N653AE

Part: CONTROL VALVE — FAULTED (ZONE 700) · airframe 53,773 hrs · 50,227 cycles

BRAKE OTBD INOPERATIVE ON GEAR DOWN SELECTION. R & R NR 100 BRAKE CONTROL VALVE IAW AMM 32-41-06. OPS CHECKED GOOD. LEAK CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BLEED VALVE — FAULTED (NR 2) · airframe 53,474 hrs · 49,884 cycles

BLEED 2 VLV FAIL CAUTION MSG ON ATTEMPTED T/O AROUND 32 KTS.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 53,474 hrs · 49,884 cycles

BLEED 1 VALVE FAIL MESSAGE ON EICAS AFTER ADVANCING THRUST LEVERS. R+R'D #100 ENGINE BLEED VALVE IAW AMM 36-11-05. LEAK CHECK GOOD. PERFORMED BLEED 1 OPS CHECK IAW AMM 36-00-00. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: BLEED VALVE — DAMAGED (NR 2 ENGINE) · airframe 53,474 hrs · 49,884 cycles

BLEED 2 VLV FAIL CAUTION MSG ON ATTEMPTED T/O AROUND 32 KTS. ENG BLEED SYSTEM R&R ENGINE 2 BLEED VALVE IRT AMM 36-11-05.OPS CHECK GOOD.OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 53,229 hrs · 49,552 cycles

EMERGENCY LIGHTING FLOOR STRIP AT SEATS 34-5A NOT ILLUMINATING. R & R FLOOR PROXIMITY LIGHT IAW AMM 33-50-12 ON STRIP FLOOR PROXIMITY 1013194 NSN PN OFF STRIP FLOOR PROXIMITY 1013194 NSN

Part: HOT WATER POT — ODOR (ZONE 900) · airframe 53,185 hrs · 49,503 cycles

ELECTRICAL BURNING SMELL FROM HOT JUG AREA OF GALLEY. INSPECTED & FOUND OUTER CONNECTOR DETERIATED. R & R HOTJUG CONNECTOR IRT SB145-25-202. HOTJUG MISSING INSTALLED HOTJUG.OPS CHECK GOOD.OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 53,117 hrs · 49,413 cycles

BRAKE DEGRADED MESSAGE DISPLAYED WHEN TAKING THE RUNWAY. MESSAGE DISPLAYS ONLY WITH TOE BRAKES. FACT 10JUL25 10:55 CLT PERFORMED FUNCTION TEST OF BRAKE SYSTEM IAW AMM 32-41-00 PER FIM 32-41-00-810-804-A. FUNCTIONAL TEST PASSED AND NO CMC MESSAGE PRESENT. NO FURTHER DEFECTS NOTED, TRANSITORY CONDITION OF BRAKE SYSTEM AT THIS TIME. A/C OK FOR SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 52,326 hrs · 48,499 cycles

ENGINE BLD VLV 1 FAIL DURING TAKEOFF ROLL. ENGINE 1 BLEED VALVE REMOVED AND REPLACED IRW AMM 36-11-05-000-801-A AND AMM 36-11-05-400-80-A. OPS CHECK GOOD. LEAK CHECK GOOD. A/C OK FOR SERVICE

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 52,238 hrs · 48,410 cycles

E1 BLD VLV FAIL MSG ON EICAS. FACT 22JAN25 00:03 PHL R+R BLEED VALVE IAW AMM 36-11-05. BLEED 1 LEAK ON EICASE DURING OPS CHK. FOUND Y DUCT AT #1 DUAL TEMP VLV LEAKING. R+R COUPLING IRW AMM 21-60-01. OPS CHK GOOD

Part: ANTI-ICE SYSTEM — FAILED · airframe 51,906 hrs · 48,045 cycles

ON DESCENT WING A/ICE FAIL DISPLAYED WITH ENG 1 A/ICE FAIL INTERMITTANT. FACT 22NOV24 18:08 PHL PERFORMED WITH A/I OPS CHK IAW AMM REF 30-10-00 AND FOUND NO DEFECTS NOTED. A/C OKAY FOR SERVICE AT THIS TIME.

Part: CONTROL UNIT — FAULTED (STAB TRIM) · airframe 51,326 hrs · 47,358 cycles

PITCH TRIM BACKUP INOP EICAS MESSAGE DISPLAYED ON APPROACH. R+R HORIZONTAL-STAB CONTROL UNIT IAW AMM- 27-40-01. OPS CHECKED CONTROLS AND UNIT IAW AMM 27-40-00 OPS CHECK GOOD OK FOR SERVICE AT THIS TIME

Part: CHANNEL — MECHANIC ERROR (FUSELAGE) · airframe 50,883 hrs · 46,826 cycles

E034713 DURING DOUBLER REPAIR FOR GALLEY (CENTER BEAM GUSSET) FOUND MIS-DRILLED HOLE ON HAT BEAM. PERFORMED CUT OUT OF DAMAGED AREA ON CENTER BEAM, FAB. EXTERNAL REPAIR DOUBLER, INSTALLED EXTERNAL REPAIR DOUBLER ON CENTER HAT BEAM IAW EMB 145 SRM 53-21-10RE FIGURES 202 SHEET 2, ITEM 3 AND EO1-53-24-0294

Part: FIREWALL — CRACKED (RT NACELLE) · airframe 50,883 hrs · 46,826 cycles

E034081 RH ENGINE PYLON FIREWALL CRACKED AT TWO LOCATIONS. REMOVED DAMAGED RH ENGINE PYLON FIREWALL, PERFORMED CUTOUT OF NEW FIREWALL, FABRICATED SPLICE, AND INSTALLED NEW FIREWALL SECTIONS AND SPLICE IAW ETD2024-145-012367 REV "A", EMB 145 SRM 51-40-02 AND EO1-54-24-306.

Part: DOOR FRAME — DAMAGED (FRM 68 S15-16L) · airframe 50,883 hrs · 46,826 cycles

E034071 CARGO DOOR CUTOUT FRAME 68 DAMAGED BETWEEN STRINGERS 15L-16L. RAR CARGO DOOR CUTOUT FRAME 68 IAW EMB 145 SRM 51-40-02

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 50,883 hrs · 46,826 cycles

E034080 LH ENGINE PYLON FIREWALL IS CRACKED 2 EACH. ERFORMED CUTOUT OF DAMAGED AREA ON L/H ENGINE PYLON FIREWALL IAW ETD2024-145-012367 REV "A". DRILLIED NEW L/H ENGINE PYLON FIREWALL, FABRICATED SPLICE AND INSTALLED REPAIR IAW ETD2024-145-012367 REV "A" AND EMB 145 SRM 51-20-03 AND EO1-54-24-0300

Part: BRACKET — CORRODED (DOOR LINER) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E031814 MAIN DOOR INTERNAL BRACKET FOR LINER HAS CORROSION AROUND NUT PLATE HOLE. RAR MAIN DOOR INTERNAL BRACKET FOR LINER IAW EMB 145 SRM 51-20-03 AND 51-40-09

Part: RIB — CRACKED (LT WING) · airframe 50,883 hrs · 46,826 cycles

E033782 LH WING RIB 21 CRACKED. ACCOMPLISHED REPAIR OF L/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 AND EO1-57-24-0301

Part: DOOR FRAME — CORRODED (CARGO) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E033182 CARGO DOOR LOWER FRAME INBD PROFILE CORRODED AT NUT PLATE HOLES. : REMOVED CORRODED AND REPLACED WITH NEW & SERVICEABLE CARGO DOOR LOWER FRAME INBOARD L-PROFILE IAW EMB-145 SRM 51-10-03, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 33-34) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032947 LH OMEGA BEAM CORRODED ON INBD LOWER FLANGE BETWEEN FR33-34. REPAIRED LH OMEGA BEAM CORROSION ON INBD LOWER FLANGE BETWEEN FR33-34 IAW EO1-53-24-0282, ETD2024-145-011457 "REV A" AND EMB 145 SRM 53-00-10, TIEM 2 FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (FRM 29) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032945 LH OMEGA BEAM CORRODED ON INBD WEB AT FR29. REPAIRE IAW IAW ETD2024-145-011455 REV. A AND PIEDMONT EO1-53-24-0271.

Part: SHEAR TIE — CRACKED (FRM 62 S6-8R) · airframe 50,883 hrs · 46,826 cycles

E032511 SHEAR CLIP AT FR.62 BETWEEN STGR. 6R-8R IS CRACKED. RAR SHEAR CLIP AT FR.62 BETWEEN STGR. 6R-8R IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 72 S7-8R) · airframe 50,883 hrs · 46,826 cycles

E032510 SHEAR CLIP AT FR.72 BETWEEN STGR. 7R-8R IS CRACKED. ACCOMPLISHED REPAIR OF SHEAR CLIP AT FR72 BETWEEN STGR. 7R-8R IAW EMB-145 SRM 53-31-04 RE. ITEM 2, FIGURE 207.

