N698CB

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER) · airframe 43,930 hrs · 39,593 cycles

RUDDER SYS 1 INOP MESSAGE ON T/O ROLL AND REJECTED T/O. PERFORMED RUDDER SYSTEM OPERATIONAL TEST IAW AMM 27-23-00. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 43,692 hrs · 39,303 cycles

ENG 1 ANTI-ICE VALVE FAILED DURING TAKE OFF ROLL. R & R NR 100 ENGINE ANTI-ICE VALVE IRT AMM 30-21-01. OPS CHECKED GOOD. A/C OK FOR SERVICE.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 43,500 hrs · 39,074 cycles

RH OVERWING EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY EXIT SIGN IRT AMM 33-50-14 PN ON EXIT SIGN 7444-36 PN OFF EXIT SIGN 7444-36

Part: INVERTER — FAULTED (ZONE 200) · airframe 43,460 hrs · 39,026 cycles

EMERGENCY EXIT LIGHT BELOW FLIGHT DECK DOOR INOP. INSTALLED NEW INVERTER P/N 1330212 IAW AMM 33-50-11 INSTALLED NEW EXIT INDENTIFER IAW AMM 33-50-13.

Part: WEB — CHAFED (CARGO DOOR) · airframe 41,698 hrs · 37,032 cycles

E052528 CARGO DOOR INTERNAL LOWER WEB IS CHAFED IN THREE (3) AREAS. INSTALLED FABRICATED REPAIR DOUBLER AT INTERSECTION OF HB3-BV2 ON LOWER CARGO DOOR INTERNAL WEB IAW EMBRAER ETD2024-145-023066 AND PIEDMONT EO1-52-24-0525.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050582 RH FLOOR SILL CORRODED BTWN FR 54-55. REMOVED AND REPLACED RH FLOOR SILL BTW FR 52-60 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E051424 LH CABIN OMEGA BEAM #2 GUSSETT IS CORRODED. : RAR THE LH CABIN OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 41,698 hrs · 37,032 cycles

E051309 SHEAR CLIP ON FRAME 24 CRACKED AT STRINGER 15R. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FRAME 24 AT STRINGER 15R IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 51,698 hrs · 37,032 cycles

E051313 SHEAR CLIP ON FRAME 25 CRACKED AT STRINGER 15R. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FRAME 25 AT STRINGER 15R IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E051427 CABIN LH #3 FLOOR SILL CORRODED. RAR LH CABIN FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E051425 LH CABIN OMEGA BEAM #3 GUSSETT IS CORRODED. RAR LH CABIN OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E051429 CABIN CENTER AISLE CROSSBEAM AT FRAME 25 CORRODED. REMOVED AND REPLACED CABIN CENTER AISLE CROSSBEAM AT FR 25 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050583 LH OMEGA BEAM GUSSET CORRODED BTWN FR 50-51. RAR THE LH OMEGA BEAM GUSSET BTWN FR 45-53 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050581 RH FLOOR SILL CORRODED BTWN FR 53-54. BLENDED TO REMOVE CORROSION ON R/H FLOOR SILL BETWEEN FR 53-54 IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS OF BLENDED AREA FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-24-02.

Part: WEB — CHAFED (CARGO DOOR) · airframe 41,698 hrs · 37,032 cycles

E050150 CARGO DOOR INTERNAL UPPER AND LWR WEB IS CHAFED IN MULTIPLES AREAS. FABRICATED DOUBLERS FOR TWO (2) PREVIOUS REPAIRS. INSTALLED DOUBLERS FOR TWO (2) PREVIOUS REPAIRS ON LOWER CARGO DOOR INTERNAL WEB IAW EMB145 SRM 51-40-02RE, AND SRM 52-30-01RE ITEM 12, FIGURE 213 AND PIEDMONT EO1-52-24-0526.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050232 CORROSION ON CARGO DOOR LOWER SILL. RAR CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,698 hrs · 37,032 cycles

E050029 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L. RAR SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L IAW EMB 145 SRM 51-40-02.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050234 CORROSION IN CARGO ON LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L. RAR THE CARGO UNDERFLOOR LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,698 hrs · 37,032 cycles

E050238 CORROSION ON FRAME 65 SHEAR CLIP BAGGAGE DOOR CUT-OUT. : RE-ACCOMPLISHED FR65 SHEAR CLIP REPAIR IAW EMB 145 SRM 53-31-04 ITEM 4.D FIGURE 212.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,698 hrs · 37,032 cycles

E050028 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R. : RAR SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R IAW EMB 145 SRM 51-40-02.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 41,698 hrs · 37,032 cycles

E049491 SCRATCH ON REAR FUSELAGE SKIN BETWEEN FR79-FR80 AND STRG 03L-04L. RFORMED CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND APPLIED EDGE SEALANT FOR REPAIR OF DAMAGED SKIN BTW FR79-80, STGR 3L-4L IAW EMB 145 SRM 53-32-01 ITEM 2 FIGURE 201 SHEET 3 AND EO1-53-24-0530

Part: NONE — NONE · airframe 40,850 hrs · 36,040 cycles

AFT EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT EMERGENCY FLASHLIGHT MISSING M PROC. C/W MEL 25-32 AUTH 050146M-C MOC ID 373623. PENDING CA

Part: NONE — NONE · airframe 40,108 hrs · 35,170 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT EMERGENCY FLASHLIGHT HOLDER IAW AMM 33-50-16, OPS CHECK GOOD

Part: NONE — NONE · airframe 40,108 hrs · 35,170 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHTBULB. OPC GOOD IAW AMM 33-50-06.

