON APPROACH. ACTIVATED FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED BOTH HIGH AND LOW PRESSURE FIRE EXTINGUISHERS. PULLED BAGGAGE SMOKE DETECTOR CIRCUIT BREAKER AND COLLZRED PER EMBRAER LETTER REF SST 1639/98. ITEM IS DEFERRED. FOUND WIRE GOING TO PIN 7 WAS HELF IN BY ONLY TWO STRANDS. REPAIRED WIRE WITH SPARE CONNECTOR AT PIN 15. OPERATIONAL CHECK GOOD. MEL CLEARED. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

DSM - FLT 4074 - UPON DESCENT, CARGO SMOKE WARNING ILLUMINATED. AS A PRECAUTION, CREW ACTIVATED CARGO FIRE EXTINGUISHERS. AIRCRAFT LANDED SAFELY, PASSENGERS DEPLANED NORMALLY. VERIFIED EVENT AS A FALSE WARNING, AS THERE WAS NO EVIDENCE OF SMOKE OR FIRE. OPENED MEL ON THE CARGO SMOKE INDICATION AND THE CARGO FIRE EXTINGUISHER SYSTEM. AIRCRAFT RETURNED TO SERVICE. NOTE: AWAITING FURTHER CORRECTIVE ACTION, TO BE FILED UPON COMPLETION. (X)

Part: SMOKE DETECTOR — FAILED (BAGGAGE COMPT)

CVG - FLT 4096 - RECEIVED BAGGAGE SMOKE WARNING. CARRIED OUT CHECKLIST ACTIONS. REQUIRED FIRE EXTINGUISHER AGENT DISCHARGE. REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. OPS CHECK GOOD IAW 26-15-01. AIRCRAFT RETURNED TO SERVICE. (X)