N694AE

Part: CLOSET — CONTAMINATED (ZONE 200) · airframe 43,052 hrs · 38,933 cycles

ODOR EMINATING FROM G1 CREW CLOSET BOTTOM AND GALLEY AREA. INSPECTED G1 CREW CLOSET AREA FOUND 2 PLASTIC BAGS WITH DRIED LIQUID RESIDUE. CLEANED AND SANITIZED THE AREA AS REQUIRED. A/C OK FOR SERVICE.

Part: CART — ODOR (GALLEY) · airframe 43,016 hrs · 38,895 cycles

ODOR EMINATING FROM G1 CREW CLOSET BOTTOM. INSPECTED COAT CLOSET ELECTRICAL COMPARTMENT FOUND ALL COMPONENTS AND WIRING IN GOOD CONDITION. CLEANED GALLEY CART STORAGE. ERADICATED THE ODOR FROM GALLEY ACFT OK FOR STORAGE AT THIS TIME.

Part: HINGE FITTING — OUT OF LIMITS (ZONE 300) · airframe 41,608 hrs · 37,259 cycles

F029600 HORIZONTAL STABILIZER LH HINGE FITTING HOUSING #2 INTERNAL DIAMETER OUT OF LIMITS. REPAIRED IAW PIEDMONT EO1-55-25-0066 AND EMB 145 SRM 55-10-02, STEP 2 THRU STEP 2 L, EXCLUDING STEP2 J.

Part: SKIN — DENTED (ZONE 200) · airframe 41,608 hrs · 37,259 cycles

F025768 FUSELAGE SKIN HAS MULTIPLE PROTRUSIONS BETWEEN FRAME 12A AND FRAME 13 AND STRINGERS 06L - 08L. REPAIRED THE PROTRUSIONS BETWEEN FR12A/13 STRINGERS 06L - 08L IAW EMBRAER ETD2025-145-901668

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F023806 PROFILE ANGLE ON RH GALLEY CROSSBEAM AT FR 23 IS CORRODED. RAR PROFILE ANGLE ON RH GALLEY CROSSBEAM AT FR 23 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F024004 GALLEY CENTER FWD DIGITAL IS CORRODED BTWN FR 14-15. REPAIRED CORROSION ON GALLEY CENTER FWD DIGITAL BTW FR 14-15 IAW PIEDMONT EO1-05-25-0065 AND ETD2025-145-900986.

Part: SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F023805 GALLEY RH FWD SILL CORRODED. REMOVED AND REPLACED GALLEY RH FWD SILL IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F023796 LH #1 CABIN FLOOR SILL CORRODED IN 2 PLACES. REMOVED AND REPLACED LH #1 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,608 hrs · 37,259 cycles

F023596 LH OMEGA BEAM CRACKED ON SIDEWALL AT FR28. REMOVED CRACKED (AT FR 28) LH OMEGA BEAM #2 AND INSTALLED NEW SERVICEABLE LH OMEGA BEAM (LH OMEGA BEAM #2) IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022549 LH LOWER SEAT TRACK BETWEEN FR 36 / 45 CORRODED ON NUMEROUS AREAS. RAR SEAT TRACK IAW EMB148 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022542 RH CENTER FLOOR GUSSET BETWEEN FR 35 / 39 CORRODED ON NUMEROUS AREAS. RAR THE RH CENTER FLOOR GUSSET BETWEEN FR35/39 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022536 LH CENTER FLOOR GUSSET BETWEEN FR 46 / 53 CORRODED ON NUMEROUS AREAS. REMOVED AND INSTALLED NEW LH CENTER FLOOR GUSSET BETWEEN FR 46 / 53 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022530 LH# 4 FLOOR BOARD SUPPORT CORRODED. R & R LH# 4 FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022533 RH # 3 FLOOR BOARD SUPPORT CORRODED. RAR RH # 3 FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022537 LH CENTER FLOOR GUSSET BETWEEN FR 38 / 45 CORRODED ON NUMEROUS AREAS. RAR THE LH CENTER FLOOR GUSSET BETWEEN FR38/45 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022548 RH LOWER SEAT TRACK BETWEEN FR 36 / 45 CORRODED ON NUMEROUS AREAS. RAR SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022551 RRH LOWER SEAT TRACK BETWEEN FR 47 / 53 CORRODED ON NUMEROUS AREAS. RAR SEAT TRACK IAW EMB145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022545 RH CENTER FLOOR GUSSET BETWEEN FR 46/ 53 CORRODED ON NUMEROUS AREAS. REMOVED AND REPLACED RH CENTER FLOOR GUSSET BETWEEN FR 46/ 53 (GUSSET #5) IAW EMB145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022543 LH CENTER FLOOR GUSSET BETWEEN FR 35 / 39 CORRODED ON NUMEROUS AREAS. RAR LH CENTER FLOOR GUSSET BETWEEN FR 35 / 39 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022550 LH LOWER SEAT TRACK BETWEEN FR 47 / 53 CORRODED ON NUMEROUS AREAS. RAR SEAT TRACK IAW EMB145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022532 LH# 6 FLOOR BOARD SUPPORT CORRODED. REMOVED & REPLACED L/H #6 FLOOR SILL IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022531 LH# 5 FLOOR BOARD SUPPORT CORRODED. REMOVED AND REPLACED L/H #5 FLOOR SILL IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,508 hrs · 37,259 cycles

F022484 LAV. CENTER FLOOR GUSSET CORRODED AT AFT END. RAR LAV CENTER FLOOR GUSSET IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022515 LH LOWER SEAT TRACK BETWEEN FR 53 / 59 HAS CORRODED AREAS. RAR LH LOWER SEAT TRACK BETWEEN FR 53 / 59 IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022482 LAV. RH FLOOR GUSSET CORRODED AROUND WATER NIPPLES. REMOVED AND REPLACED LAV RH FLOOR GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F022538 RH CENTER FLOOR GUSSET BETWEEN FR 38 / 45 CORRODED ON NUMEROUS AREAS. RAR R/H CENTER FLOOR GUSSET BETWEEN FR 38/45 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F021884 LH CARGO FLOOR BOARD SUPPORT CORRODED AT FR 71. RAR L/H CARGO FLOOR BOARD SUPPORT AT FR 71 IAW EMB 145 SRM 51-40-02

Part: ATTACH FITTING — WORN (ZONE 500) · airframe 41,608 hrs · 37,259 cycles

F021710 LH AILERON ACTUATOR ATTACHMENT FITTING WORN. REMOVED AND REPLACED LH AILERON ACTUATOR ATTACHMENT FITTING IAW PIEDMONT EO1-05-25-0065, EMB145 SRM 51-40-02 AND IC2006-145/-4319-B

Part: ATTACH FITTING — WORN (ZONE 600) · airframe 41,608 hrs · 37,259 cycles

F021742 RH AILERON ACTUATOR ATTACHMENT FITTING WORN. REMOVED AND REPLACED RH AILERON ACTUATOR ATTACHMENT FITTING IAW PIEDMONT EO1-05-25-0065, EMB145 SRM 51-40-02 AND IC2006-1454319-B

Part: TUBE — CORRODED (ZONE 300) · corrosion level 2 · airframe 41,608 hrs · 37,259 cycles

F020973 RH ELEVATOR INBD AND OTBD MASS BALANCE TUBES CORRODED. REPAIRED CORROSION ON RH ELEVATOR INBD AND OTBD MASS BALANCE TUBES IAW PIEDMONT EO1-05-25-0065, PIEDMONT FCD1-55-19-0312, IC2003-14-1934A AND SB 145-55-0040A

Part: TUBE — CORRODED (ZONE 300 ELVTR) · corrosion level 2 · airframe 41,605 hrs · 37,259 cycles

F020971 LH ELEVATOR INBD AND OTBD MASS BALANCE TUBES CORRODED. REPAIRED CORROSION ON LH ELEVATOR INBD AND OTBD MASS BALANCE TUBES IAW PIEDMONT EO1-05-25-0065, PIEDMONT FCD1-55-19-0312, IC2003-14-1934A AND SB 145-55-0040A

Part: SKIN — CANNING (ZONE 200) · airframe 41,608 hrs · 37,259 cycles

F020270 FUSELAGE SKIN HAS PREVIOUSLY ADDRESS PROTRUSION AREA THAT HAS AN OIL CANNING TYPE MOVEMENT WHEN PRESSED ON, LOCATED AT FRAME 21, BETWEEN STRINGERS12-13L. REPAIRED FUSELAGE SKIN WITH PREVIOUSLY ADDRESSED PROTRUSION WITH OIL CANNING TYPE MOVEMENT AT FR 21, BTW STR 12L-13L IAW PIEDMONT EO1-53-25-0039 AND EMB 145 SRM 53-21-01 RE, ITEM 5, FIG 202.

