N928AE

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 43,827 hrs · 39,542 cycles

CIELING AT ROW 5 AND MAIN DOOR, ALONG WITH MAIN DOOR EMERGENCY LIGHTS INOP. R & R BATTERY NR 1 IAW AMM 33-50-04.

Part: ACM — ODOR (LEFT) · airframe 43,495 hrs · 39,154 cycles

BRIEFSMOKE/ODOR IN THE COCKPIT IN FLIGHT. F.A. REPORTED A "POP" NOISE NEAR ROW 12. AIR CONDITIONING PACKS. R&R LT ACM EXUAST DUCT ASSY AND GRATE ASSY IRW EMB AMM 21-51-03 OPS CHECK GD WITH NO DEFECTS NOTED CLEAR MEL 21-15-2

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 42,491 hrs · 38,060 cycles

FAINT OIL LIKE ODOR IN FLIGHT DECK WHILE ON ENGINE BLEEDS DURING DESECENT LAST APPROX 30SECS FACT 23FEB25 13:56 PHL E1 1QT LOW. SERVICED E1 WITH 1QT AS REQUIRED. PERFORMED GVI BOTH E1 AND E2. NDN AT THIS TIME. GROUND RAN E1 AND E2 IAW PIEDMONT RUNUP MANUAL. GROUND RAN FOR APPROX 10MIN WITH BOTH BLEEDS ON WITH NO SMELLS NOTED AT THIS TIME. BOTH E1/E2 OIL PRESS AND TEMP STAYED IN GREEN RANGE. OK FOR SERVICE.

Part: NONE — NONE (NONE) · airframe 42,431 hrs · 37,998 cycles

BIRD STRIKE ON LEFT SIDE AIRCRAFT ON TAKE OFF ROLL FACT 09FEB25 04:13 ROA CLEANED AND INSPECTED IAW AMM 05-50-08 NO DEFECTS NOTED

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E046877 FOUND CORROSION ON CENTER HAT BEAM AROUND NUT PLATE HOLE AT FR59. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLER FOR REPAIR OF LAV CENTER HAT BEAM AT NUT-PLATE HOLE AT FR59 IAW ETD2024-145-020349 AND EO1-53-24-0463

Part: DRAG BRACE — CORRODED (NLG) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E046631 NLG DRAG BRACE LH BEARING CAP IS CORRODED. RAR NLG DRAG BRACE LH BEARING CAP IAW EMB 145 AMM 32-20-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,540 hrs · 36,990 cycles

E046425 PAX DOOR CUT-OUT AFT FLOOR BOARD SUPPORT CORRODED AROUND NUTT PLATES. RAR PAX DOOR CUT-OUT AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,540 hrs · 36,990 cycles

E046388 RH #1 OMEGA BEAM FLOOR SUPPORT CORRODED IN MULTIPLE AREAS. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE R/H #1 OMEGA BEAM SUPPORT IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

LH #2 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS BETWEEN FRAMES 24 TO 35. REMOVED AND REPLACED LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,540 hrs · 36,990 cycles

E046384 RH #1 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RH #1 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,540 hrs · 36,990 cycles

RH #2 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS. RAR R/H # 2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E046457 LH #1 FLOOR SILL CORRODED. RAR LH #1 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

LH #3 OMEGA BEAM FLOOR SUPPORT CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED LH #3 OMEGA BEAM FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E046499 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATE HOLES. BLENDED OUT CORROSION ON SERVICE DOOR CUTOUT CENTER SILL AROUND 3 NUT PLATE HOLES IAW EMB145 SRM 51-10-03. REMAINING THICKNESS AT BLENDED AREA ON FWD AND CENTER NUTPLATE HOLES ON SERVICE DOOR CUTOUT CENTER SILL FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-21-02AD, ITEM 3, FIG 102. INSTALLED REPAIR DOUBLER AT AFT NUTPLATE HOLE ON SERVICE DOOR CENTER SILL IAW EMB-145 SRM 53-21-02 RE, ITEM 2, FIGURE 201 AND EO1-53-24-0434.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

LAV LH FLOOR SUPPORT CORRODED BETWEEN FR 59/60. BLENDED TO REMOVE CORROSION ON LAV L/H FLOOR SUPPORT BETWEEN FR59/-60 IAW EMB145 SRM 51-10-03.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

LAV LH CENTER FLOOR GUSSET CORRODED AROUND NUT PLATE HOLES. REMOVED AND REPLACED LAV L/H CENTER FLOOR GUSSET IAW EMB145 SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

LAV CENTER FLOOR GUSSET CORRODED AROUND NUT PLATE HOLES. REMOVED AND REPLACED LAV CENTER FLOOR GUSSET IAW EMB145 SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,450 hrs · 36,990 cycles

CARGO DOOR INTERNAL LWR FRAME L SHAPE ANGLE HAS CORROSION AROUND NUTPLATES HOLES. REMOVED AND REPLACED CARGO DOOR INTERNAL LWR FRAME L SHAPE ANGLE (L-PROFILE) IAW EMB-145 SRM 51-40-02

Part: WEB — CHAFED (ZONE 800) · airframe 41,540 hrs · 36,990 cycles

E045806 CARGO DOOR INTERNAL WEB IS CHAFED IN MULTIPLE AREAS. FURTHER INVESTIGATION OF CARGO DOOR INTERNAL WEB CHAFES IN MULTIPLE AREAS SHOWS TO BE TOTAL OF 2 CHAFED (MARKED) AREAS. BLENDED 2 MARKED CHAFED AREAS IAW EMB 145 SRM 51-10-03. 1 BLENDED AREA FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 52-30-01AD. ACCOMPLISHED REPAIR OF 1 BLEND OUT AT INTERSECTION OF HB3 & VB2 ON CARGO DOOR INTERNAL WEB (LOWER SKIN) IAW PIEDMONT EO1-52-24-0472 AND EMBRAER ETD2024-145-020452.

Part: DOOR FRAME — CHAFED (ZONE 200) · airframe 41,540 hrs · 36,990 cycles

E045844 PAX DOOR AFT FRAME IS CHAFED AROUND NUT-PLATES HOLES. BLENDED TOTAL OF 7 CHAFED AREAS AROUND PAX DOOR AFT FRAME NUT-PLATE HOLES IAW EMB 145 SRM 51-10-03. 6 OF 7 BLENDED AREAS FOUND TO BE WITHIN NON-SIGNIFICANT DAMAGE LIMITS IAW EMB 145 SRM 51-10-05. PERFORMED PERMANENT REPAIR TO 1 OF 7 BLENDED AREAS IAW PIEDMONT EO1-52-24-0442 AND ETD2024-145-019775 REV D

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

CARGO DOOR CUTOUT LOWER SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

PAX DOOR LWR FWD PROFILE HAS CORROSION AROUND NUT-PLATES HOLES. REMOVED PAX DOOR LWR FWD PROFILE THAT IS CORRODED AROUND NUT-PLATES HOLES, PREPPED AND INSTALLED SERVICEABLE PAX DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-02

Part: BEAM — CRACKED (ZONE 200) · airframe 41,540 hrs · 36,990 cycles

E045789 L/H EMERGENCY EXIT DOOR BEAM #3 HAS A POSSIBLE CRACK. PERFORMED DOUBLER REPAIR ON L/H EMERGENCY EXIT DOOR BEAM #3 CRACK IAW ETD2024-145-020373 AND EO1-52-24-0464.

