N918AE

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 42,951 hrs · 38,874 cycles

DURING GEAR RETRACTION HYD QTY 1 DROPPED THAN DROPPED AGAIN DURING LEVEL CRUISE. R & R NR 1 EDP IRT AMM 29-10-03. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED. SERVICED HYD 1 SYSTEM IRT 12-13-01.

Part: A/C PACK — OVERTEMP (NR 1) · airframe 43,585 hrs · 38,960 cycles

PACK 1 OVERTEMP ON TAKE OFF ROLL. REJECTED TAKEOFF. C/W FLT CREW PROCEDURES MEL 15AUG24 06:50 FWA C22806 21-15-21 AIR COND PACK N650 AND ABOVE. REMOVED AND REPLACED #100 PACK DUAL TEMPERATURE CONTROL VALVE IN REFERENCE TO AMM 21-60-01 OPS CHECK GOOD AT THIS TIME AIRCRAFT OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,774 hrs · 36,866 cycles

EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR AND FLOOR PROXIMITY LIGHTS 1,2,AND 3 NOT WORKING.......INSPECTED #2 BATTERY PACK IAW AMM 33-50-04 AND FOUND LOOSE, REINSTALLED BATTERY. OPS CHECK GOOD.

Part: WINDOW — NONE · airframe 40,758 hrs · 35,708 cycles

AFTER TAKE OFF BIRD STRIKE ON CAPTAINS WINDSHIELD. PERFORMED BIRDSTRIKE INSP. IAW AMM 05-50-08. NO DMAGE FOUND. REMOVED BIRD REMAINS AND CLEANED CA WINDSHIELD. NO DEFECTS NOTED. A/C OK FOR SERVICE

Part: SLEEVE — TORN (NR 1 ACM) · airframe 40,724 hrs · 35,665 cycles

CLIMBING THRU 27K, CABIN ALTITUDE CONTINUED TO CLIMB, DESCENDED TO 10K AND STAB AND WING ANTI ICE INOP WITH BLEED 2 LOW TEMP AND ICE CONDTION ANTIICE INOP. FOUND NR 1 ACM SLEEVE TORN. R & R THE SLEEVE IAW AMM 21-51-03. PERFORMED LEAK CHECK, NO DEFECTS NOTED. OPS CHECKED PRESSURIZATION SYS IAW AMM 21-39-00, OPS CHECKED GOOD, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKE SYSTEM) · airframe 40,600 hrs · 35,516 cycles

BREAK DEGRADED EICAS MESSAGE WHEN BREAKS APPLIED. REMOVED CONNECTOR PLUGS ON BRAKE CONTROL UNIT INSPECTED FOUND NO DEFECTS INSTALLED CONNECTOR PLUGS. PILOT PERFORMED TAXI CHECK AND BRAKE DEGRADED MSG DID NOT APPEAR. NO FUTHER DEFECTS. OK FOR SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 40,597 hrs · 35,512 cycles

DISPLAY UNIT NR 1 FAN FAIL. REMOVED AND REPLACED DISPLAY UNIT #1 IAW AMM 34-22-01. OPS CHECK GOOD. OK FOR SERVICE.

Part: SWITCH — LACK OF LUBE (CARGO DOOR) · airframe 40,596 hrs · 35,511 cycles

CREW REPORTED BAG DOOR INDICATED OPEN IN FLIGHT. LUBRICATED BAG BAY SWITCHES. PERFORMED AMM TASK 52-76-01-700-801-A, BAG BAY DOOR WARNING SWITCHES OPERATIONAL TEST. OPS CHECK GOOD, OK FOR SERVICE

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E937971 - SSI 53-30-48 CORROSION ON CARGO DOOR LOWER SILL ... REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB145 SRM 51-40-02.

Part: SKIN — CRACKED (FRM 78 S5-6R) · airframe 40,592 hrs · 35,508 cycles

E937122 - THERE IS A POSSIBLE SKIN CRACK AT A RIVET, AT FR78, STGR 6R-5R .... ACCOMPLISHED REPAIR OF SKIN CRACK AT A RIVET BY CUT OUT AND INSTALLATION OF BUSHING AT FR78, STGR 6R-5R IAW EO1-53-22-0211.

Part: SKIN — CORRODED (INTERIOR) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938371 - SSI 53-20-27 INTERIOR PAX, THE SKIN AT THE BASE OF THE FWD HEATED NIPPLE HAS CORROSION .... ACCOMPLISHED REPAIR OF CORROSION ON INTERNAL FUSELAGE SKIN AROUND HEATED NIPPLES BTW FR 57-58 IAW EO1-53-22-0210 AND ETD# ETD2022-145-030530.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938783 - INTERIOR PAX, THE SKIN AT THE BASE OF THE AFT HEATED NIPPLE HAS CORROSION. SSI 53-20-07 .... ACCOMPLISHED REPAIR OF CORROSION ON INTERNAL FUSELAGE SKIN AROUND HEATED NIPPLES BTW FR 57-58 IAW EO1-53-22-0210 AND ETD# ETD2022-145-030530. SEE NRTC# E938371 FOR DETAILS AND REQUIRED RII INSPECTIONS.

Part: GUIDE — DAMAGED (CABIN PARTITION) · airframe 40,592 hrs · 35,508 cycles

E938354 - CDT INTERIOR CABIN, THE LOWER LH COCKPIT TO PAX PARTITION GUIDE PIN HOLE IS ELONGATED ..... COMPLETED INSTALLATION OF INTERIOR CABIN LOWER LH COCKPIT TO PAX PARTITION GUIDE PIN HOLE DOUBLER IAW EMB 145 SRM 53-21-02 SECTION 4 FIG 204

Part: YOKE — CRACKED (LT ENGINE) · airframe 40,592 hrs · 35,508 cycles

E937935 - LH ENGINE LOWER FWD YOKE IS CRACKED AT ENGINE MOUNT .... REMOVED AND REPLACED LH ENGINE PYLON YOKE FITTINGS IAW PIEDMONT FCD1-54-21-0015.

