N684JW

Part: STEERING SYS — OUT OF ADJUST (ZONE 700) · airframe 43,466 hrs · 39,446 cycles

DURING TAKE OFF ROLL ATTEMPT NWS VEERS LEFT WITHOUT TILLER ENGAGEMENT UNDER 30 KIAS. TAKE OFF REJECTED. PERFORMED TAXI CHECKS, NO DEFECTS NOTED. INSP STEERING ADJUSTMENT IRW AMM 32-50-00 AND FOUND TO BE W/I LIMITS. ACFT GOOD FOR SERVICE

Part: PRESSURE SWITCH — FAULTED (RUDDER) · airframe 41,983 hrs · 37,721 cycles

DURING CLIMBOUT APPOX 210 KNTS AT 2K FT EXPERIENCE YAW DAMPNER FAIL FOLLOWED BY RUDDER 1/2 FAIL FOLLOWED QRH WITH RUD SYS 2 DEACTIVATED FACT 18FEB25 16:14 CLT R&R RUDDER PRESSURE SWITCH IAW AMM 27-23-04. LEAK CHECK & OPS CHECK REQUIRED.(885751) OPS AND LEAK CHECK GOOD. A/C OKAY FOR SERVICE

Part: CAP — CORRODED (NLG BEARING) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F018677 NLG RH MAIN STRUT BEARING CAP IS CORRODED. RAR NLG RH MAIN STRUT BEARING CAP IAW EMB 145 AMM 32-20-01

Part: GUSSET — CORRODED · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016974 CORROSION ON LH BEAM #3 GUSSET. RAR ON LH BEAM #3 GUSSET IAW EMB- 145 SRM 51-40-02.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016961 CORROSION ON LH BEAM #5 GUSSET. REMOVED AND REPLACED LH BEAM #5 GUSSET IAW EMB145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F0016903 GALLEY, AT FR20, THE CENTER AISLE CROSSBEAM IS HEAVILY CORRODED AT MULTIPLE LOCATIONS. RAR CENTER AISLE CROSSBEAM AT FR 20 IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016938 CORROSION ON LH BEAM # 6 GUSSET. REMOVED AND REPLACED LH BEAM # 6 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016970 CORROSION ON RH OTBD #2 FLOOR SILL. RAR RH OTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016973 CORROSION ON LH OTBD #3 FLOOR SILL. RAR L/H OTBD #3 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016905 GALLEY, AT FR19, THERE IS CORROSION ON THE RH FLOOR SILL. REMOVED AND REPLACED RH FLOOR SILL AT FR19 IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016979 CORROSION ON CENTER BEAM #3 GUSSET. RAR CENTER BEAM GUSSET #3 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016973 CORROSION ON LH OTBD #3 FLOOR SILL. RAR L/H OTBD #3 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016960 CORROSION ON LH OTBD #4 FLOOR SILL. RAR L/H OUTBD #4 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016968 CORROSION ON LH OTBD #2 FLOOR SILL. RAR LH OTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016907 GALLEY, AT FR20, THERE IS CORROSION ON THE RH CROSSBEAM GUSSET. RAR DIAMOND GUSSET RH FR 20 IAW EMB 145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016913 GALLEY, AT FR23, THERE IS CORROSION ON THE RH CROSSBEAM. REMOVED AND REPLACED CROSSBEAM (ANGLE) IN GALLEY AT FR23 IAW EMB145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016862 LH FLOOR SILL #7 CORRODED. RAR THE LH FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016865 CENTER FLOOR BEAM LAVATORY FLOOR GUSSET CORRODED. REMOVED AND REPLACED CENTER FLOOR BEAM LAVATORY FLOOR GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,958 hrs · 37,697 cycles

F016866 RH FLOOR BEAM LAVATORY FLOOR GUSSET CORRODED. REMOVED AND REPLACED RH FLOOR BEAM LAVATORY FLOOR GUSSET IAW EMB 145 SRM 51-40-02

Part: DOOR — DIRTY · airframe 41,589 hrs · 37,210 cycles

MAIN CABIN DOOR HARD TO OPEN-C/A-CLEANED & LUBRICATED MAIN DOOR ROLLERS AW MM 53-21-02, OPS CHECK GOOD IAW MM 52-00-00

Part: DOOR — DIRTY (MAIN CABIN DOOR) · airframe 41,428 hrs · 37,032 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN-C/A-LUBRICATED ROLLERS ON MAIN CABIN DOOR IAW AMM 52-18-00 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (AFT OVERWING) · airframe 41,377 hrs · 36,987 cycles

SUPPLEMENTAL CA FOR RH AFT OVER WING EMERGENCY LIGHT INOP. "TRANSFERRED FROM NRWC 684-SGF-05021 ITEM 1"-C/A-REMOVED AND REPLACED RH AFT OVER WING EMERGENCY LIGHT LAMP

Part: LAMP — INOPERATIVE (RH) · airframe 41,318 hrs · 36,909 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (RH) · airframe 41,145 hrs · 36,732 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP WITH REFERENCE TO EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: NONE — BROKEN (AFT) · airframe 41,132 hrs · 36,715 cycles

