N622AE

Part: LAMP — INOPERATIVE (RH) · airframe 51,786 hrs · 47,174 cycles

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

Part: LAMP — INOPERATIVE (SD) · airframe 51,754 hrs · 47,128 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (RH) · airframe 51,636 hrs · 46,996 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (SD) · airframe 51,419 hrs · 46,742 cycles

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

Part: WINDSCREEN — CRACKED (RH) · airframe 51,399 hrs · 46,717 cycles

SUPPLEMENTAL CA FOR FO LOWER OUTSIDE EDGE OF WINDSCREEN CRACKED DECLARED EMERGENCY."TRANSFERRED TO NRWC 622-DFW-05541".-C/A-RAR THE FO,S WINDSHIELD IAW EMB145 AMM 56-10-01. OPS CHECK AND LEAK CHECK GOOD.

Part: LAMP — INOPERATIVE (RH) · airframe 51,271 hrs · 46,582 cycles

RH OVER WING EMERGENCY LIGHT INOP-C/A-RAR THE RH OVERWING EMERGENCY LT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: BATTERY — INOPERATIVE · airframe 50,963 hrs · 46,242 cycles

EMERGENCY FLOOR PROXIMITY STRIP LIGHTS INOP AT SEATS 1A THRU 7A.-C/A-RAR # 2 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHK GOOD.

Part: BATTERY — INOPERATIVE (RH) · airframe 50,963 hrs · 46,242 cycles

RH OVERWING AFT EMERGENCY LIGHT INOP.-C/A-RAR # 2 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHK GOOD.

Part: NONE — NONE · airframe 50,689 hrs · 45,924 cycles

AFT CABIN EMERGENCY FLASHLIGHT CLAMP BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT CLAMP IAW EMB 145 CMM 25-60-14.

Part: NONE — NONE · airframe 50,470 hrs · 45,658 cycles

FLIGHT ATTENDANT LED FLASHLIGHT INOP-C/A-RAR FLIGHT ATTENDANT LED FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPC GOOD.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 49,013 hrs · 43,994 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BRACKET BROKEN-C/A-DEFERRED PER MEL 25-32 AUTH# 030362M-C

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 48,856 hrs · 43,842 cycles

SERVICE DOOR EMERGENCY LIGHT HAS BROKEN WIRE. C/A-INSTALLED SPLICE TO SERVICE DOOR EMERGENCY LIGHT IAW SWPM 20-21-00. OPC GOOD. END.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 48,827 hrs · 43,817 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MISSING-C/A-RAR MISSING FA EMERGENCY FLASH LIGHT AS REQ NO MTX REQ. OP'S CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,805 hrs · 43,797 cycles

OVERWING EMERGENCY LIGHT ON ROW 12CB INOP-C/A-RAR LAMP ON OVERWING EMERGENCY LIGHT IN ROW 12CB ABOVE PASSENGER SEATS IN REF WITH EMB 145 AMM 33-50-07. OPS CHECK GOOD.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 48,497 hrs · 43,474 cycles

F/A AFT FLASHLIGHT MISSING. C/A: R & R AFT CABIN EMERGENCY FLASHLIGHT, REF AMM 33-50-16.

Part: A/C PACK — INOPERATIVE · airframe 48,301 hrs · 43,279 cycles

HAD PACK 1 VALVE CLOSED ADVISORY MESSAGE ON EICAS AND LATER IN CRUISE. FA REPORTED SMOKE IN THE CABIN DECLARED EMERGENCY. C/A: PERFORMED E145 FIM 21-20-00-810-801-A. FOUND PACK 1 AND 2 INOPERABLE, SEE ITEM 2 AND 3 OF THIS LOG PAGE FOR CONTINUED DISCREPANCY. NO SMOKE AT THIS TIME.

Part: DOOR SILL — CORRODED (FRAMES 15-18) · airframe 48,287 hrs · 43,260 cycles

SERVICE DOOR SILL HAS CORROSION. C/A REMOVED AND REPLACED SERVICE DOOR CENTER DOOR SILL, IAW EMB 145 SRM 51-40-02 AND ERS-EM-5300-4190. CENTER SILL PN: 145-22178-605.

Part: WEB — DAMAGED (CARGO DOOR) · airframe 48,287 hrs · 43,260 cycles

CARGO DOOR INNER WEBBING AFT NUTPLATE HOLE BLENDED BEYOND LIMITS. C/A: FABRICATED AND INSTALLED REPAIR DOUBLER ON CARGO DOOR INNER WEBBING AFT NUT PLATE HOLE, IAW EMB 145 SRM 52-30-01 FIG 213. MATERIAL FOR REPAIR DOUBLER PN: AL 7475-T761 (0.040 IN).

Part: WEB — DAMAGED (CARGO DOOR) · airframe 48,287 hrs · 43,260 cycles

CARGO DOOR INNER WEBBING LOWER NUTPLATE HOLE BLENDED BEYOND LIMITS. C/A: FABRICATED AND INSTALLED REPAIR DOUBLER ON CARGO DOOR INNER WEBBING LOWER NUTPLATE HOLE, IAW EMB 145 SRM 52-30-01 FIG 213. MATERIAL FOR DOUBLER PN: AL 7475-T761 (0.040 IN).

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 48,287 hrs · 43,260 cycles

CARGO FR 65 PREVIOUS SHEAR CLIP REPAIR HAS CORROSION NEAR STR 17L. C/A REMOVED AND REPLACED REPAIR SECTION OF CARGO FR 65 SHEAR CLIP, IAW EMB 145 SRM 53-31-04 FR 65 REPAIR SECTION SHEAR CLIP PN: 145-25175-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-60) · airframe 48,287 hrs · 43,260 cycles

RT LAV OMEGA BEAM CORRODED AT FWD NUTPLATE HOLE. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER ON RT LAV OMEGA BEAM AT FWD NUTPLATE HOLE, IAW ERS-EM-53MR-4186.

Part: DOOR SILL — CORRODED (FRAMES 64-68) · airframe 48,287 hrs · 43,260 cycles

CARGO DOOR ENTRANCE SILL IS CORRODED. C/A REMOVED AND REPLACED CARGO DOOR ENTRANCE SILL, IAW EMB 145 SRM 51-40-02 SILL PN: 145-25480-003.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 48,287 hrs · 43,260 cycles

EMERGENCY LIGHT STRIP NR 5 HAS BROKEN OFF CONNECTOR. C/A COMPLETE: INSTALLED SERVICEABLE CONNECTOR ON EMERGENCY LIGHT STRIP NR 5 AIRCRAFT SIDE, IAW EMB-145 SWPM 20-21-00. CALIBRATED EQUIPMENT USED: CRIMPER S/N SRM415. SEE BOW346682 FOR OPERATIONS CHECK.

Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 48,287 hrs · 43,260 cycles

STD-REQ A3265 OPS A-REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER EMB WC 33-700-19 CRJ WC 33-002 ETN-EM-25-385. P/N: 2013-1ASMI SN: 80045 POS: 3. C/A COMPLETE: REMOVED AND REPLACED NR 3 EMERGENCY LIGHTING BATTERY ASSY/BATTERY CHARGER, IAW ENVOY WC 33-700-19. OPERATIONS CHECK GOOD.

Part: SEAL — WORN (EMERGENCY LIGHT) · airframe 48,287 hrs · 43,260 cycles

LT EMERGENCY EXIT LOWER SEAL WORN. C/A COMPLETE: REMOVED AND REPLACED LT EMERGENCY EXIT LOWER SEAL, IAW EMB 145 AMM 52-21-01.