Part: SKIN — DENTED (ZONE 600) · airframe 41,608 hrs · 37,259 cycles

F020018 RH WING L/E #1 HAS DENT APROX 50 INCHES FROM INBD EDGE. INSTALLED REPAIR DOUBLER/ SPLICE PLATES AND SKIN PATCH ON RH WING LE APPROXIMATELY 50" FROM INBD EDGE IAW EMB 145 SRM 57-40-00 ITEM 2 FIG. 201 AND EO1-57-25-0060

Part: SKIN — SCRATCHED (ZONE 500) · airframe 41,608 hrs · 37,259 cycles

F020017 LH WING L/E #1 HAS SCRATCH JUST OUTBD AND FWD OF ANTI SKID PAINTED AREA. SCRATCH OUT OF BLEND LIMITS. REPAIRED IAW EMB 145 SRM 57-40-00 ITEM 2 FIG. 201 AND EO1-57-25-0061.

Part: NONE — NONE · airframe 41,406 hrs · 37,005 cycles

MAIN PASSENGER DOOR NOT OPENING PROPERLY-C/A-LUBED ON MAIN DOOR FRAME ROLLERS REF AMM 53-21-02. PERFORMED OPC OPEN/CLOSE AND INTERNAL ACTUATING HANDLE ON MAIN DOOR REF AMM 52-18-00. OPC GOOD AT THIS TIME.

Part: NONE — NONE · airframe 41,314 hrs · 36,906 cycles

FLIGHT ATTENDANTS BOTH REPORT THAT MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE.-C/A-LUBRICATED MAIN DOOR ROLLERS LOCKS AND BUMPERS IAW AMM CH 52-18-00.

Part: NONE — NONE · airframe 40,897 hrs · 36,419 cycles

WHIFF OF STRONG ELECTRICAL BURNING ODOR LASTED ABOUT 10 SECOUNDS. 3 - 5 MINUTES INTER CA SIDE MFD TURNED OFF FOR 10 SECONDS-C/A-CA PENDING

Part: NONE — INOPERATIVE (RH) · airframe 40,807 hrs · 36,328 cycles

RH OVERWING EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPC GOOD.

Part: NONE — BROKEN (FWD CABIN) · airframe 40,615 hrs · 36,125 cycles

FORWARD CABIN FA FLASHLIGHT CRADLE RETAINING CLIP BROKEN-C/A-REMOVED & REPLACED FWD FLASHLIGHT IAW ETN EM-33-059 , MM 33-50-16

Part: NONE — NONE · airframe 40,198 hrs · 35,645 cycles

AFT EMERGENCY LIGHTS AND OUTSIDE EMERGENCY LIGHTS ARE ON IN ARM POSITION-C/A-RAR #4 EMER BATTERY AND CHARGER BASE IAW EMB 145 AMM 33-50-04 OPC AND FUNC CHK GOOD

Part: NONE — NONE · airframe 40,143 hrs · 35,580 cycles

DUE TO EMERGENCY LIGHTS INOP. REPLACE #4 BATTERY AND CHARGER.-C/A-RAR #4 BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECK GOOD.

Part: NONE — NONE · airframe 40,143 hrs · 35,580 cycles

DUE TO EMERGENCY LIGHTS INOP. REPLACE #3 BATTERY AND CHARGER.-C/A-RAR #3 BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECK GOOD.

Part: NONE — NONE · airframe 40,143 hrs · 35,580 cycles

DUE TO EMERGENCY LIGHTS INOP. REPLACE #2 BATTERY AND CHARGER.-C/A-RAR #2 BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECK GOOD

Part: NONE — NONE · airframe 40,143 hrs · 35,580 cycles

DUE TO EMERGENCY LIGHTS INOP. REPLACE #1 BATTERY AND CHARGER.-C/A-RAR EMERGENCY LIGHTS #1 BATTERY AND CHARGER IAW AMM 33-50-04 OPT CHECK GOOD.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 39,073 hrs · 34,349 cycles

AFTMOST CABIN EMERGENCY LIGHT STRIP INOP-C/A-RAR AFTMOST CABIN EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12 OPS CHECK GOOD

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,404 hrs · 33,624 cycles

AFT EMERGENGY FLASHLIGHT CRADLE BROKEN MEL 2553-AUTH 01-193-C. C/A: R & R AFT EMERGENCY FLASHLIGHT AND CRADLE ASSEMBLY, IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPERATIONS CHECK GOOD. MEL RESTORED.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,374 hrs · 33,592 cycles

AFT EMERGENCY FLASHLIGHT CRADLE BROKEN. C/A: DEFERRED PER MEL 25-53 AUTH 010193-C EXP 01/22/21 M PROCEDURES COMPLIED WITH.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,014 hrs · 33,223 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR EXTERNAL EMERGENCY LIGHT, IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SWITCH — FAILED (CONTROL YOKE) · airframe 37,902 hrs · 33,106 cycles

TAXING INTO DFW FOS' PUSH TO TALK BUTTON ON. CONTROL YOKE STARTED SMOKING HAD SMOKE AND ELECTRICAL SMELL IN COCKPIT. C/A R & R FO'S AP/TRIM/PUSHER DISC SWITCH, IAW EMB145 AMM 22-11-07. AP FUNCTIONAL TEST GOOD, IAW EMB145 AMM 22-11-00.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 37,851 hrs · 33,050 cycles

DURING PS-1 CHECK FOUND RT EXTERNAL EMERGENCY ABOVE WING INOPERABLE. C/A-RAR RT EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER CONTROL) · airframe 37,819 hrs · 33,028 cycles

DURING CLIMB RUDDER SYSTEM 1-2 INOP DECLARED EMERGENCY FLIGHT CONTINUED-C/A-FOLLOWED FIM TASK 27-22-00-810-804-A . RAR #2 RUDDER PRESSURE SWITCH IAW EMB-145 AMM 27-23-04. OPS CHEK GOOD IAW EMB-145 AMM 27-23-00.

Part: ROLLER — FOD (MAIN PAX DOOR) · airframe 37,697 hrs · 32,916 cycles

MAIN CABIN DOOR STICKS WHEN OPENING FA NEEDED HELP TO OPEN. CLEANED FOD FROM MAIN CABIN DOOR ROLLERS REF 52-18-00. DOOR OPERATES GOOD IN REF TO E145 AMM 52-18-00

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 37,681 hrs · 32,898 cycles

DURING ICE PROTECTION TEST (PNEUMATIC IN FLIGHT) DURING CLIMB AT FL190, PRESSURIZATION EXPIRENCED ABNORMAL CABIN RATE FLUCUATIONS. QRH PROC COMPLIED WITH. NEITHER AUTO OR MANUAL CONTROL OF CABIN POSSIBLE. IN MAN MODE CABIN RATE FLUCUATED AND WAS UNRELATED TO MAN CONTROL KNOB POSITION. TROUBLESHOT CABIN PRESSURIZATION AS FOLLOWS: PERFORMED GVI OF PAC 2 IAW AMM 21-51-00. NO DEFECTS NOTED. PERFOMED ICE DETECTION TEST WITH BOTH ENGINES RUNNING IAW AMM 30-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. PERFORMED ENGINE RUN OF BOTH ENGINES IAW AMM 71-00-01 AND PERFORMED PRESSURIZATION TEST IN MANUAL AND AUTO MODE IAW AMM 21-31-00. OPS CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY. A/C OKAY FOR SERVICE

