N681AE

Part: FRAME — CORRODED (FR 22 S16R) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E041395 FR 22 CORRODED ABOVE STGR 16R AT SERVICE DOOR CENTER SILL ATTACHMENT BRACKET. COMPLETED INSTALLATION OF FR 22 REPAIR SECTION BTW STGR 11R-18R AND REPAIR SPLICES IAW EMB 145 SRM 53-00-04 ITEM 17 FIGURE 209 AND ETD# ETD2024-145-015504 AND PIEDMONT EO1-53-24-0363

Part: FRAME — CORRODED (FR 20 S16R) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E041393 FR 20 CORRODED ABOVE STGR 16R AT SERVICE DOOR CENTER SILL ATTACHMENT BRACKET. REMOVED AND INSTALLED SERVICEABLE FR 20 SECTION BETWEEN STGR. 4R-18R OF SERVICE DOOR CENTER SILL ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-02, ETD2024-145-015495 AND PIEDMONT EO1-53-24-0375

Part: GUSSET — CORRODED (RT NACELLE) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E041241 RH UPPER ENGINE COWLING CENTER TRIANGLE GUSSET HAS CORROSION. REMOVED AND REPLACED RH UPPER ENGINE COWLING CENTER TRIANGLE GUSSET IAW EMB 145 SRM 51-40-02

Part: LINER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040577 BAGGAGE DOOR LWR INTERAL SKIN LINER 2EA FASTENER HOLES SHOW SIGNS OF CORROSION. RAR BAGGAGE DOOR INNER LOWER SKIN IAW SRM 51-30-01

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040305 CORROSION ON CROSS FLOOR BEAM BETWEEN FRAMES 24-25. BLENDED OUT CORRODED AREAS ON CROSS FLOOR BEAM BETWEEN FRAMES 24-25 IAW EMB145 SRM 51-10-03 AND FOUND REMAINING THICKNESS TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-22-10AD.

Part: FLOOR SUPPORT — CORRODED (FRS 39-45) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040363 CENTER FUSELAGE III INTERNAL, LH FLOOR GUSSET CORRODED BETWEEN FR39/45. REMOVED AND REPLACED CENTER FUSELAGE III INTERNAL, LH FLOOR GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (FR 20) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040111 CORROSION ON CROSS FLOOR BEAM AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE CROSS FLOOR BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040122 CORROSION ON LH OTBD #1 FLOOR SILL. REMOVED AND REPLACED LH OTBD #1 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (FR 20) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040109 CORROSION ON CENTER BEAM GUSSET AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE GALLEY CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED (CARGO) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040106 CORROSION ON SERVICE DOOR CENTER SILL. RAR SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (FR 22) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040107 CORROSION ON DIAMOND GUSSET AT FRAME 22. RAR DIAMOND GUSSET AT FR 22 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040123 CORROSION IN GALLEY AREA ON LH AFT DIGITAL PREVIOUS REPAIR. FABRICATED NEW DOUBLER IAW EMB 145 SRM 51-21-10RE, APPLIED HYSOL AND INSTALLED DOUBLER ON GALLEY LH AFT DIGITAL IAW ETD2024-145-015165 AND PIEDMONT EO1-05-24-0402.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E040121 CORROSION IN GALLEY AREA ON LH INBD #1 SEAT TRACK. REMOVED AND REPLACED LH INBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E039690 CARGO DOOR CUTOUT LOWER CENTER SILL IS CORRODED. RAR THE CARGO DOOR CUT OUT LOWER CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: STRUCTURE — CORRODED (FR 65) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E039689 CARGO DOOR CUTOUT FWD L-SHAPE IS CORRODED. REPAIRED THE CARGO DOOR CUT-OUT FWD L-SHAPE AT FR65 IAW EMB 145 SRM 53-31-04 ITEM 4 FIGURE 212 AND PIEDMONT EO1-53-24-0369.

Part: SKIN — CORRODED (MAIN DOOR) · corrosion level 2 · airframe 45,871 hrs · 40,854 cycles

E039159 MAIN DOOR LOWER LINER INTERNAL SKIN SCREW HOLES CORRODED 4EA. REMOVED AND INSTALLED SERVICEABLE MAIN DOOR AFT LOWER LINER INTERNAL SKIN IAW EMB 145 SRM 51-40-02,

Part: CHARGER — FAULTED (EMERGENCY LIGHTS) · airframe 45,296 hrs · 40,186 cycles

FWD EMERGENCY LIGHT ON LH WING INOP FACT 21JAN24 08:32 SBY. DETERMINED CAUSE TO BE INOPERATIVE BATTERY CHARGER ASSEMBLY FOR THE #100 EMERGENCY BATTERY.R+R'D BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04 OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,125 hrs · 39,996 cycles

BURNING SMELL NOTED IN FLT WITH NOTED CLEARING OF SMELL WITH WINDSHIELD HEAT 2 SELECTED OFF. R+R WHSHD HEAT #2 CONTROLLER IAW 30-42-01, NO FIX. R+R'S WINDSHIELD CONTACTOR AND ASSOC FUSE IRT AMM 30-42-02. OPS CHECKED IRT 30-42-00. OPS CHECK GOOD NO BURNING SMELL NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,116 hrs · 39,986 cycles

DURING INTAL TAKEOFF ROLL W/S 2 HEAT FAIL ON EICAS WITH CLICKING NOISE. C/W FLT CREW AND MAINT PROCEDURES. P/C C/B J-20. R/R'D #200 W/S TEMP CONTROL MODULE IAW MM 30-42-01, OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,422 hrs · 39,175 cycles

STARTED APU EXPERIENCED MOMENTARY POWER LOSS WITH GPU CONNECTED AND SMELLED ELECTRIC FUMES. GPU AT GATE FOUND TO BE INOP. RAN APU OFF BATTERY FOR 10 MINUTES. NO DEFECTS NOTED AT THIS TIME, OK FOR SERVICE.

Part: BATTERY PACK — UNKNOWN (UNKNOWN) · airframe 48,896 hrs · 38,601 cycles

AFT 3 FLOOR PROX LIGHTS FLASH BUT DO NOT STAY ON. R&R'D EMERGENCY BATTERY PACK IAW AMM 33-50-04

Part: BRAKE — FAILED · airframe 42,888 hrs · 37,500 cycles

BRAKE DEGRADE SHORT FINAL WENT AROUND AND WENT AWAY .SECOND APPROACH AFTER GEAR DOWN BRAKE DEGRADE RETURNED AND REMAINED-C/A-PERFORMED MAIN BRAKE SYSTEM FUNCTIONAL CHECK IAW EMB-145 AMM 32-41-00 OPS CHECK GOOD NO MESSAGES NOTED REF FIM 32-41-00-810-804-A FOUND TO BE TRANSITORY CONDITION OF BRAKE SYSTEM

Part: LAMP — INOPERATIVE (AISLE) · airframe 42,876 hrs · 37,486 cycles

EMERGENCY AISLE LIGHT INOP-C/A-RAR EMERGENCY AISLE LIGHT LAMP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: NONE — UNSERVICEABLE (ROW 10-11) · airframe 42,494 hrs · 37,059 cycles

MEL 33-23, AUTH. NO: 050313-C. ROW 10-11 EMERGENCY FLOOR STRIP INOP. ORIGINAL LOG PAGE 4866095.-C/A-REMOVED AND REPLACED STRIP LIGHTING IAW AMM 33-50-12. OPS CHECK GOOD. MEL ITEM RESTORED.

