N623AE

Part: NONE — NONE · airframe 49,817 hrs · 45,470 cycles

AFT CABIN EMERGENCY FLASHLIGHT CRACKED-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT HOLDING CLAMP IAW ASTRONICS DME CMM 25-60-14.

Part: NONE — NONE · airframe 49,572 hrs · 45,171 cycles

TDMI 623T3367 LH WTFF EMERGENCY LIGHT HOUSING LENS MISSING LOWER SCREWS/NUT PLATES DAMAGED @ 500FC ERS-EM-33DF-035 OPS PTC-C/A-RAR LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-07-000-802-A AND 33-50-07-400-802-A AND ERS-EM-33DF-035 OPS PT C. OPC GOOD. TDMI RESTORED. END.

Part: DISPLAY — FAILED (EICAS) · airframe 49,381 hrs · 44,940 cycles

EICAS WENT BLANK FOR 3 TO 5 SECONDS. SMELLED BURNING ELECTRICAL SMELL ON PRIOR FLIGHT-C/A-RAR EICAS IAW E-145 AMM 34-22-01. OPERATIONAL CHECK GOOD. RAR EICAS BEZEL REF. 34-22-01. FOUND ODOR COMING FROM OLD UNIT. ODOR NO LONGER FOUND IN COCKPIT. A/C OKAY FOR SERVICE. C/W EMB TRIAD WORKSCOPE 9/8/21 REV. O.

Part: LIGHT — INOPERATIVE · airframe 49,104 hrs · 44,628 cycles

OVER THE WING LH EMERGENCY LIGHT INOP-C/A-R&R LH EMERGENCY LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD

Part: PROXIMITY SWITCH — FAILED (CABIN EMER LIGHT) · airframe 48,985 hrs · 44,496 cycles

DURING REMOVE FLOOR PANEL 251HF, EMERGENCY FLOOR PROXIMITY STRIP LIGHT #7 SPLICE BROKEN OFF.-C/A-RAR EMERGENCY FLOOR PROXIMITY STRIP LIGHT #7 REF AMM 33-50-12. OPC GOOD.

Part: BRAKE SYS — UNKNOWN (MLG) · airframe 48,902 hrs · 44,401 cycles

MECH / BRAKE DEGRADE , EMERGENCY DECLARED- BRAKE DEGRADED ON GEAR EXTENSION. C/W FIM TASK 32-41-00 FOUND TO BE A TRANSATORY CONDITION ON BRAKE SYSTEM , NO CMC FAULT FOUND A/C OK FOR SERVICE

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 48,765 hrs · 44,257 cycles

FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR FWD FA EMERGENCY FLASHLIGHT ASSEMBLY IAW ETN-EM-33-059

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,509 hrs · 43,985 cycles

SMOKE/BURNING ODOR (ELEC) IN COCKPIT-C/A-T/S BURNING SMELL IN CKPT PER EMB 145 FIM 21-20-00. SMELL STILL PERSISTS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,007 hrs · 43,536 cycles

FURTHEST AFT CABIN CEILING EMERGENCY LIGHT INOPERABLE. C/A: R & R FURTHEST AFT CABIN CEILING EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-08. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 47,968 hrs · 43,511 cycles

FOUND NR 3 EMERGENCY FLOOR PROXIMITY LIGHT DAMEGED (WIRE BROKEN) DURING REMOVAL OF GASPER FAN. C/A: R & R NR 3 EMERGENCY FLOOR PROXIMITY LIGHT, IAW EMB 145 AMM 33-50-12. OPERATIONS CHECK GOOD.

Part: FLANGE — GOUGED (RT WING TIP) · airframe 47,730 hrs · 43,274 cycles

RT WING TIP ATTACHMENT LOWER FLANGE IS GOUGED. C/A: REMOVED AND REPLACED RT WING TIP ATTACHMENT FLANGE, IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (FRAMES 60-61) · airframe 47,730 hrs · 43,274 cycles

TOILET WASTE VALVE SUPPORT (LAV BUCKET) IS CORRODED. C/A: REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT, IAW EMB 145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (RT OVERWING) · airframe 47,730 hrs · 43,274 cycles

RT OVERWING EXIT LOWER EDGE IS CORRODED AROUND AND UNDER FWD AND AFT BLACK TEFLON PADS. C/A: REMOVED AND REPLACED RT OVERWING EXIT LOWER PROFILE, IAW EMB 145 SRM 51-10-02.

Part: DOOR — CORRODED (LT OVERWING) · airframe 47,730 hrs · 43,274 cycles

LT OVERWING EXIT LOWER EDGE IS CORRODED AROUND AND UNDER FWD AND AFT BLACK TEFLON PADS. C/A: REMOVED AND REPLACED LT OVERWING EXIT LOWER PROFILE, IAW EMB 145 SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 47,730 hrs · 43,274 cycles

LT OMEGA BEAM IS CORRODED AT FR 20. REPAIRED LT OMEGA BEAM, IAW EMB 145 SRM 53-00-10RE.

Part: FRAME — CRACKED (FRM 73) · airframe 47,730 hrs · 43,274 cycles

FRAME 73 IS CRACKED BETWEEN STRINGERS 16R-17R. C/A: REMOVED AND REPLACED LOWER SECTION OF FRAME 73, IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (FRM 72) · airframe 47,730 hrs · 43,274 cycles

FR 72 IS CRACKED IN UPPER RADIUS BETWEEN STGR 16L-17L. C/A: REMOVED AND REPLACED LOWER SECTION OF FR 72, IAW EMB 145 SRM 51-40-02.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 47,730 hrs · 43,274 cycles

PAX DOOR EMERGENCY LIGHT INOPERABLE. C/A COMPLETE: REPAIRED THE PASSENGER DOOR EMERGENCY LIGHT INDICATING HARNESS, IAW EMB-145 SWPM 20-21-00 S/N 2890B. OPERATIONS CHECKS GOOD, IAW EMB145 AMM 33-50-00.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 47,730 hrs · 43,274 cycles