Part: ENGINE — ODOR (LEFT) · airframe 37,585 hrs · 32,831 cycles

SUPPLMENTAL BURNING SMELL PRESENT AT LOW ALTITUDE, BURING PLASTIC OR RUBBER. C/W FIM TASK 21-20-00-810-801 STEPS 1-10. NO FAULTS FOUND AT THIS TIME. PERFORMED DVI OF LT & RT RELAY PANELS LOOKING FOR DAMAGE, BURNT ITEMS & SMOKE SMELL. NO DISCREPANCIES FOUND AT THIS TIME. PERFORMED DVI OF LT AND RT ELECTRICAL DISTRIBUTION BOXES BEHIND PILOT AND FO INSPECTING BOTH FRONT AND BACK SIDES LOOKING FOR DAMAGE, BURNT ITEMS & SMOKE SMELL. NO DISCERAPNCIES NOTED AT THIS TIME. PERFORMED DVI OF BOTH PACKS WHILE RUNNING LOOKING FOR BLOWN DUCTS, DAMAGED OR LEAKING HEAT EXCHANGERS/CONDENSER MIXER. PERFORMED DVI OF BOTH RECERC FANS LOOKING FOR DAMAGE OR ELECTRICAL BURNING SMELL AND PROPER OPERATION IAW AMM 21-20-00-700-801-A. NO FAULTS FOUND AND NO SMELLS NOTED. PERFORMED DVI OF AIRCRAFT DUCTING UNDER FLOOR LOOKING FOR BLOWN OR DAMAGED DUCTS OR BROKEN JOINTS IAW AMM 21-20-04. NO DEFECTS NOTED. PERFORMED OPS CHECK OF ELECTRONIC COMPARTMENT VENTILATION SYSTEM IAW AMM 21-26-00. OPC GOOD PERFORMED IAW ETN-EM-72-034. FOUND ENGINE ODOR EMANATING FROM NR 1 ENGINE REF NRWC 694-ORD-04815 FOR DISCREPANCY. REPLACED PACK 1 OVER TEMP SWITCH IAW AMM 21-51-08 AND OVER PRESS SWITCH IAW AMM 21-51-06 DID NOT FIX PROBLEM. T/S PERFORMED ODOR EVENT ETN-EM-72-034. PERFORMED OPERATIONAL CHECK OF THE PACK SYSTEM IAW AMM TASK 21-51-00. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF THE AIR BLEED SYSTEM IAW AMM TASK 36-00-

Part: FAN — FAILED (LEFT) · airframe 37,545 hrs · 32,794 cycles

SMELL OF BURNING ELECTRONICS IN COCKPIT. C/A-REMOVED AND REPLACED LT RECIRCULATION FAN IAW 21-24-01. OPS CK AND LEAK CK GOOD. REMOVED AND REPLACED FUSE F0060 IAEW 20-13-08. REMOVED AND REPLACED RT RECIRCULATION FAN IAW AMM 21-24-01 OPS CHECK GOOD, LEAK CHECK GOOD. PERFORMED ENG ODOR EVENT ETN IAW ETN-EM-72-034 NO ODOR NOTED, NO DEFECTS NOTED. PERFORMED GVI OF FLASHLIGHTS IAW AMM 33-51-01. FUSE P/N 100FU01-030; RECIRCULATION_GASPER FAN P/N 4611028900 S/N 0997 FUSE P/N 100FU01-030; RECIRCULATION_GASPER FAN P/N 4611028900 S/N 0997.

Part: DUCT — UNSECURE (AC BAY) · airframe 37,538 hrs · 32,784 cycles

SUPPLEMENTAL FOUL SMELL COMING STRONG OUT OF FRONT AIRPLANE VENTS (DIRTY SOCK) OZONE STALE SMELL PACK1 ASSOCIATED. DEFERRED PACK 1 IAW MEL 21-30 AUTH 050203-D-C EXPIRATION 5/30/2020. FOUND DUCT OFF ON LT RAM AIR VALVE. RESECURED DUCT IAW AMM 21-25-01-04. OPS CHECK PACK SYS IAW AMM 21-00-00-02. OPC GOOD. MEL ITEM RESTORED.

Part: CHARGER — FAILED (CABIN) · airframe 37,477 hrs · 32,714 cycles

REMOVE AND REINSTALL #1 EMERGENCY BATTERY POWER SUPPLY -C/A-REMOVED AND REPLACED THE #1 BATTERY AND CHARGER IAW EMB 145 AMM 33-50-04, SYS CKS GOOD.

Part: FRAME — GOUGED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

FR 65 Z FRAME IS GOUGED AROUND 7 SCREW HOLES LH SIDE-C/A-PERFORMED REPAIR TO FR 65Z IAW ERS-EM-53MR-4084 REV1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SSI 53-20-11 LH OMEGA BEAM SIDEWALL IS PITTED ABOVE CROSSBEAM AT FR 44.-C/A-ACCOMPLISHED LH OMEGA BEAM REPAIR IAW ENVOY ERS-EM-53MR-4089

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SSI 53-20-11 LH OMEGA BEAM CORRODED ON THE SIDE AT FR 29 CROSS BEAM-C/A-ACCOMPLISHED LH OMEGA BEAM REPAIR IAW ENVOY ERS-EM-53MR-4090

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,477 hrs · 32,714 cycles

EMERGENCY LIGHT STRIP WIRE AFT OF CONNECTOR SP9115 HAS BROKEN STRANDS MARKED. FOUND ON CLOSE UP.-C/A-REPAIRED WIRE W192-8760-22 AFT OF SPLICE SP9115 IAW EMB 145 SWPM 20-21-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 37,477 hrs · 32,714 cycles

EMERGENCY LIGHT STRIP WIRE AFT OF CONNECTOR SP9036 HAS DAMAGED INSULATION.FOUND ON CLOSE UP.-C/A-REPAIRED WIRE INSULATION ON W192-8679-22 AFT OF SPLICE SP9036 IAW EMB 145 SWPM 20-21-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,477 hrs · 32,714 cycles

FLOOR PROXIMITY LIGHT STRIP # 6 WIRE BROKE OFF LIGHT.FOUND ON CLOSE UP.-C/A-REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP # 6 IAW EMB 145 AMM 33-50-12. SEE NRTC BOW339262 FOR OPS CHECK.

Part: RIB — CRACKED (LT WING) · airframe 37,477 hrs · 32,714 cycles

LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB-C/A-INSTALLED REPAIR (DOUBLER,FILLER,SHIM) FOR LH WING RIB 21 INSIDE PANEL 551CB IAW EMB 145 SRM 57-20-07,FIGURE 203

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SSI 53-20-11 LH OMEGA BEAM CORRODED AT CROSS BEAM BTW FR 33-34-C/A-INSTALLED REPAIR DOUBLER FOR LH OMEGA BEAM AT CROSS BEAM BTW FR 33-34 IAW EMB 145 SRM 53-22-10RE, FIGURE 203

Part: WEB — CRACKED (CARGO DOOR) · airframe 37,477 hrs · 32,714 cycles

SSI 52-30-08 CORROSION ON CARGO DOOR WEBBING. (3 EACH MARKED)-C/A-PERFORMED DOUBLER REPAIR ON CARGO DOOR WEBBING IAW EMB145 SRM 52-30-01 AND ETN-EM-52-043

Part: STRUCTURE — DAMAGED (LAV SERVICE) · airframe 37,477 hrs · 32,714 cycles

LAVATORY BUCKET MOUNTING FLANGE FOUND TO HAVE MULTIPLE ELONGATED HOLES AT INBOARD SIDE-C/A-INSTALLED NEW LAVATORY BUCKET MOUNTING FLANGE DIGITAL IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SERVICE DOOR CUTOUT STRUCTURE ENTRENCE SILL HAS CORROSION AT NUT PLATE HOLES-C/A-REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 37,477 hrs · 32,714 cycles

CARGO DOOR SKIN IS CRACKED NEAR EXTERNAL HANDLE-C/A-INSTALLED REPAIR FILLER AND DOUBLER IAW EMB 145 SRM 52-30-01

Part: SKIN — CRACKED (CARGO DOOR) · airframe 37,477 hrs · 32,714 cycles

CARGO DOOR SKIN IS CRACKED NEAR EXTERNAL HANDLE-C/A-PERFORMED PERMANENT REPAIR TO CARGO DOOR SKIN CRACK NEAR EXTERNAL HANDLE IAW ERS-EM-52MR-1074

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

FR 73 IS CRACKED BETWEEN STR 17R-16R-C/A-REMOVED AND REPLACED FR 73 BTW FR 17L-15R IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SSI 53-30-48 FR 65 SHEAR CLIP IS CORRODED BETWEEN STR 17L-16L-C/A-PERFORMED SPLICE REPAIR PER SRM 53-31-04, FIGURE 212