Part: NONE — NONE · airframe 42,472 hrs · 37,032 cycles

ROW 10-11 EMERGENCY FLOOR STRIP INOP-C/A-DEFER EMERGENCY STRIP PER MEL 3323. EXP DAY 5/31/22 CA PENDING

Part: NONE — NONE · airframe 42,369 hrs · 36,920 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT WILL NOT CHARGE-C/A-DEFERRED PER MEL 2532 M PROCEDURES C/W EXP 5/10/22 CA PENDING

Part: NONE — UNSERVICEABLE (LH) · airframe 42,268 hrs · 36,816 cycles

LH OVERWING PANEL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — BROKEN (FA) · airframe 42,268 hrs · 36,816 cycles

FA EMERGENCY FLASHLIGHT BRACKET CLAMP BROKEN-C/A-RAR FA EMERGENCY FLASHLIGHT BRACKET CLAMP IAW AIR LITE 2R LED FLASHLIGHTCMM 25-60-14

Part: NONE — NONE · airframe 42,055 hrs · 36,570 cycles

LH AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH AFT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: NONE — NONE · airframe 41,936 hrs · 36,434 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BROKEN REF: LOGPAGE 4804373 ITEM 2 MEL 2532 - AUTH# 020124M-C -C/A-RAR AFT FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD MEL RESTORED

Part: NONE — NONE · airframe 41,932 hrs · 36,429 cycles

CABIN AFT EMERGENCY FLIGHTLIGHT BRACKET IS BROKEN-C/A-DEFERRED PER MEL 25-32., AUTH# 020124M-C.

Part: NONE — NONE · airframe 41,814 hrs · 36,296 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A.

Part: NONE — NONE · airframe 41,585 hrs · 36,025 cycles

LH AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A OPS CHECK GOOD

Part: NONE — NONE · airframe 41,533 hrs · 35,973 cycles

AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT EMERGENCY FLIGHT ATTENDENT FLASHLIGHT M PROCEDURES C/W AUTH 11029M-C REF 25-32MOC 630997

Part: NONE — NONE · airframe 41,515 hrs · 35,952 cycles

LEFT AILERON DAMPER FITTING IS CHAFFED.(MAJOR REPAIR)-C/A-REPLACED FITTING IAW EO-EM-27MR-112

Part: NONE — NONE · airframe 41,515 hrs · 35,952 cycles

RH AILERON DAMPER FITTING IS CHAFFED. (MAJOR REPAIR)-C/A-REPLACED FITTING IAW EO-EM-27MR-112.

Part: NONE — NONE · airframe 41,515 hrs · 35,952 cycles

#6 FLOOR PROX. EMERGENCY LIGHT STRIP WIRE BROKEN AND IT HAS AN AREA OF DE-LAMINATION.-C/A-COMPLETE:REPLACED #6 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: NONE — NONE · airframe 41,515 hrs · 35,952 cycles

FOUND SCRATCHES ON THE TOP SIDE OF THE #1 FLOOR EMERGENCY PROX STRIP LIGHT ( SERVICE DOOR LOCATION)-C/A-COMPLETE:REMOVED AND REPLACED #1 FLOOR EMERGENCY PROX STRIP LIGHT ( SERVICE DOOR LOCATION) IAW AMM 33-50-12.OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 41,226 hrs · 35,606 cycles

LH EXTERNAL OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,125 hrs · 35,488 cycles

MEL 33-22 ON LOG PAGE# 4734279/1 LH/RH OVERWING EMERGENCY LIGHT INOP. AUTH# 070505D-C"TRANSFERRED TO NRWC 681-DFW-05721"-C/A-REFERENCE NRWC 681-DFW-05721 ITEM 3 REMOVED AND REPLACED #4 BATTERY POWER SUPPLY AND CHARGER ASSY. IAW EMB145 AMM 33-50-04. OPERATIONAL CHECK GOOD. MEL RESTORED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,980 hrs · 35,302 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10 OPC GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,950 hrs · 35,265 cycles

BOTH WINGS EXTERNAL OVERWING UPPER EMERGENCY LIGHTS INOP-C/A-RAI # 4 EMERGENCY LIGHT POWER SUPPLY IAW E145 AMM 33-50-04 OPS CHECK GOOD PER AMM TASK 33-50-00-700-801-A

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 40,690 hrs · 34,978 cycles

IN CRUISE FLIGHT HAD A SMELL AND SMOKE IN COCKPIT OUT OF SOMEWHERE IN THE CENTER PANE DECLARED EMERGENCYL"TRANSFERRED TO NRWC 681-SAT-05543"JOSHUA ALES 657840-C/A-C/W ENG RUNS IAW RR LMM 72-00-00 AND PERFORMED ETN# ETN-EM-72-034.NO SMOKE OR SMELL NOTICE.AIRCRAFT GOOD FOR FURTHER FLT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,649 hrs · 34,931 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EXTERNAL LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: CONNECTOR — LOOSE (WARNING SYSTEM) · airframe 40,642 hrs · 34,924 cycles

DURING TAKEOFF ROLL NO TAKE OFF CONFIG EICASS MESSAGE. NO AURAL INDICATION. AFTER ABORT RAN QRH. RECIEVED TAKEOFF OK AURAL MESSAGE AND ATTEMPTED SECOND TAKEOFF. NO TAKE OFF CONFIG EICAS MESSAGE OCCURED IN SECOND ATTEMPT W/OUT AURAL IND-C/A-INSPECTED AURAL WARNING SYSTEM AND FOUND CONNECTOR SLIGHTLY LOOSE. RETIGHTENED CONNECTOR IAW EMB 145 AMM 31-51-01. PERFORMED MULTIPLE OPS CHECKS IAW EMB 145 AMM 31-51-00. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,456 hrs · 34,721 cycles

LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A RAR BATTERY POWER SUPPLY IAW 33-50-04-000-801-A AND 33-50-04-400-801-A AND BATTERY PACK IAW 33-50-04-000-802-A AND 33-50-04-400-802-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,456 hrs · 34,721 cycles

AFT EMERGENCY EXIT FLOOR STRIP LIGHTS INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A RAR EMERGENCY LIGHT DC/AC INVERTER IAW 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: CONNECTOR — DETACHED (CABIN PRESSURE) · airframe 40,451 hrs · 34,715 cycles

CABIN DID NOT PRESSURIZE IN CLIMB IN AUTO MODE OR MAN MODE AFTER RUNNING CABIN ALTITUDE IN AMBER RANGE AND THEN PRESN AUTO FAIL CHECKLIST RETURNED TO DEPT AKP DID NOT DECLARE EMERGENCY-C/A-FOUND GROUND CONNECTION VALVE DETACHED FOUND DOWNLINE PACK SYSTEM. INSTALLED NEW GROUND CONNNECTION VALVE IAW EMB AMM 21-22-04. OPS CHECK PRESSURIZATION LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 40,411 hrs · 34,672 cycles

FWD FA EMEERGENCY FLASH LIGHT INOPMEL 2532 -AUTH# 03-204M-C LOGPAGE: 4729530 ITEM: 1 -C/A-RAR FWD FA EMERGENCYFLASH LIGHT AND BATTERY REF EMB 145 AMM 33-50-16. AND ETN-EM-33-059 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED MEL RESTORED

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 40,403 hrs · 34,660 cycles

FWD FA EMERGENCY FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT. M PROCEDURES C/W. MELAUTH# 030204M-CREF# 25-32MOC# 628765

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 40,392 hrs · 34,650 cycles

FWD CABIN EMERGENCY FLASH LIGHT HOLDER BROKEN. DEFERRED PER MEL 25-32 FWD CABIN EMERGENCY FLASHLIGHT HOLDER M PROCEDURE COMPLIED WITH-C/A-THIS IS A SUPPLEMENTAL-RAR FWD CABIN FLASHLIGHT ASSY IAW AMM 33-50-16.OPS CHECK GOOD.MEL RESTORED.

