N627AE

Part: NONE — NONE · airframe 48,045 hrs · 45,282 cycles

PDIS 627 21-31 2596072 07DEC21 PHL CLOSE ON CLIMB OUT AIRCRAFT WOULD NOT PRESSURIZE. RESET DUMP SWITCH ON GROUND. FACT 07DEC21 11:02 PHL FOUND PRESSURE CONTROLLER IN WRONG CONFIGURATION. A/C PRESSURIZATION NORMAL. OK FOR SERVICE.

Part: NONE — NONE · airframe 48,040 hrs · 45,276 cycles

PDIS 627 34-41 2596061 06DEC21 ALB CLOSE AT FL310 GPWS INOP AND WINDSHEAR INOP DISPLAYED ON EICAS. FACT 07DEC21 03:19 ALB FOUND LOOSE COAXIAL CONNECTORS ON RADIO ALTIMETER GOING TO TX AND RX ANTENNAS. FASTENED AS REQUIRED AND APPLIED TORQUE SEAL. OPS CHECK GOOD IRT EMB 145 AMM 34-41-00.

Part: SKIN — DENTED (FRAMES 22-23) · airframe 46,283 hrs · 43,396 cycles

DENT ON FUSELAGE SKIN BETWEEN FR 22-23 AND BETWEEN STR 12L-13L. INSTALLED AND EDGE SEALED SERVICEABLE REPAIR DOUBLER AND FILLER ON FUSELAGE SKIN BETWEEN FR 22-23 AND BETWEEN STR 12L-13L, IAW EMB 145 SRM 53-21-01, ITEM 5, FIGURE 202 AND EO1-53-20-0440.

Part: FRAME — CRACKED (FRM 66) · airframe 46,283 hrs · 43,396 cycles

FRAME 66 IS CRACKED AT CARGO DOOR CENTER SILL. PERFORMED REPAIR AT FR 66 BETWEEN STGR 20-L 21-L, IAW EO1-53-20-0436.

Part: TRUNNION — CRACKED (RT MLG) · airframe 46,283 hrs · 43,396 cycles

PERFORMED HFEC INSPECTION, IAW EASI NDTM RELEVANT INDICATION NOTED ON RT MLG AFT TRUNNION. ET EASI 8958 SETTINGS: FREQ. 400KHZ, ANGLE 291.1 DEG. H-61.3DB. V-77.6DB. FILTER LO PASS 500HZ. REMOVED AND REPLACED THE RT MLG AFT UPPER TRUNNION, IAW PIEDMONT EO1-57-20-0432.

Part: FLOOR SUPPORT — CORRODED (LT CABIN) · airframe 46,283 hrs · 43,396 cycles

CABIN LT OMEGA BEAM NR 6 HAS AREAS OF CORROSION. REPAIRED CABIN LT OMEGA BEAM NR 6 CORROSION, IAW EO1-53-20-0430.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 46,283 hrs · 43,396 cycles

CABIN CENTER OMEGA BEAM NR 4 HAS AREAS OF CORROSION. REPAIRED CABIN CENTER OMEGA BEAM NR 4 CORROSION, IAW PIEDMONT EO1-53-20-0431.

Part: FITTING — WORN (RT AILERON) · airframe 46,283 hrs · 43,396 cycles

RT AILERON TO PCA FITTING OUTBOARD LUGS WORN. REMOVED AND REPLACED RT AILERON TO PCA FITTING, IAW EMB 145 SRM 51-40-02, AMM 20-10-01.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 46,283 hrs · 43,396 cycles

BLENDED CHAFE ON CARGO DOOR INNER SKIN AT HB4 AND VB3 FOUND TO BE OUT OF LIMITS, REQUIRES REPAIR REFERENCE EMB 145 SRM 52-30-01 ITEM 12. REPAIRED BLENDED CHAFE ON CARGO DOOR INNER SKIN AT HB4 AND VB3, IAW PIEDMONT EO1-52-20-0435.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 46,283 hrs · 43,396 cycles

CARGO DOOR FUSELAGE SILL HAS NUMEROUS CORROSION SPOTS. R & R CARGO DOOR LOWER CENTER SILL, IAW EMB 145 SRM 51-40-02.

Part: BRACKET — CORRODED (CARGO DOOR FRAME) · airframe 46,283 hrs · 43,396 cycles

SSI 53-30-48 CARGO DOOR CUTOUT FWD LOWER CORNER L-SHAPE BRACKET HAS SURFACE CORROSION. REPAIRED CARGO DOOR CUTOUT FWD LOWER CORNER L-SHAPE BRACKET CORROSION, IAW PIEDMONT EO1-53-20-0437.

Part: STOP FITTING — CORRODED (EMERGENCY EXIT) · airframe 46,283 hrs · 43,396 cycles

LT CABIN EMERGENCY EXIT LOWER EDGE ROUND STOP HAS CORROSION AROUND THE BASE. REMOVED CORRODED NR 4 BEAM, POSITIONED, DRILLED AND INSTALLED SERVICEABLE NR 4 BEAM, IAW EMB145 SRM 51-40-02 AND SRM 51-20-03.

Part: FRAME — CHAFED (FUSELAGE) · airframe 46,283 hrs · 43,396 cycles

FR 70 BETWEEN STR 12R-13R IS CHAFED. REPAIRED FR 70 BETWEEN STR 12R-13R, IAW EO1-53-20-0428.

Part: RIB — CRACKED (LT WING) · airframe 46,283 hrs · 43,396 cycles

LT WING RIB 21 IS CRACKED IN 2 AREAS INSIDE 551CB. REPAIRED LT WING RIB 21 CRACKED IN 2 AREAS INSIDE 551CB, IAW PIEDMONT EO1-57-20-0434.