Part: FLOORBEAM — CORRODED (FRM 18) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938489 - CORROSION ON CROSS FLOOR BEAM AT FRAME 18 PREVIOUS REPAIR .... REMOVED AND REPLACED CROSS BEAM AT FR 18 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 52-57) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938024 - INTERIOR PAX, THERE IS CORROSION ON THE LH FLOOR SILL, AT FRAME 52-57. PREVIOUSLY BLENDED AREA .... BLENDED AREA ON LH FLOOR SILL BTW FR52-57 FOUND TO BE BEYOND ALLOWABLE LIMITS IAW EMB 145 SRM 53-24-10. REMOVED UNSERVICEABLE LH FLOOR SILL BTW FR 52-59 AND REPLACED WITH SERVICEABLE ONE IAW EMB-145 SRM 51-40-02, SRM 51-20-03, SRM 51-20-01. APPLIED PAINT TO L/H FLOOR SILL, AT FRAME 52-57 IAW EMB 145 CPM 51-21-06 AND PIEDMONT BULLETIN CPM 51-02.

Part: GUSSET — CORRODED (FRM 20) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938526 - CORROSION IN GALLEY AREA ON DIAMOND GUSSET AT FRAME 20 .... RAR GALLEY AREA DIAMOND GUSSET AT FRAME 20 IAW EMB 145 SRM 51-40-02

Part: ANGLE — CORRODED (FRM 23) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938535 - CORROSION IN GALLEY AREA ON CENTER HAT BEAM ANGLE PANEL AT FRAME 23 .... RAR GALLEY AREA ON CENTER HAT BEAM ANGLE PANEL AT FRAME 23 IAW EMB 145 SRM 51-40-02

Part: BEAM — CORRODED · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938516 - CORROSION IN GALLEY AREA ON CENTER BEAM GUSSET .... REMOVED CORRODED GALLEY AREA CENTER BEAM GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02, EMB 145 CPM 51-21-06, PIEDMONT BULLETIN 51-02.

Part: SHEAR TIE — CORRODED (FRM 58 S19-20R) · airframe 40,592 hrs · 35,508 cycles

E938370 - INTERIOR PAX, THERE IS A SHEAR CLIP THAT HAS CORROSION, ON FR 58, BETWEEN STGR 19R-20R. SSI 53-20-43 .... REMOVED AND REPLACED SHEAR CLIP AT FR 58 BTW STGR 19R-20R IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938456 - CORROSION ON PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT .... REMOVED AND REPLACED PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT IAW EMB145 SRM 51-40-02,

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938498 - SSI 53-20-11 CORROSION ON LH BEAM AT FRAME 20 .... REPAIRED LH OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 ITEM 2 FIGURE 201 SHEET 1.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938503 - CORROSION ON LH OTBD # 1 FLOOR SILL .... REMOVED CORRODED LH OTBD # 1 FLOOR SILL, POSITIONED DRILLED AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02, 51-20-03.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938457 - ELONGATED SCREW HOLE AND CORROSION ON PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT ....REMOVED AND REPLACED PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT IAW EMB145 SRM 51-40-02

Part: FRAME — CRACKED (FRM 72 S16-17L) · airframe 40,592 hrs · 35,508 cycles

E939229 - FR 72 CRACKED BETWEEN STGR 17L AND STGR 16L .... REMOVED AND REPLACED FR 72 LH SECTION IAW EMB-145 SRM 51-40-02.

Part: BRACKET — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E937854 - CORROSION ON BAGGAGE DOOR LOWER L BRACKET .... REMOVED AND INSTALLED NEW AND SERVICEABLE BAGGAGE DOOR LOWER 'L' BRACKET IAW EMB-145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938533 - CORROSION ON SERVICE DOOR AFT FLOOR SILL WITH SOME AREAS PREVIOUS REPAIRED .... REMOVED DAMAGED SERVICE DOOR AFT FLOOR SILL AND INSTALLED NEW SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-02

Part: BUSHING — NOT REPORTED (RT NACELLE) · airframe 40,592 hrs · 35,508 cycles

E940139 - PCR - ACCOMPLISH FCD1-54-21-0017 REV C - RIGHT PYLON - REPLACEMENT OF FORWARD PYLON LINKAGE AND BUSHINGS

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938496 - CORROSION ON CROSS FLOOR BEAM AT FRAME 20 PREVIOUS REPAIR .... REMOVED AND REPLACED CENTER AISLE CROSS FLOOR BEAM AT FR 20 IAW EMB 145 SRM 51-40-02 AND PIEDMONT BULLETIN 53-3.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E938494 - CORROSION ON LH INBD # 1 SEAT TRACK .... REMOVED AND REPLACED LH INBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E937764 - SSI 52-21-06 CORROSION ON LOWER FRAME AROUND RUBBER STOP ON RH EMERGENCY ESCAPE HATCH ... 4 REMOVED AND REPLACE LOWER FRAME AROUND RUBBER STOP ON RH EMERGENCY ESCAPE HATCH IAW EMB145 SRM 51-40-02 AND AMM 52-21-00.

Part: REINFORCEMENT — CORRODED (LT NACELLE) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E937355 - CORROSION ON 3 TRIANGLE REINFORCEMENTS ON LH ENGINE INTERNAL UPPER COWLING .... RAR 3 TRIANGLE REINFORCEMENTS ON LH ENGINE UPPER COWLING INTERNAL STRUCTURE IAW EMB 145 SRM 51-20-01 AND 51-40-02.