Part: FUSE — INOPERATIVE (EMER PWR SUPPLY) · airframe 40,347 hrs · 34,618 cycles

BOTH L/H AND R/H AFT EXTERIOR EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED FUSE ON #4 EMERGENCY LIGHT POWER SUPPLY IAW EMB 145 CMM 25-60-03. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,276 hrs · 34,560 cycles

EXTERIOR EMERGENCY LIGHTS INOP. C/A-T/S EXTERIOR EMERGENCY LIGHTS AND FOUND POWER SUPPLIES 1 AND 4 NO GOOD. R & R 1 AND 4 EMERGENCY LIGHT POWER SUPPLIES IAW AMM 33-50-04 OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,170 hrs · 34,458 cycles

SERVICE DOOR LOWER EMERGENCY LIGHT PLACARD INOPERABLE. C/A: R & R NR 2 EMERGENCY BATTERY, IAW EMB AMM TASK 33-50-04-000-802-A AND TASK 33-50-04-400-802-A AND TASK 33-50-04-000-801-A AND TASK 33-50-04-400-801-A. OPERATIONS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 40,113 hrs · 34,402 cycles

MEL 25-53 AUTH NR 120200-C AFT CABIN FLASHLIGHT INOPERABLE, REF LOG PAGE 4683946 ITEM: 1. C/A: R & R AFT CABIN FLASHLIGHT ASSEMBLY, IAW EMB 145 AMM 33-50-16 AND ETN -EM-33-059 OPERATIONS CHECK GOOD MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 40,088 hrs · 34,373 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOPERABLE. C/A: DEFERRED AFT EMERGENCY FLASHLIGHT, PER MEL 25-53 M PROCEDURE C/W.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 40,071 hrs · 34,354 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BROKEN. MEL 25-53 AUTH NR 120127-C, REF AML PG 4683929 ITEM 1. C/A: R & R AFT EMERGENCY FLASHLIGHT ASSEMBLY, IAW EMB145 AMM 33-50-16, ETN-EM-33-059. OPERATIONAL CHECK GOOD MEL NR 25-53 AUTH NR 120127-C RESTORED.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 40,060 hrs · 34,339 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BROKEN. C/A: EMERGENCY FLASHLIGHT DEFFERED, PER MEL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 40,025 hrs · 34,300 cycles

NR 4 EMERGENCY FLOOR LIGHT STRIP CONNECTOR BROKEN. C/A: INSTALLED PIN CONNECTORS FOR SPLICES SP9102 AND SP9103 ON NR 4 EMERGENCY FLOOR LIGHT STRIP, IAW EMB-145 SWPM 20-50-00. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 39,961 hrs · 34,235 cycles

FLAP LOW SPEED ADVISORY ACTIVATED AT 4000 FT MSL AND 195 KTS WHEN FLAP LEVER MOVED TO 9. C/A: DEFERRED PER MEL 27-9 AUTH NR 110198DM-B FLAP LOW SPEED MESSAGE ON EICAS. M PROCEDURE C/W.

Part: SHOCK ABSORBER — FAILED (MLG) · airframe 39,755 hrs · 34,005 cycles

LAND GEAR AIR/GROUND FAIL. AIRCRAFT REQS EXTENSION/RETRACTION CHECK DUE TO REPLACEMENT OF SHOCK ABSORBER & CARDAN JOINT. C/A LANDING GEAR EXTENSION/RETRACTION CHECKS GOOD, IAW EMB 145 AMM 32-30-00 AND 32-34-00.

Part: SPRING — DEFECTIVE (BRAKE PEDAL) · airframe 39,380 hrs · 33,604 cycles

LEFT BRAKE ON CAPTAIN SIDE FAILED. ONLY ALLOWS FULL APPLICATION OR NONE. REMOVED AND REPLACED BRAKE PEDAL TRANSDUCER SPRING IAW AMM 32-41-01. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,213 hrs · 33,414 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LIGHT — INOPERATIVE (OVERIWNG EXIT) · airframe 39,137 hrs · 33,330 cycles

LEFT AFT OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LEFT AFT OVER WING EMERGENCY LIGHT LAMP OPS CK GOOD IAW WITH AMM 33-50-10

Part: ACTUATOR — FAULTY (NLG DOOR) · airframe 39,086 hrs · 33,285 cycles

LG AIR/GROUND FAIL DURING GEAR EXTENSION ON FINAL, WENT AROUND AND IT DISAPPEARED AT 2500 MSL. 2ND ATTEMPT , EXTENDED GEAR AND INDICATION RETURNED SO WE DECLARED AN EMERGENCY AND LANDED. IT ONCE AGAIN WENT AWAY AT 700 FT AGL THIS TIME.-C/A-REMOVED AND REPLACED NLG DOOR LH ACTUATOR IAW EMB 145 AMM 32-33-03 OPS CHECK GOOD -

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,037 hrs · 33,236 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT IAW 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME. END.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 38,924 hrs · 33,126 cycles

UPPER LH EMERGENCY LIGHT ON THE EXTERIOR OF A/C FOUND INOP-C/A-REMOVED AND REPLACED OF LIGHT BULB IN UPPER LH EXTERIOR OF A/C IAW EMB145 AMM 33-50-11. OPS CHECK GOOD EMERGENCY LIGHT OPERATIVE

Part: TUBE — CHAFED (ENGINE OIL SYS) · airframe 38,628 hrs · 32,869 cycles

OIL LEAK ON #2 ENGINE-C/A-FOUND THE FCDC BYPASS PRESSURE OIL TUBE TO THE ACOC CHAFED. REMOVED AND REPLACED THE ACOC TO THE FCDC PRESSURE LINE IAW RR MM 79-00-00-400-801. LEAK CHECK AND OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,475 hrs · 32,742 cycles

LH EXTERNAL EMERGENCY LIGHT FORWARD OF LEADING EDGE WING ROOT, COCKPIT CEILING FLOOD EMERGENCY LIGHT AND AISLE #1 CEILING EMERGENCY LIGHT ARE INOP.-C/A-T/S USING WM 33-50-50. REMOVED AND REPLACED #1 EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-50-04. ALL EMERGENCY LIGHTS OPC GOOD IAW AMM 33-50-00-700-801.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 38,450 hrs · 32,726 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMVOED AND REPLACED RH OVERWING EMERG LIGHT IAW EMB 145 AMM 33-50-07. OPC GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,422 hrs · 32,703 cycles