Part: PIN — CORRODED (EMERGENCY LIGHT) · airframe 48,287 hrs · 43,260 cycles

RT EMERGENCY EXIT LOWER FWD ALIGNMENT PIN CORRODED. C/A COMPLETE: REMOVED AND REPLACED RT EMERGENCY EXIT LOWER FWD ALIGNMENT PIN, IAW EMB 145 AMM 52-21-00, SEE TASK STEP 1 FOR RIG CHECK. RIG CHECK GOOD SEE BOW 346763 TASK STEP 9 FOR CABIN LEAKAGE CHECK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 48,287 hrs · 43,260 cycles

COCKPIT STEP PANEL EMERGENCY EXIT LIGHT WIRE IS BROKEN. C/A COMPLETE: R & R COCKPIT STEP PANEL EMERGENCY EXIT LIGHT, IAW EMB 145 AMM 33-50-13. SEE NRTC BOW346682 FOR OPERATIONS CHECKS.

Part: CONNECTOR — BROKEN (CABIN) · airframe 48,159 hrs · 43,121 cycles

FOUND EMERGENCY LIGHT STRIP CONNECTION BROKEN UNDER FLOOR BOARD PANEL 261BF. INSTALLED NEW CONNECTOR FOR EMERG LIGHT STRIP FLOOR PANEL 261BF IAW SWPM 20-50-01 OPC OF EMERG LIGHTS GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 48,159 hrs · 43,121 cycles

FLOORBOARD PANEL 261 BF PROXIMITY LIGHT STRIP BROKEN. INSTALLED NEW CONNECTOR FOR EMERG LIGHT STRIP FLOOR PANEL 261BF IAW SWPM 20-50-01 OPC OF EMERG LIGHTS GOOD.

Part: FASTENER — NOT REPORTED (ELECTRICAL SYS) · airframe 47,864 hrs · 42,851 cycles

SUPPLEMENTAL WITH NUMBER 2 ENGINE RUNNING, DURING APU START MULTIPLE DISPLAY FAILURES WITH EICAS MESSAGES ACCOMPANIED BY A STRONG ELECTRICAL BURNING FUME PRESENT. NO SMOKE NOTICED "TRANSFERRED TO NRWC 622-MIA-04026"-C/A-REMOVED AND REPLACED HARDWARE ON LEFT POWER DISTRIBUTION BOX SECURING POWER CABLES TO BUS TIE CONTACTOR INTERCONNECTION BAR IAW AMM 24-65-00 AND AMM 24-60-01. OPC OK. PERFORMED ETN-EM-72-034 NO DETECTABLE SMELL

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 47,733 hrs · 42,746 cycles

SUPPLEMENTAL FOUND CRACK ON AFT UPPER SIDE OF RH DV WINDOW FRAME. THIS HAS BEEN UPGRADED TO A MAJOR REPAIR.-C/A-REPAIRED CRACK ON AFT UPPER SIDE OF RH DV WINDOW FRAME IAW ERS-EM-53MR-4037 PART A. ( THERE WAS NO DECLARED EMERGENCY)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,667 hrs · 42,689 cycles

UPPER EXIT MARKER ON RH CABIN EMERGENCY DOOR SHROUD FAILS TO ILLUMINATE.-C/A-T/S IAW WM 33-50-50. REMOVED AND REPLACED #5 INVERTER IAW AMM 33-50-11. OPC GOOD.

Part: ACTUATOR — MALFUNCTIONED (PITCH TRIM) · airframe 47,414 hrs · 42,525 cycles

PTRIM MAIN INOP EICAS MESSAGE AFTER TAKEOFF "TRANSFERRED TO NRWC 622-MIA-03884"-C/A-ACCOMPLISHED REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR IAW EMB145 AMM 27-40-02, AND PERFORMED OPERATIONAL CHECKS. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,944 hrs · 42,138 cycles

DURING PS-2 FOUND RH EXIT MARKING SIGN INOP-C/A-INSTALLED RH EXIT MARKING SIGN ASSEMBLY IAW EMMB 145 AMM 33-50-14 OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 45,984 hrs · 41,286 cycles

DURING PS-1 CHECK FOUND EXIT ROW RH EMERGENCY LT INOP.-C/A-CANON PLUG CONNECTOR LOOSE. REATTACHED IAW STANDARD MAINTENANCE PRACTICES. FUNCTION CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 45,514 hrs · 40,850 cycles

NR 4 EMERGENCY FLOOR STRIP LIGHT CONNECTION WIRES BROKEN. C/A-REMOVED AND REPLACED NR 4 EMERGENCY FLOOR STRIP LIGHT ASSEMBLY IAW AMM 33-50-12. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — OUT OF ADJUST (CABIN) · airframe 43,862 hrs · 39,281 cycles

FA FLASHLIGHT INOP. C/A-COMPLETE:PERFORMED ADJUSTMENT OF THE FA FLASHLIGHT IAW AMM 33-51-01. FUNCTION CHECK GOOD.

Part: SKIN — CRACKED (FRAME 78) · airframe 43,293 hrs · 38,783 cycles

FUSELAGE SKIN HAS CRACKS AT FRAME 78 BETWEEN STRINGERS 6L - 8L. CUTOUT THE DAMAGE AND INSTALLED A DOUBLER.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 43,293 hrs · 38,783 cycles

LT OMEGA BEAM SUPPORT AT FR 29 HAS DAMAGED/ELONGATED FASTENER HOLES. R & R LT OMEGA BEAM SUPPORT AT FR 29. SUPPORTING DOCUMENTS EMAILED TO PROGMGR UNDER THE SUBJECT: SDR RAIA201802010002.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 43,292 hrs · 38,738 cycles

CARGO DOOR SILL CORRODED. R & R THE CARGO DOOR SILL..

Part: SKIN — CORRODED (FRAMES 60-61) · airframe 43,293 hrs · 38,783 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 60 - 61, STRINGER 20 - 21L. REPAIRED THE SKIN.

Part: BRACKET — CRACKED (FRAMES 28-29) · airframe 43,293 hrs · 38,783 cycles

BRACKET CRACKED UNDER THE LT OMEGA BEAM BETWEEN FRAMES 28 - 29. REPAIRED THE BRACKET, FOUND TO BE PART OF PREVIOUS REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 43,293 hrs · 38,783 cycles

FRAME 65 SHEAR TIE CORRODED AT THE BOTTOM. REPAIRED THE SHEAR TIE.

Part: FRAME — CRACKED (FRM 73) · airframe 43,293 hrs · 38,783 cycles

FRAME 73 IS CRACKED, UNDER THE FLOOR BOARD. R & R THE FRAME.

Part: YOKE — CRACKED (LT ENGINE) · airframe 43,293 hrs · 38,783 cycles

LEFT PYLON, FWD LOWER ENGINE YOKE, FWD BRACKET IS CRACKED. R & R THE YOKE FITTING.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 43,293 hrs · 38,783 cycles

CARGO DOOR EXTERIOR HANDLE CUTOUT HAS TWO CRACKS AT THE AFT END. PERFORMED A REPAIR.

Part: SKIN — DENTED (FRAME 32) · airframe 43,293 hrs · 38,783 cycles

CENTER FUSELAGE SKIN HAS A DENT ON THE FRAME 32 BETWEEN STRINGERS 1L - 2L. REPAIRED THE SKIN.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 43,293 hrs · 38,783 cycles

CARGO DOOR TOP CENTER FRAME IS CHAFED AT THE FWD UPPER CORNER. R & R THE CARGO DOOR TOP CENTER FRAME.

