N675AE

Part: NONE — NONE · airframe 40,426 hrs · 36,205 cycles

LH OVERWING EMERGENCY LIGHT INTERMITTENT-C/A-FOUND LH OVERWING EMERGENCY LIGHT BULB SOCKET DAMAGED. RAR LH OVERWING EMERGENCY LIGHT HOUSING IAW EMB 145 AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: NONE — NONE · airframe 40,145 hrs · 35,870 cycles

AFT EMERGENCY FLASHLIGHT INOP. MEL 2532 - AUTH# 10-100M-C ORIGINAL LOGPAGE 4755585 ITEM 1-C/A-RAR EMERGENCY AFT FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD. MEL RESTORED. END

Part: NONE — NONE · airframe 40,114 hrs · 35,835 cycles

AFT LAV FLASHLIGHT HOLDER BROKEN-C/A-DEFERRED AFT LAV FLASHLIGHT HOLDER BROKEN AUTH#100100M-C EXP.10/17/21 REF. MEL 25-32

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,904 hrs · 35,592 cycles

SEAT 12A OVERWING EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM 33-50-07. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,550 hrs · 35,183 cycles

AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A NO FIX. RAR OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-07-000-802-A AND 33-50-07-400-802-A. OPC GOOD. END

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,431 hrs · 35,029 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 39,393 hrs · 34,993 cycles

FORWARD CABIN EMERGENCY FLASHLIGHT HAS BROKEN HOLDER.-C/A-RAR FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16 AND ETN-EM-33-059. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,367 hrs · 34,965 cycles

SEAT 12A AND ROW 7A AISLE EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A AND 7A AISLE EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 38,910 hrs · 34,517 cycles

LH FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR LH FWD EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10, NO FIX. PERFORMED TROUBLESHOOTING OF EMERGENCVY LIGHTING SYTEM IAW EMB 145 FIM 33-50-00 AND EMB 145 WM 33-50-50. RAR #1 EMERGENCY LIGHTING BATTERY PACK AND CHARGER IAW EMB 145 AMM 33-50-04. OPC GOOD

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 38,733 hrs · 34,334 cycles

LAV SMOKE AT GATE. C/A: PERFORMED OPERATIONAL TEST OF LAV SMOKE SYSTEM, IAW EMB AMM 26-14-00, MESSAGE CLEARED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,642 hrs · 34,240 cycles

AFT EMERGENCY LIGHT ON LT WING TO FUSELAGE PANEL INOPERABLE. C/A: REMOVED AND REPLACED EMERGENCY LIGHT BULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,546 hrs · 34,159 cycles

DURING PS-2 CHECK FOUND LT EXTERNAL EMERGENCY LIGHT INOPERABLE. C/A: R & R LT EXTERNAL EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,463 hrs · 34,076 cycles

LT AFT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R LT AFT OVERWING EMERGENCY LIGHT LAMP, IAW AMM 33-50-10. OPERATIONS CHECK GOOD, IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,356 hrs · 33,953 cycles

DURING PS-1 FOUND LT EXTERNAL EMERGENCY LIGHT ABOVE WING INOP. C/A-R & R LT EXTERNAL EMERGENCY LIGHT ABOVE WING, IAW EMB 145 AMM 33-50-10.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,287 hrs · 33,876 cycles

COCKPIT FLOOD LIGHT, AISLE LIGHT 1 EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY #1 AND CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,287 hrs · 33,876 cycles

MULITPLE INTERIOR EMERGENCY LIGHTS INOP, AISLE LIGHT 4, AISLE LIGHT 3, FLOOR STRIP 6, 7, 8-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY AND CHARGER ASSEMBLY #4 IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (TERRAIN) · airframe 38,142 hrs · 33,712 cycles

TOO LOW TERRAIN AURAL WARNING INTERMITENTLY IN FLIGHT AT CRUISE FL 240.

Part: SPAR — CRACKED (LT WING) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND THE LH WING SPAR I CRACKED AT RIB 9.-C/A-ACCOMPLISHED REPAR TO LH WING SPAR I AT RIB 9 IAW ERS-EM-57MR-1231.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND CENTER OMEGA BEAM SIDEWALL CORRODED BETWEEN FR 58-59.-C/A-REPAIRED CENTER OMEGA BEAM BETWEEN FR 58-59 IAW EO EM-53MR-1518 PT. B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND LH OMEGA BEAM SIDEWALL CORRODED BETWEEN FR 58-59.-C/A-REPAIRED LH OMEGA BEAM BETWEEN FR 58-59 IAW EO EM-53MR-1518 PT. A.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND THE FR 68 SHEAR CLIP CORRODED AT THE CARGO DOOR LWR SILL.-C/A-PERFORMED PERMANENT REPAIR TO FR 68 SHEAR CLIP AT CARGO DOOR LWR SILL IAW EMB 145 SRM 53-31-04.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LWR SILL CORRODED.-C/A-REMOVED AND REPLACED THE CARGO DOOR LWR SILL IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

DURING HMBV INSPECTION, QC FOUND THE FR 65 SHEAR CLIP CORRODED AT THE CARGO DOOR LWR SILL.-C/A-PERFORMED PERMANENT REPAIR TO FR 65 SHEAR CLIP AT CARGO DOOR LWR SILL IAW EMB 145 SRM 53-31-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

OMEGA BEAM UNDER CENTER LAV FLOOR GUSSET IS CORRODED -C/A-REPAIRED OMEGA BEAM UNDER CTR LAV FLOOR GUSSET IAW EMB 145 SRM 53-24-10RE

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

FR25 IS CRACKED BETWEEN STR 16R-15R-C/A-INSTALLED SPLICE REPAIR ON FR25 BETWEEN STR16R-15R IAW EMB 145 SRM 53-00-04

Part: YOKE — CRACKED (RT PYLON) · airframe 37,942 hrs · 33,511 cycles

RH FWD PYLON LWR YOKE CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698

Part: YOKE — CRACKED (RT FWD) · airframe 37,942 hrs · 33,511 cycles

RIGHT FWD PYLON LOWER YOKE WAS CRACKED. REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698.