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

PAX DOOR LWR AFT PROFILE HAS CORROSION AROUND NUT-PLATES HOLES. REMOVED PAX DOOR LWR AFT PROFILE WITH CORROSION AROUND NUT-PLATES HOLES, INSTALLED SERVICEABLE PAX DOOR LOWER AFT PROFILE IAW EMB 145 SRM 51-40-02.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E045597 FUSELAGE SKIN INTERNAL DOUBLER BETWEEN FRAME 60 AND FRAME 61 AND STRINGERS 19L AND 20L HAS CORROSION. REMOVED UNSERVICEABLE INTERNAL FUSELAGE SKIN DOUBLER BETWEEN FRAMES 60-61 AND STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02.INSTALLED NEW INTERNAL FUSELAGE SKIN DOUBLER BETWEEN FRAMES 60-61 AND STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,540 hrs · 36,990 cycles

E044964 CENTER FUSELAGE 4, THE POTABLE WATER SERVICING PORT DOUBLER HAS CORROSION. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE CENTER FUSELAGE 4, THE POTABLE WATER SERVICING PORT DOUBLER IAW EMB145 SRM 51-40-02.

Part: LAMP — INOPERATIVE (MAIN) · airframe 41,226 hrs · 36,705 cycles

MAIN DOOR EXT EMERGENCY DOOR LIGHT INOP-C/A-RAR MAIN DOOR EXT EMERGENCY DOOR LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,067 hrs · 36,546 cycles

DURING PS-1 CHECK FOUND INTERIOR EMERGENCY EXIT CEILING LIGHT INOP-C/A-REPLACED LAMP IAW 33-50-08. OPC GOOD.

Part: LAMP — INOPERATIVE (SD) · airframe 40,841 hrs · 36,295 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD

Part: NONE — NONE · corrosion level 2 · airframe 40,753 hrs · 36,195 cycles

AFT CARGO DOOR FRAME 65 GUSSET IS CORRODED.(LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-FRAME 65 REPAIRED IAW ERS-EM-53MR-4660.

Part: FLASHLIGHT ASSY — BROKEN (CABIN) · airframe 40,282 hrs · 35,663 cycles

FA EMERGENCY FLASHLIGHT BRACKET IS BROKEN-C/A-ACCOMPLISHED REPLACEMENT OF FA EMERGENCY FLASHLIGHT BRACKET CLAMP IAW EMB 145 CMM TASK 25-60-14. OPC GOOD NO DEFECTS NOTED.

Part: ACM — FUMES (CABIN) · airframe 40,281 hrs · 35,661 cycles

STRONG SMELL OF FUEL FUMES ON DECENT STARTING AT FL250 THROUGH 14000 FT FOLLOWED BY BURNING SMELL TILL 5000FT-C/A-C/W ETN-72-034R10 NO DEFECTS NOTED. C/W TECH SUPPORT WORKSCOPE DOWNLOADED CMC, INSPECTED UNDER FLOOR NO DEFECTS NOTED TO DUCTING OR RECIRC FANS, NO EVIDENCE OF FUEL FOUND UNDER FLOOR.

Part: INVERTER — INOPERATIVE (FWD) · airframe 40,113 hrs · 35,464 cycles

FWD EMERGENCY EXIT PLACARD INOP-C/A-T/S IAW W/M 33-50-50 FOUND INVERTER 1 AT FAULT. RAR INVERTER 1 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHECK GOOD

Part: LAMP — INOPERATIVE (MAIN) · airframe 40,013 hrs · 35,344 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 39,738 hrs · 35,022 cycles

AISLE EMERGENCY LIGHT AT 16CB INOP-C/A-RAR AISLE EMERGENCY LIGHT LAMP OPC GOOD IAW AMM 33-50-08

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,757 hrs · 33,903 cycles

AFT FLASHLIGHT CRADLE BROKEN-C/A-RAR AFT FLASHLIGHT CRADE IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 38,738 hrs · 33,877 cycles

AFT FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-FLIGHT CREW PLACARDED AFT FA EMERGENCY FLASHLIGHT HOLDER. M PROCEDURES C/W. MEL AUTH# 080225M-C REF# 25-32 MOC# 628765

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 38,675 hrs · 33,811 cycles

MAIN PAX DOOR EMERGENCY EXIT SIGN INOP-C/A-CLEANED MAIN PAX DOOR EMERGENCY EXIT SIGN ELECTRICAL CONNECTORS IAW SWPM 20-50-00 OPS CHECK GOOD

Part: LIGHT — DIM (CABIN) · airframe 38,238 hrs · 33,302 cycles

MEL 33-23 AUTH # 050266-C "FLOOR EMERGENCY LIGHTING STRIP #6 AND STRIP #8 DIM" REF AML PAGE 4761264 ITEM 1.-C/A-RAR FLOOR PROXIMITY STRIP LIGHTS #6 AND #8 REF AMM 33-50-12. OPC GOOD. MEL ITEM RESTORED.

Part: LIGHT — DIM (CABIN) · airframe 38,232 hrs · 33,297 cycles

FLOOR EMERGENCY LIGHTING STRIP #6 AND STRIP #8 DIM-C/A- "TRANSFERRED TO AML PAGE 4761264 ITEM 1"

Part: O-RING — LEAKING (APU BLEED) · airframe 38,232 hrs · 33,295 cycles

BLEED 1 LEAK CLIMBING THROUGH 8000. PERFOMED ARH STILL INDICATED LEAK. LOSS OF CABIN PRSSURE EMERGENCY DECLARED.SWAP A/C CONT -C/A-T/S IAW FIM 36-20-00-810-801-A. FOUND LEAK AT JOINT #21. RAR BLEED AIR O-RING IAW EMB 145 AMM 36-11-10. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: FITTING — GOUGED (AILERON DAMPER) · airframe 37,870 hrs · 32,922 cycles

R/H AILERON DAMPER FITTING IS GOUGED ON THE AILERON.-C/A-COMPLETE RAR R/H AILERON DAMPER FITTING IAW ENVOY EO EM-27MR-112.

Part: HINGE — EXCESS PLAY (VERTICAL STAB) · airframe 37,870 hrs · 32,922 cycles

VERTICAL STABILIZER UPPER RUDDER ATTACH POINT FITTING HAS PLAY. C/A-REPLACE VERTICAL STAB UPPER RUDDER HINGE ASSY IAW EMB145 SRM 51-40-02.

Part: BUSHING — MIGRATED (PCU ATTACH FITT) · airframe 37,870 hrs · 32,922 cycles

LEFT AILERON PCU ATTACH FITTING HAS MIGRATING BUSHINGS ON THE INBD AND OUTBD LUG. C/A-R & R LT AILERON PCA FITTING IAW EO-EM-27MR-112.