Part: MOUNT BRACKET — CRACKED (LT ENGINE) · airframe 37,477 hrs · 32,714 cycles

LH PYLON FWD LOWER YOKE FWD ENGINE MOUNT BRACKET IS CRACKED-C/A-ACCOMPLISHED REPAIR OF LH PYLON FWD LOWER YOKE FWD ENGINE MOUNT BRACKET IAW ENVOY ERS-EM-54MR-698

Part: STRUCTURE — CORRODED (LAV SERVICE) · airframe 37,477 hrs · 32,714 cycles

LAV BUCKET INSIDE WASTE PANEL HAS CORROSION-C/A-APPLIED SEALANT AND INSTALLED SERVICEABLE LAV BUCKET IAW EMB 145 SRM 51-20-01 AND 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,477 hrs · 32,714 cycles

SSI 53-30-48 CARGO DOOR LOWER SILL IS CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,286 hrs · 32,544 cycles

#7 EMER FLOOR LIGHT STRIP, WIRE BROKEN-C/A-REMOVED AND REPLACED #7 EMER LIGHT STRIP IAW EMB 145 AMM 33-50-12

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,284 hrs · 32,539 cycles

NUMBER 7 EMERGENCY LIGHT, WIRE BROKEN.-C/A-REMOVED AND REPLACED NUMBER 7 EMERGENCY LIGHT IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,284 hrs · 32,539 cycles

#5 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE A/C SIDE-C/A-REPAIRED #5 EMERGENCY LIGHT STRIP IAW EMB 145 SWPM 20-50-00. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,268 hrs · 32,521 cycles

LH FWD OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH FWD OVER WING EMERGENCY LIGHT LAMP IN REFERANCE WITH 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. TROUBLESHOOTING IAW FIM 33-50-00-810-804 REMOVED AND REPLACD BATTERY POWER SUPPLY UNIT IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A AND REMOVED AND REPLACED BATTERY PACK IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. NO FIX. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 108214. DEFERRED PER MEL 33-29 AUTH #011063D-C. REMOVED AND REPLACED #1 POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD AT THIS TIME. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N 24646. REMOVED AND REPLACED BATTERY HOLDER ASSY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD AT THIS TIME. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 24646. REMOVED AND REPLACED EMERGENGY LIGHT INVERTER IAW EMB 145 AMM 33-50-11, OPS CHECK GOOD AT THIS TIME, MEL RESTORED

Part: APU — FUMES · airframe 37,131 hrs · 32,389 cycles

FUMES DETECTED IN COCKPIT AND CABIN OF ELECRICAL AND OR OIL IN SOURCE.-C/A-ACCOMPLISHED FIM TASK 21-20-00-810-803-A AND ETN EM-72-034, FOUND APU TO BE CAUSE OF OIL FUMES IN COCKPIT WITH PACK 1 ON. DEFFERED APU "M PROCEDURES COMPLIED WITH" AUTH 010215DM-C REF 49-01

Part: UNKNOWN — ODOR (CABIN) · airframe 36,907 hrs · 32,166 cycles

AIR CONDITIONING PACK NR 1 PRODUCING AN OILY SMELL & NOT COOLING VERY WELL. PERFORMED A NR 1 PACK OPS CHECK IAW AMM 21-51-00. PERFORMED ETN -EM -72-034-ENG ODOR EVENT TROUBLESHOOTING. NO ODOR WAS DETECTED AND SYS WAS COOLING PROPERLY. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,551 hrs · 31,885 cycles

OVERWING EMERGENCY EXIT CEILING AFT SIGN INOP. REMOVED AND REPLACED #4 EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD

Part: ACM — FAILED (AC BAY) · airframe 35,701 hrs · 30,999 cycles

PACK 2 OVHTIN FLIGHT RESOLVED WITH QRH UPON LANDINGPACK 1&2TEMP CONTROL UNRESPNSIVE WITH EITHER BLEED CONFIG AND RUBBER SMELL. C/A-C/W EO EM-2100-048, REMOVED AND REPLACED #1 ACM AND CONDENSER/MIXER IAW AMM 21-51-03 AND 21-51-04, PERFORMED ODOR EVENT TROUBLESHOOTING AS PER ETN-EM-72-034 , NO ODOR NOTED. COMPLIED WITH WORK SCOPE DATED 05/28/19 REV 0. SENT PICTURES OF THE ACM TURBINE OUITLET TO REPEAT CONTROL AND FLEET MANAGER AS REQUIRED. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,097 hrs · 30,355 cycles

FLOOR EMERGENCY PROX LIGHT STRIP BETWEEN SEATS 7 THROUGH 9 INOP. REMOVED AND REPLACED FLOOR EMERGENCY PROX LIGHTS STRIP BETWEEN SEATS 7 THROUGH 9 IAW AMM 33-50-12. OPS CHECK GOOD.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 34,726 hrs · 30,027 cycles

FWD CABIN FLASHLIGHT CRADLE BROKEN-C/A-RAR FWD CABIN FLASHLIGHT CRADLE IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A..NO FURTHER DEFECTS NOTED AT THIS TIME END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,606 hrs · 29,921 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-RAR LAMP IN COCKPIT EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A OPC GOOD

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 34,275 hrs · 29,643 cycles

AFT FLASH LIGHT CRADLE BROKEN. -C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT ASSY IAW AMM 33-50-16-000-801-A/33-50-16-400-801-A OPC GOOD.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 34,112 hrs · 29,465 cycles

FA FLASHLIGHT DAMAGED. REMOVED AND REPLACED FA LASHLIGHT ASSY IAW AMM 33-50-16 OPS CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 33,558 hrs · 28,983 cycles

LAVATORY SMOKE WARNING MESSAGE DURING FLIGHT. FLIGHT ATTENDANT STATED NO EVIDENCE OF FIRE, FUMES, OR SMOKE. COMPLIED WITH AN OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM. OPS CHECKED GOOD IAW AMM 26-14-00.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 33,028 hrs · 28,515 cycles

LEFT FWD LOWER EXTERIOR EMERGENCY LIGHT INOPERATIVE, TROUBLESHOT THE EMERGENCY LIGHT IAW WM 33-50-50, FOUND THE NR 1 EMERGENCY LIGHT POWER SUPPLY DEFECTIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (RUDDER) · airframe 32,298 hrs · 27,867 cycles

NUT PLATE FOR PROTRACTOR MOUNT POINT MISSING, RIVETS PULLED THROUGH RUDDER SKIN. CUT OUT THE DAMAGED SKIN, FABRICATED A FILLER AND DOUBLER AND INSTALLED A NEW NUT PLATE IAW SRM 55-40-01.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,298 hrs · 27,867 cycles

AFT SIDE OF CENTER AISLE CEILING EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REPLACED CENTER AISLE AFT EXIT LOCATING SIGN ASSEMBLY AND PERFORMED OPERATIONAL TEST. OPERATIONAL TEST GOOD IAW AMM 33-50-15 AND 33-50-00

Part: WIRE — DAMAGED (CABIN) · airframe 32,298 hrs · 27,867 cycles

WIRE CONNECTORS FOR CABIN FLOOR LIGHTING STRIPPED FROM WIRES BETWEEN FRAMES 58-59, STRINGERS 19-21L, UNDERNEATH FLOOR PANEL 251HF. REPAIRED WIRING FOR EMERGENCY LIGHT AT FRAME 58-59 IAW SWPM 20-21-00, LIGHT OPS CHECK GOOD IAW AMM 33-50-00-700-801.

Part: SHEAR TIE — CORRODED (FRAME 60) · airframe 32,298 hrs · 27,867 cycles

CORROSION ON THE SHEAR TIE AT FRAME 60, BETWEEN STRINGERS 20R - 21R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: FRAME — BENT (FRM 72) · airframe 32,298 hrs · 27,867 cycles

FRAME 72 BENT. REPAIRED THE FRAME IAW SRM 53-00-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,298 hrs · 27,867 cycles

CRACK IN SHEAR CLIP FR 24 BETWEEN STR 16-17R. REMOVED AND REPLACED SHEAR CLIP FR 24 STR 16R-17R IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,298 hrs · 27,867 cycles

CRACK IN SHEAR CLIP FR 26 BETWEEN STR 15L -16L. REMOVED AND REPLACED SHEAR CLIP, PRE-TREATED ALL BARE METAL, PRIMED AND APPLIED TOP COAT FR 26 BETWEEN STR 15L-16L IAW SRM 51-40-02, CPM 51-21-04 51-21-05 AND 51-21-06.