Part: NONE — NONE · airframe 40,073 hrs · 35,125 cycles

RH AFT OVERWING EMERGENCY LIGHT INOP REF MEL 33-22 LG PG 4589780 ITEM 3-C/A-RAR OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10 OPC GOOD MEL RESTORED

Part: NONE — NONE · airframe 40,072 hrs · 35,124 cycles

RH AFT OVERWING EMERGENCY LIGHT INOP-C/A- "TRANSFERRED TO AML PAGE 4589780 ITEM 3" -RAR RH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM 33-50-07. NO FIX. PERFORMED TROUBLESHOOTING IAW EMB145 FIM TASK 33-50-00-810-804-A. FOUND PROPER VOLTAGE AT CANNON PLUG. DETERMINED LIGHT ASSY TO BE INOP.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 39,629 hrs · 34,583 cycles

EMERGENCY LIGHT OVER R/H WING INOP-C/A-RAR R/H OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 39,598 hrs · 34,553 cycles

RH UPPER EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR RH UPPER EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPC GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,575 hrs · 34,529 cycles

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

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 39,524 hrs · 34,470 cycles

REAR EMREGENCY FLASHLIGHT NOT WORKING PROPERLY-C/A-RAR EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 39,326 hrs · 34,245 cycles

PILOT REPORTS BURNING SMELL IN COCKPIT. PERFORMED ENGINE RUNS IAW ETN-EM-72-034. NO ODORS NOTED. NO DEFECTS NOTED.REF NRWC 698-ORD-05499 FOR COMPLETION OF TECH SUPPORT WORKSCOPE REV.1 FOR BURNING SMELL IN COCKPIT. NO ODOR NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 38,913 hrs · 33,819 cycles

EMERGENCY GALLEY LIGHT PLACARD INOP-C/A-T/S IAW EMB WM 33-50-50-005. RAR #2 EMERGENCY LIGHT DC INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 38,645 hrs · 33,546 cycles

CABIN EMERGENCY FLOOR LIGHT WIRE BROKEN AT SEAT 11A. C/A-REMOVED AND REPLACED FLOOR EMERGENCY LIGHT SPLICE SP9115 IAW EMB 145 SWPM 20-21-00. OPERATIONAL CHECK GOOD.

Part: A/C PACK — SEIZED (NR 2) · airframe 38,644 hrs · 33,545 cycles

MECH SMOKE IN CABIN AND COCKPIT IN CRUISE LEVEL FLIGHT AT FL240 NOTICED SMOKE FROM CAPTAIN SIDE VENTS AND THROUGT THE CABIN DECLARED EMERGENCY RESCUE SENT, FLT CONT.-C/A-PERFORMED FIM TASK 21-20-00-810-801-A PACK OVERHEAT AND FOUND ACM ON PACK 2 TO BE SEIZED REF ITEM 1 ON LG PG 4635121

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,326 hrs · 33,200 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW WMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPERATIONS CHECK GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 38,143 hrs · 33,005 cycles

FWD F/A EMERGENCY FLASHLIGHT INOPERABLE MEL 2553, AUTH 10-280-C LOGPAGE: 4681588. C/A: R & R FWD F/A EMERGENCY FLASHLIGHT SYSTEM ASSEMBLY, IAW EMB 145 AMM 33-50-16-04. OPERATIONS CHECK GOOD. M PROCEDURES REVERSED. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 38,136 hrs · 33,000 cycles

FWD F/A EMERGENCY FLASHLIGHT INOPERABLE. C/A: FLIGHT CREW PLACARD FWD F/A FLASHLIGHT AUTH 100280-C, REF 25-53 MOC 864015.

Part: DOOR — LEAKING (SERVICE) · airframe 37,950 hrs · 32,837 cycles

FA REPORTS LOUD WHISTLING FROM SERVICE DOOR DURING CLIMB STOPED AT CRUISE ALT 37000 "TRANSFERRED FROM LOG PAGE #4676996"-C/A-PERFORMED PRESSURIZATION CONTROL SYSTEM TEST AS PER AMM 21-31-00. CHECKED OK. PRESSURIZATION NORMAL . NO FURTHER DEFECTS. SEE NRWC# 698-MIA-0548 FOR ADDITIONAL WORK PERFORMED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,845 hrs · 32,771 cycles

DURING PS-2 CHECK, FOUND RH AFT EXTERNAL EMERGENCY LIGHT TO BE INOPERATIVE. R & R RT AFT EMERGENCY LIGHT IAW AMM 33-50-10. NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,678 hrs · 32,585 cycles

DURING PS-1 CHECK, FOUND THE RT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,614 hrs · 32,518 cycles

SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP-C/A-TS IAW EMB AMM 33-50-00-810-804-A EMOVED AND REPLACED POSITION 2 BACK BATTERY PACK IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A AND CHARGER ASSY IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME, BATTERY CHARGER ASSY P/N 11-0049 S/N 11652

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND PAX DOOR LOWER FRAME CORRODED AT LINER NUT PLATE HOLES.-C/A-PERFORMED PERMANENT REPAIR TO CORRODED AREAS ON PAX DOOR LOWER FRAME AT NUT PLATE HOLES IAW EMB 145 SRM 52-10-04RE AND ETN-EM-52-041.