Part: RIB — CRACKED (RT WING) · airframe 46,283 hrs · 43,396 cycles

RT WING RIB 21 IS CRACKED INSIDE PANEL 651CB. REPAIRED RT WING RIB 21 CRACK INSIDE PANEL 651CB, IAW PIEDMONT EO1-57-20-0433.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 49,450 hrs · 43,533 cycles

MASTER WARNING LDG DISAGREE ON TAKE OFF. MAINTENANCE: FOLLOWED FIM TASK 32-32-00-810-803-A UP TO BLOCK DIAGRAM STEP 22 AND FOUND TO BE TRANSITORY CONDITION OF THE LANDING GEAR. AS A PRECAUTION WE BLEED BOTH HYDRAULIC SYSTEMS. OK FOR SERVICE. FOLLOW UP: REMOVED EICAS AND PERFORMED LANDING GEAR PROXIMITY SWITCH FUNCTIONAL CHECK. C/W W/C 32-70-01, 32-70-02, AND 32-70-03, NO DEFECTS NOTED. REINSTALLED EICAS AND PERFORMED EICAS OPS CHECK IAW TASK 31-41-00-700-802-A. REMOVAL AND INSTALLATION MADE IAW AMM 34-22-01.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 45,718 hrs · 42,761 cycles

W/S HEAT 1 FAILED INTERMITTENTLY OUTSIDE OF ICING CONDITIONS. REMOVED AND REPLACED WINDSHEILD #1 TEMP CONTROLLER. OPS CHECK GOOD AT THIS TIME, REF AMM 30-42-01. PILOT SEAT REMOVED AND REINSTALLED TO FOM , REF AMM 25-11-01. RII C/W.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,188 hrs · 42,155 cycles

BLD 1 VLV FAIL,PACK 1 FAIL, WG A/ICE FAIL, STAB ICE FAIL, ICE COND A/ICE FAIL ON TAXI.....FIX: OPS CHECK OF ENG BLEED AND A/ICE SYSTEM C/W. NO DEFECTS.CND. REF AMM 30-00-00

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,172 hrs · 42,136 cycles

MDIS 627 21-01 1898121 27OCT19 PHL CLOSE STRONG BURNING ODOR IN FLT COMPARTMENT DURING FLIGHT , NO ABNORMAL INDICATIONS OR EICAS MSGS FACT 27OCT19 16:50 PHL RAN #1 PACK WITH APU BLEED AND ENG 1 BLEED AIR. NO B URNING SMELL IN COCKPIT AND NO RELATED CMC MESSAGES. A/C GOOF FOR SERVICE

Part: CLAMP — LOOSE (BLEED VALVE) · airframe 44,629 hrs · 41,519 cycles

BLEED 2 LEAK WARNING IN FLIGHT. FIX: RETIGHTENED FWD V-BAND CLAMP ON #2 ENG BLEED VALVE IN PYLON. RAN ENG 2 PLUS BLEED 2 FOR 30 MIN LEAK CHECK GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,122 hrs · 40,940 cycles

EMERGENCY LIGHTS BATTERY INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW WORKCARD 33-70-19, OK FOR SERVICE.

Part: VANE — OUT OF ALIGNMENT (AOA) · airframe 42,822 hrs · 39,444 cycles

SPS ADVANCED DISPLAYED ON EICAS AFTER TAKEOFF, AND WENT AWAY AT TOUCHDOWN. ALIGNED AOA VANES AND PERFORMED OPS CK IAW 27-36-00. OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 42,327 hrs · 38,871 cycles

CARGO DOOR SILL HAS SEVERAL SPOTS OF CORROSION BETWEEN FRAMES 65 AND 68. REMOVE AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02, AND EO1-53-18-0113.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 42,287 hrs · 38,961 cycles

SERVICE DOOR CENTER SILL HAS MULTIPLE AREAS OF CORROSION. R & R SERVICE DOOR SILL.

Part: SWITCH — SHORTED (PNUMATIC SYS) · airframe 40,534 hrs · 36,963 cycles

RAN QRH FOR A LEAK EICAS MESSAGE INFLIGHT AT 10000 FT. MESSAGE DID NOT EXTINGUISH. ALSO HAD A NR 2 BLEED VALVE CLOSED MESSAGE. INSPECTED AND FOUND GROUND AIR TEMPERATURE SWITCH SHORTED TO GROUND. CLEANED AND SEALED IAW AMM 20-30-03. PERFORMED BLEED AIR TEST IAW AMM.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 40,217 hrs · 36,607 cycles

DURING ANTI-ICE SYSTEM TEST, THE WING ANTI-ICE FAILED EICAS MESSAGE ACTIVATED. REMOVED AND REPLACED RT WING ANTI-ICE VALVE IAW AMM 30-11-01 AND TIGHTENED DAMPER LINE ON ANTI-ICE MANIFOLD IAW AMM 30-11-14 PAGE 4.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTOR) · airframe 40,146 hrs · 36,535 cycles

NR 1 ENGINE FIRE DETECTOR FAILED CAUTION MESSAGE ILLUMINATED IN FLIGHT. EXTINGUISHED PRIOR TO LANDING. CREW SHUT DOWN ENGINE DURING TAXI IN. CREW REPORTED NO FIRE INDICATION. INSPECTED CMC FOR CODES. NO CODES PRESENT.INSPECTED AND CLEANED ENGINE AND PYLON FIRE DETECTOR CONNECTORS. PERFORMED FIRE SYSTEM TEST IAW 26-10-00-700-802-A. NO DISCREPANCIES NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 39,288 hrs · 35,588 cycles

FWA CLOSE SPOILER FAIL EICAS MESSAGE ON TAXI MESSAGE EXTINGUISHED AFTER 30 SECONDS. FLAPS WERE AT 9 DEGREES. INSPECTED AND FOUND TO BE TRANSITORY CONDITION OF THE SPOILER CONTROL UNIT. NO RELATED MESSAGES ON EICAS CMC 27-63-00-810-802-A. OK FOR SERVICE.