Part: REINFORCEMENT — CORRODED (FRMS 61-63) · corrosion level 2 · airframe 40,592 hrs · 35,508 cycles

E937968 - SSI 53-30-07 CORROSION ON INTERNAL FUSELAGE LOWER SKIN REINFORCEMENT PLATE BETWEEN FRAME 61-63 STRINGERS 21L-19L .... REMOVED AND INSTALLED SERVICEABLE DOUBLER AT FR 62-63, STGR 19L-20L IAW EMB 145 SRM 51-40-02 ALSO REMOVED AND INSTALLED THE FABRICATED DOUBLER AT FRAME 61-62, AND STRINGERS 19L-20L IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 40,096 hrs · 34,901 cycles

FRAME 10 BENT BETWEEN STR 20R/21R. (MAJOR REPAIR)-C/A-PERFORMED DENT REPAIR IAW ERS-EM-53MR-4533

Part: NONE — NONE · airframe 40,096 hrs · 34,901 cycles

FUSELAGE SKIN PUNCTURED BETWEEN FR 10/11 AND STR 20R/21R.( MAJOR REPAIR)-C/A-INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER IAW ERS-EM-53MR-4533

Part: NONE — UNSERVICEABLE ([0000] [-] [) · airframe 40,026 hrs · 34,815 cycles

GPWS COMPUTER BURNING EGPWS CARDS-C/A-RAR GPWS COMPUTER IAW EMB AMM 34-41-01-000-802-A AND 34-41-01-400-802-A. OPC GOOD. END.

Part: NONE — NONE · airframe 39,113 hrs · 33,754 cycles

LEFT WING EMERGENCY EXTERIOR LIGHT INOP-C/A-RAR LEFT WING EMERGENCY EXTERIOR LIGHT IAW AMM 33-50-10. OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,486 hrs · 33,053 cycles

ROW 12 EMERGENCY LIGHT INOP-C/A-RAR ROW 12 EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,750 hrs · 32,302 cycles

ALL EMERGENCY LIGHTS RELATED TO EMERGENCY LIGHT BATTERY NR 1 INOPERABLE. C/A: R & R NR 1 EMERGENCY BATTERY AND CHARGER ASSEMBLY, IAW ENVOY W/C 33-700-19. OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 37,676 hrs · 32,229 cycles

DURING PS-1 CHECK FOUND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOPERABLE. C/A: R & R NR 4 EMERGENCY FLOOR PROXIMITY STRIP LIGHT, IAW AMM 33-50-12. OPERATIONS CHECK GOOD.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 37,639 hrs · 32,198 cycles

ENTRYWAY EMERGENCY FLASHLIGHT CRADLE BROKEN. C/A: R & R ENTRYWAY EMERGENCY FLASHLIGHT ASSEMBLY, IAW AMM 33-50-16. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: SENSOR — FAILED (NLG) · airframe 37,336 hrs · 31,926 cycles

ABNORMAL LND GEAR AIR GND FAIL MESSAGE ON CLIMB OUT ENG 1-2 REV DISAGREE MSG FOLLOWED A FEW MINUTES AFTER BOTH MESSAGES DISAPPEARED WHEN GEAR WAS EXTENED EMERGENCY DECLARED. LANDED SAFELY.-C/A-PERFOMED CMC DOWNLOAD FOUND FWD NLG PROXIMTY SENSOR WAS BAD WOW R&R SENSOR NLG IAW 32-63-02 OPS CHECK GOOD IAW ETN-EM 32-245

Part: LIGHT — INOPERATIVE (ROW 4C) · airframe 37,338 hrs · 31,928 cycles

ROW 4C EMERGENCY FLOOR STRIP LIGHT INOP-C/A-RAR ROW 4C EMERGENCY FLOOR STRIP LIGHT IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS CHECK GOOD

Part: CONNECTOR — DISCONNECTED (NLG) · airframe 36,979 hrs · 31,576 cycles

LG AIR/GND FAIL AFTER ROTATION/TAKEOFF/ENG 1(2) REV FAIL AFTER TAKEOFF-C/A-INSTALLED NOSE LANDING GEAR WOW CANNON PLUG IAW EMB 145 AMM 32-63-05. OPS CHECK, INCLUDING GEAR SWING, GOOD. FOUND NO DISCRAPANCIES.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 36,745 hrs · 31,358 cycles

CANNOT OPEN MAIN CABIN DOOR FROM OUTSIDE-C/A-INSPECTED MAIN CABIN DOOR FOUND TOP BRACKET HITTING WHEN DOOR IS CLOSING DESC REMAINS OPEN. ADJUSTED PASSENGER DOOR IAW AMM 52-18-00, RECORDED A OUT OFF DOCK VALE OF 30 LBS TO OPEN THE DOOR WHICH IS WITH IN LIMITS IAW AMM 52-18-00. C/W THE MAIN DOOR WARNING MESSAGES AND CHECKED GOOD IAW AMM 52-73-00. PRESSURE CHECK ON PAX DOOR CHECK GOOD IAW AMM 21-31-00.

Part: SKIN — CRACKED (FRAMES 74-76) · airframe 36,678 hrs · 31,296 cycles

RH REAR FUSELAGE 1, FR 75 ABOVE STR2R CRACK FOUND AT .500 ABOVE STR 2R.-C/A- REPAIR CARRIED OUT IAW SRM 53-31-01. NEEDED TO STOP FACE CARRIED OUT IAW SRM 51-75-00.

Part: SKIN — CRACKED (FRAMES 74-76) · airframe 36,678 hrs · 31,296 cycles

REAR FUSELAGE 1, LH SIDE AT FR75, 2 CRACK FOUND 1 IS .500 ABOVE STR 2L AND OTHER .750 BELOW STR 2L-C/A- REPAIRED IAW SRM53-31-01.

