N688AE

Part: UNKNOWN — ODOR (CABIN) · airframe 43,665 hrs · 38,873 cycles

OIL SMELL IN CABIN WITH PACKS RUNNING. OPS CHECKED PACKS HOT AND COLD EACH. IAW AMM 21-51-00 NO SMELLS NOTED AC OK FOR SERVICE

Part: SOCKET — FOULED (ZONE 200) · airframe 42,333 hrs · 37,344 cycles

LH OVERWING EMERGENCY LIGHT IS INOP. RAR LIGHT ASSY AS REQUIRED WITH RETAINED HARDWARE.

Part: SKIN — CHAFED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F007648 CHAFFED AREA ON FWD FUSELAGE BTW FR3-4 BTW STR18-21L. ACCOMLISHED REPAIR BTW FR 3-4 STGR 18L-21L IAW ETD# ETD2024-145-031452 AND EO1-53-24-0708

Part: CUP — CORRODED (ZONE 700) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F0007279 CORROSION ON LH MLG AFT BEARING CUP. RAR LH MLG AFT BEARING CAP IAW EMB 145 AMM 32-10-01

Part: BEARING — CORRODED (ZONE 700) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F007282 RH MLG AFT BEARING CAP IS CORRODED AND GOUGED. RAR RH MLG AFT BEARING CAP IAW EMB 145 AMM 32-10-01

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F066712 FO'S IB FLOOR GUSSET CORRODED ON NUMEROUS AREAS. R & R GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006714 CAPTAIN'S OB FLOOR GUSSET CORRODED ON NUMEROUS AREAS. RAR GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006713 FO'S OB FLOOR GUSSET CORRODED ON NUMEROUS AREAS. RAR GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

CAPTAIN'S IB FLOOR GUSSET CORRODED ON NUMEROUS AREAS. RAR GUSSET IAW SRM 51-40-02

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006546 PAX DOOR STRUCTURE LWR CUT-OUT FWD AND AFT FLOOR SILL SUPPORT BRACKETS CORRODED. RAR BRACKETS IAW SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006533 RH FLOOR BEAM CORRODED AT FR23. REPAIRED IAW EO1-53-24-0690

Part: STRINGER — CRACKED (ZONE 200) · airframe 42,189 hrs · 37,176 cycles

F006604 MACHINED STRINGER 3L IS CRACKED BTW FR19-20. R & R MACHINED STRINGER IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006540 SERVICE DOOR STRUCTURE FWD LWR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: ATTACH BRACKET — GOUGED (ZONE 200) · airframe 42,189 hrs · 37,176 cycles

PILOT'S BULKHEAD UPPER OB ATTACH BRACKET GOUGED WITH ELONGATED HOLE. REPAIRED IAW EO 1-53-24-0674.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006506 CARGO DOOR CUT-OUT LWR CTR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006367 LH #6 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F006321 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006355 CTR FLOOR BEAM #6 GUSSET CORRODED. RAR GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006387 LH FLOOR SILL #4 CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F0006385 LH #2 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F006323 SHEAR CLIP CRACKED AT FR26 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006390 FLOOR SUPPORT CROSS BEAM CORRODED AT FR35 BTW LH #3 FLOOR SILL AND LH FLOOR BEAM. RAR CROSS BEAM IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F006325 SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006346 LH #7 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006393 RH #2 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F006324 SHEAR CLIP CRACKED AT FR26 BTW STR14-15R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006379 LH #5 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006356 FLOOR SUPPORT BRACKET CORRODED AT FR57 BTW LH FLOOR SILL AND LH FLOOR BEAM. RAR SUPPRT BRACKET IAW SRM 51-40-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006237 INTERIOR SKIN DOUBLER CORRODED AT BTW FR6162 BTW STR20-21L. REPAIRED IAW EO1-53-24-0672

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F006320 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006386 LH #3 FLOOR SIL CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 20) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006400 RH #3 FLOOR SILL CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006362 CTR FLOOR SUPPORT IB SIDE CORRODED BTW FR49-53. REPARIED FLOOR BEAM EO1-53-24-0694

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006392 LH FLOOR BEAM #4 GUSSET CORRODED. RAR GUSSET IAW SRM 51-04-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F006354 CTR FLOOR SUPPORT IB SIDE4 CORRODED AT BTW FR54-56. REPAIRED IAW EO1-53-24-0689

Part: SKIN — CRACKED (ZONE 200) · airframe 42,189 hrs · 37,176 cycles

F005671 RH SIDE SKIN CRACKED ON RIVET HOLE AT FR77 BTW STR3-4R. REPAIRED IAW EO1-53-24-0696

Part: SKIN — GOUGED (ZONE 800) · airframe 42,189 hrs · 37,176 cycles

F005165 BAG DOOR INNER SKIN GOUGED. REPAIRED IAW EO1-52-24-0695

Part: RIB — CORRODED (ZONE 400) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F005232 CORROSION ON #2 ENGINE UPPER COWLING ON 3 PROFILE REINFORCEMENTS AT CNT RIB. RAR REINFORCEMENTS IAW SRM 51-40-02

Part: STOP FITTING — BENT (ZONE 100) · airframe 42,189 hrs · 37,176 cycles

F005155 BAG DOOR FWD CONTINUOUS STOP IS BENT AT LWR END. REPAIRED IAW EO1-52-24-0693

Part: LONGERON — CORRODED (ZONE 400) · corrosion level 2 · airframe 42,189 hrs · 37,176 cycles

