N649PP

Part: AMPLIFIER — FAULTED (ZONE 200)

CABIN EMERG LIGHTS WONT TURN OFF. PERFORMED ELECTRICAL RESET. NO FIX. RESET PA C/B NO FIX. INSTALLED NEW F/A HANDSET IN THE #100 & #200 POS, NO FIX. REINSTALLED ORGINAL HANDSETS REF AMM 23-13-03. RERACKED PA AMPLIFIER NO FIX. REMOVED AND REPLACED PA AMPLIFIER IAW AMM 23-31-01. OPS CK GOOD

Part: STRUT — DISCHARGED (ZONE 700) · airframe 53,301 hrs · 50,389 cycles

LG AIR GROUND FAIL MSG UPON GEAR RETRACTION FACT 30DEC24 10:16 ROA C/W FIM 32-63-00-810-802-A PERFORMED NLG SHOCK I SERVICING IAW AMM 32-20-01-600-801-A FOUND LH MLG WOW CANNON PLUG NOT SEATED WITH IMPROPER GAP AND NLG WOW IMPROPER GAP RESEATED LH MLG AFT WOW AND NLG WOW IAW AMM 32-63-05-700-809-A OPS CHECK GOOD LEAK CHECK GOOD

Part: SOLENOID VALVE — FAULTED (ZONE 700) · airframe 52,982 hrs · 50,053 cycles

THUMPING SOUND OBSERVED IN NOSE WHEEL BAY FOLLOWING GEAR RETRACTION FACT 27OCT24 04:50 ROA R/R'D LANDING GEAR SOLENOID VALVE IAW AMM 32-33-04-00-801-A. LEAK AND OPS CHECKS GOOD. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 52,498 hrs · 49,485 cycles

FAINT ELECTRICAL BURNING SMELL IN FLIGHT DECK. UPON ARRIVAL NO ELECTRICAL SMELL NOTED IN FLIGHT DECK OR CABIN. RAN PACKS OFF OF APU FOR 10 MINUTES WITH ALL DISPLAYS ON FULL BRIGHT. TURNED OFF PACKS AND WAITED ANOTHER 10 MIN NO ELECTRICAL SMELL. NO DEFECTS NOTED A/C OK FOR SERVICE.

Part: FRAME — CHAFED (FR 67) · airframe 52,406 hrs · 49,389 cycles

E040391 CARGO FR-67 BETWEEN STGRS 6R/7R HAS A CRACK. RAR FR-67 IN CARGO BETWEEN STRINGERS1R-15R IAW EMB 145 SRM 51-40-02.

Part: WEB — CHAFED (CARGO DOOR) · airframe 52,406 hrs · 49,389 cycles

E040278 CARGO DOOR LOWER INTERIOR WEB CHAFED AT NUTPLATE. PERFORMED DOUBLER REPAIR ON CARGO DOOR LOWER WEB AT JUNCTION OF LOWER HORIZONTAL FRAME& VB3 IAW EMB-145 SRM 52-30-01 RE, ITEM 12, FIGURE 213 AND EO1-52-24-0346

Part: WEB — CHAFED (CARGO DOOR) · airframe 52,406 hrs · 49,389 cycles

E040279 CARGO DOOR LOWER INTERIOR WEB CHAFED AT HB3 AND VB3 INTERSECTION. PERFORMED DOUBLER REPAIR ON CARGO DOOR INTERIOR WEB AT HB3 AND VB3 INTERSECTION IAW EMB145 SRM 52-30-01 RE ITEM 12 FIGURE 213, EMBRAER ETD2024-145-015164, AND EO1-52-24-0344

Part: SKIN — NONE (NONE) · airframe 52,406 hrs · 49,389 cycles

E040142 NO REPAIR INFO FOUND FOR FUSELAGE EXTERNAL SKIN DOUBLER AT FR15/16 STR 16R/17R. REMOVED EXISTING REPAIR DOUBLER BTW FR 15-16, STR 16R-17R IAW EMB 145 SRM 51-40-02 AND ACCOMPLISHED (CIRCULAR TYPE A) REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0399, EMB 145 IC2005-145/3540 AND PRINCIPLES OF EMB145 SRM 53-21-01, ITEM 4, FIG 206

Part: FITTING — WORN (AILERON PCA) · airframe 52,406 hrs · 49,389 cycles

E039831 LH AILERON PCA ACTUATOR FITTING HAS WORN / GOUGED LUG HOLE. REMOVED AND REPLACED LH AILERON PCA ACTUATOR FITTING IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.

