N630AE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,176 hrs · 49,127 cycles

FUEL SMELL IN CABIN IN CRUISE. GROUND RAN A/C AT VARIOUS POWER SETTINGS WITH AND WITHOUT PACKS. NO FUEL SMELL NOTED. A/C OKAY FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,121 hrs · 49,063 cycles

AFTER GEAR RETRACTION 3 NORMAL INDICATIONS SHOWED. SHORTLY AFTER R/H MLG CYCLED TO LOCKED / UNLOCKED POSITION CONTINUOUSLY.........JACKED AND SWUNG GEAR ISSUE WAS VISIBLE ALSO ASSOSIATED WITH HYD THUMPING. R&R'D R/H MLG UPLOCK BOX IN REF TO AMM 32-33-10-000/400-801-A. OPS CHECK LEAK CHECK GOOD. RETURNED AIRCRAFT TO NORMAL CONFIGURATIONS OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,550 hrs · 48,407 cycles

ON TAKEOFF ROLL FUEL 2 LOW LEVEL CAUTION/WARNING DISPLAYED. ON TAXI BACK FUEL 2 LOW LEVEL WARNING DISPLAYED AND FUEL QTY 1 SHOWED DASHES. AT GATE FUEL IMBALANCE EICAS AND QTY FOR THE NO.1 TANK SHOWS 0. AFTER SLAVING IN NEW FCU MESSAGE CLEARED ONCE ORIGINAL FCU WAS REINSTALLED. R/R FCU IAW 28-41-01. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME R/R FCU FOR MX CONVIENENCE.

Part: NONE — NONE · airframe 49,206 hrs · 46,900 cycles

E922505 - LH PYLON SPAR 2 YOKE FASTENER HOLE THROUGH UPPER SKIN GOUGED. .... ACCOMPLISHED REPAIR OF LH PYLON SPAR 2 YOKE FASTENER HOLE IAW EMB SB# 145-54-0008 AND EO1-54-22-0141.

Part: NONE — NONE · airframe 49,206 hrs · 46,900 cycles

E922303 - FRAME 67 IS CRACKED AT CARGO DOOR SILL .... REMOVED AND REPLACED FRAME 67 (LOWER FRAME SECTION) AT CARGO DOOR SILL IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 49,206 hrs · 46,900 cycles

E920591 - PILOT BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED .... ACCOMPLISHED REPAIR AT PILOT BULKHEAD UPPER OTBD GUIDE PIN HOLE IAW EMB 145 SRM 53-21-02 RE SECTION 4 AND EO1-53-22-0140.

Part: NONE — NONE · airframe 49,206 hrs · 46,900 cycles

E919773 - BAGGAGE DOOR UPPER AFT FRAME IS GOUGED AROUND NUTPLATE HOLE .... REPAIRED BAGGAGE DOOR UPPER AFT FRAME GOUGE AROUND NUTPLATE HOLE IAW PIEDMONT EO1-52-22-0139

Part: NONE — NONE · airframe 49,206 hrs · 46,900 cycles

E920263 - CARGO DOOR LOWER SILL IS CORRODED. .... REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 49,206 hrs · 46,900 cycles

E920543 - CORROSION ON DIAMOND GUSSET AT FRAME 22 GALLEY AREA .... REMOVED AND REPLACED DIAMOND GUSSET AT FRAME 22 GALLEY AREA IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 49,206 hrs · 46,900 cycles

E920541 - CORROSION ON FLOOR CROSS BEAM AT FRAME 20 GALLEY AREA .... REMOVED AND REPLACED FLOOR CROSS BEAM AT FRAME 20 GALLEY AREA.IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 49,206 hrs · 46,900 cycles

E920658 - CABIN CENTER AISLE FLOOR CROSSBEAM AT FR 25 CORRODED .... REMOVED CORRODED CABIN CENTER AISLE FLOOR CROSSBEAM AT FR 25 AND INSTALLED SERVICEABLE CROSSBEAM IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (ZONE 100) · airframe 49,206 hrs · 46,900 cycles

E920281 - FR 72 IS CRACKED BTW STR 17L-16L .... REMOVED AND REPLACED FR 72 BTW STR 15L-14R. IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 49,206 hrs · 46,900 cycles

E920360 - LAV CENTER BEAM GUSSET IS CORRODED AROUND FWD AND AFT SCREW HOLES .... REMOVED AND REPLACED LAV CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: GUSSET — CORRODED (LAVATORY) · corrosion level 2 · airframe 49,206 hrs · 46,900 cycles

E920357 - LAV LH BEAM GUSSET IS CORRODED AROUND FWD AND AFT SCREW HOLES .... REMOVED AND REPLACED LAV LH BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,645 hrs · 46,262 cycles

PREVIOUS CREW REPORTS OF BURNING SMELL IN FLIGHT DECK, CREW DID NOT REPORT TO MOCC. GROUND RAN A/C W/ #1 AND #2 ENG BLEED AND APU BLEED FOR 40 MIN W/ REF TO AMM 21-51-00-700-802-A. OPS CHECK GOOD. NO BURNING SMELLS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM) · airframe 48,056 hrs · 45,594 cycles

PITCH TRIM MAIN INOP. R+R HSCU IRW EMB 145 AMM 27-40-01. OPS CHECK GOOD(MX CTRL NOTE: HSCU WAS CHANGED AS A PRECAUTION. FIM TASK 27-43-00-810-801-A WAS FOLLOWED TO BLOCK 7 WHICH DETERMINED AS A TRANSITORY CONDITION.)

Part: SWITCH — HANDLER ERROR · airframe 47,073 hrs · 44,497 cycles

EICAS DISPLAYED E1 FUEL LOW LEVEL COUPLED WITH DASHED FUEL QUANTITIES ON MFD AND EICAS. UPON INSPECTION FOUND REFUEL SWITCH ON SPR PANEL TO BE IN OPEN POSITION. INSP SPR PANEL AND PERFORMED FUEL QUNTY OPERATIONAL CHECK, IAW 28-41-00, NO DEFECTS NOTED. ALL INDICATIONS NORMAL. (CREW REPORTED REFUEL SWITCH WAS LEFT OPEN).