F005173 CORROSION ON #1 ENGINE UPPER COWLING OB LONGERON CTR AND AFT EDGE. REPAIRED IAW ETD2024-145-031103 AND EO1-05-24-0704

Part: LAMP — INOPERATIVE (LH) · airframe 42,156 hrs · 37,141 cycles

LH OVERWING EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (RH) · airframe 42,024 hrs · 37,001 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT IAW AMM 33-50-07-04 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (RH) · airframe 42,001 hrs · 36,975 cycles

RH ABOVE WING EMERGENCY LIGHT IS INOP-C/A-RAR RH ABOVE WING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPC GOOD

Part: NONE — UNSERVICEABLE (AFT) · airframe 41,853 hrs · 36,794 cycles

REF MEL 25-32 ORIGINAL LOG PAGE 4866139/2 AFT CABIN EMERGENCY FLASLIGHT INOP.-C/A-RAI AFT CABIN EMERGENCY FLASHLIGHT LED ASSEMBLY IAW AMM EMB145 TASK 33-50-16. OPERATIONAL CHECK GOOD PER AMM 33-51-01 THIS MEL IS RESTORED.

Part: NONE — NONE · airframe 41,829 hrs · 36,763 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP-C/A-ITEM DEFERRED PER MEL 25-32 AUTH# 050389M-C (M) PROCEDURES C/W CA PENDING

Part: LAMP — INOPERATIVE (RH) · airframe 41,829 hrs · 36,763 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACE THE RH OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-07. OPC GOOD.

Part: NONE — INOPERATIVE (RH) · airframe 41,787 hrs · 36,717 cycles

R/H OVERWING EMERGENCY LIGHT INOP-C/A-RAR R/H OVERWING EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD

Part: NONE — NONE · airframe 41,771 hrs · 36,694 cycles

DURING PS-2 FOUND LH WING EMERGENCY LIGHT INOP-C/A-R&R BATTERY POWER SUPPLY #4 IAW AMM 33-50-04 OP'S CHECK GOOD

Part: LAMP — INOPERATIVE (RH) · airframe 41,660 hrs · 36,571 cycles

FWD EMERGENCY LIGHT AT RH WING INOP.-C/A-RAR FWD EMERGENCY LIGHT BULB AT RH WING IAW AMM 33-50-10. OPS CHECK GOOD

Part: NONE — UNSERVICEABLE ([0000] [4] [) · airframe 41,596 hrs · 36,502 cycles

DURING PS-1 CHECK WALK AROUND FOUND BOTH OVER WING EXTERIOR EMEGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 BATTER CHARGER ASSY IAW AMM 33-50-04. OPS CHECK GOOD

Part: NOT REPORTED — NOT REPORTED · airframe 41,368 hrs · 36,264 cycles

AFT CABIN EMERGENCY FLASHLIGHT MOUNT BROKEN-C/A-RAR AFT EMERGENCY FLASHLIGHT ASSY. IAW EMB-145 AMM TASK 30-50-16. NO DEFECTS NOTED. OPC GOOD.

Part: NONE — NONE · airframe 40,599 hrs · 35,416 cycles

FA REPORTS MAIN CABIN DOOR IS HARD TO OPERATE-C/A-LUBRICTAED MAIN CABIN DOOR IAW E145 AMM 53-21-02, OPS CHECK GOOD, IAW AMM 52-00-00

Part: NONE — NONE · airframe 40,590 hrs · 35,410 cycles

FA REPORTS MAIN CABIN DOOR HARD TO CLOSE-C/A-LUBRICATED DOOR HANDLE, OPERATIONAL CHECK OF DOOR NORMAL AMM 52-10-01

Part: PSU — FAILED (SEAT 1A) · airframe 40,275 hrs · 35,034 cycles

FA REPORTS BURNING SMELLS NEAR COCKPIT"TRANSFERRED TO NRWC 688-MIA-05603"-C/A-DURING INITIAL EVALUATION, WAS FOUND PASSENGER CABIN LIGHTTING POWERED ON WITH NO OPTION TO POWER IT OFF FROM THE FA LIGHT CONTROL PANEL AND FOUND PSU 1A OVERHEATED AND BURNED SMELL COMING OUT. PERFORMED FIM TASK 33-21-00-810-801-A, FOUND CONTROL MODULE ASSY DAMAGED AND WITH INTERNAL BURNED SIGNS.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 39,892 hrs · 34,616 cycles

FWD FA EMERGENCY FLASHLIGHT INOP-C/A-RAR FWD FA EMERGENCY FLASHLIGHT IAW E145 AMM 33-50-16 OPC GOOD

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 39,869 hrs · 34,589 cycles

AFT FA EMERGENCY FLASHLIGHT CRADLE BROKENMEL 25-32 AUTH# 050137M- REF AML PAGE 4506896 ITEM 2-C/A-RAR AFT FA EMERGENCY FLASHLIGHT CRADLE IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD. MEL 25-32 AUTH # 050137M-C RESTORED.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 39,836 hrs · 34,548 cycles