Part: SHEAR TIE — CRACKED (FR 66 S7-9L) · airframe 52,406 hrs · 49,389 cycles

E039805 CARGO SHEAR CLIP AT FR-66 BETWEEN STGRS 7L/9L HAS A CRACK. REMOVED CRACKED SINGLE PIECE SHEAR CLIP. IN CARGO AT FR-66 BETWEEN STGRS 7L/9L AND INSTALLED 2PC REPAIR SHEAR CLIP IAW PIEDMONT EO1-53-24-0401 AND EMB145 SRM 53-31-04RE, ITEM 2, FIG 203

Part: NONE — NONE (NONE) · airframe 52,406 hrs · 49,389 cycles

E039702 NO REPAIR INFO FOUND FOR RUDDER II LH SKIN DOUBLER AT NUTPLATE HOLE ABOVE PANEL 327CL. ACCOMPLISHED REPAIR ON RUDDER II LH SKIN AT NUTPLATE HOLE ABOVE PANEL 327CL IAW PIEDMONT EO1-55-24-0396 AND ETD2018-145-015492.

Part: FITTING — GOUGED (AILERON PCA) · airframe 52,406 hrs · 49,389 cycles

E039830 RH AILERON PCA ACTUATOR FITTING HAS WORN / GOUGED LUG HOLE. REMOVED AND REPLACED RH AILERON PCA ACTUATOR FITTING IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.

Part: SHEAR TIE — CRACKED (FR 61 S6-7L) · airframe 52,406 hrs · 49,389 cycles

E038933 CARGO SHEAR CLIP AT FR-61 BETWEEN STGRS 6L/7L HAS A POSSIBLE CRACK. REMOVED AND REPLACED CARGO SHEAR CLIP AT FR-61 BETWEEN STGRS 6L/7L IAW EMB 145 SRM 51-40-02.

Part: PROFILE — CRACKED (LT OVERWING) · airframe 52,406 hrs · 49,389 cycles

E039053 LH OVERWING ESCAPE HATCH FWD PROFILE CRACKED AT LOWER END. REMOVED CRACKED LH OVERWING ESCAPE HATCH FWD PROFILE AND INSTALLED SERVICEABLE PROFILE IAW EMB 145 SRM 51-40-02.

Part: SKIN — GOUGED (FR 70 S12-13R) · airframe 52,406 hrs · 49,389 cycles

E038958 CARGO FR-70 BETWEEN STGRS 12R/13R IS GOUGED AT PREVIOUS REPAIR. REPAIRED CARGO FR 70 BTW STR 12R-13R GOUGE AT PREVIOUS REPAIR IAW EO1-53-24-0394 AND ETD2018-145-123916 REV A.

Part: ACCESS DOOR — GOUGED (COCKPIT) · airframe 53,406 hrs · 49,389 cycles

E038880 COCKPIT UNDERFLOOR ACCESS HATCH (123BL) EXTERIOR SKIN HAS 1 GOUGE. REPAIRED COCKPIT UNDERFLOOR ACCESS HATCH (123BL) EXTERIOR SKIN 1 GOUGE IAW PIEDMONT EO1-52-24-0394 AND ETD2024-145-014341.

Part: SHEAR TIE — CRACKED (FR 67 S6-7R) · airframe 52,406 hrs · 49,389 cycles

E038940 CARGO FR-67 BETWEEN STGRS 6R/7R HAS SHEAR CLIP WITH A POSSIBLE CRACK. REMOVED AND REPLACED SHEAR CLIP AT FR67 BETWEEN 6R ANDS 7R IAW EMB 145 SRM 51-40-02

Part: DOUBLER — NONE · airframe 52,406 hrs · 49,389 cycles

E039073 NO REPAIR INFO FOUND FOR PASSENGER DOOR LOWER FRAME FWD DOUBLE. REMOVED EXISTING REPAIR ON PASSENGER DOOR LOWER FRAME FWD DOUBLER IAW EMB 145 SRM 51-40-02. PERFORMED REPAIR TO SAME AREA OF LOWER FRAME IAW PIEDMONT EO1-52-24-0397 AND ETD-2024-145-016728.