Part: SKIN — DENTED (FRAME 30) · airframe 43,293 hrs · 38,783 cycles

CENTER SKIN HAS A DENT AT FRAME 30 BETWEEN STRINGERS 6L - 7L. CUT OUT THE DAMAGE AND INSTALLED A FILLER & DOUBLER.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 43,100 hrs · 38,619 cycles

CAPTAINS EMERGENCY FLASHLIGNT DOES NOT ILLUMINATE. REPLACED FLASHLIGHT AND OPS CHECKED GOOD.

Part: UPLOCK — MALFUNCTIONED (MLG) · airframe 42,440 hrs · 38,037 cycles

POUNDING NOISE COMING FROM MAIN GEAR WHEN LANDING GEAR RETRACTED. LEFT MAIN GEAR SHOWING INTERMITTENT TRANSIT WHEN GEAR BROUGHT UP. R & R MAIN LANDING GEAR UPLOCK BOX, OPS CHECK GOOD. OPEN

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 41,648 hrs · 37,321 cycles

PRESSURE AUTO FAIL B AMBER ON CAPT ALT TO DASH LINE MAIN MODE. R&R DIGITAL CONTROLLER. R&R ELECTRO PNEUNIMATIC OUTFLOW VALVE. OPS CHECK GOOD.

Part: ROD END — BROKEN (UPLOCK ACTUATOR) · airframe 41,398 hrs · 37,118 cycles

RT MAIN LANDING GEAR DIDN'T COME UP EICAS MESSAGE. R & R THE RT MLG UNLOCKING ACTUATOR IAW 32-33-09. PERFORMED LANDING GEAR EXTENTION & RETRACTION IAW AMM 32-30-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BUSS — FAILED · airframe 39,480 hrs · 35,640 cycles

115 VAC BUSS FAIL AND GPWS, TERRAIN AND WINDSHEAR INOPERATIVE. RESET 115 AC SYSTEM AND OPS CHECK GOOD.

Part: SWITCH — FALSE INDICATION (E/E BAY DOOR) · airframe 38,967 hrs · 35,231 cycles

FWD AVIONICS ACCESS DOOR SHOWED OPEN AFTER TAKEOFF. . MAINTENANCE REPLACED SWITCH, OPS CHECK GOOD.

Part: PIN — DEFECTIVE (CABIN) · airframe 38,961 hrs · 35,225 cycles

LEFT OVERWING EMER EXIT, AFT EXIT LIGHT INOPERATIVE. R & R CONNECTOR PIN ON SPLICE SP9126 IAW AMM 33-50-00.

Part: WIRE — BROKEN (CABIN) · airframe 38,961 hrs · 35,225 cycles

LEFT NR 1 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE. REPAIRED BROKEN WIRE ON LT NR 1 FLOOR PROXIMITY LIGHT STRIP IAW SWPM 20-21-00.

Part: FRAME — CHAFED (FUSELAGE) · airframe 38,959 hrs · 35,223 cycles

FRAME 70, BETWEEN STRINGER 12R - 13R CHAFED. REPAIRED FRAME 70 BETWEEN STRINGER 12R - 13R IAW ERS-EM-53MR-1534R1. SEE WIPS & TASKS FOR FURTHER DETAILS.

Part: TRUNNION — DEFECTIVE (LT MLG) · airframe 38,959 hrs · 35,223 cycles

LEFT MLG AFT UPPER TRUNNION HAS DEFECT INDICATION ON OTBD LOWER VERTICAL TO HORIZONTAL TRANSITION AREA INBD SIDE, 400 KHZ, H-67, V-84, LPF 100. ACCOMPLISHED LT MLG AFT UPPER TRUNNION REPAIR IAW ERS-EM-57MR-494R1. SEE WIPS & TASK FOR DETAILS.

Part: CONNECTOR — MISSING (CABIN) · airframe 38,959 hrs · 35,223 cycles

WIRE FOR EMER LIGHT STRIP IS MISSING CONNECTOR AT FRAME 49. INSTALLED SERVICEABLE CONNECTOR ON EMER LIGHT STRIP WIRE AT FRAME 49 IAW SWPM 20-21-00 & SWPM 20-50-01. SEE BOW 198917 FOR OPERATIONS CHECK. FOUND DURING CLOSE-UP.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,959 hrs · 35,223 cycles

SERVICE DOOR CUT OUT FRAME 20 CORRODED BELOW LOWER DOOR ROLLER. REPAIRED SERVICE DOOR CUT OUT ON FRAME 20 BELOW LOWER DOOR ROLLER IAW ERS-EM-53MR-1538.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,959 hrs · 35,223 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" LONG. EASI 8071 USED WITH A 100-500KHZ PROBE, 400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. FUSELAGE SKIN CRACK REPAIRED IAW ERS-EM-53MR-1566. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,959 hrs · 35,223 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75 AT THE FIRST TWO FASTENERS BELOW STRINGER 2R. CRACKS ARE APPROX 1/4" LONG. REPAIRED IAW ERS EM-53MR-1567. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: WIRE — BROKEN (CABIN) · airframe 38,959 hrs · 35,223 cycles

CABIN EMER LIGHT STRIP NR 3, WIRE IS BROKEN. R & R CABIN EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. SEE BOW 198917 FOR FINAL INSTALLATION & OPERATIONAL TEST OF THE EMER STRIP LIGHTS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 38,916 hrs · 35,179 cycles

CAPTAIN`S FLASHLIGHT NOT WORKING INOPERATIVE. FLIGHT CREW PLACARDED IAW MEL 2553. REMOVED AND REPLACED CAPT'S FLASHLIGHT AND CRADLE ASSY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPC GOOD MEL RESTORED END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,804 hrs · 35,078 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT BULB IAW AMM 33-50-09. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,604 hrs · 34,876 cycles

FORWARD CABIN FLASHLIGHT WILL NOT CHARGE PROPERLY. R & R FWD CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LUG — GOUGED (LT AILERON) · airframe 37,974 hrs · 34,313 cycles

LEFT AILERON PCA ROD END MOUNT HAS 2 GOUGES. LT SIDE OF MOUNT GOUGE .0215 DEEP X .0730 H X .1645 L. RT SIDE OF MOUNT GOUGE .0160 X .140 H X .1825 L. ACCOMPLISHED PERMANENT REPAIR OF LT PCA ATTACH LUGS IAW ERS-EM-27MR-039.

Part: GEARBOX — DAMAGED (RT ENGINE) · airframe 36,904 hrs · 33,423 cycles

RIGHT ENG AGB PMA SHAFT RADIAL MOVEMENT OUT OF LIMITS SEE NRWC 622-DFW-02143. R & R RT ENG AGB IAW AMM 72-61-01 & RR MM 72-63-10. OPERATIONS & LEAK CHECKS GOOD.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 36,754 hrs · 33,280 cycles

EICAS DISPLAYED E1 HYD PUMP FAIL AS WELL AS HYD SYS 1 FAIL. HYD FLUID QTY SHOWED IN AMBER RANGE. AOM PROCEDURES COMPLIED WITH. PRESS FLUCTUATIONS WERE OBSERVED BETWEEN 2300 - 300 PSI. R & R NR 1 ENG EDP HYD OPERATIONAL & LEAK CHECKED OK IAW AMM 29-10-03.

Part: TIRE — SEPARATED (LT MLG) · airframe 36,682 hrs · 33,212 cycles

LEFT MAIN INBD TIRE TREAD SEPARATED FROM TIRE. PERFORMED LG TIRE TREAD FAILURE INSPECTION CHECK IAW AMM 05-50-15. R & R NR 2 MLG WHEEL & TIRE ASSEMBLY IAW WC 32-700-11.