Part: BATTERY PACK — INOPERATIVE (EXTERNAL LIGHT) · airframe 36,678 hrs · 31,296 cycles

EMERGENCY AISLE LIGHT 2 AND EXTERNAL WING FUSELAGE FRONT FAIRING R/H LIGHT INOP WHEN EMERGENCY LIGHTS SET TO ON-C/A-AFTER TROUBELSHOOTING IAW WM 33-50-50 FOUND BATTERY #2 POWER CHARGER FAULTY BATTERY CHARGER #2 REPLACED IAW AMM 33-50-04 AND IPC 33-50-04 ITEM 60 EMERGENCY AISLELIGHT 2 AND EXTERNAL FWD R/H WING TO FUSELAGE FAIRING LIGHT TESTED IAW AMM 33-50-00 NO FAULT FOUND

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 36,678 hrs · 31,296 cycles

SERVICE DOOR CHANEL CORRODED-C/A-SERVICE DOOR CHANNEL CORROSION BLENDED OUT OF LIMITS, REMOVED AIW SRM 51-40-02 SERVICE DOOR CHENNEL REMOVED ADN EPLACED WITH NEW IAW SRM 51-40-02

Part: LIGHT — DAMAGED (CABIN) · airframe 36,576 hrs · 31,186 cycles

NUMEROUS FLOOR PATH LIGHT STRIP PROFILE PIECES ARE DAMAGED. EVALUATED AND RECIEVED NEW FLOOR PATH LIGHT STRIP PROFILE PIECES FROM PARTS. INSTALLED FLOOR PATH LIGHT STRIPS IAW AMM 33-50-12 OPS TEST GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,767 hrs · 30,442 cycles

INTERMITTENT ELECTRICAL BURNING ODOR DURING FLIGHT. COMPLIED WITH ETN-EM-72-034. ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. NO BURNING ODOR DETECTED AT THIS TIME.

Part: DUCT — LEAKING (AC BAY) · airframe 35,555 hrs · 30,314 cycles

PACK 2 VALVE CLSD AIRCRAFT UNABLE TO PRESS. C/A-WHILE T/S #2 PACK, FOUND DUCTS BETWEEN "Y" PIPE AND DUAL TEMP CONTROL VALVE LEAKING AND FOUND DUCT ASSY ON HEAT EXCHANGER LEAKING, RAR DUCTS BETWEEN "Y" PIPE AND DTCV, AND DUCT ASSY ON HEAT EXCHANGER AS PER AMM 21-51-02 AND 21-61-01 OPC GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,116 hrs · 29,018 cycles

A/C DID NOT PRESSURIZATION / PRESSURIZE. RETURNED TO DFW. NO EICAS ALERTS, LANDED AT APPROX 39,000 LBS. DEFERRED AUTOMATIC PRESSURIZATION MODE .C/W MAINT ACTION. PERFORMED MANUAL PRESSURIZATION & FOUND WORKING PROPERLY IAW MM 21-31-00. C/W "M" PROCEDURES AND REACTIVATED ELECTROPNUMATIC OUTFLOW VALVE IAW EMB AMM 21-31-03-440-801-A. REMOVED AND REPLACED DIGITAL CONTROLER IAW EMB AMM 21-31-01-000-801-A AND 21-31-01-400-801-A OPC GOOD MEL RESTORED

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 34,061 hrs · 28,975 cycles

AUTO PRESSURIZATION SYSTEM FAILED AT 33,000 FT.-C/A-DEFERRED AUTO PRESSURIZATION SYSTEM, M PROCEDURES COMPLIED WITH. MEL# 21-17 AUTH# 120087DM-C. .REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER IAW EMB AMM 21-31-02. OPS CHECK OK IAW EMB AMM 21-31-00 AND PERFORMED FUNCTION TEST OF PRESSURIZATION CONTROL SYSTEM IN AUTOMATIC MODE AS PER EMB145 AMM 21-31-00-700-802-A. OPC GOOD. MEL RESTORED.

Part: RELAY — INOPERATIVE (CONFIGURATION) · airframe 33,977 hrs · 28,910 cycles

ABORTED TAKEOFF. BREAKS DID NOT OVERHEAT DUE TO MASTERWARNING NO TO CONFIG TRANSFERRED TO NRWC 918-ORD-03868 -C/A-CREW DEBRIEF INDICATED "NO TAKEOFF CONFIG" MESSAGE HAPPENED WITH NO AURAL MESSAGE. TROUBLESHOT IAW FIM TASK 31-51-00-810-804-A. REMOVED AND REPLACED RELAY K0212 IAW EMB 145 AMM 20-13-02. PERFORMED AURAL WARNING OPERATIONAL CHECK IAW EMB 145 AMM 31-51-00 P/T STEPS 2. J. (P) - (U). OPERATIONAL CHECK GOOD.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 33,745 hrs · 28,707 cycles

RAMPERS REPORT ELECTRICAL SMOKE SMELL IN BAGGAGE COMPARTMENT. PERFORMED INSPECTION OF CARGO COMPARTMENT VERIFIED COMPARTMENT LIGHTING AND NO SMELLS NOTED. IAW AMM 33-31-00 NO DEFECTS NOTED NO SMELL NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: ACM — OVERHEATED (NR 1) · airframe 33,384 hrs · 28,334 cycles

NR 1 A/C PACK OVERHEATED WITH PACK BLOWING HOT AND A FOUL ODOR DURING APPROACH TO LAND. REMOVED AND REPLACED THE NR 1 ACM AND PERFORMED AN OPS CHECK IAW AMM 21-51-00 OPS CHECKED GOOD, NO DEFECT NOTED.

Part: ADC — FAILED (LEFT) · airframe 32,578 hrs · 27,577 cycles

CAPTAIN`S AIRSPEED UNRELIABLE DURING DESCENT. LOST 40KTS ACCORDING TO IT THEN A GAIN OF AROUND 60KTS WITH NO THRUST CHANGE. REMOVED AND REPLACED THE NR 1 ADC IAW AMM 34-15-01, OPERATES OK IAW AMM 34-15-00, PITOT/STATIC LEAK CHECKED OK IAW AMM 34-13-00.