NR 6 EMERGENCY LIGHT STRIP WIRE CONNECTOR BROKEN UNDER FLOOR. C/A COMPLETE: REPAIRED NR 6 EMERGENCY LIGHT STRIP CONNECTOR, IAW EMB-145 SWPM 20-50-01. SEE NRTC E810792 FOR OPERATIONS CHECK

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 47,730 hrs · 43,274 cycles

NR 2 EMERGENCY LIGHT STRIP WIRE CONECTOR BROKEN UNDER FLOOR. C/A COMPLETE: REPAIRED NR 2 EMERGENCY LIGHT STRIP CONNECTOR, IAW EMB-145 SWPM 20-50-01. SEE NRTC E810792 FOR OPERATIONS CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,730 hrs · 43,274 cycles

CEILING PANEL 233 BLC EMERGENCY LIGHT INOPERABLE. C/A COMPLETE: REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY AND CHARGING ASSEMBLY, IAW ENVOY WORK CARD 33-700-19. SEE NRTC E819046 FOR FNC CHECK.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 47,649 hrs · 43,218 cycles

LH AFT OVER WING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE-C/A-REMOVED AND REPLACED LH AFT OVER WING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,257 hrs · 42,801 cycles

EMERGENCY LIGHT STRIPS 2 AND 3 ON CABIN FLOOR ARE INOP-C/A-AFTER INSTALLATION OF THE EMERGENCY EQUIPMENT STOWAGE WHICH CONTAINS THE EMERGENCY LIGHT SWITCH C/W OPERATIONAL CHECK OF THE EMERGENCY STOWAGE IAW AMM 33-50-00. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMEGENCY LIGHT) · airframe 47,191 hrs · 42,751 cycles

FOUND WIRE BROKEN ON #3 FLOOR EMERGENCY LIGHT STRIP-C/A-REMOVED AND REPLACED #3 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPC GOOD

Part: SKIN — CRACKED (FRAMES 9 - 10) · airframe 46,638 hrs · 42,244 cycles

FUSELAGE CRACK BETWEEN FO WINDSHIELD AND DV WINDOW-C/A-REPAIRED UPPER SKIN PANEL I/A/W ENVOY ERS-EM-56MR-162

Part: WINDOW — LEAKING (COCKPIT) · airframe 46,626 hrs · 42,231 cycles

DISCREPANCY: 21-30 AIR CONDITIONINGPRESSURATION CONTROL - WHILE PERFORMING CABIN PRESSURIZATION NOTICED AIR LEAK AT FWD BOTTOM CORNER OF FO'S DV WINDOW, CONFIRMED LEAKING OUT OF CRACK ON OUTSIDE OF FO'S DV WINDOW TO WINDSHIELD FRAME STRAP. MAJOR REPAIR-C/A-REPAIRED FO DV WINDOW TO WINDSHIELD STRAP IAW ERS-EM-56MR-162

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,534 hrs · 42,167 cycles

RH OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVER WING EMERGENCY LIGHT ASSY IAW E145 AMM 30-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 46,168 hrs · 41,808 cycles

EMERGENCY LIGHT MOUNTED IN MAIN PAX DOOR HINGE COVER IS INOP. C/A-REMOVED AND INSTALL LAMP IN MAIN PAX DOOR EMERG LIGHT. REF AMM 33-50-10. OPS CHK GOOD PER AMM TASK 33-50-00-700-801-A/500.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,168 hrs · 41,808 cycles

LT WING EMERGENCY EXIT LIGHT MOUNTED IN PSU COVER IS INOP. C/A-REMOVED AND INSTALL LAMP AT SEAT ROW 12A LT WING EMERG EXIT. REF AMM 33-50-08. OPS CHK GOOD PER AMM TASK 33-50-00-700-801-A/500

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 46,168 hrs · 41,808 cycles

EMERGENCY LIGHT MOUNTED IN SERICE DOOR HINGE COVER IS INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,962 hrs · 41,663 cycles

AFTER LANDING STRONG SMELL OF OIL IN THE COCKPIT. SMELL DISSIPATED AFTER SWITCHING BLEEDS TO APU AND TURNING OFF RECIRCULATING FAN. TRANSFERRED TO NRWC #623-MIA-03121-C/A-COMPLIED WITH ETN-EM-72-034 . NO SMELL OF OIL NOTED DURING TEST. C/W FIM TASK 21-20-00-810-803-A.NO SMELL OF OIL NOTED DURING TEST. PERFORMED GVI INSPECTION USING A ULTRAVIOLET LIGHT ON LEFT & RIGHT ENGINES. NO SIGNS OF OIL LEAKAGE NOTED AT THIS TIME, IAW RRMM 72-00-00-200-802.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,758 hrs · 41,458 cycles

REF LGPG 4545587-2 TERRAIN AURAL WARNING MSG RANDOMLY CLIMBING OUT OF 6000FT UP TO ALTITUDE,DESENDING-TERRAIN MSG PERSISTED AND SINK RATE MSG ON APPROACH, ERRONEOUS MINIMUM CALL. AIRCRAFT REQ. INSPECTION FOR FERRY FLT. C/A-THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLT AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLT.

Part: SWITCH — FAILED (NR 1 A/C PACK) · airframe 45,548 hrs · 41,250 cycles

PACK #1 OVERLOAD-C/A-FLIGHT CREW PLACARDED PACK # 1 AUTH # 050917D-C MEL 21-28 MOC # 607040. T/S PER FIM 21-51-00-810-801. REMOVED AND DREPLACED PACK 1 OVER PRESSURE SWITCH AND OVERTEMP SWITCH IAW AMM 21-51-06 AND 21-51-08. OPC GOOD IAW 21-51-00. MEL RESTORED. NO M PROCEDURES APPLICABLE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,135 hrs · 40,850 cycles

ROW 12 OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED ROW 12 AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD NO DEFECTS NOTED. END.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 44,839 hrs · 40,525 cycles