AFT EMERGENCYFLASHLIGHT CRADLE BROKEN-C/A-DEFERRED PER MEL 25-32 AUTHORIZATION # 050137M-C. EXPIRATION 05/19/21

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 39,673 hrs · 34,372 cycles

BAGGAGE SMOKE DETECT ON EICAS / REQ CFR AT GATE - BAGG SMOKE EICAS MSG WOULD DISPLAY INTERMITTENLY ON TAXI IN TO GATE. MEL 5205 - AUTH# 040061-C BAGG DOOR WARNING SYSTEM INOP LOGPAGE: 4723842-C/A-VISUAL CHECK INSIDE CARGO COMPARTMENT FOR HALLON SMELLING, NOTHING.SMOKE DETECTION OPERATION CHECK IAW E145 26-15-00 AMM. LUBRICATED/CLEANED BAGGAGE DOOR MICROSWITCHES IAW EMB 145 AMM 20-30-02 OPC GOOD. MEL 5205 RESTORED. A/C RETURM TO SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,590 hrs · 34,285 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP.-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT ASSY IAW EMB145 AMM 33-50-10. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,524 hrs · 34,215 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,904 hrs · 33,618 cycles

FLIGHT ATTENDANT FOUND THE AFT FLASHLIGHT BRACKET TO BE BROKEN. C/A: R & R AFT FLASHLIGHT ASSEMBLY, IAW EMB-145 M/M 33-50-16. OPERATIONS CHECK GOOD.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,843 hrs · 32,527 cycles

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

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LOWER SHEAR CLIP AT FR 65 CORRODED-C/A-PERFORMED PERMANENT REPAIR ON CARGO DOOR CUTOUT LOWER SHEAR CLIP IAW EMB 145 SRM 53-31-04-RE ITEM 4. (REPAIR MATERIAL: SHEAR CLIP P/N 145-25175-001)

Part: SKIN — CRACKED (E/E DOOR) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND AFT AVIONICS DOOR 272DR CRACKED UNDER EYELET.-C/A-REPAIRED AFT AVIONICS DOOR 272DR IAW EMB 145 SRM 52-44-02-RE ITEM 2 AND ERS-EM-5200-1043. (REPAIR MATERIALS: DOUBLER, 2024T3 0.050, FILLER, 2024T3 05050)

Part: SKIN — CRACKED (FRAME 75) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND RH AFT FUSELAGE SKIN CRACKED IN 2 AREAS ON FR 75 STGR 3R-C/A-REPAIRED CRACKS ON RH AFT FUSELAGE SKIN AT FR 75 AND STGR 3R IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER 2024-T3, 0.080?, FILLER: 2024-T3, 0.063?, ANGLE: 2024-T3, 0.050?, SHIM 2024-T3, 0.032?)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND THE LH VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE CRACKED.-C/A-REMOVED AND REPLACED LH VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IAW EMB 145 SRM 51-40-02

Part: SKIN — CRACKED (FRAME 75) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND LH AFT FUSELAGE SKIN CRACKED AT FR 75 ABOVE STGR 2L.-C/A-PERFORMED PERMANENT REPAIR TO CRACK ON LH REAR FUSELAGE I SKIN AT FR 75 ABOVE STGR 2L IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER 2024-T3, 0.080?, FILLER: 2024-T3, 0.063?, ANGLE: 2024-T3, 0.050?, SHIM 2024-T3, 0.032?)

Part: WEB — CRACKED (LT WING) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QA FOUND THE LH WING RIB 21 CRACKED INSIDE 551CB-C/A-PERFORMED PERMANENT REPAIR ON LH WING RIB 21 IAW EMB 145 SRM 57-20-07-RE ITEM 4.(REPAIR MATERIALS: FILLER-2024T3, 0.040, DOUBLER; 7475 T761, 0.050, SHIM; 2024T3, 0.032)

Part: STRINGER — CRACKED (FRAMES 12-13) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND STR 6R CRACKED BETWEEN FR 12-13.-C/A-REMOVED AND REPLACED STR 6R BETWEEN FR 12-13 IAW EMB 145 SRM 51-40-02.

Part: WEB — CRACKED (RH WING RIB 21) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, FOUND THE RT WING RIB 21 CRACKED INSIDE 551CB. PERFORMED A PERMANENT REPAIR ON THE RT WING RIB IAW SRM 57-20-07-RE ITEM 4.

Part: CHANNEL — CORRODED (FRAMES 19A-22) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND SERVICE DOOR CENTER SILL CORRODED.-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, FOUND FRAME 68 SHEAR TIE CORRODED AT CARGO DOOR LOWER SILL. REPAIRED THE SHEAR TIE IAW SRM 53-21-04-RE ITEM 4.

Part: PROFILE — CORRODED (CARGO DOOR FRAME) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, FOUND THE CARGO LOWER FRAME PROFILE CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER FRAME PROFILE IAW SRM 51-40-02.

Part: WEB — CORRODED (CARGO DOOR) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, FOUND CARGO DOOR INNER WEB CORRODED AROUND 1 SCREW HOLE. REPAIRED THE CARGO DOOR INNER WEB IAW SRM 52-30-01-RE ITEM 12 AND ETN-EM-52-043.

Part: YOKE — CRACKED (LT PYLON) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND LH PYLON FWD LOWER YOKE FITTING CRACKED.-C/A-REMOVED AND REPLACED YOKE FITTING IAW ERS-EM-54MR-698.