Part: BUSHING — MIGRATED (PCU ATTCH FITTIN) · airframe 37,870 hrs · 32,922 cycles

RIGHT AILERON PCU ATTACH FITTING HAS MIGRATING BUSHINGS ON THE INBD AND OUTBD LUG. C/A-R & R RT AILERON PCU ATTACH FITTING IAW EO-EM-27MR-112.

Part: ANGLE — CRACKED (FLOORBEAM) · airframe 37,870 hrs · 32,922 cycles

RIGHT FLOOR SUPPORT ANGLE AT FR 59 IS CRACKED ON OUTBD EDGE. -C/A- INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 37,870 hrs · 32,922 cycles

ONE EA FRAME CLEAT IS CRACKED ON FR 67 BETWEEN STRS 7L AND 8L. C/A-R & R'D 1 EA FRAME CLEAT ON FR 67 BETWEEN STRS 7L AND 8L IAW SRM EMB145 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 37,870 hrs · 32,922 cycles

RIGHT FRAME 73 CLEAT IS CRACKED BETWEEN STR 9R AND STR 10R. REPLACED SHEAR CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 37,870 hrs · 32,922 cycles

1 EA FRAME CLEAT IS CRACKED ON FR 66 BETWEEN STRS 8L AND 9L. (SHOULD HAVE READ 6L AND 7L)-C/A-R & R SHEAR CLIP (FRAME CLEAT) AT FR 66 BETWEEN STGR 6L AND 7L IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 37,870 hrs · 32,922 cycles

ONE EA FRAME CLEAT IS CRACKED ON FR 66 BETWEEN STRS 9L AND 10L. C/A-R & R'D CLEAT IAW SRM 53-31-04.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 37,870 hrs · 32,922 cycles

L/H FRAME 73 CLEAT IS CRACKED BETWEEN STR 9L AND STR 10L.-C/A-RAR SHEAR CLIP AT FR 73 BETWEEN STGR 9L AND 10L IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 37,870 hrs · 32,922 cycles

SERVICE DOOR SILL IS CORRODED AT THE NUT PLATE HOLES. C/A-R & R SVC DOOR CENTER SILL IAW SRM 51-40-02.

Part: PLATE — CORRODED (CARGO DOOR SILL) · airframe 37,870 hrs · 32,922 cycles

AFT CARGO DOOR SILL PLATE IS CORRODED. (LEVEL 1 CORROSION)-C/A-REMOVED AND REPLACED AFT CARGO DOOR SILL PLATE IAW SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 37,870 hrs · 32,922 cycles

FLOOR PROXIMITY STRIP LIGHT HAS BROKEN WIRE AT FLOOR PANEL 251BF.-C/A-COMPLETE:REPLACED MISSING SP9102 IAW SWPM 20-00-03.

Part: LIGHT — CRACKED (CABIN) · airframe 37,870 hrs · 32,922 cycles

NUMEROUS L/H AND R/H FLOOR PATH LIGHTING PROFILES ARE CRACKED/DAMAGED.-C/A-COMPLETE:COMPLETED: RAR NUMEROUS L/H AND R/H FLOOR PATH LIGHTING PROFILES THAT WERE DAMAGED WITH NEW IAW AMM 33-50-12

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,870 hrs · 32,922 cycles

CABIN EMERGENCY FLOOR LIGHT STRIP #3 DOES NOT ILLUMINATE.-C/A-COMPLETE:REMOVED AND REPLACED CABIN EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD

Part: INVERTER — ABNORMAL (EMERGENCY LIGHTS) · airframe 37,753 hrs · 32,799 cycles

FOUND EMERGENCY EXIT SIGN OVER RT WING EXIT INOPERABLE. C/A: R & R NR 5 EMERGENCY LIGHT INVERTER. OPERATIONS CHECK GOOD, IAW EMB 145 AMM 33-50-11.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,618 hrs · 32,640 cycles

RT ESCAPE ROW EMERGENCY LIGHT SIGN INOPERABLE. C/A: RAR EPSU NR 3 BATTERY AND CHARGER. OPERATIONS CHECK GOOD, IAW W/C 33-700-19.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 37,586 hrs · 32,607 cycles

MEL 25-53 AUTH 110375C AFT CABIN EMERGENCY FLASHLIGHT INOPERABLE. C/A: R & R AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY AMM 25-60-00 MEL RESTORED.

Part: LIGHT — INOPERATIVE (RT CABIN) · airframe 37,586 hrs · 32,607 cycles

DURING PS-1 CHECK, FOUND RT EMERGENCY EXIT LIGHT TO BE INOPERABLE. C/A: REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT, IAW AMM 33-50-14. OPERATIONS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 37,584 hrs · 32,606 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOPERABLE. C/A: FLIGHT CREW PLACARDED AFT CABIN EMERGENCY FLASHLIGHT. MEL: 25-53AUTH: 110375-C MOC: 730088.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITCH TRIM) · airframe 37,289 hrs · 32,296 cycles

PTRIM BACKUP INOPERABLE WARNING MESSAGE ON EICAS ON APROACH. C/A CYCLED PTRIM 1 & 2 BREAKERS AND FOUND BACKUP SYSTEM CUTOUT BUTTON ACTUATED. DE-SELECTED BUTTON AND TRIM SYSTEM, NOW OPERATIONS CHECKS GOOD IAW EMB145 AMM 27-40-00.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,230 hrs · 32,232 cycles

EMERGENCY EXIT SIGN PAX DOOR INOP. R & R EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-14 OPS CHECK GOOD IAW EMB 145 AMM 33-50-00

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,815 hrs · 31,783 cycles

AFT CEILING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED AFT CEILING EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD

Part: INVERTER — FAILED (CABIN) · airframe 36,815 hrs · 31,783 cycles

EMERGENCY EXIT SIGN AT SEAT 3BC INOP-C/A-T/S ,REPLACEDAND REMOVED EXIT IDENTIFYER SIGN IAW EMB AMM 33-50-13-000-801-A ZND 33-50-13-400-801-A, NO FIX. REMOVED AND REPLACED # 2 EMERGENCY BATTERY IAW EMB AMM 33-50-04-000-801-A ND 33-50-04-400-801-A, NO FIX. RAR #3 INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 80160

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,836 hrs · 30,908 cycles

DURING PS-1 CHECK, FOUND PASSENGER DOOR EMERGENCY EXIT LIGHTED SIGN INOP-C/A-REMOVED AND REPLACED EMERGENCY EXIT LIGHTED SIGN IAW AMM 33-50-14. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: PANEL — INOPERATIVE (CABIN) · airframe 35,560 hrs · 30,668 cycles

FOUND GALLEY WALL EMERGENCY EXIT PANEL INOP DURING PS1 CHECK. C/A-RAR GALLEY WALL EMERGENCY PANEL EXIT LIGHT IAW AMM 33-50-14. OPS CHECK GOOD.