Part: WINDSHIELD WIPER — UNWANTED DEPLOY (NR 2) · airframe 32,228 hrs · 27,288 cycles

NR 2 WINDSHIELD WIPER DEPLOYED IN FLIGHT, UNCOMMANDED AT FL320. DIVERTED. ADJUSTED THE CO PILOTS WINDSHIELD WIPER ARM IAW AMM 30-41-03. OPS CHECKEED GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 31,837 hrs · 26,907 cycles

WHILE CRUISING AT FL250 SMOKE WAS SMELLED IN COCKPIT THE FOLLOWED BY SMOKE ENTERING THE COCKPIT VIA OVERHEAD VENTS. PERFORMED RUNS AND PACK SYSTEMS TROUBLESHOOTING AND FOUND THAT NR 1 PACK SYSTEM ACM IS CEASED UP. DEFERRED NR 1 AC PACK SYSTEM REF 21-30 AUTH 120090D-C. REMOVED AND REPLACED L/H ACM, IAW EMB AMM 21-51-03.

Part: ELECTRONIC UNIT — FAILED (TE FLAPS) · airframe 31,633 hrs · 26,740 cycles

FLAP FAIL IN FLIGHT. TROUBLESHOT IAW FIM 27-51-00-810-813-A, OPS CHECKED FLAP SYSTEM AND OPERATION CHECK FAILED. CMC MESSAGE FLAP LT MOTOR BRAKE FAIL. REMOVED AND REPLACED FECU IAW AMM 27-536-02, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 12 BC) · airframe 30,954 hrs · 26,053 cycles

ROW 12 BC OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A, AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: LINER — DAMAGED (PAX DOOR) · airframe 30,608 hrs · 25,725 cycles

PAX DOOR WILL NOT OPEN. FOUND MAIN PAX DOOR INNER LINER DAMAGED. PERFORMED A TEMP REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,588 hrs · 25,701 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 25-23-04. OPC GOOD IAW AMM 33-50-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,456 hrs · 25,594 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP FOUND INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD

Part: SHUTTLE VALVE — FAILED (MLG) · airframe 30,326 hrs · 25,460 cycles

LEFT MAIN GEAR APPEARS TO HAVE HYDRAULIC LEAK, FLUID ON GROUND.- NR 2 MLG BRAKE SHUTTLE VALVE LEAKING. R & R THE NR 2 BRAKE SHUTTLE VALVE IAW AMM 32-49-03, LEAK & OPS CHECKED GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 30,202 hrs · 25,348 cycles

ALL EMERGENCY LIGHTS ON NR 1 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY AND CHARGER, OP/C GOOD, IAW AMM 33-50-04. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 101808

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,666 hrs · 24,848 cycles

BOTH FLIGHT DECK FLASHLIGHTS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,666 hrs · 24,848 cycles

F/O FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: ACM — FAILED (AC BAY) · airframe 29,029 hrs · 24,292 cycles

NOTICED BURNED ODOR FUMES IN COCKPIT AND CABIN WHEN OPERATING PACK 1 USING THE APU AT THE GATE. DETERMINED ODOR FROM NR 1 PACK AND DEFERRED NR 1 PACK. MEL REF 21-30 AUTH 070552D-C. R & R NR 1 PACK ACM IAW AMM 21-51-03. OPS CHECK GOOD. MEL 2130 RESTORED.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 28,880 hrs · 24,144 cycles

AFT FLASHLIGHT BRACKET BROKEN. R & R AFT FLASHLIGHT ASSY, OPC GOOD IAW AMM 33-50-16.

Part: RELAY — FAILED · airframe 28,777 hrs · 24,058 cycles

RECEIVED NO TAKEOFF CONFIG, EICAS WARNING MESSAGE WHILE ADVANCING THRUST ON TAKEOFF ROLL. PREVIOUS TO CONFIG CHECK, OK. PERFORMED SLOW SPEED ABORT, RESENT TRIMS SPOILERS, FLAPS, AND BRAKES. TESTED TO CONFIG AND GOT, OK, ADVANCED TAKE OFF LEVER FOR TAKEOFF AND GO, NO T/O CONFIG, WARNING AGAIN. RELAY V0212 IAW EMB 145, AMM 20-13-02. OPC GOOD IAW TASK 31-51-00-810-804-A.

Part: CONNECTOR — LOOSE (BRAKE SYSTEM) · airframe 28,758 hrs · 24,044 cycles

RECEIVED BRAKE ON LIGHT WHILE ENROUTE. PLACARD BRAKE ON LIGHT M-PROCEDURES COMPLIED WITH IAW MEL 3206. FOUND LOOSE CONNECTOR ON EMERGENCY, PARKING BRAKE PRESSURE SWITCH. TIGHTENED AND CLEANED CONNECTOR IAW SWPM 20-50-00. OPC GOOD IAW AMM TASK 32-44-00-720-002-A, MEL ITEM RESTORED.

Part: INDICATOR — FROZEN (COCKPIT) · airframe 28,547 hrs · 23,837 cycles

JUST BEFORE DESCENT, AFTER APPROX 1 HR AT 37,000', IAS CAS MSG. CAPTAINS AIRSPEED FROZEN, STBY AIRSPEED & FIRST OFFICERS AIRSPEED READS NORMAL. SAT -51 TAT -26 AT 28,000' AIRSPEED READS NORMAL AGAIN. INSPECTED BOTH PITOT DRAINS FOR WATER & PERFORMED INSPECTION CHECK OF PITOT STATIC SYSTEMS IAW AMM 34-13-00, NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,449 hrs · 23,757 cycles

RIGHT OVERWING EMER EXIT SIDEWALL EXIT SIGN INOPERATIVE. R & R EMER LIGHT INVERTER NR 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,156 hrs · 23,492 cycles

FIRST OFFICERS FLASHLIGHT SWITCH INOPERATIVE. R & R FIRST OFFICERS FLASHLIGHT AS REQUIRED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,038 hrs · 23,389 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR INOPERATIVE. R & R SERVICE DOOR EMER EXIT SIGN INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,739 hrs · 23,099 cycles

SPOILER FAIL MSG IN FLIGHT. TROUBLE SHOT IAW FIM TASK 27-63-00-810-802-A. NO CMC MSGS NOTED. PERFORM OPERATIONS CHECK IAW AMM 27-63-02. OPERATIONS CHECKED GOOD, NO MSGS NOTED & NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 26,916 hrs · 22,343 cycles

BAGG SMOKE INDICATION ON EICAS & OVERHEAD PANEL IN FLIGHT. R & R FWD & AFT BAGG SMOKE DETECTORS IAW MM 26-15-01. OPERATIONS CHECKED GOOD AT THIS TIME. CARGO AREA SMOKE DETECTOR FWD PN 473597-13 & SN 3445.