LH FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY AND CHARGER, OPC GOOD, IAW EMB AMM 33-50-04. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 77460

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,264 hrs · 32,565 cycles

MAINDOOR OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAINDOOR OVERHEAD EMERGENCY LIGHT IAW EMB AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME. END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,136 hrs · 32,462 cycles

EMERGENCY LIGHT ABOVE LH WING INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT ABOVE LH WING IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,064 hrs · 32,376 cycles

DURING PS-2 CHECK, FOUND LT SIDE CENTER FAIRING EMERG LIGHT INOP. REMOVED AND REPLACED EMERG LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 37,833 hrs · 32,133 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB, IAW AMM 33-50-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,733 hrs · 32,059 cycles

CENTER AISLE EMERGENCY LIGHT SYSTEM IS INOP. REMOVED AND REPLACED THE NR 5 DC/AC INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: BLEED VALVE — FAILED (APU) · airframe 37,708 hrs · 32,028 cycles

APU BLEED VALVE FAIL WITH THE OPEN INSCRIPTION ILLUMINATED. REMOVED AND REPLACED APU BLEED VALVE IAW AMM 36-12-03. OPC GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 37,695 hrs · 32,015 cycles

LH OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH OVER WING EMERGENCY LIGHT IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 37,436 hrs · 31,744 cycles

#8 EMERGENCY FLOOR LIGHTING STRIP ON A/C SIDE HAS DAMAGED CONNECTOR. C/A-INSTALLED NEW CONNECTORS ON WIRES W192-8832-22 AND W192-8833-22 IAW SWPM 20-21-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,436 hrs · 31,744 cycles

#4 EMERGENCY BATTERY/CHARGER INOP. C/A-REMOVED AND REPLACED BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04, OPERATIONALLY CHECKED GOOD.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 37,436 hrs · 31,744 cycles

TDMI PERFORM PERMANENT REPAIR OF DENT LOWER AFT CORNER OF SERVICE DOOR-C/A-PERFORMED PERMANENT REPAIR OF SERVICE DOOR LOWER AFT CORNER IAW ERS-EM-52MR-998

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 37,436 hrs · 31,744 cycles

LOWER MOST NUTPLATE HOLE ON FWD EDGE OF CARGO DOOR IS OUT OF LIMITS.-C/A-REPAIRED LOWER NUTPLATE HOLE ON FWD EDGE OF CARGO DOOR IAW EMB 145 SRM 52-30-04.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 37,436 hrs · 31,744 cycles

SERVICE DOOR CENTER SILL IS CORRODED-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 37,436 hrs · 31,744 cycles

CARGO DOOR LOWER NUT PLATE HOLES HAVE CORROSION.-C/A- INSTALLED SERVICEABLE CARGO DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-24) · airframe 37,436 hrs · 31,744 cycles

LEFT OMEGA BEAM CORRODED FROM FRAMES 22 TO 24. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3818.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 37,436 hrs · 31,744 cycles

CARGO DOOR UPPER NUT PLATE HOLES HAVE CORROSION 4 EA.-C/A-REMOVED AND REPLACED CARGO DOOR UPPER PROFILE IAW EMB 145 SRM 51-20-02.

Part: LIGHT — BROKEN (CABIN) · airframe 37,436 hrs · 31,744 cycles

NUMBER 3 EMERGENCY FLOOR LIGHT STRIP WIRE BROKEN. REMOVED AND REPLACED LIGHT ON NUMBER 3 EMERGENCY FLOOR LIGHT STRIPS IAW EMB 145 AMM 33-50-12.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,436 hrs · 31,744 cycles

BAGGAGE DOOR SILL IS CORRODED. REMOVED AND REPLACED BAGGAGE DOOR SILL IAW EMB 145 SRM 53-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,295 hrs · 31,588 cycles

AFT AISLE EMERGENCY LIGHT INOP. C/A-AFT AISLE EMERGENCY LIGHT BULB REPLACED IAW AMM 33-50-08. LIGHTING TEST GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,295 hrs · 31,588 cycles

WING TO FUSELAGE EMERG LIGHT LT AFT INOP. C/A-WING TO FUSELAGE LT AFT EMERG LIGHT RELAMPED IAW AMM 33-50-10 OPC GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (CABIN PRESSURE) · airframe 36,932 hrs · 31,328 cycles

CABIN ALT DISPLAYED AMBER DASHES ON DEPARTURE, INDICATION RETURNED DURING DESCENT.-C/A-AT THIS TIME C/W OPS CK ON MANUAL PRESS. SYST PER AMM 21-31-00, FOUND SYST WORKING PROPERLY.

Part: RELAY — MALFUNCTIONED (OXYGEN SYSTEM) · airframe 36,697 hrs · 31,117 cycles

OXYGEN LO PRESS IMMEDIATLEY AFTER TAKE OFF OXY PREE GAUGE READS 0 PSI-C/A-FOUND 02 GAUGE TO BE READING 1650 PSI. COCKPIT INDICATION READS ZERO DEFERRED OXYGEN PRESSURE INDICATION SYSTEM MEL 35-01 AUTH 020878-B. REMOVED AND REPLACED O2 CTRL TRANSFERRELAY K0417 NO DEFECTS NOTED CB'SOK O2 INDICATIONJ NOW READING OK MEL ITEM RESTORED.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 36,645 hrs · 31,055 cycles

LT AND RT OVER WING EMERGENCY LIGHTS INOP. FOUND FUSE BLOWN ON #4 EMERGENCY BATTERY CHARGER. REMOVED AND REPLACED FUSE IAW CMM 25-60-03. OPS CHECK GOOD IAW AMM 33-50-00-700-801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,623 hrs · 31,028 cycles

RH AFT EXTERNAL OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH AFT EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND EMB AMM 33-50-10-400-801-A. DID NOT FIX. SUSPECT #4 EMERGENCY BATTERY AND POWER SUPPLY BAD. REMOVED AND REPLACED #4 EMERGENCY BATTERY AND POWER SUPPLY IAW EMB AMM 33-50-04-000-801-A, EMB AMM 33-50-04-400-801-A, EMB AMM 33-50-04-000-802-A. AND EMB AMM 33-50-04-400-802-A. OPS CHECK GOOD. NO MORE DEFECTS NOTED AT THIS TIME. END. BATTERY CHARGER ASSY P/N 11-0049 S/N 19233

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,608 hrs · 31,011 cycles

UPON PS-1 INSPECTION CHECK PART 11-C FOUND EXTERNAL EMERGENCY LIGHT LT-RT TOP INOP. R&R BATTERY PACK AND BATTERY CHARGER ON NR 4 REF AMM 33-50-04. OPS CHECK GOOD. MEL ITEM RESTORED. BATTERY CHARGER ASSY P/N 11-0049 S/N 19285

Part: NOZZLE — DIRTY (AC PACK) · airframe 35,777 hrs · 30,236 cycles

ON TAKEOFF WITH THRUST SET, EXCESSIVE MOISTURE/SMOKE NOTICED-C/A-CLEANED WATER SPRAY NOZZLE ON NR 1 PACK IAW AMM 21-51-13. OPS CHECK OF NR 1 PACK GOOD IAW AMM 21-51-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,152 hrs · 29,693 cycles