SUPPLEMENTAL AFTER TAKEOFF LG/LEVER DISAGREE ON EICAS GEAR WOULD NOT RETRACT. C/A-ON INITIAL POWER UP, LG AIR/GND FAIL CAUTION MSG WAS DISPLAYED ON EICAS. CHECKED CMC MSGS IAW AMM 45-45-00. NO RELATED CMC MSGS NOTED. CHECKED LANDING GEAR PROXIMITY SWITCHES IAW AMM 32-63-05. ON GROUND ALL SWITCHES CHECKED GOOD. JACKED A/C IAW AMM 07-10-00. GEAR WOULD NOT RETRACT WHEN TRIED IAW AMM 32-30-00. NOSE LANDING GEAR PROXIMITY SWITCH WAS FOUND FAILED WITH A/C WEIGHT OFF WHEELS. REMOVED AND REPLACED NLG WOW PROX SWITCH IAW AMM 32-63-05. LG AIR/GND FAIL CAUTION MSG NO LONGER DISPLAYED. PERFORMED MULTIPLE LANDING GEAR EXTENSION AND RETRACTION CHECKS IAW AMM 32-30-00. ALL OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. RAR NOSE LANDING GEAR WOW PROXIMITY SWITCH IAW AMM 32-63-05. PERFORMED MULTIPLE RETRACTION CHECKS IAW AMM 32-30-00. ALL OPS CHECKS GOOD. NO DEFECTS NOTED.

Part: GCU — FAILED (NR 4) · airframe 44,560 hrs · 40,310 cycles

GEN1-4 OFF BUS EICAS MESSAGE DISPLAYED INTERMITTENTLY THEN RETURNED TO GEN 1 OFF BUS WHICH IS NORMAL CONDITION DUE TO CURRENT MEL. REMOVED AND REPLACED NR 4 GCU IAW AMM 24-31-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 44,221 hrs · 39,965 cycles

LT OVER WING EMERGENCY LIGHT INOP. -C/A-REMOVED AND REPLACED OVER WING EMERGENCY LIGHT BULB IAW AMM 33-50-10 OPS CHECK GOOD IAW AMM 33-50-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 44,170 hrs · 39,907 cycles

ON PS-1 CHECK FOUND CABIN GALLEY CEILING EMERGENCY EXIT LOCATOR SIGN INOP. FOUND NR 1 DC/AC INVERTER TO BE CAUSING LIGHT TO BE INOP. REMOVED AND REPLACED NR 1 DC/AC INVERTER IAW AMM 33-50-11-04. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,111 hrs · 38,959 cycles

RIGHT EMERGENCY DOOR FLOOD LIGHT IS INOPERATIVE. R & R THE FLOOD LIGHT BULB, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 43-44) · airframe 43,259 hrs · 38,755 cycles

LEFT OMEGA BEAM IS CORRODED UNDER CROSSBEAM, BETWEEN FRAMES 43 - 44. REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · airframe 42,972 hrs · 38,843 cycles

LEFT OMEGA BEAM IS CORRODED UNDER CROSSBEAM BETWEEN FRAMES 58 - 59. REPAIRED THE OMEGA BEAM.

Part: SIDEWALL SUPPORT — CORRODED (FRAMES 58-59) · airframe 42,972 hrs · 38,843 cycles

LEFT OMEGA SIDEWALL IS CORRODED BETWEEN FRAMES 58 - 59 ABOVE THE CROSSBEAM. REPAIRED THE OMEGA SIDEWALL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 49-50) · airframe 43,259 hrs · 38,755 cycles

CENTER OMEGA BEAM IS CORRODED UNDER CROSSBEAM BETWEEN FR49 - 50. REPAIRED THE OMEGA BEAM.

Part: MOUNT — CRACKED (RT ENGINE) · airframe 43,259 hrs · 38,755 cycles

RIGHT ENGINE FWD YOKE LOWER FWD FITTING CRACKED. R & R THE RT ENGINE FWD YOKE LOWER FWD FITTING.

Part: ACM — SEIZED (RIGHT) · airframe 42,250 hrs · 38,188 cycles

LIGHT BURNING SMELL THROUGHOUT CABIN AT 12000' ON DEPARTURE. SMELL DISSIPATED ON APPROACH BACK TO DEPARTURE. UPON FURTHER INSPECTION FOUND NR 2 PACK ACM SEIZED. R & R NR 2 ACM OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,918 hrs · 37,870 cycles

MAIN DOOR EXTERIOR FLOOD LIGHT NR 1 LOCATED ON BOTTOM OF PLUG DOOR HINGE IS INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,808 hrs · 36,940 cycles

EMERGENCY EXIT SIGN AT GALLEY WALL IS INOPERATIVE. R & R THE BATTERY POWER SUPPLY AND OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,808 hrs · 36,940 cycles

SERVICE DOOR EMERGENCY EXIT SIGN IS INOPERATIVE. R & R THE EMERGENCY BATTERY POWER SUPPLY AND OPS CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 40,105 hrs · 36,381 cycles

EMERGENCY LIGHT ABOVE SERVICE DOOR, SERVICE DOOR EMERGENCY EXIT MARKER NR 12 INOPERATIVE. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,372 hrs · 35,784 cycles

PASSENGER DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT NR 1 BULB. OPS CHECK GOOD.

Part: ACM — LOCKED (NR 2) · airframe 39,135 hrs · 35,592 cycles

CREW REPORTED SMOKE IN THE CABIN. COMPLIED WITH FIM TASK 21-20-00 FOUND FAULTY NR 2 COOLING TURBINE TO BE THE SOURCE OF SMOKE. DEFERRED PACK NR 2. R & R AIR CYCLE MACHINE. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,010 hrs · 35,488 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 IS INOPERATIVE. R & R SERVICE DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,010 hrs · 35,488 cycles

PASSENGER DOOR EMERGENCY FLOOD LIGHT NR 1 IS INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 38,488 hrs · 35,042 cycles

TRAILING EDGE DELAMINATION ON UPPER & LOWER SKIN LT INBD FLAP. REPAIRED IAW ERS-EM - 57MR-481.