Part: FITTING — CRACKED (LT FWD ENG YOKE) · airframe 37,942 hrs · 33,511 cycles

LH ENGINE FWD YOKE LWR FWD FITTING CRACKED. REMOVED AND INSTALLED A SERVICABLE LT FWD YOKE LWR FWD FITTING IAW EO ERS-EM-54MR-698.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 37,942 hrs · 33,511 cycles

CARGO DOOR INNER LWR SKIN SECTION HAS MULTIPLE GOUGES AND CORRODED FASTENER HOLE-C/A-REPAIRED BAGGAGE DOOR INNER LWR SKIN SECTION INSTALLED DOUBLER IAW EMB 145 SRM 52-30-01

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

CROSSBEAM BETWEEN FR 24-25 IS CORRODED.-C/A-COMPLETE:REMOVED AND REPLACED CROSSBEAM BETWEEN FR 24-25 WITH SERVICEABLE PART IAW EMB 145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 37,942 hrs · 33,511 cycles

CROSSBEAM AT FR 20 IS CORRODED.-C/A-COMPLETE:REMOVED AND REPLACED CROSSBEAM AT FR 20 IAW EMB145 SRM 51-40-02, ETN-EM-53-139

Part: WIRE — BROKEN (CABIN) · airframe 37,942 hrs · 33,511 cycles

L/H EMERGENCY LIGHT STRIP #4 HAS A BROKEN WIRE.-C/A-COMPLETE:REPAIRED BROKEN WIRE ON #4 EMERGENCY LIGHT STRIP IAW EMB 145 SWPN 20-21-00. SEE E770710 FOR OPC OF EMERGENCY LIGHTING

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 37,752 hrs · 33,313 cycles

ON PS CHECK FOUND RH FWD EXTERIOR EMG LIGHT INOP-C/A-REMOVED AND REPLACED RH FWD EXTERIOR EMG LIGHT BULB IAW AMM 33-50-10 OPS CHECK GOOD

Part: LIGHT — DAMAGED (FWD CABIN) · airframe 37,734 hrs · 33,294 cycles

FWD, RH PROXIMITY FLOOR STRIP IS DAMAGED.-C/A-REMOVED AND REPLACED RH PROXIMITY STRIP IAW AMM 33-50-12.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 37,734 hrs · 33,294 cycles

MOST AFT PROXIMITY FLOOR LIGHT STRIP ELECTRICAL CONNECTOR BROKE OFF WIRING ON A/C SIDE.-C/A-INSTALLED NEW CONNECTOR IAW SWPM 20-50-01, COMPLIED WITH OPS CHECK IAW AMM 33-50-12 OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,702 hrs · 33,258 cycles

AFT EMERG. CEILING LIGHT IS INOP-C/A-REMOVED AND REPLACED AFT EMERG. CEILING LIGHT LAMP, OPC GOOD, IAW AMM 33-50-08

Part: ACM — FAILED (RIGHT) · airframe 36,946 hrs · 32,530 cycles

AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND A BURNING SMELL. ALSO REPORTED AN ABNORMAL SOUND COMING FROM ENGINE OR ACM. "TRANSFERRED TO NRWC 675-SGF-03210" DD 626301-C/A-T/S PER FIM 21-20-00-810-801-A, REMOVED AND REPLACED RH ACM, HEAT EXCHANGER, CONDENSER/MIXER, OVERPRESSURE SWITCH, DUCT OVERTEMP SWITCH, PACK VALVE OPC GOOD. ACCOMPLSHED INSPECTION OF ACM IAW EO EM-2100-048 AND FOUND CONDENCER MIXER AND HEAT EXCHANGER BAD. REMOVED AND REPLACED RH CONDENSER/MIXER IAW AMM 21-51-04 LEAK CHECK GOOD. REMOVED AND REPLACED OUTLET DUCT ON RH HEAT EXCHANGER IAW AMM 21-51-02. REMOVED AND REPLACED RH PACK VALVE IAW EMB AMM 21-51-01, OPC GOOD IAW EMB AMM 21-51-00. REMOVED AND REPLACED RH PACK OVERPRESSURE AND OVERTEMP SWITCH OPC AND LEAK CHECK GOOD. DOWNLOADED CMC IAW WC 45-900-00. RH HEAT EXCHANGER P/N 816630-2 S/N 200403183. RH CONDENSER MIXER P/N 816650-2 S/N 200212103. AMBIENT TEMPERATURE SENSOR P/N 815289-2 S/N 03935.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 36,414 hrs · 32,097 cycles

EXIT SIGN OVER THE SERVICE DOOR IS BROKEN AND COMING OFF-C/A-REMOVED AND REPLACED EXIT SIGN I/A/W A.M.M. 33-50-15 OPS CHECK NORMAL.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,364 hrs · 32,053 cycles

FROM SEATS 8A TO 11A [FLOOR STRIPS 4&5] FLOOR EMERGENCY PROXIMITY LIGHTS INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER 5 IAW AMM 33-50-11,OPS TEST GOOD.

Part: HOLDER — FAILED (COCKPIT) · airframe 36,353 hrs · 32,036 cycles

FO CHART HOLDER SMOKING-C/A-FOUND SMOKE COMING FROM CHART HOLDER LIGHT AND COCKPIT READING LIGHT CB POPED. RAR CHART HOLDER ASSEMBLY REF AMM 25-12-11. OPS CHECK GOOD WITH NO DEFECTS NOTED.

