N674RJ

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,164 hrs · 33,070 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT BULB, OPC BAD, IAW EMB AMM 33-50-07

Part: O-RING — LEAKING (BLEED DUCT) · airframe 36,953 hrs · 32,848 cycles

BLEED 1 LEAK INFLIGHT-C/A-REMOVED AND REPLACED BLEED JOINT 29 O-RINGS IAW ETN EM-36-064.

Part: CONTROL VALVE — LEAKING (NR 1 BLEED) · airframe 36,938 hrs · 32,836 cycles

BLD 1 LEAK WARNING MESSAGE PRESENTED W/O ENG 1 RUNNING OR BLD 1 SELECTED OPEN. OCCURED 2X @ GATE-C/A-PERFORMED #1 BLEED LEAK CHECK AS PER EMB145 AMM 36-00-00, FOUND #1 DUAL TEMP. CONTROL VALVE LEAKING. REMOVED AND REPLACED #1 DUAL TEMP CONTROL VALVE AS PER EMB145 AMM 21-60-01. OPC GOOD. LEAK CHECK GOOD.

Part: COUPLING — FAILED (BLEED SYSTEM) · airframe 36,925 hrs · 32,829 cycles

BLD 1 LEAK CLIMBING THROUGH FL180. AIR RETURN TO CMH. WE BURNED OFF THE EXTRA FUEL FOR A NORMAL LANDING. "TRANSFERRED TO NRWC 674-CMH-04717" G. DAVID GOULD JR. 151543-C/A-FOUND COUPLING #12 OM #1 PACK VALVE LEAKING. REMOVED AND REPLACD COUPLING IAW ETN-EM-21-056. OPS AND LEAK CHECK GOOD IAW AMM 21-51-01. OPS CHECK GOOD. NO LEAKS DETECTED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 36,790 hrs · 32,720 cycles

RT UPPER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT OVERWING EMERGENCY LIGHT IAW IAW AMM 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,610 hrs · 32,524 cycles

FOUND INVERTER #1 INOP. C/A-REMOVED AND REPLACED INVERTER #1 IAW AMM 33-50-11. OPS CHECK GOOD.

Part: SHROUD — CRACKED (RT AILERON) · airframe 36,610 hrs · 32,524 cycles

RIGHT WING LOWER AILERON SHROUD ATTACH FLANGE IS CRACKED AND BENT APPROXIMATELY 2 INCHES OUTBOARD OF #3 AILERON HINGE. C/A-C/W REPAIR OF RT WING AILERON LOWER AILERON SHROUD ATTACH FLANGE IAW ERS-EM-57MR-1160.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND FR 65 SHEAR CLIP CORRODED AT LWR END OF CARGO DOOR OPENING. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REMOVED AND REPLACED FR 65 SHEAR CLIP IAW SRM 51-40-02. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND FR 65 CORRODED BELOW LWR CARGO DOOR GUIDE PLATE. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REMOVED AND REPLACED FR 65 IAW SRM 51-40-02. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND 2 CRACKS AROUND RIVETS ON RT REAR FUSELAGE I SKIN AT FR 75 BELOW STR 2R. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED PERMANENT REPAIR TO CRACKS ON RT REAR FUSELAGE I SKIN AT FR 75 BELOW STR 2R IAW SRM 53-31-01-RE REPAIR #11. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. (REPAIR MATERIALS: DOUBLER ALCLAD 2024-T3, 0.080?, FILLER: ALCLAD 2024-T3, 0.063?, ANGLE: ALCLAD 2024-T3, 0.050?, SHIM ALCLAD 2024-T3, 0.032?)

Part: SKIN — DENTED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND A DENT ON UPPER FUSELAGE SKIN BETWEEN FR 68-69, STR 2R-3R. DENT OIL CANNED AFTER RECONTOUR. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED PERMANENT REPAIR TO DENT ON UPPER FUSELAGE SKIN BETWEEN FR 68-69, STR 2R-3R IAW SRM 53-31-01 RE REPAIR # 3. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. (REPAIR MATERIALS: DOUBLER ALCLAD 2024-T3, 0.050?, FILLER: ALCLAD 2024-T3, 0.040?)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND FR 68 SHEAR CLIP CORRODED AT LWR END OF CARGO DOOR OPENING. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REPAIRED FR 68 SHEAR CLIP IAW SRM 53-31-04 RE ITEM 4. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. (REPAIR MATERIAL: SECTION OF SHEAR CLIP P/N 145-25369-603)