Part: FITTING — CORRODED (FUSELAGE) · airframe 38,485 hrs · 35,039 cycles

DURING INSPECTION, QA FOUND FRAME 65 SHEAR CLIP CORRODED. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR TO FRAME 65 SHEAR CLIP IAW SRM 53-31-04 SECTION 4F. REPAIR PART, SHEAR CLIP PN 145-25175-001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,485 hrs · 35,039 cycles

WHILE RE-EVALUATING ADL 64 & 16, FOUND 2 DENTS WITH CREASES BETWEEN FRAME 19 - 20, STRINGER 11L - 15L. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION. PERFORMED PERMANENT REPAIR ON 2 DENTS WITH CREASES BETWEEN FRAME 19 - 20 & STRINGER 11L - 15L IAW ERS-EM-53MR-1405. ACFT WILL BE RETURNED TO SERVICE AFTER INSPECTION. REPAIR MATERIALS, DOUBLER AL2024-T3 0.050", FILLER AL2024T-3 0.080".

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,485 hrs · 35,040 cycles

DURING INSPECTION, QA FOUND 2 CRACKS ON LT REAR FUSELAGE I SKIN AT FRAME 75 ABOVE AND BELOW STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKS ON LT REAR FUSELAGE I SKIN AT FRAME 75 ABOVE & BELOW STRINGER 2L IAW ERS-EM-53MR-1420. REPAIR MATERIAL, DOUBLER ALCLAD 2024-T3, 0.080, FILLER ALCLAD 2024-T3, 0.063, ANGLE ALCLAD 2024-T3, 0.050, SHIM ACLAD 2024-T3-0.032.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,485 hrs · 35,040 cycles

DURING INSPECTION, QA FOUND 2 CRACKS ON RT REAR FUSELAGE I SKIN AT FRAME 75 BELOW STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKS ON RT REAR FUSELAGE I SKIN AT FRAME 75 BELOW STRINGER 2R IAW ERS-EM-53MR-1419. REPAIR MATERIAL, DOUBLER ALCLAD 2024-T3, 0.080, FILLER ALCLAD 2024-T3, 0.063, ANGLE ALCLAD 2024-T3 0.050, SHIM ACLAD 2024-T3-0.032.

Part: FITTING — CRACKED (LT WING) · airframe 38,485 hrs · 35,040 cycles

DURING INSPECTION, QA FOUND THE LT WING REAR SIDE BRACE FITTING REINFORCEMENT BETWEEN RIB 3 & RIB 4 TO BE CRACKED ON THE OTBD SIDE OF RIB 3. AIRCRAFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. R & R THE LT WING REAR SIDE BRACE FITTING REINFORCEMENT BETWEEN RIB 3 & 4 IAW SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,485 hrs · 35,039 cycles

DURING INSPECTION, QA FOUND CORROSION ON FRAME 65 AROUND TWO NUTPLATE HOLES ABOVE LT FLOOR SUPPORT. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR TO CORRODED NUTPLATE HOLES ON FRAME 65 ABOVE LT FLOOR SUPPORT IAW ERS-EM-53MR-1396. REPAIR DOUBLER 2024T3 .050".

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,484 hrs · 35,038 cycles

CENTER FLOORBEAM LT ANGLE IS CRACKED BELOW GUSSET. R & R CTR FLOORBEAM LT ANGLE BELOW GUSSET IAW SRM 51-40-02. SEE TURNOVER FOR DETAILS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,484 hrs · 35,038 cycles

LEFT FLOORBEAM INBD & OTBD ANGLES ARE CRACKED & BROKEN BELOW GUSSET. INSTALLED NEW SERVICEABLE LT FLOORBEAM INBD AND OTBD ANGLES BELOW GUSSET IAW SRM 51-40-02 & SRM 51-20-01.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 38,484 hrs · 35,038 cycles

RIGHT OVERWING EMER LIGHT CONNECTOR P8562 BROKEN. R & R ADAPTER PART OF CONNECTOR ON RT OVERWING EMER LIGHT CONNECTOR P8562 IAW SWPM 20-50-01. OPERATIONS CHECKED GOOD. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,484 hrs · 35,038 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 1/2 INCH IN LENGTH. FREQ=400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100, 100-500 KHZ PROBE. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1420. SEE TURNOVER FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,484 hrs · 35,038 cycles

FRAME 65 HAS CORROSION AROUND NUTPLATE HOLES AT CARGO DOOR GUIDE PLATE. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1396. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,484 hrs · 35,038 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75 AT FIRST & SECOND FASTENERS BELOW STRINGER 2R. CRACK IS APPROX 1/4 INCH IN LENGTH. FREQ=400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100, 100-500 KHZ PROBE. PERFORMED REPAIR ON RT FUSELAGE SKIN CRACK AT FRAME 75, STRINGER 2R IAW ERS-EM-53MR-1419. SEE TURNOVER FOR DETAILS.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 38,484 hrs · 35,038 cycles

BROKEN ELEC CONNECTOR ON LT EMER LIGHT ON ACFT UNDER FWD FUSELAGE FAIRING. R & R ELEC CONNECTOR FOR LT EMER LIGHT ON ACFT UNDER FWD FUSELAGE FAIRING P08561 IAW SWPM 20-50-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,484 hrs · 35,038 cycles

THE FWD OVERWING EMER LIGHT ON THE RT WING DOES NOT ILLUMINATE. R & R BATTERY POWER SUPPLY & BATTERY POWERING THE FWD OVERWING EMER LIGHT ON THE RT WING IAW AMM 33-50-04 & WC 33-700-19. EMER LIGHT OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,327 hrs · 34,874 cycles

EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERATIVE. R & R EMER EXIT SIGN LIGHT ABOVE SERVICE DOOR IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: CONTACT — DEFECTIVE (CABIN) · airframe 38,327 hrs · 34,874 cycles

CEILING EMER LIGHT EXIT SIGN AT FWD OVERWING AISLE POSITION INOPERATIVE. REPLACED CONTACT AT SPLICE SP9209 IAW SWPM 20-50-01. EMER LIGHT OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,807 hrs · 34,318 cycles

WHILE PERFORMING PS 2 INSPECTION FOUND EMERGENCY LIGHT NR 8, AFT CABIN INOPERATIVE. REPLACED THE ELECTRICAL CONNECTORS IAW SWPM-2430-20-50-00. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 37,427 hrs · 33,953 cycles