Part: CRADLE — INOPERATIVE (FWD FLASHLIGHT) · airframe 35,167 hrs · 30,356 cycles

FWD FA FLASHLIGHT INOPERATIVE, FOUND CHARGER TO BE INOPERATIVE. R & R FWD FA FLAHSLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: BRAKE — FAILED (MLG) · airframe 34,615 hrs · 29,887 cycles

NR 4 BRAKE FAILS CARBON INSPECTION. C/A-REMOVED AND REPLACED NR 4 MLG BRAKE IAW W/C 32-600-14 OPS CHECK GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 34,581 hrs · 29,849 cycles

SMOKE IN COCKPIT COMING FROM AIR VENTS LEVEL CRUISE FL 230 FA REPORTED LOUD GRINDING NOISE FROM UNDER WING AREA AROUND SAME TIME AS SMOKE EVENT. C/A-INSPECTED FOUND NUM 1 PACK ACM DAMAGED FAILURE. PERFORMED ETN-EM-72-034 COULDNT DUPLICATE SMOKE IN COCKPIT WHILE RUNNING PACK 2. REATTACHED DUCT IAW ETN-EM-21-056 CLOSED AND SECURED PANEL. FOUND ACM SEIZED REMOVED AND REPLACED IAW AMM 21-51-03 PERFORMED OPS CHECK IAW AMM 21-51-00-700-802-A OPS CHECK GOOD. FOUND DUAL TEMP CONTROL VLV TO HEAT EXCHANGER DUCT DAMAGED. REMOVED AND REPLACED DUAL TEMP CTRL VLV TO HEAT EXCHANGER DUCT IAW AMM 21-60-01 AND REMOVED AND REPLACED COUPLINGS AND CLAMPS IAW ETN-EM-21-056.OPC AND LEAK CHECK GOOD IAW AMM 21-51-00 MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,133 hrs · 29,332 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD.

Part: PROBE — FAILED (FUEL TANK) · airframe 34,052 hrs · 29,249 cycles

LH FUEL QTY AMBER DASHES ON MFD. PRESSURE REFUEL INOP. COULD NOT DUPLICATE FAULT. PERFORMED MFD FUEL QUANTITY OPC IAW AMM 28-41-00. OPC GOOD. TRANSFERRED 1000LBS OF FUEL TO EACH WING IAW AMM 28-10-00 TO ENSURE CORRECT INDICATIONS ARE SHOWN ON MFD AND REPEATER PANEL. PERFORMED TEST OF REPEATER PANEL IAW AMM 28-23-08. NO FAULT MSG'S SHOWN. REMOVED AND REPLACED TANK UNIT #3 IAW AMM 28-41-02 OPS CHECK GOOD . PERFORMED RESSURE REFUING IAW AMM 12-11-01 OPS CHECK GOOD FUEL QUANTITY INDICATION CHECKS GOOD.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 33,186 hrs · 28,406 cycles

SERVICE DOOR CUTOUT REINFORCEMENT STRUCTURE HAS CORROSION ON THE AFT SIDE AROUND THE LOWER NUTPLATE HOLE. ACCOMPLISHED REPAIR TO FRAME 22 SERVICE DOOR CUTOUT IAW ERS-EM-53MR-3396 R1.

Part: SKIN — DENTED (CARGO DOOR) · airframe 33,186 hrs · 28,406 cycles

CARGO DOOR EXTERNAL SKIN SCRATCHED AND DENTED APPROX 16" FROM UPPER EDGE AND 14" FROM THE AFT EDGE. ACCOMPLISHED PERMANENT REPAIR TO CARGO DOOR SKIN IAW ERS-EM-52MR-897.

Part: CONNECTOR — BROKEN (CABIN) · airframe 33,186 hrs · 28,406 cycles

NR 5 EMERGENCY LIGHT STRIP CONNECTOR ON A/C BROKEN (FOUND ON OPEN). REMOVED AND REPLACED #5 EMERGENCY LIGHT STRIP CONNECTOR ON A/C IAW SWPM 20-00-03.

Part: WIRE — BROKEN (CABIN) · airframe 33,186 hrs · 28,406 cycles

NR 7 EMERGENCY LIGHT STRIP HAS BROKEN WIRE (FOUND ON OPEN). REMOVED AND REPLACED NR 7 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 33,186 hrs · 28,406 cycles

NR 6 EMERGENCY LIGHT STRIP HAS BROKEN WIRE (FOUND ON OPEN). REMOVED AND REPLACED NR 6 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 33,186 hrs · 28,406 cycles

NR 4 EMERGENCY LIGHT STRIP HAS BROKEN WIRE (FOUND ON OPEN). REMOVED AND REPLACED NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 33,186 hrs · 28,406 cycles

LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD NOSE RIB HAS POSSIBLE CRACKS IN 2 LOCATIONS. REMOVED AND REPLACED LT ELEVATOR INBD HINGE CUTOUT INBD NOSE RIB IAW SRM 51-40-02, 51-20-03 AND ETN-EM-55-073 R2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,186 hrs · 28,406 cycles

RT OMEGA BEAM PREVIOUSLY BLENDED AREA HAS CORROSION AT FRAME 24. INSTALLED DOUBLER REPAIR ON RT OMEGA BEAM AT FRAME 24 AREA IAW SRM 53-22-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,186 hrs · 28,406 cycles

53-20-11, SERVICE DOOR CENTER SILL CORRODED. REMOVED AND INSTALLED NEW SERVICE DOOR CENTER SILL IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 33,186 hrs · 28,406 cycles

SERVICE DOOR HAS CORROSION AROUND THE LOWER FWD AND AFT NUTPLATE HOLES. -ACCOMPLISHED PERMANENT REPAIR TO SERVICE DOOR LOWER NUTPLATE HOLES IAW ERS-EM-52MR-898.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,186 hrs · 28,406 cycles

LT OMEGA BEAM CORRODED AT CROSS BEAM BETWEEN FR-58 AND FR-59. ACCOMPLISHED REPAIR OF LT OMEGA BEAM BETWEEN FR58 AND 59 IAW EO EM-53MR-1518R3 PART A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,186 hrs · 28,406 cycles

EMERGENCY EXIT LIGHT ON BOTTOM OF GALLEY SERVICE DOOR INOP. PERFORMED OCK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,610 hrs · 27,915 cycles

EMERGENCY EXIT SIGN ON THE AFT GALLEY WALL WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14-000-801-A, AND 33-50-14-400-801-A. OPS CHECKED GOOD.

Part: DOOR SEAL — DAMAGED (CABIN DOOR) · airframe 30,963 hrs · 26,347 cycles

LOUD WHISTLING SOUND COMING FROM MAIN CABIN DOOR IN CRUISE. REPAIRED SEAL UPPER FILLER SEAL IAW AMM 56-00-01.