Part: SKIN — DAMAGED (RUDDER) · airframe 36,414 hrs · 32,365 cycles

AIRCRAFT ARRIVED FOR HMBV INSPECTION WITH AN OPEN TDMI 674T5564 FOR RUDDER II LT SIDE ELONGATED NUT PLATE HOLE WHERE PROTRACTOR ATTACHES. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED PERMANENT REPAIR ON RUDDER II LT SIDE ELONGATED NUT PLATE HOLE WHERE PROTRACTOR ATTACHES IAW ERS-EM-55MR-771. REPAIR MATERIALS: DOUBLER : AL2024-T3, 0.040? FILLER : AL2024-T3, 0.020?

Part: SKIN — DENTED (CARGO DOOR) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QA FOUND A LARGE DENT ON THE CARGO DOOR SKIN JUST ABOVE HORIZONTAL BEAM 3 JUST AFT OF FWD EDGE. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED A PERMANENT REPAIR ON THE CARGO DOOR LARGE DENT ON SKIN JUST ABOVE HORIZONTAL BEAM 3 JUST AFT OF FWD EDGE IAW ERS-EM-52MR-1002. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. REPAIR MATERIALS: DOUBLER : AL2024-T3 ? 0.063? FILLER: AL2024-T3 - 0.032?

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND THE RT FLOOR BEAM CORRODED AT FR 23 CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED DOUBLER REPAIR TO RT FLOORBEAM AT FR 23 IAW SRM 53-21-10RE FIG 205 SHEET 1. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. / REPAIR MATERIALS: DOUBLER : AL CLAD 2024-T3, 0.050?

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND FRAME 65 ?Z? FRAME CRACKED AT STR 9L. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REPAIRED CRACK ON FRAME 65 Z FRAME IAW ERS-EM-53MR-3825 . AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. (REPAIR MATERIALS: DOUBLER 2024 T3, 0.050?, FILLER 2024 T3, 0.040?)

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LWR SILL CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REMOVED AND REPLACED CARGO DOOR LWR SILL IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,414 hrs · 32,365 cycles

DURING HMBV INSPECTION, QC FOUND THE SERVICE DOOR CENTER SILL CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: STRIP — DAMAGED (CABIN) · airframe 36,414 hrs · 32,365 cycles

FLOOR PROXIMITY LIGHT FILLER STRIPS ARE DAMAGED-C/A-COMPLETE:REMOVED AND REPLACED FLOOR PROXIMITY LIGHT FILLER STRIPS IAW EMB 145 AMM 33-50-12

Part: WIRE — BROKEN (CABIN) · airframe 36,414 hrs · 32,365 cycles

1EA PROX LIGHT WITH ARROWS AND 1EA PROX LIGHT WITH OUT ARROWS HAVE BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 1EA PROX LIGHT WITH ARROWS AND 1EA PROX LIGHT WITH OUT ARROWS IAW EMB 145 AMM 33-50-12 SEE NRTC BOW324322 FOR FINAL INSTALL AND OPS CHECKS

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 36,079 hrs · 32,013 cycles

EMERGENCY LIGHT FLOOR PROXIMITY STRIP 4 AND 5 INOP AND FWD EXIT IDENTIFIER LIGHTS INOP-C/A-T/S PER EMB 145 WM 33-50-50 RAR #3 EMERGENCY BATTERY AND CHARGER IAW ENVOY W/C 33-700-19 NO FIX REMOVED AND REPLACED #5 INVERTER IAW EMB 145 AMM 33-50-11 OPS CHECK GOOD A/C OK FOR SERVICE. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 67810

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,760 hrs · 31,680 cycles

EMERGENCY EXIT MARKING SIGN NEAR PASSENGER DOOR FOUND INOP DURING PS1 CHECK. C/A-REMOVED AND REPLACED EMERGENCY EXIT MARKING SIGN IAW AMM 33-50-14. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,068 hrs · 31,093 cycles