Part: SEAT TRACK — CORRODED (RT NR 4) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032437 R/H UPPER SEAT TRACK #4 HAS MULTIPLE DAMAGE AND CORROSION. R&R RH UPPER SEAT TRACK #4 IAW EMB145 AMM 53-01-06.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032492 SERVICE DOOR CENTER SILL IS CORRODED AT FWD AND CENTER SCREW HOLES. REMOVED CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (WATER LINE) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032424 LAV L/H WATER LINE SUPPORT IS CORRODED UNDERNEATH. RAR THE LAV LH WATER LINE SUPPORT IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032427 R/H UPPER SEAT TRACK #5 HAS MULTIPLE DAMAGE AND CORROSION. REMOVED AND REPLACED R/H OUTBD SEAT TRACK #5 IAW EMB 145 AMM 53-01-06. TQW S/N 2105

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032378 SERVICE DOOR CUTOUT LWR CENTER SILL CORRODED. BLENDED AS REQUIRED TO REMOVE DAMAGE FROM SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB-145 SRM 51-10-03. UT CHECK INDICATES 0.063" REMAINING THICKNESS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLED BLENDED AREA WITH HYSOL IAW EMB-145 SRM 53-21-02 RE ITEM 2, FIGURE 201 AND EO1-53-24-0299

Part: SEAT TRACK — CORRODED (LT NR 5) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032440 L/H LWR SEAT TRACK #5 HAS MULTIPLE DAMAGE A CORROSION. RAR CABIN LH #5 LOWER SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032428 R/H LWR SEAT TRACK #5 HAS MULTIPLE DAMAGE AND CORROSION. REMOVED AND REPLACED R/H INBD SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032377 SERVICE DOOR CUTOUT LWR AFT SILL CORRODED. RAR SERVICE DOOR CUTOUT LWR AFT SILL IAW EMB 145 SRM 51-40-02

Part: GUSSET — CORRODED · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032379 GALLEY CENTER BEAM GUSSET CORRODED. RAR GUSSET IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 26 S16-17R) · airframe 50,883 hrs · 46,826 cycles

E032412 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 16R-17R IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (RT NR 4) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032438 R/H LWR SEAT TRACK #4 HAS MULTIPLE DAMAGE AND CORROSION. R&R RH INBD SEAT TRACK #4 IAW EMB145 AMM 53-01-06.

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032381 CROSS SUPPORT BEAM CORRODED AT FR20. RAR CROSS SUPPORT BEAM AT FR20 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: SUPPORT BRACKET — CORRODED (FRM 20) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032383 RAMP SUPPORT FLANGE BRACKET CORRODED AT FR20. REMOVED AND REPLACED RAMP SUPPORT FLANGE BRACKET AT FR20 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (LT NR 6) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032430 L/H SEAT TRACK #6 HAS MULTIPLE DAMAGE AND CORROSION. R&R LH INBD SEAT TRACK #6 IAW EMB145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (FRM 39) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032464 CENTER OMEGA BEAM GUSSET AROUND NUTPLATE HOLE AT FR-39 HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032376 SERVICE DOOR CUTOUT LWR FWD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR CUTOUT LWR FWD SILL IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (LT NR 5) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032439 L/H UPPER SEAT TRACK #5 HAS MULTIPLE DAMAGE AND CORROSION. R&R LH UPPER SEAT TRACK #5 IAW EMB145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032479 LH #3 FLOOR SILL CORRODED. RAR L/H #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRM 49) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032449 L/H OMEGA BEAM GUSSET AT FR-49 HAS CORROSION. RAR #6 L/H OMEGA BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (LT NR 6) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032429 L/H UPPER SEAT TRACK #6 HAS MULTIPLE DAMAGE AND CORROSION. : RAR L/H UPPER SEAT TRACK #6 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032461 R/H FLOOR SILL #3 HAS CORROSION AT MULTIPLE AREAS. REMOVED AND REPLACED R/H FLOOR SILL #3 IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (FRM 18) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032382 CROSS SUPPORT BEAM CORRODED AT FR18. RAR THE CROSS SUPPORT BEAM AT FR18 IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRM 68) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032052 CARGO DOOR STRUCTURE CUTOUT FR68 SHEAR CLIP SPLICE CORRODED. RAR CARGO DOOR STRUCTURE CUTOUT FR68 SHEAR CLIP IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRM 65) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032051 CARGO DOOR STRUCTURE CUTOUT FR65 SHEAR CLIP SPLICE CORRODED. RAR PREVIOUS REPAIR OF THE CARGO DOOR STRUCTURE CUT OUT FR65 SHEAR CLIP IAW EMB 145 SRM 53-31-04, ITEM 4, FIGURE 212. PREPPED, PRIMED AND PAINTED CARGO DOOR CUTOUT FR65 SHEAR CLIP AS REQUIRED IAW EMB 145 CPM 51-21-06 AND PDT BULLETIN 51-02

Part: SHEAR TIE — CRACKED (FRM 65 S18-19L) · airframe 50,883 hrs · 46,826 cycles

E032047 SHEAR CLIP POSSIBLE CRACK AT FR65 BETWEEN STRGS 19L-18L. RAR SHEAR CLIP AT FR65 BETWEEN STGRS 19L-18L IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED (CARGO) · corrosion level 2 · airframe 50,883 hrs · 46,826 cycles

E032049 CARGO DOOR STRUCTURE CUTOUT LWR CENTER SILL CORRODED. RAR THE CARGO DOOR STRUCTURE CUTOUT LWR CENTER SILL IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 73 S16-17L) · airframe 50,883 hrs · 46,826 cycles

E032046 SHEAR CLIP CRACKED AT FR73 BETWEEN STRGS 17L-16L. REMOVED AND INSTALLED NEW AND SERVICEABLE SHEAR CLIP AT FR73 BETWEEN STRGS 17L-16L IAW EMB-145 SRM 51-40-02.

Part: SKIN — CRACKED (FRM 79) · airframe 50,883 hrs · 46,826 cycles

E031667 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 79. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 79 STR 3L-4L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303

Part: SKIN — CRACKED (FRM 78) · airframe 50,883 hrs · 46,826 cycles

E031612 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 78. ABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 78 STR 4R-5R AND 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302

Part: SKIN — CRACKED (FRM 80) · airframe 50,883 hrs · 46,826 cycles

E031613 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 80. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 80 STR 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302

Part: YOKE — CORRODED (RT ENGINE) · airframe 50,883 hrs · 46,826 cycles

E031858 R/H ENG. FWD. ENGINE YOKE, FWD. FITTING HAS POSSIBLE CRACK. : REMOVED AND INSTALLED NEW R/H ENG. YOKE UPPER AND LOWER FWD. AND AFT LINKAGE IAW FCD1-54-21-0017D

Part: SKIN — CRACKED (FRM 77) · airframe 50,883 hrs · 46,826 cycles

E031665 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUNDRIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 4L-5L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303

Part: SKIN — CRACKED (FRM 77) · airframe 50,883 hrs · 46,826 cycles

E031611 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 5R-6R IAW EMB 145 SRM 53-32-01. ITEM 9, FIGURE 213 AND EO1-53-24-0302

Part: ANGLE — CORRODED (VERT TO FUSE) · airframe 50,883 hrs · 46,826 cycles

E031084 LH VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK TOWARDS THE FWD END. RAR CRACKED LH VERTICAL STAB TO FUSELAGE ANGLE AND REPAIR ANGLE DOUBLER INCORPORATED WITH ANGLE IAW EMB 145 SRM 51-40-02

Part: VALVE — FAULTED · airframe 50,855 hrs · 46,798 cycles

BLD 2 OVER TEMP DURING CLIMB BETWEEN 16K AND 18K IN ICING CONDITIONS. REMOVED AN REPLACED #200 FAN AIR VALVE IAW AMM 36-11-03. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: SENSOR — FALSE INDICATION (BLEED TEMP) · airframe 50,851 hrs · 46,793 cycles

BLEED 2 OVERTEMP MSG IN ICING CONDITIONS FACT 30MAR24 20:00 PHL R+R BLEED 2 TEMP SENSOR AT PRECOOLER IAW AMM 36-20-01. OPS CHECK GOOD IAW 36-00-00-700-806A AND 30-00-00-700-801A, 802B

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,954 hrs · 45,790 cycles

SMOKE AND FUMES IN THE CABIN AND COCKPIT, AND EVACUATED. (THE CAPT SAID F/O WAS THE FIRST,FOLLOWED BY THE CAPTAIN, THEN THE FLIGHT ATTENDANT NOTICED THERE WAS SMOKE EVERYWHERE. THEY FOLLOWED THE EMERGENCY PROCEDURE GRABBED THE LOG BOOK AND EVAC. MX INSPECTED A/C AND RAN ENGINES WITH NO DEFECTS NOTED. RAN BOTH PACKS, PACK 1 OPS CHECK GOOD. PACK 2 OVERHEAT DISPLAYED. SEE SEQ 2 THIS LP FOR PACK 2 DEFERRAL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,677 hrs · 45,477 cycles