Part: LIGHT — MALFUNCTIONED (LT OVERWING) · airframe 35,643 hrs · 31,356 cycles

LH OVER-WING EMERGENCY LIGHT IS INOP.-C/A-COMPLIED WITH OPERATIONAL CHECK OF LH OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. NO DEFECT NOTED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 35,637 hrs · 31,351 cycles

FLAP FAIL ON FINAL-C/A-RAI LH FSA #1,#2 ,#3 IAW EMB 145 AMM 27-51-09 AND AMM 27-51-10 OPS TEST GOOD. REMOVED AND REPLACED LH FVS AIRFRAME CONNECTOR J1111 IAW EMB 145 SWPM 20-50-01. RECHECKED WIRING OF LH FVS FOR INSULATION AND CONTINUITY IAW 20-20-03. NO DEFECT NOTED. FLAP SYSTEM OPS CHECK GOOD IAW EMB 145 AMM 27-51-00 AT THIS TIME. RESISTANCE AND INSULATION CHECKS OF LH FTB AND CIRCUIT TEST GOOD. CURRENT DRAW ALSO FOUND TO BE 1.10 A ON BOTH CHANNELS. NO DEFECTS NOTED IAW EMB 145 SWPM 20-20-03.

Part: SHAFT — CONTAMINATED (TE FLAP) · airframe 35,633 hrs · 31,347 cycles

FLAP FAIL ON APPROACH AFTER FCF, 30 MIN IN FLT A/C COLD SOAKED FLAP FAIL ON EICAS UPON SELECTING FLAPS 9 DEGREES. C/A-TROUBLE SHOT IAW FIM 27-51-00-810-804-A FOUND FLAP FLEXIBLE SHAFT SECTION 3 HAVING MOISTURE PENETRATION. REMOVED AND REPLACED CONTACTS 40, 41 ,42, 43, 44, 45, 46, 47, 88, 89, 90, 91 AND 112 AT P1104 IAW SWPM 20-50-01. OPS CHECK GOOD IAW AMM 27-51-00. PERFORMED AMM TASK 27-53-04-700-801-A, ZERO RIG CHECK GOOD REF WORK ITEM TURN OVER. PERFORMED INSPECTION OF LT FLAP FLEXIABLE SHAFT IAW AMM 27-51-00-200-802-A. REMOVED AND REPLACED #3 FLEX SHAFT IAW AMM 27-51-06 OPS TEST GOOD.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 35,335 hrs · 31,087 cycles

AFTER PERFORMING ICE DET TEST IN THE AIR, E1 "OPEN" INSCRIPTION LIGHT EXTINGUISHED...WHICH IS REQ TO BE ILLUMINATED PER MEL 30-11.-C/A-REMOVED AND REPLACED #1 ENGINE ANTI ICE VALVE IAW EMB 145 AMM 30-21-01. AND PERFORMED OPERTIONAL CHECK IAW EMB 145 AMM 30-00-00-700-802-A. NO FAULTS NOTED OPS CHECKS GOOD.

Part: BRAKE ASSY — LEAKING (NR 4) · airframe 33,761 hrs · 29,779 cycles

DURING LANDING, SMOKE REPORTED COMING FROM LEFT LANDING GEAR. FOUND THE NR 4 BRAKE ASSEMBLY LEAKING. REPLACED IAW 32-600-14. FOUND THE NR 4 TIRE WORN TO LIMITS. REPLACED THE 4 TIRE IAW 32-700-11.

Part: ECU — FAILED (TE FLAPS) · airframe 33,486 hrs · 29,552 cycles

DURING APPROACH, A FLAP FAILED MESSAGE WITH FLAPS AT 9 DEGREES. PERFORMED A VISUAL INSPECTION OF THE FLAPS AND FLAP HANDLE. FOUND BOTH TO BE AT 9 DEGREES. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECKED SATISFACTORY. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 33,485 hrs · 29,551 cycles

FLAP FAILED ON APPROACH. REMOVED AND REPLACED THE LT FLAP VELOCITY SENSOR, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,350 hrs · 29,421 cycles

DURING A PS-1 CHECK, FOUND THE LT FRONT AREA OF WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW 33-700-19.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 33,350 hrs · 29,421 cycles

FOUND THE LT WING EMERGENCY LIGHT HOUSING TO BE DAMAGED, R & R THE LT EMERGENCY LIGHT HOUSING IAW AMM 33-50-10, OPS CHECKED GOOD IAW WC 33-700-17. NO DEFECTS NOTED.

Part: CLAMP — LOOSE · airframe 33,214 hrs · 29,301 cycles

FA REPORTS BURNT RUBBER SMELL FROM AFT COCKPIT FA JUMPSEAT AREA ALSO. PERFORMED INSPECTION OF PACK 1 AND 2 IAW AMM 21-51-14-06. RESECURED AND TIGHTENED CLAMPS. NO FURTHER DEFECTS NOTED AT THIS TIME. C/W ETN-EM-72-034 FINDINGS NOTED ON ETN DA 755657. C/W ETN-EM-72-034 . NO SMELL/ ODOR NOTED.

Part: ISIS — FAILED (STDBY ATTITUDE) · airframe 33,051 hrs · 29,160 cycles

STANDBY ATTITUDE INDICATOR FAILED SHORTLY AFTER TAKEOFF. R & R ISIS IAW EMB145 AMM 34-01-01. OPS CHECK GOOD BUT REQUIRES LEAK TEST. REF TO AML PAGE 4195071 ITEM #3

Part: CHARGER — FAILED (CABIN) · airframe 32,827 hrs · 28,926 cycles

EMERGENCY AISLE LIGHT 1, LT FRONT FUSELAGE FAIRING AND COCKPIT FLOOD LIGHT INOP. ALL CONNECTED TO EPSU 1 CHARGER PIN 9. REMOVED AND REPLACED 1 EPSU CHARGER ASSY, OPC GOOD IAW AMM 33-50-04

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,744 hrs · 28,837 cycles

NR 4 AND NR 5 FLOOR EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED NR 3 BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,744 hrs · 28,837 cycles

LAST 2 LT FLOOR PROXIMITY FLOOR LIGHTS WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ON. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY HOLDER AND CHARGER IAW AMM 33-50-04.