AFT CABIN EMERGENCY FLASHLIGHT CLIP BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT CLIP IAW ASTRONICS CMM 25-60-14 OPC GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,071 hrs · 35,467 cycles

MEL 33-22 AUTH# 090117D-C REF LOGPAGE 4798868-2 "SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP". REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,070 hrs · 35,464 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A . NO FIX. NEEDS NEW SERVICE-DOOR EMERGENCY-LIGHT AS-SEMBLY. NO DEFECTS NOTED. END. "TRANSFERRED TO AML PAGE 4798868 ITEM 2"

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 39,567 hrs · 34,884 cycles

AFT FA EMERGENCY FLASHLIGHT INOP. R & R AFT FA'S FLASH LIGHT IAW EMB 145 AMM 33-50-16. OPERATIONAL CHECK GOOD.MEL RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,413 hrs · 34,720 cycles

SERVICE DOOR CIELING EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR CEILING EMERGENCY LIGHT LAMP IN REF WITH EMB 145 AMM 33-50-09.

Part: LIGHT — INCORRECT (CABIN FLOOR) · airframe 39,354 hrs · 34,658 cycles

REFERENCE AML#4406520 ITEM 1. EMERGENCY LIGHT FLOOR PROXMITY STRAP EXIT LOCATOR AMBER LIGHT INCORRECTLY.-C/A-RAR EMERGENCY LIGHT FLOOR PROXIMITY STRAP IAW EMB AMM 33-50-00.OPC GOOD.(INSTALLED AT ROW 9)

Part: LIGHT — INOPERATIVE (CENTER FAIRING) · airframe 39,324 hrs · 34,625 cycles

LH CENTER FAIRING EXTERNAL EMERGENCY LIGHT INOP.-C/A-RAR LH CENTER FAIRING EXTERNAL EMERGENCY LIGHTIAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,144 hrs · 34,432 cycles

RH EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR RH EXTERIOR EMERGENCY LAMP IAW AMM 33-50-10 OPC GOOD

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,898 hrs · 34,174 cycles

REAR EMERGENCY FLASH LIGHT HAS BROKEN HOLDER. C/A: R & R REAR EMERGENCY FLASH LIGHT, IAW PS2 WC.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 38,801 hrs · 34,081 cycles

MEL 3330-AUTH NR 120137-C 4688475/2 EMERGENCY LIGHT FLOOR STRIP NR 4 INOPERABLE. C/A: R & R FLOOR LIGHT STRIP NR 4, IAW AMM 33-50-12. OPERATIONS CHECK GOOD. MEL ITEM RESTORED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 38,790 hrs · 34,070 cycles

EMERGENCY LIGHTING FLOOR STRIP NR 4 HAS DAMAGED CONNECTORS. C/A: DEFFERED PER MEL 33-30.

Part: CHARGER — NOT REPORTED (EMERGENCY LIGHTS) · airframe 38,745 hrs · 34,025 cycles

NR 2 EMERGENCY BATTERY POWER SUPPLY CHARGER AND BATTERY PACK REQUIRE REPLACEMENT. C/A: R & R NR 2 EMERGENCY BATTERY POWER SUPPLY CHARGER AND BATTERY PACK, IAW EMB145 AMM 33-50-04. OPERATIONS CHECK GOOD. EMERGENCY LIGHT BATTERY ASSEMBLY P/N 2013-1A REMOVED, P/N 2013-1ASMI INSTALLED, REF ETN EM-33-020R1 FOR INTERCHANGEABILITY.

Part: LAMP — INOPERATIVE (RT WING E LIGHT) · airframe 38,745 hrs · 34,025 cycles

RT FWD WING EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND REPLACED RT FWD EXTERNAL EMERGENCY LIGHT LAMP, IAW EMB145 AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: HANDSET — MALFUNCTIONED (INTERPHONE) · airframe 38,229 hrs · 33,547 cycles

PILOT EMERGENCY LIGHT ILLUMINATED ON FA FWD INTERPHONE AND AFT PANEL. R & R FWD FLIGHT ATTENDANT'S HANDSET IAW AMM 23-31-03. OPS CHECKED SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,038 hrs · 33,391 cycles

FOUND LAST FLOOR PROXIMITY STRIP LIGHT OUT. REMOVED AND REPLACED LAST FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12 OPS CHECKED GOOD

Part: DOUBLER — SCRATCHED (MAIN DOOR) · airframe 37,794 hrs · 33,121 cycles

MAIN DOOR EXTERIOR AFT LOWER EDGE REPAIR DOUBLER IS SCRATCHED-C/A-BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 51-10-03. REMOVED AND REPLACED REPAIR FILLER AND DOUBLER IAW ERS-EM-52MR-1062 FILLER= 2024 T3 0.08 DOUBLER= 2024 T3 0.080