Part: SHEAR TIE — CORRODED (FR 65) · corrosion level 2 · airframe 52,406 hrs · 49,389 cycles

CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP ABOVE LWR CENTER SILL IS CORRODED. REMOVED EXISTING CORRODED SHEAR CLIP SECTION ON CARGO DOOR FUSELAGE CUT-OUT AT FR 65 ABOVE CENTER SILL AND ACCOMPLISHED REPAIR AT AREA IAW PIEDMONT EO1-53-24-0398

Part: SKIN — CHAFED (RUDDER) · airframe 52,406 hrs · 49,389 cycles

E038379 RUDDER 1 EXTERNAL SKIN CHAFED JUST ABOVE ACCESS PANEL 326EL. PERFORMED DOUBLER REPAIR FOR RUDDER 1 EXTERNAL SKIN JUST ABOVE ACCESS PANEL 326EL IAW ETD2024-145-015198 AND EO1-55-24-0357

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 52,406 hrs · 49,389 cycles

E037244 LH PYLON CENTER FIREWALL CRACKED. RAR LH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0327

Part: FIREWALL — CRACKED (RT NACELLE) · airframe 52,406 hrs · 49,389 cycles

E037246 RH PYLON CENTER FIREWALL CRACKED. RAR RH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0326

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,406 hrs · 49,389 cycles

E037054 EXTERIOR FUSELAGE RH DV WINDOW CUTOUT AFT UPPER CORNER IS CRACKED. REPAIRED CRACKED EXTERIOR FUSELAGE RH DV WINDOW CUTOUT AFT UPPER CORNER IAW PIEDMONT EO1-53-24-0335 AND EMB 145 ETD2024-145-013969

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,709 hrs · 48,609 cycles

ON APPROACH WHEN SELECTING FLAPS TO 9 FLAP FAIL ON EICAS. FLAPS REMAINED AT 0. UPON ARRIVAL TO A/C, FLAP FAIL EICAS MSG WAS HARD FAULT. RESET FLAP 1/2 C/B NO FIX. PERFORMED FLAP RESET. EICAS MSG EXTINGUISHED AND FLAPS OPERATED NORMALLY. CHECKED FECU , NVM, NO CODES STORED. R/R'D FECU AS PRECAUTION REF AMM 27-53-02. OPS CHECK GOOD, OK FOR SERVICE AT THIS TIME.

Part: DISTRIBUTION BOX — BURNED (LEFT) · airframe 51,349 hrs · 48,216 cycles

SMOKE COMING OUT OF LEFT DISTRIBUTION BOX. CAPTAIN SAID ONLY A COUPLE OF CLEANERS WERE ONBOARD DURING PREFLIGHT THE CAPTAIN SAID THEY SMELLED AN ELECTRICAL BURING SMELL THAT CAME FROM LEFT DISTRIBUTION BOX. FOUND K0291 BURNT, REMOVED AND REPLACED APU LINE CONTACTOR IAW AMM 24-34-03.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,294 hrs · 48,149 cycles

DUURING CLIMB AROUND 9000FT LOUD POP HEARD THEN CABIN STARTED TO DEPRESSURIZE...NOTE PACK 1 CURRENTLY ON MEL. REF LP 289288 SEQ 1 FOUND BLOWN DUCT ON #2 HEAT EXCHANGER. R&R'D DUCT A/C PRESSURIZED CHECK GOOD. #2 PACK OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN)

AFTER TAKEOFF NO CABIN ALT OR CABIN RATE PRESENTED. ONLY DASH MARKS

Part: NONE — NONE · airframe 48,951 hrs · 45,395 cycles

PDIS 649 21-32 2725351 23APR22 CLT CLOSE AT 34,000 FEET. CABIN DIFFERENTIAL PRESSURE INDICATED 8.1 IN AMBER. CABIN ALTTITUDE INDICATED 9700. INDCATIONS STABILIZED AFTER DESCENT DOWN TO 15K FEET (CAB ALT INDICATED 2300 FT). PRESURIZATION CONTROL IN AUTO MODE. FACT 23APR22 20:09 CLT MX RE-ACTIVATED AND SECURED THE ELECTRO-PNEUMATIC VALVE OPEN, SEE LOGPAGE 272536-1 FOR NEW DEFERRAL. SUPPLEMENTAL INFORMATION: R&R'D MANUAL PRESSURE CONTROLLER IAW AMM 21-32-02. OPS CHECK GOOD IAW AMM 21-31-00-700-801A. CLEAR MEL