Part: SKIN — PUNCTURED (RUDDER) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND RUDDER II TRAILING EDGE LOWER LH SKIN PUNCTURED.-C/A-REPAIRED RUDDER II LOWER LH SKIN IAW ERS-EM-55MR-841.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND LAV BUCKET CORRODED AROUND TOILET WASTE VALVE MOUNTING FLANGE.-C/A-REMOVED AND REPLACED LAV BUCKET IAW EMB 145 SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND PAX DOOR HANDLE BOX SUPPORT ASSY BRACKET CRACKED.-C/A-REMOVED AND REPLACED PAX DOOR HANDLE BOX SUPPORT BRACKET IAW EMB 145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND CORROSION ON FR 22 AT SERVICE DOOR LOWER CUT-OUT.-C/A-PERFORMED PERMANENT REPAIR TO FR 22 AT SERVICE DOOR CUT-OUT IAW EMB 145 SRM 53-00-04RE.

Part: RIB — CRACKED (LT WING) · airframe 37,581 hrs · 32,481 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

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND FR 72 CRACKED BETWEEN STGR 16L-17L.-C/A-PERFORMED PERMANENT REPAIR TO CRACK ON FR 72 IAW EMB 145 SRM 53-00-04RE.

Part: FITTING — DAMAGED (RT AILERON) · airframe 37,581 hrs · 32,481 cycles

DURING HMBV INSPECTION, QC FOUND A RH AILERON DAMPER FITTING BUSHING HOLE ELONGATED. -C/A-REMOVED AND REPLACED RH AILERON DAMPER FITTING IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,581 hrs · 32,481 cycles

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

Part: FITTING — GOUGED (LT AILERON) · airframe 37,581 hrs · 32,481 cycles

LH AILERON DAMPNER BRACKET GOUGED. -C/A-REMOVED AND INSTALLED SERVICABLE DAMPNER FITTING IAW EO EM-27MR-112

Part: YOKE — CRACKED (RT ENGINE) · airframe 37,581 hrs · 32,481 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,581 hrs · 32,481 cycles

CARGO DOOR LWR SILL IS CORRODED-C/A-REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02

Part: FITTING — CRACKED (LT ENGINE) · airframe 37,581 hrs · 32,481 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,581 hrs · 32,481 cycles

L/H # 1 EMERGENCY LIGHT INOP .-C/A-COMPLETE:REMOVED AND REPLACED L/H # 1 EMERGENCY LIGHT IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD .

Part: LIGHT — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

L/H #5 LIGHT STRIP PANEL BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #5 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION

Part: LIGHT — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

L/H #8 EMERGENCY LIGHT STRIP PANEL BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #8 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION.

Part: LIGHT — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

R/H #2 EMERGENCY LIGHT STRIP PANEL BROKEN-C/A-COMPLETE:REMOVED AND REPLACED BROKEN R/H #2 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION .

Part: LIGHT — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

L/H #6 EMERGENCY LIGHT STRIP BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #6 EMERGENGY LIGHT STRIP IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION AND OPS CHECK .

Part: CONNECTOR — MISSING (CABIN) · airframe 37,581 hrs · 32,481 cycles

CABIN FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE/MISSING CONNECTOR AT FR 38-C/A-COMPLETE:REPAIRED EMERGENCY LIGHT STRIP AT FR 38 IAW EMB 145 SWPM 20-21-00. EASI #6277 AND #6224H.. SEE THIS NRTC FOR ALL WIP AND TASK DETAILS

Part: WIRE — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

L/H #8 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE .-C/A-COMPLETE:REMOVED AND REPLACED CORRECTART # FOR L/H #8 LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD .

Part: LIGHT — BROKEN (CABIN) · airframe 37,581 hrs · 32,481 cycles

R/H #5 EMERGENCY LIGHT STRIP PANEL BROKEN-C/A-COMPLETE:REMOVED AND REPLACED BROKEN R/H #5 EMERGENCY LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION.

Part: CHARGER — FAILED (CABIN) · airframe 37,568 hrs · 32,463 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOP-C/A- T/S FOUND EMERGENCY BATTERY NOT WORKING REMOVED AND REPLACED EMERGENCY BATTERY #2 AND CHARGER IAW ENVOY W/C 33-700-19 OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104854

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,167 hrs · 32,110 cycles

AFT OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY BATTERY AND CHARGER IAW EMB 145 AMM 33-50-04 OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 11448 / +

Part: CONTROLLER — FAILED (FLT GUIDANCE) · airframe 37,144 hrs · 32,079 cycles

FA AND GATE AGENT REPORTED 'BURNING SMELL" IN FORWARD CABIN TAXIING UP TO THE GATE.-C/A-FOUND STRONG ELECTRICAL SMELL COMING FROM FLIGHT GUIDANCE CONTROLLER (FGC). REMOVED AND REPLACED FGC IAW AMM 22-11-01. OPERATIONAL CHECKS GOOD.

Part: SKIN — DENTED (FRAMES 78-79) · airframe 36,780 hrs · 31,810 cycles

DENT AND SCRATCH LH REAR FUSELAGE II BETWEEN FR 78 AND FR 79 AND STR 5L AND 7L-C/A-PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-3952

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 36,346 hrs · 31,414 cycles

PTRIM MAIN INOP "TRANSFERRED TO NRWC 698-ORD-04545". WLS 1 HEAT FAIL. C/A-REMOVED AND REPLACED HORIZONTAL-STABILIZER ACTUATOR IAW AMM 27-40-02 PERFORMED ELECTRICAL ZERO POSITION OF THE HORIZONTAL STABILIZER IAW AMM 27-40-02. OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK IAW 30-42-00 COULD NOT DUPLICATE. OPS CHECK GOOD.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 36,343 hrs · 31,411 cycles

PTRIM MAIN INOP FL 270, BACKUP PTRIM OPERATED NORMALLY. "TRANSFERRED TO NRWC 698-ORD-04543" PTRIM MAIN INOP. C/A-REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPC GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 35,370 hrs · 30,434 cycles