Part: WIRE — BROKEN (CABIN) · airframe 32,744 hrs · 28,837 cycles

NR 4 FLOOR EMERGENCY LITE STRIP HAS BROKEN WIRE. REPAIRED NR 4 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00.

Part: CONNECTOR — MISSING (CABIN) · airframe 32,744 hrs · 28,837 cycles

EMERGENCY LIGHT CONNECTOR AT 251DF MISSING (AIRCRAFT SIDE). INSTALLED MISSING CONNECTOR AT FLOOR PANEL 251DF (AIRCRAFT SIDE) SP9115 IAW SWPM 20-21-00.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,744 hrs · 28,837 cycles

SERVICE DOOR CENTER SILL HAS CORROSION AROUND FORWARD AND CENTER NUTPLATE HOLES. REPAIRED SERVICE DOOR CENTER SILL CORROSION AROUND FORWARD AND CENTER NUTPLATE HOLES IAW SRM 53-21-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 32,744 hrs · 28,837 cycles

RT HAT BEAM HAS CORROSION AROUND NUTPLATE AT FRAME 23. REPAIRED R/H HAT BEAM CORROSION AROUND NUTPLATE AT FRAME 23 IAW SRM 53-21-10.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,739 hrs · 28,827 cycles

LEFT FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,726 hrs · 28,812 cycles

FWD EXTERNAL EMERGENCY LIGHT ON LT SIDE INOPERATIVE. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD IAW 33-50-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 32,135 hrs · 28,245 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPAIRED A WIRE SPLICE SP8930 IAW SWPM 20-21-00. THE EMERGENCY LIGHT OPS CHECKED GOOD IAW AMM 33-50-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,853 hrs · 25,822 cycles

DURING PREFLIGHT IT WAS REPORTED THAT THE FWD EMERGENCY LIGHT WAS INOPERATIVE. THE EMERGENCY LIGHT BATTERIES WERE CHARGED, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,853 hrs · 25,822 cycles

DURING PREFLIGHT IT WAS REPORTED THAT THE FWD EMERGENCY LIGHT WAS INOPERATIVE. THE EMERGENCY LIGHT BATTERIES WERE CHARGED, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 28,794 hrs · 24,773 cycles

DURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE BULKHEAD AT 3B WAS OUT, THE 3RD CEILING EMERGENCY LIGHT WAS OUT, AND THE NR 1 OVERWING EMERGENCY EXIT LIGHT WAS ALSO OUT. MAINTENANCE RECONNECTED THE EMERGENCY LOCATOR SIGN AT THE BULKHEAD AT 3B, RECONNECTED THE CONNECTOR PLUG ON THE NR 2 CEILING EMERGENCY LIGHT, OPERATIONALLY TESTED THE NR 1 OVERWING LIGHT WITH NO DEFECTS NOTED, ALL EMERGENCY LIGHTS WERE OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 28,794 hrs · 24,773 cycles

DURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE BULKHEAD AT 3B WAS OUT, THE 3RD CEILING EMERGENCY LIGHT WAS OUT, AND THE NR 1 OVERWING EMERGENCY EXIT LIGHT WAS ALSO OUT. MAINTENANCE RECONNECTED THE EMERGENCY LOCATOR SIGN AT THE BULKHEAD AT 3B, RECONNECTED THE CONNECTOR PLUG ON THE NR 2 CEILING EMERGENCY LIGHT, OPERATIONALLY TESTED THE NR 1 OVERWING LIGHT WITH NO DEFECTS NOTED, ALL EMERGENCY LIGHTS WERE OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CRADLE — OVERHEATED (FLASHLIGHT) · airframe 27,899 hrs · 23,921 cycles

THE CREW REPORTED ELEC SMOKE ODOR EMITTING FROM FLIGHT DECK. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND THE ODOR TO BE COMING FROM THE COCKPIT FLASHLIGHT BRACKET ASSY. R & R THE COCKPIT FLASHLIGHT AND FLASHLIGHT BRACKET ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLASHLIGHT ASSY — OVERHEATED (COCKPIT) · airframe 27,899 hrs · 23,921 cycles

THE CREW REPORTED ELEC SMOKE ODOR EMITTING FROM FLIGHT DECK. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND THE ODOR TO BE COMING FROM THE COCKPIT FLASHLIGHT BRACKET ASSY. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,822 hrs · 23,848 cycles

EMERGENCY FLOOR PROXIMITY LIGHTS AT SEAT Y 7 - 12. BOTH EXIT DIM QUICKLY AFTER BEING TURNED ON. R & R NR 3 EMER BATTERY & CHARGER IAW WC 33-700-19.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

DURING MBV INSPECTION, QA FOUND RT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN IAW ERS-EM-53MR-1193. REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .050 & ANGLE FILLER 2024T3 .032.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QA FOUND A SHEAR CLIP CRACKED AT FRAME 68 BETWEEN STRINGERS 6L - 7L. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REPAIRED SHEAR CLIP IAW ERS-EM-53MR-1191. REPAIR MATERIALS, SHEAR CLIP PN'S 140-04102-601 & 140-04102-603.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

DURING MBV INSPECTION, QA FOUND LAVATORY RT FLOORBEAM CORRODED UNDER GUSSET AT FWD NUTPLATE HOLE. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO LAVATORY RT FLOORBEAM UNDER GUSSET AT FWD NUTPLATE HOLE IAW ERS-EM-53MR-1187. REPAIR MATERIALS, DOUBLER 2024T3 .050.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

DURING MBV INSPECTION, QA FOUND RT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN IAW ERS-EM-53MR-1191. REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .050 & ANGLE FILLER 2024T3 .032.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH A DEFERRAL FOR A CTR FUSELAGE II SKIN DENT AT FRAME 26 BETWEEN STRINGERS 16L - 17L. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. RE-CONTOURED DENT ON CTR FUSELAGE II IAW EO EM-5300-2194 & ERS-EM-53MR-1180.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH A DEFERRAL FOR A CTR FUSELAGE II SKIN DENT AT FRAME 26 BETWEEN STRINGERS 16L - 17L. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. RE-CONTOURED DENT ON CTR FUSELAGE II IAW EO EM-5300-2194 & ERS-EM-53MR-1180.