Part: WIRE — BURNED · airframe 39,246 hrs · 35,539 cycles

WIRE W102-0268-16 IS BURNED BETWEEN PINS C2 RELAY K0058 AND C1 RELAY K1237 ON NR 3 PITOT. STATIC HEATING SYS. REPLACED WIRE W102-0268-16 BETWEEN PINS C2 RELAY K0058 AND C1 RELAY K1237 IAW WM 30-31-50 AND SWPM 20-21-00. USED PINS, PN M39029/92-536 IAW AD2007-04-03. R & R RELAY K0058 AND K0058 RELAY BASE IAW AMM 20-13-02. NR 3 PITOT. STATIC HEATING OPS CHECKED GOOD IAW AMM 30-31-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,020 hrs · 35,239 cycles

CREW REPORTS ODOR FROM LT ELECTRICAL DISTRIBUTION PANEL AREA. INSPECTED ELECTRICAL DISTRIBUTION PANEL AREA AND ASSOCIATED WIRING C/N/D AFTER POWERING UP SEVERAL TIMES. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,008 hrs · 35,225 cycles

APU RUNNING, WITH NR 2 ENGINE BLEEDS ON 30 SEC LATER STRONG ODOR IN FLIGHT DECK AND FWD CABIN SHUTOFF BLEEDS AND RECIRCULATING FAN ODOR DISSAPATED. GROUND RAN A/C. C/W FIM 21-20-00-810-801A, NO DEFECTS NOTED. C/W FIG FIM 21-20-00-810-803A, NO ODOR FROM EITHER ENGINE BLEED, APU BLEED OR PACKS 1 & 2. CND IF CONDITION OCCURES AGAIN, MORE DETAILS ARE REQUIRED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 38,866 hrs · 35,032 cycles

CLOSE EICAS MESSAGE DISPLAYED E2 NO DISPLAY. INSPECTED ACFT FOR CODES ON IAW AMM 45-45-00. NO CODES FOUND. POWERED ACFT DOWN & UP. EICAS MESSAGE CLEARED. ACFT OK. FOR SERVICE.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND A PREVIOUS BLENDED AREA AT FWD EDGE OF THE CARGO DOOR OPENING. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO BLENDED AREA IAW ERS-EM-53MR-1653. REPAIR MATERIALS, DOUBLER 2024T3, .080, FILLER 2024T3, .080.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND 1 CRACK ON LT REAR FUSELAGE I SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON CRACK IAW ERS-EM-53MR-1657. REPAIR MATERIAL, DOUBLER 2024-T3, 0.080, FILLER 2024-T3, 0.063, ANGLE 2024-T3, 0.050, SHIM 2024-T3-0.032.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND 1 CRACK ON RT REAR FUSELAGE I SKIN, JUST AFT OF FRAME 75 ABOVE STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON CRACK ON RT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1624. REPAIR MATERIAL, DOUBLER 2024-T3, 0.080, FILLER 2024-T3, 0.063, ANGLE 2024-T3, 0.050, SHIM 2024-T3-0.032.

Part: SKIN — CHAFED (FUSELAGE) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND THE FUSELAGE SKIN CHAFED INSIDE LT PYLON PANEL 414DB. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED CHAFE DAMAGE IAW ERS-EM-53MR-1622. REPAIR MATERIALS, DOUBLER 2024T3, .063, FILLER, 2024T3, .063.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND PAX DOOR REINFORCEMENT FITTING CRACKED AT FRAME 20 & STRINGER 3L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R PAX DOOR REINFORCEMENT FITTING IAW SRM 51-40-02, 51 20-03 & AMM 20-10-01. REPLACEMENT PART 145-24109-603.

Part: HINGE FITTING — WORN (RUDDER) · airframe 38,726 hrs · 34,830 cycles

DURING MBV INSPECTION, QA FOUND RUDDER I LOWER HINGE FITTING WORN. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R RUDDER I LOWER HINGE FITTING IAW SRM 51-40-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,726 hrs · 34,830 cycles

EMERGENCY FLOOR LIGHTS 1 - 3 INOPERATIVE. R & R NR 2 EMER BATTERY ASSEMBLY IAW AMM 33-50-04. CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 38,479 hrs · 34,573 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 38,379 hrs · 34,482 cycles

AFT EMERGENCY LIGHT STRIP FOUND INOPERATIVE. LIGHT R & R IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: BRAKE — LEAKING (MLG) · airframe 38,302 hrs · 34,415 cycles

LEFT SIDE INBD BRAKE LEAKING HYD FLUID. TIGHTENED UPPER FWD CAP ON NR 2 BRAKE ASSEMBLY IAW AMM 32-49-03. LEAK CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 38,230 hrs · 34,363 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53. COMPLIED WITH MX PROCEDURES. R & R CAPTAINS FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD MEL RESTORED.

Part: FAN — FAILED (CABIN) · airframe 38,050 hrs · 34,223 cycles

JUST AFTER PUSHBACK, FLIGHT ATTENDANT CALLED WITH SMOKE IN CABIN, FINE MIST OF SMOKE, HOT AIR AT FLOW VENT OF ROW 5A. FLIGHT ATTENDANT REPORTED GRINDING NOISE AT 9B+C, SMELL WAS ELEC WITH VISIBLE SMOKE IN FWD CABIN. R & R NR 2 RECIRC FAN & RT ACM IAW NRWC 627-DFW-02384 & 627-DFW-02383 FOR WORK ACCOMPLISHED. OPERATIONS CHECKED GOOD IAW ETN-EM-72-034, NO DEFECTS NOTED. ACM PN 8152403 & SN 200107198.