AC GOT HIT BY LIGHTNING ON RIGHT SIDE OF NOSE. THE PILOTS THEN NOTICED A BURNING SMELL. TRANSFERRED TO NRWC 681-MIA-03705. COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW W/C 05-200-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,675 hrs · 29,323 cycles

RIGHT EXTERNAL WING AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: SKIN — DENTED (FRAME 2) · airframe 34,593 hrs · 29,229 cycles

FOUND A LARGE DENT AND CRACK IN THE FWD RT FUSELAGE SKIN, FRAME 2, STRINGER 15R. REPAIRED THE DAMAGE IAW ERS-EM-53MR-3219.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,519 hrs · 29,165 cycles

RIGHT ESCAPE HATCH UPPER EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE SIGN. OPS CHECKED GOOD IAW AMM 33-50-14.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 34,231 hrs · 28,945 cycles

SERVICE DOOR LINING EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE DURING VISUAL INSPECTION. SPLICED THE WIRE IAW SWPM-2430-20-21-00. OPS CHECKED GOOD. NO FURTHER DISCREPANCIES FOUND.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,780 hrs · 28,564 cycles

SERVICE DOOR EMERGENCY LIGHT EXIT INOPERATIVE. FOUND TWO CONNECTORS UNSECURE. SECURED THE CONNECTORS, OPS CHECKED GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 33,774 hrs · 28,559 cycles

SERVICE DOOR EMERGENCY LT INOP. R&R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A OPS CHECK FAILED, REMOVED AND REPAIRED NR 2 EMERGENCY BATTERY CHARGER ASSEMBLY AND EMERGENCY BATTERY IAW W/C 33-700-19 OPS CHECK FAILED, TROUBLE SHOT AND FOUND BROKEN GROUND WIRE IN SERVICE DOOR HINGE AREA, SPLICED GROUND WIRE BACK TOGETHER IAW WM 33-50-50 & SWPM 20-13-01 OPS CHECKED IAW W/C 33-700-17 OPS CHECK GOOD AT THIS TIME NO FURTHER DEFECTS NOTED END. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 60690

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,763 hrs · 28,543 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,420 hrs · 28,210 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 33,310 hrs · 28,112 cycles

OVERHEAD EMERGENCY EXIT SIGN AND AT THE SERVICE DOOR INOPERATIVE. TROUBLESHOT AND FOUND THE NR 1 INVERTER TO BE BAD IAW WM 33-50-50. INSTALLED A USED INVERTER AND OPS CHECKED IAW W/C 33-700-17, OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,230 hrs · 27,996 cycles

RT OVERWING EXIT SIGN INOP AT SEAT 12 B/C. ALLOWED EMERGENCY SYSTEM CHARGE FOR 30 MIN AND THEN PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECK GOOD.

Part: BLEED VALVE — FAILED (RT ENGINE) · airframe 33,116 hrs · 27,863 cycles

AT 17,000 FT ICING CONDITIONS BLEED 2 VALVE FAILED, WING ANTI ICE FAILED AND ICE COND-ANTI ICE INOPERATIVE MESSAGES. REMOVED AND REPLACED THE RT ENGINE BLEED VALVE IAW AMM 36-11-05. OPS CHECKED GOOD. NO DEFECT NOTED ACCOMPLISHED OPERATIONAL TEST OF ANTI ICE SYSTEM IAW IAW AMM 30-00-00. OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 32,490 hrs · 27,356 cycles

NR 7 FLOOR PROXIMITY LIGHT HAS BROKEN WIRES. REMOVED AND REPLACED NR 7 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,489 hrs · 27,355 cycles

CRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L. PERFORMED PERMANENT REPAIR OF CRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L IAW SRM 53-31-01 RE FIG 219, SHEET 2.

Part: SKIN — BURNED (FUSELAGE) · airframe 32,489 hrs · 27,355 cycles

3 BURNS IN SKIN BETWEEN FRAMES 26-27 STRINGERS 21L-21R. REPAIRED FUSELAGE SKIN BURNS BETWEEN FRAMES 26-27 STRINGERS 21L-21R IAW SRM 53-22-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,489 hrs · 27,355 cycles

FRAME 65 IS CORRODED AT LOWER GUIDE PLATE. FABRICATED AND INSTALLED REPAIR DOUBLER ON FRAME 65 AT LWR GUIDE PLATE IAW SRM 53-31-04, FIG 212, SHEET 2

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,489 hrs · 27,355 cycles

CARGO DOOR CUTOUT LATERAL L-SHAPE IS CORRODED AT LWR GUIDE PLATE ON FRAME 65. REPAIRED CARGO DOOR CUTOUT LATERAL L-SHAPE CORROSION AT LWR GUIDE PLATE ON FRAME 65 IAW SRM 53-31-04.

Part: FITTING — CRACKED (LT PYLON) · airframe 32,489 hrs · 27,355 cycles

LT PYLON FWD YOKE LOWER FWD FITTING CRACKED. REMOVED AND REPLACED LT LOWER FORWARD YOKE FITTING IAW EO EM-54MR-386.

Part: LIGHT — CRACKED (CABIN) · airframe 32,489 hrs · 27,355 cycles

LT EMERGENCY LIGHT EXTRUSION NR 1 AND NR 3 CRACKED. REMOVED AND REPLACED LT EMERGENCY LIGHT EXTRUSION NR 1 AND NR 3 IAW AMM 33-50-12. SEE NRTC BOW246051 FOR INSTALLATION

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,306 hrs · 27,185 cycles

LT OVERWING EMERGENCY LIGHT INOP. R&R BATTERY CHARGER NR 4 IAW AMM 33-50-04. R&R BATTERY PACK NR 4 IAW AMM 33-50-04. OPS CK OF EMERGENCY LIGHTS GOOD. NO FURTHUR DEFECTS NOTED. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 68896

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 32,154 hrs · 27,052 cycles

BLEED 2 OVERTEMP IN ICING CONDITION. T/S IAW FIM 36-11-00-810-804-A. REMOVED AND REPLACED FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06.

Part: FILTER — FAILED (AIR VALVE) · airframe 32,145 hrs · 27,047 cycles

NR 2 BLEED OVERTEMP DURING ICE PROTECTION TEST IN FLIGHT. REMOVED AND REPLACED THE RT FAN AIR VALVE FILTER IAW W/C 36-100-05. OPS CHECKED GOOD IAW AMM 36-00-00.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 32,046 hrs · 26,944 cycles

LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT SYSTEM CHARGER NR 4 AND BATTERY NR 4 IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 31,942 hrs · 26,843 cycles

AFTER TAKEOFF, THE RT MLG INDICATED LANDING LEVER DISAGREE AND RED WARNING INDICATION, DECLARED AN EMERGENCY.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT MLG) · airframe 31,942 hrs · 26,843 cycles

AFTER TAKEOFF, RT MLG INDICATED LANDING LEVER DISAGREE. INSPECTED MLG AND MLG UPLOCK, DOWNLOCK, AND WOW PROX SWITCHES IAW AMM 32-63-05. VERIFIED CMC MSGS AND FOUND NO MESSAGES ON CMC. PERFORMED LANDING GEAR SYS EXT AND RETRACTION TEST (4 TIMES) IAW AMM 32-30-00-700-801. NO DEFECTS NOTED OPS CHECK GOOD. PERFORMED MLG SHOCK ABSORBER INSPECTION AND EXT CHECK IAW AMM 32-10-02. NO DEFECTS NOTED. OK FOR SERVICE

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,788 hrs · 26,704 cycles

CABIN FWD AISLE EXIT LIGHTS AND RT OVERWING FWD EMERGENCY EXIT LIGHTS INOPERATIVE. NR 2 POWER SUPPY BATTERY PACK AND BATTERY POWER SUPPLY R & R IAW WORKCARD 33-70-19. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,634 hrs · 26,559 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-50-04 AND OPS CHECKED IAW W/C 33-700-17. TESTED SATISFACTORY.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,546 hrs · 26,472 cycles

RIGHT UPPER EMERGENCY EXIT SIGN INOPERATIVE ON EXIT DOOR. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,690 hrs · 25,714 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPS CHECKED GOOD AT THIS TIME.