Part: AUDIO PANEL — FAULTED · airframe 48,825 hrs · 45,259 cycles

FO COMM POS UNABLE TO HEAR FA OR ALTITUDE ALERTING SYS. UNABLE TO DISCERN FROM CAPT AND ATC. WHEN USING OBS DAP AND JACK NORMAL OPS. NOTE CONSTANT BACK- GROUND NOISE LIKE AN OPEN MIC ON FO SIDE. CREW ALSO REPORTED SQUEAL ON COMM 3. REMOVED AND REPLACED DIGITAL AUDIO PANEL IAW AMM 23-51-01. OPERATIONAL TEST GOOD. OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 48,586 hrs · 44,991 cycles

PDIS 649 34-32 2749062 07FEB22 CLT CLOSE ON APPROACH TO FAY, BOTH LOC DROPPED OFF WITH RED X ACROSS CDI, SIGNAL WAS VERY WEAK FACT 07FEB22 17:38 CLT PERFORMED VOR/ILS/GS/MB OPS CHECK IAW AMM 34-32-00-700-801-A AND PERFORMED SENSITIVITY TEST WITH TEST BOX T-36C, OPS CHECK GOOD. A/C OK FOR SERVICE FOLLOWUP WAS C/W: CHECKED SIGNAL BALANCE AND LOC RECEIVER AFTER R+R OFNAV UNIT. REFERENCE LOGBOOK PAGE 274908 SEQ 1 FOR SIGNOFF OF R+R OF NEW UNIT. FOUND TO BE WITHIN LIMITS

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

L/H WING RIB 21 INSIDE 551CB CRACKED .... PERFORMED REPAIR ON L/H WING RIB 21 INSIDE 551CB PNL IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 DET C AND PIEDMONT EO1-57-21-0280

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

SERVICE DOOR CUTOUT FR 22 CORRODED UNDERNEATH LOWER AFT SERVICE DOOR STOP .... INSTALLED FR-22 BETWEEN STGR 8R-17R, AND DOUBLER REPAIR PARTS IAW ETD2021-145-031861 AND PIEDMONT EO1-53-21-0278

Part: NONE — CORRODED · airframe 48,074 hrs · 44,390 cycles

CORROSION ON RH LAV-TO-CARGO BULKHEAD SUPPORT (BANANA PANEL) LOWER END AT FRAME 61 .... REMOVED CORROSION ON LOWER END OF RH LAV-TO-CARGO BULKHEAD SUPPORT (BANANA PANEL) AT FRAME 61 IAW EMB145 SRM 51-10-03. FOUND CORROSION ON RH LAV-TO-CARGO BULKHEAD SUPPORT (BANANA PANEL) TO BE EXTENSIVE AND BEYOND ANY ALLOWABLE LIMITS. REMOVED AND REPLACED RH LAV-TO- CARGO BULKHEAD SUPPORT (BANANA PANEL) AT FRAME 61 IAW EMB145 SRM 51-40-02, EMB 145 SRM 51-20-03, AND EMB 145 SRM 51-40-09.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

STRINGER 17R CORRODED BETWEEN FRAMES 19A - 20 AND FRAMES 22- 22A .... REMOVED, PREPPED, AND INSTALLED STRINGER 17R REPAIR SECTION, STRINGER SPLICE, AND JSHAPE IAW EMB 145 SRM 53-00-03 ITEM 7. 51-40-02 AND EO1-53-21-0282

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

RUDDER 2 LH AND RH SIDE SKINS HAVE A HOLE IN THE LOWER TRAILING EDGE .... ACCOMPLISHED REPAIR OF RUDDER 2 LH AND RH SIDE SKINS AT LOWER TRAILING EDGE IAW ETD# ETD2021-145-033969 AND EO1-55-21-0290

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

LH OMEGA BEAM SEAT TRACK #6 IS CORRODED AT NUMEROUS AREA'S .... PERFORMED BLEND OUT OF DAMAGE IAW EMB 145 SRM 51-10-03 AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW EMB 145 SRM 53-00-11. EASI 7496. RAR LH OMEGA BEAM SEAT TRACK #6 IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

LH OUTBD UPPER SEAT TRACK #4 IS CORRODED AT NUMEROUS AREA'S .... REMOVED AND INSTALLED LH OUTBD SEAT TRACK #4 IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

SUPPLEMENTAL INFORMATION - DUPLICATE DISCREPANCY - NEW DISCREPANCY - CENTER BEAM SEAT TRACK #5 IS CORRODED AT NUMEROUS AREA'S .... PERFORMED BLEND OUT OF DAMAGE IAW EMB 145 SRM 51-10-03 AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW EMB 145 SRM 53-00-11. EASI 7496. RAR CENTER BEAM SEAT TRACK #5 IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