LAV SMOKE INDICATION IN FLIGHT WITH VAPE LIKE FUMES VISUALLY INSPECTED LAV AND LAV INDICATOR FOR DEFECTS. NO DEFECTS NOTED AT THIS TIME PERFORMED LAV SMOKE DETECTION OPS CHECK IAW AMM 26-14-00 OPS CHECK OK. A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,614 hrs · 45,407 cycles

EICAS BLANKED OUT WITH BURNING SMELL SWAPPED EICAS AND FO MFD IAW AMM 34-22-01 PER MEL 34-1. OPS CHECK GOOD. INSPECTED ELECTRICAL CONNECTORS WITH NO DEFECTS NOTED. SEE THIS LP SEQ 2 FOR MEL. SWAPPED EICAS AND FO MFD DUE TO EICAS BLANKING OUT WITH BURNING SMELL. MAIN PANEL DISPLAYS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,344 hrs · 45,102 cycles

EMERGENCY LIGHTS WILL NOT WORK FROM FA PANEL. REMOVED AND REPLACED FA CONTROL PANEL IAW AMM 25-27-09. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,226 hrs · 44,959 cycles

AFTER TAKE OFF E1/E2 TR DISAGREE MESSAGE ON EICAS. FACT 02MAY23 15:07 CLT INSPECTED FOR DEFECTS. NONE NOTED AT THIS TIME. PERFORMED OPS CHECK IAW EMB 145 AMM 78-32-00. SYSTEM OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,226 hrs · 44,959 cycles

AFTER TAKE OFF L/G AIR/GND FAIL MESSAGE DISPLAYED ON EICAS. MESSAGE PERSISTED THROUGHOUT FLIGHT, AND EXTINGUISHED DURING APPROACH. INSP. NLG PROX SWITCH FOR MISALIGNMENT. OPS CHECKED PROX SWITCH IAW AMM 32-63-05 TASK 32-63-05-700-801-A OPS CHECK GOOD. PERFORMED GEAR SWING MULTIPLE TIMES NO DEFECTS NOTED. SYSTEM CHECK GOOD AT THIS TIME. REF LOGPAGE 276679 SEQ 2 AND 3 LOGPAGE 276680 SEQ 1 AND 2 AND LOGPAGE 276681 SEQ 2 FOR ADDITIONAL MX.PER MOC SERVICE NLG STRUT. SUSPECT INCORRECT SERVICING. FOUND NOSE GEAR TO BE INCORRECTLY SERVICED. RE-SERVICED NOSE GEAR STRUT IAW AMM 32-20-01. A/C OK FOR SERVICE. WHILE TORUBLESHOOTING LP 276679-1 WITH WORKCARD 32-70-16 FOUND MLG #1 FWD PROX SWITCH FAIL. FACT 01MAY23 17:05 CLT REMOVED AND REPLACED AIR/GROUND RELAYS IN POSITIONS K0352, K0353, AND K0453. SEE LP 276679-1 FOR OPS CHECK. RELAYS R&R IRT AMM 20-13-02

Part: BATTERY — INOPERATIVE (RH) · airframe 48,165 hrs · 43,769 cycles

RH OVER WING INTERIOR EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING INTERIOR EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD

Part: NONE — NONE · airframe 47,679 hrs · 43,230 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. TROUBLESHOT AND FOUND WIRE BROKEN FROM FEMALE CONNECTOR, INSTALLED NEW PIN AND CONNECTOR ONTO HOUSING WIRE IN REFERENCE WITH ENVOY WIRING MANUAL 33-50-50. OPS CHECK GOOD. END.

Part: CRADLE — FAILED (AFT FLASHLIGHT) · airframe 46,689 hrs · 42,100 cycles

AFT FLASHLIGHT CRADEL NOT CHARGING-C/A-RAR AFT FLASHLIGHT CRADEL IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPS CHECK GOOD

Part: BUSHING — MIGRATED (LT AILERON) · airframe 46,636 hrs · 42,033 cycles

LEFT AILERON FUTTER DAMPER FITTING HAS MIGRATING BUSHINGS.(MAJOR REPAIR)-C/A-COMPLETE: RAR LH AILERON DAMPER FITTING IAW EO EM-27MR-112.

Part: SKIN — CORRODED (FR 57-58) · corrosion level 2 · airframe 46,636 hrs · 42,033 cycles

EXTERIOR FUSELAGE SKIN IS CORRODED BETWEEN FR 57 RT AND 58 RT AND BETWEEN STR 19 RT AND STR 20 RT (LEVEL2 CORROSION) (MAJOR REPAIR)-C/A-COMPLETE:RAR POTABLE WATER FILL/OVERFLOW NIPPLE DOUBLER IAW SRM 51-40-02.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 46,636 hrs · 42,033 cycles

EMERGENCY FLASHLIGHT HOLDER/CHARGER LOCATED ON THE LAV BULKHEAD IS INOP.-C/A-COMPLETE:RAR EMERGENCY FLASHLIGHT ASSEMBLY LOCATED AT THE LAV BULKHEAD IAW AMM 33-50-16. OPC GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 46,636 hrs · 42,033 cycles

EMERGENCY FLOOR PROXIMITY STRIP LIGHT #1 HAS DAMAGED WIRE ON AIRCRAFT SIDE.-C/A-COMPLETE:REPAIRED WIRE IAW SWPM 20-21-00 SEE PS-2 FOR OPS CHECK

Part: BUSHING — MIGRATED (PCU ATTACHMENT) · airframe 46,636 hrs · 42,033 cycles

LH AILERON INBD PCU ATTACHMENT FITTING HAS MIGRATING BUSHING. RAR'D LH AILERON PCU FITTING IAW EO# EM-27MR-112.

Part: FRAME — CRACKED (FRM 68) · airframe 46,636 hrs · 42,033 cycles

FRAME 68 FRAME HALF IS CRACKED UNDERNEATH BAGGAGE DOOR HOLD OPEN ROD BRACKET.-C/A-COMPLETE:REPAIRED FRAME 68 IAW SRM 53-31-04 AND ERS-EM-5300-4380.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 46,636 hrs · 42,033 cycles

EMERGENCY EXIT FLOOR PROXIMITY LIGHT STRIP WIRE CONNECTOR IS BROKEN AT FLOORBOARD 251DF, NEAR FRAME 44.-C/A-COMPLETE:INSTALLED NEW WIRE SPLICE CONNECTOR AT FLOORBOARD 251DF (NEAR FRAME 44) IAW EMB145 SWPM 20-21-00. SEE BOW357503 FOR EMERGENCY LIGHTS OPS CHECK.

Part: LIGHT — DIM (CABIN) · airframe 46,636 hrs · 42,033 cycles

L/H #6 EMERGENCY LIGHT STRIP IS DIM.-C/A-COMPLETE:INSTALLED NEW LH #6 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. SEE E874420 FOR OP'S CHECK.

Part: FRAME — CRACKED (FRM 25 S15-16R) · airframe 46,636 hrs · 42,033 cycles

RH FR25 IS CRACKED BETWEEN STR 16R-15R. COMPLETE:REPAIRED RH FR 25 IAW SRM 53-00-04.

Part: BUSHING — MISSING (RT AILERON) · airframe 46,636 hrs · 42,033 cycles

RH AILERON FLUTTER DAMPER FITTING IS SCORED AND MISSING BUSHINGS.-C/A-COMPLETE:RAR FITTING ASSY ON RH AILERON IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (FRMS 65-68) · airframe 46,636 hrs · 42,033 cycles

BAGGAGE DOOR SILL IS CORRODED.(LEVEL 1 CORROSION)(MAJOR REPAIR)-C/A-COMPLETE:COMPLETED INSTALLATION OF CARGO DOOR SILL IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 46,636 hrs · 42,033 cycles

SVC DOOR CUTOUT CENTER SILL IS CORRODED.(LEVEL 1 CORROSION)(MAJOR REPAIR)-C/A-COMPLETE:RAR'D SERVICE DOOR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CRACKED (FRM 66) · airframe 46,636 hrs · 42,033 cycles

FRAME 66 IS CRACKED AT CARGO DOOR SILL-C/A-COMPLETE:REPAIRED FRAME 66 AT CARGO DOOR SILL AREA IAW SRM 53-00-04

Part: SUPPORT — CRACKED (FRMS 67-68) · airframe 46,636 hrs · 42,033 cycles

CRACK ON LOWER SUPPORT BETWEEN FR.67 FR.68, UNDER CARGO LIFT MECHANISM LOWER ATTACH BRACKET (@ FWD OF 3 HI-LOC).-C/A-COMPLETE:RAR'D LOWER SUPPORT BETWEEN FR.67 FR.68 FOR CARGO DOOR LIFT/LOWER MECHANISM IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (FRMS 59-60) · airframe 46,636 hrs · 42,033 cycles

RIGHT DIDGITAL BETWEEN FRAME 59-60 HAS A 1/4" CRACK.-C/A-COMPLETE:RAR'D RH DIGITIAL BETWEEN FRAMES 59-61 IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 66) · airframe 46,636 hrs · 42,033 cycles