FWD CABIN FLASHLIGHT CRADLE BROKEN-C/A-REMOVED AND REPLACED FWD CABIN FLASHLIGHT ASSY, OPC GOOD IAW EMB AMM 33-50-16

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,986 hrs · 30,147 cycles

AISLE EMERGENCY LIGHT ROW 3 INOP-C/A-REMOVED AND REPLACED AISLE EMERGENCY LIGHT ROW 3 LAMP, OPC GOOD IAW EMB AMM 33-50-08

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 34,945 hrs · 30,104 cycles

FA REPORTS EMERG LIGHTS WOULD NOT TEST. REINITIALIZED POWER TO A/C EMERG LIGHTS OPS CK GOOD IAW AMM 33-50-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (INBD BRAKE) · airframe 33,892 hrs · 29,081 cycles

INBD BRAKE INOPERATIVE ON FINAL.. CREW REPORTED INDICATIONS NORMAL ON TAXI TO GATE AFTER LANDING. PERFORMED GVI OF BOTH MLG AND BOTH INBD AND OTBD BRAKES, NO DEFECTS NOTED. BRAKE SYSTEM OPERATES NORMAL IAW AMM 32-41-00 PAR J .(2.). NO CMC MESSAGES DISPLAYED, NO FAULTS FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,567 hrs · 28,814 cycles

DURING CRUISE AT 19000 FT, ODOR ELECTRICAL WHILE IN VMC. COMPLIED WITH FIM 1-20-00-810-801. INSPECTED & OPERATED THE SENSOR, HEATING PACKS, RECIRCULATION, GASPERS, WINDSHIELD HEAT, COCKPIT LIGHTING & DISPLAYS. NO DEFECTS OR ODORS NOTED.

Part: STARTER GEN — FAILED (APU) · airframe 33,483 hrs · 28,735 cycles

ON GROUND POWER, APU PNEUMATICS, PACK 2 ON, GROUND RAMPERS REPORTED SMOKE OUT OF APU STARTER OUTFLOW EXHAUST. SMELL OF SMOKE IN THE FLIGHT DECK-C/A-FLIGHT CREW PLACARDED APU GEN FUNCTION MEL 2408 AUTH 060363-D MOC 056048. DEFERRAL PER MEL 49-1 AUTH # 060368DM-C (M) PRECEDURES C/W. REMOVED AND REPLACED APU START GEN IAW AMM 24-34-01. MEL ITEM RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,143 hrs · 28,391 cycles

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

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 32,788 hrs · 28,062 cycles

DURING APPROCH, AT POWER IDLE, AN ODOR OF SOMETHING BURNING. STARTED IN COCKPIT AND WORKED ITS WAY THROUGH THE CABIN. ONLY LASTED 30 SECONDS IN COCKPIT. PERFORMED ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. PERFORMED ENGINE RUNS IAW ETN-EM72-034. COULD NOT DUPLICATE THE BURNING ODOR. NO FURTHER DEFECTS NOTED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,687 hrs · 27,966 cycles

MULTIPLE EMERGENCY LIGHTS, SIGNS AND FLOOR STRIPS NOT ILLUMINATING. REMOVED AND REPLACED NUMBER 2 BATTERY POWER SUPPLY AND CHARGER IAW WORK CARD 33-700-19 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 71928.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACKED LT SHEAR CLIP AT FRAME 25 STRINGER 15L. REMOVED SHEAR CLIP AT FRAME 25 STRINGER 15L, FABRICATED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02 AND 51-30-01. RESTORED PROTECTIVE COATING IAW CPM 51-21-03, 51-21-04 AND 51-21-05 FABRICATED FROM 7475-T761 0.032 NDT'D IAW NDTM INTRODUCTION SECTION D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP FRAME 68 BETWEEN STRINGER 6R AND 7R. REMOVED CRACKED SHEAR CLIP LOCATED DRILLED ALODINED NEW CENTER AND UPPER CLIP IAW SRM 51-20-03 AND CPM 51-21-04 FABRICATED LOWER CLIP WITH 7475-T761 0.050 IAW DRAWING 140-04102 NDT'D IAW NDTM INTRODUCTION SECTION D INSTALLED IAW SRM 53-31-04 AND RESTORED PROTECTIVE COATING IAW CPM 51-21-04, 51-21-05 51-21-06. SHEAR CLIP P/N 140-04102-607.

Part: STRUCTURE — CORRODED (DOOR FRAME 65) · corrosion level 2 · airframe 32,687 hrs · 27,966 cycles

CORROSION IN LATERAL L SHAPE AT FRAME 65, DOOR STOP. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED DAMAGED AREA, LOCATED , DRILLED AND INSTALLED A SPLICE. ALODINED, PRIMED, AND PAINTED IAW SRM 53-31-04, 51-20-03, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 32,687 hrs · 27,966 cycles

CRACKED SHEAR TIE AT FRAME 65, BETWEEN STRINGERS 7L AND 9L. LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED A NEW SHEAR TIE IAW ARM 51-20-03, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06

Part: FLOOR SUPPORT — CORRODED (FRAMES 53-59) · corrosion level 2 · airframe 32,687 hrs · 27,966 cycles

CORROSION ON LH/SIDE OF CENTER OMEGA AT CARBON CROSS MEMBER BETWEEN FRAME 58-59-C/A-REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-24-10, REMOVED CARBON CRESS BEAM AND OMEGA BEAM BETWEEN FRM 53-59 IAW EMB 145 SRM 51-40-02.LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW BEAM BETWEEN FRAME 53-59 IAW EMB 145 SRM 51-20-03, 51-40-02 AND CPM 51-21-04 AND 51-21-05 REINSTALLED CROSSBEAM IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRAMES 53-59) · corrosion level 2 · airframe 32,687 hrs · 27,966 cycles