FLIGHT ATTENDANT'S FLASHLIGHT HOLDER BROKEN, WILL NOT HOLD FLASHLIGHT. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: NUT PLATE — BROKEN (EXTERIOR LIGHT) · airframe 36,080 hrs · 32,807 cycles

LEFT FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY HAS BROKEN NUTPLATES. R & R LT FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,080 hrs · 32,807 cycles

LEFT FWD WING EXT EMERGENCY LIGHT INOPERATIVE. AFTER T/S R & R NR 1 EMERGENCY LIGHT CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,031 hrs · 32,769 cycles

NR 2 EMERGENCY BATTERY REPLACED DUE TO CONNECTED EMERGENCY LIGHTING INOPERATIVE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,031 hrs · 32,769 cycles

NR 2 EMERGENCY BATTERY REPLACED DUE TO CONNECTED EMERGENCY LIGHTING INOPERATIVE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 35,641 hrs · 32,468 cycles

EMERGENCY LIGHT INOPERATIVE AT GALLEY CABIN PARTITION WALL. SECURED ELEC CONNECTOR FOR EXIT IDENTIFIER SIGN AT GALLEY, CABIN PARTITION IAW AMM 33-50-13 STEP I 3 B. OPERATIONS CHECKED GOOD.

Part: SEAL — DAMAGED (NR 1 ENGINE) · airframe 35,269 hrs · 32,161 cycles

FIRST OFFICER FOUND SMOKE COMING FROM THE NR 1 ENG TAIL PIPE, SHUTDOWN FOR MORE THAN 5 MINUTES. R & R AGB BREATHER SEAL & LPT SHAFT PLUG WITHIN 50 FHS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,900 hrs · 31,857 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT 3BC INOPERATIVE. R & R THE AISLE EMERGENCY LIGHT BULB AT SEAT ROW 3 IAW EMB-145 AMM 33-50-08. OPERATIONS TESTED GOOD. USED A BULB FROM THE SPARE BULB KIT.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 34,799 hrs · 31,771 cycles

CREW REPORTED DURING CLIMB ABOVE FL270, NR 1 ENGINE ROLLED BACK TWICE LOSING 10 PERCENT N1, WOULD NOT ACCELERATE AT CRUISE ALTITUDE. THRUST WAS IN DETENT AND AT FULL POWER, THRUST LEVERS WERE NOT LOOSE, CRUISE ALT FL 370. ALL ENGINE INDICATIONS REMAINED IN GREEN RANGE. NR 1 FADECS DID NOT ALTERNATE. AFTER LANDING NR 1 ENGINE SHORT DISP EICAS MESSAGE. RETURNED TO DEPARTURE AND DID NOT DECLARE AN EMERGENCY DUE TO THE ENGINE CONTINUED TO OPERATE NORMALLY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD AND FOUND BIT 27 THAT RECORD E1 FADEC A FAIL. R & R THE FADEC A IAW AMM 73-22-01. THE OPS CHECK WAS GOOD. NO MESSAGE FOR SHORT DISP NOTED THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 34,596 hrs · 31,617 cycles

RIGHT OVER WING EMERGENCY LIGHT IS INOPERATIVE. R & R RIGHT OVER WING EMERGENCY LIGHT IAW AMM33-50-07. OPS CHECK IS GOOD.

Part: LIGHT — WRONG PART (CABIN) · airframe 34,517 hrs · 31,549 cycles

LEFT NR 8 EMERGENCY LIGHT STRIP, WRONG PN INSTALLED. R & R LT NR 8 EMERGENCY LIGHT STRIP IAW AMM 33-50-1.

Part: CHANNEL — GOUGED (FUSELAGE) · airframe 34,545 hrs · 31,575 cycles

CARGO CENTER BEAM DAMAGED AROUND NUTPLATE HOLE FWD OF FR 73. REPAIRED CARGO CENTER BEAM AROUND NUTPLATE HOLE FWD OF FR 73 IAW EO EM-53MR-2214.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,545 hrs · 31,575 cycles

INNER FUSELAGE SKIN CORRODED BETWEEN FRAMES 9-10 AND S20-21L. REPAIRED IAW EO-EM-53MR-2211.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,545 hrs · 31,575 cycles

FRAME 65 DENTED AND GOUGED BETWEEN S12-13R. REPAIRED IAW EO-EM-53MR-2212.

Part: FRAME — GOUGED (FUSELAGE) · airframe 34,545 hrs · 31,575 cycles

FR 65 GOUGED BETWEEN STR 12R/13R JUST BELOW STR 12R. PERFORMED REPAIR IAW EO-EM-53MR-2213.

Part: MOUNT — CRACKED (ENGINE) · airframe 34,516 hrs · 31,549 cycles

CRACK ON LT FWD LOWER, FWD ENGINE YOKE INBD SIDE UPPER OTBD RADIUS. PERFORMED REPAIR IAW AEA EO EM-54MR-386.

Part: LIGHT — WRONG PART (CABIN) · airframe 34,517 hrs · 31,549 cycles

NR 8 EMERGENCY LIGHT STRIP INCORRECT PN INSTALLED. R & R NR 8 EMERGENCY LIGHT STRIP IAW EMB 145, AMM 33-50-12. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,517 hrs · 31,549 cycles

LT NR 4 EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED BROKEN WIRE ON LT NR 4 EMERGENCY LIGHT STRIP HARNESS, AIRCRAFT SIDE IAW SWPM 20-21-00. BOW139255 FOR OPS CHECK, TURN OVER FOR DETAILS.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 34,516 hrs · 31,550 cycles

NR 1 AND NR 4 PROXIMITY LIGHT STRIPS HAVE BROKEN CONNECTORS. R & R CONNECTORS IAW WM 90-10-02, AND SWPM 20-00-03.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,517 hrs · 31,549 cycles

BATTERY POWER SUPPLY INOPERATIVE.