Part: FITTING — CRACKED (RT YOKE) · airframe 37,843 hrs · 32,527 cycles

DURING HMBV INSPECTION, QC FOUND RH PYLON FWD LOWER YOKE FITTING CRACKED.-C/A-REMOVED AND REPLACED YOKE FITTING IAW ERS-EM-54MR-698.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 37,603 hrs · 32,288 cycles

FOUND FLASH LIGHT AT FA STATION INOP DURING PS-1.-C/A-REMOVED AND REPLACED FA FLASHLIGHT IAW EMB 145 AMM 33-50-16-04.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 37,420 hrs · 32,129 cycles

SUPPLEMENTAL LAV SMOKE WARNING IN FLIGHT. C/A-FOLLOWED FIM TASK 26-14-00-810-802-A. FOUND POSSIBLE FAULTY DETECTOR. DEFERRED LAVATORY SMOKE DETECTION SYS. "M" PROCEDURES C/W..MEL# 26-01 AUTH# 090669DM-C. INSPECTED LAVATORY LIGHTS AND BALLAST. RAR COURTESY LIGHTS FLOURESCENT LAMPS IAW AMM 33-28-03, OPS CHECK GOOD IAW 33-28-00. FURTHER TROUBLESHOOTING REQUIRED. MELS REMAINS OPEN. C/W LAVATORY SMOKE DETECTION SYSTEM OPERATIONAL CHECK IAW AMM 26-14-00 OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. MEL RESTORED. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR PANEL AND SENSOR IAW AMM 26-14-01 OPS CHECK GOOD IAW AMM 26-14-00-700-801-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,102 hrs · 31,849 cycles

ELECTRICAL FUMES IN COCKPIT AND AT FWD FA SEAT. COMPLETD STEP 1 BLOCK 001 PAGE 201 TO PAGE 205 BLOCK 1 STEP 2 TO BLOCK 2 OF PAGE 207 STEP 3 TO 6 BLOCK 6 STEP 7 TO 9 OF PAGE 208 TO BLOCK 6 STEP 7 TO 9 OF PAGE 208 TO BLOCK 9 OF PAGE 209 STEP 10 TO 11 AS PER FIM 21-20-00-816-811A FOUND NO ABNORMAL SMELL IN CABIN / COCKPIT. REMOVED AND REPLACED OF RECIRC FAN 2 IAW AMM 21-24-01. BOTH RECIRC FANS OPC GOOD IAW AMM 21-20-00-700-801. REMOVED AND REPLACED R/H RECERCUIATION FAN ATTENUATOR DUCT IAW 21-24-02 . C/W LEAK CHECK OF RECIRC FAN DUCTS DURING RECIRCF FAN OPC IAW AMM 21-20-00-700-801. NO LEAKS FOUND. C/W PACK AIR DISTRIBUTION OPC IAW AMM 21-20-00-700-801. USED APU BLEED AS PER AMM AND RAN BOTH ENGINES IAW RR MM 72-00-00-700-801 FOR ALTERNATE BLEED SOURCE DURING THE 30 MINUTE DISTRIBUTION TEST. CONFIRMED BOTH RECIRC FANS OPC GOOD. NO ODORS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,029 hrs · 31,776 cycles

SUPPLEMENTAL DURING PS-1 FOUND EMERGENCY LIGHT FLOOR STRIP AT SEAT 9A PARTIALLY OUT. C/A-DEFERRED EMERGENCY LIGHT STRIP AT SEAT 9A PER MEL 33-30. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM 33- 50-12 OPS CHECK GOOD MEL ITEM RESTORED.

Part: SENSOR — FAILED (WINDOW HEAT) · airframe 37,018 hrs · 31,766 cycles

W/S HEAT 2 MASTER CAUTION LIGHT ILLUMINATED THEN BURNING SMELL COMING THROUGH COCKPIT. WE SHUT OFF W/S HEAT 2 SMELL DISSAPATED. "TRANSFERRED TO NRWC 688-ORD-04297". C/A-PERFORMED WINDSHIELD TEMP CONTROLLER INSPEDTION IAW AMM 30-42-01-200-801, NO DEFECTS NOTED. INSPECTED WINDSHIELD HEAT CONTACTOR AND FUSE NO DEFECTS NOTED. INSPECTED WINDSHIELD 2 HEAT TERMINAL BLOCK NO DEFECTS NOTED. PERFORMED WINDSHIELD HEATING OPS/FUNCTIONAL CHECKS IAW AMM 30-42-00, OPS CHECK FAIL. REMOVED AND REPLACED WINDSHIELD 2 HEAT CONTROLLER IAW AMM 30-42-01, OPS CHECK FAIL. SWAPPED WINDSHIELD HEAT SENSOR LEADS FROM SPARE SENSOR (S3,S4) TO MAIN SENSOR (S1,S2) IAW AMM 30-42-00-700-801. WINDSHIELD HEAT OPS CHECK GOOD IAW AMM 30-42-00.

Part: FAN — FAILED (RECIRCULATION) · airframe 36,819 hrs · 31,571 cycles

AFTER ENCOUNTERING WX STRONG SMELL IN COCKPIT AND A/C AFTER ENCOUNTERING TURBULENCE WEATHER TURBULENCE LT TO MOD-C/A-PERFORMED ETN-EM-72-034 ODOR EVENT T/S NO FAULTS FOUND ALL FAULTS NO ODOR PERFORMED FIM TASK 21-20-00-810-001-A NO FAULTS FOUND NO FIX. PERFOMRED FIM TASK 30-42-00 RH LH WINDSHEILD HEAT INOP NO FIX. WINDSHEILD HEATING SYSTEM OPS CHECK GOOD IAW AMM 30-42-00 INSPECTED WINDSHEILD HEAT WIRING FOUND NO DEFECTS. REMOVED AND REPLACED COCKIT RECIRC FAN IAW EMB AMM 21-24-01 OPC GOOD.