Part: DOOR — DENTED (CABIN) · airframe 26,894 hrs · 22,324 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH A DEFERRAL FOR A PAX DOOR AFT UPPER EDGE DENT. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION. PERFORMED PERMANENT REPAIR TO PAX DOOR AFT UPPER EDGE DENT IAW ERS-EM-52MR-043. ACFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REPAIR MATERIALS DOUBLER 2024T3 .080, FILLER 2024T3 .080.

Part: WIRE — CUT (EMERGENCY LIGHTS) · airframe 26,893 hrs · 22,323 cycles

DURING IMBV INSPECTION, QA FOUND 2 EMERGENCY LIGHT WIRES CUT & FRAYED AT FRAME 32 UNDER LEFT FLOOR SILL. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON WIRES W-192-8679-22 & W192-8678-22 AT FRAME 32 UNDER LEFT FLOOR SILL IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REPAIR SPLICE PN D-436-82.

Part: GUSSET — CORRODED (FRAMES 50-51) · airframe 26,893 hrs · 22,323 cycles

DURING IMBV INSPECTION, QA FOUND THE CENTER BEAM BETWEEN FRAME 50 - 51 HAD CORROSION AFT OF WING BOX. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON CENTER BEAM BETWEEN FRAME 50 - 51 JUST AFT OF WING BOX IAW ERS-EM-53MR-1522. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION, REPAIR MATERIALS, GUSSET A7475-T761 0.040, LEFT SPLICE AL 7475 - T761, 0.040.

Part: SKIN — DAMAGED (FRAMES 23-25) · airframe 26,893 hrs · 22,323 cycles

DURING MBV INSPECTION, QA FOUND A SCRATCH & GOUGE BETWEEN FRAME 23 - 25 & STRINGER 20L & 20R. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION. PERFORMED PERMANENT REPAIR ON SCRATCH & GOUGE BETWEEN FR 23 - 25 & STRINGERS 20L & 20 IAW ERS-EM-53MR-1505. AIRCRAFT T WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIR MATERIALS, DOUBLER AL2024-T3 0.063

Part: WIRE — BROKEN (CABIN) · airframe 26,893 hrs · 22,323 cycles

EMERGENCY PROXIMITY LIGHT STRIPS 2, 3, 4, 7 & 8 HAVE CHAFED & BROKEN WIRES. R & R EMER PROXIMITY LIGHT STRIPS 2, 3, 4, 7 & 8 IAW AMM 33-50-12. SEE NRTC BOW 197217 FOR FINAL INSTALL & OPERATIONS CHECK.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 26,893 hrs · 22,323 cycles

STRINGER 21L IS CORRODED BETWEEN FRAMES 10 - 11. R & R STRINGER 21L BETWEEN FRAMES 10 - 11 IAW SRM 51-40-02. SEE TASKS & WIPS FOR DETAILS.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 26,532 hrs · 22,027 cycles

MECH GEAR PROBLEM, FLIGHT DECLARED EMER. FLIGHT LANDED SAFELY. FLIGHT CANCELLED. R & R NLG WOW PROX SWITCH IAW MM CH 32-63-00.

Part: MUFFLER — DEFECTIVE (AC BAY) · airframe 25,572 hrs · 21,247 cycles

DURING CLIMB OUT, PASSING THROUGH 3000FT FLIGHT ATTENDANT CALLED ABOUT A VERY LOUD SQUEAL WAS COMING FROM MIDDLE OF CABIN, AROUND ROW 10. WE HEARD THE SQUEAL THROUGH THE INTERPHONE. WHEN WE LEVELED OFF AT 10000 FT SQUEAL STOPPED, PLANE WAS PRESSURIZING NORMALLY, WE RETURNED & SQUEAL STARTED AGAIN DURING TAXI & STOPPED WHEN PARKED. R & R NR 1 PACK RECIRCULATION SYS MUFFLER. OPERATIONS CHECKED GOOD IAW 21-24-02.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,544 hrs · 21,222 cycles

CAPTAIN`S EMER FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S EMER FLASHLIGHT 33-50-00.

Part: DOOR — OUT OF RIG (CABIN) · airframe 25,467 hrs · 21,134 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. INSPECTED DOOR FOUND DOOR TO BE OUT OF RIGGING IAW AMM 52-00-00-6.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 25,466 hrs · 21,133 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBE MAIN CABIN DOOR ROLLERS. OPERATIONS CHECKED GOOD IAW AMM 52-10-01.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 25,411 hrs · 21,089 cycles

FLIGHT ATTENDANT HAD VERY DIFFICULT TIME OPENING MAIN CABIN DOOR, WAS COMING PARTIALLY OPEN & WAS CATCHING ON SOMETHING, FINALLY CAME FREE. LUBED MAIN DOOR EXTERNAL HANDLE MECHANISM & FUSELAGE ROLLERS. OPERATIONS CHECKED OK IAW AMM 52 18 00.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 25,395 hrs · 21,077 cycles

COCKPIT FLASHLIGHT IS BROKEN. LIGHT ACTUALLY WORKS BUT BUTTON IS BROKEN. REPLACED FLASHLIGHT IAW MM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EXIT SIGN) · airframe 24,488 hrs · 20,313 cycles

SERVICE DOOR OVERHEAD EMER EXIT SIGN INOPERATIVE. DISCONNECTED, CLEANED & REINSTALLED SERVICE DOOR OVERHEAD EMER EXIT SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: HOSE — UNSECURE (AC BAY) · airframe 24,420 hrs · 20,246 cycles

LARGE AMOUNT OF AIR CONDITIONING SMOKE AT FLOOR LEVEL BY ROWS 8, 9 & 10. SECURED PACK OUTLET HOSE TO CABIN DISTRIBUTION VLV IAW 21-22-01.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 24,274 hrs · 20,087 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED, LUBED ROLLERS & OPERATIONS CHECK MAIN CABIN DOOR IAW AMM 52-10-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,219 hrs · 20,026 cycles

EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WILL NOT LIGHT UP DURING THE TEST. SECURED CONNECTORS IAW AMM 33-50-14. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 24,038 hrs · 19,848 cycles

FORWARD CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A, OPERATIONS CHECKED GOOD.