Part: BATTERY — OVERTEMP (MAIN) · airframe 36,636 hrs · 33,167 cycles

BATTERY 2 OVER TEMP. R & R NR 1 & 2 MAIN BATTERIES IAW WC 24-600-00. OPERATIONS CHECKED GOOD. NO MSG NOTED. LT PN 32248-001 & SN 10800544.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 36,370 hrs · 32,932 cycles

DURING TAKEOFF ROLL AFTER ENGINE SPOOL UP, THE COCKPIT & FWD CABIN FILLED WITH SMOKE. TROUBLESHOT IAW FIM 79-37-00, FOUND OIL IN LT ENGINE WATER WASH PORT. NO EVIDENCE OF OIL LEAKAGE FOUND AT CARBON SEAL AREA. NO OIL LEAKAGE FOUND AT FRONT SUMP BOLT HEADS IAW ETN-EM-79-014. R & R RT RECIRCIRULATION FAN IAW AMM 21-24-01, OPS CHECKED GOOD. R & R NR 1 ENGINE IAW WC 71-00-00. COMPLETED ENGINE CHANGE STEPS 5 ITEM R THRU CLOSE UP IAW AE WORK CARD 71-000-00. OPS & LEAK CHECKED GOOD IAW NRWC-622-DFW-2010 ITEM 1.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,563 hrs · 32,328 cycles

FLIGHT ATTENDANT REPORTS REAR FLASHLIGHT INOPERATIVE. SECURED IAW AMM 33-50-16, OPERATIONS CHECKED GOOD, NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,769 hrs · 31,695 cycles

RT FWD FUSELAGE EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD IAW AMM 33-50-10.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 34,427 hrs · 31,391 cycles

THE CREW REPORTED THAT AT FL 320 WITH AUTOPILOT ENGAGED, WE RECEIVED EICAS "AP ELEV MISTRIM". THE CREW DISCONNECTED THE AUTOPILOT AND SHORTLY AFTER RECEIVED EICAS "PTRIM MAIN INOP". THE CREW DECLARED AN EMERGENCY AND UTILIZED BACKUP PITCH TRIM FOR LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE HORIZONTAL STAB ACTUATOR IAW AMM 27-40-02. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,425 hrs · 31,388 cycles

FLOOR EMERGENCY PROXIMITY LIGHTS 2 AND 3 INOPERATIVE. R & R BATTERY PACK AND CHARGER IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: SKIN — TORN (RUDDER) · airframe 34,425 hrs · 31,388 cycles

AFT RT EDGE OF RUDDER 1 CRACKED/ TORN. CUT-OUT DAMAGE, FABRICATE AND INSTALLED REPAIR DOUBLER, FILLER IAW EO-EM-53MR-438.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,425 hrs · 31,388 cycles

FUSELAGE SKIN BETWEEN FRAME 13-14 AND BETWEEN STRINGERS 19L-19R ON INSIDE CORRODED. EO-EM-53MR-2190, PART A WAS SATISFACTORY ACCOMPLISHED.

Part: STRUCTURE — CRACKED (E/E BAY DOOR) · airframe 34,425 hrs · 31,388 cycles

REAR ELECTRONICS COMPARTMENT DOOR INNER EDGE CRACKED AROUND 2 RIVETS ON UPPER MOUNTING CLIP. REPAIRED CRACK IAW EO EM-52MR-366. WC 52-200-07, CRACK LENGTHS .20, .23, .30, .25.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,425 hrs · 31,388 cycles

SERVICE DOOR BOTTOM EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,425 hrs · 31,388 cycles

EMERGENCY LIGHT NR 2 & 3 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY BATTERY.

Part: LINER — OUT OF POSITION (EMERGENCY EXIT) · airframe 34,425 hrs · 31,388 cycles

RT EMERGENCY EXIT HARD TO OPEN. REMOVED AFT UPPER SCREW OF RT EMERGENCY EXIT LINING, REPOSITIONED LINING, AND REINSTALLED AFT UPPER SCREW OF RT EMERGENCY EXIT LINING IAW AMM 25-23-03.

Part: HOLDER — MALFUNCTIONED (BATTERY) · airframe 34,425 hrs · 31,388 cycles

LIGHT STRIP NR 2 & NR 3 INOPERATIVE. REMOVED BATTERY HOLDER ASSY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,445 hrs · 31,412 cycles

CORROSION ON SHEAR TIE 65 AT CARGO DOOR CUTOUT BETWEEN 16L-18L. REPAIRED SHEAR TIE FRAME 65 IAW AEA EO EM-53MR-1129, PART A.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 34,425 hrs · 31,388 cycles

SERVICE DOOR EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW AMM 33-50-10, OPS CHECKED GOOD IAW AMM 33-50-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 34,169 hrs · 31,175 cycles

DURIING MX INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: ACM — FAULTY (AC BAY) · airframe 33,895 hrs · 30,938 cycles

THE CREW REPORTED THAT DURING CRUISE THEY NOTICED SMOKE AND FUMES IN THE COCKPIT AND CABIN OVER SPS ENROUTE. THE CREW DECLARED AN EMERGENCY AND DIVERTED. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT IAW ETN-EM-72-034. INSPECTION FOUND CABIN/COCKPIT NR 2 AIR CYCLE MACHINE RUBBING AND GRINDING. R & R THE NR 2 AIR CYCLE MACHINE IAW AMM 21-51-03. THE OPS CHECK WAS GOOD IAW AMM 21-51-00. THE ACFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 33,709 hrs · 30,781 cycles

ON FLIGHT 3280 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BOTH UPPER AND LOWER AFT DOOR ROLLERS FROZEN. LUBRICATED AND PERFORMED AN OPERATIONAL CHECK AS PER 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSECURE (CABIN) · airframe 33,550 hrs · 30,665 cycles

ON FLIGHT 3597 THE CREW REPORTED THE FLASHLIGHT ABOVE THE FLIGHT ATTENDANT SEAT WAS NOT SECURED AND DID NOT SHOW THAT IT WAS ALWAYS CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESCURED THE FLIGHT ATTENDANT SEAT FLASHLIGHT IAW EMB 145 MM 25-60. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 33,535 hrs · 30,655 cycles

ON FLIGHT 3494 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR AS PER EMB 145 AMM 52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 33,461 hrs · 30,602 cycles

ON FLIGHT 4074 THE CREW REPORTED THE AFT CABIN FLASHLIGHT FALLS OUT OF ITS MOUNT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CREW FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 33,123 hrs · 30,340 cycles

WHILE TROUBLESHOOTING HYDRAULIC SYSTEM 1 PUMP FAIL FOUND LEFT GROUND SPOILER ACTUATOR CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HYDRAULIC PUMP & THE GROUND SPOILER ACTUATOR: PART # 3604401003. ALSO REMOVED AND REPLACED O-RING: PART # NAS1611-014A. O-RING: PART # NAS1612-4A. O-RING: PART # NAS1612-8A. PACKING: PART #NAS1612-10A. O-RING: PART # SDI3030290-113. GASKET: PART # AS3492-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — INOPERATIVE (RT WING TE FLAPS) · airframe 32,852 hrs · 30,145 cycles

FLIGHT 2763. CREW REPORTED ON DESCENT, ATTEMPTED TO SELECT FLAPS 9. RECEIVED AN EICAS FLAP FAIL MESSAGE. CAPTAIN RAN APPROPRIATE CHECKLIST AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED FROM SERVICE. PERFORMED ANTI-ICE SYSTEM OPS CHECKS AND WERE FOUND TO BE GOOD AMM 30-00-00. NO DISCREPANCIES NOTED. REMOVED AND INSTALLED RIGHT HAND FLAP VELOCITY SENSOR IAW MM 27-51-12. OPS CHECKED GOOD. NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — UNSERVICEABLE (TE FLAP) · airframe 32,856 hrs · 30,148 cycles