Part: BRAKE ASSY — FAILED (NR 3) · airframe 36,750 hrs · 31,510 cycles

IB & OB BRAKE TEMP ON THE RIGHT MLG GOES ALL THE TO THE TOP OF AMBER RNAGE WHILE USING MIN BRAKES. WHILE THE LEFT SIDE IB & OB STAYS GREEN-C/A-FOUND #3 AND #4 BRAKES DETTERIORATED AND WORN BEYOND LIMITS AND REMOVED AND REPLACED #3 AND #4 BRAKES IAW WORKCARD 32-600-14 OPS CHECK GOOD NO FAULTS NOTED ALSO WORKCARD 32-700-11. LR MAIN BRAKE ASSY P/N 2-1707-2 S/N 1107

Part: ACM — SEIZED (AC BAY) · airframe 36,156 hrs · 30,927 cycles

BURNING SMELL IN FLIGHT WITH PACK 1 OVHT CAUTION ON LANDING "TRANSFERRED TO NRWC 688-MIA-03996". C/A-FOUND NR 1 ACM SEIZED, REMOVED AND REPLACED ACM IAW AMM 21-51-03 OPS CHK IAW 21-51-00 AND ETN -EM-72-034 REF: PERFORMED ENGINE RUNS IAW ETN-EM-72-034 FOR ODOR EVENTS.OPS CHK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,399 hrs · 30,275 cycles

PASSENGER AND FA REPORT ELECTRICAL SMELL FROM CEILING BATTERY COMPARTMENT AT ROW 15 HOT TO THE TOUCH IN FLIGHT. INSPECTED CABIN LIGHTING AND EMERGENCY LIGHTING AND PSU LIGHTING NO DEFECTS NOTED NO SMELL NOTED ACFT CHECK GOOD ACFT OK FOR SERVICE IAW AMM 30-50-00.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 35,364 hrs · 30,242 cycles

FA REPORTS MAIN CABIN DOOR VERY HARD TO OPEN/CLOSE-C/A-LUBRICATED MAIN DOOR FRAME ROLLERS IAW EMB 145 AMM 53-21-02. OPC CHECK GOOD. NO DEFECT NOTED AT THIS TIME IAW AMM 52-00-00.

Part: DUCT — DEFECTIVE (AC BAY) · airframe 35,332 hrs · 30,198 cycles

SUPPLEMENTAL BLEED 1 LEAK DURING CLIMB AT AROUND 10,200FT MESSAGE DISAPPEARED AFTER CHECLIST PROCEDURE WAS COMPLIED WITH ANTI-ICE OVERRIDE KNOB IN ''ALL'' POSITION AT THE TIME IN COMPLIANCE WITH 30-25. C/A- TROUBLE SHOT IAW FIM 36-20-00, REMOVED AND REPLACED NR 1 PACK DUAL TEMP CONTROL Y DUCT TUBE ASSY. IAW AMM 21-60-01. OPS AND LEAK TEST, GOOD IAW AMM 36-00-00 AND AMM 21-51-00. REMOVED AND REPLACED BLEED AIR DUCT ORINGS AT JOINT 11, 28, 30, 31 IAW AMM 36-11-10. LEAK CHECK GOOD IAW W/C 36-700-06. REMOVED AND REPLACED LT DUCT CLAMP ON CROSS BLEED VALVE IAW AMM 36-10-01. LEAK CHECK GOOD IAW W/C 36-700-06. PERFORMED OPC OF THE BLEED AIR SYSTEM IAW AMM TASK 36-00-00, OPC OF THE ANTI-ICING SYSTEM IAW AMM TASK 30-00-00 AND OPC OF THE COOLING SYSTEM IAW AMM TASK 21-51-00-- NO DEFECTS NOTED--OCK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 34,447 hrs · 29,324 cycles

LEFT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-07 , OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,087 hrs · 28,978 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-07-000-801 AND AMM 33-50-07-400-801. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,876 hrs · 28,808 cycles

EMERGENCY LIGHT 120 NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: LEVER — OUT OF ADJUST (CARGO DOOR) · airframe 33,491 hrs · 28,447 cycles

AFTER TAKEOFF CARGO DOOR OPEN INDICATION ON EICAS AND ON T/O PAGE OF MFD. BAGGAGE DOOR WARNING (POSITION ON EICAS & MFD) DEFERRED, VERIFIED CLOSED. WAS ABLE TO GENERATE FAULT OF BAGGAGE DOOR INDICATING CLOSED WHEN IT IS ACTUALLY OPEN. DETERMINED THAT BOTH MICROSWITCH ASSEMBLIES ARE PROVIDING AN INTERMITTENT GROUND. WORK PERFORMED IAW AMM 52-76-01. NO TIME TO CHECK EACH INDIVIDUAL MICROSWITCH ASSEMBLY. SEEMS LIKE BOTH SWITCHES ARE ON THE THRESHOLD OF HAVING OPEN OR CLOSED CONTACTS. TROUBLESHOT BAGGAGE DOOR OPEN MESSAGE IAW FIM 52-70-00. COMPLETED STEPS 1-3 OF THE FAULT ISOLATION PROCEDURES WITH NO FAULTS FOUND. FURTHER TROUBLESHOOTING REQUIRED. RECONNECTED BOTH ROD ENDS AT LOWER ATTACHMENT POINTS OF THE CARGO DOOR UPPER CRANK LOCK LEVERS IAW AMM 52-31-700-801 SEC 2 J AND FIG 503. ADJUSTED UPPER AFT CRANK LOCK LEVER IAW AMM 52-31-00.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 33,467 hrs · 28,431 cycles

INOP AFT CABIN FLASHLIGHT HOLDER-C/A-REPLACE BASE IAW AMM 33-50-16

Part: FLASHLIGHT — INOPERATIVE (ROW 18) · airframe 32,850 hrs · 27,883 cycles

FA`S FLASHLIGHT AT ROW 18 IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25

Part: ANGLE — CRACKED (WING) · airframe 32,847 hrs · 27,876 cycles

RT LOWER WING TO FUSELAGE ANGLE AT FR 46 IS CRACKED. REPAIRED LOWER WING TO FUSELAGE ANGLE AT FRAME 46 IAW SRM 51-40-02 AND ETN-EM-53-142.