Part: WIRE — DAMAGED (ANTI-ICE SYSTEM) · airframe 37,010 hrs · 33,311 cycles

STAB ANTI-ICE FAIL DURING CLIMB. CHECKLIST PERFORMED, MSG REMAINED. TRANSFERRED TO NRWC 627-ABI-02170. REPAIRED WIRE W311-0031-22N & W311-0030-22 IAW SWPM 20-21-00, NO FURTHER DEFECTS NOTED. REPAIRED & REPLACE HORIZONTAL STABILIZER ANTI-ICING DIFFERENTIAL PRESS SWITCH IAW AMM 30-12-04. OPERATIONS CHECK FAILED.

Part: SWITCH — MALFUNCTIONED (AUTOPILOT SYS) · airframe 36,996 hrs · 33,300 cycles

ON ILS APPROACH AP ON AT LOC CAPTURE AUTO PILOT COMMANDED & UNCOMMANDED TO & GA. FD STILL COMMANDED TO & GA WITH AP DISCONNECTED. ON CLIMB OUT WHEN SPEED MODE SELECTED & UNCOMMANDED FD TO ROL & GA. TRANSFERRED TO NRWC 627-DFW-02156. R & R RT GA SWITCH. OPERATIONS CHECKED GOOD IAW AMM 22-11-00. ACFT IS COMPLIANT FOR CAT II OPERATIONS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,839 hrs · 33,180 cycles

OVERWING EXTERNAL EMER LIGHTS WILL NOT ILLUMINATE. R & R NR 4 EMER LIGHT BATTERY & CHARGER ASSEMBLY IAW WORK CARD 33-700-19. OPERATIONS CHECKED GOOD IAW WORK CARD 33-700-17. EMER LIGHTING BATTERY PN 2013-1A SN 110532.

Part: EPSU — FAULTY (CABIN) · airframe 36,839 hrs · 33,180 cycles

DURING PREFLIGHT NOTICED EMER LIGHT STRIP ON FLOOR STAYED ON WITH SWITCH IN ARM MODE. EMER LIGHTS THAT WERE ON WERE FROM ROW 14 TO 18 ON THE A SIDE OF SEATS. R & R NR 4 EPSU ASSEMBLY. OPERATIONS CHECKED GOOD IAW WC 33-700-19. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 & SN C00652.

Part: VALVE — FAULTY (AC BAY) · airframe 36,369 hrs · 32,775 cycles

AUTO PRESS FAIL CABIN ALT IN AMBER 8100 ON EICAS, ACTUAL ALT 7400. R & R GND CONNECTION VLV IAW AMM 21-22-04.

Part: UNKNOWN — MALFUNCTIONED (RUDDER) · airframe 36,328 hrs · 32,746 cycles

RUDDER SYS 1 - 2 FAIL INFLIGHT. FOLLOWED FIM PROCEDURES. PERFORMED OPERATIONAL CHECK OF RUDDER SYS IAW AMM 27-25-00 NO FAULTS FOUND. COULD NOT DUPLICATE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 35,694 hrs · 32,260 cycles

RIGHT UPPER WING EMER LIGHT INOPERATIVE. R & R RT WING EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 35,333 hrs · 31,953 cycles

FLASHLIGHT HOLDER REAR CABIN FLASHLIGHT BROKEN. R & R FLASHLIGHT SYS IAW 25-60-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 34,890 hrs · 31,577 cycles

FLASHLIGHT BEHIND ROW 18 BRACKET BROKEN. ACFT WAS REMOVED FROM SERVICE. R & R AFT FLASHLIGHT HOLDER IAW AMM 53-50-16, MEL RESTORED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,373 hrs · 31,158 cycles

LEFT & RT OVERWING & LAST FLOOR STRIP EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW 145 AMM 33-50-04, OPERATIONS GOOD.

Part: SKIN — CORRODED (FRAMES 13-14) · airframe 34,310 hrs · 31,107 cycles

DURING HMBV INSPECTION, QC FOUND FUSELAGE SKIN CORRODED BETWEEN FR 13-14,STRINGERS 19L-19R. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON CENTER FUSELAGE I SKIN BETWEEN FR 13-14 AND STR 19L-19R IAW ERS-EM-53MR-025 ACFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,310 hrs · 31,107 cycles

PROXIMITY LIGHT STRIPS NR 1 & NR 6 DAMAGED. R & R FLOOR PROXIMITY LIGHT STRIPS NR 1 & NR 6 AS REQUIRED SEE BOW141502 FOR LIGHT STRIPS INSTALLATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,310 hrs · 31,107 cycles

FLOOR PROXIMITY LIGHT STRIPS NR 7 DAMAGED. R & R FLOOR PROXIMITY LIGHT STRIP NR 7 IAW EMB 145 AMM 33-50-12. SEE NRTC BOW141502 FOR OCK.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,310 hrs · 31,107 cycles

SHEAR CLIP ON FR 65 CORRODED BETWEEN STRINGER 15L & 16L. REPAIRED SHEAR CLIP ON FR 65 IAW AEA EO-EM-53MR-1129.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,208 hrs · 31,031 cycles

EMERGENCY LIGHTS AT LT UPPER OVER WING EMERGENCY EXIT DOOR AND AFT CEILING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 INVERTER. OPS CHECKED GOOD IAW AMM 33-50-11 AND AE W/C 33-700-17.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 33,601 hrs · 30,545 cycles

SERVICE DOOR LOWER EXIT MARKER AND CABIN FIRST FLOOR EMERGENCY STRIP DID NOT ILLUMINATE. RAR NR 2 DC/AC INVERTER IAW AMM 33-50-11. OPC OF EMERGENCY LIGHTS GOOD AT THIS TIME IAW AMM 33-50-00. NO OTHER DEFECTS NOTED.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 33,261 hrs · 30,249 cycles

DURING MX INSPECTION, FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 EMERGENCY BATTERY POWER SUPPLY F3 FUSE IAW CMM 25-60-03. THE OPS. CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 33,261 hrs · 30,249 cycles