Part: LIGHT — DAMAGED (EXTERIOR) · airframe 46,665 hrs · 44,041 cycles

LEFT EXTERIOR EMERGENCY LIGHT ABOVE WING BELOW DOOR INOPERATIVE. R & R THE LEFT EXTERIOR EMERGENCY LIGHT ABOVE WING. FURTHER INSPECTION FOUND BAD NUT PLATES. R & R THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10-000/400-801A. OP CHECKED GOOD, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 45,848 hrs · 43,102 cycles

REJECTED TAKEOFF AT 5 KNOTS DUE TO A MOMENTARY NOSE WHEEL STEERING INOPERATIVE MESSAGE. CREW RESET NOSE WHEEL STEERING AND DEPARTED, NO MAINTENANCE ACTION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 45,536 hrs · 42,768 cycles

ABI - BROKEN WIRE CONNECTOR FOR EMERGENCY LIGHT STRIP #8 .... REPAIRED WIRE CONNECTOR FOR EMERGENCY LIGHT STRIP #8 IAW EMB 145 SW-PM 20-21-00

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 45,536 hrs · 42,768 cycles

ABI - FLOOR EMERGENCY LIGHT WIRE IS CHAFED AT FRAME 20. REPAIRED FLOOR EMERGENCY LIGHT WIRE T FRAME 20 IAW EMB 145 SWPM 20·21 ·00

Part: FIRE WARNING — ILLUMINATED (CARGO BAY) · airframe 45,023 hrs · 42,191 cycles

RECEIVED A BAGGAGE SMOKE INDICATION AFTER TAKE OFF,CREW PUSHED BAGG EXTINGUISHING BUTTON. R & R BAGGAGE BAY FIRE EXT. BOTTLES,HRD & METERING BOTTLES IAW AMM 26-23-01. ON LANDING FIRE TRUCK ROLLED ON, MET A/C. NO O2 MASKS DOWNED OR CALL FOR PAX BRACE. A/C TAXIED TO GATE UNDER OWN POWER.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 44,935 hrs · 42,098 cycles

PDIS 630 21-01 2097683 20MAY19 GSO CLOSE IN CRUISE FLIGHT AT 25K BOTH FLIGHT DECK AND CABIN EXPERIENCED LIGHT SMOKE. C/W QRH PROCEDURE AND SMOKE DISSIPATED 24934 00 EK HISTORY: FACT 21MAY19 12:02 GSO R&R NR 1 AIR CYCLE MACHIINE IAW 21-51-03. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 44,684 hrs · 41,824 cycles

PDIS 630 26-15 2055741 07APR19 PHL CLOSE ON TAXI OUT MASTER WARNING TRIPLE CHIME EICAS MESSAGE BAG SMOKE. FIRE EXTINGUSHER BAG BUTTON ILLUMINATED .CREW PERFORMED MEMORY ITEMS (RELEASED EXTIG AGENT)RAN QRH FA PERFORMED VISUAL INSPECTION.FIRE DEPT CONF IRMED NO SMOKE/FIRE/EXCESS HEAT TAXIED BACK TO GATE FACT 07APR19 20:14 PHL INSPECTED AND VERIFIED NO EVIDENCE OF FIRE. BOTH FIRE BOTTLE HARNESS ELECTRICLY TESTED GOOD. R&R BAG BAY FIRE BOTTLES IAW 26-23-01. OPS CK GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION · airframe 43,926 hrs · 40,951 cycles

FOLLOW UP ACTION: NDIS 630 26-10 0014510 12NOV18 SBY CLOSE F/U TO LAV SMOKE DETECTOR EICAS MESSAGE DISPLAYING FACT 12NOV18 10:39 SBY R & R'D LAV SMOKE DETECTOR IAW AMM TASK 26-14-01- (000/400)-801-A

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 43,926 hrs · 40,951 cycles

PDIS 630 26-23 1660181 12NOV18 CLT CLOSE LAV SMOKE EICAS MESSAGE DISPLAYED ENROUTE. CBS E12 AND E13 PULLED PER QRH FACT 12NOV18 18:11 CLT INSP. AND TESTED LAV SMOKE DET. NO DEFECTS NOTED. GROUND RAN A/C WITH PACKS 1&2 ON. AT FULL HOT. NO SMOKE OR SMELL DETECTED. (SHORT SIGN) INSPECTED AND FOUND AFT FLASHLIGHT INOP. REF. L/P 166016-2 R&R'D AFT FLASHLIGHT AND BASE IAW AMM 33-50-16-04. GRND RN A/C. NO ODORS NOTED. RE-SET C/B E12 & E13 AT THIS TIME.

Part: FLASHLIGHT — ODOR (CABIN) · airframe 43,926 hrs · 40,951 cycles

630 26-23 1660162 10NOV18 PHL CLOSE DURING INITIAL CLIMBOUT RECEIVED LAV SMOKE AURAL WAR NING AND LAV SMOKE EICAS MSG. FACT 10NOV18 18:48 PHL DETERMINED SOURCE OF SMELL WAS AFT FA'S FLASH LIGHT. R&R'D FLASH LIGHT IAW 33-50-16-04 OPS CHECK GOOD OK FOR SERVICE

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 43,733 hrs · 40,738 cycles

PDIS 630 34-41 1674792 02OCT18 PHL CLOSE RADAR FAILED IN FLIGHT. 39524 00 LLS FACT 02OCT18 16:06 PHL PERFORMED RADAR OPS CHECK, TEST PASSED. NO DEFECTS NOTED AT THIS TIME, REF AMM 34-42-00-05. OK FOR SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 43,485 hrs · 40,434 cycles

CARGO SMOKE INDICATION ON EICAS IN FLIGHT, IMMEDIATELY EXTINGUISHED, THE FIRE EXTG CARGO BUTTON REMAINED ILLUMINATED, EXTINGUISHED WITH FIRE TEST ON GROUND. PERFORMED AN OPS CHECK OF THE CARGO SMOKE INDICATION SYSTEM IAW AMM 26-15-00, OPS CHECK GOOD. OK FOR SERVICE

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 43,323 hrs · 40,243 cycles

E2 FIRE DETECT FAIL MSG DURING FLT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,162 hrs · 40,083 cycles

EMERGENCY LIGHT WAS INOPERATIVE ABOVE THE GALLEY EXIT. R & R THE EMERGENCY LIGHT INVERTER.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 43,030 hrs · 39,944 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE BY THE EMERGENCY EXIT DOOR. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: LIGHT — CONTAMINATED · airframe 42,352 hrs · 39,184 cycles

RIGHT LOWER EMERGENCY LIGHT HAS MOISTURE INSIDE OF THE LENS. REMOVED, CLEANED MOISTURE AND REINSTALLED IAW AMM 33-50-10-000/400-801-A. OK FOR SERVICE.

Part: CONTROL UNIT — BROKEN (HORIZ STAB) · airframe 42,166 hrs · 38,984 cycles

PITCH TRIM MAIN INOP EICAS WARNING MESSAGE. REPAIRED BROKEN WIRE UNDER TRIM CNLT PNL, NO FIX. R&R HOZ STAB CNTL UNIT OPS CK GOOD IAW AMM 27.40.01.00.801.A AND 27.40.00.400.801.A. ACFT OK FOR SERVICE.