Part: ANGLE — CRACKED (WING) · airframe 32,847 hrs · 27,876 cycles

RT LOWER WING TO FUSELAGE ANGLE AT FR 50 IS CRACKED. REMOVED AND REPLACED ANGLE IAW ETN-EM-53-142 REV 2.

Part: SUPPORT ANGLE — CRACKED (FRAME 61) · airframe 32,847 hrs · 27,876 cycles

BRACKET FOR CARGO DOOR ASSIST TORSION ARM HAS AN 1/8 INCH CRACK AT FRAME 61 ON FWD LOWER CORNER RADIUS. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02.

Part: ANGLE — CRACKED (WING) · airframe 32,847 hrs · 27,876 cycles

RT LOWER WING TO FUSELAGE ANGLE AT FR 48 IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.

Part: LIGHT — CRACKED (CABIN) · airframe 32,847 hrs · 27,876 cycles

SEVERAL EMERGENCY LIGHTS ARE CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHTS IAW AMM 33-50-12.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 32,466 hrs · 27,507 cycles

RADAR FAILED MESSAGE, WHEN IN TEST MODE. AMBER WX INSCRIPTION ON MFD WHEN IN WX MODE WITH NO RADAR RETURN. REMOVED AND REPLACED THE WEATHER RADAR RTA IAW AMM 34-42-01 OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 32,191 hrs · 27,203 cycles

FWD FLIGHT ATTENDENT EMERGENCY FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: SEAL — UNSECURE (PAX DOOR) · airframe 30,787 hrs · 25,983 cycles

CLIMBING THRU 10,000 FT DTP REPORTED A WHISTLEING SOUND COMMING FROM ERN ROW FORWARD. PAX COMPLAIN FLT ATT ALSO REPORTED WHISTLING SOUND FROM PAX AND SERVICE DOOR WHISTLEING SOUND. OPENED NR 1 AND 2 ACM PANELS, CHECKED ACMS FOR LEAKS, NONE FOUND. SECURED BOTH PANELS, INSPECTED BOTH PASSENGER DOOR SEALS AND SERVICE DOOR SEAL, FOUND SERVICE DOOR UPPER FWD TRIM SEAL LOOSE. SECURED LOOSE SEAL AS IAW AMM 52-20-01. COMPLIED WITH CABIN PRESSURRIZATION TEST IAW AMM 21-31-00. NO LEAKS NOTED TESTED GOOD.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 29,455 hrs · 24,796 cycles

DURING TAKEOFF ROLL, FIRST OFFICER COULD NOT HEAR ANYTHING THRU HIS HEADSET. CAPTAIN COULD HEAR HIM TALK, BUT FIRST OFFICER WOULD INTERMITTENTLY LOSE ALL AUDIO. HE SAID IT WAS CONSISTENTLY FADING OUT. TRIED ALL 3 DIFFERENT HEADSETS. R & R FIRST OFFICERS DIGITAL AUDIO PANEL. OPERATIONAL TEST IS GOOD IAW AMM 23-51-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,964 hrs · 24,369 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. PERFORMED AFT FLIGHT ATTENDANT FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-50-00, COULD NOT DUPLICATE FAULT.

Part: PLATE — CRACKED (SERVICE DOOR) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. SERVICE DOOR BACKING PLATE CRACKED & BENT. PERFORMED REPAIR OF SERVICE DOOR BACKING PLATE IAW ERS-EM-53MR-1727.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR OUTER LE IAW SRM 51-20-01, 51-40-02, 51-20-03, 55-20-01, ETN-EM-55-073R2, ETN-EM-55-076 & ERS-EM-5500-355.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R RT FWD FUSELAGE I SKIN IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, 53-11-01-SI, EM-51-118 & EM-53-235.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE. R & R RT ELEVATOR OUTER LE IAW SRM 51-40-02, 55-20-01, 51-20-01, 51-20-03, 51-40-06, ETN-ETM-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, 55-20-01, 51-20-01, 51-20-03, 51-40-06, ETN-ETM-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. R & R LT FWD FUSELAGE I SKIN IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, 53-11-01-SI & ETNS EM-51-118 & EM-53-235.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R CTR FUSELAGE II, TOP SKIN IAW SRM 51-20-03, 51-40-06, 51-20-01, 51-40-03, 51-40-02, 53-22-01-S1, ETN-EM-51-118 & ETN-EM-53-263.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R REAR FUSELAGE I TOP SKIN IAW SRM 51-40-02, 51-40-03, 53-31-01-SI, 51-20-01, 51-20-03, 51-40-0, ETN-118 & ETN-EM-53-266.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R FWD FUSELAGE II SKIN WIPER IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 53-12-01-SI, ETN-EM-51-118 & ETN-EM-53-206.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