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 32,298 hrs · 27,867 cycles

CRACKED SHEAR TIE, FRAME 26 BETWEEN STRINGERS 15R - 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 32,298 hrs · 27,867 cycles

CRACK IN SHEAR TIE AT FRAME 25 BETWEEN STRINGERS 15R - 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,298 hrs · 27,867 cycles

CRACK IN LT OMEGA BEAM O/B SUPPORT FROM FR 47-48. REMOVED AND REPLACED LT OMEGA BEAM O/B SUPPORT BETWEEN FR 47 -48 IAW SRM 53-23-02.

Part: BUSHING — MISSING (PAX DOOR) · airframe 32,298 hrs · 27,867 cycles

PAX DOOR HINGE ARM FRAME SIDE TOP UPPER FITTING BUSHING MISSING-C/A-REAMED PAX DOOR HINGE ARM FRAME SIDE TOP UPPER FITTING BUSHING TO .5938 DIAMETER TO INSTALL NEW OVERSIZED BUSHING IAW EMB 145 SRM 52-18-02. FABRICATED REPAIR BUSHING IAW SRM 52-18-02,INSTALLED REPAIR BUSHING ON PAX DOOR HINGE ARM FRAME SIDE TOP UPPER FITTING IAW SRM 51-20-09

Part: OIL COOLER — MALFUNCTIONED (NR 2 ENG OIL) · airframe 31,573 hrs · 27,170 cycles

CLIMBING THROUGH 11 - 12,000FT, THE NR 2 ENGINE OIL TEMP WENT TO 158 DEGREES, REDUCED POWER, RAN CHECKLIST WHILE BRING POWER BACK UP TEMP FLUCTUATED A FEW TIMES THEN RETURN TO NORMAL WITH LIMITS FOR CRUISE POWER. REMOVED AND REPLACED THE NR 2 AIR OIL COOLER IAW MM 79-25-10, LEAK AND OPS CHECKED GOOD IAW MM 72-00-00. BOTH ENGS. 90 DEGREE C AFTER THREE MINUTES.

Part: SENSOR — FAILED (OIL TEMP) · airframe 31,403 hrs · 26,993 cycles

DURING DESCENT OUT OF FL 250, DISCOVERED THE NR 2 ENGINE OIL TEMP IN RED, INDICATION SHOWING 156 DEGREES AND CLIMBED TO 205 DEGREES, DURING AN IDLE DESCENT. OIL TEMP DID DECREASE TO GREEN RANGE FOR ABOUT 2 MINUTES THEN CLIMBED BACK TO RED RANGE AGAIN. A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. NO FIRE OR SMOKE INDICATING IN FLIGHT OF AFTER LANDING, LANDED SINGLE ENGINE. POSTFLIGHT FOUND SMOKE LIKE STAIN. REMOVED AND REPLACED OIL TEMPERATURE SWITCH IAW MANUAL 79-31-10. R & R OIL LOW PRESSURE SWITCH IAW MANUAL 79-33-10. OPS & LEAK CHECKED GOOD.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 31,249 hrs · 26,858 cycles

ELECTRICAL SMOKE IN THE CABIN ENROUTE. REMOVED AND REPLACED REAR EMERGENCY FLASHLIGHT IAW-EMB-AMM-33-50-16. NO DEFECTS NOTED.

Part: PROXIMITY SWITCH — FAILED (RT SPOILER) · airframe 30,146 hrs · 25,914 cycles

SPOILER FAIL MESSAGE ON EICAS SPOILER DID NOT OPEN, BUT SPLRS INDICATED OPEN ON EICAS WITH SPEED BRAKE CLOSED MESSAGE. CLEARED AFTER 5 MINUTES REPEAT ISSUE SEE LOGPAGE 3967284 ITEM 2. REPLACED RT I/B SPOILER PROX SWITCH IAW 27-63-04. OPS CHECK GOOD IAW 27-63-01.

Part: WARNING LIGHT — FALSE ACTIVATION (SPOILERS) · airframe 30,129 hrs · 25,896 cycles

SPOILER FAIL MESSAGE ON EICAS WITH SPEEDBRAKE OPEN DURING DESCENT. WOULD NOT CLEAR. RAN QRH PROCEDURE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED AN OPS CHECK OF SPOILER SYSTEM IAW AMM 27-63-01. OPS CHECK AND LEAK CHECK GOOD

Part: TRANSDUCER — MALFUNCTIONED (NR 1 ENGINE) · airframe 28,527 hrs · 24,360 cycles

E1 ANTI-ICE FAIL CAUTION ON EICAS FOLLOWED BY E1 ANTI-ICE OVER PRESSURE ADVISORY. R & R NR 1 PRESS TRANSDUCER IAW AMM 30-21-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,526 hrs · 24,359 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R LAMP IN MAIN CABIN DOOR EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,099 hrs · 23,984 cycles

FLASHLIGHT BEHIND PILOT SEAT INOPERATIVE. R & R FLASHLIGHT BEHIND PILOT SEAT IAW AMM 33 0-16. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 ABOVE STRINGER 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 ABOVE STRINGER 2R IAW ERS-EM-53MR-1791.

Part: SKIN — CRACKED (RUDDER) · airframe 28,036 hrs · 23,934 cycles

RUDDER II LOWER RT SIDE, SKIN CRACKED. PERFORMED DOUBLER REPAIR ON RT RUDDER II IAW ERS-EM-55MR-380.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,036 hrs · 23,934 cycles

EMERGENCY LIGHTS ON CABIN CEILING PANELS 253CLC & 263ALC ARE INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED OK. BATTERY CHARGER ASSEMBLY PN 11-0049.

Part: WIRE — DAMAGED (CABIN) · airframe 28,036 hrs · 23,934 cycles

LEFT NR 2 EMER LIGHT STRIP WIRES PULLED OFF. R & R LT NR 2 FLOOR EMER LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 ABOVE STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-1790.

Part: WIRE — BROKEN (CABIN) · airframe 28,036 hrs · 23,934 cycles

AFT EXIT SIGN AT 252CRW HAS BROKEN WIRE, ACFT SIDE. INSTALLED CONNECTOR ON WIRE W192-8743-22, ACFT SIDE, AT SP9104 IAW SWPM 20-50-00.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 28,036 hrs · 23,934 cycles

R & R NR 3 EMER LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER. R & R BATTERY ASSEMBLY & BATTERY CHARGER ASSEMBLY IAW WC 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049.

Part: SKIN — CHAFED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

FUSELAGE SKIN CHAFED UNDER PANEL 414DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 414DB IAW ERS-EM-53MR-1778.

Part: CONNECTOR — MISSING (CABIN) · airframe 28,036 hrs · 23,934 cycles

EMERGENCY LIGHT STRIP CONNECTOR AT FLOOR PANEL 261BF MISSING, ACFT SIDE. INSTALLED MISSING CONNECTOR AT FLOOR PANEL 261BF, ACFT SIDE, SP9212 WIRE NR W192-8832-22 IAW SWPM 20-50-00.

Part: SKIN — CHAFED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

FUSELAGE SKIN CHAFED UNDER PANEL 424DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 424DB IAW ERS-EM-53MR-1779.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

TOP OF FRAME 66 CRACKED AT LAST FASTENER HOLE AT CARGO DOOR LOWER SILL. REPAIRED TOP OF FRAME 66 CRACKED AT LAST FASTENER HOLE IAW ERS-EM-53MR-1772.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

TOP OF FRAME 6, CRACKED AT LAST FASTENER HOLE AT CARGO DOOR LOWER SILL. REPAIRED TOP OF FRAME 67, CRACK AT LAST FASTENER HOLE IAW ERS-EM-53MR-1772.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

CARGO DOOR SILL HAS AREAS OF CORROSION. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,036 hrs · 23,934 cycles

LEFT NR 1 EMER LIGHT STRIP WIRES PULLED OFF. R & R LT NR 1 FLOOR EMER LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

RIGHT AFT FUSELAGE SKIN CRACKED AT FASTENER AREA FRAME 75, BELOW STRINGER 2R. REPAIR SATISFACTORILY ACCOMPLISHED IAW ERS-EM-53MR-1791.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

RIGHT BEAM INBD SUPPORT IS CRACKED, BETWEEN FRAME 47 & 48. REMOVED CRACKED RT BEAM INBD SUPPORT, BETWEEN FRAME 46 - 50. INSTALLED SERVICEABLE RT BEAM INBD SUPPORT, BETWEEN 46 - 50 IAW SRM 51-40-02.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 28,036 hrs · 23,934 cycles

AFT CABIN FLASHLIGHT INTERMITTENT. R & R CABIN FLASHLIGHT IAW 145-EEL-08-12.