Part: CLAMP — LOOSE (EXHAUST DUCT) · airframe 30,701 hrs · 26,068 cycles

WING ANTI ICE FAIL CAUTION IN FLIGHT DURING ANTI ICE TEST, CLIMBING TO ALTITUDE. TIGHTENED LOOSE CLAMP ON EXHAUST DUCT OPS CHECKED GOOD IAW 30-00-00-700-802A

Part: UNKNOWN — ODOR (CABIN) · airframe 30,245 hrs · 25,653 cycles

BURNING ODOR DURING FLIGHT THRU TURBULENCE. DISSIPATED AFTER APPROXIMATELY 1 MINUTE. COMPLETED ALL ITEM IAW ETN-EM-72-034. NO DISCREPANCY NOTED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,216 hrs · 25,628 cycles

DURING TAKE OFF ROLL AT 100 KTS GOT TAKE OFF CONFIG WARNING AND TRIM ABORTED TAKE OFF. PERFORMED OPS CHECK IAW AMM 22-11-00-05 OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,251 hrs · 24,777 cycles

AISLE EMERGENCY LIGHT NR 2, FAILED TO ILLUMINATE. R & R THE LAMP IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: FRAME — BENT (FUSELAGE) · airframe 28,952 hrs · 24,512 cycles

FRAME 72 IS BENT BETWEEN STR 16L-15L. REPAIRED FRAME 72 BETWEEN STR 16L AND 15L IAW ERS-EM-53MR-2256.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,952 hrs · 24,512 cycles

RIGHT OTBD OMEGA BEAM CRACKED AROUND NUTPLATE HOLE. REPAIRED RT OTBD OMEGA BEAM IAW ERS-EM-53MR-2254.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,932 hrs · 24,497 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 13 AND 14 STR 21L AND 20L. REPAIRED INTERNAL FUSELAGE SKIN BETWEEN FRAMES 13 AND 14, STR 21L AND 20L BY INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-75-01,53-21-01, CPM 51-21-05,51-21-06 AND ETN-GN-51-011, ETN-EM-51-075, ETN-EM-51-091, ETN-GN-51-120.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,932 hrs · 24,497 cycles

RIGHT UPPER AFT FUSELAGE SKIN CRACKED ABOVE STR 2R AND AFT OF FRAME 75. REPAIRED RT AFT FUSELAGE SKIN AFT OF FRAME 75 ABOVE STR 2R IAW SRM 53-31-01, ITM 11, FIG 219.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 28,687 hrs · 24,281 cycles

UPON ENTERING AIRCRAFT, AN ELECTRICAL SMOKE ODOR WAS PREVALENT NEAR THE FWD CLOSET, SEAT 1A. APU WAS RUNNING, PACKS ON, GPU WAS DESCONECTED. REMOVED AND REPLACED AND OPS CHECKED GOOD CABIN LIGHTS CONTROL MODULE IAW AMMS 33-21-01 AND 25-26-03.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,437 hrs · 24,045 cycles

LAST THREE FLOOR PROXIMITY STRIPS INOPERATIVE. R & R NR 6 ELS INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: SENSOR — DIRTY (SMOKE DETECTOR) · airframe 27,319 hrs · 23,045 cycles

LAVATORY SMOKE EICAS MSG, NO INDICATION OR SMOKE OR FIRE. TROUBLE SHOT LAVATORY SMOKE MSG IAW FIM TASK 26-14-00-810-802. CLEANED SMOKE DETECTOR SENSOR IAW AMM 26-14-01. OPERATIONS CHECKED GOOD IAW AMM 26-14-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,163 hrs · 22,896 cycles

SEVERAL FWD EMER LIGHT, FLOOR STRIP LIGHTS INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 14895.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,548 hrs · 22,318 cycles

GALLEY EMERGENCY LIGHT INOPERATIVE. R & R GALLEY EMERGENCY LAMP IAW AMM 33-50-09-000-801 33-50-09-400-801. NO FIX FOUND, CONNECTOR DISCONNECTED. RECONNECTED IAW AMM 33-50-09-000-802 33-50-09-400-802. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,510 hrs · 22,292 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASH LIGHT IAW AMM 25-60-01. OPERATIONS CHECKED GOOD.

Part: CONTACT — OUT OF ADJUST (FLASHLIGHT) · airframe 26,177 hrs · 22,008 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. ADJUSTED LIGHT CONTACT INSIDE FLASH LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW 33-51-01 AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,068 hrs · 21,929 cycles

EMERGENCY EXIT SIGN IFO SEAT 3CB INOPERATIVE. R & R BATTERY CHARGER ABOVE SERVICE DOOR. OPERATIONS CHECKED GOOD IAW 33-50-14.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,380 hrs · 20,566 cycles

FLOOR PROXIMITY LIGHT WIRE LT NR 7 MISSING CONNECTOR. REPAIRED FLOOR PROXIMITY LIGHT WIRE LT NR 7 IAW SWPM 20-21-00. FOUND DURING ACFT OPEN UP.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,380 hrs · 20,566 cycles

LEFT NR 5 FLOOR PROXIMITY LIGHT STRIP DAMAGED. REPLACED IAW AMM 33-50-12 FOUND DURING OPEN UP.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,380 hrs · 20,566 cycles

FLOOR PROXIMITY LIGHT WIRE LT NR 1 MISSING CONNECTOR. REPAIRED FLOOR PROXIMITY LIGHT WIRE IAW SWPM 20-21-00 FOUND DURING ACFT OPEN UP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,380 hrs · 20,566 cycles

LEFT UPPER FUSELAGE SKIN HAS A SMALL CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, APPROX 3/8 INCHES IN LENGTH. PERFORMED PERMANENT REPAIR OF LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 ABOVE & STRINGER 2L IAW ERS-EM-53MR-727.

Part: SKIN — GOUGED (PAX DOOR) · airframe 24,380 hrs · 20,566 cycles

PASSENGER DOOR SKIN GOUGED AFT LOWER EDGE. REPAIRED IAW ERS-EM-5200-203. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,380 hrs · 20,566 cycles

LAVATORY RT BEAM GUSSET HAS CORROSION SPOTS. COMPLIED WITH ERS-EM-5300-713 LAVATORY RT CORROSION REPAIR.

Part: PROFILE — CRACKED (LT WING) · airframe 24,380 hrs · 20,566 cycles

PERFORM PERMANENT REPAIR ON 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART C. REMOVED DAMAGED LT WW PROFILE & INSTALLED SERVICEABLE PROFILE AT LT AFT WING STUB IAW ERS ERS-EM-57DF-082 PART C.

Part: STRUCTURE — CRACKED (E&E BAY) · airframe 24,380 hrs · 20,566 cycles

FORWARD AVIONICS BAY FLOOR CRACKED AT RT END OF NLG UPLOCK BOX AFT CROSS MEMBER. REPAIRED FWD AVIONICS BAY FLOOR AT RT END OF NLG UPLOCK BOX AFT CROSS MEMBER IAW ERS-EM-5300-718.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,380 hrs · 20,566 cycles

RIGHT HAT BEAM SUPPORT CRACKED OVER THE WING BOX BETWEEN FRAME 47 & 48. R & R RT HAT BEAM SUPPORT OVER THE WING BOX IAW SRM 53-23-02.