RH OUTBD UPPER SEAT TRACK #3 IS CORRODED AT NUMEROUS AREA'S .... REMOVED AND INSTALLED SERVICEABLE R/H UPPER OUTBD #3 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

LH OUTBD UPPER SEAT TRACK # 6 IS CORRODED AT NUMEROUS AREA'S .... REMOVED AND INSTALLED LH OUTBD UPPER SEAT TRACK # 6 IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

CENTER OMEGA BEAM SEAT TRACK #4 IS CORRODED AT NUMEROUS AREA'S .... REMOVED AND INSTALLED CENTER OMEGA BEAM SEAT TRACK #4 IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

CENTER OMEGA BEAM SEAT TRACK #3 IS CORRODED AT NUMEROUS AREA'S .... RAR CENTER OMEGA BEAM SEAT TRACK #3 IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

SERVICE DOOR ENTRANCE SILL HAS CORROSION .... PERFORMED DOUBLER REPAIR ON SERVICE DOOR ENTRANCE SILL CENTER AND AFT NUTPLATES IAW EMB-145 SRM 53-21-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

LH OUTBD UPPER SEAT TRACK # 5 IS CORRODED AT NUMEROUS AREA'S .... REMOVED AND REPLACED LH OUTBD UPPER SEAT TRACK # 5 IAW EMB 145 AMM 53-01-03.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

RH OUTBD FLOOR SILL IS CORRODED UNDER CARBON BEAM BTW FR 60-61 .... REMOVED CORRODED RH OUTBOARD FLOOR SILL UNDER CARBON BEAM BTW FR 60-61 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02, EMB 145 SRM 51-20-03, EMB 145 SRM 51-40-09.

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

PILOTS AFT BULKHEAD LOWER PIN HOLE CHAFED .... REMOVED DAMAGED PREVIOUS REPAIR DOUBLER FROM PILOT'S SIDE AFT BULKHEAD LOWER GUIDE PIN HOLE AND FABRICATED AND INSTALLED NEW SACRIFICIAL PLATE AND DOUBLER IAW EMB-145 SRM 53-21-02 RE ITEM 4 AND PIEDMONT EO1-53-21-0279

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

LH OUTBD FLOOR SILL #6 IS PITTED .... REMOVED AND INSTALLED NEW LH OUTBD FLOOR SILL #6 IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

RH OUTBD UPPER SEAT TRACK #5 IS CORRODED AT NUMEROUS AREA'S .... RAR OTBD UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-05.

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

FUSELAGE FRAME 25 CRACKED BETWEEN STRINGERS 15R AND 16R EVALUATION .... REMOVED, FABRICATED AND INSTALLED NEW SERVICEABLE FR25 FRAME SECTION (LOCATED FROM STR 15R TO STR 20R ) AND INSTALLED INTERNAL "U" SHAPED SPLICE DOUBLER IAW EMB145 SRM 53-00-04RE, ITEM 4, FIG 201 AND SRM 51-40-02 AND EO1-53-21-0266

Part: NONE — NONE · corrosion level 2 · airframe 48,074 hrs · 44,390 cycles

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

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

BAGGAGE DOOR WEBBING IS GOUGED ON PREVIOUS REPAIR 2 EACH .... FABRICATED AND INSTALLED SERVICEABLE REPAIR DOUBLER ON BAGGAGE DOOR INNER WEBBING (LOWER CENTER AREA) IAW EMB 145 SRM 52-30-01, ITEM 12, FIG. 213 AND EO1-52-21-0264

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 21 RIVETS AT FR 77 BTW STR 2R-9R .... PERFORMED PT INSPECTION IAW EASI NDTM. FOUND CRACKS AT 1 RIVET .... ACCOMPLISHED REPAIR OF CRACKED SKIN AROUND 1 FASTENER AT FR 77 BTW STGR 3R-4R IAW EMB 145 SRM 53-32-01 ITEM 9 AND EO1-53-21-0288

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 13 RIVETS AT FR 79 BTW STR 3L-9L .... PERFORMED PT INSPECTION IAW EASI NDTM. FOUND CRACKS AT 2 RIVETS. CRACK ENDS MARKED. EASI S/N 0452 .... ACCOMPLISHED REPAIR OF SKIN CRACKS AT 2 FASTENERS AT FR 79 BTW STGR 3L-4L AND STGR 8L-9L IAW EMB 145 SRM 53-32-1 ITEM 9 AND EO-1-53-21-0287