Part: STRUCTURE — CRACKED (CABIN) · airframe 28,036 hrs · 23,934 cycles

FLOOR EXTRUSION AT 231FF IS CRACKED. R & R FLOOR EXTRUSION AT 231FF IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,036 hrs · 23,934 cycles

LEFT AFT FUSELAGE SKIN CRACKED AT FASTENER AREA FRAME 75, BELOW STRINGER 2L. LEFT AFT FUSELAGE SKIN CRACKED FRAME 75 SATISFACTORILY ACCOMPLISHED IAW ERS-EM-53MR-1790. SEE TURNOVER FOR DETAILS.

Part: CHECK VALVE — FAILED (BRAKE SYSTEM) · airframe 28,036 hrs · 23,934 cycles

EMERGENCY PARKING BRAKE SYS RETURN LINE CHECK VLV FAILED OPERATIONAL CHECK. R & R EMER PARKING BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-44-08. LEAK CHECKED GOOD. TQ WR EASI 8301.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,963 hrs · 23,852 cycles

FLIGHT ATTENDANT AFT FLASHLIGHT INOPERATIVE. R & R AFT FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A.

Part: TIRE — WORN (NLG) · airframe 27,838 hrs · 23,729 cycles

NOSE WHEEL VIBRATES AT HIGH SPEED ON LANDING. FOUND NOSE TIRES TO BE WORN & OUT OF ROUND. R & R BOTH NOSE WHEEL & TIRE ASSEMBLIES IAW WC 32-700-17. NLG WHEEL NR 2 PN 31551 & SN 17182940P.

Part: SCREW — STRIPPED (EXTERIOR LIGHT) · airframe 27,827 hrs · 23,716 cycles

FOUND A STRIPPED OUT SCREW ON THE LT OVERWING EMER LIGHT. R & R LT OVERWING EXTERNAL EMER LIGHT ASSEMBLY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 27,462 hrs · 23,378 cycles

FORWARD CABIN EMERGENCY FLASH LIGHT INOPERATIVE. R & R FORWARD EMERGENCY FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 27,281 hrs · 23,209 cycles

HYD 1 PUMP FAIL & HYD 1 LOW QTY IN FLIGHT. ELEC PUMP HELD AT 2900 PSI REMAINDER OF FLIGHT. UPON LANDING ELEC PUMP WENT TO 100 PSI & LOST STEERING. TRANSFERRED TO NRWC 694-ORD-02076. FROM NRWC 694-ORD-02076, REPLACED E1 HYD PUMP IAW AMM 29-10-03. REF ITEM'S 2 & 3 LOG PAGE 3922807 & ITEM NR 1 LOG PAGE 3922808 FOR REPLACEMENT OF E1 HYD HOSE & CARBON SEAL. R & R NR 1 ENG HYD HOSE & HYD PUMP IAW AMM 29-10-13.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,849 hrs · 22,826 cycles

AFT EMER FLASHLIGHT BY LAVATORY INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 26,416 hrs · 22,459 cycles

FIRST OFFICER`S FLASHLIGHT EMITTING ELEC ODOR. REPLACED FIRST OFFICER`S FLASHLIGHT IAW 33-50-16.

Part: LENS — OUT OF ADJUST (FLASHLIGHT) · airframe 26,042 hrs · 22,153 cycles

FIRST OFFICER'S FLASHLIGHT IS BROKEN. PERFORMED FIRST OFFICER'S FLASHLIGHT LENS ADJUSTMENT & PERFORMED OPERATIONS CHECK & FOUND WORKING PROPERLY IAW AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,929 hrs · 22,038 cycles

RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-04. EMER LIGHTING BATTERY PN 2013-1A & SN 103960.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,881 hrs · 21,990 cycles

RIGHT OVERWING FWD EMER LIGHT INOPERATIVE. R & R RT FWD EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: RETAINER — BROKEN (FLASHLIGHT) · airframe 25,830 hrs · 21,931 cycles

FLIGHT ATTENDANT FWD EMER FLASHLIGHT RETAINER BROKEN. R & R IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,755 hrs · 21,842 cycles

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

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,536 hrs · 21,602 cycles

MAIN DOOR EXIT MARKING SIGN INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER 1 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 25,478 hrs · 21,553 cycles

ABORTED TAKEOFF DUE TO TAKEOFF CONFIG WARNING APPROXIMATELY 100 KTS SPEED. TRIM, WAS GREEN BUT GAVE TRIM WARNING AT 8 UP. PERFORMED TROUBLESHOOTING IAW FIM TASK 31-51-00-810-804-A. R & R HSCU IAW AMM 27-40-01. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,432 hrs · 21,500 cycles

AFT CABIN EMER FLOOR LIGHTING INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER NR 6 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,332 hrs · 21,395 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT BULB IAW AMM 33-50-07.

Part: PRESSURE SWITCH — FAILED (AC BAY) · airframe 24,877 hrs · 20,939 cycles

DURING FLIGHT 3196 CREW REPORTED PACK 1 OVERLOAD IAW LG PG 3622567, MEL 2129 THE ACFT WAS REMOVED FROM SERVICE. R & R OVER PRESS SWITCH IAW MM 21-51-06. PERFORMED TROUBLESHOOTING IAW FIM 21-51-00-810-801 STEPS 1 - 3. MEL IS RESTORED, THE ACFT RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,017 hrs · 20,244 cycles

NUMBER 4 LIGHT STRIP HAS BROKEN WIRE ACFT SIDE. REPAIRED NR 4 LIGHT STRIP CONNECTORS ACFT SIDE IAW SWPM 20-50-01 & 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 24,017 hrs · 20,244 cycles

NUMBER 8 LIGHT STRIP HAS BROKEN WIRE AIRCRAFT SIDE. REPAIRED NR 8 LIGHT STRIP CONNECTORS AIRCRAFT SIDE IAW SWPM 20-50-01 & 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 24,017 hrs · 20,244 cycles

NUMBER 8 LIGHT STRIP HAS BROKEN WIRES. ACFT WAS REMOVED FROM SERVICE. R & R LIGHT STRIP NR 8 ASSEMBLY IAW AMM 33-50-12 STEPS 2 I 3 FOR REMOVAL & STEPS 3 I 1 FOR INSTALL.

Part: WIRE — BROKEN (CABIN) · airframe 24,017 hrs · 20,244 cycles

NUMBER 4 LIGHT STRIP TO HAVE BROKEN WIRES. ACFT WAS REMOVED FROM SERVICE. R & R LIGHT STRIPS NR 4 ASSEMBLY IAW AMM 33-50-12 STEPS 2 I 3 FOR REMOVAL & STEPS 3.I 1 FOR INSTALL.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 24,017 hrs · 20,244 cycles

DURING MX INSPECTION ON FLIGHT 9802 FOUND CARGO DOOR CUT OUT L BRACKET CORRODED ABOVE & UNDER FWD CARGO TRIM PIECE. ACFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 65 SHEAR CLIP IAW AEA EO EM-53MR-1129 PART B FOUND DURING INSPECTION.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 24,017 hrs · 20,244 cycles

EMERGENCY LIGHTS ON GALLEY CEILING PANEL & AFT SIDE OF AFT GALLEY WILL NOT LIGHT UP. RESEATED THE CONNECTOR P8530 TO GALLEY CEILING PANEL FOR THE EMERGENCY LIGHTS ON GALLEY CEILING PANEL & AFT SIDE OF AFT GALLEY THAT DID NOT LIGHT UP IAW SWPM 20-50-00 STEP 2, SYS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,818 hrs · 20,090 cycles

NUMBER 2 EMERGENCY CEILING LIGHT INOPERATIVE. R & R NR 2 BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,812 hrs · 20,082 cycles

NR 2 EMERGENCY CEILING LIGHT INOPERATIVE. R & R NR 2 BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,464 hrs · 19,809 cycles

MAIN DOOR CEILING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 22,808 hrs · 19,238 cycles

AFTER CREW LEFT OPS, NOTICED THAT EMERGENCY LIGHT TURNED ON AND TURNED BACK OFF AFTER 10 MINUTES. PERFORMED CHARGING ON EMERGENCY LIGHT BATTERIES IAW CMM 25-60-03. PERFORMED OPS TEST IAW AMM 33-50-00.