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

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R LT HORIZONTAL STABILIZER, UPPER SKIN IAW SRM 51-40-02, 55-10-01-SI, 51-20-01, 51-20-03, 51-40-06 & ETN EM-55-073R2.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R STAB UPPER SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-10-01SI & ETN EM-55-073R2 & ENT EM-55-074.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM 51-40-02, 55-20-01, 51-20-01, 51-20-03, 51-40-06 & ETN-ETM-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R LT CTR FUSELAGE I, UPPER SKIN IAW SRM 51-40-02, 53-21-01-SI, 51-20-01, 51-20-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R RT CTR FUSELAGE I, UPPER SKIN IAW SRM 51-40-02, 53-21-01-SI, 51-20-01, 51-20-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,857 hrs · 24,285 cycles

HAIL DAMAGE EVENT. R & R CTR FUSELAGE IV, TOP SKIN IAW SRM 51-20-03, 51-40-06, 51-20-01, 51-40-03, 51-40-02, 53-24-01-S1, ETN-EM-51-118 & ETN-EM-53-265.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,854 hrs · 24,284 cycles

FOUND RT FUSELAGE DAMAGED ABOVE N NUMBER. FOUND ACRACK FROM SPAR FRAMES 56 - 57 & STRINGERS 4R - 5R. THE CRACK IS FIVE INCHES & OUT OF LIMITS IAW SRM 53-24-01. R & R SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 53-54-01 SI, 51-40-03, ETN-EM-51-118 & ETN-EM-53-265.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 28,851 hrs · 24,280 cycles

ON FINAL DESCENT, LAVATORY SMOKE WARNING, PRESENTED. FOLLOW THE PROCEDURE NO EVIDENCE OF FIRE OR SMOKE ON THE LAVATORY. PERFORMED OPERATIONS CHECK OF LAVATORY SMOKE DETECTOR IAW AMM 26-14-00. NO DEFECTS NOTED.

Part: HANDLE — LACK OF LUBE · airframe 28,492 hrs · 23,980 cycles

MAIN CABIN DOOR HANDLE HANGS UP DURING OPENING. DOOR IS OPEN ABOUT 3/4" WHEN IT HANGS, THEN IT WILL NOT OPEN THE REST OF THE WAY. 15 LBS FORCE TO OPEN, 30 TO CLOSE, WITHIN LIMITS. CLEANED & LUBED MAIN DOOR EXTERIOR HANDLE MECHANISM, FUSELAGE ROLLERS & DOOR LOCKS. OPERATIONS CHECKED OK IAW AMM 52 18 00.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,885 hrs · 23,433 cycles

CARGO DOOR SILL IS CORRODED. REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,885 hrs · 23,433 cycles

SUPPORT CLIP AT FRAME 72 BETWEEN 16L & 17/L HAS A 1/2" CRACK. R & R SHEAR CLIP AT FRAME 72 BETWEEN STRINGER 16L & 17L IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,885 hrs · 23,433 cycles

FRAME 80 HAS A CRACKED SHEAR CLIP BETWEEN STRINGERS 6L & 7L 3/4 INCH LONG. R & R SHEAR CLIP BETWEEN STRINGERS 6L & 7L ON FRAME 80 IAW SRM 51-40-02.

Part: FITTING — GOUGED (RT AILERON) · airframe 27,885 hrs · 23,433 cycles

RIGHT AILERON DAMPER FITTING IS GOUGED. RT AILERON PCA FITTING FLANGED BUSHINGS ARE PITTED, SCORED & GOUGED. INSTALLED NEW RT AILERON DAMPER FITTING IAW EO EM-27MR-112. REPLACED PCA FITTING IAW EO EM-27MR-112. FITTING PN 145-6982-610.

Part: WIRE — PULLED (CABIN) · airframe 27,885 hrs · 23,433 cycles

EMERGENCY FLOOR LIGHT STRIP NR 5 WIRES PULLED OUT. R & R EMER FLOOR LIGHT STRIP NR 5 IAW AMM 33-50-12. REF BOW 186307 FOR OPERATIONS CHECK.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,592 hrs · 23,150 cycles

CAPTAIN`S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: UNKNOWN — MALFUNCTIONED (RUDDER) · airframe 27,501 hrs · 23,047 cycles

SLIP SKID INDICATOR UNCOMMANDED, TOO FAR RIGHT, WE CORRECTED TURN & IT WENT TOO FAR LEFT. NO INDICATION ON EICAS, YAW INDICATION. CORRECT INDICATION ON STANDBY & SLIP SKID. COMPLIED WITH RUDDER MANUAL & AUTH SHUTOFF ADJUSTMENT. TESTED IAW 24-25-00 & YAW TRIM ACTUATOR ADJUSTMENT TEST IAW 27-24-00. ALL CHECKS PASSED.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 26,878 hrs · 22,522 cycles

FIRST OFFICER'S FLASHLIGHT INOPERATIVE. LAMPED IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,766 hrs · 22,415 cycles

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

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 26,710 hrs · 22,364 cycles

DURING 5A INSPECTION RT ELEVATOR TIP, TWO EACH AFT SCREW NUTPLATE ATTACHMENT HOLES DAMAGED BY LIGHTNING STRIKE. SATISFACTORILY ACCOMPLISHED ERS-EM-55MR-170.

Part: HEAT EXCHANGER — CRACKED (AC BAY) · airframe 26,185 hrs · 21,929 cycles

DURING REMOVING NR 1ACM FOUND CRACK ON NR 1 HEAT EXCHANGER. R & R NR 1 HEAT EXCHANGER IAW AMM 21-51-02.