THE CREW REPORTED THE F/O’S FLASHLIGHT WOULD NOT CHARGE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O`S FLASHLIGHT IAW AMM 33-51-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER UNIT — DEFECTIVE (FLASHLIGHT) · airframe 33,102 hrs · 30,134 cycles

ON FLIGHT 3350 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE (CHARGING LIGHT SHOWS FLASHLIGHT CHARGING BUT FAILS TO ILLUMINATE). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT POWER UNIT IAW EMB AMM145 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,330 hrs · 29,568 cycles

DURING B INSPECTION FOUND THE FORWARD GROUND PROXIMITY EMERGENCY AISLE LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND BATTERY PACK IAW WORK CARD 33-700-19. THE OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED AT THIS TIME END. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LEAD — LOOSE (EMERGENCY LIGHT) · airframe 32,216 hrs · 29,472 cycles

DURING B INSPECTION FOUND THE EMERGENCY CEILING LIGHT AT 11B AND 11A INOPERATIVE ON BACK SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ATTACHED EMERGENCY LIGHT LEADS IAW EMB AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — INOPERATIVE (MLG) · airframe 31,116 hrs · 28,585 cycles

FLIGHT 3450, JUST AFTER TAKEOFF WHEN THE CREW PUT THE LANDING GEAR LEVER UP THE INDICATION ON THE EICAS WAS THE LEFT MAIN WAS STILL INTRANSIT. THEY GOT THE EICAS MESSAGE LANDING GEAR DISAGREE. FOLLOWED AOM VOL.1 CYCLED THE GEAR GOT 3 GREEN. NEVER EXCEEDED 200 KTS. THE CREW DECLARED AN EMERGENCY AND RETURNED FOR LANDING. THE LANDING WAS BELOW LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM 32-33-10. OPS CHECK GOOD IAW W/C 32-700-01 AND W/C 32-700-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — CRACKED (ACCESS DOOR) · airframe 30,900 hrs · 28,421 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND THE ACCESS DOOR PIN RECEPTACLE BENT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW EO EM-52MR-316. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,804 hrs · 28,341 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT SYSTEM FLOOR LIGHT STRIP INOPERATIVE AT ROWS 3-4. REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP AT ROW 3/4 IAW AMM 33-50-12. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,797 hrs · 28,334 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIP AT ROW 18 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROW 18 IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 30,058 hrs · 27,768 cycles

FLIGHT 2942, CREW REPORTED THAT AFTER SHUTDOWN, EMERGENCY LIGHTS ROW 1-7 WOULD NOT TURN OFF. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT EMERGENCY LIGHTS AND FOUND NR 2 CHARGER ASSEMBLY BAD. REMOVED AND REPLACED NR 2 BATTERY AND CHARGER ASSEMBLY IAW W/C 33-700-19. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,048 hrs · 27,762 cycles

FLIGHT 2807, THE CREW REPORTED THAT AFTER SHUTDOWN EMERGENCY LIGHTS ROW 1-7 WOULD NOT TURN OFF. AIRCRAFT REMOVED FROM SERVICE. ELECTRICAL POWER RESET. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 29,912 hrs · 27,657 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE CENTER AISLE CEILING EMERGENCY LIGHT ON AFT SIDE ROW 12 DO NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFT CEILING EXIT LOCATION SIGN ROW 12 CONNECTORS WERE REPOSITIONED AND THE LIGHT OPERATIONAL CHECK WAS GOOD IAW 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 29,855 hrs · 27,613 cycles

DURING B-INSPECTION FOUND THE LEFT EMERGENCY EXIT SIGN AFT OF THE LEFT OVERWING EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED SPLICES SP9126 SP9127 OF LEFT EMERGENCY EXIT MARKER DS8507-251 IAW EMB SWPM 20-50-01. PERFORMED OPERATIONAL CHECK OF THE LEFT EMERGENCY EXIT MARKER DS8507-251 IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,646 hrs · 27,448 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT IN AFT POSITION INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 29,093 hrs · 27,065 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN OVERHEAD AFT EMERGENCY LIGHT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED CABIN OVERHEAD PANEL AFT EMERGENCY LIGHT AND THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-15 SUBTASK 33-50-15-710-001-A00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,093 hrs · 27,065 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING PANEL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING PANEL EMERGENCY LIGHT IAW EMB 145 AMM SUB TASK 33-50-10-020-003-A00 AND 33-50-10-420-003-A00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,093 hrs · 27,065 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING PANEL EMERGENCY LIGHT IAW EMB 145 AMM SUBTASK 33-50-10-020-003-A00 AND 33-50-10-420-003-A00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,370 hrs · 26,482 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT GALLEY EMERGENCY EXIT SIGN DOES NOT LIGHT DURING TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE DETECTOR — FAULTY (CARGO BAY) · airframe 27,523 hrs · 25,828 cycles

ON FLIGHT 3640 ON LANDING THE CREW REPORTED THAT THE BAGGAGE SMOKE INDICATION ON ECIAS CAME ON. THE CREW PRESSED THE FIRE EXTINGUISHER BUTTON. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH BAGGAGE FIRE EXTINGUISHER BOTTLE P/N: 346000731 - S/N: 33861F1 AND P/N: 337000271 - S/N: 70563D1. ALSO REMOVED AND REPLACED BOTH FIRE DETECTORS P/N: 47359713 S/N: 0085 AND 1610. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD WIPER — DEFECTIVE (WINDSHIELD) · airframe 26,125 hrs · 24,765 cycles

ON FLIGHT 3233 DURING THE TAKEOFF ROLL THE CREW REPORTED THE CAPTAIN’S WINDSHIELD WIPER MOVED UNCOMMANDED TO FULL DOWN POSITION AND WIPER STAYED 2 TO 3 INCHES OFF THE WINDSHIELD. THE WIPER MOVED 1/4 WAY UP WINDOW DURING FLIGHT AND STAYED, WINDOW WAS WET WITH DEW ON TAKEOFF ROLL. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S WIPER ARM IAW EMB 145 MM 30-41-03. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,831 hrs · 24,529 cycles