FRAME 67 IS CRACKED AT CARGO DOOR SILL-C/A-COMPLETE:REPAIRED FRAME 67 AT CARGO DOOR SILL AREA IAW SRM 53-00-04

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 46,494 hrs · 41,857 cycles

AFT CABIN EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-51-01. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 46,459 hrs · 41,812 cycles

INBND MIA DECLARED EMEREGNCY FOR SPOILER FAIL. COMPLIED W/QRH, NO CHANGE. THEN AT BASE LEG DROPPED MLG, CONFIGURED FOR LANDING, EICAS MSG -INDICATIONS WENT AWAY. REF. LOG PAGE 4770561-1 - C/W DEACTIVATION OF SPOILERS BY PULLING AND COLLARING CB S F13, F14 AND F21 - THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT AND FOUND TO BE BE IN SAFE CONDITION FOR FERRY FLIGHT. OPEN

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 46,457 hrs · 41,811 cycles

SPOILER FAIL EICAS MESSAGE AT CRUISE WITH SPLRS INDICATION SHOWING OPN BUT SPOILERS VERIFIED CLOSED BY FA DECLARED EMERGENCY. QRH PROCEDURE C/W MESSAGES CLEARED AFTER PULLING CBS INSTRUCTED IN QRH-C/A-T/S PER FIM RAR SPOILER CONTROL UNIT IAW AMM 27-63-02 OPS CHECK GOOD A/C OK FOR SERVICE

Part: PROXIMITY SENSOR — FAULTED (SPOILERS) · airframe 46,453 hrs · 41,805 cycles

SPOILER FAIL, EMERGENCY DECLARED.- R/H & L/H OUTBOARD SPOILER PROXIMITY SWITCH CONNECTOR IS CORRODED.-C/A-RAR L/H OB SPOILER PROX. SWITCH IAW EMB-145 MM 27-63-04. OPS CK GOOD. REF NRWC 653-ORD-05471 FOR SUPPORTING ACTION

Part: TORQUE LINK — LOOSE (NLG) · airframe 46,350 hrs · 41,694 cycles

NOSE WHEEL SHYMMY ON BOTH HIGH AND LOW SPEED ROLLOUT.-C/A-FOUND TORQUE LINK TO BE LOOSE. TIGHTEN AND RESECURED TORQUE LINK CASTLATED NUT IAW AMM 32-20-10. TAXI CHECK GOOD.

Part: CHARGER — NOT REPORTED (EMERGENCY LIGHTS) · airframe 45,758 hrs · 41,043 cycles

REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY CHARGER EMB WC 33-700-19 ETN-EM-25-385. C/A: REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY CHARGER, IAW E145 WORK CARD 33-700-19. OPERATIONS CHECKED GOOD, IAW E145 WORK CARD 33-700-17.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,251 hrs · 40,522 cycles

LT EMERGENCY LIGHT INOPERABLE. C/A RAR LT EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,314 hrs · 39,655 cycles

MAIN DOOR OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR OVERHEAD EMERGENCY LIGHT IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,720 hrs · 39,091 cycles

FOUND EXIT LIGHT OVER SERVICING DOOR INOP DURING PS-1 CHECK. REMOVED AND REPLACED #2 EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS CHECK GOOD IAW AMM 33-50-00

Part: SWITCH — STUCK (FO MICROPHONE) · airframe 43,270 hrs · 38,691 cycles

STUCK MICROPHONE COMMS 2, T/S & FOUND F/O GLARESHIELD PTT STUCK IN TX POSITION, RELEASED SWITCH & MESSAGE EXTINGUSHED. REMOVED AND REPLACED FIRST OFFICER`S PTT SWITCH IAW AMM 23-51-03 OPS CHECK GOOD.

Part: UPLOCK — FAILED (RT MLG) · airframe 43,179 hrs · 38,606 cycles

SIPPLEMENTAL KNOCKING SOUND FROM UNDERSIDE OF AIRCRAFT ON TAKEOFF. RIGHT LANDING GEAR INDICATION FLUCTUATING FROM UP/TRANISIENT "TRANSFERRED TO NRWC 653-ORD-04231"/ C/A- REMOVED AND REPLACED R/H MLG UPLOCK BOX IAW AMM 32-33-10. OPS CHECK GOOD. COULD NOT DUPLICATE KNOCKING.

Part: PITOT LINE — CONTAMINATED · airframe 42,951 hrs · 38,425 cycles

LOST ALL AHRS INSTRUMENTS IN CLB. UNRELIABLE ADC INSTURMENTS. SPS ADVANCED. PERFORMED PITOT DRAINS HOSE INSP AND FOUND WATER ACCUMULATOI. DRAIN WATER AND PERFORMED OPS TEST OF PITOT-STATIC SYSTEM AS PER MEB 145 AMM 34-13-00. OPC OF AHARS GOOD AS PER EMB 145 AMM 34-21-00. OPC OF ADC SYSTEM AS PER EMB 145 AMM 34-15-00. ALL CHECKS GOOD

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 42,896 hrs · 38,382 cycles

PILOT`S WINDSHIELD CUTOUT HAS ELONGATED HOLE ON UPPER OUTBD SIDE-C/A-REMOVED AND REPLACED PILOT?S LH WINDOW STRUT IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,896 hrs · 38,382 cycles

SSI-53-20-02 FWD LWR SERVICE DOOR FRAME HAS CORROSION AROUND NUTPLATE HOLE (MARKED). C/A-PERFORMED PERMANENT REPAIR OF SERVICE DOOR FRAME IAW SRM 53-00-04-RE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,896 hrs · 38,382 cycles

LT OMEGA BEAM PREVIOUS REPAIR CORRODED AT FRAME 25. C/A-REPAIRED PREVIOUS REPAIR ON LT OMEGA BEAM AT FRAME 25 IAW SRM 51-40-02.

Part: SHUNT — CORRODED (APU) · airframe 42,896 hrs · 38,382 cycles

CORROSION AND ARCHING ON APU CONNECTING BAR MOUNTING SUFACE SHUNT. C/A-PERFORMED PERMANENT REPAIR ON APU CONNECTING BAR SHUNT AND FR 80 IAW ERS-EM-53MR-3794.

Part: SUPPORT — CORRODED (WASTE VALVE) · airframe 42,896 hrs · 38,382 cycles

TOILET WASTE VALVE SUPPORT CORRODED. C/A-REPAIRED TOILET WASTE VALVE SUPPORT IAW SRM 53-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,896 hrs · 38,382 cycles

SERVICE DOOR CENTER SILL CORRODED AROUND SERVAL NUTPLATES. C/A-REMOVED AND REPLACE SERVICEABLE SERVICE DOOR CENTER SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,896 hrs · 38,382 cycles

CARGO DOOR SILL CORRODED AT NUT PLATE HOLE. C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02 AND SRM 51-20-03.

Part: LIGHT — CRACKED (CABIN) · airframe 42,896 hrs · 38,382 cycles

#1 AND #4 RH ISLE FLOOR EXTRUSION CRACKED-C/A-COMPLETE:REMOVED AND REPLACED #1 AND #4 RH ISLE FLOOR EXTRUSION IAW EMB 145 AMM 33-50-12

Part: LIGHT — CRACKED (CABIN) · airframe 42,896 hrs · 38,382 cycles

#1 EMERGENCY FLOOR LIGHT EXTRUSION CRACKED-C/A-COMPLETE:REMOVED AND REPLACED #1 EMERGENCY FLOOR LIGHT EXTRUSION IAW EMB 145 AMM 33-50-12

Part: LIGHT — BROKEN (COCKPIT) · airframe 42,896 hrs · 38,382 cycles

FLIGHT DECK EMERGENCY LIGHT ASSEMBLY BROKEN REQUIRES REPLACEMENT. OLD PART TEMP INSTALLED UNTIL PROCUREMENT OF NEW ASSEMBLY.-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY LIGHT IN FLIGHT DECK IAW EMB 145 AMM 33-30-01.

Part: FCU — FAILED (FUEL SYSTEM) · airframe 42,893 hrs · 38,377 cycles

FUEL IMBALANCE CAUTION MESSAGE ON EICAS APPROXIMATELY 300 FEET AGL. TANK 1 TOTAL QTY INDICATING 0 LBS. DID NOT SUSPECT FUEL LEAK. C/A-FUEL PANEL SHOWS FCU 1 FAIL REMOVED AND REPLACED FCU IAW AMM 28-41-01 CHECK GOOD AT THIS TIME.

Part: CHARGER — FAILED (CABIN) · airframe 42,812 hrs · 38,287 cycles

LT AND RT OVER WING EMERGENCY LIGHTS INOP. C/A-REMOVED AND REPLACED NR 4 EPSU BATTERY AND CHARGER, OPC GOOD, IAW AMM 33-50-04. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 78160.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,799 hrs · 38,273 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP 2X IAW 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 42,506 hrs · 37,981 cycles

AFT CABIN FLASHLIGHT WON'T STAY SECURE IN CRADLE. C/A-REMOVED AND REPLACED AFT FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16.OPS CHK GOOD.