Part: DOOR FRAME — CORRODED (FRM 22) · airframe 37,794 hrs · 33,121 cycles

SSI 53-20-10 SERVICE DOOR CUTOUT AFT FRAME 22 IS CORRODED AROUND LOWER NUTPLATE HOLE-C/A-PERMFORMED PERMANENT REPAIR TO SERVICE DOOR CUTOUT AFT FRAME 22 AROUND LOWER NUTPLATE HOLE IAW ERS-EM-53MR-4051 REV: ORIGINAL

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 37,794 hrs · 33,121 cycles

SSI 53-20-00 CABIN LH OMEGA BEAM SIDE AT FRAME 29 AT CROSSMEMBER IS CORRODED.-C/A-PERFORMED PERMANENT REPAIR TO LH OMEGA BEAM SIDE AT FRAME 29 AT CROSSMEMBER IAW ERS-EM-53MR-4052 PT. A REV: ORIGINAL.

Part: SKIN — CHAFED (FRAMES 67-68) · airframe 37,794 hrs · 33,121 cycles

FUSELAGE SKIN IS CHAFFED INSIDE RH PYLON PANEL 424DB -C/A-PERFORMED PERMANENT REPAIR TO CHAFED FUSELAGE SKIN INSIDE RH PYLON PANEL 424DB IAW ERS-EM-53MR-4053 PT. A REV: ORIGINAL.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,794 hrs · 33,121 cycles

SSI 53-30-03: FRAME 65 SHEAR CLIP CORRODED AT LOWER END OF CARGO DOOR OPENING-C/A-BLENDED CORROSION ON FRAME 65 SHEAR CLIP IAW EMB 145 SRM 51-10-03. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FRAME 65 SHEAR CLIP SECTION IAW EMB 145 SRM 51-40-02, SRM 53-31-04. FRAME 65 SHEAR CLIP SECTION P/N: 145-25175-001.

Part: FAIRING — CORRODED (CARGO DOOR) · airframe 37,794 hrs · 33,121 cycles

CARGO DOOR SCREW HOLES FOR FAIRINGS HAVE CORROSION-C/A-PERFORMED BLEND OUT OF CORROSION ON CARGO DOOR FAIRING SCREW HOLES IAW EMB 145 SRM 51-10-03. SCREW HOLES OUTSIDE OF THE REPAIR AREA FOUND TO BE WITHIN LIMITS IAW EMB 145 SRM 52-30-04 ACCOMPLISHED SHIM, DOUBLER AND WEB FILLER REPAIR TO LOWER FWD CORNER OF CARGO DOOR IAW EMB 145 SRM 51-20-01, 51-40-02 AND 52-30-04. SHIM: 2024-T3 .080, DOUBLER: 2024-T3 .063, FILLER 2024-T3 .050.

Part: DOOR FRAME — CORRODED (FRAMES 65-68) · airframe 37,794 hrs · 33,121 cycles

SSI 53-30-48: CARGO DOOR CUTOUT LWR STRUCTURE CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02, SRM 51-40-06 AND SRM 51-20-03. INSTALLED CARGO DOOR LOWER SILL P/N 145-25-480-603SD.

Part: STANCHION — CRACKED (FRAME 29) · airframe 37,794 hrs · 33,121 cycles

LH OMEGA BEAM STANCHION AT FRAME 29 IS CRACKED-C/A-REMOVED AND REPLACED LH OMEGA BEAM STANCHION AT FRAME 29 IAW EMB 145 SRM 51-40-02. INSTALLED STANCHION P/N 145-30660-002.

Part: CHANNEL — CORRODED (FRAMES 20-22) · airframe 37,794 hrs · 33,121 cycles

GALLEY SERVICE DOOR CENTER SILL HAS CORROSION AT MULTIPLE LOCATIONS.-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: FITTING — CRACKED (LT NACELLE) · airframe 37,794 hrs · 33,121 cycles

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

Part: WIRE — BROKEN (COCKPIT) · airframe 37,794 hrs · 33,121 cycles

EMERGENCY EXIT LIGHT ON COCKPIT STEP PNL HAS A BROKEN WIRE-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON COCKPIT STEP PNL IAW EMB 145 AMM 33-50-13. SEE NRTC# E778330 FOR COMPELTION OF EMERGENCY LIGHT OPS CHECK.

Part: ESCAPE ROPE — FRAYED (COCKPIT) · airframe 37,794 hrs · 33,121 cycles

COPILOT AND PILOTS EMERGENCY ESCAPE ROPE FRAYED-C/A-COMPLETE:REMOVED AND REPLACED COPILOT AND PILOTS EMERGENCY ESCAPE ROPE IAW EMB145 AMM 25-60-07, 20-10-01, EASI TQ WR: EASI 7409.