Part: SKIN — DAMAGED (FRAME 21) · airframe 27,820 hrs · 23,845 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH A PREVIOUSLY REPAIRED LIGHTNING STRIKE AT FRAME 21 BETWEEN STRINGER 17L - 18L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIR TO LIGHTNING STRIKE WAS ACCOMPLISHED IAW SRM 53-21-01. THIS REPAIR IS RECLASSIFIED AS A MAJOR REPAIR IAW ERS-EM-53MR-1178.

Part: FITTING — WORN (RT AILERON) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QA FOUND RT AILERON DAMPENER FITTING HAT BUSHING HOLE WORN. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. R & R RT AILERON DAMPENER FITTING IAW EO EM-27MR-112.

Part: SUPPORT — WORN (RT AILERON) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QA FOUND RT AILERON PCA FITTING HAT BUSHING HOLE WORN. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. R & R RT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QA FOUND A DENT ON CTR FUSELAGE I BETWEEN FRAME 14 - 15 ON STRINGER 14R. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. DENT ON CTR FUSELAGE I BETWEEN FRAME 14 - 15, ON STRINGER 14R ACCEPTED AS IS IAW ERS-EM-53MR-1155.

Part: TORQUE BOX — CHAFED (RT WING) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QC FOUND THE RT WING NR 1 TORQUE BOX UPPER SKIN CHAFED. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. BLENDED AFFECTED AREA ON RT NR 1 TORQUE BOX UPPER SKIN IAW SRM 51-10-03. THIS WAS ACCEPTED AS A PERMANENT REPAIR IAW ERS-EM-57MR-401.

Part: PROFILE — CORRODED (SERVICE DOOR) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QC FOUND THE SERVICE DOOR LOWER & REAR PROFILES HAVE NUTPLATE HOLES CORRODED. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. BLENDED OUT AFFECTED AREAS ON SERVICE DOOR LOWER & REAR PROFILES IAW SRM 51-10-03. THIS WAS ACCEPTED AS A PERMANENT REPAIR IAW ERS-EM-52MR-303.

Part: DOUBLER — CRACKED (ACCESS HATCH) · airframe 27,820 hrs · 23,845 cycles

DURING IMBV INSPECTION, QC FOUND THE COCKPIT UNDERFLOOR ACCESS HATCH 123BL PREVIOUS REPAIR DOUBLER CRACKED UNDER THE HINGE PIN BRACKET. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED A PERMANENT REPAIR ON THE COCKPIT UNDERFLOOR HATCH 123BL IAW ERS-EM-52MR-306.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 27,820 hrs · 23,845 cycles

SERVICE DOOR AFT SIDE LOWER 2 NUTPLATE HOLES CORRODED. SERVICE DOOR AFT SIDE LOWER 2 NUTPLATE HOLES BLENDED, CORROSION ACCEPTED AS IS IAW ERS-EM-52MR-303.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 27,820 hrs · 23,845 cycles

SERVICE DOOR LOWER SIDE HAS 4 NUTPLATE HOLES CORRODED. SERVICE DOOR LOWER SIDE 2 NUTPLATE HOLES BLENDED, CORROSION ACCEPTED AS IS IAW ERS-EM-52MR-303.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,820 hrs · 23,845 cycles

LAVATORY LT FLOORBEAM CORRODED UNDER GUSSET AT FWD NUTPLATE HOLE. PERFORMED PERMANENT REPAIR ON THE LAVATORY LT FLOORBEAM CORRODED UNDER GUSSET AT FWD NUTPLATE HOLE IAW ERS-EM-53MR-1198. SEE TURNOVER FOR DETAILS.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 27,698 hrs · 23,765 cycles

FUEL ON BOARD 6500LBS, LG LEVER DISAGREE EICAS MSG DISPLAYED WITH THE LT MAIN GEAR INDICATOR RED NOSE & RT MAIN UP IN GREEN RATE OF DESCENT 50FPM. R & R LGEU & PERFORMED OPERATIONAL TEST OF LG EXTENTION & RETRACTION IAW AMM 32-32-01 & 32-30-00 AS IAW STEVE. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SKIN — CRACKED (LT WING) · airframe 27,165 hrs · 23,238 cycles

TRANSFERRED FROM AML PAGE 3740057 ITEM 3. FOUND CRACK IN WING SKIN AT MIDDLE ATTACH FITTING FOR INBD SPOILER ON LT WING. COMPLIED WITH PERMANENT REPAIR OF LT WING CRACK REPAIR IAW ERS-EM-57MR-319.