EMERGENCY EXIT SIGN AT FLIGHT ATT SEAT INOP-C/A-T/S WM 33-50-50 FOUND #1 EMERGENCY BATTERY AND CHARGER TO BE BAD REMOVED AND REPLACED IAW W/C 33-700-19 OPC GOOD NO DEFECTS NOTED AT THIS TIME END. BATTERY CHARGER ASSY P/N 11-0049 S/N 13658

Part: LIGHT — NONE (NONE) · airframe 34,946 hrs · 30,965 cycles

PAX DOOR EMERGENCY LT INOP-C/A-PERFORMED OPS CHECK OF PAX DOOR EMERGENCY LT IAW EMB AMM TASK 33-50-00-700-801-A OPS CHECK GOOD

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,463 hrs · 30,530 cycles

CABIN WILL NOT PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION CHECKS OK. REACTIVATED ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. PERFORMED FNC OF PRESSURIZATION CONTROL SYS IN AUTO MODE IAW AMM 21-31-00-802-A. OPS CHECK GOOD AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 34,261 hrs · 30,364 cycles

EMERGENCY LIGHT FLOOR STRIP AT SEAT 1A INOP. REMOVED AND REPLACED NR 2 BATTERY IAW AMM 33-50-04-000-802-A AND 33-50-04-400-802-A AND POWER SUPPLY IAW AMM 33-50-04-000-801-A AND 33-50-04-400-801-A, NO FIX. R&R NR 2 INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 81257.

Part: ACM — ODOR (NR 1) · airframe 31,755 hrs · 28,043 cycles

DURING TAXI, A BURNED RUBBER ODOR COMING FROM COCKPIT AIR CON SYS. REMOVED AND REPLACED THE NR 1 ACM IAW AMM 21-51-03. OPS CHECKED GOOD IAW AMM 21-00-00.

Part: SUPPORT BRACKET — CRACKED (FRAME 20) · airframe 31,623 hrs · 27,917 cycles

SUPPORT BRACKET IS CRACKED AT FRAME 20, STRINGER 3L. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 31,623 hrs · 27,917 cycles

CARGO DOOR HAS CORROSION AROUND TWO NUTPLATES ON FWD FRAME BELOW LOWER GUIDE. PERFORMED A PERMANENT REPAIR IAW ERS-EM-52MR-762.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 31,623 hrs · 27,917 cycles

EMERGENCY LIGHT HAS A DAMAGED WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM TASK 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,623 hrs · 27,917 cycles

NR 2 FLOOR PROXIMITY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 31,421 hrs · 27,754 cycles

BLD 2 VALVE FAIL THEN PHL LANDING A/I INOP. THEN A/I FAIL IN CLOUDS W/ICE COND AT 12000 ON CLIMBOUT. REMOVED AND REPLACED E-2 PRSOV IAW AMM CH 36-11-05 OPS CK GOOD

Part: CRADLE — BROKEN (FA FLASHLIGHT) · airframe 30,722 hrs · 27,125 cycles

FA FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16-000-801-A/400 AND 33-50-16-400-801-A/400 OPS CHECKED GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 30,680 hrs · 27,090 cycles

HYD SYSTEM NR 1 FAILURE IN FLIGHT. HYD NR 1 QUIANTY INDICATOR AMBER FULL SCALE LEFT. RAN PROCEDURE. REMOVED AND REPLACED THE NR 1 EDP IAW AMM 29-10-03, AND PRESSURE LINE. LEAK CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,382 hrs · 26,822 cycles

FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT ASSEMBLY IAW 33-51-01

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 30,180 hrs · 26,648 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R COCKPIT EMERGENCY LIGHT BULB IAW AMM 33-50-05. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,150 hrs · 26,621 cycles

EMERGENCY LIGHTS 2 AND 3 INOPERATIVE. REMOVED AND REPLACED THE NR 2 EPSU IAW AMM 33-50-04. OPS CHECKED GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,134 hrs · 26,603 cycles

SERVICE DOOR EMERGENCY LIGHT IS INTERMITTENT. REMOVED AND REPLACED THE LIGHT SOCKET IAW 33-50-10. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,134 hrs · 26,603 cycles