Part: RELAY — FAILED (CABIN PRESSURE) · airframe 21,325 hrs · 18,039 cycles

ON FLIGHT 4256 THE CREW REPORTED THAT AT FLIGHT LEVEL 270 THEY RECEIVED AN PRESSURIZATION AUTO FAIL MESSAGE ON EICAS. THE CREW PERFORMED THE AOM VOL 1 CHECKLIST, DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET. THE CREW SELECTED MANUAL MODE, CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RELAY K0264 COMPLIED FUNCTIONAL CHECK IN AUTOMATIC MODE ALL OPS NORMAL MEL RESTORED PLACARD REMOVED ALL IAW EMB 145 21-31-00-700-802 AND 21-31-03-420-001-A00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK SWITCH — FAULTY (NLG) · airframe 20,518 hrs · 17,406 cycles

ON FLIGHT 4208 THE CREW REPORTED THAT ON CLIMBOUT AT APPROX 225 KNOTS THE CREW HEARD A LOUD BANGING FROM NOSE GEAR AREA IT INCREASED AS THEY ACCELERATED TO 240 KNOTS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO BWI. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND NOSE LANDING GEAR UPLOCK SWITCH POO42 FAULTY. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK SWITCH POO47 AND SAME HARNESS IAW EMB 145 AMM# 32-61-01/32-62-00. INSPECTED ALL LANDING GEAR UPLOCK SWITCHES CHECKED GOOD IAW SWPM # 20-50-00. EXTENSION AND RETRACTION TEST GOOD IAW EMB 145 AMM # 32-30-00/32-62-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,491 hrs · 16,576 cycles

DURING B INSPECTION FOUND THE RIGHT FLOOR PROXIMITY STRIPS NR 3 AND NR 4 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN RIGHT FLOOR PROXIMITY STRIPS NR 3 AND NR 4 IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,491 hrs · 16,576 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EMERGENCY LIGHT STRIP ASSEMBLY CRACKED AND HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY LIGHT STRIP ASSEMBLY IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,491 hrs · 16,576 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 4 EMERGENCY LIGHTING SYSTEM POWER SUPPLY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — TORN (PAX DOOR) · airframe 19,320 hrs · 16,438 cycles

ON FLIGHT 2882 THE CREW REPORTED THAT WHILE DEPLANING THE AIRCRAFT THE FLIGHT ATTENDANT NOTICE A TEAR IN THE MAIN CABIN DOOR SEAL HALF WAY UP TRAILING EDGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR MAIN CABIN DOOR SEAL IAW EMB 145 AMM 52-00-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 19,310 hrs · 16,428 cycles

ON FLIGHT 2762 THE CREW REPORTED, NOTICED A BURNT ODOR IMMEDIATELY AFTER TAKEOFF. THE ODOR DISSIPATED AFTER APPROXIMATELY ONE MINUTE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. DEBRIEFED FLIGHT CREW NO OIL OR ELECTRICAL ODOR NOTED AND NO VISIBLE HAZE ON WALK AROUND OF AIRCRAFT. BIRD INGESTION WAS FOUND IN LEFT ENGINE. PERFORMED INSPECTION OF LEFT ENGINE IAW ROLLS-ROYCE MM 05-50-00. NO EXTERNAL DAMAGE NOTED. PERFORMED LEFT ENGINE BORESCOPE INSPECTION INLET GUIDE VANES, 1ST STAGE BLADES, AND 14TH STAGE BLADES IAW ROLLS-ROYCE MM 72-30-00-200-801 AND ENT # EM 72-026. NO DAMAGE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 17,380 hrs · 14,970 cycles

ON FLIGHT 2952 THE CREW REPORTED THAT ON ROTATION NOTICED FUMES IN THE COCKPIT AND VISIBLE SMOKE IN THE CABIN AND LAVATORY. THE ALARM SOUNDED AND THE CREW ACCOMPLISHED AOM-1 PROCEDURES. THE CAPTAIN DECLARED AN EMERGENCY RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 17,380 hrs · 14,970 cycles

ON FLIGHT 2952 THE CREW REPORTED THAT ON ROTATION NOTICED FUMES IN THE COCKPIT AND VISIBLE SMOKE IN CABIN AND THE LAV SMOKE ALARM SOUNDED ACCOMPLISHED AOM-1 PROCEDURES AND LANDED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECK WAS GOOD. THIS MAY HAVE BEEN SUBMITTED VIA FAX OR E-MAIL TO THE FAA---NO RECORD CONNECTS THIS TO AN EXISTING SDR REPORT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INSULATION — UNSECURE (COCKPIT) · airframe 14,892 hrs · 13,033 cycles

ON FLIGHT 3389 THE CREW REPORTED VIA TELEPHONE -- WHILE CLIMBING OUT OF DFW A FAN STARTED TO MAKE EXCESSIVE NOISE BEHIND THE INSTRUMENT PANEL. THE CREW REPORTED THE NOISE WAS SO EXCESSIVE IT WAS MAKING THE SHIPS RADIO INAUDIBLE. THE NOISE DID NOT CHANGE WITH AIRSPEED OR CONFIGURATION. THE CREW ELECTED TO RETURN TO DFW. THE NOISE STOPPED AFTER 10 SECONDS ON THE GROUND. THE AIRCRAFT WAS REMOVED FROM SERVICE. UPON INSPECTION FOUND INSULATION TAPE STOCKED INSIDE THE FORWARD RIGHT FAN, REMOVED AND RE-SECURED INSULATION AS PER 25-80-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — FAILED (CABIN) · airframe 14,478 hrs · 12,708 cycles

DURING MAINTENANCE BASE VISIT FOUND THE OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER. DETERMINED NO FIX AFTER REMOVING AND REPLACING THE NR 4 BATTERY AND BATTERY CHARGER. REPINNED CONNECTOR P8503 PINS 7 & 9 AND REPLACED THE BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 13,389 hrs · 11,808 cycles

ON FLIGHT 3302 DURING CRUISE THE CREW REPORTED AN INFLIGHT LANDING AIR/GROUND FAIL MESSAGE ON EICAS FOLLOWED BY AN ENGINE 1 & 2 THRUST REVERSE DISAGREE MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED NOSE LANDING GEAR IAW 32-20-01. THE PROXIMITY SWITCH WAS NOT MAKING CONTACT DUE TO LOW STRUT. NO PARTS WERE REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THERMAL SWITCH — INOPERATIVE (BLEED SYSTEM) · airframe 13,319 hrs · 11,752 cycles

ON FLIGHT 3456 DURING CRUISE, CREW REPORTED THEY RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. THEY CLOSED CROSS BLEED AND BOTH ENGINE VALVES. THE MESSAGE WAS INTERMITTENT THEN WENT ON AND DID NOT DISAPPEAR. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SGF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE THERMAL SWITCH IN LT PYLON PER AMM 36-20-02 ALL OPERATIONAL CHECKS ARE GOOD IAW EMB AMM 36-20-02-700-801A. ALSO PERFORMED OPERATIONAL TEST OF THE AIR BLEED SYSTEM. NO FAULTS OR MESSAGES NOTED AT THIS TIME IAW AMM 36-00-00-710-001-A00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — FAILED (BLEED DUCT) · airframe 13,164 hrs · 11,632 cycles

ON FLIGHT 2738 DURING CRUISE THE CREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT FAULT IAW EMB-FIM 36-20-00-810-801-A. INSPECTED ALL DUCT LINE’S JOINT OF THE LEFT AIR BLEED SYSTEM IAW AMM 36-11-09. REMOVED AND REPLACED CLAMPS AT THE LEFT FUEL TEMPERATURE CONTROL VALVE IAW AMM 21-60-01. THE OPERATIONAL TEST WAS GOOD. NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DEFECTIVE (BLEED AIR SYS) · airframe 13,132 hrs · 11,607 cycles