Part: SKIN — CRACKED (LT WING) · airframe 27,163 hrs · 23,237 cycles

FOUND CRACK IN WING SKIN AT MIDDLE ATTACH FITTING FOR INBD SPOILER ON LT WING. TRANSFERRED TO NRWC 675-MQT-01789. COMPLIED WITH PERMANENT REPAIR OF LT WING CRACK REPAIR IAW ERS-EM-57MR-319.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,106 hrs · 23,177 cycles

LEFT WING AFT FUSELAGE EMER LIGHT INOPERATIVE. R & R LT WING AFT FUSELAGE EMER LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: ROLLER — DEFECTIVE (DOOR FRAME) · airframe 26,732 hrs · 22,873 cycles

FLIGHT ATTENDANT NOTED THAT MAIN CABIN DOOR HARD TO OPEN. R & R MAIN DOOR UPPER ADT FRAME J ROLLER IAW AMM 53-21-02. LUBRICATED REMAINING MAIN DOOR FRAME ROLLERS IAW ETN EM-52-048. OPERATIONS CHECKED GOOD.

Part: SHUTTLE VALVE — FAULTY (BRAKE SYSTEM) · airframe 26,693 hrs · 22,828 cycles

EMERGENCY PARKING BRAKE LOW PRESS, WERE NOT ABLE TO SET PARKING BRAKE AFTER PUSH BACK. R & R NR 2 BRAKE SHUTTLE VLV. LEAK CHECK & OPERATIONS CHECKED GOOD IAW ETN-EM-2-236.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,365 hrs · 22,587 cycles

OVERWING AFT EMER LIGHTS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. NO OTHER DEFECTS NOTED. EMER LIGHTING BATTERY PN 2013-1ASMI & SN 68785.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,115 hrs · 22,371 cycles

LEFT & RIGHT AFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. R & R NR 4 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,026 hrs · 22,293 cycles

OUTSIDE OVER THE WING AFT EMER LIGHTS INOPERATIVE ON BOTH SIDES. R & R NR 4 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. EMER BATTERY LIGHT PN 2013-1A, SN 68896.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 25,810 hrs · 22,121 cycles

MAIN CABIN DOOR HARD TO OPEN & CLOSE. PERFORMED MAIN DOOR FRAME ROLLERS LUBRICATION IAW AMM 53-21-02. OPERATIONS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,655 hrs · 21,999 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY PACK & CHARGER ASSEMBLY.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,655 hrs · 21,999 cycles

EMERGENCY CEILING LIGHT AT PAX SEAT 16A INOPERATIVE BULB WAS REPLACED LIGHT STILL NOT WORKING. R & R BATTERY PACK & CHARGER FOR EMERGENCY CEILING LIGHT AT PAX SEAT 16A IAW AMM 33-51-17. IAW NRWC 675-MQT-01527 FOR PART R & R INFORMATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,655 hrs · 21,999 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK & CHARGER FOR LT & RT OVERWING EMERGENCY LIGHTS IAW AMM 33-51-17.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,580 hrs · 21,928 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY POWER SUPPLY & BATTERY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,473 hrs · 21,840 cycles

LEFT CTR FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — LOW PRESSURE · airframe 25,341 hrs · 21,707 cycles

EMERGENCY BRAKE LOW PRESS ON EICAS. CHARGE HYD SYS IAW AMM 29-10-00. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 25,275 hrs · 21,638 cycles

CLIMBING THIS FL 270 FLIGHT ATTENDANT REPORTED SMOKE SMELL IN CABIN. PAX REPORTED SEEING SMOKE ABOVE SEAT 4 BC. ALSO LIGHT BULB BURNED OUT, DECLARED EMERGENCY & LANDED IN STL, LANDING WAS UNDER WEIGHT.

Part: DISPLAY — FAILED (COCKPIT) · airframe 25,219 hrs · 21,583 cycles

DURING DESCENT NOTICED STRONG ELEC SMELL THEN WE LOST THE CAPTAIN`S MFD WITH MFD CB POPPED. R & R CAPTAIN`S SIDE MFD IAW AMM 34-22-02. OPERATIONAL CHECK IAW 34-22-00, FOUND OK, NO FAULT OR DISCREPANCIES FOUND.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,836 hrs · 21,273 cycles

DURING MAINTENANCE INSPECTION FOUND LT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. R & R NR 4 BATTERY POWER SUPPLY IAW EMB MM 33-50-04, CHECKED GOOD.

Part: UNKNOWN — ODOR (FORWARD CABIN) · airframe 24,422 hrs · 20,926 cycles

PASSENGER COMPLAINED OF FOUL ODOR COMING FROM FORWARD CABIN. COULD NOT DETECT ANY FOUL ODOR IN CABIN AT THIS TIME, NO DEFECT NOTED.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 24,318 hrs · 20,838 cycles

MAIN CABIN DOOR HANDLE DIFFICULT TO OPEN AND CLOSE. LUBE AND TESTED MAIN CABIN DOOR IAW AMM 52-18-00, OPS CK GOOD.

Part: HINGE FITTING — CRACKED (E/E BAY DOOR) · airframe 24,073 hrs · 20,633 cycles

REAR ELECTRONICS COMPARTMENT ACCESS HATCH HAS CRACKS UNDER HINGE SUPPORT. REPAIRED IAW AEA EO EM-52MR-369.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 24,073 hrs · 20,633 cycles

LEFT ELEVATOR HAS EVIDENCE OF LIGHTNING STRIKE ON OTBD EDGE NEAR 2ND FROM OTBD STATIC WICK BASE. PERFORMED REPAIR IAW AEA EO-EM-55MR-437.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 24,073 hrs · 20,633 cycles

WIRE HARNESS TO EMERGENCY LIGHT NR 3 HAS DAMAGED INSULATION NEAR THE ELECTRICAL CONNECTOR. REPAIRED WIRE IAW SPWM 20-21-00. OPS TEST GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,969 hrs · 20,530 cycles

BOTH LEFT AND RIGHT AFT OVERWING EXTERNAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. R & R 5 AMP FUSE IN NR 4 EMERGENCY LIGHTING BATTERY CHARGER IAW CMM 25-60-03. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 23,351 hrs · 20,042 cycles

DURING MX INSPECTION, FOUND THE RT OVER WING EMERGENCY LIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 23,064 hrs · 19,810 cycles