Part: UNKNOWN — NOISE · airframe 41,991 hrs · 38,813 cycles

PILOT REPORTED A LOUD NOISE SIMILAR TO WHATS HEARD DURING GEAR EXTENSION. NO GEAR INDICATION ANOMALIES. NOISE WENT AWAY AFTER FEELING MECHANICAL THUMP BELOW PILOTS FEET. PERFORMED GEAR EXTENSION AND RETRACTION, OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 41,519 hrs · 38,333 cycles

DURING TAKE OFF, CONFIGURATION CHECK FLAPS WARNING AURAL MESSAGE WAS HEARD. POWERED DOWN AND POWERED UP AIRCRAFT, CYCLED CIRCUIT BREAKERS F16, F19, AND FLAPS RESET SWITCH ON MAINTENANCE PANEL. ACCOMPLISHED TASK 27-53-00-700-802A, OPS CHECKED GOOD, OK FOR SERVICE.

Part: CIRCUIT BREAKER — MALFUNCTIONED (HYD PUMP) · airframe 41,332 hrs · 38,141 cycles

ELECTRIC HYD PUMP NR 2 CIRCUIT BREAKER FOUND TRIPPED. STRONG ELECTRICAL ODOR WHEN MAINT RESET THE CIRCUIT BREAKER. CIRCUIT BREAKER PULLED. TRIPPED AGAIN WHEN POWER APPLIED. INSPECTED UNDER COCKPIT FLOOR. NO ODOR OR DEFECTS NOTED. POWERED ACFT DOWN AND BACK UP. RESET THE CIRCUIT BREAKER. OPERATED HYDRAULIC PUMPS. OPS CHECKED NORMAL. OKAY FOR SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 41,298 hrs · 38,107 cycles

CARGO SMOKE WARNING LIGHT APPEARED ON EICAS WITH ASSOCIATED EXTINGUISHER CARGO OVERHEAD BUTTON LIGHT. INSPECTED BAGGAGE COMP FOR EVIDENCE OF SMOKE OR FIRE, NO DEFECTS NOTED PERFORMED A VISUAL INSPECTION OF CARGO SMOKE DETECTORS IAW 26-15-01 AND BAGGAGE BAY SMOKE DETECTOR OPS TEST IAW 26-15-00. NO DEFECTS. OK FOR SERVICE. R & R HIGH RATE AND METERING FIRE EXTINGUISHER BOTTLES IAW AMM 26-23-01. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

COCKPIT FLOOR SUPPORT CRACKED UNDER 221GF. PERFORMED PERMANENT REPAIR OF COCKPIT FLOOR SUPPORT CRACKED UNDER 221GF IAW ERS-EM-53MR-2680.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

CORROSION IN CABIN ON STR 21L BETWEEN FRAMES 30 AND 31. ACCOMPLISHED PERMANENT REPAIR CORROSION IN CABIN ON STR 21L BETWEEN FRAMES 30 AND 31 IAW ERS-EM-53MR-2673.

Part: SPAR — CRACKED (LT WING) · airframe 41,292 hrs · 38,099 cycles

LT WING SPAR I LEADING EDGE LOWER ATTACHMENT FLANGE IS CRACKED AT RIB 9. REPAIRED LT WING SPAR I LEADING EDGE LOWER ATTACHMENT FLANGE AT RIB 9 IAW ERS-EM-57MR-799.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

FR 73 CRACKED BTW STR 16R-17R (BELOW CARGO BULKHEAD SUPPORT BEAM). PERFORMED PERMANENT REPAIR OF FR 73 CRACKED BTW STR 16R-17R IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

LT FR10 CRACKED. REMOVED AND REPLACED LT FR 10 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

CORROSION ON LT OMEGA BEAM BETWEEN FRAMES 58-59. REMOVED AND REPLACED LT OMEGA BEAM IAW SRM 51-40-02 AND SRM 51-20-01.

Part: FRAME — GOUGED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

GOUGE ON PREVIOUS REPAIR AT FR64 BETWEEN STR 6R AND 7R. REPAIRED PREVIOUS REPAIR AT FR64 BETWEEN STR 6R AND 7R IAW ERS-EM-53MR-2651

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,292 hrs · 38,099 cycles

GOUGE BTW FR 17-18 STR 21L-21R. GOUGE BTW FR 17-18 STR 21L-21R.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,292 hrs · 38,099 cycles

FA EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FA EMERGENCY FLASHLIGHT IAW AMM 33-50-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,274 hrs · 38,080 cycles

DURING PS-1 CHECK, FOUND RT EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (FWD CARGO) · airframe 40,209 hrs · 37,135 cycles

CARGO EXTINGUISHER BUTTON WILL NOT ILLUMINATE DURING FIRE TEST. REMOVED AND REPLACED SMOKE DETECTOR IN THE CARGO COMPARTMENT IAW 26-15-01. OPS CHECKED GOOD, NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,285 hrs · 36,279 cycles

LEFT FWD EMER LIGHT INOPERATIVE. R & R LT FWD EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,985 hrs · 36,021 cycles

RIGHT EXTERNAL OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,785 hrs · 35,849 cycles

NUMBER 2 OVERHEAD EMER LIGHT INOPERATIVE. R & R NR 2 OVERHEAD EMER LIGHT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 38,477 hrs · 35,530 cycles

NUMBER 1 EMER FLOOR STRIP INOPERATIVE. FIXED BROKEN WIRE TO NR 1 EMER FLOOR STRIP IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 38,212 hrs · 35,285 cycles

LEFT EMER EXIT LOWER FRAME, CORRODED UNDER CIRCULAR TEFLON GUIDE. R & R NEW LT EMER EXIT LOWER FRAME IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,212 hrs · 35,285 cycles

FRAME 75 FUSELAGE SKIN CRACKED ABOVE STRINGER 2R, RT SIDE. PERFORMED PERMANENT REPAIR OF FRAME 75, FUSELAGE SKIN CRACK ABOVE STRINGER 2R, RT SIDE IAW ERS-EM-53MR-1726.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,212 hrs · 35,285 cycles

ALL EMER LIGHTS CONNECTED TO BATTERY NR 4, DO NOT COME ON. R & R BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 38,212 hrs · 35,285 cycles

FUSELAGE SKIN BETWEEN FRAME 23 -24, STRINGER 11R - 12R, PUNCTURED. REPAIRED FUSELAGE SKIN PUNCTURE IAW ERS-EM-53MR-1717.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,212 hrs · 35,285 cycles

TWO LIGHTNING STRIKES, DAMAGE TO CTR FUSELAGE 1 SKIN, BETWEEN FRAME 23 - 24, STRINGER 20R - 21R. REPAIRED TWO LIGHTNING STRIKES DAMAGE IAW ERS-EM-53MR-1719.