Part: PUMP — LEAKING (RT ENGINE) · airframe 30,620 hrs · 25,640 cycles

HYDRAULIC SYS 1 LO QTY AT CRUISE FL 350. FLIGHT CREW DECLARED EMER. RETURN TO FIELD. UPON PERFORMING LEAK INSPECTION FOUND NR 2 EDP LEAKING. SERVICED SYS 1 HYD IAW AMM 12-13-01. NO LEAKS FOUND. R & R NR 2 EDP IAW AMM 29-10-03. OPERATIONS CHECKED GOOD LEAK CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN) · airframe 30,465 hrs · 25,488 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED MAIN CABIN DOOR ROLLER LUBRICATION IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,013 hrs · 25,063 cycles

CAPTAINS EMER FLASHLIGHT INOPERATIVE. R & R CAPTAINS EMER FLASHLIGHT LAMP IAW CMM 25-60-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,013 hrs · 25,063 cycles

RIGHT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. R & R RT OVERWING EXTERIOR EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: MOUNT — BROKEN (FLASHLIGHT) · airframe 29,991 hrs · 25,048 cycles

AFT CABIN FLASHLIGHT MOUNT BROKEN. R & R AFT FLIGHT ATTENDANT FLASHLIGHT BRACKET ASSEMBLY IAW AMM 33-60-01.

Part: PITOT SYSTEM — CONTAMINATED (NR 1) · airframe 28,629 hrs · 23,793 cycles

LOSS OF CAPTAIN'S AIRSPEED AT FL360 IN ICING CONDITIONS. CAPTAINS SIDE AIRSPEED 40KTS LESS THAN FIRST OFFICER`S AIRSPEED & STBY AIRSPEED. DECLARED EMER, TROUBLESHOOTING AIRSPEED DIFFERENCE IAW FIM 34-22-00-810-816. FOUND WATER IN NR 1 PITOT SYS. DRAINED WATER, OPERATIONS CHECKED GOOD IAW AMM 34-13-00.

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 27,710 hrs · 22,948 cycles

RIGHT VERTICAL STAB FWD SUPPORT ANGLE IS CRACKED IN 2 AREAS AT THE RIVETS ON THE AFT END NEAR FRAME 76. R & R RT VERTICAL STAB FWD SUPPORT ANGLE IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

RIGHT FUSELAGE SKIN IS CRACKED 1/8 INCH AT A RIVET AT THE BASE OF THE VERTICAL STAB FRAME 75 RT. REPAIRED RT FUSELAGE SKIN IAW ERS-EM-53MR-1010.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

CARGO DOOR LIFTING & LOWERING MECHANISM AFT SUPPORT BRACKET HAS SEVERAL CRACKS. R & R AFT SUPPORT BRACKETS IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (LT MLG WW) · airframe 27,710 hrs · 22,948 cycles

LEFT MLG WELL AT FRAME 50 HAS A CRACKED PANEL SUPPORT FLANGE FOR 155QZ. R & R LT CRACKED PANEL SUPPORT FLANGE FOR 155QZ IN LT MLG WELL IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

SHEAR CLIP BELOW FLOOR AT FRAME 72 LT IS CRACKED. R & R SHEAR CLIP BELOW FLOOR AT FRAME 72 IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

CARGO DOOR LIFTING & LOWERING MECHANISM FWD SUPPORT BRACKET IS CRACKED. R & R FWD SUPPORT BRACKET IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 27,710 hrs · 22,948 cycles

LEFT UPPER WING TO FUSELAGE LOWER ATTACHMENT ANGLE ON WING FWD OF SPAR 3 HAS A 1 INCH CRACK ON THE FWD EDGE OF ANGLE. REPAIRED IAW ETN EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

LEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACHMENT ANGLE ON FUSELAGE HAS 1/4 INCH CRACK BETWEEN FRAMES 41 - 42. REPAIRED IAW SRM 53-23-12.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,710 hrs · 22,948 cycles

BAGGAGE DOOR SILL IS CORRODED. R & R BAGGAGE DOOR SILL IAW SRM 51-40-02. RESTORED SURFACE FINISH TO SILL IAW CPM 51-21-05, CPM 51-21-06 & ETN-EM-51-091.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,822 hrs · 22,125 cycles

FORWARD CEILING EMER LIGHT AT EXIT ROW INOPERATIVE. R & R NR 6 INVERTER IAW AMM 33-50-11, STEPS 2J & 3I. OPERATIONS GOOD IAW AMM TASK 33-50-00-700-801-A.

Part: ENGINE — FAILED (NR 1) · airframe 26,451 hrs · 21,788 cycles

ENG 1 OUT AT APPROX 11000 FT HEARD A POP & THE ACFT SHUTTERED. EICAS ENG 1 OUT MSG THE ENG NR 1 INDICATION SPOOLED DOWN DID NOT ATTEMPT A RESTART. TRANSFERRED TO NRWC 681-DFW-01944. REMOVED AND REPLACED NR 1 ENGINE IAW WC 71-000-00. LEAK AND OPS CHECKED GOOD IAW NRWC 681-DFW-01944.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,307 hrs · 21,673 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R WITH SERVICEABLE AFT CABIN FLASHLIGHT IAW AMM 33 50 16. OPERATIONS CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,900 hrs · 21,344 cycles

EMERGENCY BATTERIES DEAD. R & R EMERGENCY BATTERY ON ROW 12A IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,899 hrs · 21,343 cycles

EMERGENCY LIGHTING BATTERIES DEAD. R &R FWD WARDROBE EMERGENCY BATTERY IAW AMM 33-50-04 OPERATIONS CHECKED GOOD. REF ITEM NR 1 LOG PAGE 3418170 FOR OTHER BATTERY REPLACEMENT.