Part: STRINGER — BENT (FUSELAGE) · airframe 42,288 hrs · 37,752 cycles

STRINGER 13L BENT BETWEEN FR 22 AND FR 23. REPAIRED STRINGER 13L AT FR 22 AND FR 23 IAW SRM 53-00-03 AND ERS EM-53MR-3621.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 42,288 hrs · 37,752 cycles

STRINGER 13L BENT BETWEEN FR. 22 AND FR 23. C/A-REPAIRED STRINGER 13L AT FR. 22 AND FR 23 IAW SRM 53-00-03 AND ERS ?EM-53MR-3621.

Part: FRAME — DEFORMED (FUSELAGE) · airframe 42,288 hrs · 37,752 cycles

FRAME 21 DEFORMED BETWEEN STRINGERS 12L / 16L. INSTALLED REPAIR PARTS FOR REPAIR OF FRAME 21 BETWEEN STR 12L AND 17L IAW SRM 53-00-04 AND ERS EM-5300-3619.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 42,288 hrs · 37,752 cycles

ONE OF THE GALLEY OVERHEAD EMERGENCY LIGHTS IS OUT-C/A-REMOVED AND REPLACED THE GALLEY OVERHEAD EMERGENCY LIGHTS IAW EMB-145 AMM 35-50-09. OPS CHECK GOOD

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 42,288 hrs · 37,752 cycles

TEMPORARY DOUBLER INSTALLED BETWEEN FRAMES 21-22 STRINGERS 8L-11L MAJOR REPAIR. INSTALLED REPAIR FILLER, DOUBLER, AND TRIPLER FOR SKIN REPAIR BETWEEN FR21-22 AND STR 8L-11L IAW ERS- EM-53MR-3626.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 42,288 hrs · 37,752 cycles

TEMPORARY DOUBLER INSTALLED BETWEEN FRAMES 20-24 STRINGERS 11L-17L MAJOR REPAIR. REMOVED AND REPLACED LOWER LT CENTER FUSELAGE I SKIN IAW SRM 51-40-02, 51-20-01, ERS-EM-5300-3612 AND ETN-EM-53-292R2. REPAIR IS MAJOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,286 hrs · 37,751 cycles

FOUND FRAME 23 CRACKED BTW STR 10L -17L. MAJOR REPAIR. C/A-ACCOMPLISHED REPAIR OF FRAME 23 IAW ETD 2019-145-001597.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,286 hrs · 37,751 cycles

FOUND FRAME 22 CRACKED BTW STR 12L -17L. MAJOR REPAIR. C/A-ACCOMPLISHED REPAIR OF FRAME 22 BETWEEN STRINGERS 12L-17L IAW ETD-2019-145-001597.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 41,568 hrs · 37,027 cycles

FWD CABIN FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED FWD CABIN FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. NO FURTHER DISCREPANCIES WERE FOUND.

Part: ENGINE — FAILED (LEFT) · airframe 39,424 hrs · 35,084 cycles

STRONG OIL COMBUSTION ODOR WITH THE ENGINE BLEEDS DRIVING PACKS. DIMINISHED DURING CRUISE, STRONG AGAIN AT LOW IDLE THRUST, DURING DECENT. DIMMINISHED WITH INCREASED THRUST. STRONGER BEFORE SHUTTING DOWN AFTER NR 1. TROUBLESHOT IAW FIM 72-00-00-810-814. PERFORMED ETN-EM-79-015. INSPECTED 1ST TO 3RD STAGE LPT BLADES AND RTBS AND FOUND OIL WETNESS AND SIGNS OF PUDDLING. ETN EM-79-015 STEP 13 SUGGESTS ENGINE CHANGE REQUIRED. LPT INSPECTION DONE IAW 72-51-00-06 AND 72-41-01-200-801A. REMOVED AND REPLACED THE LT ENGINE IAW WC 71-000-00, OPS & LEAK CHECKED GOOD

Part: UNKNOWN — ODOR (CABIN) · airframe 39,415 hrs · 35,076 cycles

ACRID ODOR IN CABIN WHEN ENGINE BLEEDS DRIVE THE AC PACKS. THE ODOR GOES AWAY WHEN APU RUNS THE PACKS. COMPLIED WITH EM- 72-034. TROUBLESHOT, NO OIL DETECTABLE ODOR AT CONFIGURATIONS. CLEANED COWL AND GVI BOTH ENGINES.

Part: FIRE DETECTOR — FALSE ACTIVATION (APU BAY) · airframe 38,358 hrs · 34,097 cycles

PERFORMED SHUTDOWN OF THE APU. APU FIRE MESSAGE FOLLOWED EPC, FIRE STILL SHOWED. AFTER PRESSING THE FIRE EXTINGUISHER BOTTLE, THE FIRE NOW SHOWS OUT. GVI INSPECTION, NO FIRE NOTED. HAD TAIL WIND NOTED. REMOVED AND REPLACED THE APU FIRE DETECTOR IAW AMM 26-12-01. OPS CHECKED GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (APU) · airframe 37,915 hrs · 33,719 cycles

APU SHUT DOWN, FIRE WARNING AND BELL AND CLEAR. APU FIRE BOTTLE WAS NOT DISCHARGED, PERFORMED ADJ/TEST OF FIRE DETECTION SYSTEM , SYS TEST OK IAW AMM 26-10-00

Part: LIGHT — CRACKED (CABIN) · airframe 37,906 hrs · 33,711 cycles

FLOOR PROXIMITY LIGHT NR 1 IS CRACKED. REMOVED & REPLACED THE LIGHT IAW AMM 33-50-12.

Part: FLOOR SUPPORT — PUNCTURED (FRAMES 48-49) · airframe 37,906 hrs · 33,711 cycles

PUNCTURE ON RT FLOOR SUPPORT LOWER FLANGE BETWEEN FRAMES 48-49. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-2514.

Part: FITTING — GOUGED (RT AILERON) · airframe 37,906 hrs · 33,711 cycles

RIGHT AILERON DAMPER FITTING GOUGED. REMOVED AND REPLACED THE DAMPER FITTING IAW SRM 51-40-02, AND 51-20-03.

Part: FITTING — GOUGED (RT AILERON) · airframe 37,906 hrs · 33,711 cycles

RIGHT AILERON DAMPER FITTING GOUGED. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112

Part: BUSHING — MIGRATED (RT AILERON) · airframe 37,906 hrs · 33,711 cycles

RIGHT AILERON PCA FITTING HAS MIGRATED HAT BUSHINGS WITH WORN BUSHING HOLES. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02, AND 51-20-03

Part: FITTING — WORN (RT AILERON) · airframe 37,906 hrs · 33,711 cycles

RIGHT AILERON PCA FITTING HAS MIGRATED HAT BUSHINGS WITH WORN BUSHING HOLES. REMOVED AND REPLACED THE PCA FITTING IAW EO EM-27MR--112.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 37,906 hrs · 33,711 cycles

CORROSION ON SERVICE DOOR CENTER SILL. REMOVED AND REPLACED DOOR SILL IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 8) · airframe 37,906 hrs · 33,711 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT FRAME 8 BELOW STRINGER 9L. ACCOMPLISHED REPAIR TO EXTERNAL FUSELAGE SKIN IAW ERS-EM-53MR-2510.

Part: TRUNNION — CRACKED (LT MLG) · airframe 37,906 hrs · 33,711 cycles

LT MLG AFT UPPER TRUNNION CRACKED. REMOVED AND REPLACED SERVICABLE LT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-758

Part: FLOOR SUPPORT — CRACKED (FRAMES 59-60) · airframe 37,906 hrs · 33,711 cycles

CRACK ON RT LAV FLOOR SUPPORT AT AFT NUTPLATE HOLE. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-24-10 ITEM 3.

Part: SKIN — CRACKED (FRAME 8) · airframe 37,906 hrs · 33,711 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT FRAME 8 BELOW STRINGER 9L. ACCOMPLISHED REPAIR TO EXTERNAL FUSELAGE SKIN IAW ETD2016-145-113094.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 37,906 hrs · 33,711 cycles

SERVICE DOOR LOWER FRAME CORRODED AROUND AFT SCREW HOLE. ACCOMPLISHED REPAIR OF SERVICE DOOR LOWER FRAME IAW ERS-EM-52MR-688

Part: FLOOR SUPPORT — CRACKED (FRAMES 59-60) · airframe 37,906 hrs · 33,711 cycles

CRACK ON RT LAV FLOOR SUPPORT AT FWD NUTPLATE HOLE. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM RT LAV FLOOR SUPPORT AND FABRICATED AND INSTALLED DOUBLER IAW SRM 53-24-10 ITEM 3.

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,906 hrs · 33,711 cycles

RIGHT AFT UPPER TRUNNION CRACKED. REMOVED AND REPLACED THE RT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-757.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 37,906 hrs · 33,711 cycles

CARGO DOOR SILL CORRODED. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 37,906 hrs · 33,711 cycles

PASSENGER CABIN EMERGENCY LIGHT NR 6 HAS BROKEN CONNECTOR. INSTALLED SERVICEABLE CONNECTOR AND CONTACT ON EMERGENCY LIGHT STRIP NR 6 IAW EMB 145 SWPM 20-21-00.