ON FLIGHT 3211 THE CREW REPORTED DURING CRUISE THAT A NUMBER 1 BLEED LEAK MESSAGE WOULD NOT GO OUT. THE CREW FOLLOWED AIRCRAFT OPERATING MANUAL PROCEDURES AND SHUT DOWN THE NUMBER 1 ENGINE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SAT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NUMBER 1 BLEED LEAK MESSAGE NEVER DID CLEAR AFTER LANDING WITH THE PLANE ON THE GROUND AND THE ENGINE OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE D-CLAMP AT THE UPPER BLEED AIR CHECK VALVE IAW EMB 145 AMM 36-11-01. PERFORMED OPERATIONAL CHECK AND IT WAS GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAULTY (CABIN) · airframe 12,373 hrs · 11,043 cycles

FLT 3348 ON FINAL FLT ATT REPORTED HEAVY SMOKE AND ELEC FIRE ODOR IN CABIN, SOURCE WAS AROUND 7B/7C. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AC WAS REMOVED FROM SERVICE. EVIDENCE OF BURNED MARKS. SHORTED WIRE W166-8611, REPAIRED WIRE W166-8611-22 IAW WM 20-21-00, ON CIRCUIT BOARDS 8BC, 9A, 9BC. R&R CIRCUIT BOARDS 8BC 9A 9BV IAW CMM 25-28-23. 7A, 8A, 9A AND 10A WALL AND CEILING LIGHTS INOP. R&R LIGHT BULB S 7A, 8A, 9A AND 10A, IAW EMB 145 33-21-00 AMM. SOCKETS ARE GOOD. THE 1A AND 2A CEILING LIGHT INOP. R&R LIGHT BULBS AT 1A AND 2A. INSPECTED LIGHT SOCKETS. FOUND GOOD WITH NO BURN MARK FOUND. OPERATIONAL CHECK IS GOOD IAW EMB 145 33-20-00 AMM. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — SHORTED (PSU) · airframe 12,373 hrs · 11,043 cycles

FLIGHT 3348 ON SHORT FINAL THE FLIGHT ATTENDANT REPORTED HEAVY SMOKE AND ELECTRICAL FIRE ODOR IN CABIN. THE SOURCE WAS AROUND 7B/7C. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. EVIDENCE OF BURNED MARKS. FOUND SHORTED WIRE W166-8611, REPAIRED SHORTED WIRE W166-8611-22 IAW WM 20-21-00, ON CIRCUIT BOARDS 8BC, 9A, 9BC. REMOVED AND REPLACED CIRCUIT BOARDS 8BC 9A 9BV IAW CMM 25-28-23. THE 7A, 8A, 9A AND 10A WALL AND CEILING LIGHTS BURNED OUT. REMOVED AND REPLACED LIGHT BULB S 7A, 8A, 9A AND 10A, WALL AND CEILING LIGHTS IAW EMB 145 33-21-00 AMM. ALL SOCKETS ARE GOOD. THE 1A AND 2A CEILING LIGHT BURN OUT. REMOVED AND REPLACED LIGHT BULBS AT 1A AND 2A. INSPECTED LIGHT SOCKETS. FOUND GOOD WITH NO BURN MARK FOUND. OPERATIONAL CHECK IS GOOD IAW EMB 145 33-20-00 AMM. AIRCRAFT RETURNED TO SERVICE.

Part: PRINTED CKT BOARD — DEFECTIVE (CABIN) · airframe 12,126 hrs · 10,854 cycles

ON FLIGHT 3209 - THE CREW REPORTED SMOKE AND FUMES AROUND ROW 7 AND 8A. THE CREW DECLARED AN EMERGENCY INTO MLU AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PRINTER CIRCUIT BOARDS AT ROWS 7 AND 8A AS PER EMB AMM 33-24-04. OPERATIONAL CHECKS GOOD. NO FURTHER DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — BURNED (COCKPIT) · airframe 11,564 hrs · 10,407 cycles

ON FLIGHT 3218, CREW REPORTED AFTER PUSH BACK DURING NR 1 ENGINE START PFD NR 1 WENT BLANK. COCKPIT FILLED WITH FUMES AND ELECT SMOKE. EVACUATION PASSENGERS WITHOUT INCIDENT. CFR CALLED. CFR DEPT DISCONNECT BATTERIES AND DID CABIN INSPECTION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 CAPTAINS PFD IAW AMM CH 24-34-02 TEST GOOD. CONFIRMED ODOR WAS FROM DISPLAY UNIT AND RECONNECTED BATTERIES IAW AMM CH 24-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 11,564 hrs · 10,407 cycles

ON FLIGHT 3218, CREW REPORTED AFTER PUSHBACK DURING NR 1 ENGINE START PFD NR 1 WENT BLANK. COCKPIT FILLED WITH FUMES AND ELECT SMOKE. EVACUATED PASSENGERS WITHOUT INCIDENT. CFR CALLED. CFR DEPT DISCONNECT BATTERIES AND DID CABIN INSPECTION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 CAPTAINS PFD IAW AMM CH 24-34-02, TEST GOOD. CONFIRMED ODOR WAS FROM DISPLAY UNIT AND RECONNECTED BATTERIES IAW AMM CH 24-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (CABIN) · airframe 11,094 hrs · 10,036 cycles

ON FLIGHT 3829 CREW REPORTED CLIMBING THRU 18000 FEET STRONG SMELL OF SMOKE POSSIBLY ELECTRICAL. CREW ELECTED TO RETURN TO DFW. AIRCRAFT REMOVED FROM SERVICE. GROUND RAN AIRCRAFT FOUND RIGHT RECIRCULATION FAN INOPERATIVE. REMOVED AND REPLACED RIGHT RECIRCULATION FAN IAW 21-24-01, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PITOT HEAD — CONTAMINATED · airframe 8,110 hrs · 7,421 cycles

ON FLIGHT 3378, AFTER TAKEOFF STANDBY ATTITUDE INDICATED (OUT OF ORDER). CAPT DECIDED TO RETURN TO GPT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLUID IN PITOT STATIC PORT DRAINED FLUID FROM PITOT STATIC LINES IAW AMM 34-13-00 AND COMPLETED OPS CHECK IAW AMM 34-24-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — ODOR (CABIN)

MELD PSU LIGHTS FLICKERED DURING TAXI FOLLOWED BY ELECTRICAL ODOR IN CABIN AND COCKPIT. REMOVED AND REPLACED PCB ASSY PER AMM 25-22-05. OPS CHECK OK RESTORED MEL. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTTLE VALVE — FAILED (ZONE 200) · airframe 7,246 hrs · 6,689 cycles

HYDRAULIC SYSTEM ONE FAILURE MESSAGE, CFR CALLED. RETURNED TO DFW. REMOVED AND REPLACED NUMBER FOUR BRAKE SHUTTLE VALVE AND TIGHTENED RESERVOIR REFILL CHECK VALVE AND LINE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT CARD — BURNED (PSU) · airframe 5,411 hrs · 5,088 cycles

BURNING ELECTRICAL ODOR AT ROW 4 ON TAXI. REMOVED AND REPLACED PSU CIRCUIT CARD AT ROW 7 IAW EMB AMM 25-28-23. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE GALLEY FLOOR FORWARD DIGITAL WAS FOUND CORRODED. PERFORMED CUT OUT OF THE FORWARD DIGITAL TO REMOVE THE DAMAGE. PREPARED A REPLACEMENT STRAP. FABRICATED A DOUBLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 34, CHAPTER 53-51. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE DAMAGE. PREPARED DOUBLER, FILLER, SHIMS AND REPAIR PLATES. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 34, CHAPTER 53-00-10 FIG 201. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPUTER — FAILED (ADC)

ON CLIMB-OUT BOTH ADC`S FAILED, RETURNED TO DFW. PER PILOT DEBRIEF NR 1 PFD HAD RED X ON AIRSPEED TAPE. RAI NR 1 ADC COMPUTER IAW AMM II 34-15-01, OPS CHECK GOOD, IAW EMB AMM 34-15-00. RETURNED AIRCRAFT TO SERVICE. (M)

Part: ADC — FAILED (NR 1)

ON CLIMB-OUT WHLE PASSING THROUGH 8,000 FT, NR 1 ADC FAILED.

Part: SMOKE DETECTOR — DEFECTIVE (LAVITORY)

LAVITORY SMOKE IN FLIGHT. REPLACED LAVITORY SMOKE DETECTOR WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED. (K)