Part: STRUCTURE — CRACKED (LT WING) · airframe 24,380 hrs · 20,566 cycles

PERFORM REPETITIVE INSPECTION ON 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART B. ACCOMPLISHED PERMANENT REPAIR OF 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART C. REFER TO NRTC E403463 FOR DETAILS. TDMI 928T5714 RESTORED. REPETITIVE INSPECTION IAW ERS-EM-57DF-082 PART B NO LONGER REQUIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,380 hrs · 20,566 cycles

LEFT UPPER FUSELAGE SKIN HAS SMALL CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L APPROX 3/8 INCH IN LENGTH. EASI 6581 USED. FREQ=400, LPF =100, V GAIN=74, H GAIN=63. REPAIRED IAW ERS-EM-53MR-727. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: CHECK VALVE — FAILED (BRAKE SYSTEM) · airframe 24,380 hrs · 20,566 cycles

EMERGENCY LINE CHECK VLV OF THE EMER PARKING BRAKE SYS FAILS OPERATIONS CHECK. R & R EMER LINE CHECK VLV OF THE EMER PARKING BRAKE SYS IAW AMM 32-44-08. LEAK CHECKED GOOD. TORQUE WRENCH 4484.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,380 hrs · 20,566 cycles

LAVATORY CTR BEAM GUSSET HAS CORROSION. COMPLIED WITH ERS-EM-5300-713 LT CTR BEAM GUSSET CORROSION REPAIR.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 24,380 hrs · 20,566 cycles

FORWARD CARGO DOOR LIFTING MECHANISM SUPPORT BRACKET IS CRACKED. R & R FWD CARGO DOOR LIFTING LOWERING MECHANISM SUPPORT BRACKET IAW SRM 51-40-02 & IAW INFORMATION CONTAINED IN EO-GN-5100-003 R6 & ETN -EM-51-091 R3 SEE TURNOVER FOR DETAILS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,392 hrs · 19,704 cycles

CABIN CEILING DIRECTION EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER, OPERATIONS CHECKED GOOD IAW AEWC 33-700-19 CC 678051.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,361 hrs · 19,679 cycles

AFT NR 4 EMERGENCY LIGHT INOPERATIVE. R & R NR 4 BATTERY & CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,361 hrs · 19,679 cycles

7A AISLE EMERGENCY LIGHT CEILING INOPERATIVE. R & R 7A CEILING AISLE EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPERATIONS CHECKED GOOD IAW 33-50-00.

Part: LINE — LOOSE (ANTI-ICE SYSTEM) · airframe 22,679 hrs · 19,129 cycles

ON INFLIGHT ICE PNEUMATIC TEST WARNING. ANTI-ICE FAIL CAME ON AROUND 20 SECS & STAYED ON ENTIRE FLIGHT, 18,000 FT TAT 3. AIRFOIL LINE TO DAMPER LOOSE ON RT SIDE WING ANTI-ICE SYS, SECURED LINE, OPERATIONS CHECKED GOOD IAW AMM 30-10-00.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,854 hrs · 18,462 cycles

EMERGENCY LIGHTS ON REAR HALF OF ACFT REMAIN ON AFTER POWER DOWN. COMPLIED WITH EMERGENCY LIGHT SYSTEM RESET. OPS CHECK OF EMERGENCY LIGHT SYSTEM PASSED IAW AMM 33-50-00-700-801-A.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 21,015 hrs · 17,763 cycles

NR 1 ENGINE SHOWING 8 QTS OF OIL IN FLIGHT. NOTICED A STRONG OIL ODOR ON DECENT. ACFT REMOVED FROM SERVICE. INSPECTED NR 1 ENGINE AND IT SHOWED SIGNS OF AN OIL LEAK. REMOVED AND REPLACED CARBON SEAL ASSEMBLY IAW AMM 72-25-25. NO LEAKS OR ODORS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,404 hrs · 17,287 cycles

ON FLIGHT 2860 THE CREW REPORTED WITH NR 1 PACK ON ONLY THEY DETECTED A SMELL ON THE FLIGHT DECK. NO SMELLS IN CABIN. SMELL DETECTED THOUGHOUT THE FLIGHT. COMPLIED WITH EMB FIM TASK 21-20-00 AND ETN EM-72-034. FOUND NR 1 PACK TO HAVE A SMELL IN HOT MODE. RAN LEFT PACK FOR 4 HOURS ON HOT WITH APU PNEUMATICS AND LEFT ENGINE ODOR DISSIPATED AFTER 1 HOUR AND DID NOT RETURN. RAN LEFT PACK IAW EMB MM 21-00-00. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,397 hrs · 17,279 cycles

ON FLIGHT 3424 THE CREW REPORTED AFTER POWERING DOWN AIRCRAFT IN CORRECT SEQUENCE THE AFT PORTION OF THE CABIN EMERGENCY LIGHTS REMAINED ON AND EXTERIOR LIGHTS REMAINED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT REMOVED AND REPLACED BATTERY PACK AND BATTERY POWER SUPPLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB MM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,360 hrs · 17,241 cycles

FOR FLIGHT 3226 THE CREW REPORTED THAT AFTER SHUTTING DOWN THE AIRCRAFT THE AFT CABIN EMERGENCY LIGHTS REMAIN ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS GOOD IAW EMB145 AMM 33-50-00. RESET AND FOUND THE RIGHT EXT LIGHT INOPERABLE. REPLACED BULB AT RIGHT EXIT CENTER FAIRING LIGHT IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAULTY (AC BAY) · airframe 20,045 hrs · 16,980 cycles

ON FLIGHT 2977 THE CREW REPORTED AN OCCASIONAL STRONG OIL SMELL APPARENT IN THE COCKPIT AND GALLEY AREA AND OCCURS AT RANDOM TIMES AND DOES NOT SEEM ASSOCIATED WITH ANT PARTICULAR THRUST OR BLEED SETTINGS. THE PILOT STATED HE BELIEVES THE SMELL TO BE COMING FROM NUMBER 1 ENGINE WHEN ANTI-ICING IS ON. REMOVED AND REPLACED THE NR 1 ACM IAW AMM 21-51-03. GROUND RUNS OPS CHECK GOOD IAW ETN# EM-72-034. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN)

MAIN DOOR EMERGENCY LIGHT INTERMITTENT. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 19,750 hrs · 16,749 cycles

ON FLIGHT 3339 THE CREW REPORTED THE FLAPS FAILED AT 22 DEGREES WOULD NOT RETRACT. RECEIVED AN "FLAP FAIL" MESSAGE ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD; FLAP JAMMING MSG ON CMC. COMPLIED WITH STEPS 1, 2 & 10 OF FIM 27-51-00-810-808-A. PERFORMED OPERATIONAL CHECK OF FLAP CONTROL SYSTEM AND FOUND WORKING PROPERLY IAW AMM 27-51-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,728 hrs · 16,730 cycles

DURING B INSPECTION FOUND THE GALLEY AFT DIAMOND GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY AFT DIAMOND GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,728 hrs · 16,730 cycles

DURING B INSPECTION FOUND THE LAV RIGHT FLOOR SILL CORRODED JUST FORWARD OF THE CARBON BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV RIGHT FLOOR SILL JUST FORWARD OF THE CARBON BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,728 hrs · 16,730 cycles