CORROSION ON INBD SIDE OF THE LT OMEGA AT CARBON CROSS MEMBER BETWEEN FRAME 53 - 59. REMOVED THE OMEGA BEAM, DISCONNECTED BONDING JUMPER, REMOVED DOUBLER SND SUPPORT IAW AMM 51-40-02, AND 20-13-21. FABRICATED A DOUBLER AND SUPPORT IAW SRM 51-20-03, AND ENGINEERING DRAWING 145-01079. APPLIED ALODINE, PRIMER AND PAINT IAW CPM 51-21-03, 51-21-04, AND 51-21-05. LOCATED DRILLED AND INSTALLED THE NEW OMEGA BEAM BETWEEN FRAMES 53-59 IAW SRM 51-40-02. REINSTALLED BONDING JUMPER AND CROSSBEAM IAW AMM 20-13-21, AND SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 32,687 hrs · 27,966 cycles

CRACKED SHEAR TIE AT FRAME 68, BETWEEN STRINGERS 6L AND 7L. REMOVED, FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 53-31-04, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: DOOR FRAME — GOUGED (CARGO DOOR WAY) · airframe 32,687 hrs · 27,966 cycles

CARGO DOOR HAS A GOUGE AROUND NUTPLATE HOLE ON AFT FRAME SIDE. REMOVED DAMAGE, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED, FABRICATED AND INSTALLED A FILLER AND DOUBLER. INSTALLED THE DOUBLER AND FILLER IAW SRM 52-30-04, NDTM 51-00-00-916-801-00, CPM 51-21-04, 51-21-05 51-21-06, AND NCR EM-52-048.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACKED LT SHEAR CLIP AT FRAME 27 STRINGER 15L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 STR 15L-16L IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16R-17R IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 18L-19L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 65 BETWEEN STRINGER 18L-19L IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP AT FRAME 27 BETWEEN STRINGER 15R -16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 27 BETWEEN STRINGER 15R-16R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,687 hrs · 27,966 cycles

RT OMEGA BEAM CORRODED AT FRAME 23. REMOVED CORROSION FROM RT OMEGA BEAM AT FRAME 23 REPAIR DOUBLER. NO DAMAGE ALLOWED. FABRICATED .LOCATED AND DRILLED REPLACEMENT DOUBLER. PERFORMED NDT NO DEFECTS NOTED, ALODINED PRIMED, AND INSTALLED IAW SRM51-10-03, 51-40-02,CPM 51-21-04, 51-21-05 AND NDTM 51-00-00-918-803 TYPE 1 METHOD C, SENSITIVITY LEVEL 3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,687 hrs · 27,966 cycles

CORROSION IN CENTER OMEGA BEAM AT FRAME 59. CORROSION IN CENTER OMEGA BEAM AT FRAME 59 NUT PLATE HOLE FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND PERFORMED NDT INSPECTION, NO DEFECTS NOTED . FABRICATED, LOCATED AND DRILLED DOUBLER FROM 2024TS 0.080. APPLIED ALODINE, PRIMER, TOP COAT AND INSTALLED DOUBLER TO CENTER OMEGA BEAM IAW SRM 53-24-10, NDTM 51-00-00-916-801-A00 AND CPM 51-21-04,51-21-05 AND 51-21-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,687 hrs · 27,966 cycles

CRACK IN SHEAR CLIP AT FRAME 72 BETWEEN STRINGER 17L-18L. REMOVED CRACKED SHEAR CLIP, FABRICATED NEW CLIP FROM 7075-T761 0.032, LOCATED AND DRILLED HOLES AND ALODINED AND PRIMED THEN INSTALLED CLIP IAW SRM 51-40-02, 51-30-01, CPM 51-21-04, 51-21-05 AND ENGINEERING DRAWING 145-44878-010.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 31,444 hrs · 26,921 cycles

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

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,173 hrs · 26,665 cycles

AFT FACING EXIT LOCATOR SIGN AT ROW 12 WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER NR 3 IAW AMM 33-50-04 AND INVERTER NR 4 IAW AMM 33-50-11 OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 28,460 hrs · 24,160 cycles

CAPTAIN SIDE FLASHLIGHT INOPERATIVE. R & R LIGHT BULB FOR CAPTAINS FLASHLIGHT IAW STD MX. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,445 hrs · 24,144 cycles

DURING PS 1 CHECK, FOUND AFT CEILING EMER EXIT LIGHT STRIP INOPERATIVE. R & R AFT CEILING EMER EXIT LIGHT STRIP IAW MM 33-50-15. OPERATIONS CHECKED GOOD.