FLIGHT 3983, AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 22,776 hrs · 19,568 cycles

FOR FLIGHT 2917 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — INOPERATIVE (AC BAY) · airframe 22,522 hrs · 19,374 cycles

ON FLIGHT 3419 THE CREW REPORTED THAT DURING CRUISE THEY NOTICED AN ELECTRICAL ODOR BRIEFLY ACCOMPANIED BY A FAINT MECHANICAL NOISE IN THE FORWARD PART OF THE CABIN, WITHIN TWO MINUTES THE ODOR SMELL AND NOISE WAS GONE. DURING THE DESCENT THE ODOR REOCCURED. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING FOUND NR 1 PACK SYSTEM ACM INOP AND CAUSING THE SMELL. PACK NR 1 DEFERRED PER MEL 21-29 AUTH#011286D-C. INSPECTED CABIN AND COCKPIT FOR ANY OTHER EVIDENCE OF SMELL AND NO DEFECTS NOTED. REMOVED AND REPLACED THE ACM IAW AMM 21-51-03. MEL RESTORED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,774 hrs · 18,795 cycles

ON FLIGHT 4285 THE CREW REPORTED THE FLASHLIGHT BEHIND THE CAPTAIN'S SEAT STOPPED WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW EMB 145 AMM 33-51-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — LOOSE (STARTER) · airframe 21,541 hrs · 18,600 cycles

FOR FLIGHT 4028 THE CREW REPORTED A HUNG START ON ENGINE NR 2. NO ROTATION ON DRY MOTORING, NO IGNITION. NOTICED THE ODOR OF FUEL IN THE CABIN AND FLIGHT DECK. THE TOWER REPORTING SMOKE FROM ENGINE NR 2. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED LOOSE CONNECTION ON STARTER DUCT. RAN ENGINE WITH CREW AND THE OPERATIONAL CHECK WAS OK PER AMM 80-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (FLASHLIGHT) · airframe 21,475 hrs · 18,548 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED CHARGER AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD PER EMB 145 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,844 hrs · 18,043 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT BULB IAW EMB 145 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,479 hrs · 17,734 cycles

DURING B INSPECTION FOUND THE RIGHT WALL EMERGENCY LIGHT BY ESCAPE HATCH INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11 IAW W/C 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 20,110 hrs · 17,456 cycles

DURING MAINTENANCE INSPECTION FOUND THE BAGGAGE SMOKE DETECTOR WILL NOT TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 1 SMOKE DETECTOR (CARGO ) IAW EMB 145 AMM 26-15-01. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,100 hrs · 17,448 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY STRIP LIGHT AT ROW 14 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY STRIP LIGHT IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 20,098 hrs · 17,444 cycles

ON FLIGHT 2714 THE CREW REPORTED NO BAGGAGE SMOKE INDICATION WHEN DOING FIRE DETECTION TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 CARGO SMOKE DETECTOR IAW EMB 145 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MISINSTALLED (EMERGENCY EXIT) · airframe 19,520 hrs · 17,027 cycles

ON FLIGHT 2964 THE CREW REPORTED THE EMERGENCY EXIT DOOR HANDLE WAS INSTALLED UP SIDE DOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED UPPER HANDLE COVER ON RIGHT EMERGENCY EXIT DOOR IN CORRECT POSITION, REFERENCE EMB 145 AMM 52-20-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THERMOSTAT — DEFECTIVE (BLEED AIR SYS) · airframe 19,396 hrs · 16,953 cycles

ON FLIGHT 3203 THE CREW REPORTED THAT ENTERED ICING AFTER TAKEOFF APPROX 4000 FT SEVERAL EICAS MESSAGE PRESSED PCK 2 VALVE FAIL MESSAGE BLEED 2 VALVE FAIL MESSAGE. WING ANTI-ICE FAIL MSG AS WELL. CYCLE BLEED 2 BUTTON AND EICAS DISPLAYED BLEED 2 OVERTEMP MESSAGE. ON RETURN TO DFW AIRCRAFT WAS OPERATING ON BLEED 1 WITH CROSSBLEED OPEN. ENTER ICING AGAIN AND GOT WING ANTI ICE FAIL SEVERAL TIMES. OPEN ENCRYPTION WERE ALWAYS ON IN ALL FOUR. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 2 FAN AIR CONTROL THERMOSTAT IAW EMB-145 AMM 36-11-06. REMOVED AND REPLACED THE FORWARD HOSE ASSY ON FAN CONTROL THERMOSTAT IAW AMM 20-10-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (NR 1) · airframe 19,216 hrs · 16,822 cycles

ON FLIGHT 2735 THE DURING THE CLIMB THE CREW REPORTED THAT AFTER THE ICE PROTECTION TEST SMOKE CAME IN THE CABIN AND COCKPIT ALONG WITH A LOUD HUM OVER THE WING ROOT AREA. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE IAW AMM 21-51-03. THE OPERATIONAL CHECKS WERE GOOD. NO SMOKE PRESENT (CONFIRMED NR 1 ACM WAS SOURCE OF SMOKE). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 18,100 hrs · 15,975 cycles

ON FLIGHT 4172 THE CREW REPORTED THAT AT 24000 FEET JUST BEFORE DESCENDING FOR LANDING THE CAPTAIN, THE FIRST OFFICER AND THE FLIGHT ATTENDANT AND SOME PASSENGERS SMELLED SOMETHING BURNING FOR ABOUT 4 SECONDS, THEN THE ODOR THEN WENT AWAY AND NEVER RETURNED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND NR 1 PACK TO BE SEIZED. REMOVED AND REPLACED THE AIR CYCLE MACHINE IAW EMB-145 AMM 21-51-0. PARTS REMOVED AND REPLACED: FLEXIBLE COUPLING P/N 815113-7. CLAMPS P/N TSS36S330, SEAL P/N 6969J336. THE OPERATIONAL CHECK WAS GOOD IAW EMB-145 21-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,241 hrs · 13,830 cycles