EXTERNAL OVER THE WING EMERGENCY LIGHT ON RIGHT WING IS INOPERATIVE. REMOVED AND REPLACED AND OPS CHECKED EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: GROUND WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,828 hrs · 26,324 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPS CHECK FAILED, INSPECTED AND FOUND GROUND CONNECTION FOR LAMP TO THE ASSEMBLY TO BE INADEQUATE, CLEANED AND RECONNECTED GROUND CONTACT TERMINAL IAW SWPM 20-13-21-910-802-A, SERVICE DOOR ARM LINER REMOVED AN REINSTALLED IN REFERENCE WITH EMB AMM 25-23-05-000-801-A END

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 29,577 hrs · 26,108 cycles

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

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 29,506 hrs · 26,042 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM TASK 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,642 hrs · 25,292 cycles

RIGHT AFT OVERWING EMER LIGHT INOPERATIVE. RELAMPED RT AFT OVERWING EMER LIGHT IAW AMM 33-50-07. TESTED SATISFACTORY IAW WC 33-700-17.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,564 hrs · 25,219 cycles

EMERGENCY LIGHT ON SERVICE DOOR INOPERATIVE. R & R LAMP IN SERVICE DOOR EMER LIGHT ASSEMBLY IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE I RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE I RT SKIN PANEL IAW SRM 53-21-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-262. ACFT WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II RT SKIN PANEL IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118, ETN-EM-53-206 & ERS-EM-5300-1763. INSTALLED SKIN PN 145-35659-005.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R REAR FUSELAGE I TOP SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118, & ETN-EM-53-263. ACFT WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II CROWN SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II CROWN SKIN PANEL IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-206.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE IV TOP SKIN PANEL IAW SRM 53-24-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-265.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE II TOP SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-263. ACFT WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE I RT SKIN PANEL IAW SRM 53-11-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-235.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE II RT SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-263.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE I LT SKIN PANEL IAW SRM 53-11-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-235.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN, WIPER PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II SKIN IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, CPM 51-21-04, ETN-EM-51--118 & ETN-EM-53-206.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE I LT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE I LT SKIN PANEL IAW SRM 53-21-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R LT STAB UPPER SKIN IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-40-03, 51-20-01, 55-10-01SI, ETN-EM-55-073R2 & ETN-EM-55-074.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE RT STAB UPPER SKIN. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R RT STAB UPPER SKIN IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-40-03, 51-20-01, 55-10-01SI, ETN-EM-55-073R2 & ETN-EM-55-074.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. DURING CTR I LT FUSELAGE SKIN REPLACEMENT, FOUND DAMAGED SHEAR CLIP ON FRAME 23, BETWEEN STRINGER 5L & 6L. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. FABRICATED SHEAR CLIP IAW SRM 51-30-01 & R & R SHEAR CLIP IAW SRM 51-40-0. ACFT WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. REPAIR MATERIAL AL 7475T761 .032.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN PN 145-27270-005. R & R LT ELEVATOR UPPER CTR SKIN PN 145-27270-005 IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06 & ETN EM-51-073 & EM-51-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW EMB SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, & ETN EM-51-073, EM-51-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,450 hrs · 25,109 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03,51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN-EM-55-076.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,150 hrs · 24,808 cycles

GALLEY SERVICE DOOR EMERGENCY LAMP INOPERATIVE. R & R GALLEY SERVICE DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD END.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,089 hrs · 24,757 cycles

LEFT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R LT EXTERNAL OVERWING EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 27,205 hrs · 23,981 cycles

DURING IMBV INSPECTION, QA FOUND A DENT BETWEEN FRAME 68 - 69, ABOVE STRINGER 19R. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. DENT ACCEPTED AS IS IAW ERS-EM-53MR-1104.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 27,205 hrs · 23,981 cycles

DURING IMBV INSPECTION, QA FOUND 5 DENTS & 1 PROTRUSION BETWEEN FRAMES 65 & 70, BETWEEN STRINGERS 18L - 21L. AC FT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. DENTS & PROTRUSION ARE ACCEPTED AS IS IAW ERS-EM-53MR-1104.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 27,205 hrs · 23,981 cycles

SERVICE DOOR INNER FRAME AFT OF LOWER FWD STOP IS CRACKED. PERFORMED PERMANENT REPAIR ON THE SERVICE DOOR INNER FRAME AFT OF LOWER FWD STOP CRACK IAW ERS-EM-52MR-300. SEE TURNOVER FOR DETAILS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,070 hrs · 23,828 cycles

LEFT EXTERNAL WING EMER LAMP INOPERATIVE. R & R LT EXTERNAL WING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: SKIN — DENTED (EMERGENCY EXIT) · airframe 26,829 hrs · 23,615 cycles

PERMANENT REPAIR RT OVERWING EMER EXIT DOOR. PERFORMED PERMANENT REPAIR OF RT PAX CABIN ESCAPE HATCH SKIN DENTS IAW ERS ERS-EM-52DF-212 PART B REV 1 TDMI 674T5213 RESTORED.