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

DENT AT L/H FWD FUSELAGE BETWEEN FRAMES 6 AND 7 AND STRINGERS 16L AND 17L UNDER GPU ACCESS PANEL .... ACCOMPLISHED REPAIR OF DENT ON LH FWD FUSELAGE BETWEEN FR 6 AND 7 UNDER GPU ACCESS PANEL IAW EMB 145 SRM 53-12-01 ITEM 2 AND FIGURE 201 AND EO1-53-21-0281

Part: NONE — NONE · airframe 48,074 hrs · 44,390 cycles

LAV WASTE BUCKET CORRODED AROUND DUMP HANDLE....RAR LAV WASTE BUCKET IAW EMB-145 SRM 51-40-02.

Part: CONNECTOR — DISCONNECTED (PROX SWITCH) · airframe 47,701 hrs · 43,976 cycles

AFTER T/O MLG A/G FAIL AND E 1/2 REV. DISAGREE MESSAGES DISPLAYED. T/S USING FIM 32-63-00-810-801-A BLOCKS 1-2 AND 12 THEN USED FIM 32-63-00-810-802-A BLOCKS 1-2 AND 3 WHILE INSPECTING THE NLG WOW PROX SWITCH FOUND ITS HARNESS AND CANNON PLUG TO BE DISCONNECTED AT THE NLG BULKHEAD. RESECURED CANNON PLUG AND L/G AIR GROUND FAIL MSG EXTINGUISHED. AC OK FOR SERVICE AT THIS TIME NO OTHER DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,273 hrs · 43,522 cycles

NDIS 649 33-50 0019460 13FEB21 RIC CLOSE LH EMERG EXIT LIGHT WILL NOT ILLUMINATE FACT 13FEB21 08:52 RIC R&R #500 EMERGENCY LIGHT AC/DC INVERTED IAW AMM 33-50-11-000/400-801-A OPS CHECK GOOD OK FOR SERVICE

Part: WARNING BUZZER — FALSE ACTIVATION · airframe 47,238 hrs · 43,474 cycles

PDIS 649 27-41 2557032 02FEB21 CLT CLOSE. AFTER TAKEOFF, PITCH AURAL WARNING CAME ON, FOLLOWED BY PTRIM MAIN INOP MSG ON EICAS, C/W QRH MSG DID NOT EXTINGUISH. BACK UP TRIM WORKED NORMAL. FACT 02FEB21 20:00 CLT. FOUND MAIN SYSTEM CUTOUT PUSHED IN. RETURNED TO NORMAL. FOLLOWED FIM TASK 27-43-00-810-801-A FOUND TO BE TRANSITORY. C/W OPS CHECK IAW AMM 27-40-00-700-802-A. OPS CHECK GOOD OK FOR SERVICE.

Part: HANDLE — MALFUNCTIONED (TE FLAP SYSTEM) · airframe 46,987 hrs · 43,191 cycles

AT 8000 FEET AT 240 KNOTS FLAP FAIL EICAS MESSAGE WHEN FLAP SELECTED TO 9 DEGREES. FLAPS REMAINED AT 0 DEGREES. MAINTENANCE: REMOVED AND REPLACED FLAP SELECTOR HANDLE, IAW EMB 145 AMM 27-53-03. OPERATIONS CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (LE FLAPS) · airframe 46,985 hrs · 43,189 cycles

PDIS 649 27-51 2313812 16NOV20 PWM. CLOSE FLAP FAIL EICAS MESSAGE FLT AT 240 KTS WHEN SELECTING FLAPS 9 DEGREES. FACT 16NOV20 23:26 PWM. R & R FLAP ELECTRONIC CONTROL UNIT WITH SERVICEABLE UNIT. WORK DONE, IN REF TO EMB 145 AMM 25-53-02. OPERATIONS CHECK GOOD.

Part: SKIN — DENTED (FRAMES 2-3) · airframe 46,898 hrs · 43,096 cycles

FWD FUSELAGE 1, TWO DENTS LOCATED BETWEEN FRAMES 2 AND 3, STR 04L AND 06L. MAINTENANCE REPAIRED, IAW E01-53-20-0357, EO1-53-20-0355, SRM53-10-01, AND SRM 51-75-04.