Part: CARBON SEAL — FAILED (STARTER) · airframe 37,768 hrs · 33,582 cycles

NR 2 ENGINE FAILED TO START. NO ROTATION. REMOVED AND REPLACED NR 2 STARTER IAW AMM 80-10-01. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED NR 2 ENGINE ATS CLAMP IAW AMM 80-10-01. REMOVED AND REPLACED STARTER MAGNETIC CARBON SEAL IAW RRM 72-63-10. LEAK CHECKED GOOD.

Part: CARBON SEAL — DAMAGED (ENGINE) · airframe 37,364 hrs · 33,199 cycles

STRONG ODOR DURING TAKEOFF CLIMB AND DESCENTS. TRANSFERRED FROM LG PG 4066130, ITEM 1. AFTER CARBON SEAL REPLACEMENT SEE NRWC 653-DFW-02716, PERFORMED ETN-EM-72-034, NO ODOR AT THIS TIME TRANSFERRED TO AML LG PG 4066130, ITEM 1.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,348 hrs · 33,180 cycles

BAD ODOR IN THE COCKPIT. SEEMS LIKE OIL COMMING THROUGH THE PACKS. MORE SIGNIFICANT ON TAKEOFF AND CLIMB OUT. C/W ETN EM-72-034 R9 AND ENGINE RUNS, NO ODOR DETECTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,159 hrs · 33,010 cycles

LEFT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LT FWD EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECK FAILED. R & R LT FWD EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECK FAILED. R & R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04-000-801-A & 33-50-04-400-801-A. R & R NR 1 BATTERY PACK IAW AMM 33-50-04-000-802-A & 33-50-04-400-802-A. OPS CHECK GOOD AT THIS TIME END. EMERGENCY LIGHTNING BATTERY, PN 2013-1A, SN 64142.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 37,092 hrs · 32,950 cycles

LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 1 CHARGER, OPS CHECKED GOOD IAW AMM 35-50-04.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 37,088 hrs · 32,946 cycles

HIGH STAGE VALVE 1 FAILED ON DECENT, LATER CLEARED. NOTICED POSSIBLE OIL IN PACK, ODOR. RT ENGINE 1 HIGH STAGE VALVE IAW AMM 36-11-02. OPS AND LEAKS CHECK GOOD. SEE ITEM 1, LOG PAGE 4010164 FOR POSSIBLE OIL AND PACK SMALL. PERFORMED ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. NO ODOR OR SMOKE DETECTED.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 37,068 hrs · 32,927 cycles

EMERGENCY LIGHTS IN COCKPIT, CEILING, AISLE CEILING, AND LT EXTERIOR FWD WING LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 1 EPSU IAW WC 33-700-19. OPS CHECKED GOOD IAW 33-700-17.

Part: CHARGER — FAILED (CABIN) · airframe 37,039 hrs · 32,903 cycles

LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. T/S AND FOUND THERE WAS NO VOLTAGE AT CONNECTOR PLUG. R & R NR 1 EMERGENCY BATTERY AND POWER SUPPLY IAW W/C 33-700-19. OPC GOOD AT THIS TIME. EMERGENCY LIGHTING BATTERY, PN 2013-1ASMI, SN 82630.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 36,974 hrs · 32,837 cycles

LOWER LT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY AND CHARGER ASSY OPS CHECKED GOOD IAW AMM 33-50-04

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,620 hrs · 32,520 cycles

LEFT FWD EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE. R & R NR 1 EMER LIGHTING POWER SUPPLY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: FLASHLIGHT — UNSECURE (COCKPIT) · airframe 35,446 hrs · 31,481 cycles

CAPTAINS FLASHLIGHT DOES NOT STAY SECURED IN HOLDER. CAPTAIN FLASHLIGHT DEFERRED, M PROCEDURES COMPLIED WITH. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD MEL ITEM RESTORED.

Part: BRACKET — OUT OF ADJUST (ACCESS DOOR) · airframe 35,263 hrs · 31,317 cycles

NOSE ACCESS DOOR OPEN CAUTION. FLIGHT CREW PLACARDED, ACCESS DOOR INDICATION M PROCEDURES COMPLIED WITH. CHECK FWD ELECTRONICS DOOR MICRO SWITCH, NO DEFECTS NOTED. ADJUSTED & LUBED SLIDING DOOR BRACKET. PERFORMED OPERATIONS CHECK IAW AMM 52-71-00. OPERATIONS CHECKED OK. MEL 52-7 RESTORED.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 35,168 hrs · 31,234 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT DAMAGED, DEFERRED ORIG AML PG 3924724-1 MEL 25-53. R & R AFT FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 33-50-16, OPERATION CHECKED GOOD. MEL ITEM RESTORED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,012 hrs · 31,078 cycles

HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE I RT SKIN. R & R CTR FUSELAGE I RT SKIN IAW SRM 51-40-02, 53-20-01, 51-20-03, 51-40-06, 51-20-01 & ETN EM-53-262 R1 & EM-51-118.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT. CTR FUSELAGE I, RT TOP SKIN TEAR STRAP AT FRAME 22 HAS ELONGATED HOLE. REPAIRED IAW ERS-EM-53MR-1542.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT. ONE TOOLING MARK ON FRAME 61 BETWEEN 1L - 1R. PERFORMED REPAIR ON FRAME 61 IAW ERS-EM-53MR-1527.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT. LEFT HORIZONTAL STABILIZER UPPER SKIN TOOL MARK. PERFORMED DOUBLER REPAIR ON LT STABILIZER UPPER SKIN IAW ERS-EM-55MR-335.

Part: FRAME — DAMAGED (FUEELAGE) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT. ELONGATED HOLE ON FRAME 4, INBOARD OF STRINGER 06R. COMPLETED INSTALLATION OF REPAIR PARTS ON FRAME 4 IAW ERS-EM-53MR-1516.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,012 hrs · 31,078 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN 145-33816-003. R & R CTR FUSELAGE IV SKIN IAW SRM 53-24-01SI, 51-40-02, 51-20-01, 51-20-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-265.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE FWD FUSELAGE II SKIN, WIPER. R & R FWD FUSELAGE II SKIN IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, CPM 51-21-04, ETN-EM-51-118 & ETN-EM-53-206.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN 145-27270-006 IAW SRM 55-20-01, 51-20-01 03, 51-40-02 06, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 53-24-01SI, SRM 51-2003, 51-40-03, 51-20-01, 51-40-02, 51-40-06, ETN-EM-51-118 & ETN-EM-53-265.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-2001, 512003, 51-40-06, 55-20-01, ETN EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 55-21-01, 51-40-02, ETN-EM-55-073 & ETN-EM--55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

RIGHT ELEVATOR OTBD UPPER SKIN TIP DAMAGED. R & R RT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 55-20-01, 51-20-01, 51-40-02, 51-40-06, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR INBD LE. REMOVED & INSTALLED, & APPLIED EDGE SEALANT TO LT ELEVATOR INBD LE IAW SRM 55-20-01, 51-20-01, 51-40-02 & ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR MID SKIN TI. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-06, 51-20-01, 51-40-02 & ETN-EM-55-076. SEE NRTC BOW 198154 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,011 hrs · 31,077 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR OUTER LE. R & R RT ELEVATOR OUTER LE 145-30807-004 IAW SRM 51-20-01, 51-40-02, 55-20-01, ERS-EM-5500-331, ETN-EM-55-073 & ETN-EM-55-076.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 34,605 hrs · 30,706 cycles

SPS 1 INOPERATIVE. WARNING & SPS ADVANCED CAUTION ON EICAS. PERFORMED STALL PROTECTION. OPERATIONAL CHECKED IAW AMM 27-36-00. OPERATIONS CHECKED GOOD.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 34,605 hrs · 30,706 cycles

SPS 1 INOPERATIVE. WARNING ON EICAS PLU SPS ADVANCED CAUTION ON EICAS, ON CAPTAINS PFD AOA INDICATION BUTTON LT CORNER. R & R SPS COMPUTER IAW AMM 27-36-02. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,510 hrs · 30,624 cycles

FOUND CABIN EMER FLOOR PROXIMITY STRIP ASSEMBLY 2 & 3 INOPERATIVE IAW PS 2 INSPECTION. R & R NR 2 EMER LIGHTING SYS POWER SUPPLY BATTERY & BATTERY CHARGER IAW AMM 33-50-04. OPERATIONS CHECK FAIL, DID NOT FIX. SEE NRWC 653-ORD-02078 ITEM 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,115 hrs · 30,239 cycles

ROW 3 AISLE EMER LIGHT INOPERATIVE. R & R ROW 3 AISLE EMER LAMP IAW AMM TASK 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,115 hrs · 30,239 cycles

FLIGHT ATTENDANT'S EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT'S EMER FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 33,913 hrs · 30,072 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. TRANSFERRED TO NRWC 653-DFW-01933. ACCOMPLISHED MULTIPLE NRWC FOR ADJUSTMENT. ACCOMPLISHED MAIN DOOR INTERNAL HANDLE TEST, PASSED WITH 40 LBS IAW AMM 52-18-00. TRANSFERRED FROM NRWC 653-DFW-01933.