Part: BRACKET — CRACKED (FLASHLIGHT) · airframe 25,596 hrs · 21,105 cycles

FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CHARGING BRACKET CRACKED. R & R FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CHARGING BRACKET IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 25,250 hrs · 20,838 cycles

FLIGHT OFFICER`S FLASHLIGHT ON OFF SWITCH BROKEN. R & R FLIGHT OFFICER`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED. MEL RESTORED.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 25,138 hrs · 20,751 cycles

ON FLIGHT 2945 CREW REPORTED ON DESCENT INTO CVG, FUMES WERE SMELT IN COCKPIT, DECLARED EMERGENCY, FUMES BEGAN AT 14000 FEET. COMPLIED WITH AOM PROCEDURES FOR FUMES IN COCKPIT & A/C SMOKE. FCF FOUND SATISFACTORY BY FLIGHT CREW 622752.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 23,874 hrs · 19,742 cycles

DURING MX INSPECTION, FOUND SERVICE DOOR FWD SILL CORRODED. ACFT REMOVED FROM SERVICE. R & R FWD DOOR SILL, DRILLED AND INSTALLED A NEW SILL IAW SRM 51-20-03 AND SRM 51-40-02. ACFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 23,874 hrs · 19,742 cycles

DURING MX INSPECTION, FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. REPAIRED WIRE W716-0008-20 IAW AWM 20-21-00, STEP 4.A.- 4.B.(1-2 ). OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: HOLDER — DAMAGED (FLASHLIGHT) · airframe 23,822 hrs · 19,694 cycles

THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER BOTTOM LATCH WAS LOOSE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FLASHLIGHT AND FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 23,725 hrs · 19,611 cycles

DURING MX INSPECTION FOUND THE F/A FLASHLIGHT CRACKED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FLASHLIGHT ASSY IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,714 hrs · 19,604 cycles

DURING CRUISE, RECEIVED AN EICAS MESSAGE "GEN4 BRNG FAIL', SECONDS LATER A STRONG ODOR BURNING ELECTRICAL WAS NOTICED. NO SMOKE DETECTED. DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED ODOR EVENT TROUBLESHOOTING IAW ETN EM-72-034 COULD NOT DUPLICATE BURNING ODOR. ACFT RELEASED FOR FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT WAS FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 23,711 hrs · 19,601 cycles

THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS BROKEN AT THE ON/OFF SWITCH. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPATIN’S FLASHLIGHT IAW AMM 33-51-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,376 hrs · 19,340 cycles

DURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL WAS CHECK GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 23,230 hrs · 19,227 cycles

DURING MAINTENANCE INSPECTION FOUND THE FRAME 5 DAMAGED JUST BELOW STR 11R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGED FRAME 5 IAW AEA EO EM-53MR-2112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 23,230 hrs · 19,227 cycles

DURING MAINTENANCE INSPECTION FOUND THE SKIN PANEL P/N 145-54052-003 DAMAGE BETWEEN FR 4 AND FR6 JUST BELOW STR 11R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMGED SKIN IAW AEA EO EM-53MR-2112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 23,230 hrs · 19,227 cycles

DURING MAINTENANCE INSPECTION FOUND THE SKIN PANEL 145-35659-001 DAMAGED AT FR6 FWD AND AFT AT STR 11R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGED SKIN IAW AEA EO EM-53MR-2112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 23,230 hrs · 19,227 cycles

DURING MAINTENANCE INSPECTION FOUND THE FRAME 6 DAMAGED JUST BELOW STR 11R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMGED FRAME 6 IAW AEA EO EM-53MR-2112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,379 hrs · 18,545 cycles

ON FLIGHT 3423 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,349 hrs · 18,516 cycles

DURING B INSPECTION FOUND THE AFT CABIN CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN CEILING EMERGENCY LAMP IAW EMB AMM TASK 33-50-08-000-801/33-50-08-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (SPOILER) · airframe 22,205 hrs · 18,403 cycles

ON FLIGHT 3499 THE CREW REPORTED THE SPOILER DID NOT OPEN IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED SPOILER SYSTEM/SPEED BRAKE OPS CHECK IAW AMM 27-63-01 NORMALLY. THE SYSTEM OPERATIONAL CHECK WAS OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,777 hrs · 18,051 cycles

ON FLIGHT 4138 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT CRADLE WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY PER EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,754 hrs · 18,032 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE LEFT OVERWING EMERGENCY LIGHT FAILS TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROWS 5-7) · airframe 21,272 hrs · 17,667 cycles

FLIGHT 2854, CREW REPORTED THE EMERGENCY LIGHTS AT ROWS 5-7 INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,164 hrs · 17,571 cycles

DURING B INSPECTIONS FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,863 hrs · 17,338 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 4,123 hrs · 17,322 cycles

DURING B INSPECTION FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LAMP IAW EMB 145 AMM 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: BATTERY — DISCHARGED (CABIN) · airframe 20,721 hrs · 17,230 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND NO POWER TO LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY AND LIGHT BULB. PART NUMBERS FOR LAMPS: 1317 & 30-2510-3. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (GALLEY) · airframe 20,371 hrs · 16,936 cycles

ON FLIGHT 2881 THE CREW REPORTED THAT UPON TAXI INTO PARKING, A BURNING ODOR WAS NOTICED COMING FROM THE GALLEY AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW FIM 25-31-00. REMOVED AND REPLACED CONNECTOR P8001 IAW WM 25-31-50. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — CHAFED (ELECTRICAL SYS) · airframe 20,267 hrs · 16,865 cycles

DURING MAINTENANCE INSPECTION FOUND CHAFE WIRE 681-110403 COMPLIED WITH SPECIAL REQUEST FOR INSPECTION OR REPLACEMENT OF WIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE W166-8611-22 CHAFED REMOVED AND REPLACED WIRE. THE AIRCRAFT RETURN TO SERVICE.

Part: PRINTED CKT BOARD — DEFECTIVE (CABIN) · airframe 20,240 hrs · 16,836 cycles

ON FLIGHT 2764 THE CREW REPORTED A STRONG ELECTRICAL ODOR BETWEEN ROW 10-12. THE CREW ELECTED TO DIVERT TO SHV AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND SOURCE OF ODOR TO BE PSU 9A CIRCUIT BOARD. REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD ON PSU PANEL AT SEAT 9A IAW EMB-145 AMM 33-25-04. THE OPERATIONAL CHECK WAS GOOD IAW 33-25-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,208 hrs · 16,809 cycles

DURING MAINTENANCE INSPECTION FOUND BOTH OVERWING EXTERNAL EMERGENCY LIGHTS INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER PER MM 33-50-04. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,050 hrs · 16,691 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT UPPER EXTERIOR EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND BATTERY CHARGER NR 4 IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRINTED CKT BOARD — FAULTY (CABIN) · airframe 19,791 hrs · 16,513 cycles

IN CRUSE 7B CALL LIGHT FLICKERED THE STARTED SMOKING AND SMELL /RESET PSU SMOKE AND SMELL DISSIPATED NO EMERGENCY DECLARED. REMOVED AND REPLACED PSU PRINTED CIRCUIT BOARD AT 9BC, 7BC, 8A, AND 9A IAW EMB 145 AMM 33-25-04, OPS CHECK GOOD.