DURING MAINTENANCE BASE VISIT FOUND THE OVERHEAD EMERGENCY LIGHT AT SEAT 12B AND 12C TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ABOVE SEAT 12B AND 12C IAW EMB 145 AMM33-50-08-000-801-A/33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY) · airframe 25,810 hrs · 24,518 cycles

ON FLIGHT 2862 DURING TAXI THE CREW RECEIVED A BAGGAGE SMOKE EICAS MESSAGE WITH A TRIPLE CHIME. THE CREW DISCHARGED THE BAGGAGE EXTINGUISHER. THE BAGGAGE EXTINGUISHER LIGHT ON THE OVERHEAD BUTTON REMAINED ON. NO INDICATION OF FIRE OR SMOKE. BOTH THE HIGH DISCHARGE FIRE BOTTLE DISCHARGED AND METERING FIRE BOTTLE DISCHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FUNCTIONAL CHECK OF BAGGAGE SMOKE DETECTORS IAW EMB 145 AMM 26-15-00. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE HIGH DISCHARGE FIRE BOTTLE IAW EMB 145 AMM 26-23-01 AND REMOVED AND REPLACED THE METERING FIRE BOTTLE IAW EMB 145 AMM 26-26-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,786 hrs · 24,503 cycles

FOR FLIGHT 2721 DURING AN OPERATIONAL CHECK FOUND THE EMERGENCY LIGHTS AFT OF THE GALLEY EMERGENCY EXIT SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,575 hrs · 24,347 cycles

FOR FLIGHT 2969 DURING MAINTENANCE THE EMERGENCY LIGHT ON AFT GALLEY WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,362 hrs · 24,182 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT LIGHT IN FRONT OF FRONT ROW DOUBLE SEAT ON BULKHEAD WALL DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC LINE — LOOSE (NLG) · airframe 24,948 hrs · 23,865 cycles

ON FLIGHT 9801 AFTER TAKEOFF THE CREW REPORTED THAT THE HYDRAULIC SYSTEM 1 QUANTITY WENT TO ZERO WITH ASSOCIATED EICAS MESSAGES. THE CREW COMPLIED WITH THE AIRCRAFT OPERATING MANUAL VOL 1. THE CREW ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TORQUED HYDRAULIC HOSE LINE IN NOSE LANDING GEAR BAY AT THE LEFT NOSE LANDING GEAR ACTUATOR AND SERVICED HYDRAULIC SYSTEM NR 1 IAW EMB 145 AMM 20-10-03 AND 12-13-01. LEAK CHECKED GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUESLAGE) · corrosion level 2 · airframe 24,947 hrs · 23,864 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT TORQUE TUBE SUPPORT TO BE CORRODED BETWEEN FRAMES 12/13 AND STR 20L/21L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED SUPPORT AND INSTALLED SERVICEABLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,947 hrs · 23,864 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT TORQUE TUBE SUPPORT BETWEEN FRAME 12/13 AND STRINGER 20/21R TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,947 hrs · 23,864 cycles

DURING MAINTENANCE BASE VISIT THE EMERGENCY LIGHT STRIPS L1, L2, L3, L5 & L7 WERE FOUND TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIPS L1, L2, L3, L5, & L7 IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 24,930 hrs · 23,845 cycles

ON FLIGHT 4034 THE CREW REPORTED THAT THE CARGO DOOR INDICATION REMAINED OPEN AND WOULD NOT INDICATE THAT IT WAS CLOSED. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED CARGO DOOR MICRO SWITCHES IAW EMB AMM 52 76 00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — FAILED (NLG) · airframe 24,733 hrs · 23,683 cycles

ON FLIGHT 3683 THE CREW REPORTED THAT AFTER TAKEOFF WHEN SELECTED GEAR UP, HEARD A STRANGE NOISE COMING FROM THE NOSE LANDING GEAR AREA. THE NOSE LANDING GEAR SHOWED AN AMBER INDICATION AND NEVER WENT TO GREEN. THE RESULT WAS A LEVER DISAGREE MESSAGE. THE CREW CYCLED THE GEAR DOWN AND THE NOSE LANDING GEAR SHOWED A GREEN INDICATION. ATTEMPTED ONE MORE TIME TO BRING THE GEAR UP WITH SAME RESULTS. BROUGHT THE GEAR BACK DOWN AND RETURNED BACK TO CID. LANDED OVERWEIGHT. HOWEVER THE RATE OF DESCENT WAS LESS THAN 300 FEET PER MINUTE. NO OVERWEIGHT INSPECTION REQUIRED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX IAW AMM 52-33-07. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — INOPERATIVE (RT MLG) · airframe 23,808 hrs · 22,949 cycles

ON FLIGHT 3892, THE CREW REPORTED THAT AFTER TAKEOFF THEY HEARD A LOUD THUMPING NOISE IN THE NOSE LANDING GEAR AREA. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10 AND DID EXTENSION AND RETRACTION CHECKS. OPERATIONAL TESTS WERE GOOD, FCF PASSED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (YAW DAMPER) · airframe 23,804 hrs · 22,944 cycles

DURING FLIGHT 3830, THE CREW REPORTED THAT AFTER TAKEOFF AT APPROXIMATELY 500 FEET WITH THE YAW DAMPER ENGAGED, THE CREW RECEIVED A RUDDER 12 FAIL MESSAGE ALONG WITH A YAW DAMPER FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED RELAY K0387. OPERATIONAL CHECK GOOD IAW 27-23-00-700-804. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM IAW EMB 145 27-23-00-700-804-A. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT WAS RETUNED TO SERVICE.