Part: LIGHT — BROKEN (CABIN) · airframe 34,517 hrs · 31,549 cycles

EMERGENCY LIGHT NR 7 BROKEN. R & R IAW AMM 33-50-12, STEPS 2.I. AND 3.I.(1) AND (3).

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 34,517 hrs · 31,549 cycles

CO-PILOTS EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS TESTED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,517 hrs · 31,549 cycles

EMERGENCY LIGHT AT MAIN ENTRANCE CEILING PANEL (233 ALC) INOPERATIVE. R & R BATTERY POWER SUPPLY NR 1 IAW AMM 33-50-04. OPS TESTED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,517 hrs · 31,549 cycles

INNER FUSELAGE SKIN CORRODED BETWEEN FRAMES 9-10 AND S20-21L. REPAIRED IAW EO-EM-53MR-2211.

Part: CRADLE — INOPERATIVE (BATTERY) · airframe 34,517 hrs · 31,549 cycles

REMOVE BATTERY HOLDER ASSY, REMOVE BATTERY HOLDER ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,483 hrs · 31,521 cycles

RT EMERGENCY OVERWING LIGHT IS INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,423 hrs · 31,471 cycles

EMERGENCY LIGHT RT OVERWING INOPERATIVE. R & R LAMP IAW AMM 33-50-10, OPS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,178 hrs · 31,262 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R NR 1 EMERGENCY BATTERY AND CHARGER ASSY IAW AMM 33-50-04, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: FLASHLIGHT ASSY — MALFUNCTIONED (FWD CABIN) · airframe 34,158 hrs · 31,247 cycles

F/A REPORTS FLASHLIGHT WORKS BUT IS NOT CHARGING. REPLACED FWD F/A EMERGENCY FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED NORMAL IAW 33-51-01.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 34,155 hrs · 31,245 cycles

F/A REPORTS FLASHLIGHT INOPERATIVE. REPLACED LAMPS, OPS CHECKED GOOD. STD MX PRACTICES.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 33,413 hrs · 30,654 cycles

DURING B INSPECTION FOUND THE LEFT EXIT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXIT OVERWING EMERGENCY LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,276 hrs · 30,549 cycles

ON FLIGHT 2803 THE CREW REPORTED A STRONG AND PUNGENT ODOR IN THE COCKPIT DURING THE TAKEOFF ROLL. THE CREW ELECTED TO MAKE A HIGH SPEED ABORT AROUND 120 KTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH INSP 05-50-16 EMB MM NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF BOTH PACK IAW AMB AMM 21-51-00 WITH APU ON ENG OFF. NUMBER ONE AIR CYCLE MACHINE NEEDED TO BE CHANGED. REMOVED AND REPLACED A PERFECTLY GOOD AIR CYCLE MACHINE AS DIRECTED IAW EMB AMM 21-51-03 AND THE OPERATIONAL CHECK WAS GOOD IAW 21-51-00 AND IAW ETN-EM-72-034. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,093 hrs · 30,410 cycles

DURING B INSPECTION FOUND THE LEFT EXIT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY & BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-19. REMOVED AND REPLACED THE LEFT EXIT OVERWING EMERGENCY LIGHT ASSEMBLY. PART NUMBER 30-2510-3. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 30-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,776 hrs · 30,170 cycles

DURING B INSPECTION FOUND THE AFT CEILING EMERGENCY LIGHT IINOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,737 hrs · 30,140 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT HOLDER IAW EMB 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 31,037 hrs · 28,792 cycles

DURING B INSPECTIONS, FOUND THE OVERWING AISLE CEILING EMERGENCY EXIT LOCATOR SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,467 hrs · 28,405 cycles

DURING B-INSPECTION, FOUND THE EMERGANCY LIGHT AFT SIDE OF GALLEY INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW MM 33-50-15. OPS CHECKED GOOD IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — DETACHED (CABIN) · airframe 30,335 hrs · 28,294 cycles

ON FLIGHT 3443 THE FLIGHT ATTENDANT REPORTED THE EXIT SIGN ADJACENT TO GALLEY WAS DETACHED (CELLING). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CELLING EMERGENCY LIGHT IAW EMB 145 M/M 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 30,276 hrs · 28,235 cycles

ON FLIGHT 3243 THE CREW REPORTED THEY WERE UNABLE TO OPEN THE CABIN DOOR FROM INSIDE. THEY REQUIRED OUTSIDE PERSONNEL TO OPEN THE DOOR. THE LEVER INSIDE ONLY LIFTED PARTIALLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED MAIN DOOR CABLES IAW EMB AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 30,271 hrs · 28,230 cycles

ON FLIGHT 2873 THE CREW REPORTED THE MAIN DOOR WAS VERY DIFFICULT TO OPEN, HAD TO OPEN FROM OUTSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED & LUBED MAIN DOOR. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DEFECTIVE (PAX DOOR) · airframe 30,273 hrs · 28,232 cycles

ON FLIGHT 2787 THE FLIGHT ATTENDANT WAS UNABLE TO OPEN CABIN DOOR AT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN DOOR ROLLERS IAW ETN-EM-53-068R1. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 29,977 hrs · 27,982 cycles

DURING MAINTENANCE INSPECTION FOUND THE SCREW HOLES IN BOTTOM OF SERVICE DOOR ARE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-52MR-301. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,896 hrs · 27,922 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT IN REFERENCE WITH EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,818 hrs · 27,866 cycles

DURING MAINTENANCE BASE INSPECTION FOUND BOTH OVER THE WING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGNCY POWER SUPPLY AND CHARGER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,778 hrs · 27,834 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY ASSEMBLY AND BATTERY CHARGER IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,654 hrs · 27,444 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIB 5 LEFT WING HAS MULTIPLE CRACKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIB 5 ON LEFT WING IAW EO EM-57MR-594. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,739 hrs · 27,808 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY AND BATTERY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 29,731 hrs · 27,802 cycles

ON FLIGHT 2827 THE CREW REPORTED THE FLASHLIGHT BRACKET OVER THE FLIGHT ATTENDANT JUMPSEAT WAS BROKEN. THE FLASHLIGHT WAS NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,780 hrs · 27,780 cycles

DURING MANTENANCE INSPECTION FOUND THE OVERHEAD GALLEY EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE OVERHEAD, CEILING GALLEY EMERGENCY LAMP IAW EMB 145 AMM TASKS 33-50-09-000-801-A & 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,657 hrs · 27,753 cycles

FOR FLIGHT 2881 DURING MAINTENANCE INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND BATTTERY CHARGER IAW W/C 33-700-19 AND W/C 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 28,921 hrs · 57,191 cycles

CONSTANT SMOKE SMELL IN THE BACK AREA OF THE CABIN. BOTH ENGINES RUNNING / APU OFF (DURING TAXI OPS). FOUND BAD LIGHTING BALLAST OVER SEAT 17A. REMOVED AND REPLACED BALLASTS AT 17A AND AT 16A.