ON FLIGHT 3283 THE CREW REPORTED THAT ON APPROACH THEY SELECTED FLAPS 9 AND GOT A FLAP FAIL MSG - FLAPS STAYED AT 0. THE AIRCRAFT WAS REMOVED FROM SERVICE. CMC = FLAP JAMMING WITH PREVIOUS MESSAGES OF RIGHT SENSOR FAIL. REMOVED AND REPLACED RIGHT TRANSMISSON BRAKE IAW AMM CH 27-51-01. BRAKE FCK CHECK OK IAW AMM CH 27-51-01. FLAP SYSTEM OPS CHECK OK IAW AMM CH 27-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 32,849 hrs · 30,142 cycles

ON FLIGHT 3393 THE CREW REPORTED THAT ON APPROACH TO AMA AND AFTER SELECTED FLAPS 9, THEY RECEIVED A FLAP FAIL EICAS MESSAGE. EICAS WAS INDICATING 0 FLAPS. THE CREW FOLLOWED EMERGENCY FLAP FAIL PROCEDURES. THE CREW DECLARED AN EMERGENCY AND REQUESTED CRASH, FIRE & RESCUE. THE AIRCRAFT LANDED WITH INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND RESET FLAPS PER FIM 27-50-00. PERFORMED OPERATIONAL CHECK IAW AMM 27-50-00 AND THE SYSTEM CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 32,798 hrs · 30,098 cycles

ON FLIGHT 3226 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPT'S FLASHLIGHT IAW EMB 145 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 32,246 hrs · 29,656 cycles

ON FLIGHT 2775 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT ON/OFF SWITCH WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 32,130 hrs · 29,566 cycles

ON FLIGHT 3302 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS MISSING THE ON/OFF SWITCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 31,987 hrs · 29,444 cycles

ON FLIGHT 3229 THE CREW REPORTED THAT WHILE TAXIING RECEIVED A MASTER WARNING CHIME WITH THE BAGGAGE SMOKE WARNING ON EICAS ASSOCIATED WITH THE ILLUMINATION OF THE BUTTON ON THE OVERHEAD PANEL. THEY CREW RAN EPC/AOM CHECKLIST AND ADVISED THE GROUND OF FIRE EMERGENCY AND HAD CRASH, FIRE AND RESCUE TO MEET AIRCRAFT ON TAXI WAY. CFR FOUND NO EVIDENCE OF FIRE OR SMOKE AND THE AIRCRAFT WAS CLEARED TO TAXI TO THE GATE WHILE THEY FOLLOWED. THE PASSENGERS DEPLANED NORMALLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR IAW EMB-145 AMM 26-15-01 AND THE OPERATIONAL TEST WAS GOOD REF AMM 26-15-00. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,916 hrs · 29,401 cycles

DURING B INSPECTION FOUND THE AFT AISLE CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 31,736 hrs · 29,254 cycles

FLIGHT 3343, FLIGHT ATTENDANT REPORTED MAIN DOOR WAS HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBED MAIN DOOR HINGE AND ROLLER. OPS CHECKED GOOD IAW 52-10-00 AMM. AIRCRAFT RETURNED TO SERVICE.

Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 2,773 hrs · 29,038 cycles

DURING B INSPECTION, FOUND WALL EMERGENCY LIGHT AT SEAT 12C HAS MISSING SCREW. AIRCRAFT REMOVED FROM SERVICE. INSTALLED LOWER FORWARD SCREW INTO WALL EMERGENCY LIGHT FRAME IAW AMM 33-50-14. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,362 hrs · 28,949 cycles

ON FLIGHT 4219 THE FLIGHT ATTEDANT REPORTED THE PASSENGER ENTRY DOOR WAS DIFFICULT TO OPEN/CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR ROLLERS IAW EMB 145 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. ALSO REMOVED SECURITY TAPE FROM INSIDE DOOR SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,100 hrs · 28,729 cycles

DURING B INSPECTION, FOUND THE COCKPIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BUTTON — UNSECURE (COCKPIT) · airframe 30,608 hrs · 28,348 cycles

ON FLIGHT 3529 THE CREW REPORTED THEY WERE UNABLE TO ENGAGE AN LATERAL FLT DIR MODE ROLL, HDG, NAV VSI & SPD MODES WORKED INTERMITTENTLY AL HOLD WORKED. THE CREW ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED PUSH BUTTONS ON SWITCHES ROLL, HOG , NAV, VSI, SPD IAW AMM 22-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 30,265 hrs · 28,096 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT FLOOR STRIPS NR 2 & NR 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 30,265 hrs · 28,096 cycles

DURING B-INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. (EXTERNAL) THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EXTERNAL LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,230 hrs · 28,071 cycles

DURING MAINTENANCE INSPECTION FOUND THE 3 AFT FLOOR SECTIONS OF EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT BATTERY AND CHARGER IAW EMB 145 AMM 30-50-04. THE OPERATIONAL CHECK WAS OK IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,018 hrs · 27,926 cycles

ON FLIGHT 2724 THE CREW REPORTED THEY RECEIVED A FLAP FAIL CAUTION DURING APPROACH UPON SELECTING FLAPS 9 DEGREE FLAPS REMAINED AT 0. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP ZERO RIG THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VELOCITY SENSOR — MALFUNCTIONED (TE FLAP) · airframe 29,974 hrs · 27,897 cycles

ON FLIGHT 2938 ON THE APPROACH THE CREW REPORTED THEY SELECTED FLAPS TO NINE DEGREES AND GOT A FLAP FAIL MESSAGE. FLAPS WERE AT ZERO AND WOULD NOT MOVE. COMPLIED WITH AOM PROCEDURES AND LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT FLAP VELOCITY SENSOR IAW EMB 145 AMM 27-51-12, PERFORMED OPERATIONAL CHECKS. THE OPERATIONAL CHECKS WERE GOOD, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WING) · airframe 29,956 hrs · 27,880 cycles

ON FLIGHT 4296 THE CREW REPORTED THE WING ANT-ICE FAILED DURING TEST ON CLIMBOUT. THE CREW ELECTED TO RETURN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED CMC FOR ASSOCIATED MESSAGES FOR WING A/I. PERFORMED ANTI-ICING SYSTEM OPERATIONAL TEST IAW EMB 145 AMM 30-00-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS OR ASSOCIATED CMC MESSAGES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLEX DRIVE — INOPERATIVE (TE FLAP) · airframe 29,955 hrs · 27,879 cycles

THE CREW REPORTED THE RECEIVED A FLAP FAIL MESSAGE DURING DESCENT INTO GRR. THE CREW DECLARED AN EMERGECNY AND DIVERTED TO ORD DUE TO DEGRADE BRAKING CONDITIONS IN GRR. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE NR 3 LEFT FLEXIBLE SHAFT IAW AMM 27-51-06. (LEFT WING) THE OPERATIONAL FLAP SYSTEM CHECK WAS GOOD IAW AMM 27-51-00. THE FLAP CONTROL SYSTEM CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,845 hrs · 27,806 cycles