Part: CONTROL UNIT — FAILED (MLG BRAKES) · airframe 23,771 hrs · 22,912 cycles

FLIGHT 3885, CREW REPORTED BRAKES OUT ON LANDING. POST LANDING INSPECTION FOUND 4 BLOWN MAIN TIRES. ACFT REMOVED FROM SERVICE. R & R NR 1, 2, 3, &4 MLG ASSEMBLIES IAW AE WORK CARD 32-700-11. COMPLIED WITH WORKSCOPE PROVIDED BY MANUFACTURER. ALL OPS CHKS GOOD. R & R BRAKE CONTROL UNIT IAW AMM 32-41-01 & NR 4 BRAKE PEDAL TRANSDUCER PER MANUFACTURER REQUEST IAW 32-41-02. OPS CHK GOOD. COMPLIED WITH SIDE LOAD INSP IAW AEWC 05-200-00. NO DEFECTS NOTED. PERFORMED MAIN BRAKE SYS CHK IAW AMM 32-41-00. OPS CHK GOOD. PERFORMED MLG EXTENSION & RETRACTION & FREE FALL CHK IAW AMM 32-30-00 & 32-34-00. OPS CHK GOOD. PERFORMED VISUAL INSP OF MLG BRAKES IAW 32-49-03. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: SKIN — CUT (FUSELAGE) · airframe 23,177 hrs · 22,361 cycles

DURING RAMP OPERATIONS, IN CARGO LOADER HIT ACFT BELOW CARGO DOOR AREA. DAMAGE IS A CUT .2500 INCH WIDE AND 30 INCHES LONG ALONG BOTTOM OF ACFT. MX TEMP REPAIRED AND FERRIED ACFT FOR PERMANENT REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,177 hrs · 22,361 cycles

DISC - DURING RAMP OPERATIONS AIRCRAFT WAS DAMAGED BELOW CARGO DOOR AREA. DAMAGE IS .25 INCH WIDE AND 30 INCHES LONG ALONG THE BOTTOM OF AIRCRAFT. AIRCRAFT REMOVED FROM SERVICE. TEMPORARY REPAIR APPLIED AND AIRCRAFT REPOSITIONED TO MQT FOR REPAIRS. AIRCRAFT WAS REPAIRED IAW EO EM-53MR-1306. AIRCRAFT RETURNED BACK TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,174 hrs · 19,850 cycles

DURING A MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND CORRODED AROUND A NUT PLATE HOLE 8" AFT OF FRAME 22. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION AND PERFORM NDT. FILLED THE BLENDED AREA WITH HYSOL EA934NA RESIN AND CURDED. FABRICATED. A REPAIR DOUBLER FROM AL 2024-T3, CLEANED AND TREATED REPAIR PART. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/ 1142 REV 39) CHAPTER 53-21-10 FIGURE 206. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (LAV) · airframe 20,174 hrs · 19,850 cycles

DURING A MBV INSPECTION, THE TOILET WASTE DRAIN SUPPORT WAS FOUND CORRODED. REMOVED DAMAGED SUPPORT AND CLEANED THE AREA. POSITIONED NEW SUPPORT P/N 145-25599-001 MARKED AND DRILLED FASTENERS HOLES. REMOVED NEW SUPPORT, CLEANED AND TREATED THE SUPPORT AND THE REPAIR AREA. WORK DONE IAW 145 SRM (SRM EMB 145/1142 REV 39) CHAPTERS 51-40-02, 51-20-03, 51-20-01, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,174 hrs · 19,850 cycles

DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED THE NEW SILL P/N 145-25480-603, NEW ANGLES P/N 145-25681-607 AND 145-25681-007, MARKED AND DRILLED FASTENERS HOLES. WORK DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTERS 51-40-02, 51-21-04, 51-40-06 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 19,027 hrs · 18,794 cycles

IN CRUISE FLT AT FL250 HAD A SLOW CABIN DEPRESSURIZATION. CABIN ALT GOT TO 10,100 FEET. DID EMERGENCY DESCENT TO 10,000 FEET. RAN PRESS AUTO FAIL AND CABIN ALTITUDE IN AMBER RANGE CHECK LISTS. LEVEL AT 10,000 FEET. CABIN ALT STABILIZED AT 8,000 IN MANUAL MODE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,962 hrs · 18,725 cycles

EMERGENCY LIGHTS AFT OF ROW 13 DOES NOT WORK, THEY COME ON INITIALLY THEN GO DARK. REMOVED AND REPLACED EMERGENCY BATTERY IAW 33-50-04-000-801-A AND 33-50-04-400-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL VALVE — FAILED (BRAKES) · airframe 17,546 hrs · 17,315 cycles

OUTBOARD BRAKE INOPERATIVE MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED AND REPLACED OUTBOARD BRAKE CONTROL VALVE IAW EMB AMM TASK 32-41-06-000-801-A AND TASK 32-41-06-400-801-A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — BENT (FUSELAGE)

DURING MBV, FOUND FRAME 72 BENT JUST ABOVE FLOOR LEVEL ON LEFT SIDE OF BAGGAGE COMPARTMENT. REPAIRED FRAME 72 IAW SRM 53-00-04 FIGURE 201 BY CUTTING OUT DAMAGE AND SPLICING IN A NEW PIECE OF FRAME. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 18-24 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 30-36 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06 AND I/C 2006-145/4615. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 24-30 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND RIGHT OUTBOARD UPPER SEAT TRACK BETWEEN FRAMES 24-30 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND INBOARD SEAT TRACK BETWEEN FRAMES 24-30 IS CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 36 TO 47 CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND RIGHT OUTBOARD UPPER SEAT TRACK CORRODED BETWEEN FRAMES 47-53. REMOVED AND INSTALLED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 36-47 IS CORRODED. REMOVED AND INSTALLED TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV FOUND LEFT OUTBOARD UPPER SEAT TRACK CORRODED BETWEEN FRAMES 47-52. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV, FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 30-36 IS CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND RIGHT OUTBOARD UPPER SEAT TRACK BETWEEN FRAMES 36-47 IS CORRODED. REMOVED AND INSTALLED TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV, FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47-53 IS CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV FOUND RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 30 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB 145 AMM 53-01-06-000-801A/400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV, FOUND LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB 145 AMM 53-01-06-000-801A/400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING IMBV, FOUND 3 DENTS IN AIRCRAFT SKIN BETWEEN FRAMES 15-16 AND STRINGERS 19L-20L. REPAIRED DENTS IAW SRM 53-21-01 FIGURE 204 BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 12,114 hrs · 12,333 cycles

CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM.(K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER SHIMS. REPAIR DONE IAW SRM.