Part: TRANSDUCER — FAILED (ANTI-ICE SYS) · airframe 26,724 hrs · 23,530 cycles

SHORTLY AFTER TAKEOFF RECEIVED ENG 2 ANTI-ICE FAIL MSG, FOLLOWED BY NO ICE ANTI-ICE ON MSGE. THEN ANTI-ICE OVR PRESS MSG, THESE CYCLED ON & OFF DURING RETURN FLIGHT. R & R E2 ANTI-ICING PRESS TRANSDUCER & OPERATIONS CHECKED GOOD IAW AMM 30-21-06 & 30-21-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,638 hrs · 23,456 cycles

TRANSFERRED FROM AML PAGE 3667646 ITEM 2. REF ITEM 3 LOG 3667645 AFTER INTERNAL INSPECTION OF DAMAGED AREA FOUND CRACKED FRAME, SEVERAL PULLED RIVETS & DAMAGED SKIN PANEL ON SAME AREA AS EXTERNAL DAMAGE. PERFORMED REPAIR IAW ERS-EM-53MR-847.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,637 hrs · 23,455 cycles

REF ITEM 3 LOG 3667645 AFTER INTERNAL INSPECTION OF DAMAGED AREA FOUND CRACKED FRAME, SEVERAL PULLED RIVETS & DAMAGED SKIN PANEL ON SAME AREA AS EXTERNAL DAMAGE. TRANSFERRED TO NRWC 674-ABI-02296. PERFORMED REPAIR IAW ERS-EM-53MR-847.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 26,579 hrs · 23,405 cycles

LOW SPEED ABORT ON TAKEOFF ROLL THROUGH 40 KTS, SMOKE IN COCKPIT & SMOKE IN CABIN LIGHT GRAY BLUE SMOKE. TRANSFERRED TO NRWC 674-DFW-02281. R & R E1 0 CARBON SEAL IAW RR MM 72-25-25 REFERENCE NRWC 674-DFW-02281.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 25,925 hrs · 22,844 cycles

E1 ANTI-ICE FAIL DURING CLIMB ITT E1 US E2 50 HOTTER E1 PROBLEM. E1 ANTI-ICE FAIL WENT AWAY DURING RETURN. R & R E1 ANTI-ICE VLV IAW AMM 30-21-01 & OPERATIONS CHECKED IAW AMM 30-00-00. OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (SPOILER) · airframe 25,872 hrs · 22,801 cycles

SPOILER FAIL MSG DURING DESCENT. R & R SPOILER CONTROL UNIT IAW AMM 27-63-02. OPERATIONS CHECKED NORMALLY NO FAIL MSGS IAW AMM 27-63-01.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 25,610 hrs · 22,592 cycles

PAX ENTRY DOOR HARD TO OPEN, IT GETS STUCK. CLEANED & LUBED OUTSIDE DOOR HANDLE 52 10 01.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 25,350 hrs · 22,377 cycles

AFT CABIN FLASHLIGHT IS LOOSE IN HOLDER, SAFETY HAZARD. R & R AFT CABIN FLASHLIGHT & CHARGER ASSEMBLY, OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 25,183 hrs · 22,246 cycles

INFLIGHT ON DECENT INTO FWA WE RECEIVED A NR 2 HYD LOW MSG. THE FLUID CONTINUED TO DROP, AOM PROCEDURES WERE APPLIED. ON LANDING WE RECEIVED A HYD 2 PUMP FAIL MSG. R & R E2 EDP IAW AMM 29-10-03. LEAK CHECK PERFORMED IAW MM 72-00-00. OPERATIONS CHECKED GOOD, NO LEAKS NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 24,360 hrs · 21,600 cycles