Part: WIRE — DAMAGED (CABIN) · airframe 37,794 hrs · 33,121 cycles

EMERGENCY LIGHT STRIP WIRE AT FR 45 ON AIRCRAFT SIDE IS DAMAGED-C/A-COMPLETE:UPON FURTHER INVESTIGATION BROKEN EMERGENCY LIGHT STRIP WIRE AT FR49 TO BE DAMAGED. RAR DAMAGED CONNECTOR FOR EMERGENCY LIGHT STRIP AT FR49 IAW EMB 145 SWPM 20-21-00. FOR OPC OF EMERGENCY LIGHTING SYSTEM

Part: WIRE — BROKEN (CABIN) · airframe 37,794 hrs · 33,121 cycles

2EA PROX LIGHT WITH ARROWS, 1EA SERVICE DOOR EXIT PROX LIGHT, AND 1EA PROX LIGHT WITHOUT ARROWS HAVE BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 2EA PROX LIGHT WITH ARROWS, 1EA SERVICE DOOR EXIT PROX LIGHT, AND 1EA PROX LIGHT WITHOUT ARROWS IAW EMB 145 AMM 33-50-12 SEE NRTC BOW 340146 FOR FINAL INSTALL AND OPS CHECKS

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,794 hrs · 33,121 cycles

EMERGENCY LIGHT ON MAIN ENTRY WAY INOP-C/A-COMPLETE:REMOVED AND REPLACED BATTERY SUPPLY #1 IAW EMB 145 AMM 33-50-04. OPC GOOD.

Part: WIRE SPLICE — BROKEN (FLASHLIGHT) · airframe 37,794 hrs · 33,121 cycles

AFT FLASHLIGHT CHARGER ON LAV TOILET WALL SPLICE BROKEN AND BROKEN ON THE OPPOSITE SIDE ON THE LAV CEILING.-C/A-COMPLETE:REPAIRED WIRE TO SPLICE SP3557 IAW EMB 145 SWPM 20-21-00 AND WM 33-51-50

Part: HOLDER — CRACKED (CABIN) · airframe 37,794 hrs · 33,121 cycles

4EA PROX LIGHT HOLDER AND 4EA RH SIDEWALLS ARE CRACKED-C/A-COMPLETE:REMOVED AND REPLACED 4EA PROX LIGHT HOLDER AND 4EA RH SIDEWALLS IAW EMB 145 AMM 33-50-12 SEE NRTC BOW340146 FOR FINAL INSTALL

Part: WIRE — BROKEN (CABIN) · airframe 37,794 hrs · 33,121 cycles

EMERGENCY LIGHT STRIP WIRE FOR #1 LIGHT STRIP HAS BROKEN WIRE AT PIN ON AIRCRAFT SIDE-C/A-COMPLETE:RE TERMINATED EMERGENCY LIGHT STRIP #1 LIGHT STRIP WIRE AT PIN ON AIRCRAFT SIDE IAW EMB 145 WM 33-50-50, SWPM 20-00-03, 20-21-00. SEE TURNOVER FOR DETAILS

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,716 hrs · 33,031 cycles

FLAP LOW SPEED ADVISORY ON APPROACH-C/A-DEFERRED FLAP LOW SPEED, CH-2. M PROCEDURES C/WED.CMC MSG "FLAP L/H MOTOR BRAKE FAIL"MEL AUTH# 010786DM-B REF# 27-9

Part: WARNING MESSAGE — ILLUMINATED (FLAP SYSTEM) · airframe 37,305 hrs · 32,677 cycles

FLAP LOW SPEED ON FINAL APPROACH-C/A-DEFERRED FLAP CHANNEL #2. "M" PROCEDURES C/W. CMC MESSAGE "FLAP LH MOTOR BRAKE FAIL".

Part: DISPLAY — FAILED (COCKPIT) · airframe 37,103 hrs · 32,491 cycles

FO PFD INOP ELECTRICAL BURN SMELL. SOURCE OF ODOR FOUND AND CORRECTED. INSTALLED NR 2 PFD IAW MM 34-22-01. OPS CK GOOD IAW EMB MM 34-22-00. GROUND RAN AIRCRAFT PER R/R MM 72-00-00. OPERATED PACKS, COCKPIT LIGHTING AND WINDSHIELD HEAT. NO ODORS FOUND, OK FOR SERVICE

Part: SIGN — UNSECURE (ROW 1A) · airframe 37,063 hrs · 32,453 cycles

EXIT SIGN AT 1A UNSECURE. SECURED THE EXIT SIGN AT 1A IAW AMM 25-60-00.

Part: LIGHT — BURNED (COCKPIT) · airframe 37,033 hrs · 32,428 cycles

VISIBLE SMOKE AND ASSOCIATIED ELECTRICAL BURNING SMELL EMINATING FROM CAPTAINS YOKE, FLOOR AREA. INTERNAL APU POWER WAS SUPPYING ELECTRICAL LOADS. EVENT OCCURED AFTER STICK SHAKER/PUSHER, TRIM AND HYDFLIGHT CONTROL TESTS. TOKE MAP LIGHT WAS OFF. TESTS WERE SATISFACTORY. NO EICAS CAUTION/ALERT ASSCOC ANNUNCIATORS-C/A-PERFORMED GVI OF COCKPIT PAY PARTICULAR ATTENTION TO CAPTAINS YOKE ACCESSABLE WIRING, AND COCKPIT RELAY PANELS. FOUND CAPTAINS YOKE MOUNTED CHART HOLDER LIGHT TO HAVE 1 BULB BURNED. REF AML 4496693 ITEM # 3 FOR DEFERRAL. NO OTHER DEFECTS NOTED.