Part: LIGHT — INTERMITTENT (RT WING) · airframe 28,538 hrs · 26,908 cycles

ON FLIGHT 2712 THE CREW REPORTED THE RIGHT WING AFT EMERGENCY LIGHT WORKED INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RE-INSTALLED THE SAME BULB IAW EMB 145 AMM 33-50-10. DISCOVERED THAT THE BULB WAS LOOSE IN THE SOCKET. NO NEW PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 28,522 hrs · 26,897 cycles

FLIGHT 2951, MX REPORTED A STRANGE ODOR NEAR THE GALLEY. THE AIRCRAFT WAS REMOVED FROM SERVICE. UPON INSPECTION FOUND THE FORWARD BALLAST AT SEAT 1A TO BE BAD AND CAUSING THE ODOR. REMOVED AND REPLACED BALLAST IAW AMM 33-21-03. OPERATIONAL CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — INOPERATIVE (AHRS) · airframe 27,801 hrs · 26,367 cycles

ON FLIGHT 3644 DURING TAXI THE CREW REPORTED A HOT ELECTRICAL WIRE INSULATION ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ATTITUDE HEADING REFERENCE UNIT FAN IAW AMM 34-21-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,289 hrs · 24,441 cycles

DURING MAINTENANCE BASE VISIT DISCOVERED THE RIGHT OVERHEAD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10-000-801A & 33-50-10-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 25,202 hrs · 24,385 cycles

FOR FLIGHT 3348 FOUND THE LEFT UPPER EMERGENCY EXIT DOOR HATCH LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 INVERTER IAW EMB AMM 33-50-11. THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,070 hrs · 24,260 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER OMEGA BEAM AT FRAME 25 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB 145 SRM 53-00-10 FIGURE 203 SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,647 hrs · 23,923 cycles

DURING PS 2 CHECK FOUND THAT THE EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 7A AND 12A TO BE INOPERABLE. ALSO FOUND THE LOWER EMERGENCY LIGHT EXIT SIGNS ON THE LEFT AND RIGHT EMERGENCY EXIT DOORS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT AC/DC INVERTER IAW EMB 145 AMM 33-50-11. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,311 hrs · 22,787 cycles

DISC - MAINTENANCE FOUND DURING PS/1 CHECK THAT AFT EMERGENCY EXIT SIGN AT ROW 12A INOP. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AND OPERATIONALLY CHECKED GOOD IAW EMBRAER AMM 33-50-13. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,311 hrs · 22,787 cycles

MAINTENANCE FOUND DURING PS-1 CHECK THAT AFT EMERGENCY EXIT SIGN AT ROW 12A INOP. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AND OPERATIONAL CHECKED GOOD IAW AMM 33-50-13. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 23,231 hrs · 22,700 cycles

ON FLIGHT 4264, CREW REPORTED ELECTRICAL ODOR EMANATING AROUND ROW 1 AND THE GALLEY AREA. FLIGHT ATTENDANT TURNED OFF SIDEWALL LIGHTING AND COFFEE URN. ELECTRICAL ODOR DISSIPATED. THERE WAS NO VISIBLE SMOKE. NO OTHER ABNORMALITIES NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BALLAST ABOVE SEAT 2A IAW AMM 33-21-05. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAILED (SEAT8A/12A) · airframe 23,097 hrs · 22,583 cycles

ON FLIGHT 4418 MAINTENANCE REPORTED EMERGENCY FLOOR LIGHTS STRIPS AT SEAT 8A AND 12A INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHTS IAW EMB MM 33-50-12. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,151 hrs · 19,934 cycles

DURING MBV INSPECTION, FOUND TOP SIDE OF FORWARD DIGITAL CORRODED AT FRAME 15. REPAIRED DIGITAL IAW ETA EM-5300-013. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,151 hrs · 19,934 cycles

DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED ON INBOARD SIDE AT CARBON CROSS MEMBER AT FRAME 20. REPAIRED OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW — LEAKING (COCKPIT) · airframe 18,465 hrs · 18,460 cycles

CAPTAIN DV WINDOW SQUEALING THROUGH 20,000 FEET WITH CABIN ALTITUDE 6.8 PSI. RETORQUED FRONT FRONT WINDSHIELD IAW EMB AMM 56-10-01. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — FAILED (EMEGENCY LIGHTS) · airframe 17,824 hrs · 17,869 cycles

FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER THREE EMERGENCY POWER SUPPLY ASSEMBLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 17,711 hrs · 17,770 cycles

FOUND EMERGENCY FLOOR STRIP BETWEEN ROW 8 AND 12 INOPERATIVE, OVERWING EXIT WALL LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER 3 BATTERY POWER SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BALLAST — ODOR (CABIN)

ELECTRICAL SMELL AT SEATS 8A AND 9A. RAI BALLAST AT SEAT 8A. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

RT FWD OB SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

RT OB SEAT TRACK, 2ND ONE AFT, CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

LT OB SEAT TRACK, 4TH ONE AFT, CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

RT IB SEAT TRACK 3RD ONE AFT CORRODED. REMOVE AND REPLACED SEAT TRACK IAW AMM. AIRCRAFT RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (CABIN)

SERVICE DOOR FORWARD SILL CORRODED. REPAIRED SILL IAW SRM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

RT FWD IB SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

LT FWD OB SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

RT IB SEAT TRACK, 2ND ONE AFT, CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. (K)