DURING MAINTENANCE BASE VISIT THE LEFT FORWARD OVERWING AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING UPPER AFT EXTERNAL EMERGENCY EXIT LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VELOCITY SENSOR — MALFUNCTIONED (TE FLAP) · airframe 15,205 hrs · 13,801 cycles

ON FLIGHT 3642 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MIA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT FLAP VELOCITY SENSOR IAW EMB AMM 27-51-12. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 15,063 hrs · 13,692 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY LIGHT FLOOR STRIP CONNECTION TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — CRACKED (ACCESS HATCH) · airframe 14,575 hrs · 13,286 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE COCKPIT UNDER FLOOR, ACCESS HATCH, AND FRAME TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACK IAW EO EM-52MR-235. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,575 hrs · 13,286 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OMEGA BEAM CORRODED AT THE FRAME 24-25 CROSS MEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE OMEGA BEAM WITH A DOUBLER REPAIR IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,575 hrs · 13,286 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 24-25 CROSS MEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM WITH A DOUBLER REPAIR IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (LANDING GEAR) · airframe 13,691 hrs · 12,583 cycles

ON FLIGHT 3891 RIGHT AFTER TAKEOFF THE CREW REPORTED RECEIVED A LANDING GEAR/LEVER DISAGREE WARNING. THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFTER RESETTING THE OVER-RIDE SWITCH, PERFORMED THREE LANDING GEAR EXTENSION AND RETRACTION CYCLES IAW EMB 145 AMM 32-30-00. OPERATIONAL CHECK IS GOOD. NO PARTS REMOVED OR REPLACED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 13,690 hrs · 12,582 cycles

FLT 2796 DURING CLIMBOUT CREW REPORTED A SYSTEM 1 HYD FAILURE & COMPLETE SYS 1 FLUID LOSS. EMERGENCY DECLARED & DIVERTED. ACFT LANDED WITHOUT INCIDENT. ACFT TOWED FROM RUNWAY DUE TO LOSS OF HYD STEERING. ACFT REMOVED FROM SERVICE. R & R O-RING IAW CMM 78-30-54. NO LEAKS NOTED. R & R NR 1 HYD EDP IAW AMM 29-10-03. R & R NR 1 ELECTRIC MOTOR DRIVEN PUMP IAW 29-10-04. OPERATIONAL CHECK AND LEAK CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT)

ON FLIGHT 4176 CREW REPORTED RECEIVING A LAV SMOKE INDICATION ON CLIMB ON EICAS FOLLOWED BY FA REPORT OF SMOKE IN CABIN. CREW RETURNED FOR AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A DETERMINED OIL/SMOKE SMELL TO BE COMING FROM NR 2 ENGINE. R&R NR 2 ENGINE IAW AE MTC 71-000-00. OPS CHECKS AND LEAK CK GOOD. NO DEFECTS FOUND AT THIS TIME. ACFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (MLG)

ON FLIGHT 4402, CREW REPORTED ON TAKEOFF RECEIVED A LANDING GEAR AIR/GND FAIL CAUTION MESSAGE. LANDING GEAR WOULD NOT RETRACT. CREW ELECTED TO RETURN TO FIELD. ACFT REMOVED FROM SERVICE. FOUND CONNECTOR J0775 LOOSE. RE-TIGHTENED, OPERATIONAL CHECKED GOOD IAW AMM 32-30-00 AND AMM 32-34-00. ACFT RETURNED TO SERVICE. (S)

Part: CONNECTOR — LOOSE (MLG)

ON FLIGHT 4402 - CREW REPORTED ON TAKEOFF, RECEIVED A LG AIR/GND FAIL CAUTION MESSAGE. LANDING GEAR WOULD NOT RETRACT AND CREW ELECTED TO RETURN TO FIELD. AIRCRAFT REMOVED FROM SERVICE. FOUND CONNECTOR J0775 LOOSE. RETIGHTENED OPERATIONAL CHECK GOOD IAW AMM 32-30-00 AND AMM 32-34-00. AIRCRAFT RETURNED TO SERVICE. (A)

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 9,418 hrs · 8,841 cycles

ON FLIGHT 4372, CREW REPORTED THEY RETURNED TO FIELD FOR LANDING GEAR AIR GROUND FAIL MESSAGE. GEAR WOULD NOT RETRACT. CMC MESSAGE LAND GEAR PROX SW FAIL. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE GEAR AIR/GROUND PROX SWITCH HAD FAILED REMOVED AND REPLACED PROX SWITCH RETRACTION CHECK GOOD IAW 145 AMM 32-30-00-700-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — CONTAMINATED (A/C PACK)

ORD - FLT 4447 - PASSENGERS AND CREW COMPLAINED OF BURNING SENSATION ALONG WITH A ODOR COMING FROM THE PACKS IN FLIGHT. CLEANED DUCTING OF RESIDUAL OIL FROM APU, APU MEL`D. RETURNED AIRCRAFT TO SERVICE. (M)

Part: ENGINE — CONTAMINATED (APU)

LAVATORY SMOKE DETECTOR WENT OFF DURING AIRCRAFT PUSHBACK. NO REPORT OF EITHER VISUAL SMOKE OR SMOKE ODOR. FOUND APU TURBINE WET WITH OIL. OPENED MEL 49-01, LAV SMOKE DETECTOR. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (AVIONIC BAY) · airframe 1,638 hrs · 1,620 cycles

CREW REPORTED A DUAL PITCH TRIM FAILURE DURING TAXI AFTER LANDING. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502367) (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT, THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO ORD FOR REPAIRS. MAINTENANCE REPLACED THE FORWARD FLOOR STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)