ON FLIGHT 3162 CREW REPORTED LAVATORY SMOKE, SMOKE IN COCKPIT, SMOKE OUTSIDE AC AFTER LANDING & DECLARED EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED FIM TASK 21-20-00-810-801-A & FIM TASK 21-20-00-810-803-A, NO FAULTS FOUND. CW ETN-EM-72-034, NO ODORS DETECTED, NO FAULTS FOUND. INSPECTED PACK DUCTS IAW EMB AMM 21-51-14, NO FAULTS FOUND. INSPECTED ACM IAW EMB AMM 21-51-03, NO FAULTS FOUND. THE AIRCRAFT RETURN TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 24,084 hrs · 21,382 cycles

FLASHLIGHT APPEARS TO NOT BE CHARGING, NO RED CHARGE LIGHT. R & R COCKPIT FLASHLIGHT ASSY, OPS CHECKED GOOD IAW AMM.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 24,033 hrs · 21,339 cycles

FLASHLIGHT HOLDER BEHIND CAPTAIN`S SEAT IS BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 25-60-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,031 hrs · 21,336 cycles

GALLEY EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AND CHARGING ASSY IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: LATCH — MALFUNCTIONED (MAIN DOOR) · airframe 23,971 hrs · 21,279 cycles

F/A REPORT THAT MAIN DOOR LATCHING MECH IS IN DOUGHT. RESECURE DOOR HANDLE ACTUATOR BRACKET, LUBE ALL DOOR ROLLERS, OPS CHECKED GOOD IAW 52-10-00 AMM AND 52-21-02.

Part: DISPLAY — FAILED (RIGHT) · airframe 23,917 hrs · 21,240 cycles

CREW REPORTED AT 36000 FT, NOTICED AN ELECTRICAL BURNING ODOR IN COCKPIT. MFD WENT BLANK AND CIRCUIT BREAKER TRIPPED. DECLARED AN EMERGENCY AND DIVERTED. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED MFD 1, INSPECTED CONNECTOR AND WIRING, AND REPLACED MFD 1 IAW AMM 34-22-01. ACFT RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 23,629 hrs · 21,006 cycles

DURING MBV INSPECTION, FOUND FRAME 15 GOUGED AT STR 2R. ACFT REMOVED FROM SERVICE . PERFORMED PERMANENT REPAIR ON FRAME IAW EO-EM-53MR-2185.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 23,629 hrs · 21,006 cycles

FLOOR PROXIMITY LIGHT STRIP WIRE HARNESS HAS A CONNECTOR MISSING. REPAIRED FLOOR PROXIMITY, EMERGENCY LIGHT STRIP WIRE W192-8760-22 IAW SWPM 20-21-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 23,629 hrs · 21,006 cycles

NR 8 FLOOR PROXIMITY LIGHT STRIP HAS DAMAGED WIRE. R & R NR 8 EMERGENCY PROXIMITY LIGHT STRIP FROM THE PANEL COVER AS REQUIRED, BOW136806 FOR EMERGENCY LIGHT STRIPS REMOVAL AND REINSTALLMENT.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 23,629 hrs · 21,006 cycles

EIGHT FLOOR PROXIMITY LIGHT STRIP PANEL COVERS CRACKED. R & R 8 EA PANEL COVERS FOR FLOOR LIGHT PROXIMITY STRIPS AS REQUIRED SEE BOW 136806 FOR REMOVAL AND REINSTALLATION OF PROXIMTY FLOOR LIGHT STRIPS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,629 hrs · 21,006 cycles

R & R EMERGENCY LIGHTING BATTERY ASSY, BATTERY CHARGER, WC 33-700-19, WC 33-002, NR 4 PN 2013-1A, SN 68535- EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER, WC 33-700-19, NR 4, PN 2013-1A, SN 68535 WAS REPLACED AT SGF ON 07 AUG 2013. VERIFIED ON VISUAL INSPECTION AND ENTRIES. PN 2013-1A, SN 83870 IS INSTALLED.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 23,321 hrs · 20,746 cycles