Part: WIRE — DAMAGED (CABIN) · airframe 38,212 hrs · 35,285 cycles

NUMBER 2 LT EMER LIGHT WIRE PULLED OFF. R & R NR 2 LT EMER LIGHT STRIP IAW AMM 33-50-12.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 38,212 hrs · 35,285 cycles

LAVATORY AREA HAS SUSPECTED AREA OF CORROSION. PERFORMED PERMANENT REPAIR, INSTALLED DOUBLER IAW SRM 53-31-02.

Part: WIRE — BROKEN (CABIN) · airframe 38,212 hrs · 35,285 cycles

EMERGENCY LIGHT STRIP AT FRAME 41 IS BROKEN. REPAIRED NR 4 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: WIRE — BROKEN (CABIN) · airframe 38,212 hrs · 35,285 cycles

EMERGENCY LIGHT STRIP AT FRAME 35 IS BROKEN. REPAIRED NR 3 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,212 hrs · 35,285 cycles

ALL EMER LIGHTS CONNECTED TO BATTERY NR 4 DO NOT COME ON DURING TEST. R & R NR 4 BATTERY & CHARGER IAW AMM 33-50-04 & WC 33-700-19. SEE BOW 203494 FOR OPERATIONS CHECK. EMER LIGHTING BATTERY PN 2013-1A.

Part: STRUCTURE — CRACKED (CABIN) · airframe 38,212 hrs · 35,285 cycles

RIGHT NR 1 EMER LIGHT EXTRUSION CRACKED. R & R RT NR 1 EMER LIGHT EXTRUSION IAW AMM 33-50-12.

Part: STRUCTURE — CRACKED (CABIN) · airframe 38,212 hrs · 35,285 cycles

LEFT NR 1 EMER LIGHT RAMP EXTRUSION CRACKED. R & R LT NR 1 EMER LIGHT RAMP EXTRUSION IAW AMM 33-50-12.

Part: STRIP — DAMAGED (CABIN) · airframe 38,212 hrs · 35,285 cycles

EMERGENCY LIGHT STRIP PLASTIC EXTRUSION TORN & CRACKED AT 12A. R & R EMER LIGHT STRIP PLASTIC EXTRUSION AT 12A IAW AMM-33-50-12. OPERATIONS CHECKED GOOD.

Part: YOKE — CRACKED (LT NACELLE) · airframe 38,212 hrs · 35,285 cycles

LEFT FWD LOWER YOKE, FWD SIDE IS CRACKED. REMOVED DAMAGED YOKE FITTING & PREPPED SERVICEABLE FITTING IAW EM-54MR-386.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 38,212 hrs · 35,285 cycles

CROSSBEAM ABOVE FRAME 20 IS CORRODED. R & R CTR AISLE CROSSBEAM FRAME 20 IAW SRM 51-20-04 & ETN EM 53-139R4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,126 hrs · 35,209 cycles

TWO LIGHTNING STRIKE DAMAGES, BETWEEN FRAME 61R & 60R, STRINGER 20R & 21R. REMOVED LIGHTNING DAMAGE, INSTALLED DOUBLER, FILLER, RIVET IAW ERS-EM-53MR-1642.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,090 hrs · 35,175 cycles

CABIN LT OVERWING EMER LIGHT INOPERATIVE. R & R CABIN LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,823 hrs · 34,930 cycles

EMERGENCY LIGHT UNDER COCKPIT DOOR INOPERATIVE IAW 630 CVG 02355. R & R EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,014 hrs · 34,159 cycles

BURNING SMELL ON THE FLIGHT DECK FIRST OFFICER SIDE. NOTICED NO MALODOROUS SCENTS IN ACFT FWD OR CABIN. RAN BOTH PAC 1 & 2 OFF OF APU AT FULL HOT & FULL COLD INDIVIDUALLY ON 4 MINS CYCLES. CHECKED ALL FLIGHT DECK LIGHTS & POWERED ON ALL AVIONICS, STILL NO ODORS ANYWHERE AT THIS TIME. PILOTS REPORTED SMELL ON INITIAL POWER UP OFF OF GPU WITH NO APU OR ENGS RUNNING.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,846 hrs · 34,032 cycles

FLIGHT ATTENDANT REPORTS AFT FLASHLIGHT NOT CHARGING. R & R AFT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,606 hrs · 33,782 cycles

FORWARD CABIN FLASHLIGHT INOPERATIVE, INDICATES CHARGING THOUGH. REPLACED FWD FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BUTTON — INOPERATIVE (COCKPIT) · airframe 36,367 hrs · 33,572 cycles

EMERGENCY PARKING LIGHT INOPERATIVE WITH BRAKE SET. DEFERRED IAW MEL 32-6. COMPLIED WITH THE MEL PROCEDURES. R & R EMER PARKING BRAKE LIGHTED PUSH BUTTON ASSEMBLY & OPERATIONS CHECKED GOOD IAW AMM 20-13-04. MEL ITEM RESTORED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,026 hrs · 33,278 cycles

FLASHLIGHT HOLDER FIRST OFFICER SIDE BROKEN. R & R IAW EMB AMM 33-50-16. OPERATIONAL CHECKED GOOD.

Part: TRANSDUCER — FAILED (ANTI-SKID SYS) · airframe 35,977 hrs · 33,241 cycles

AFTER LANDING DURING TAXI BRAKE DEGRADED MSG, CAUTION, ON EICAS. BRAKING & STEERING DURING LANDING & TAXI NORMAL. BRAKE TEMPS NORMAL, GREEN. UPON INSPECTION FOUND NR 4 WHEEL SPEED TRANSDUCER FAILED TWICE. R & R NR 4 WHEEL SPEED TRANSDUCER & OPERATIONS CHECKED GOOD IAW AMM 32-41-03 & 32-41-00.

Part: CONNECTOR — DIRTY (COCKPIT) · airframe 35,853 hrs · 33,138 cycles

COCKPIT STEP EMER EXIT IDENTIFIER INOPERATIVE. DISCONNECTED, CLEANED & RECONNECTED THE ELEC CONNECTORS. OPERATIONS CHECKED GOOD IAW AMM 33-50-13.