Part: O-RING — FAILED (NR 2 BLEED SYS) · airframe 36,850 hrs · 32,234 cycles

BLEED 2 LEAK AFTER AUDIBLE POP SOUND. REMOVED AND REPLACED O-RINGS AND COUPLING COVER AT BLEED COUPLING #8 IAW AMM 36-11-10. BLEED 2 LEAK CHECK GOOD IAW AMM 36-11-09-200-803.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,674 hrs · 32,031 cycles

CEILING EMERGENCY LIGHT AT ROW 17 INOP. C/A-REMOVED AND REPLACED CEILING EMERGENCY LIGHT LAMP AT ROW 17 IAW AMM 33-50-08 OPC GOOD.

Part: FAN — FAILED (RECIRCULATION) · airframe 36,354 hrs · 31,776 cycles

SMELL OF RUBBERY SMOKE AT FL 260 ALL COCKPIT INDICATIONS IN COCKPIT WERE NORMAL AOM PERFORMED AND DIVERTED AS REQUIRED.-C/A-INSPECTED GALLEY AND CABIN BALLETS LAMPS AND FLASH LIGHTS AND COCKPIT LIGHTS FOR ABNORRMAL SMELL COMPLIED WITH ETN-EM-72-034 R 10 NO SMELL NOTED. REMOVED AND REPLACED #1 RECIRCULATION FAN AS PER AMM 21-24-01. OPS CHECK GOOD AS PER AMM 21-20-00. REMOVED AND REPLACED #2 INVERTER ASSY AS PER AMM 21-26-03. OPS CHECK GOOD AS PER AMM 21-26-00. REMOVED COLLARS AND CLOSED CIRCUIT BRAKERS AS PER AMM 21-26-03 AND AMM 21-24-01. SYSTEMS RESTORED.

Part: LIGHT — INOPERATIVE (ROW 7 & 9) · airframe 36,040 hrs · 31,446 cycles

EMERGENCY LIGHT BETWEEN ROW 7 & 9 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP FROM ROW 7 8 9 PER 33-50-12 OPS CK GOOD

Part: COUPLING — DETACHED (AC BAY) · airframe 34,858 hrs · 30,482 cycles

BLEED 1 LEAK ON CLIMB OUT. REATTACHED HOSE COUPLING AT ACM NR 1 IAW MM CH 21-51-04.

Part: SLEEVE — DAMAGED (AC BAY) · airframe 34,852 hrs · 30,476 cycles

BLEED 1 LEAK CLIMBING OUT OF 6,000 AND CABIN ALT CONTINUED TO CLIMB. REMOVED PACK 1 PANEL IAW 06-41-01 OF AMM. PERFORMED GVI OF PACK 1 FOUND COUPLER ABOVE ACM LEAKING ISOLATED PACK 1 AND RAN ENGINE FOR 5 MIN IAW GHC WITH BLEED 1 SELECTED NO MESSAGES NOTED. REMOVED AND REPLACED UPPER AND LOWER DUCT COUPLER SLEEVES IAW AMM 21-51-02-420-002-A. OPS CHECK GOOD IAW MM CH 49-10-00.

Part: DUCT — LEAKING (AC BAY) · airframe 34,683 hrs · 30,298 cycles

BLD 1 LEAK DURING CLIMBOUT, EPC C/W. -C/A-PERFORMED REMOVED AND REPLACED OF DUAL TEMP CONTROL VALVE Y-DUCT IAW AMM 21-60-01. LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,077 hrs · 29,720 cycles

CEILING EMERGENCY LT AT ROW 17 INOP. R&R AISLE EMERGENCY LIGHT LAMP AT ROW 17 IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A, OPS CHECK GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,761 hrs · 29,440 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,390 hrs · 29,080 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECKED GOOD IAW AMM 33-50-10

Part: FLASHLIGHT — NOT REPORTED (AFT CABIN) · airframe 32,742 hrs · 28,507 cycles

AFT CABIN EMERGENCY FLASHLIGHT NEEDS TO BE REPLACED-C/A-REMOVED AND REPLACED EMERGENCY FLASHLIGHT AS REQUIRED, NO OTHER DEFECTS NOTED AT THIS TIME.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 32,674 hrs · 28,430 cycles

TEAR STRAP DAMAGED AT FRAME 22L BETWEEN STR 13L AND 14L. MAJOR REPAIR, PERFORMED REPAIR DAMAGED TEAR STRAP AT FRAME 22 BETWEEN STR 13L AND 14L IAW ERS-EM-53MR-3021.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,608 hrs · 28,357 cycles

LT AFT FUSELAGE FR75 HAS SKIN CRACK ABOVE STR 2L. REPAIRED LT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR 2L IAW SRM 53-31-01 ITEM 11 FIG 219.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,608 hrs · 28,357 cycles