Part: TRIM PANEL — LOOSE (CABIN DOOR) · airframe 28,315 hrs · 24,019 cycles

TRIM PIECE ON MAIN CABIN DOOR IS LOOSE & MAKING DOOR DIFFICULT TO OPEN. TRIM PIECE WAS REMOVED & DEFERRED MAIN PAX DOOR TRIM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

LEFT UPPER FUSELAGE SKIN CRACKED 2 PLACES. CRACK 1= 1/4"CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK 2 =1/4" CRACK ON FRAME 75, AT FIRST FASTENER BELOW STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1840. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

TOP OF FRAME 66 CRACKED, BETWEEN RIVET HOLES FOR LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT. REPAIRED LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT AT FRAME 66 IAW ERS-EM-53MR-1837. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

LEFT FWD CARGO FLOOR SUPPORT, FWD OF CROSSBEAM HAS CORROSION AROUND NUTPLATE. REMOVED THE CORRODED LT FWD CARGO FLOOR SUPPORT & INSTALLED THE NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

TOP OF FRAME 67 CRACKED, BETWEEN RIVET HOLES FOR LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT. REPAIRED LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT AT FRAME 67 IAW ERS-EM-53MR-1837. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,241 hrs · 23,943 cycles

EMERGENCY LIGHT STRIP NR 8, PANEL 261 BF, HAS BROKEN CONNECTOR. REPAIRED SPLICE CONNECTOR ON PLANE SIDE FOR EMER LIGHT STRIP NR 8 IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK IS APPROX 1/4" LONG. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1840. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 28,241 hrs · 23,943 cycles

CORROSION FOUND ON LT UNDER THE GUSSET, ON BEAM AT FRAME, BETWEEN 59 & 60. REPAIRED THE LT BEAM UNDER THE GUSSET IAW ERS-EM-53MR-1839. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: PRESSURE SWITCH — MALFUNCTIONED (AC BAY) · airframe 27,793 hrs · 23,523 cycles

PACK 2 OVLD IN CRUISE FLIGHT AT FL 300 MEL 21-29. R & R NR 2 PACK OVERPRESSURE SWITCH IAW AMM-21-51-06. OPERATIONS CHECKED GOOD AT THIS TIME, MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,972 hrs · 22,775 cycles

AFT CABIN EMER FLASHLIGHT WILL NOT CHARGE. R & R AFT CABIN EMER FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 26,798 hrs · 22,649 cycles

LANDING GEAR LEVER DISAGREEMENT, AIR TURN BACK. LG DID NOT RETRACT AFTER TAKEOFF. GEAR IN TRANSIT ALL THREE GEARS CAME ON & STAYED ON WITH GEAR HANDLE UP. LG DISAGREE EICAS MSG CAME ON AFTER 10 SECS. GEAR HANDLE MOVED TO DOWN & ALL THREE GEAR DOWN INDICATION DISPLAYED. ABNORMAL GEAR EXTENSION PROCEDURE WAS ACCOMPLISHED IAW AOM VOL 1. NORMAL RATE OF DECENT FOR LANDING. R & R LG CONTROL LEVER. PERFORMED OPERATIONAL CHECK OF THE LG EXTENSION & RETRACTION CYCLE & PERFORMED GVI OF NLG & MLG COMPONENTS & WW WITH NO DEFECTS NOTED. LG OPERATIONS CHECKED GOOD IAW AMM 32-32-02 & 32-30-00 EMB AMM.

Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 26,647 hrs · 22,517 cycles

ON INITIAL CLIMB OUT WE GOT BLEED 2 OVERTEMP. CONFIRMED OPERATIONS OF FAN AIR VLV 2. NO LEAKS AT PRE COOLER 2. R & R WITH SERVICEABLE PRE COOLER 2 OUTLET TEMP SENSOR IAW EMB AMM 36 20 01, OPERATIONS CHECKED IAW AMM 36 00 00, 700 - 803A.

Part: BRAKE — FAILED (TE FLAP) · airframe 25,586 hrs · 21,627 cycles

FLAP LOW SPEED ADVISORY MSG ON EICAS AFTER LANDING. ITEM DEFERRED IAW MEL 27-9. FLAP LT MOTOR BRAKE FAIL M PROCEDURE COMPLIED WITH.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,368 hrs · 21,440 cycles

LEFT OVERWING AFT EMER LIGHT INOPERATIVE. R & R LT OVERWING AFT EMER LIGHT ASSEMBLY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 25,040 hrs · 21,133 cycles

PNEUMATIC ICE TEST INFLIGHT DID NOT SHOW OPEN INSCRIPTION ON WING. ALL OTHER INDICATES NORMAL. R & R LIGHT BULBS IAW AMM 20-13-04. OPERATIONS CHECKED IAW AMM 30-00-00. OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (BRAKE LIGHT) · airframe 25,024 hrs · 21,112 cycles

PARKING BRAKE LIGHT INOPERATIVE. R & R THE LAMPS IAW AMM 20-13-04. OPS CHECKED GOOD.

Part: RELAY — INOPERATIVE (RAM AIR VALVE) · airframe 24,748 hrs · 20,860 cycles

RAM AIR VLV FAIL. DURING CLIMB CREW RECEIVED EICAS PACK 2 VLV CLSD & RAM AIR VLV FAIL MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES & WAS ABLE TO RESET THE NR 2 PACK, HOWEVER THE RAM AIR VLV FAIL MSG REMAINED. CREW ELECTED TO RETURN & LANDED WITHOUT INCIDENT. PERFORMED RAM AIR VLV ADJUSTMENT & TEST IAW AMM 21-25-01. BOTH VLVS REMAIN CLOSED. R & R RELAY K0804 IAW AMM 21-13-02. OPERATIONS CHECKED GOOD IAW AMM 21-25-01 & 21-60-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,987 hrs · 20,190 cycles

RIGHT OMEGA BEAM AT FRAME 23 CORRODED ON PREVIOUS BLEND. REPAIRED CORRODED AREA IAW ERS-EM-53MR-231.