Part: HANDLE — OUT OF ADJUST (CABIN DOOR) · airframe 33,889 hrs · 30,046 cycles

MAIN CABIN DOOR DIFFICULT TO UNLOCK & OPERATE HANDLE. REQUIRES UNUSUAL AMOUNT OF FORCE TO OPEN. TRANSFERRED TO NRWC 653-DFW-01932. ADJUSTED DOOR HANDLE & FRAME ROLLERS IAW AMM 52-18-00. OPERATIONS CHECKED AT THIS TIME.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 33,883 hrs · 30,041 cycles

MAIN CABIN DOOR IS VERY HARD TO CLOSE & OPEN. TRANSFERRED TO NRWC 653-ABI-01930. ADJUSTED LT & RT UPPER MAIN DOOR ROLLERS IAW AMM 52-18-00 & ETN-EM-52-052. MEL RESTORED. OPERATIONS CHECKED GOOD. SEE NRWC 653-ABI-01930 ACTION TAKEN.

Part: NUT PLATE — BROKEN (PAX DOOR) · airframe 33,875 hrs · 30,032 cycles

TRANSFERRED FROM AML PAGE 3665100 ITEM 3. MAIN CABIN DOOR HARD TO CLOSE & OPEN. PERFORMED MAIN DOOR INTERNAL ACTUATING TEST IAW AMM 52-18-00. OPERATIONS CHECKED GOOD. REF NRWC 653-DFW-01923 ADJUSTED BOTH UPPER DOOR ROLLERS IAW AMM 52-18-00. PERFORMED MAIN DOOR INTERNAL ACTUATING TEST IAW AMM 52-18-00. OPERATIONS CHECKED GOOD. REF TO NRWC 653-DFW-01923 FOUND FWD UPPER DOOR ROLLER TOUCHING THE TRACK WHEN DOOR IS CLOSED & OPENED. FOUND LOWER 3/8 `S BOLT JUST SPINNING IN ROLLER BRACKET WHEN TRYING TO ADJUST ROLLER, NUTPLATE BROKEN. R & R NUTPLATE IAW SRM 51-40-09.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 33,821 hrs · 29,986 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. REPEAT WRITE-UP SEE PG 3665077 ITEM 2. REPOSITION CABIN ENTRY CURTAIN & CLEANED DOOR & FRAME SEAL IAW AMM 52-18-00.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 33,808 hrs · 29,970 cycles

HARD TO OPEN CABIN DOOR. LUBRICATED MAIN PAX DOOR. OPERATIONS CHECKED OK IAW AMM-52-18-00.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 33,623 hrs · 29,760 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN & CLOSE. LUBRICATED MAIN DOOR ROLLERS IAW AMM 52-21-02 & ETN EM-52-061. OPERATIONS CHECKED GOOD IAW AMM 51-18-00.

Part: SIGNAL COND UNIT — INOPERATIVE (FUEL SYSTEM) · airframe 33,230 hrs · 29,359 cycles

AFTER TAKEOFF LOST ALL FUEL INDICATION. MFD & EICAS INOPERATIVE REMAINDER OF FLIGHT. R & R FUEL CONDITION SIGNAL UNIT IAW MM 28-41-01 & PERFORMED OPERATIONS CHECK IAW MM 28-41-00, NO DASHES SHOWN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,104 hrs · 29,244 cycles

LEFT ENG PPH WENT TO 0 & TURNED RED & BLINKED AT APPROX 120 IAS. ABORTED TAKEOFF WT APPROX 41K LBS. HAD CREW PERFORM HI POWER RUN. ALL INDICATIONS NORMAL IAW RR MM 72-00-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,930 hrs · 29,079 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. INSTALLED REPAIR DOUBLER, FILLER, SHIM & REPAIR ANGLE IAW ERS EM-53MR-655.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,930 hrs · 29,079 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. INSTALLED REPAIR DOUBLER, FILLER, SHIM & REPAIR ANGLE IAW ERS-EM-53MR-616.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 32,930 hrs · 29,079 cycles

GALLEY ABOVE FLOOR FRAME 15 CHAFED AT STRINGER 02R. INSTALLED L SHAPED DOUBLER IAW ERS- EM-53MR-648.

Part: WIRE — BROKEN (CABIN) · airframe 32,930 hrs · 29,079 cycles

NUMBER 1 EMER LIGHT STRIP HAS BROKEN WIRES. INSTALLED CONNECTOR AT NR 1 LIGHT STRIP IAW WM 91-10-02 & SWPM 20-00-03, FOR OPERATIONS CHECK SEE BOW 160456.

Part: WIRE — BROKEN (CABIN) · airframe 32,930 hrs · 29,079 cycles

FIRST EMER LIGHT STRIP WIRE BROKEN. REPLACED ELEC CONNECTOR, MALE, ON THE POWER SUPPLY HARNESS ACFT SIDE TO THE FLOOR PROXIMITY STRIP LIGHT NR 1 IN THE MAIN CABIN IAW SWPM 20-21-00, 20-50-00 & 20-50-01 & IAW AMM 33-50-12 & 33-50-00, OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — INOPERATIVE (COMMS 1) · airframe 32,120 hrs · 28,448 cycles

AFTER DEPARTURE, BOTH COMMS 1 & 2 ARE CARRIER WAVE ONLY. NO VOICE COULD HEAR ATC ON COMMS 1 & 2. R & R NR 1 COMMS UNIT IAW AMM 23-00-01. OPS CHECKED GOOD.

Part: ACTUATOR — OUT OF ADJUST (RUDDER) · airframe 31,889 hrs · 28,272 cycles

ON TAKE OFF A/C YAWED TO THE RIGHT ABRUPTLY. WE WERE ABLE TO APPLY LEFT RUDDER PRESSURE AND CONTROL THE AIRPLANE WITH RUDDER, BUT YAW TRIM WAS STUCK IN FULL RIGHT POSITION. AFTER SEVERAL MINUTES OF FLYING WE WERE ABLE TO GET YAW TRIM TO WORK NORMALLY AND RECENTERED TRIM. ACCOMPLISHED ADJUSTMENT/TEST OF YAW TRIM ACUTATOR IAW EMB 145 AMM 27-24-00. NO DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,762 hrs · 28,175 cycles

FORWARD CABIN FLASHLIGHT CHARGE LIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,949 hrs · 27,519 cycles

2FLOOR PROXIMITY LIGHT INOPERATIVE. R & R NR 2 EMERGENCY LIGHT IAW AMM 33-50-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,919 hrs · 27,498 cycles

NR 2 FLOOR PROXIMITY LIGHT INOPERATIVE. R & R NR 2 EMERGENCY LIGHTS IAW AMM 33-50-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,944 hrs · 26,697 cycles

DURING B INSPECTION, FOUND THE REAR CABIN EMERGENCY FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE REAR CABIN FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,703 hrs · 26,515 cycles

DURING MAINTENANCE INSPECTION FOUND THE INTERIOR EMERGENCY LIGHT INOPERABLE ON THE RIGHT EXIT ROW ON PSU PANEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT INTERIOR EMERGENCY LIGHT IN EXIT ROW PSU PANEL IAW EMB-145-AMM-33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — TORN (CABIN DOOR) · airframe 29,589 hrs · 26,421 cycles

ON FLIGHT 42497 THE CREW REPORTED THE CABIN DOOR WAS VERY HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. WHILE TROUBLESHOOTING DISCOVERED UPPER FLAP TRIM SEAL TO HAVE BECOME TORN/UNGLUED. REPAIRED MAIN PASSENGER DOOR RUBBER TRIM SEAL FILLER STRIP IAW EMB AMM 52-00-01. ALSO FOUND THE PASSENGER DOOR INTERIOR DOOR HANDLE LOCK BOX ASSEMBLY TO HAVE BECOME LOOSENED. TIGHTENED LOCK BOX ASSEMBLY BOLT IAW ETN-EM-52-052. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — LOOSE (EMERGENCY LIGHT) · airframe 29,299 hrs · 26,176 cycles

DURING B INSPECTION FOUND LOOSE SCREWS IN THE LEFT OVERWING EMERGENCY LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED SCREWS IN THE LEFT OVERWING EMERGENCY LIGHT IN REF TO EMB AMM 53-04-20-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — UNSERVICEABLE (COCKPIT) · airframe 28,888 hrs · 25,832 cycles

ON FLIGHT 4033 THE CREW REPORTED THE LOWER CLIP MISSING FROM THE CAPTAIN’S FLASHLIGHT CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT CRADLE IAW EMB MM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 28,868 hrs · 25,815 cycles

DURING B INSPECTION FOUND THE MAIN CABIN DOOR EMERGENCY LIGHT INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,222 hrs · 25,289 cycles