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 25,763 hrs · 21,486 cycles

DURING FLIGHT 3779, NR 2 ENGINE OIL 7 QTS RUNNING IN FLIGHT, SHORT FINAL WENT TO 6 QTS. SHUTDOWN NR 2 ENGINE ON GROUND FOR TAXI UNUSUALLY HIGH AMOUNT OF OIL CONSUMPTION CONSIDERING SERVICED PREVIOUS TURN. AIRCRAFT REMOVED FROM SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,749 hrs · 21,475 cycles

FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY, OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 24,884 hrs · 20,785 cycles

CREW MEMBER FLASHLIGHTS & HOLDERS, CAPTAIN`S FLASHLIGHT WON’T STAY IN HOLDER. R & R CAPTAIN'S EMERGENCY FLASHLIGHT & BASE IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL RESTORED, PLACARDS REMOVED.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 24,315 hrs · 20,334 cycles

PAX DOOR DIFFUCULT TO OPERATE. PERFORMED MAIN CABIN DOOR ROLLER AND LOCKING HANDLE LUBRICATION IAW AMM 52-10-01. OPS CK GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 24,256 hrs · 20,290 cycles

LAV OMEGA BEAM CORRODED AROUND FORWARD NUTPLATE HOLE. FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW EO EM-53MR-2223 AND ETD 2013-145-048632A.

Part: LIGHT — INTERMITTENT (NR 3) · airframe 24,318 hrs · 20,338 cycles

NR 3 EMERGENCY LIGHT INTERMITTENT. R & R NR 3 EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,755 hrs · 19,100 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDSET — OUT OF POSITION (CABIN) · airframe 22,692 hrs · 19,055 cycles

ON FLIGHT 3488 THE CREW REPORTED THE CABIN INTERPHONE AND THE CABIN EMERGENCY LIGHT ILUMINATED AND WOULD NOT EXTINGUISH. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFT HANDSET INCORRECTLY STOWED. STOWED CORRECTLY IAW AMM 23-40. LIGHTS SYSTEM CHECK OK. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 22,487 hrs · 18,905 cycles

ON FLIGHT 3986 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT HOLDER IAW EMB 145 MM 25-60-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,259 hrs · 18,731 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — UNSERVICEABLE (CABIN DOOR) · airframe 21,532 hrs · 18,126 cycles

ON FLIGHT 2814 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD LOWER MAIN DOOR GUIDE REF AMM 53-71-06. THE OPERATIONAL CHECK WAS GOOD REF AMM 52-18-00. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,352 hrs · 17,993 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,167 hrs · 17,851 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY, NR 4 BATTERY, AND LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-04 AND AMM 33-50-07. ACFT RETURNED TO SERVICE.

Part: MECHANISM — INOPERATIVE (DOOR LOCKING) · airframe 20,033 hrs · 16,929 cycles

ON FLIGHT 3207, THE CREW REPORTED THE MAIN DOOR WAS VERY DIFFICULT TO CLOSE/OPEN-OPERATE. AIRCRAFT REMOVED FROM SERVICE. MAIN DOOR FORWARD ACTUATING AND LOCKING MECHANISM WAS REMOVED AND REPLACED AND OPS CHECKED GOOD IAW AMM 52-18-06. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,949 hrs · 16,865 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVER WING EMERGENCY LIGHT IAW EMB 145 AMM TASKS 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,908 hrs · 16,833 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,796 hrs · 16,733 cycles

ON FLIGHT 2874 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DISCONNECTED (FLASHLIGHT) · airframe 19,732 hrs · 16,678 cycles

DURING MAINTENANCE INSPECTION FOUND THE CO-PILOT FLASHLIGHT CHARGE INDICATOR LIGHT SHOWS FLASHLIGHT NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED FLASHLIGHT, RETRIEVED WIRE FROM UNDER RIGHT CONSOLE, RECONNECTED WIRE AND REINSTALLED FLASHLIGHT IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,952 hrs · 16,064 cycles

FORWARD PASSENGER CABIN EMERGENCY FLASH LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD PASSENGER CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 17,922 hrs · 15,317 cycles

ON FLIGHT 2939 DURING THE DESCENT THE CREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. THE CREW RAN EPC AND AOM CHECKLIST THERE WAS NO BLEED VALVE FAIL MESSAGE BUT THE BLEED 1 LEAK MESSAGE REMAINED ON SO THE CREW DID A PRECAUTIONARY ENGINE SHUTDOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BLEED SEALS AT JOINT 28 AFT AVIONICS BAY AS PER EMB 145 AMM 36-11-10. RAN AIRCRAFT, NO LEAKS OR FAULT MESSAGES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,098 hrs · 13,212 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY EXIT LOCATOR FORWARD LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT SIGN ASSEMBLY IAW EMB AMM 33-50-15 AND INVERTER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH FITTING — DAMAGED (AILERON) · airframe 14,627 hrs · 12,817 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON, PCA ATTACH FITTING HAS DAMAGE FROM BOLT REMOVAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PCA ATTACH FITTING IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A MBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT, INSTALLED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 33, CHAPTERS 53-00-10 FIG 201 SHEET 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 543 hrs · 525 cycles

DURING EMERGENCY LIGHT TEST ALL LIGHTS ILLUMINATE MOMENTARILY THEN ALL LIGHTS AFT OF ROW 7 DIM AND GO OUT. REPLACED NR1, NR2, NR3 AND NR4 BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. BATTERY PN 2013BR SN OFF NR1-B2425/ NR2-B2430 / NR3-B2433 / NR4-B2434. (SW21200501809) (K)