Part: HOUSING — CORRODED (HORIZ STAB) · airframe 23,987 hrs · 20,190 cycles

FOUND CORROSION IN LT & RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING. REWORKED BOTH LT & RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSINGS TO THE FIRST OVER SIZE TO REMOVE ALL CORROSION IAW SRM 55-30-02. SEE NRTC E363658 FOR HORIZONTAL STAB INSTALLATION & SEE NRTC E365978 FOR DIHEDRAL & INCIDENCE CHECK.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,987 hrs · 20,190 cycles

SHEAR CLIP ON FRAME 65 CRACKED BETWEEN 6L - 8L. REMOVED CRACKED SHEAR CLIP ON FRAME 65 BETWEEN 6L - 8L. PREPPED & INSTALLED SERVICEABLE SHEAR CLIPS IAW SRM 53-31-04.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 23,987 hrs · 20,190 cycles

FRAME 20 CTR ALUMINUM CROSS BEAM IS CORRODED. INSTALLED SERVICEABLE FRAME 20 ALUMINUM CROSS BEAM IAW AEA ETN EM 53-139 R3.

Part: FILTER — DEFECTIVE (BLEED AIR SYS) · airframe 23,803 hrs · 20,047 cycles

BLEED 2 OVER TEMPERATURE CLIMBING THROUGH FL 220. REPLACE FAN AIR VLV FILTER IAW FIM 36-11-00-810-804A. FAN ACFT OPERATIONS CHECKED GOOD 72-00-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,749 hrs · 20,004 cycles

CA FLASHLIGHT INOPERATIVE. REPLACED CA FLASHLIGHT IAW 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,498 hrs · 19,806 cycles

AFT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. R & R AFT AISLE CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,478 hrs · 19,790 cycles

DRING COURTESY CHECK FOUND NR 4 EMERGENCY LIGHT TO BE INOPERATIVE. R & R NR 4 EPSU BATTERY IAW AMM 33-50-04, OPS CHECK GOOD EMERGENCY LIGHT OPERABLE.

Part: COVER — DAMAGED (CABIN) · airframe 21,555 hrs · 18,271 cycles

DURING B INSPECTION FOUND THE MAIN-DOOR EMERGENCY LIGHT COVER HAS MULTIPLE HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN-DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 25-23-04 STEPS 2(J)3 AND 3(I)3. EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 21,442 hrs · 18,176 cycles

ON FLIGHT 3402 THE CREW REPORTED THE REAR CABIN FLASHLIGHT HOLDER HAS A BROKEN CLIP AND WOULD NOT HOLD FLASHLIGHT IN PLACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE REAR CABIN FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 21,144 hrs · 17,943 cycles

FOR FLIGHT 2840 THE CREW REPORTED THAT ON TAXI IN ON ENGINE NR 2 OPERATING ADVANCED NR 2 THRUST LEVER THE NR 2 GEN OVERLOADED AND THEN THE NR 2 ENGINE SHUT DOWN. STARTED THE NR 1 ENGINE WITH APU ASSISTING THE ENGINE START. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH RR FIM TASK 72-00-00-810-815 WITH NO DEFECTS NOTED. FDR DOWNLOAD SHOWS NR 2 ENGINE HAD NORMAL SHUT DOWN AFTER NR 1 ENGINE WAS RESTARTED. PERFORMED ENGINE RUNS IAW RR MM 72-00-00 NO DEFECTS NOTED. THE NR 2 ENGINE OPERATIONAL CHECKS WERE GOOD. REMOVED AND REPLACED THE NR 2 GENERATOR IAW EMB145 MTX W/C 24-800-00. THE OPERATIONAL & LEAK CHECKS WERE GOOD. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT IAW EMB 145 AMM 24-31-02. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,735 hrs · 17,613 cycles

DURING B INSPECTION FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CEILING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — LOOSE (COCKPIT) · airframe 20,607 hrs · 17,509 cycles

ON FLIGHT 2977 THE CREW REPORTED THE COCKPIT FLASHLIGHT BRACKET WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED COCKPIT FLASHLIGHT BRACKET IAW EMB-145 MM 25-60-00. OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,392 hrs · 17,331 cycles

ON FLIGHT 4306 THE FLIGHT ATTENDANT REPORTED THAT UPON DESCENT TO ORD SHE NOTICED THE AFT CABIN GOT HOT AND SAID SHE DETECTED A FAINT BURNING ELECTRICAL ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF CABIN COMPARTMENT LIGHTS. CYCLED ELECTRICAL POWER. RAN APU WITH BOTH PACKS ON. COULD NOT DUPLICATE. NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 20,172 hrs · 17,159 cycles

DURING PS2 INSPECTION FOUND THE RIGHT EMERGENCY LIGHT OVER WING BURNT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BURNT EMERGENCY BULB OVER RIGHT WING IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,293 hrs · 16,455 cycles

DURING MAINTENANCE INSPECTION, FOUND THE MAIN DOOR EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EXIT EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 19,283 hrs · 16,449 cycles

DURING B INSPECTION, FOUND THE NR 4 CABIN PROXIMITY LIGHT CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 CABIN PROXIMITY LIGHT IAW AMM 33-50-12, NRTC BOW93438. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 19,283 hrs · 16,449 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR CUTOUT FORWARD FRAME HAS CORROSION AT LOWER AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR CUTOUT FORWARD FRAME IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — GOUGED (ESCAPE HATCH) · airframe 19,269 hrs · 16,437 cycles

LEFT OVERWING EMERGENCY ESCAPE HATCH SKIN GOUGED AT LOWER FWD END NEAR METAL CLIP.(MARKED) REPAIRED LT OVERWING EMERGECY ESCAPE HATCH SKIN GOUGE AT LOWER FWD END NEAR METAL CLIP IAW EO EM-52MR-310.