Part: ANGLE — CORRODED (FUSELAGE)

STIFFENER ON HAT BEAM AFT OF FRAME 20 CORRODED. REMOVED AND REPLACED STIFFENER IAW SRM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

LT IB SEAT TRACK, 3RD ONE AFT CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

LT OB SEAT TRACK 2ND FROM AFT, CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

LT IB SEAT TRACK 2ND ONE AFT CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (SERVICE DOOR)

DURING MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED AREA TO REMOVE CORROSION. FABRICATED 2 INTERNAL DOUBLERS. REPAIR DONE IAW ETN EM 53-036R2. (SW21200500290)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FR 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE OMEGA BEAM. FABRICATED A FILLER AND DOUBLERS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142, REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,806 hrs · 12,306 cycles

RT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED ARA ON THE RT OMEGA BEAM. FABRICATED AN EXTERNAL DOUBLER. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290)

Part: STARTER — BROKEN (NR 1 ENGINE)

FLT 3712 - CVG - DURING TAKEOFF, 500 FT AIR CREW REPORTED E1 FIRE INDICATION FOLLOWED BY FIRE WARNING BELL ABOUT 1.5 MINUTES LATER. FOUND NR 1 ENGINE AIR TURBINE STARTER BROKEN OFF THE MOUNTING PAD SEVERING FLUID LINES IN THE AREA WHICH CAUSED FIRE. NR 1 ENGINE WAS CHANGED DUE OT FIRE DAMAGE TO THE OUTER BYPASS DUCT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LOCKPIN — LACK OF LUBE (COCKPIT)

CMH - FLT 4394 - DURING TAKEOFF, BOTH CAPTAIN AND FIRST OFFICER SEATS SLIDE OFF POSITION. CREW WAS UNABLE TO SET LOCK PIN. MAINTENANCE PERFORMED INSPECTION OF CAPTAINS AND FIRST OFFICERS SEAT LOCKING PIN AND SEAT TRACKS. SEAT TRACKS AND LOCKING PINS WERE CLEANED AND LUBED. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MOTOR — FAILED (NR 2 FLAP DRIVE)

YOW - FLT 4098 - DURING DESCENT, CREW REPORTED A FLAP FAIL MESSAGE WITH FLAPS STUCK AT 1 DEGREE. CREW RESET PER AOM WITH NO HELP. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 FLAP DRIVE MOTOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAT WAS RETURNED TO SERVICE. (M)

Part: WIRE — DAMAGED (CABIN)

HOU - FLT 3786 - DURING CREW PREFLIGHT, THE FLOOR PROXIMITY EMERGENCY LGIHTS FROM ROW 7 TO 10 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A WIRE ON THE FLOOR LIGHT STRIP. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACM — MALFUNCTIONED (A/C BAY)

CLE - FLT 4204 - CREW REPORTED SMOKE IN THE CABIN, DECLARED EMERGENCY AND LANDED IN CLE WITHOUT INCIDENT. RAI RIGHT ACM IAW AMM 21-51-03. OPS CHECKED GOOD. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

ABI - FOUND CARGO DOOR SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED NEW BEAM IAW EMB-145 SRM 145/1142, CHAPTER 51, REV 18) 51-20-03, 51-40-03 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - FOUND STRINGER 19L GOUGED. BLENDED GOUGE. FABRICATED TWO DOUBLER, FOUR SHIMS. REPAIR DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 18, 53-24-02, EMB GST 2298/02A, AND STANDARD SRM PRACTICES. (M)

Part: CLIP — CORRODED (CARGO DOOR)

ABI - FOUND CARGO DOOR SHEAR CLIP CORRODED AT FRAME 68. REMOVED CORROSION BY CUTOUT. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW EMB GST-2231-02, AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMVOED PREVIOUS REPAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 18) 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - FOUND STRINGER 19R GOUGED. BLENDED GOUGE. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53 REV 18, 53-24-02, AND STANDARD SRM PRACTICES. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - FLT 3432 - FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY LIGHTS EXIT SIGN AT THE OVERWING POSITINO IS INOPERATIVE. MAINTENANCE REPAIRED OVERWING EXIT LIGHT BUTTON SWITCH WIRE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — INOPERATIVE (PARKING BRAKE)

DFW - FLT 3681 - DURING TAKEOFF ROLL, CREW WITNESS CONFIG WARNING. RETURNED TO GATE NO FURTHER INCIDENT WERE REPORTED. REMOVED AND REPLACED PARKING BRAKE PRESSURE SWITCH. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

GRR - FLT 3796 - EMERGENCY FLOOR LIGHTING NUMBER 2 AND 3 INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING STRIPS. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

GRR - FLT 3796 - EMERGENCY FLOOR LIGHT OUT AT NR 2 AND NR 3 POSITION. REMOVED AND REPLACED NR 2 AND NR 3 FLOOR PROXIMITY STRIP LIGHTS. OPS CHECK GOOD. (M)

Part: BULB — FAILED (LT WING)

ORD - FLT 4265 - LEFT WING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

ISP - FLT 4245 - BAGGAGE SMOKE INDICATION CAME ON IN-FLIGHT. CREW DISCHARGED FIRE EXTINGUISHERS. INSPECTED BAGGAGE COMPARTMENT AND VERIFIED EVENT AS A FALSE WARNING. ISSUED MEL AGAINST THE BAGGAGE SMOKE DETECTION SYSTEM PER MEL 26-15. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. MEL ITEM RESTORED ON 5-13-99. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 99ZZZX2627. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

ISP - FLT 4245 - BAGGAGE SMOKE INDICATION CAME ON IN-FLIGHT. CREW DISCHARGED FIRE EXTINGUISHERS. INSPECTED BAGGAGE COMPARTMENT AND VERIFIED EVENT AS A FALSE WARNING. ISSUED MEL AGAINST THE BAGGAGE SMOKE DETECTION SYSTEM PER MEL 26-15. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. MEL ITEM RESTORED ON 5-13-99. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA991235.