DURING UNSCHEDULED MAINTENANCE VISIT TROUBLESHOT AN ODOR COMING FROM AROUND ROW 16 POSSIBLY FROM A BLEED OR PACK BECAUSE IT WAS ISOLATED NR 2 BY TURNING NR 2 BLEED & PACK ODOR WENT AWAY WHILE IN CRUISE FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN #EM-72-034R4 ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. NO DEFECTS NOTED AT THIS TIME WITH NR 2 PACK OR NR 2 BLEED SYSTEM. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 29,758 hrs · 27,742 cycles

DURING MAINTENANCE BASE INSPECTION THE BATTERY FAILED THE EMERGENCY LIGHT CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — INOPERATIVE (TE FLAP) · airframe 29,664 hrs · 276,772 cycles

ON FLIGHT 4142 ON APPROACH THE CREW REPORTED THEY RECEIVED A CAPTAINS PITCH TRIM FAIL MESSAGE AND FLAP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S CONTROL YOKE PITCH TRIM SWITCH IAW EMB 145 AMM 27-40-03. THE OPERATIONAL CHECK WAS GOOD. PERFORMED GENERAL VISUAL INSPECTION OF FLAP MECHANICAL LINE NO DEFECTS NOTED. PERFORMED LEFT FLAP VELOCITY SENSOR ELECTRICAL TEST FOUND SENSOR GOOD AS PER FIM 27-51-00-810-816-A. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB 145 AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD. COULD NOT DUPLICATE THE MESSAGE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRIVE UNIT — FAILED (TE FLAP) · airframe 29,663 hrs · 27,671 cycles

ON FLIGHT 4190 THE CREW REPORTED THAT ON APPROACH THEY HAD A FLAP FAIL. THE CREW DECLARED AND EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP DRIVE UNIT IAW EMB AMM 27-53-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DEFECTIVE (AC BAY) · airframe 29,272 hrs · 27,377 cycles

ON FLIGHT 3335 THE CREW REPORTED, DURING CRUISE HAD A GRADUAL LOSS OF PRESSURE AND COULD NOT MAINTAIN CABIN ALTITUDE. THE CREW ELECTED TO DIVERT TO SGF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SLEEVE CLAMPS AT NR 1 HEAT EXCHANGER & DUAL TEMPERATURE CONTROL VALVE TUBE NR 1 IAW EMB AMM 21-60-01 & EMB AMM 21-51-02. THE PRESSURE CONTROL SYSTEM TESTS WERE GOOD IAW EMB AMM 21-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — DAMAGED (LANDING GEAR) · airframe 29,190 hrs · 27,313 cycles

FOR FLIGHT 2807 DURING THE POST FLIGHT INSPECTION THE CREW FOUND THE NR 1 TIRE SHREADED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 WHEEL AND TIRE ASSEMBLY IAW WORK CARD 32-700-11 AND COMPLIED WITH BRAKE ASSEMBLY INSPECTION IAW AE WORK CARD 32-700-18. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 29,165 hrs · 27,291 cycles

FOR FLIGHT 2704 TEN MINUTES AFTER NR 1 ENGINE SHUTDOWN RESIDUE WHITE SMOKE WAS STILL COMING OUT OF REAR END OF ENGINE DURING POST FLIGHT. THE SMOKE WAS NOTICED BY CREW AND RAMPERS. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED LEFT ENGINE CHANGE IAW WORK CARD 71-000-00. ALL OPERATIONAL AND LEAK CHECKS WERE NORMAL. REFERENCE NRWC 622-DFW-00501. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 28,640 hrs · 26,860 cycles

ON FLIGHT 3505 THE CREW REPORTED THAT DURING THE CLIMB RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. THE CREW NOTICED THE CABIN WAS LOOSING PRESSURIZATION. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS AT JOINTS 17 LEFT LATERAL AFT OF THE CARGO BLEED DUCT IAW AE W/C 36-000-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — INOPERATIVE (NR 3 BRAKE) · airframe 28,621 hrs · 26,844 cycles

ON FLIGHT 4180 THE CREW REPORTED THAT DURING LANDING RECEIVED A BRAKE DEGRADE MESSAGE ON EICAS. THEY REPORTED VERY WEAK BRAKING WITH SLOW DESELECTION. BOTH OUTBOARD BRAKE TEMPERATURE INDICATIONS WERE HIGH IN THE AMBER RANGE BOTH INBOARD LOW GREEN RANGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BRAKE TRANSDUCER IAW EMB AMM 32-41-03. THE OPERATIONAL CHECK WAS GOOD, NO MESSAGES NOTED. P/N OFF 140197, S/N OFF 543, P/N ON 140197, S/N ON 1054

Part: FCU — MALFUNCTIONED (TE FLAP) · airframe 28,473 hrs · 26,745 cycles

ON FLIGHT 3310 THE CREW REPORTED THAT DURING APPROACH RECEIVED A FLAP FAIL MESSAGE ON EICAS, THE FLAPS ARE WERE INOPERABLE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB 145 27-53-02 AMM. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 28,465 hrs · 26,741 cycles

ON FLIGHT 2807 THE CREW REPORTED THAT ON APPROACH TO LANDING SELECTED FLAPS 9 DEGREES AND IMMEDIATELY GOT A FLAP FAIL EICAS MESSAGE. THE FLAP STUCK AT 0 DEGREES. THE CREW FOLLOWED AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP SYSTEM RESET PER EMB 145 FIM 27-51-00-810-804-A. FOUND TO BE IN A TRANSITORY CONDITION. THE FLAP SYSTEM OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC LINE — RUPTURED (NR 1 ENGINE) · airframe 27,434 hrs · 26,000 cycles

ON FLIGHT 3931 DURING DESCENT THE CREW REPORTED A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE FOLLOWED BY HYDRAULIC SYSTEM 1 FAIL. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND PRESSURE LINE FROM NR 1 ENGINE HYDRAULIC PUMP RUPTURED. REMOVED AND REPLACED PRESSURE HOSE IAW STANDARD MAINTENANCE PRACTICES 20-10-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — INOPERATIVE (TE FLAP) · airframe 26,676 hrs · 25,402 cycles

ON FLIGHT 3650 DURING THE DESCENT THE CREW REPORTED A FLAP FAIL ON EICAS WHEN SELECTING FLAPS AT 22 DEGREES. FLAP FAIL CAUTION ILLUMINATED AND FLAPS INDICATED 11 DEGREES. RETRACTED FLAPS TO 0 DEGREES AND STILL INDICATED 11 DEGREES ON THE GROUND. CYCLED FLAPS 22 DEGREES AND BACK TO 0 FLAPS INDICATED 11 DEG. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP MOTOR UNIT AMM 37-53-01 FLAP ELECTRONIC CONTROL UNIT IAW EMB AMM 27-53-02 AND FUSE IAW EMB STANDARD PRACTICES TASK 20-13-08-200-801-A AND TASK 20-13-08-420-001 A00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,988 hrs · 24,856 cycles

FOR FLIGHT 4057 WHILE ON THE GROUND THE CREW NOTICED A BURNING ODOR. THE ODOR SMELLED LIKE FISHY BURNING PLASTIC. NO VISIBLE SMOKE WAS NOTICED. THE ODOR APPEARED ONLY IN THE COCKPIT. PASSENGERS ON BOARD DID NOT SEEM TO NOTICE ANY BURNING ODORS. THE CREW DID NOT RECEIVE ANY EICAS MESSAGES. THE AUXILIARY POWER UNIT AND WINDSHIELD HEAT WERE BOTH OFF, PACKS WERE ON. THE ODOR DISSIPATED AFTER SHUTTING DOWN ENGINES. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE INSPECTED COCKPIT AND COMPONENTS FOR ANY TYPE OF ODOR. GROUND RAN AIRCRAFT FOR 30 MINUTES WITH PACK NR 1 ON AND OFF. NO BURNING SMELL NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,943 hrs · 24,822 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BULB IAW EMB AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,943 hrs · 24,822 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT FLOOR STRIP AT PASSENGER SEATS 8 AND 9 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 25,888 hrs · 24,780 cycles