FOUL ODOR WHEN NR 1 PACK WAS SELECTED AND ON ENGINE BLEED SOURCE ODOR IS LESS WITH APU BLEED SOURCE, AND GONE WITH THE PACK OFF. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED ETN-EM-72-034 AND DETERMINED ENGINE NR 1 BLEED TO BE THE SOURCE OF ODOR. FOLLOWING THE FIM 72-00-00-810-814 UP THROUGH STEP BLOCK 10, SOME EVIDENCE OF OIL STAINS WERE FOUND ON IGV BLADES. ALSO BLOCK 12 WAS CHECKED AND SPANNER LOCK-NUT PLUG DIAPHRAM FOUND IN GOOD CONDITION. R & R NR 1 ENG 0 CARBON SEAL UP TO SUB TASK 72-25-25-965-001 IAW MM 72-25-25 NO DEFECTS NOTED ON DIMENSIONAL CHECK CARBON SEAL. ACCOMPLISHED E1 ETN NO DETECTABLE SMELL IAW ETN-EM-72-034. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,587 hrs · 20,171 cycles

ON FLIGHT 2857 THE CREW REPORTED THAT BOTH CABIN AND CABIN EMERGENCY LIGHTS ON ICU PANEL WOULD NOT GO OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET AFT FLIGHT ATTEDNANT EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 20,628 hrs · 18,643 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT ON SERVICE DOOR ( EXTERNAL LIGHT) HAS BROKEN WIRE IN WIRE BUNDLE. LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED BROKEN WIRE IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 20,268 hrs · 18,351 cycles

DURING B INSPECTION FOUND THE RIGHT UPPER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT UPPER EMERGENCY LIGHT ASSEMBLY IAW AMM TASK 33-50-10-020-004-A00 AND 33-50-10-420-004-A00. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 19,659 hrs · 17,845 cycles

ON PREFLIGHT FOR FLIGHT 2834, THE ATTENDANT NOTICED THAT THE EMERGENCY ROW LIGHTNING WAS INSTALLED INCORRECTLY. EMERGENCY FLOOR LIGHT INDICATIED WRONG ROW. AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED LIGHTS IAW AMM 33-50-08. OPS CHECKED AS PER AMM 33-50-00 . AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,565 hrs · 17,747 cycles

DURING B-INSPECTION FOUND THE EMERGENCY FLOOR LIGHTS AND CEILING LIGHS AFT OF SEAT ROW 14 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY HOLDER AND CHARGER IAW AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — UNKNOWN (MAIN DOOR) · airframe 19,506 hrs · 17,702 cycles

ON FLIGHT 3519 THE CREW REPORTED THEY WERE UNABLE TO OPEN BOARDING DOOR FROM THE INSIDE. DOOR OPENS OK FROM THE OUTSIDE. TOP DOOR FLAP DOES NOT GO DOWN ENOUGH WHEN USING THE INSIDE HANDLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REINSTALL MAIN DOOR INTERNAL ACTUATING HANDLE IAW AMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,242 hrs · 17,489 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EXIT EMERGENCY LEFT FORWARD WING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXIT FORWARD EMERGENCY LIGHT IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 19,201 hrs · 17,451 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHTS FLOOR PROXIMITY STRIP. LIGHTING STRIP FWD ROW 8/9 INCORRECT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 8/9 EMERGENCY LIGHT FLOOR STRIP IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 9A) · airframe 19,174 hrs · 17,435 cycles

FLIGHT 4047, FLOOR EMERGENCY LIGHT AT ROW 9A INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPSL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,134 hrs · 17,409 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT STRIP ROW 9 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP AT ROW 9 IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,172 hrs · 17,433 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LIGHT ON EMERGENCY FLASHLIGHT ON FORWARD LAV WALL PARTITION DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PUSHED IN THE OVERHEAD PANEL BREAKER FLASHLIGHT AND THE LIGHT ON THE EMERGENCY FLASHLIGHT ON THE FORWARD LAV WALL PARTITION WORKS NOW. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL CABLE — FAILED (AILERON) · airframe 19,129 hrs · 17,405 cycles

FOR FLIGHT 3935 THE CREW REPORTED THAT PRIOR TO TAKEOFF WHILE EXERCISING THE FLIGHT CONTROL THE AILERONS DID NOT MOVE SMOOTHLY BOTH RIGHT AND LEFT AILERONS INPUT AS WELL THE AILERONS DO NOT RETURN TO NEUTRAL POSITION SMOOTHLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RT OUTBD CENTER AILERON CABLE AND TENSIONED IAW AMM 27-11-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 19,172 hrs · 17,433 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE ENERGENCY LIGHTS STRIP NR 2 AND NR 8 HAVE BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGECNY LIGHT LIGHTS STRIP NR 2 AND NR 8 IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 19,031 hrs · 17,330 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE RIGHT OVERWING EMERGENCY LIGHT LAMP TO BE IMPROPERLY INSTALLED, REMOVED AND REINSTALLED LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — SEIZED (MLG) · airframe 18,407 hrs · 16,896 cycles