Part: SOLENOID VALVE — FAILED (LANDING GEAR) · airframe 35,800 hrs · 33,087 cycles

LANDING GEAR DISAGREE ON CLIMB OUT. AOM PROCEDURES FOLLOWED. TRANSFERRED TO NRWC 630-DFW-01943. R & R LG SOLENOID VLV IAW AMM 32-33-04. OPERATIONS CHECKS & LEAK CHECKS GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,271 hrs · 32,582 cycles

ON ROTATION STRUCK MULTIPLE BIRDS, FOLLOWED BY SMELL IN COCKPIT. OVER WEIGHT LANDING VERTICAL SPEED LESS THAN 50' PER MINUTE, LANDING WEIGHT 47000 POUNDS. TRANSFERRED TO NRWC 630-DFW-01844. FOLLOWING TURNOVER OF THIS NRWC COMPLETED BIRD STRIKE INSPECTION IAW WC 05-200-07. OVERWEIGHT LANDING INSPECTION IS NOT REQUIRED IAW AMM 05-50-25 & CREW REPORTED CONDITIONS. SEE NRWC 630-DFW-01845 FOR SMELL IN COCKPIT ITEM. PERFORMED ENG RUNS IAW RR MM 72-00-00. RAN PACKS IAW AMM 21-00-00. NO ABNORMAL SMELL OBSERVED, NO FURTHER FAULTS FOUND.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,648 hrs · 32,026 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 34,073 hrs · 31,565 cycles

ON FLIGHT 3090 DURING CLIMB OUT AT 5000FT, ANTI-ICE 2 FAIL. OVERRIDE IN AUTO. JUST PRIOR TO REACHING ICING CONDITIONS, EMERGENCY WAS DECLARED & RETURNED TO ORD. LANDING WEIGHT WAS BELOW MAXIMUM AT 42600 LBS. THE ACFT WAS REMOVED FROM SERVICE. APPROPRIATE INDICATIONS WERE NOTED DURING ENG RUN M PROCEDURES OF MEL 30-11. REMOVED AND REPLACED ANTI-ICE VALVE IAW EMB AMM 30-21-01. OPS CHECK GOOD.

Part: SPAR — CRACKED (LT WING) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION LT WING SPAR 3 CRACK REPAIR REQUIRES EO-EM-57MR-682 PT. COMPLETED REPAIR OF LT WING SPAR III WEB IAW EO EM-57MR-682 R2 PTB.

Part: STRAP — CRACKED (FUSELAGE) · airframe 34,049 hrs · 31,544 cycles

DURING 3C CHECK FOUND FWD EQUIPMENT COMPARTMENT HAS A CRACKED WEB AT FS 193. LT SIDE APPROXIMATELY .250 LONG. REPAIRED LT LONGITUDINAL SKIN SPLICE STRAP BETWEEN FRAMES 13 AND 14 IAW SRM 53-00-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION FOUND SERVICE DOOR CTR SILL HAS CORROSION. REMOVE AND REPLACE SERVICE DOOR CENTER SILL IAW EMB SRM 51-40-02.

Part: SKIN — CORRODED (FRAME 13) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND INTERIOR FUSELAGE SKIN CORRODED AFT OF FRAME 13 NEAR STRINGER 20L. COMPLETED REPAIR AND INSTALLATION OF NEW SKIN AND SPLICE STRAP IAW ERS-EM-53MR-023.

Part: FRAME — GOUGED (FRAME 70) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND RIGHT CARGO BAY FRAME 70 GOUGED. REPAIRED IAW ERS-EM-53MR-018.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND RT WING TO FUSELAGE PANEL LOWER NUT PLATE SUPPORT ANGLE IS CRACKED AT FRAME 47. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND RT AILERON HAS TWO MIGRATED HAT BUSHINGS AND ONE WORN HAT BUSHING. REPLACED RT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: SUPPORT ANGLE — CRACKED (FRAME 41) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION FOUND RT WING TO FUSELAGE PANEL LOWER NUT PLATE SUPPORT ANGLE IS CRACKED AT FRAME 41. REPLACED SUPPORT ANGLE IAW SRM 51-40-02 AND ETN EM-53-142.

Part: SUPPORT ANGLE — CRACKED (FRAME 41) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND LT WING TO FUSELAGE PANEL LOWER NUT PLATE SUPPORT ANGLE CRACKED AT FRAME 41. REPAIRED SUPPORT ANGLE IAW ETN-EM-53-142R2.

Part: FITTING — DAMAGED (LT AILERON) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND LEFT AILERON PCA ATTACH POINT IS MISSING OTBD HAT BUSHING. REPLACED LT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND FRAME 80 SHEAR TIE BETWEEN STRINGERS 5-6L CRACKED. REPLACED SHEAR TIE IAW SRM 51-40-02 AND ERS-EM-5300-070.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND FRAME 68 LT SHEAR TIE ABOVE THE CARGO DOOR CUT OUT CRACKED. REPLACED SHEAR TIE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAME 10) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND FRAME 10 RT UPPER ATTACH RETAINER ANGLE IS CRACKED. REMOVE AND REPLACE UPPER ATTACH RETAINER ANGLE ON FRAME 10 IAW SRM 51-40-02.

Part: SILL — CORRODED (FRAME 65-68) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND CARGO DOOR SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: BRACKET — CRACKED (LT WING) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND FUEL LINE SUPPORT BRACKET AT LT RIB 3 BENEATH PANEL 531AB CRACKED. REMOVED AND REPLACED FUEL LINE SUPPORT BRACKET IAW AMM 28-00-00 AND 20-10-01.

Part: FLOORBEAM — CRACKED (FRAME 66) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND CARGO FLOORBEAM ANGLE AT FRAME 66 CRACKED. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FRAME 10) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSP, FOUND FRAME 10 LT IS CRACKED AT THE UPPER ATTACH POINTS. REPAIRED IAW SRM.

Part: DOOR — CRACKED (COCKPIT FLOOR) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND COCKPIT UNDERFLOOR HATCH HAS A CRACK BETWEEN THE TWO SCREWS OF THE EYELIT BRACKET. REPAIRED HATCH IAW ERS-EM-5200-009.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND FRAME 80 SHEAR TIE BETWEEN STRINGERS 5-6L CRACKED. REPLACED SHEAR TIE IAW SRM 51-40-02 AND ERS-EM-5300-070.

Part: DOOR FRAME — CRACKED (COCKPIT FLOOR) · airframe 34,049 hrs · 31,544 cycles

DURING HMBV INSPECTION, FOUND COCKPIT UNDERFLOOR HATCH IS CRACKED IN TWO SPOTS AT THE AFT RT LOCKING PIN BRACKET. REMOVED AND REPLACED HATCH SURROUND FRAME IAW SRM 51-40-02. PRESSURE LEAK CHECKED GOOD IAW AMM 21-31-00-700-808A. NO LEAKS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,988 hrs · 31,495 cycles

ALL CABIN EMEGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-50-04. OPS CHECKED OK.