Part: RMU — FAILED (COCKPIT) · airframe 23,759 hrs · 19,603 cycles

AT ROTATION NR 1 RMU WENT BLANK FOLLOWED BY AN ELEC SMELL IN THE COCKPIT. RETURNED FOR LANDING. R & R MRU IAW AMM 23-81-01. OPERATIONS CHECKED GOOD.

Part: DOOR — DIRTY (CABIN) · airframe 23,745 hrs · 19,588 cycles

MAIN CABIN DOOR HARD TO OPEN. CLEANED, LUBED & PERFORMED LOAD TEST ON MAIN DOOR IAW AMM 52-10-01. OPERATIONS CHECKED GOOD, REQUIRED 27LBS TO OPEN DOOR.

Part: DOOR — DENTED (CABIN) · airframe 23,650 hrs · 19,511 cycles

COMPLIED WITH ERS-EM-52MR-043 PT B, RECURRING INSPECTION, ONLY PASS AFT UPPER EDGE DENT. REF TDMI 918T526 LG PG 3383675 4. PERFORMED PERMANENT REPAIR TO PAX DOOR DENT AT UPPER AFT EDGE IAW ERS-EM-52MR-043 PT C, TDMI RESTORED. SEE NRTC E457289 FOR DETAILS.

Part: FLAPPER VALVE — STUCK (GROUND AIR) · airframe 23,536 hrs · 19,429 cycles

DURING CLIMB ACFT UNABLE TO HOLD PRESSURIZATION IN CABIN ALT CLIMBED WITH ALT. NEITHER AUTO OR MAIN MODE WAS ABLE TO CONTROL CABIN PRESSURIZATION. FOUND GND AIR CONDITION HOOK UP FLAPPER VLV STUCK IN THE FULL OPEN POSITION. CLEANED & LUBRICATED HINGE & SPRING. PERFORMED OPERATIONS CHECK PRESSURIZATION CONTROL SYS IN NORMAL MODE IAW AMM 21-22-04 & 21-31-00.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 23,122 hrs · 19,078 cycles

LEFT SIDEWALL SEAT TRACK SUPPORT IS CORRODED AROUND RIVETS BETWEEN FRAME 45 - 46. R & R SEAT TRACK SUPPORT IAW SRM CH 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 23,123 hrs · 19,078 cycles

DURING MBV INSPECTION FOUND RT OVERWING NR 2 ATTACH ANGLE IS CRACKED. R & R ANGLE WITH NEW IAW ETN-EM-53-142 & SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 23,123 hrs · 19,078 cycles

DURING MBV INSPECTION FOUND RT OVERWING NR 1 ATTACH ANGLE IS CRACKED. REMOVED DAMAGED SECTION OF THE RT OVERWING NR 1 ATTACH ANGLE & REPLACED WITH NEW IAW ETN-EM-53-142, & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,123 hrs · 19,078 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 29. REPAIRED LEFT HAND OMEGA BEAM AT FRAME 29 IAW ERS-EM-53MR-126.

Part: FITTING — DAMAGED (RT AILERON) · airframe 23,123 hrs · 19,078 cycles

RIGHT AILERON PCA FITTING ON AILERON IS DAMAGED. REMOVED AND REPLACED RIGHT HAND AILERON PCA FITTING IAW EO EM-27MR-112.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 21,352 hrs · 17,618 cycles

DURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD, NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 20,741 hrs · 17,130 cycles

ON FLIGHT 4028 THE CREW REPORTED THE FLASHLIGHT OVER THE FLIGHT ATTENDANT’S JUMPSEAT HAD A BROKEN BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S JUMPSEAT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (LANDING GEAR) · airframe 20,076 hrs · 20,076 cycles

ON FLIGHT 4393 THE CREW ABORTED TAKEOFF AT 70 KNOTS. THE AIRPLANE PULLED EXCESSIVELY TO THE RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED NOSE LANDING GEAR WHEEL TIRE INSPECTION AS PER EMNB-145 AMM 32-49-04 NO DEFECTS NOTED. NOSE WHEEL STEERING CHECK COMPLIED WITH PER EMB-145 AMM 32-50-00 NO DEFECTS NOTED. PERFORMED GROUND TAXI CHECK, NO DESCEPANCIES FOUND. CONDUCTED HIGH SPEED TAXI AND NO DEFECTS NOTED. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 19,482 hrs · 16,142 cycles

FLIGHT 4023, FLIGHT ATTENDANT FLASHLIGHT MISSING. INSTALLED NEW FLASHLIGHT. AIRCRAFT RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 19,367 hrs · 16,048 cycles

DURING MAINTENANCE, FOUND THE LEFT FLOOR SUPPORT HAS CORROSION AT FRAME 30 AND FRAME 32. AIRCRAFT REMOVED FROM SERVICE. REMOVED LEFT FLOOR SUPPORT AT FRAME 30 AND 32 IN REF TO SRM 51-40-02. LOCATED AND DRILLED LEFT FLOOR SUPPORT AT FR 30 AND 32 IN REF TO SRM 51-40-02. INSTALLED NEW SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,059 hrs · 15,816 cycles