Part: SKIN — DENTED (ACCESS DOOR)

DURING A MBV INSPECTION, ACCESS DOOR 123BL WAS FOUND DENTED. PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200501184)

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

DURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. (SW21200501184)

Part: FRAME — CRACKED (FUSELAGE)

DURING AN INSPECTION OF AN EXISTING REPAIR TO FRAME 73 AT STRINGER 15L ADDITIONAL DAMAGE IN THE FORM OF A .75 INCH LONG CRACK, WAS FOUND. REMOVED THE EXISTING REPAIR PERFORMED AN EDDY CURRENT INSPECTION TO CONFIRM CRACK ENDED AT A RIVET HOLE. FABRICATED AN L-SHAPE REINFORCEMENT AND INSTALLED INTO FIR AIRCRAFT. REPAIR DONE IAW MM REPAIR STATEMENT AND STANDARD MFG SRM PRACTICES.

Part: SILL — CORRODED (CARGO DOOR)

DURING AN IMBV INSPECTION, CARGO DOOR LOWER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CARGO DOOR LOWER SILL. INSTALLED SERVICEABLE SILL IAW MFG SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURNG AN IMBV INSPECTION, THE GALLEY AREA FORWARD DIGITAL WAS FOUND TO BE CORRODED. FABRICATED A SHIM AND TWO DOUBLERS. REPAIRED IAW EMB-145 SRM 145/1142, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION, MAINTENANCE FOUND CORROSION ON GALLEY CENTER FLOOR BEAM. CUT OUT SECTION GALLEY CENTER BEAM. FABRICATED A U-BEAM DOUBLER, FILLER. REPAIR DONE IAE EMB-145 SRM 145/1142, CHAPTER 51, REV 19, 51-40-02, ENB GST-1736/02-C ETN EM-53-034 R1, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED. BLENDED CHAFED AREA. PERFORMED AN NON DESTRUCTIVE TESTING INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE AND TWO SHIMS. REPAIR DONE IAW MFG SRM AND STANDARD SRM PRACTICES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, INBOARD SEAT TRACK FOR SEAT 1A-4A WERE FOUND TO BE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB 145 AMM 53-01-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LOWER CARGO DOOR SILL CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB 145 SRM 51-41-02. (M)

Part: PIN — CORRODED (HORIZ STAB) · corrosion level 2

THIS A LEVEL 2 FINDING, HORIZONTAL STABILIZER PINS ARE CORRODED. REMOVED AND REPLACED PINS IAW EMB 145 AMM 55-10-00. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA CENTER BEAM HAS CORROSION. INSTALLED REPAIR DOUBLER AND FILLER IAW EMB GST-1736/02C AND ETN EM 53-034R1. (M)

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

THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RAMP SUPPORT HAS CORROSION. INSTALLED SERVICEABLE RAMP SUPPORT IN GALLEY IAW EMB SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY ARE AFT DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE RIGHT SILL IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RIGHT FORWARD SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

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

THIS IS A LEVEL 2 FINDING. GALLEY AREA LEFT SILL HAS CORROSION. PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING, GALLEY CENTER BEAM GUSSET HAS CORROSION. INSTALLED SERVICEABLE GALLEY CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA AFT CROSSBEAM AND PROFILER HAS CORROSION. INSTALLED SERVICEABLE AFT CROSSBEAM AND PROFILE IAW EMB145 SRM 51-40-02. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

ORD - FLT 4174 - DURNIG CRUISE, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED. THE FLIGHT CREW ELECTED TO CONTINUE TO ORD. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB 145 AMM 56-10-01. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW EMB 145 AMM. OPERATIONALLY CHECKED GOOD. (M)

Part: CONTROLLER — MALFUNCTIONED (ELEVATOR)

DFW - FLT 3350 - UNCOMMANDED PITCH TRIM MOVEMENT FROM 4 DEGREES TO 2 DEGREES DOWN WHILE TAXIING. PERFORMED OPS CHECK OF PITCH TRIM SYSTEM IAW AMM. COULD NOT DUPLICATE, NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

DFW - FLT 3785 - DURING CLIMB-OUT, CREW NOTED MASTER WARNING ON PITCH TRIM 2 FAIL AND PITCH TRIM IND WAS SHOWING DASHES. CREW ELECTED TO RETURN TO DFW. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF PITCH HORIZONTAL STABILIZER IAW EMB 145 AMM 27-10-00-700-002A. COULD NOT DUPLICATE, OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: UNKNOWN — SMOKE (CABIN)

DAL - FLT 3448 - CLIMBING THROUGH 14,000 FEET STARTED TO GET FUMES SMELL IN CABIN. CREW PREFORMED SMOKE AND FUMES CHECKLIST AND SMOKE REMOVAL CHECKLIST. CREW WENT ON OXYGEN AND RETURNED TO DAL. PERFORMED EXTENSIVE GROUND RUNS OF BOTH ENGINES AND APU IAW EMB145 MM 80-00-00. COULD NOT DUPLICATE. PERFORMED OPS CHECK OF A/C HEATING AND BOTH PACKS. NO SMOKE SMELL FOUND. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUSE — BLOWN (ROW 7)

DFW - FLT 3618 - FOUND ROW 7 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE AT EMERGENCY BATTERY PACK. (M)