Part: CONNECTOR — NOT SEATED (HORIZONTAL STAB) · airframe 46,764 hrs · 42,930 cycles

BACKUP PITCH TRIM INOPERATIVE DURING CRUISE. CMC SHOWS HORIZONTAL STAB CONTROL UNIT FAILED. REMOVED AND RESEATED THE CONNECTOR PLUGS ON HSCU. RAN SYS, OPS CHECKED GOOD IAW AMM 27-40-01-000/400-801-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD PUMP) · airframe 46,729 hrs · 42,894 cycles

DURING CRUISE WITH ELEC PUMPS SET TO AUTO. HYD SYS 1 OVHT MESSAGE ON EICAS APPEARED.... HAS HISTORY. MAINTENANCE: T/S IN REF TO FIM 29-30-00-810-803-A STEPS 1 AND 5. GROUND RAN A/C AT 90%. NO DEFECTS NOTED. CLEANED CANNON PLUG AT THERMAL SWITCH. OPS CHECK GOOD OK FOR SERVICE.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 46,627 hrs · 42,764 cycles

DURING CLIMB HYD SYS 1 OVHT MESSAGE. PER QRH TURNED OFF HYD SYS 1. R & R ENGINE DRIVEN PUMP FOR NR 1 ENGINE IRW AMM 29-10-03. DURING TROUBLESHOOTING PER FIM 29-30-00-810-803A PER FIM 29-30-00-810-803A. R & R THERMAL SWITCH IRW AMM 29-30-05. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (INTERPHONE) · airframe 46,249 hrs · 42,331 cycles

NDIS 649 23-31 0010750 12FEB20 SBY CLOSE FWD F/A HANDSET/CRADLE EMERGENCY LIGHT INOP. 11412 00 BAD FACT 12FEB20 11:21 SBY R&R COCKPIT BULKHEAD ATTN HEADSET IAW AMM 23-31-03. OPS CHK GOOD. OK FOR RTS

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,730 hrs · 40,611 cycles

649 30-41 1912633 27MAY19 RIC CLOSE W/S HT 2 EICAS ASSOCIATED W/ BURN SMELL, SELECTED W/S HT 2 OFF, WAITED, SELECTED ON AND ODOR INTENSIFIED FACT 27MAY19 18:32 RIC INSPECT FLT DECK FOR DEFECTS IAW FIM 21-20-00-810-801-A. NO DEFECTS NOTED. PERF W/S HT OPS CHK IAW AMM 30-42-00-700-801-A. OPS CHECK GOOD OKAY FOR SERVICE AT THIS TIME.

Part: FUSE — BLOWN (WINDSHIELD HEAT) · airframe 44,730 hrs · 40,611 cycles

649 30-41 1912642 27MAY19 RIC CLOSE REF LP 1912643 WS HT 2 PLACED ON MEL AS PRECAUTION.PULLED AND COLLARED CB J20 PER MEL MX PROCEDURE MEL 27MAY19 15:45 RIC C14722 30-15 WINDSHIELD HEATING SYSTEMS FACT 28MAY19 05:36 PHL R&R FUSE F0002 IAW AMM 20-13-08-04. PERFORMED OPS CHECK IAW AMM 30-42-00. OPS CHECK GOOD. NO SMOKE OR SMELL NOTICED AT THIS TIME. CLEAR MEL 30-15

Part: RELAY — FAILED (K0173) · airframe 44,589 hrs · 40,448 cycles

PDIS 649 36-21 2050831 27APR19 PHL CLOSE BLD 1 VLV FAIL EICAS CAUT MESS ON T/O. 29061 00 LLS HISTORY: APR 17 FACT 28APR19 06:25 PHL T/S IN REF TO FIM 36-11-00-810-805-A RNR RELAY K0173 IN REF TO AMM 36-11-00 OPS CHECK IAW AMM 36-11-05-700-802-A OPS CHECK GOOD OK FOR SERVICE.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 44,537 hrs · 40,392 cycles

PDIS 649 36-21 2050731 17APR19 CLT CLOSE BLD 1 VLV FAIL MESS INTERMITTENT. MX DEACTIVATED NO1 BLD VALVE PER MEL MX PROCEDURES. FACT 17APR19 06:13 ROA R/R'D #1 ENG BLEED VALVE PER AMM 36-11-05. OPS CHECK S GOOD. OPS CK'D IAW EMB MM 36-11-05-700-802-A. CLEA R MEL.