DURING B INSPECTION FOUND THE CARGO DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 19,728 hrs · 16,730 cycles

RT BEAM IN GALLEY AREA HAS CORROSION AT FR 23. REPAIRED BEAM IAW EO EM-53MR-2035.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,728 hrs · 16,730 cycles

DURING B INSPECTION FOUND THE LEFT NR 1 FLOOR SILL CORRODED BETWEEN FRAMES 19-20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 FLOOR SILL IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 19,728 hrs · 16,730 cycles

CARGO DOOR CUTOUT FRAME 65 LATERAL "L" SHAPE CORRODED JUST ABOVE THE CENTER SILL. REPAIRED CARGO DOOR CUTOUT FRAME 65 "L" SHAPE (SHEAR CLIP) ABOVE CENTER SILL WITH ACCOMPLISHMENT OF AEA EO EM-53MR-1129 PART A

Part: HOLDER — LOOSE (COCKPIT) · airframe 3,502 hrs · 15,703 cycles

FOR FLIGHT 3502 ON POST FLIGHT INSPECTION THE CREW FOUND THE CAPTAIN’S FLASHLIGHT HOLDER LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,020 hrs · 15,397 cycles

DURING B-INSPECTION FOUND THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW EMB AMM 33-50-07 IAW EMB AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 17,898 hrs · 15,313 cycles

ON FLIGHT 4146 THE FIRST OFFICER AND THE FLIGHT ATTENDANT REPORTED SMOKE FUMES IN COCKPIT. THE DURATION OF THE ODOR LASTED 30 SECONDS. REPORTED IT SMELLED LIKE RUBBER & ELECTRICAL FUMES. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW EMB 145 FIM TASK 21-20-00-810-801-A, BLOCK 1 TO 26, THROUGH BLOCK 33. NO FAULTS FOUND. ODOR WAS ONLY IN THE COCKPIT. AIR CONDITIONING SYSTEM WAS NOT OPERATING AT TIME OF ODOR. THERE WAS NO FURTHER ODOR OR INDICATIONS OF SMOKE DURING TROUBLESHOOTING. NO FAULTS FOUND AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (EXTERIOR) · airframe 17,663 hrs · 15,131 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR EXTERNAL EMERGENCY LIGHT INTERMITTANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A/33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,485 hrs · 15,003 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY AND BATTERY ASSMEBLY IAW EMB 145 AMM 33-50-04 PERFORMED OPERATIONAL CHECK IAW WORKCARD 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — MISSING (GROUND CONNECT) · airframe 17,237 hrs · 14,806 cycles

ON FLIGHT 4110 THE CREW REPORTED THAT AFTER TAKEOFF THE AIRCRAFT WAS UNABLE TO PRESSURIZE PROPERLY. THE CREW FOLLOWED AOM VOL 1 PROCEDURES AND KEPT CABIN ALT BELOW 10,000 AT ALL TIMES. AOM VOL 1 PROCEDURES DID NOT SOLVE SITUATION I.E. RETURN SITUATION TO NORMAL. THE CREW ELECTED TO DIVERT TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE GROUND CONNECT VALVE MISSING. REPLACED GROUND CONNECT VALVE IAW EMB 145 AMM 21-22-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (SPOILER) · airframe 17,228 hrs · 14,799 cycles

ON FLIGHT 3519 THE CREW REPORTED THE FLIGHT SPOILER DID NOT EXTEND WITH SPEED BRAKE LEVER SELECTED WHEN DESCENDING THROUGH 5,000 FT. NO CAUTION OR ADVISORY MESSAGES. ON LANDING ROLL "SPOILER FAIL" CAUTION. CIRCUIT BREAKER F13 "SPEED BRAKE" POPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW 27-63-02 AND GROUND SPOILER VALVE IAW 27-62-03. PERFORMED SEVERAL OPERATIONAL CHECKS OF THE SPOILERS IAW EMB AMM 27-63-01. THE OPERATIONAL CHECKS WERE GOOD. THE CIRCUIT BREAKER NEVER POPPED DURING TEST OF SPOILERS. THE OPERATIONAL CHECK WAS GOOD NOT DEFECT NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,170 hrs · 14,759 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVER WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,635 hrs · 14,333 cycles

MTX FOUND EMERGENCY LIGHTS CONTROLLED BY EMERGENCY POWER. BATTERY SUPPLY NR 2 INOP. REMOVED AND REPLACED EMERGENCY BATTERY SUPPLY CHARGER AND BATTERY NR 2.

Part: LEVER — INOPERATIVE (MLG MODULE) · airframe 14,820 hrs · 12,997 cycles

ON FLIGHT 3323 THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR IN THE UP POSTION DID NOT RETRACT. NO EICAS MESSAGE WAS NOTED, AND THE GEAR INDICATED THREE GREEN THE WHOLE TIME. THE CREW ELECTED TO RETURN TO DFW. THE CREW SELECTED THE GEAR HANDLE TO THE DOWN POSITION FOR LANDING, STILL NO ABNROMAL INDICATIONS. NO LIMITATION EXCEEDED AND NORMAL LANDING BELOW MAX LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. VERIFIED FAULT WITH GEAR HANDLE UP, NO MOVEMENT NO FAULTS. REMOVED AND REPLACED GEAR CONTROL LEVER IAW AMM II CH 32-32-02. LANDING EXTENSION AND RETRACTION SYSTEM OPERATIONAL CHECK OK IAW AMM II 32-32-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (CABIN DOOR) · corrosion level 2 · airframe 14,778 hrs · 12,969 cycles

DURING MAINTENANCE BASE VISIT FOUND CORROSION ON LOWER INNER SURFACE OF MAIN CABIN DOOR, AROUND FOUR NUT PLATE HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CORROSION ON LOWER INNER SURFACE OF MAIN DOOR AROUND FOUR NUT PLATE HOLES IAW EO EM-52MR-275. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — CRACKED (E&E BAY) · airframe 14,778 hrs · 12,969 cycles

DURING MAINTENANCE BASE VISIT FOUND THE REAR ELECTRONICS DOOR CRACKED UNDER HINGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED REAR ELECTRONICS DOOR IAW EO EM-53MR274. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 13,893 hrs · 12,290 cycles

ON FLIGHT 2829 SMOKE BEGAN TO FILL THE COCKPIT AND CABIN WHEN THROTTLES WERE SET FOR TAKEOFF. THE SMOKE STOPPED AFTER THROTTLES BROUGHT TO IDLE DURING ABORTED TAKEOFF. ENGINE BLEEDS AND PACKS WERE OPEN WHILE AUXILIARY POWER UNIT WAS OFF DURING THE SMOKE. THE ODOR WAS SIMILAR TO COMPRESSOR WASH. THE FLIGHT ATTENDANT DESCRIBED THE ODOR AS BURNING PLASTIC. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED LEFT ENGINE S/N 312812 AND INSTALLED ENGINE S/N CAE31388 IAW ENGINE REMOVAL AND INSTALLATION WORK CARD 71-00-00. THE LEAK CHECK AND OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. THE CAUSE OF THE SMOKE WAS DETERMINED TO BE FROM THE NR 4 CABON SEAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,479 hrs · 11,175 cycles