ON FLIGHT 3921 THE CREW REPORTED THE AIRCRAFT PULLED HARD TO THE RIGHT DURING LANDING. THE CREW HAD TO RELEASE RIGHT BRAKE PRESSURE TO KEEP STRAIGHT. LEFT OUTBOARD AND RIGHT INBOARD TEMPERATURE INDICATORS WENT WELL INTO THE AMBER RANGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 WHEEL SPEED TRANSDUCER AND DUST CAP (AFTER FINDING IT SEIZED) IAW EMB 145 AMM 32-41-03. THE FUNCTIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 18,081 hrs · 16,576 cycles

ON FLIGHT 3960 DURING CLIMBOUT THE CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW TRIED AUTO AND MANUAL MODE. NO EICAS MESSAGES RELATED TO PRESSURIZATION. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE ELECTRIC PNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

FOR FLIGHT 3934 DURING RAMP OPERATIONS AT NIGHT WHEN GROUND POWER WAS PULLED ALL THE EMERGENCY LIGHTS CAME ON. MAINTENANCE WAS CALLED TO EVALUATE EMERGENCY LIGHT SYSTEM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED NR 3 AND NR 4 CHARGER AND BATTERY FOR EMERGENCY LIGHT IAW W/C 33-700-17 AND W/C 33-700-19. PARTS NUMBERS AND SERIAL NUMBERS ARE: BA50933901/13270, BA50933901/20114, 20131A/68861, 20131A/66540. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,414 hrs · 1,530 cycles

DURING TAXI FOR FLIGHT 4372 THE CREW FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT CHARGER TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,112 hrs · 13,467 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM AT FRAME 25 TO BE CORRODED AT THE FORWARD EDGE OF CROSS BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR OF LEFT OMEGA BEAM AT FRAME 25 WITH A DOUBLER REPAIR IAW SRM 53-00-10 FIG 202 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,112 hrs · 13,467 cycles

DURING MAINTENANCE BASE VISIT, FOUND CORROSION UNDER FLOOR SUPPORT AT FRAME 38 ON THE LEFT OMEGA BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 38 FLOOR SUPPORT WITH A DOUBLER REPAIR IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (MLG) · airframe 8,444 hrs · 8,014 cycles

LANDING GEAR AURAL WARNING WITH GEAR DOWN, FLAPS 22 AT 1680 FEET. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-33-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 8,104 hrs · 7,654 cycles

AUTO PRESSURE CONTROL INOPERATIVE, DIVERTED TO ACT. PERFORMED OPERATIONAL OF PRESSURE CONTROL SYSTEM IN AUTO MODE IAW EMB AMM 21-31-00 WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,091 hrs · 7,632 cycles

BURNED ODOR NOTICED IN GALLEY AND ROW THREE, NO SMOKE NOTICED. INSPECTED AIRCRAFT IN STANDARD OPERATIONAL CONFIGURATION WITH ALL PACKS ON RECERT FANS, LIGHTS AND AMENITIES OPERATING WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL C CHECK FLIGHT WITH NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — LEAKING (LEFT)

SMOKE SMELL IN AFT CABIN WITH ASSOCIATED LAVATORY SMOKE DETECTOR WARNING. REPLACED LT ENGINE AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: ENGINE — FAILED (NR 2)

ON CLIMB-OUT CREW REPORTED A LOUD BANG. ENGINE NR 2 ROLL BACK AND UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (NR 2 TE FLAP)

FSM - FLT 3695 - FLAPS FAILED AT 9 DEGREES ON FINAL. FOUND NR 2 FLAP VELOCITY SENSOR CONNECTOR LOOSE AND TIGHTENED. PERFORMED OPERATIONAL CHECK OF FLAP ELECTRICAL/ELECTRONIC COMPONENT ADJUSTMENT. AIRCRAFT RETURNED TO SERVICE. (M)