SKIN CRACK AROUND RIVET AT FR75 BTW STGRS 2R-3R. REPAIRED SKIN CRACK AROUND RIVET AT FR 75 BTW STGRS 2R-3R IAW SRM 53-31-01 ITEM 11 FIG 219.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,608 hrs · 28,357 cycles

CORROSION ON INTERNAL SKIN FR 60-61 STR 20L-21L. REMOVED AND INSTALLED SERVICEABLE INT FUSELAGE REINFORCEMENT PLATE BTW FR 60-61 STR 20L-21L IAW SRM 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,608 hrs · 28,357 cycles

EMERGENCY LIGHT FLOOR ROWS 6 - 8 INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,608 hrs · 28,357 cycles

PAX DOOR EMERGECY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 1 POWER SUPPLY IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 32,413 hrs · 28,149 cycles

DURING TAKEOFF E2 ATTCS NO MARGIN WARNING MSG. ABORT AT 90 KTS. AFTER ABORT E 2 EXCEEDANCE CAUTION MSG. OUTSIDE AIR TEMP, ATIS AND REF TO TEMP ALL 31C MAX ITT WAS 922C. REMOVED AND REPLACED RT ENG COMP BLEED VALVES AND RT ENG CABCV. PERFORMED ENGINE GROUND RUNS WITH NO EXCEEDANCES NOTICES IAW AMM 71-00-01.

Part: WIRE — BROKEN (CABIN) · airframe 27,944 hrs · 23,527 cycles

NUMBER 6 EMER LIGHT STRIP HAS BROKEN WIRE. REPAIRED WIRE ON NR 6 EMER LIGHT STRIP IAW SWPM 20-21-00.

Part: SKIN — CHAFED (FUSELAGE) · airframe 27,944 hrs · 23,527 cycles

FUSELAGE SKIN CHAFED INSIDE PANEL 414DB. PERFORMED REPAIR IAW ERS-EM-53MR-1206.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,944 hrs · 23,527 cycles

EMERGENCY LIGHT STRIP HARNESS HAS BROKEN CONNECTOR AT FLOOR PANEL 251FF. R & R THE EMER LIGHT STRIP HARNESS CONNECTOR AT FLOOR PANEL 251FF SP9211 IAW SWPM 20-00-03.

Part: EPSU — UNKNOWN (CABIN) · airframe 27,944 hrs · 23,527 cycles

REPLACE EPSU 3. R & R EMER EPSU 3 IAW MNTC WC 33-700-19.

Part: EPSU — UNKNOWN (CABIN) · airframe 27,944 hrs · 23,527 cycles

REPLACE EPSU 4. R & R EPSU 4 IAW MNTC WC 33-700-19.

Part: EPSU — UNKNOWN (CABIN) · airframe 27,944 hrs · 23,527 cycles

REPLACE EPSU 2. R & R EPSU 2 IAW MNTC WC 33-700-19.

Part: EPSU — UNKNOWN (CABIN) · airframe 27,944 hrs · 23,527 cycles

R & R EPSU 1 IAW MNTC WC 33-700-19.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 27,944 hrs · 23,527 cycles

SERVICE DOOR CUT OUT STRUCTURE HAS SURFACE CORROSION AT LOWER FWD NUTPLATE HOLE. PERFORMED ERS-EM-52MR-1186 FOUND TO BE ACCEPTED AS IS.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 27,944 hrs · 23,527 cycles

CARGO DOOR LOWER INBD EDGE MEMBER NUTPLATE HOLES ARE CORRODED. REMOVED CORROSION FROM CARGO DOOR LOWER INBD EDGE MEMBER NUTPLATE HOLES & FOUND TO BE ACCEPTED AS IS IAW ERS-EM-52MR-312. SEE TURNOVER FOR DETAILS.

Part: TIRE — WORN (NLG) · airframe 27,391 hrs · 23,057 cycles

ON SHORT FINAL, NOSE GEAR WAS MAKING A THUMPING SOUND. EXECUTED GO AROUND, CYCLED LG, & HEARD SAME THUMPING SOUND. APPROX 15 - 20 THUMPS IN 15 MINUTES. BOTH NOSE TIRES WORN TO LIMITS, DECLARED EMER. R & R LT NLG WHEEL ASSEMBLY & RT NLG WHEEL ASSEMBLY IAW WC 32-700-17.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 27,119 hrs · 22,808 cycles

HYD 2 LOW QTY ON EICAS. SERVICED NR 2 HYDR RESERVOIR IAW EMB 145MM 12-13-01. TROUBLESHOOTING ITEM 1 ABOVE. FOUND NR 2 EDP TO BE LEAKING. REPLACED NR 2 EDP IAW EMB 145MM 29-10-03. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (PARKING BRAKE) · airframe 27,103 hrs · 22,792 cycles

PARKING BRAKE LIGHT IS INOPERATIVE. R & R BRAKE LIGHT BULBS IAW AMM 20-13-04.