DURING MAINTENANCE WHILE THE CLEANERS WERE ON THE AIRCRAFT OVERNIGHT THE EMERGENCY LIGHTS AT THE EMERGENCY EXIT DOORS OVERWING CAME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY PACK ON BATTERY POWER SUPPLY NR 3 THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-04 AND 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DIRTY (AVIONICS MASTER) · airframe 9,148 hrs · 8,019 cycles

ON FLIGHT 3830 DURING CRUISE CREW REPORTED, LOST VARIOUS INSTRUMENTS AND BOTH TRANSPONDERS. ADVISED ATC THEY WERE RVSM UNABLE AND STOPPED CLIMB AT FL260. CONTACTED MAINTENANCE AND COULD NOT RESOLVE PROBLEM. AFTER ABOUT 20 MINUTES DISCOVERED AVIONICS MASTER NR 1 HAD RELEASED HALF WAY OUT WITH NO INDICATION SUCH AS THE SWITCH ILLUMINATING. RESETTING THE SWITCH RESTORED ALL INSTRUMENTS. AIRCRART REMOVED FROM SERVICE. CLEANED SWITCH AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLAPPER VALVE — LEAKING (LT WING)

ON FLIGHT 9808 CREW REPORTED AN ABORTED TAKE OFF FOR LT WING FUEL LEAKING FROM WING VENT. C/A R&R LT OUTBOARD FLAP VALVE. LEAK CHECK GOOD IAW AMM 28-11-04. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

ON FLIGHT 3567 - CREW REPORTED ALL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL EMERGENCY BATTERIES IAW EMB AMM 33-50-04 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 7,073 hrs · 6,378 cycles

ON FLIGHT 3509 CREW REPORTED YAW DAMPER FAIL AND AUTO PILOT KICKED OFF DURING CLIMB FOLLOWED BY RUDDER SYSTEM 1/2 INOP EICAS MESSAGE. CREW ELECTED TO RETURN TO DFW FOR MAINTENANCE DECLARED EMERGENCY PRIOR TO LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RUDDER NR 2 PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM, J2 AMM 27-23-00. OPERATIONAL CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 7,076 hrs · 6,382 cycles

ON FLIGHT 3821 CREW REPORTED A ABORTED TAKE-OFF DUE TO STRONG SMOKE ODOR IN THE COCKPIT. NO VISIBLE SMOKE OBSERVED. DFW MTX CONFIRMED WAS OIL ODOR IN COCKPIT. NO ODOR IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT ENGINE IAW WC 71-000-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 7,050 hrs · 6,335 cycles

ON FLIGHT 3686 - CREW REPORTED AUTOPILOT DISENGAGED WITH RUDDER 1-2 INOP EICAS MESSAGE.AFTER A FEW SECONDS, THE MESSAGE DISAPPEARED. THE CREW RE-ENGAGED THE AUTOPILOT AND THE MESSAGE RETURNED. THE CREW FOLLOWED THE PROCEDURE IN THE AOM AND THE RUDDER SYSTEM 2 WAS TURNED OFF. THE DECISION WAS MADE TO DECLARE AN EMERGENCY. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT AND LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. PRESSURIZE HYDRAULIC SYSTEM IAW EMB-145 AMM 29-10-00. NO RUDDER SYS EICAS MSG SHOWN, FOLLOWED FIM 27-23-00-810-802 A, CONNECTED PITO/STATIC SYS TEST TO SIMULATE AIR SPEED TO 140 KNOTS IAW EMB-145 AMM 34-13-00 RUDDER SYS 2 INOP EICAS MESSAGE NOT SHOWN ON EICAS, CAN NOT DUPLICATE AT THIS TIME, AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER SYS) · airframe 5,384 hrs · 4,826 cycles

APORTED TAKEOFF RUDDER SYSTEM 1 INOP MESSAGE. PERFORMED OPERATIONAL CHECKS OF THE RUDDER SYSTEM IAW EMB MM. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: SEAL — LOOSE (COCKPIT WINDOW) · airframe 52,109 hrs · 4,706 cycles

HEARD NOISE FROM CAPTAIN'S DV WINDOW AND SEAL COMING OFF WINDOW ON CLIMBOUT, RETURNED TO JAN. REPAIRED CAPTAIN'S DV WINDOW SEAL IAW EMB AMM. PRESSURE CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 4,890 hrs · 4,447 cycles

DENT FOUND IN FUSELAGE SKIN AFT OF FRAME 26 AND BETWEEN STRINGERS 20R AND 21R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 53-22-01. AIRCRAFT RETURNED TO SERVICE.

Part: GYRO — FAILED (E/E COMPT)

CLT/HKY - FLT 5092 - ON APPROACH TO HKY, THE PILOT'S ARTIFICIAL HORIZON WENT BLANK. DUE TO HEAVY RAIN, PILOT HAD TO ABORT APPROACH TO HKY. AIRCRAFT RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 DG. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: PROP BLADE — LOOSE (RT ENGINE)

CLT - FLT 5172 - ON FLIGHT FROM CLT TO NTS, AIRCREW REPORTED A SEVERE VIBRATION AFTER TAKEOFF. AIRCRAFT RETURNED TO CLT. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND ONE OF THE BLADES, IN THE RIGHT PROP, HAD SLIPPED IN THE HUB. RT PROPELLER REMOVED AND REPLACED. ENGINE RUN, RIGGED, LEAK AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES: 11,367. (X)

Part: ENGINE — FLAMED OUT (RIGHT)

LEX - FLT 5167 - ON FLT FROM LEX TO CLT, AT LEX, THE AIRPORT AUTHORITY WAS BLOWING AND SCRAPPING DOWN RUNWAYS/TAXI AND RAMP AREA. THERE WAS 12 INCHES OF ACCUMULATED SNOW AND SNOW BANKS, FROM 12 INCHES TO 4 FEET. AIRCREW BOARDED PASSENGERS AND GOT DE-ICED. THE AIRCRAFT THEN PROCEEDED TO FOLLOW A SNOW PLOW TO HELP CLEAR THE WAY TO THE TAXI WAY. THE RIGHT ENGINE FLAMED OUT. AIRCRAFT WENT BACK TO RAMP. AIRCREW MADE A GROUND ENGINE RUN, WITH NO PROBLEMS NOTED. THE AIRCRAFT THEN HAD A FERRY FLIGHT TO CLT WITH NO PROBLEMS NOTED. MAINTENANCE AT CLT PERFORMED A POST FLAME OUT INSPECTION, NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: EGT PIG TAIL — SHORTED (RT ENG)

FLT NR 4762 - BNA - ON DESCENT RIGHT ENGINE EGT WENT TO 750 DEG PILOT SHUT DOWN ENGINE WF AND TQ STAYED THE SAME. MAINTENANCE INSPECTED AND FOUND RIGHT ENGINE EGT HARNESS PIG TAIL SHORTED. MAINTENANCE REPLACED HARNESS, ENG TEST RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)