FOR FLIGHT 3659 DURING THE PREFLIGHT INSPECTION THE FLIGHT ATTENDANT FOUND THE FORWARD PERSONAL BREATHING EQUIPMENT FOIL POUCH TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PERSONAL BREATHING EQUIPMENT AT THE FORWARD CABIN. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,462 hrs · 24,430 cycles

FOR FLIGHT 3272 DISPATCH REPORTED THE AIRCRAFT WAS RETURNING TO PIA WITH A LIGHTNING STRIKE FOLLOWED BY A SLIGHT ELECTRICAL SMELL THAT WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW MAINTENANCE WORK CARD 05-200-00. FOUND LIGHTNING STRIKE-3 RIVETS WITH LIGHTNING STRIKE DAMAGE ON CENTER FUSELAGE II BETWEEN FRAMES 30 & 33 AND BETWEEN STRINGERS 6L & 7L. PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE ON CENTER FUSELAGE II LT IAW E.O. EM-5300-1486 PT. B ON OR BEFORE 10FC. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 24,962 hrs · 24,035 cycles

DURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE CARGO DOOR CUTOUT FORWARD SHEAR CLIP CORRODED AT THE LOWER CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE SHEAR CLIP IAW EO EM-53MR-1129. THE CORROSION LEVEL WAS DETERMINED TO BE LEVEL 1, BUT CONSIDERED TO BE A REPORTABLE REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,962 hrs · 24,035 cycles

DURING MAINTENANCE BASE HEAVY CHECK FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 38 AND FRAME 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM WITH DOUBLER REPAIRS IAW EMB SRM 53-00-10 AND EO EM-5300-1149. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,962 hrs · 24,035 cycles

DURING THE MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 38 AND FRAME 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM WITH DOUBLER REPAIRS IAW EMB SRM 53-00-10 AND EO EM-5300-1149. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,962 hrs · 24,035 cycles

DURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM WITH A DOUBLER IAW EMB SRM 53-00-10 AND EO EM-5300-1149. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — GOUGED (AILERON) · airframe 24,962 hrs · 24,035 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON PCA BRACKET GOUGED ON THE INSIDE OF THE OUTBOARD BUSHING HOUSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,962 hrs · 24,035 cycles

DURING MAINTENANCE BASE HEAVY CHECK FOUND THE CENTER OMEGA BEAM AT FRAME 29 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,962 hrs · 24,035 cycles

DURNG MAINTENACE BASE HEAVY CHECK FOUND THE LEFT HAND OMEGA BEAM CORRODED AT FRAME 29 AND AT 33. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORROSION LEVEL IS INDICATED AS LEVEL 2. REPAIRED THE OMEGA BEAM AT FRAME 29 AND FRAME 33 WITH DOUBLER REPAIR IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,612 hrs · 22,947 cycles

ON PS CHECK CENTER CABIN OVERHEAD EXIT SIGN FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN OPS CHECK GOOD. ACFT RETURN TO SERVICE.

Part: DUCT — ODOR (CABIN DIST) · airframe 20,316 hrs · 20,026 cycles

ON FLIGHT 3786 CREW DIVERTED TO MSY, FLIGHT ATTENDANT REPORTING PLASTIC BURNING ODOR AND GREY HAZE IN CABIN. NO WARNING MESSAGES OF ANY KIND. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT UNDER SEAT 7-8BC MELTED FROM NR 2 PACK. REMOVED AND REPLACED SERVICEABLE NR 2 PACK INTAKE DUCT IAW AMM 21-20-05 UNDER SEAT 7-8BC.& 8194; AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — OVERHEATED (NR 1) · airframe 20,221 hrs · 19,906 cycles

ON FLIGHT 3475, NUMBER ONE PACK OVERHEATED SMOKE IN CABIN AND COCKPIT. SMOKE LASTED 20 SECONDS. PACK OVERHEAT LASTED 3 SEC. REMOVED AND REPLACED NUMBER TWO ENGINE PER AE W/C 71-000-00, OPS AND LEAK CHECK GOOD. RELEASED FROM TRIAD. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — SMOKE (NR 2) · airframe 20,191 hrs · 19,877 cycles

PACK NR 2 FED BY APU CAUSED SMOKE IN CABIN AND COCKPIT. REMOVED AND REPLACED NR 2 ACM IAW 21-51-03, OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ANTI-ICE SYSTEM — NO TEST · airframe 20,176 hrs · 19,861 cycles

AIR TURN BACK DUE TO WING A/I FAIL AND EXPECTING ICE CONDITIONS REROUTE. PERFORMED ICE TEST AIRBORNE ALL OK EXCEPT WING A/ICE FAIL. PERFORMED OPS CHECK WING A/ICE SYSTEM IAW EMB 145 AMM 30-10-00. COULD NOT DUPLICATE THIS PROBLEM AT THIS TIME. NO PARTS CHANGED, AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,852 hrs · 19,576 cycles

EN ROUTE TO CRP FLIGHT ATTENDANT NOTICED BURNING ODOR IN CABIN. FLIGHT DIVERTED TO AUS. LANDED UNEVENTFULLY. EMERGENCY WAS DECLARED. DID NOT LAND OVERWEIGHT. PERFORMED OPS CHECK OF A/C COOLING SYSTEM IAW AMM 21-20-00 RAN BOTH PACKS ON APU BLEED FOR 1 HR OPS CHECK WERE GOOD NO SMOKE IN COCKPIT OR CABIN. RAN BOTH PACKS FOR 1HR ON ENG BLEEDS AGAIN COULD NOT DUPLICATE SMOKE PROBLEM. CHECKED BOTH ENG FOR LEAKS NO INTERNAL OR EXTERNAL LEAKS NOTED AT THIS TIME. REMOVED FLOOR BOARDS IN CABIN INCEPTED AC DUCTS NO DEFECTS FOUND. FUNCTIONAL CHECK FLIGHT PASSED SATISFACTORY AIRCRAFT RETURN TO SERVICE.

Part: FIXTURE — ODOR (CABIN LIGHTS) · airframe 19,745 hrs · 19,485 cycles

ON TAXI IN, PAX AND FLIGHT ATTENDANT NOTICED A BURNING ODOR AROUND ROW 3. REMOVED AND REPLACED LIGHTNING FIXTURE IAW AMM 33-21-06. MEL RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 19,279 hrs · 19,055 cycles

RECEIVED AIR/GROUND FAIL MESSAGE AND GEAR HANDLE STUCK IN DOWN POSITION - RETURNED TO BNA. PERFORMED AIR/GROUND SYSTEM SIMULATION IAW EMB 32-63-00 AND LANDING GEAR EXTENSION AND RETRACTION IAW EMB 32-30-00 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR HANDLE IAW EMB 32-30-00. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — FAILED (GALLEY LIGHT)

DFW - FLT 3519 - REPORTED AN ELECTRICAL/BURNING ODOR IN THE CABIN AT THE GATE. REMOVED AND REPLACED GALLEY LIGHT BALLAST, IAW AMM 33-20-00. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. PREPARED A FILLER DOUBLER, SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

DFW - FLT 3533 - FOUND EMERGENCY EXIT LIGHT ABOVE GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT LOCATOR IAW EMB MM 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEARING — WORN (HORIZONTAL STAB)

DURING MBV INSPECTION, THE RT AND LT HORIZONTAL STABILIZER HINGE BEARINGS WERE FOUND TO HAVE PLAY. REMOVED AND REPLACED RT AND LT HORIZONTAL TO VERTICAL SPHERICAL BEARINGS IAW MFG AMM AND SB.