Part: LIGHT — LOOSE (CABIN) · airframe 33,849 hrs · 31,380 cycles

FWD OVERHEAD EMERGENCY LIGHT INOP AT SEAT ROW 12. RESECURED CONNECTION ON FWD OVERHEAD EMERGENCY LIGHT AT ROW 12. OPS CHECKS GOOD IAW AMM 33-50-00.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 BLEED) · airframe 33,602 hrs · 31,167 cycles

10 MINUTES AFTER PACK 1 OVERLOAD RECEIVED EICAS BLEED NR 1 LEAK. RAN PROCEDURE DECLARED EMERGENCY AND DIVERTED. INDICATION WENT OUT APPROXIMATELY 2 MINUTES AFTER BLEED SHUTDOWN, FIM TASK 36-11-00-810-811. SUPPLIED PNEUMATIC ENERGY, AIR BLEED THROUGH THE APU IAW AMM 36-00-00. NO BLEED LEAKS NOTED.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 33,434 hrs · 31,016 cycles

AFT FLASHLIGHT MISSING. FLASHLIGHT INSTALLED AND OPS CHECKED GOOD IAW AMM 33-50-16. RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 33,162 hrs · 30,793 cycles

DURING MX INSPECTION, FOUND THE LT OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE AFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,018 hrs · 30,683 cycles

DURING B INSP FOUND THE LT LATERAL PANEL EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R LT LATERAL PANEL EMERGENCY LIGHT IAW AMM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,454 hrs · 30,233 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPAR — CRACKED (LT WING) · airframe 32,448 hrs · 30,228 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT WING SPAR 3 CRACKED AT 10 O’CLOCK AND 4 O’CLOCK POSITIONS AT MLG HARNESS 10 O’CLOCK POSITION 2.10, 4 O`CLOCK POSITION 1.50 VIABLE FROM FORWARD AND AFT SIDES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AS PER EO EM-57MR-682 REV 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPAR — CRACKED (LT WING) · airframe 32,446 hrs · 30,226 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT WING SPAR 3 CRACKED AT 10 AND 4 O`CLOCK POSITIONS AT MAIN LANDING GEAR HARNESS. 10 O`CLOCK POSITION 2.10 IN 4 O`CLOCK POSITION 1.50 IN. VISABLE FROM FORWARD AND AFT SIDES. THE AIRCRAFT WAS REMOVED FROM SERVICE. THIS AIRCRAFT HAD BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT. STOP DRILLED CRACK ON LEFT WING SPAR 3 AT 10 O'CLOCK AND 4 O'CLOCK POSITIONS AT MAIN LANDING GEAR HARNESS IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (FLASHLIGHT) · airframe 32,365 hrs · 30,163 cycles

ON FLIGHT 3577 THE CREW REPORTED THE CABIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED FLASHLIGHT CONNECTOR. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 32,301 hrs · 30,112 cycles

DURING B INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. NO FIX. FOUND WIRES CHAFED AT CONNECTOR. REMOVED AND REPLACED THE CONNECTORS IAW EMB 145 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (INTERPHONE) · airframe 32,242 hrs · 30,065 cycles

ON FLIGHT 3450 THE CREW REPORTED THE CABIN AND CABIN EMERGENCY LIGHTS ON ICU PANEL WOULD NOT GO OUT. UNABLE TO COMMUNICATE WITH FLIGHT ATTENDANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET INTERPHONE CONTROL UNIT FOR FORWARD FLIGHT ATTENDANT AND OPS CHECK GOOD IAW EMB AMM 23-31-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 32,229 hrs · 30,051 cycles

ON FLIGHT 3563 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE - HANDLE ACTIVATION SEEMED STIFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED DOOR JAMB ROLLERS AND PERFORMED OPERATIONAL CHECK OF CABIN ENTRY DOOR AND FOUND TO BE WORKING NORMALLY IAW EMB AMM 52-22-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,997 hrs · 29,869 cycles

DURING PS1 CHECK FOUND THE RIGHT OVERWING EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP ON THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — SMOKE (MLG) · airframe 31,758 hrs · 29,696 cycles

ON FLIGHT 3975 AIR TRAFFIC CONTROL ADVISED THE CREW THAT ONE OF THE BRAKES APPEARED TO BE SMOKING AS WE BRAKED ON THE RUNWAY. THE GEAR WAS SOAKED WITH DE-ICING FLUID AT THE DEPT STATION, IT MAY HAVE BEEN THE CAUSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF ALL BRAKES, NO DEFECTS NOTED ALL BRAKE TEMPS WERE NORMAL, FOUND LARGE AMOUNT OF DEICE FLUID IN GEAR AREA. NO OTHER DEFECTS NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — ROUGH (CABIN DOOR) · airframe 31,366 hrs · 29,373 cycles

FOR FLIGHT 3207 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SMOOTHED OUT ROUGH EDGES ON FORWARD GUIDE BLOCKS AND LUBED FRAME ROLLERS IAW EMB-145 AMM 53-21-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,252 hrs · 29,282 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,118 hrs · 29,178 cycles

DURING B INSPECTION FOUND ROW 12 RIGHT SIDEWALL EMERGENCY DOOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,873 hrs · 28,972 cycles

DURING B INSPECTION, FOUND THE FIRST FLOOR STRIP AND SERVICE DOOR EXIT IDENTIFIER EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER OVER GALLEY IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 30,745 hrs · 28,876 cycles

DURING PS1 CHECK, FOUND THE RIGHT WING OVERWING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-14. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,378 hrs · 28,590 cycles

DURING B INSPECTIONS FOUND THE EMERGENCY FLOOR TRACK LIGHT STRIP (NR 1) FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 (FRONT) EMERGENCY FLOOR PROX STRIP LIGHT IAW EMB-145 M/M 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROD — OUT OF ADJUST (PAX DOOR) · airframe 29,849 hrs · 28,184 cycles

ON FLIGHT 3407 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN/CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED PASSENGER MAIN CABIN DOOR. ADJUSTED INTERCONNECTION ROD V IAW AMM 52-18-00 DOOR OPEN/CLOSES NORMALLY AT THIS TIME NO DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,818 hrs · 28,156 cycles

DURING MAINTENANCE INSPECTION, FOUND FUSELAGE CORROSION BETWEEN FRAME 13 AND 14, STRINGER 20 RIGHT AND 21 RIGHT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIRS IAW EO-EM-53MR-1954. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 29,818 hrs · 28,156 cycles

DURING MAINTENANCE INSPECTION FOUND THE CENTER OMEGA BEAM MISDRILLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1545 PART C. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 29,831 hrs · 28,170 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT STRIP AT ROW 18 HAS A BROKEN CONNECTOR. AIRCRAFT REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT CONNECTOR IAW SWPM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,831 hrs · 28,170 cycles

CORROSION AROUND NUTPLATE HOLES ON RT OMEGA BEAM ABOVE FR 23. REPAIRED RT OMEGA BEAM ABOVE FR 23 IAW AE EO EM-53MR-1958.