Part: CONNECTOR — SHORTED (CABIN) · airframe 19,771 hrs · 16,595 cycles

BOTH OVERWING EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. FOUND SHORT IN ELECTRICAL CONNECTOR P8562 (RIGHT OVERWING EMERGENCY LIGHT). REMOVED AND REPLACED CONNECTOR AND PINS REF SWPM 20-50-00. OPS CHECK OF LIGHTS GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 19,700 hrs · 16,445 cycles

DURING MAINTENANCE VISIT FOUND THE RIGHT AND LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY FUSE IAW RADIANT CMM 25-60-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,514 hrs · 16,299 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRINTED CKT BOARD — MALFUNCTIONED (CABIN) · airframe 19,460 hrs · 16,257 cycles

ON FLIGHT 3900 THE CREW REPORTED THE FLIGHT ATTENDANT CALL BUTTON LIGHTS FOR ROWS 7, 8, 9, 10 CAME ON UNCOMMANDED FOLLOWED BY REPORTS OF FUMES AND POSSIBLE LIGHT SMOKE. THE LIGHTS REMAINED ON UNTIL AIRCRAFT POWERED DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BURNT PRINTED CIRCUIT BOARD CARD AT SEAT 7BC. REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD CARD IAW EMB MM 33-25-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRINTED CKT BOARD — BURNED (CABIN) · airframe 19,440 hrs · 16,239 cycles

ON FLIGHT 3900 THE CREW REPORTED THE FLIGHT ATTENDANT CALL BUTTON LIGHTS FOR ROWS 7, 8, 9, 10 CAME ON UNCOMMANDED FOLLOWED BY REPORTS OF FUMES AND POSSIBLE LIGHT SMOKE. LIGHTS REMAINED ON UNTIL AIRCRAFT POWERED DOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BURNT PCB CARD AT SEAT 7BC. REMOVED AND REPLACED THE PCB CARD IAW EMB MM 33-25-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,308 hrs · 16,156 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 65 TO HAVE AN EXTRA HOLE UNDER NUT PLATE AT 12 O'CLOCK POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 65 IAW EO EM-53MR-1877. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,308 hrs · 16,156 cycles

DURING MAINTENANCE BASE VISIT FOUND THE BAGGAGE COMPARTMENT DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DOOR SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,308 hrs · 16,156 cycles

DURING INSPECTION, FOUND THE LT OMEGA BEAM CORRODED AT CROSSMEMBER ON FRAME 29. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (LT AILERON) · airframe 19,308 hrs · 16,156 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT AILERON PCA ATTACH FITTING IS GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FITTING IAW EO-EM-27MR-112.-1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,308 hrs · 16,156 cycles

DURING INSPECTION FOUND THE CENTER OMEGA BEAM HAS CORROSION AT CROSSMEMBER ON FRAME 29. REPAIRED CENTER OEMGA BEAM AT FRAME 29 IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (RT AILERON) · airframe 19,308 hrs · 16,156 cycles

DURING INSPECTION, FOUND RIGHT AILERON DAMPER FITTING GOUGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON PCA AND DAMPNER FITTING IAW EO EM-27MR-112

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 18,734 hrs · 15,693 cycles

ON FLIGHT 4176 THE CREW REPORTED THAT WHILE ON APPROACH WHEN LOWERED GEAR HEARD THE DOORS COME OPEN. THE CREW RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THE CREW REPORTED THEY DID NOT HEAR THE GEAR GO DOWN. THE CREW MANUALLY DROPPED THE GEAR. THE CREW DID A FLYBY TO CONFIRM THE GEAR WAS DOWN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — DAMAGED (PSU) · airframe 18,252 hrs · 15,358 cycles

ON FLIGHT 2795 THE CREW REPORTED THAT DURING CRUISE AT 37000 FEET THE FLIGHT ATTENDANT REPORTED SMELLING ELECTRICAL SMOKE COMING FROM THE CABIN. THE FUMES STARTED AFTER THE FLIGHT ATTENDANT CALL BUTTON FROM 8A WAS PRESSED. NO VISIBLE SMOKE WAS PRESENT. THE FLIGHT ATTENDANT CALL BUTTON THEN STARTED TO FLICKER AFTER ABOUT 10 MINUTES AND THE 8A CALL BUTTON BECAME INOPERABLE AND STOPPED WORKING. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO MGM. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND PSU CIRCUIT BOARD DAMAGED. REMOVED AND REPLACED THE PSU CIRCUIT BOARD. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRINTED CKT BOARD — DEFECTIVE (PSU) · airframe 16,549 hrs · 14,111 cycles

ON FLIGHT 4356 THE CREW REPORTED THAT AT CRUISE FLIGHT LEVEL 350 A PUFF OF SMOKE AND ELECTRICAL BURNING ODOR WAS DETECTED OVER SEATS 7A-10A. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO STL. THE CREW TURNED SHED BUS OFF AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERIVCE. FOUND PASSENGER SERVICE UNIT CIRCUIT BOARD FOR SEAT 9A FLIGHT ATTENDANT CALL BURNED. REMOVED AND REPLACED THE PASSENGER SERVICE CALL BUTTON SWITCH ASSEMBLY AND THE PASSENGER SERVICE CIRCUIT BOARDS AT ROWS 7A TO 10A. SECURED THE PASSENGER SERVICE UNIT PANELS AT SEATS 7ABC THROUGH 10ABC AS PER EMB AMM 25-22-05. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 15,870 hrs · 13,582 cycles

ON PS1 CHECK FOR FLIGHT 2762 THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — ODOR (FLASHLIGHT)

ON FLIGHT 2762 THE CREW REPORTED THAT DURING THE CLIMB AND DESCENT DETECTED AN ODOR LIKE BURNING SULFUR. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THAT THE FIRST OFFICER’S FLASHLIGHT HAD A SULFUR ODOR. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW EMB-145 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF ADJUST (CABIN DOOR) · airframe 14,886 hrs · 12,813 cycles

ON FLIGHT 9802 THE CREW REPORTED THAT THE MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. THE LEVER WILL MOVE PART WAY THEN HANGS UP. THE DOOR DOES OPEN FROM OUTSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THAT THE INSIDE HANDLE WAS NOT CONNECTED TO THE LOCKING MECHANISM PROPERLY. ADJUSTED THE INSIDE HANDLE IAW 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT FITTING — CRACKED (AILERONS) · airframe 14,329 hrs · 12,341 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AILERON SUPPORT BRACKET ON THE RIGHT AILERON HAS BEEN CUT IN THE MIDDLE OF THE BRACKET SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED WITH SERVICEABLE BRACKET IAW EMB SRM 51-40-02 AND EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ON DURING DEPLANE, RAN DOWN BATTERIES FOR EMERGENCY LIGHTS. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE REMOVED AND REPLACED NR 1, 3 AND 4 EMERGENCY POWER PACKS AND BATTERIES FOUND NR 2 TO BE OKAY. OPERATIONAL CHECK IAW EMB MM 33-50-00 AND PARTS REPLACED IAW EMB MM 33-50-04. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — STUCK (LAVATORY) · airframe 8,784 hrs · 7,812 cycles

LAV DOOR STUCK CLOSED. REMOVED AND REPLACED LAV DOOR IAW EMB 145 AMM 25-44-01, OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

ABI - FOUND THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT THE DAMAGE. PREPARED A FILLER, DOUBLER, REPAIR PLATE AND TWO SHIMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

RST - FLT 3986 - CREW REPORTED THE EMERGENCY AT COCKPIT STEP TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXIT MARKING SIGN ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

ON FINAL TO ORD WITH FLAPS AT 9 DEGREES AND SPEED BRAKES TRANSFERRING OPEN TO CLOSE, RECEIVED EICAS MESSAGE PITCH TRIM MAIN INOP AND PITCH TRIM BACK UP FAIL. CHECKLIST PROCEDURES FOLLOWED AND MESSAGE CLEARED. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)