Part: SIGN — UNSECURE (CABIN) · airframe 24,621 hrs · 20,798 cycles

OVERHEAD EXIT SIGN IN CEILING FALLING DOWN 12A. SECURED CTR AISLE EXIT SIGN AT ROW 12 IAW STANDARD MTX PRACTICES.

Part: LIGHT — INOPERATIVE (SEAT 6) · airframe 24,451 hrs · 20,653 cycles

FLOOR PROXIMITY LIGHT STRIP AT SEAT 6 IS INOPERATIVE. R & R LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO FURTHER DEFECTS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,922 hrs · 20,233 cycles

CAPTAIN`S FLASHLIGHT MUST BE SHAKEN TO WORK. R & R FLASHLIGHT IAW AMM 33-21-06. FLASHLIGHT OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 23,884 hrs · 20,201 cycles

NR 1 EMERGENCY LIGHT HAS BROKEN WIRES. R & R LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,834 hrs · 20,157 cycles

EMERGENCY LIGHT ON AFT WALL OF GALLEY IS INOPERATIVE. R & R NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW AE W/C 33-700-17.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 23,119 hrs · 19,586 cycles

ON FLIGHT 3588 THE CREW REPORTED AN INTERMITTENT "BRAKE ON" INDICATION INFLIGHT. EMERG/PARK BRAKE LEVER WAS IN RELEASED POSITION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CAPTAIN SAID THAT BRAKE LIGHT WAS INTERMITTENT ONLY IN FLIGHT AND WORKED NORMAL ON THE GROUND. CHECKED CMC AND NO MESSAGE NOTED IAW AMM 73-22-01. PERFORMED OPERATIONAL CHECK OF EMERGENCY PARKING BRAKE IAW EMB-145-MM-32-44-07, NO FAULTS NOTED, OPS CHECK GOOD. REMOVED AND REPLACED PRESSURE SWITCH EMERGENCY PARKING BRAKE IAW AMM 145 32-44-07. REMOVED AND REPLACED RELAY FIN #K0212 AS PER ASM 32-44-50 AND REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 32-44-07. OPS CHECK GOOD. NO FAULTS NOTED. REF NRWC #684-MIA-01158. ACCOMPLISHED FIM TASK PROCEDURES 73-10-00-810-812 AND PERFORMED OPS CHECK IAW AMM 71-00-01, OPS CHECK GOOD NO FAULTS, MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 22,949 hrs · 19,440 cycles

DURING B INSPECTION FOUND THE PILOTS EMERGENCY FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT AND CRADDLE IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MALFUNCTIONED (CABIN) · airframe 22,922 hrs · 19,421 cycles

ON FLIGHT 3585 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT ABOVE JUMP SEAT APPEARS TO NOT BE CHARGING BECAUSE THE RED LIGHT IS NOT ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FLASHLIGHT CHARGING IAW AMM 33-30-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,768 hrs · 19,304 cycles

DURING B INSPECTION FOUND THE AFT GALLEY SEAT 3BC EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT GALLEY EMERGENCY EXIT SIGN IAW EMB AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,726 hrs · 19,275 cycles

DURING B INSPECTION FOUND THE EMERGENCY CEILING LIGHT 2ND FROM FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY ASSEMBLY AND CHARGER AND LAMP, PART #1317 IAW W/C 33-700-19. ALL EMERGENCY LIGHTS OPC GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,370 hrs · 18,998 cycles

DURING MAINTENANCE CHECK FOUND THE OUTSIDE FORWARD RIGHT EMERGENCY LIGHT AND NR 2 AISLE OVERHEAD LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY CHARGER AND BATTERY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 22,369 hrs · 18,997 cycles

ON FLIGHT 3273 THE CREW REPORTED THE READING LIGHT AT 8C SMELLED HOT. REMOVED AND REPLACED THE READING LIGHT LAMP AT SEAT 8C IAW EMB 145 AMM 33-25-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — POWER LOSS (NR 2) · airframe 22,336 hrs · 18,969 cycles

ON FLIGHT 3422 THE CREW ABORTED TAKEOFF DUE TO GREATER 80 KNOTS TAKEOFF POWER LOSS ON NR 2 ENGINE AND LOSS OF NR 2 ITT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FADEC 2A AND 2B, CLEAN CONNECTOR CHECK CORROSION ON CONNECTOR PER ROLLS ROYCE FIM 77-21-00-810-801. RUN ENGINE 2 TO MAXIMUM POWER PER FIM 77-21-00-810-801 ROLLS ROYCE MTX MANUAL, OPT CHECK GOOD, COULD NOT DUPLICATE PROBLEM AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,481 hrs · 18,251 cycles

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

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 21,361 hrs · 18,147 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,171 hrs · 18,009 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT EMERGENCY EXIT LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RELAMPED EMERGENCY LIGHT IAW MM 33-50-10. TESTED SATISFACTORY. AIRCRAFT WS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,171 hrs · 18,009 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. LAMPED EMERGENCY LIGHT IAW MM 33-50-10. TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,989 hrs · 17,874 cycles