Part: HOLDER — BROKEN (CABIN) · airframe 29,515 hrs · 27,930 cycles

ON FLIGHT 3546 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,813 hrs · 26,638 cycles

DURING MAINTENANCE BASE VISIT FOUND FLOOR PROXIMITY EMERGENCY LIGHT SECOND FROM FORWARD INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT SECOND FROM FORWARD IAW EMB 145 AMM 33-50-12 FNC GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — FIRE (NR 4) · airframe 27,701 hrs · 26,550 cycles

ON FLIGHT 2710 AFTER LANDING AT DFW THE TOWER REPORTED TO THE CREW, FIRE ON RIGHT MAIN LANDING GEAR. THE AIRCRAFT EXITED THE RUNWAY AND STOPPED ON THE TAXI WAY. EMERGENCY, FIRE, AND RESCUE WERE DISPATCHED AND PASSENGERS WERE DEPLANED ON TAXI WAY AND THE FIRE PUT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 MAIN BRAKE ASSEMBLY IAW WORK CARD 32-600-14. REMOVED AND REPLACED THE NR 4 MAIN TIRE IAW WORK CARD 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,298 hrs · 26,263 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — UNSERVICEABLE (CABIN) · airframe 26,618 hrs · 25,733 cycles

FOR FLIGHT 4144 A BURNING ELECTRICAL ODOR WAS DETECTED AROUND ROW 12. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 11 AND 12 LEFT SIDEWALL BALLASTS IAW EMB-145 AMM 33-21-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 26,382 hrs · 25,574 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT FACING EMERGENCY EXIT SIGN OVER ROW 12 AISLE TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND A LOOSE WIRE AT THE SIGN IN CEILING PANEL. RECONNECTED THE LOOSE WIRE AT THE CONNECTOR. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 26,095 hrs · 25,350 cycles

PRIOR TO FLIGHT 2964 THE AIRCRAFT SUSTAINED A SEVEN BY 4 INCH GASH IN THE FORWARD SECTION OF THE FUSELAGE THAT OCCURRED WHEN HIGH GUSTY WINDS PUSHED A BAGGAGE CART INTO THE AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH PART B OF AEA EO EM-53MR-1679. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,760 hrs · 25,068 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHTS, FROM EMERGENCY EXITS HATCHES AFT, TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SPLICE SP9115 IAW EMB SWPM 20-21-00. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 IAW AMM 33-50-04. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 6 IAW AMM 33-50-11. THE EMERGENCY LIGHTING SYSTEM OPERATION CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,745 hrs · 25,053 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD EXIT LOCATOR SIGN ABOVE THE CENTER TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 AND NR 4 EMERGENCY LIGHTING SYSTEM POWER SUPPLIES. COMPLETED THE FUNCTIONAL CHECK IAW AMWC 33-700-19. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,493 hrs · 24,843 cycles

ON FLIGHT 4067 MAINTENANCE FOUND MID CABIN FORWARD EXIT SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MID CABIN FORWARD EXIT SIGN IAW EMB 145 AMM 33-50-15, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 24,882 hrs · 24,352 cycles

DURING MAINTENANCE BASE VISIT DAMAGED FRAME 33 BY STATION WHILE SETTING A RIVET DURING REPAIR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 33 IAW SRM 53-00-04 FIG 206. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 24,882 hrs · 24,352 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 70 ON THE RIGHT SIDE HAS A TOOLING MARK BETWEEN STRINGERS 11 RIGHT AND 12 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 70 IN ACCORDANCE WITH ENGINEERING ORDER EM-53MR-1539. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 24,882 hrs · 24,352 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 64 TO HAVE A TOOLING MARK BETWEEN STRINGER 6 RIGHT AND STRINGER 7 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 64 WITH DOUBLER IAW ENGINEERING ORDER EM-53MR-1534. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 21,254 hrs · 21,266 cycles

ON FLIGHT 4286, DURING DESCENT CREW RECEIVED A PFD FAILED MESSAGE FOLLOWED BY SLIGHT ELECTRICAL BURNING ODOR. CREW PULLED PFD NR 1 CB AND ODOR SLOWLY EXTINGUISHED. ACFT REMOVED FROM SERVICE, ISSUED MEL 34-01. REMOVED AND REPLACE NR 1 PFD IAW EMB-145 MM 34-22-01. OPERATIONAL CHECK GOOD MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

ON FLIGHT 4105 CREW ADVISES CEILING EMERGENCY EXIT LIGHT OVER ISLE ROW 11 IS INOPERATIVE. ACFT REMOVED FROM SERVICE. C/A RESET AND RESCUED CEILING EMERGENCY EXIT LIGHT ON ROW 11 IAW AE EMB 145 AMM STANDARD MX PRACTICES. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,980 hrs · 19,927 cycles

DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL TO BE CORRODED. REMOVED AND REPLACED FORWARD SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,980 hrs · 19,927 cycles

DURING MBV INSPECTION FOUND AFT SERVICE DOOR SILL TO BE CORRODED. REPAIRED AFT SILL BY INSTALLING A DOUBLER IAW ETA-EM-5300-065. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANTI-ICE VALVE — INOPERATIVE (WING) · airframe 19,889 hrs · 19,843 cycles

ON FLIGHT 3422, CREW REPORTED RETURN TO FIELD FOR ANTI-ICE CONDITION INOP MESSAGES WITH WING AND STAB MESSAGES. THE CREW DID DECLARE AN EMERGENCY. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING ANTI-ICING VALVE. OPERATIONAL CHECK GOOD AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (RECIRCULATION) · airframe 18,808 hrs · 18,868 cycles

DURING TAXI OUT FLIGHT ATTENDANT ADVISED CREW OF ODOR OF SMOKE IN CABIN. PAX COMPLAINED OF THERE FEET FELT HOT ON THE FLOOR. A/C RETURN TO GATE. OTHER PAX CONFIRMED ODOR OF SMOKE. INSPECTED BLEED AIR SYSTEM NO DEFECT NOTED. REMOVE FLOOR PANEL TO INSPECT THE RECIRCULATION FAN. FAN WAS INOP. MEL RECIRCULATION FAN. REMOVED AND REPLACED RECIRCULATION FAN. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OPEN (STARTER) · airframe 18,400 hrs · 18,478 cycles

BUFFET FELT FIVE MINUTES AFTER CLIMB-OUT AT APPROXIMATELY 12,000 FEET, AT CRUISE AIRCRAFT ACCELERATED ONLY TO 232 KNOTS AT 33,000 FEET. RIGHT ENGINE PARAMETERS HIGHER THAN LEFT ENGINE, POST FLIGHT INSPECTION REVEALED AIR TURBINE STARTER DOOR OPEN AND OUTER BYPASS DUCT ACCESS PANEL MISSING ON THE NUMBER ONE ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,337 hrs · 17,475 cycles

FOUND MID-CEILING FOWARD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN IAW EMB AMM 33-50-15. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM)