Part: LINER — OUT OF POSITION (EMERGENCY EXIT) · airframe 19,283 hrs · 16,449 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY EXIT HATCH CATCHES AT UPPER END WHILE OPENING. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED LEFT OVERWING EMERGENCY EXIT HATCH LINING IAW AMM 52-21-00. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,556 hrs · 15,880 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP 2 & 3 ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB-145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,508 hrs · 15,848 cycles

ON FLIGHT 2836 THE CREW REPORTED THE EMERGENCY LIGHT PROXIMITY STRIP AT 6-8A AND THE EMERGENCY EXIT LIGHTS FROM ROW 3 THRU 8 TO BE INOPERABLE (FLOOR STRIP LIGHTS). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHT PROXIMITY STRIP AT ROW 6-8A. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-12. REMOVED AND REPLACED THE EMERGENCY PROXIMITY STRIP AT ROW 3-8A. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 18,405 hrs · 15,778 cycles

ON FLIGHT 3275 THE CREW REPORTED A BURNING ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICER’S MULTI FUNCTION DISPLAY UNIT IAW EMB-145 AMM 34-22-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLEEVE — DEFECTIVE (WING) · airframe 18,386 hrs · 15,766 cycles

ON FLIGHT 3302 THE CREW REPORTED THAT ON APPROACH THEY DECLARED AN EMERGENCY FOR A WING ANTI-ICE FAIL FOLLOWED BY A BLEED 2 VALVE FAIL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CMC POSTED WING 1 LEAK REPLACED COUPLINGS AT LEFT DUAL TEMP CONTROL VALVE NORMAL PACK OPERATION EMB 145 AMM 21-51-00. OPERATIONAL TEST OF ANTI-ICING SYSYTEM IAW EMB 145 AMM 30-00-00 CHECKS GOOD. BLEED 2 VALVE CHECKS GOOD EMB AMM 36-11-05. REMOVED AND REPLACED COUPLING GOING TO HEAT EXCHANGER IAW EMB 145 AMM 21-51-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 21-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,245 hrs · 15,470 cycles

LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 BATTERY PACK AND CHARGER.

Part: CARTRIDGE — INOPERATIVE (GUST LOCK) · airframe 13,333 hrs · 11,940 cycles

ON FLIGHT 4319 THE CREW REPORTED THAT THE GUST LOCK DID NOT FULLY RELEASE ON TAKEOFF. THE CREW ELECTED TO ABORT THE TAKEOFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH GUST LOCK SPRING CARTRIDGES IAW EMB 145 AMM 27-71-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WHEEL — SEPARATED (MLG) · airframe 10,128 hrs · 9,122 cycles

ON FLIGHT 3992 AFTER TAKEOFF DURING GEAR RETRACTION CREW RECEIVED A L/G DISAGREE AND RIGHT L/G RED. CREW RAN CHECKLIST AND NOTED NORMAL ONLY WHEN GEAR DOWN. CREW RETURNED FOR LANDING AND WAS ADVISED BY CONTROL TOWER THAT THE NR 3 TIRE WAS BLOWN. AFTER LANDING CREW RECEIVED L/G AIR/GND FAIL, BRAKE DISAGREE, PITOT 3 INOP, E1/2 IDLE STOP FAIL MESSAGES. ALSO WASN’T ABLE TO PUT GUST LOCK ON. A/C TOWED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 WHEEL/TIRE ASSEMBLY, RT GEAR BRAKE TEMP HARNESS, WOW HARNESS REPLACED SEVERAL HARNESS CLAMPS, RT MLG WHEEL SPEED TRANSDUCER HARNESS, NUMBER 3 BRAKE LINES. RETRACTION CHECK COMPLETED. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (SERVICE DOOR) · airframe 8,135 hrs · 7,149 cycles

ON FLIGHT 3484 DURING CLIMB AT 280, CREW REPORTED SERVICE DOOR WARNING INDICATION ILLUMINATED. PRESSURIZATION HELD. CREW DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE MEASURED GAPS AROUND SERVICE DOOR AND OPERATIONAL CHECKED THE DOOR, ISSUED MEL 52-04. ADJUSTED MICROSWITCH S7246 IAW EMB 145 AMM 52-74-01. OPERATIONAL TEST GOOD. THIS RESTORES MEL 52-04. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — CHAFED · airframe 5,042 hrs · 4,408 cycles

HEARD CIRCUIT BREAK EBV-2(C-21) POP OUT. REPAIRED CHAFED WIRE AT RELAY K0542 IAW EMB AMM 20-10-00. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 2)

CLIMBING THROUGH 36,000 FEET, THE NR 2 ENGINE OIL QUANTITY STARTED DROPPING AT A STEADY RATE, DIVERTED TO NEAREST SUITABLE AIRPORT. DURING DESCENT OIL LEVEL GOT DOWN TO 3 QUARTS AND OIL PRESSURE WAS FOLLOWING LOWEST PRESSURE NOTED WAS 15 POUNDS PER SQUARE INCH BEFORE SHUTTING DOWN ENGINE. (M)

Part: TUBE — BROKEN (BLEED AIR SYS)

DFW - FLT 3788 - SULFUR INSULATION SMELL IN FLIGHT ACCOMPANIED BY WINDSHIELD FOGGING OVER. NO EICAS MSG RECEIVED. DISCOVERED LARGE BLEED AIR LEAK FROM THE PACK VALVE, PACK INLET BLEED TUBE. REMOVED AND INSTALLED BLEED TUBE IAW EMB145 AMM 31-51-01 AND PACK INLET PRESSURE SENSE LINE IAW EMB 145 AMM 21-80-01. NO LEAKS NOTED. RAN A/C PACK COOLING SYSTEM OPERATING TESTS. NO FAULTS NOTED OR ODORS DETECTED. AIRCRAFT RETURNED TO SERVICE. (M)