DURING B INSPECTION, FOUND THE FORWARD FLOOR EMERGENCY STRIP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND GS 8508DC TO NOT HAVE A GOOD CONNECTION. RESECURED IAW WM 20-21-00. OPC IAW WC 33-700-17. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 20,684 hrs · 17,637 cycles

FLIGHT 3527, AFTER SELECTING IGNITION ON IN MODERATE RAIN AND TURBULENCE, NOTICED A STRONG ELECTRICAL BURNING ODOR IN COCKPIT AND FORWARD CABIN. ODOR DISAPPEARED AFTER SELECTING IGNITION TO AUTO. NO SMOKE OBSERVED AT ANY TIME. AIRCRAFT REMOVED FROM SERVICE. INSPECTED POWERPLANT CONTROL MODULE, COMPLIED WITH GENERAL INSPECTION OF FORWARD AVIONICS ELECTRICAL COMPARTMENT. NO DEFECT NOTED. PERFORMED ENGINES OPS CHECK IAW AMM 71-00-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,498 hrs · 17,495 cycles

ON FLIGHT 3514 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW MM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,092 hrs · 17,184 cycles

DURING B-INSPECTION FOUND SEAT 1 AND 2 EMERGENCY FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT 1A/2A EMERGENCY FLOOR STRIP IAW EMB AMM TASK 33-50-12-000-801A/33-50-12-40-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,899 hrs · 17,046 cycles

DURING B-INSPECTION, FOUND THE RIGHT OVERWING EMERGENGY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVER WING EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,609 hrs · 19,609 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR STRIP IAW EMB 145 AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 19,585 hrs · 16,834 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE AT NR 1 FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 19,585 hrs · 16,834 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT BASE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT BASE IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,585 hrs · 16,834 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST THREE FLOOR PROXIMITY LIGHT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 AND NR 3 EMERGENCY LIGHT DC/AC INVERTERS IAW EMB 145 AMM 33-50-11 AND REMOVED AND REPLACED RIGHT AFT EMERGENCY OVERWING LIGHT LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 19,585 hrs · 16,834 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP ELECTRICAL CONNECTOR MISSING AT FLOOR PANEL 251DF. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT STRIP ELECTRICAL CONNECTOR AT FLOOR PANEL 251DF IAW EMB 145 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 16,620 hrs · 14,679 cycles

ON FLIGHT 2889 DURING TAKEOFF THE CREW REPORTED A SMOKE AND BURNING ODOR IN THE AFT CABIN. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE IAW AE WORK CARD 71-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE. FINDINGS FROM THE TEARDOWN REPORT DETERMINED THE CAUSE OF THE SMOKE WAS FROM A FRONT FRAME OIL LEAK.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 15,069 hrs · 13,455 cycles

ON FLIGHT 4107 THE CAPTAIN REPORTED THAT AFTER TAKEOFF DURING CLIMB APPROXIMATELY AT 13,000 FEET, LOST ALL CAPTAIN’S PRIMARY FLIGHT DISPLAY ATTITUDE/ALTIMETER AND AIR SPEED INDICATIONS. DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THIS WAS NOT AN OVERWEIGHT LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. ALL DATA WHICH IS DESCRIBED AS LOST ON CAPTAIN'S PRIMARY FLIGHT DISPLAY, WAS AVAILABLE ON CAPTAIN'S MULTI FUNCTION DISPLAY AFTER SELECTING REVERSIONARY MODE. LOSS OF DATA ON PRIMARY FLIGHT DISPLAY NR 1 WAS A DISPLAY PROBLEM. MAINTENANCE WAS ABLE TO DUPLICATE ON GROUND -- NOTE: AUTOPILOT STAYED ENGAGED THROUGHOUT DISCREPANCY. REMOVED AND REPLACED THE CAPTAIN'S PRIMARY FLIGHT DISPLAY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH FITTING — LACK OF LUBE (CABIN DOOR) · airframe 14,667 hrs · 13,136 cycles

ON FLIGHT 4082 THE CREW REPORTED, UNABLE TO PROPERLY CLOSE THE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED ATTACH FITTINGS AND PERFORMED AN OPERATIONAL CHECK IAW EMB145 AMM 52-18-00. NO DEFECTS NOTED THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,532 hrs · 13,010 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT AND NR 2 CABIN CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE BATTERY/ CHARGER ASSEMBLY AND OPERATION CHECKED GOOD IAW EMBRAER AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (AILERON) · airframe 14,532 hrs · 13,010 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING AND THE AILERON ASSEMBLY IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 12,780 hrs · 11,635 cycles

ON FLIGHT 3741 - CREW REPORTED ENGINE 1 FAILED (UNCOMMANDED SHUTDOWN) ON TAKEOFF AT APPROXIMATELY 10 KNOTS. AIRCRAFT REMOVED FROM SERVICE. AWAITING FOLLOW-UP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED BEAM AT FRAME 20 IAW EMB 145 SRM 53-00-10 FIGURE 201 BY INSTALLING A DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED AFTER NORMAL SHUTDOWN EMERGENCY LIGHTS AT ROWS 8 THROUGH 12. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)