CORROSION ON L ANGLE AT FRAME 65 AND BAGGAGE DOOR SILL. REPAIRED IAW EO EM-53MR-1129.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 19,366 hrs · 16,047 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT OMEGA BEAM OUTBOARD SUPPORT CRACKED BEFORE FRAME 47 AND 48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SUPPORT OMEGA BEAM OUTBOARD AND CUTOUT FORWARD PART LOCATED, DRILLED NEW PART IAW SRM: 53-23-02 TRIMMED AFT SECTION PER SRM 53-23-02. INSTALLED SUPPORT OMEGA BEAM OUTBOARD IAW SRM: 51-40-02 AND INSTALLED BRACKET REMOVE FOR ACCESS IAW SRM: 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THRUST REVERSER — OBSTRUCTED (NR 1 ENGINE)

ON FLIGHT 3353 UPON LANDING AT AMA THE CREW REPORTED, RECEIVED AN ENGINE 1 REVERSE DISAGREE FAIL MESSAGE FOLLOWED BY AN ENGINE 1 UNCOMMANDED SHUTDOWN. DURING AFTER LANDING CHECKLIST, FLAPS RETRACTED TO 0 FOLLOWED BY FLAP FAIL MESSAGE ON EICAS. ON PARKING, FOUND PARKING BRAKE STUCK AND UNABLE TO ENGAGE PARKING BRAKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ICE AND SNOW PACKED INTO ALL 4 FLAP WELLS AND NOSE LANDING GEAR WHEEL WELL. REMOVED SNOW AND ICE FROM THRUST REVERSER AND VISUALLY INSPECTED ENGINE 1 AND FOUND NO DAMAGE. PERFORMED ENGINE GROUND RUNS ON BOTH ENGINES IAW RRMM 72-00-00, CHECKED TR IAW EMB AMM 78-31-01. NO DISCREPANCIES NOTED DURING RUNS AND CHECKS. REMOVED ICE AND SNOW FROM NOSE LANDING GEAR WELLS AND CHECKED PARKING BRAKE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 9,581 hrs · 8,466 cycles

DURING A IMBV INSPECTION A PREVIOUS REWORKED AREA ON THE SERVICE DOOR CUT OUT LOWER CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS, CLEANED AND PERFORMED NDT INSPECTIONS. APPLIED EPOXY PRIMER TO BLENDED AREAS. FABRICATED FORWARD DOUBLER, CLEANED AND TREATED THE DOUBLER. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-21-02. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2

DURING A IMBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED DOOR SILL. POSITIONED NEW SILL AND DRILLED, CLEANED, ALODINED AND PRIMED NEW SILL AND SILL AREA. REPAIR DONE IAW EMBRAER SRM (SRM EMB 145/1142 REV 40) CHAPTER 51-40-02.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,581 hrs · 8,466 cycles

DURING A IMBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED DOOR SILL. POSITIONED NEW SILL AND DRILLED. CLEANED, ALODINED AND PRIMED NEW SILL AND SILL AREA. REPAIR DONE IAW EMBRAER SRM (SRM EMB 145/1142 REV 40) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — ODOR (RIGHT) · airframe 6,949 hrs · 6,231 cycles

ON TAKEOFF APPROX 500 ', LAV SMOKE ILLUMINATED WITH ODOR OF SMOKE. FLIGHT ATTENDANT REPORTS HAZE BY LAV, AT 5000' LIGHT EXTINGUISHED. ODOR SUBSIDED. A/C RETURNED TO ORD. REMOVED AND REPLACED RT ENGINE ASSY IAW W/C 71-000-00 OPERATIONAL AND LEAK CHECK GOOD COMPLETED A FCF AND PASSED. AIRCRAFT RETURN TO SERVICE

Part: SMOKE DETECTOR — UNKNOWN (LAVATORY) · airframe 6,901 hrs · 6,188 cycles

LAV SMOKE CAME ON DURING CLIMB. PULLED CB'S E11 AND E12 PER PROCEDURES. ALSO LAV SMOKE SYSTEM TEST PER PROCEDURE DID NOT TEST PROPERLY. PURGED OF DEICING FLUID ODOR IAW AE3007A FIM 72-00-00-810-814 AND AE3007A MM 72-00-00 BY RUNNING ENGINES AT HIGH POWER. PERFORMED OPS CHK OF LAV SMOKE DETECTION SYSTEM IAW EMB145 AMM 26-14-00. OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,550 hrs · 5,829 cycles

EMERGENCY EXIT SIGN INOP LOCATED BELOW COCKPIT DOOR. REMOVED AND REPLACED FORWARD LOWER EXIT SIGN IAW EMB145 AMM 33-50-13. AIRCRAFT RETURNED TO SERVICE.

Part: YOKE — STICKING (CONTROL COLUMN) · airframe 6,015 hrs · 5,301 cycles

CONTROL YOKE FEELS LIKE IT IS JAMMING WHEN MOVING LEFT AILERON.

Part: CONTROL COLUMN — STUCK (COCKPIT) · airframe 5,994 hrs · 5,283 cycles

DURING TAXI CHECK, FLIGHT CONTROL JAMMED WHEN MOVING LEFT AILERON CONTROL COLUMN UN-JAMMED AFTER FEW MINUTES. RETURNED TO THE BLOCK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,778 hrs · 4,284 cycles

FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORMED CUTOUT OF DAMAGE. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-10 AND 51-40-02. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE.

Part: SKIN PANEL — DENTED (FUSELAGE)

PERFORM PERMANENT REPAIR ON RIGHT FORWARD FUSELAGE ONE IAW EO EM-53MR-632R2 DUE TO DENT IN SKIN. REPAIRED FUSELAGE IAW EO EM-53MR-632R2 BY REPLACING SKIN PANEL. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — ODOR (WINGS) · airframe 2,792 hrs · 2,455 cycles

LAVATORY SMOKE AT 2000 FT ON CLIMBOUT. SMELL IN AIRCRAFT. REPLACED ENGINE 1 AND ENGINE 2, OPERATIONAL CHECK OK. FCF SUCCESSFUL. AIRCRAFT RETURNED TO SERVICE. (K)