AT FL 220, GOT EICAS MESSAGES FOR ICE CONDITION, ANTI-ICE INOPERATIVE AND WING ANTI-ICE FAIL. CAPT CALLED ON LAND LINE AFTER DIVERTING TO IND. THERE WAS WX IN ORD AND CAPT DID NOT FEEL SAFE CONTINUING TO ORD. RAI LOW PRESSURE SWITCH, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYDRAULIC LINE — MISROUTED (LT MLG)

AIRCRAFT WOULD NOT STOP WHEN BRAKES APPLIED, VEERED TO RIGHT AND WENT OFF RUNWAY. FOUND FLEXABLE HYDRAULIC LINES AT TOP PIVOT POINT FOR LT MLG, INBOARD AND OUTBOARD LINES, TO BE CROSSED. INSTALLED INBOARD AND OUTBOARD HYDRAULIC LINES TO PROPER POSITION IAW EMB 145 AMM 32-10-01 AND LEAK/OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

FOUND OMEGA BEAM DOUBLER AT FRAME 20 CORRODED. REPLACED DOUBLER IAW SRM 53-00-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CABIN)

FOUND SERVICE DOOR CENTER SILL BETWEEN FRAMES 20-22 CORRODED. REPLACED SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CABIN)

FOUND FORWARD SERVICE DOOR SILL CORRODED. REPLACED SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - FOUND RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 30-36 IS CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND FUSELAGE SKIN HAS 2 DENTS JUST AFT OF FUSELAGE DRAIN. REPAIRED FUSELAGE SKIN IAW EMB SRM 53-31-01 BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 12,094 hrs · 12,686 cycles

CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS FROM ROW 8 THRU 12 DO NOT STAY ON WHEN TESTED THEY COME ON THEN IMMEDIATELY GO OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CREW REPORTED THE EMERGENCY LIGHTS AT SEATS 8 THRU 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER CONTROL)

ORD - FLT 4244 - LOST RUDDER CONTROL DURING LANDING. EICAS DISPLAYED RUDDER 1-2 SYSTEM INOPERATIVE. PERFORMED TROUBLESHOOTING PROCEDURES FOR RUDDER 1-2 INOPERATIVE IAW EMB145 FAULT ISOLATION MANUAL. PERFORMED OPERATIONAL CHECK OF RUDDER IAW EMB 145 AMM 27-23-00. NO DEFECTS NOTED. COMPLIED WITH FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT A SECTION OF THE CENTER OMEGA BEAM. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 19) CHAPTER 53-21-10 AND EMB 145 GST-3087/02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A SECTION OF THE CENTER OMEGA BEAM. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (EMB SRM 145.1142 REV 19) CHAPTER 53-22-10 AND EMB 145 GST 3087/02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS IN THREE AREAS. BLENDED THE THREE DAMAGED AREAS, CLEANED AND TREATED. FABRICATED THREE REINFORCEMENT DOUBLERS. REPAIR DONE IAW AE ETN EM-53-036, FIG 5. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND THE LEFT OMEGA BEAM AT FRAME 20 CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF LEFT OMEGA BEAM. FABRICATED A FILLER, SHIMS, BACK PLATE AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 19) CHAPTER 53-21-10 FIG 201. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, GALLEY RIGHT BEAM, WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED DAMAGED BEAM AND INSTALLED NEW BEAM IAW EMB 145 SRM (EMB 145/1142 REV 19) CHAPTER 51-40-02. (M)

Part: FRAME — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION FRAME 81, LOWER HALF WAS FOUND CHAFED BELOW SRM LIMITS. REMOVED DAMAGED FRAME SECTION. INSTALLED NEW FRAME IAW EMB 145 SRM (EMB SRM 145/1142 REV 19) CHAPTER 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER BEAM. INSTALLED NEW BEAM IAW AE ETN EM-53-028R1 AND EMB145 SRM (145/1142 REV 19) CHAPTER 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR OPENING LOWER CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL. INSTALLED NEW SILL IAW EMB 145 SRM 9145/1142 REV 19) CHAPTER 51-20-01 AND STANDARD SRM PROCEDURE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 16.5 INCHES BY 19.625 INCH SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR DONE IAW EMB-145, SRM 145/1142, CHAPTER 53 REV 19, 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

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

Part: STRINGER — CHAFED (FUSELAGE)

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

Part: SQUAT SWITCH — FAULTY (NLG & MLG)

DFW - FLT 3545 - ON CLIMB-OUT, THRUST REVERSER DISAGREE MESSAGE ON EICAS. DECLARED EMERGENCY AND RETURNED TO DFW C/A RAI NOSE LANDING GEAR AND MLG AIR TO GROUND SWITCHES PART NUMBERS OFF 8-527-01 SERIAL A9940/A8147 AND PART NR ON 8-527-01 SERIAL NR'S A10750/A22001. (M)

Part: WINDSHIELD — BROKEN (COCKPIT)

MTY - FLT 3494 - DURING FLIGHT, THE CAPTAINS WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM 56-10-01. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

IND - FLT 4048 - IN CRUISE CAPTAINS WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

IND - FLT 4048 - IN CRUISE, CAPTAIN''S WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND LANDED IN IND. (M)

Part: SEAL — WORN (BLEED AIR)

ORD - FLT 4351 - ON CLIMB-OUT, CREW NOTED E1 BLEED LEAK ON EICAS, RETURNED TO ORD FOR MAINTENANCE. RAI DUCT SEALS BEHIND RIGHT CARGO LINER. LEAK CHECK GOOD. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

GRR - FLT 4152 - LAVATORY SMOKE INDICATION CAME ON AFTER TAKEOFF AND WENT OUT 1 MINUTE LATER. CREW DECLARED AN EMERGENCY AND RETURNED TO GRR. NO EVIDENCE OF SMOKE OR BURNING. PERFORMED OPS CHECK OF SYSTEM, SYSTEM FOUND GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

DFW - FLT 3603 - AFTER TAKEOFF, BAGGAGE SMOKE INDICATION CAME ON. CREW DISCHARGED BOTH FIRE EXTINGUISHERS. DECLARED AN EMERGENCY AND RETURNED TO DFW. VERIFIED EVENT AS FALSE WARNING AND DEFERRED BAGGAGE SMOKE DETECTION SYSTEM AND FIRE EXTINGUISHER SYSTE. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. MEL WAS RESTORED AND THE AIRCRAFT WAS AGAIN RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

HOU - FLT 3544 - BAGGAGE SMOKE WARNING INDICATION CAME ON IN-FLIGHT. DISCHARGED FIRE EXTINGUISHER. RETURNED TO HOUSTON. VERIFIED EVENT AS A FALSE WARNING AND DEFERRED BAGGAGE SMOKE WARNING SYSTEM. ON 5-31-99, THE BAGGAGE SMOKE WARNING SYSTEM WAS OPERATIONALLY CHECKED WITH NO DISCREPANCIES NOTED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X)