Part: THRUST REVERSER — CRACKED (RT ENGINE)

DURING MBV INSPECTION THE RT THRUST REVERSER HAS APPROXIMATE 3 INCH CRACK AT THE FORWARD LOWER OB SECTION. REPAIRED CRACK IAW MFG SRM.

Part: SKIN PANEL — BIRD STRIKE (FUSELAGE)

DURING MBV INSPECTION THE LT FORWARD FUSELAGE SKIN DAMAGED FROM BIRD STRIKE. REPLACED DAMAGED SKIN IAW SRM.

Part: CHANNEL — WORN (FUSELAGE)

DURING MBV INSPECTION THE SERVICE DOOR SILL BETWEEN FRAMES 20 AND 22 RT SIDE WAS FOUND CORRODED. REMOVED AND REPLACED THE CHANNEL IAW MFG SRM.

Part: BUSHING — WORN (HORIZONTAL STAB)

DURING MBV INSPECTION THE LT HORIZONTAL STABILIZER OB BUSHING WAS FOUND TO BE MIGRATING. REPLACED BUSHINGS IAW MFG SRM.

Part: LANDING GEAR — MALFUNCTIONED (RIGHT)

OMA - FLT 4108 - AFTER TAKEOFF, THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE WHEN GEAR HANDLE WAS SELECTED UP. THE RIGHT MLG DID NOT RETRACT. CREW RETURNED TO OMA WITH NO FURTHER INCIDENTS REPORTED. CFR DID RESPOND. (M)

Part: BEAM — ELONGATED (FRAME 20)

DURING AN IMBV INSPECTION FOUND CENTER BEAM UPRIGHT AT FRAME 20 HAD AN ELONGATGED HOLE. REMOVED DAMAGED UPRIGHT. FRABRICATED A SERVICEABLE UPRIGHT IAW STANDARD SRM PRACTICES.

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION MAINTENANCE, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM. REMOVED CORRODED GALLEY RIGHT BEAM. INSTALLED NEW BEAM IAW EMB SRM 145/1142, CHAPTER 51, REV 18, 51-40-02, GST-1826/02, ITEM NR 1, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, TWO SHIMS. INSTALLED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW CENTER BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18, 51-40-02, ETN-EM53-020, AND STANDARD SRM PRACTICES. (M)

Part: FRAME — DENTED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND LOWER PORTION OF RIGHT FRAME 72 DENTED. RECONTOURED DENT. PERFORMED NDT, NO DEFECTS. FABRICATED TWO L SHAPE DOUBLERS. INSTALLED IAW EMB GST-1776/02, ITEM NR 3 GST-1784/02, AND STANDARD SRM PRACTICES. (M)

Part: CLIP — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CARGO DOOR CUT OUT SHEAR CLIP CORRODED. REMOVED CORRODED SHEAR CLIP. INSTALLED NEW CLIP IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18, 51-20-03, 51-40-02, ETN EM-51-020 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, FOUND CARGO DOOR LOWER SILL PLATE BETWEEN FRAMES 65 AND 68 CORRODED. REMOVED CORRODED SILL (BEAM). INSTALLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 18, 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND STRINGER 19L CHAFED AT FRAME 53. BLENDED CHAFE. FABRICATED AND INSTALLED DOUBLER ANGLE, WITH TWO SHIMS IAW EMB 145 (145/1142, CHAPTER 53, REV 18) 532-24-02, ETN EM-51-020, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR FORWARD DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED DOUBLER, IAW EMB SST-2906/00, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED DOUBLER ANGLE, FILLER, PLATE, WITH TWO SHIMS IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18, 53-21-10, AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON LEFT OMEGA BEAM UNDER EDGE OF COMPOSITE FLOOR CROSSBEAM BETWEEN FRAMES 24-25. FABRICATED AND INSTALLED A DOUBLER, IAW EMB145 SRM 53-21-10. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT HAT BEAM HAS CORROSION. INSTALLED SERVICEABLE RIGHT HAT BEAM IAW EMB145 SRM 51-40-02 AND GST-1826/02. (M)

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

THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20 HAS CORROSION. INSTALLED SERVICEABLE REPAIR DOUBLER, FILLER, PLATE AND SHIMS IAW EMB145 SRM 53-21-10. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY LEFT SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB145 SRM 51-20-03, 51-40-06 AND 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THIS IS A LEVEL 2 FINDING ON CRIC NR 36201. GALLEY FORWARD DIAMOND GUSSET HAS CORROSION INSTALLED SERVICEABLE DIAMOND GUSSET IAW SRM.

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

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

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY RAMP SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE GALLEY RAMP IAW EMB 145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FR 23, GALLEY)

THIS IS A LEVEL 2 FINDING ON CRIC NR 36200. GALLEY CROSSBEAM AND PROFILE HAS CORROSION AT FRAME 23. C/A- INSTALLED NEW CROSSBEAM AND PROFILE IAW SRM.

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE AFT SILL IAW EMB145 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. C/A-REMOVED AND REPLACED GUSSET IAW SRM.

Part: ACTUATOR — FAILED (HORIZONTAL STAB)

MEM - FLT 3256 - DURING CLIMB, CREW REPORTED CHATTERING NOISE FROM RELAYS FOLLOWED BY THE PITCH TRIM SWITCHES FOR THE FIRST OFFICER AND THE CAPTAIN NOT RESPONDING. CREW RETURNED TO MEM. DURING RETURN CREW HEARD ONE CLICK FROM A RELAY FOLLOWED BY BOTH FIRST OFFICER AND CAPTAINS PITCH TRIM SWITCHES WORKING. AIRCRAFT WAS LANDED SAFELY. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL ACTUATOR IAW AMM. OPS CHECK GOOD. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

CID - FLT 3954 - AFTER TAKEOFF, THE CAPTAIN AND FIRST OFFICERS YOKE TRIM SWITCHES FAILED. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER ELECTRONIC CONTROL UNIT. AIRCRAFT PASSED A FUNCTIONAL CHECK FLIGHT AND WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

CID - FLT 3954 - AFTER TAKEOFF, THE CAPTAIN AND FIRST OFFICERS YOKE TRIM SWITCHES FAILED. REMVOED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW AMM. OPS CHECK GOOD. FCF GOOD. (M)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB)

DFW - FLT 3560 - WHILE HAND FLYING PITCH TRIM MOVED DOWN WITHOUT PITCH DOWN IMPUT FROM PILOT. PERFORMED READING OF THE FDR AND VERIFIED THAT THERE WAS NO RECOREDED MOVEMENT OF THE HORIZONTAL STAB. REPLACED HORIZONTAL STAB CONTROL UNIT AND PERFORMED SYSTEM TEST PER MANUFACTURES PRECAUTIONARY RECOMMENDATION. EXTENSIVE FUNCTIONAL TEST FLIGHT COMPLETED AND ALL SYSTEMS FOUND SATISFACTORY. (M)

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY)

CLE - FLT 4216 - ON CLIMB-OUT, RECEIVED BAG SMOKE INDICATION. DECLARED EMERGENCY INTO CLE AND DISCHARGED THE FIRE BOTTLES. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK OF BAGGAGE SMOKE DETECTION SYSTEM AND FOUND NO DISCREPANCY. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)