ON FLIGHT 9801 THE CREW REPORTED THE AFT EMERGENCY FLOOR LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT DC/AC INVERTER NR 6 IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNKNOWN (CABIN) · airframe 28,222 hrs · 25,289 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY NR 4 REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY NR 4 AND CHARGER IAW AEA MTX WC 33-700-19 AND 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,922 hrs · 25,059 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHT OUT AT 12A PSU PANEL. THE AIRCRAFT WAS REMOVED FROM AND REMOVED AND REPLACED EMERGENCY LIGHT LAMP AS PER EMB AMM 33-50-00, OPS CHECKED GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 26,887 hrs · 24,207 cycles

DURING MAINTENANCE INSPECTION FOUND ROW 8 EMERGENCY LIGHT FLOOR STRIP WIRES BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT FLOOR STRIP IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOSE — CRACKED (AC BAY) · airframe 26,719 hrs · 24,087 cycles

ON FLIGHT 3453 THE CREW REPORTED THEY ENCOUNTERED MODERATE TURBULANCE EN ROUTE FOLLOWED IMMEDIATELY BY AN ODOR OF BURNING RUBBER MOSTLY IN THE COCKPIT. THE ODOR RETURNED ONCE MORE DURING DESCENT NO INDICATIONS FROM ANY SYSTEMS THAT WERE OUT OF THE ORDNARY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE LEFT AND RIGHT ACM DRAIN COLLECTOR HOSES PER AMM 21-51-05. PERFORMED OPERATIONAL CHECK OF THE COOLING SYSTEM WITH ENGINES AND APU RUNNING. NO BURNING ODOR AT THIS TIME. ALSO, COOLING SYSTEM WORKING PROPERLY NO FAULTS AT THIS TIME IAW EMB145 MM 21-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,471 hrs · 23,095 cycles

DURING ELECTRICAL EMERGENCY, EMERGENCY LIGHTS BATTERIES WERE DRAINED. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 23,809 hrs · 21,830 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 BATTERY PACK IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (REQUEST TO MAKE SEPARATE SDR’S)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,809 hrs · 21,830 cycles

(REQUEST TO MAKE SEPARATE SDR’S) DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,217 hrs · 21,400 cycles

FOR FLIGHT 2747 STATION OPERATIONS NOTIFIED MOC THAT ALL THE EMERGENCY LIGHTS HAD COME ON BY THEMSELF AND WENT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 AND NR 4 BATTERY PACKS AND CHARGER ASSEMBLY IAW MTX W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 22,992 hrs · 21,221 cycles

ON FLIGHT 3650 THE MAIN CABIN DOOR WILL NOT OPEN. THE DOOR APPEARS TO BE HANGING UP ON THE TOP FORWARD POINT OF CONTACT. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED THE FORWARD AND AFT TOP MAIN DOOR FRAME ROLLERS. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-18-00 AND 53-21-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 21,604 hrs · 20,142 cycles

ON FLIGHT 3331 AFTER TAKEOFF THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT THAT DISSIPATED AFTER ABOUT A MINUTE OR TWO. THE SMELL RESEMBLED SOMETHING BURNING IN AN OVEN. THE AIRCRAFT LANDED AT THE DESTINATION WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED BOTH ENGINE RUN UP STATIC CHECK AT TAKE OFF POWER AND DIFFERENT POWER SETTINGS, UNABLE TO DUPLICATE ANY BURNING ODOR. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE 71-00-00.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 21,335 hrs · 19,928 cycles

FOR FLIGHT 3509 THE CAPTAIN WAS ON THE RUNWAY HOLDING AND ENGAGED THE EMERGENCY BRAKE AND DID NOT GET THE "BRAKE ON" LIGHT. THE CAPTAIN ELECTED TO RETURN TO THE GATE TO GET MAINTENANCE. REMOVED AND REPLACED LIGHT INDICATOR SWITCH IAW EMB145 AMM 20-13-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 20,960 hrs · 19,633 cycles

FLIGHT 3789, RIGHT AFTER TAKEOFF CREW REPORTED RECEIVING A LAVATORY SMOKE MESSAGE ON EICAS. FOLLOWED AOM PROCEDURES & REQUESTED CRASH, FIRE & RESCUE UPON LANDING. ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCIDENT. AFTER LANDING, FIRE DEPARTMENT INFORMED CAPTAIN THAT IT APPEARED THAT THE RT OUTBOARD BRAKE WAS FROZEN & NR 4 TIRE DRAGGING. NO OTHER EICAS MESSAGES NOTED. ACFT REMOVED FROM SERVICE. R & R NR 4 MLG BRAKE ASSY IAW 32-600-14. R & R NR 4 MLG TIRE IAW 32-700-11. R & I SERVICEABLE SMOKE DETECTOR IN LAVATORY IAW 26-12-01. TEAR DOWN REPORT INDICATES CAUSE OF SMOKE IN ENGINE 1 DUE TO FAILURE OF NR 4 CARBON SEAL. ACFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — FAILED (ZONE 200) · airframe 14,476 hrs · 14,203 cycles

DURING GEAR EXTENSION RECEIVED LANDING GEAR DISAGREE, LANDING GEAR AIR/GROUND FAIL MESSAGE WITH THREE GREEN LIGHTS. PERFORMED MANUAL GEAR EXTENSION, DECLARED EMERGENCY. PERFORMED CENTRAL MAINTENANCE SYSTEM DOWNLOAD IAW EMB AMM 45-900-00 AND FLIGHT DATA RECORDER DOWNLOAD IAW AMERICAN EAGLE WORKCARD 31-700-05. PERFORMED OPERATIONAL CHECK OF AIR/GROUND SYSTEM IAW AMERICAN EAGLE WORKCARD32-700-16 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT AND PERFORMED OPERATIONAL CHECKS IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,302 hrs · 13,162 cycles

DENT WITH GOUGES FOUND ON LEFT REAR FUSELAGE BETWEEN FRAME 78 AND JUNCTION 7 AND STRINGERS 5L AND 7L. PERFORMED CUTOUT OF DAMAGED AREA. FABRICATED FILLER, REPAIR DOUBLER. INSTALLED REPAIR PIECES AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-32-01. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,302 hrs · 13,162 cycles

FOUND CARGO DOOR FRAME CENTER SILL CORRODED. REMOVED AND REPLACED SILL, CLEANED AND TREATED AREA. RESTORED SURFACE PROTECTIVE FINISH IAW EMB SRM 51-21-04, 51-21-05 AND 51-21-06. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,302 hrs · 13,162 cycles

FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED EXISTING REPAIR. CLEAN AND TREATED AREA. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,302 hrs · 13,162 cycles

SERVICE DOOR FRAME CENTER SILL CORRODED. CLEANED AND TREATED AREA, REMOVED AND REPLACED CENTER SILL IAW EMB SRM 51-20-03, 51-40-02 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE.

Part: SWITCH — FAILED (LT ENGINE)

E-1 REVERSER DISAGREE WARNING ON TAKEOFF. TROUBLESHOT IAW EMB. REPLACED UPPER OB STOW SWITCH IAW EMB AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVIC. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, TWO SHIMS AND DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 28, CHAPTER 53-22-10, FIG 201. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND THE SERVICE DOOR SILL CORRODED. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTERS 51-20-01, 03, 51-40-02, 03, 04, 05, 06 AND 09. (M)

Part: COUPLING — DAMAGED (BLEED AIR SYS) · airframe 8,304 hrs · 8,455 cycles

CREW REPORTED A BLEED 1 LEAK FOLLOWED BY A LOUD BANG FOLLOWED BY A BLEED 2 MESSAGE. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT BLEED COUPLING IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502363) (K)

Part: SWITCH — SHORTED (CAPTAIN'S YOKE) · airframe 8,259 hrs · 8,405 cycles

CREW REPORTED THE CAPTAINS YOKE NEAR EMITTING SMOKE NEAR THE STEERING DISCONNECT SWITCH WHEN AIRCRAFT IS ON GROUND. MAINTENANCE REPLACED THE CAPTAIN AUTOPILOT DISCONNECT SWITCH AND CHART HOLDER. IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW200502010) (K)

Part: SKIN — DAMAGED (FUSELAGE)

AIRCRAFT ARRIVED FOR REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FRAMES 25 AND 26 AND STRINGERS 19 AND 21. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3988, DATED NOVEMBER 25, 2003 AND EMB 145 SRM, SRM EMB 145/1142 REV 24, CHAPTER 53-22-01. (M)

Part: SKIN — CORRODED (FUSELAGE)

ABI - DURING A MBV INSPECTION, TWO DENTS WERE FOND BETWEEN SKIN JUNCTION 07 AND FRAME 77, STRINGER 18R AND 19R. REMOVED BOTH DENTS WITH SINGLE CUTOUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-32-01, TYPE A, FIG 201 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE CENTER FLOORBEAM AT FRAME 20. REMOVED CORRODED AREA BY CUTOUT. FABRICATED AN EXTERNAL U-SHAPED DOUBLER. REPAIR DONE IAW EMB-145 SRM (145/1142, REV 20) 53-21-10 PARA 5 FIG 204 SHEET 2, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE AREA. NO DEFECTS NOTED. FABRICATED AND A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M)