Part: LEVER — MALFUNCTIONED (MLG) · airframe 44,464 hrs · 40,304 cycles

PDIS 649 32-30 2050593 02APR19 PHL CLOSE ON CLIMBOUT, LG/LEVER DISAGREE WARNING EICAS MESSAGE C/W QRH, OPS NORMAL. 31575 00 LLS FACT 02APR19 05:10 PHL T/S I.A.W EMB 145 FIM 32=32-00. R&R MODULE LEVER ASSY I.A.W EMB 145 AMM 32-32-02 OPS CHECK GOOD. PERFORMED LG EXTENSION AND RETRACTION I.A.W EMB 145 AMM 32-30-00 OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,339 hrs · 40,158 cycles

PDIS 649 27-60 1911341 08MAR19 PHL CLOSE AT TAKEOFF E1 T/R DISAGREE AND SPOILER FAIL EICAS MESSAGES. WHEN LANDING GEAR EXTENDED MESSAGES EXTINGUISHED. FACT 08MAR19 13:34 PHL OPS CHECKED THRUST REVERSER AND SPOILER SYSTEMS IAW AMM 27-63-01 AND 78-31-01. PERFORMED ELECTRICAL RESET. OPS CHECK GOOD. NO DEFECTS OR MESSAGES FOUND. OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 44,342 hrs · 40,162 cycles

NDIS 649 33-51 0003390 08MAR19 SBY CLOSE LT OVERWING EMERGENCY LIGHT INOP. FACT 08MAR19 10:27 SBY REMOVED AND REPLACED EMERGENCY LIGHT ON LT OVERWING POSITION OPS CHECK GOOD OK FOR SERVICE PART INSTALLED/REMOVED LAMP 1317.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 44,074 hrs · 39,859 cycles

PDIS 649 32-30 1914283 13JAN19 MDT CLOSE AFTER TAKEOFF GEAR UP CONSTANT KNOCKING NOISE HEARD IN FRONT AND BELOW FO, IN ADDITION LEFT MAIN DOOR INDICATION GOES FROM RETRACTED TO TRANSITION REPEATEDLY DURING FLIGHT. HISTORY: FACT 13JAN19 16:52 PHL REPLACED LT MAIN GEAR UPLOCK PROX SWITCH C/P, OPS CHECK GOOD. PROX SWITCH CHANGED AS PRECAUTION MEASURE. ALL WEATHER SEAL REPLACED. OK FOR SERVICE REF 32-61-01.

Part: WIRE HARNESS — DEFECTIVE (LANDING GEAR) · airframe 44,074 hrs · 39,859 cycles

PDIS 649 32-30 1914291 13JAN19 PHL CLOSE AFTER TAKEOFF GEAR CONSTANT KNOCKING NOISE HEARD INFRONT AND BELOW FO. IN ADDITION NR 1 HYD PRESSURE FLUCTUATION FROM 2900 TO 3000 PSI. KNOCKING NOISE AT SAME PACE AS PRESSURE FLUCTUATION. FACT 14JAN19 17:28 PHL TROUBLESHOT WITH EMB 145 FIM 32-61-00-810-801-A UP TO STEP 5. FOUND PIN A AT PLUG P0048 DID NOT HAVE ADEQUATE VOLTAGE. R&R UP PROX SWITCH 2 HARNESS ON LT WING AS REQUIRED. ELECTRICAL TEST GOOD. OPS CHECKED IAW AMM 32-30-00 OPS CHECKS GOOD OK FOR SERVICE.

Part: CONNECTOR — LOOSE (LANDING GEAR) · airframe 44,073 hrs · 39,857 cycles

PDIS 649 32-30 1914271 12JAN19 PHL CLOSE LEFT MAIN GEAR CYCLED UP AND DOWN WHEN ATTEMPTING TO RETRACT GEAR. CYCLED GEAR LEVER AND LEVER DISAGREE WARNING DISPLAYED. HISTORY: FACT 12JAN19 16:20 PHL FOUND PROX SWITCH CANNON PLUG LOOSE TIGHTENED AS REQUIRED C/W FIM TASK 32-32-00-810-803-A STEPS 1,2.9 AND 22 NO DEFECT FOUND TRANSITORY CONDITION OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 43,945 hrs · 39,714 cycles

DISCREPANCY: CEILING PANEL EMERGENCY LIGHT (AFT) AT EMERGENCY EXIT ROW DOES NOT ILLUMINATE. ACTION TAKEN: R&R CONNECTORS ON WIRE ENDS. OPS CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,943 hrs · 39,713 cycles

MAIN ENTRANCE DOOR EMERGENCY FLOOD LIGHT INOP-C/A-REMOVED AND REPLACED MAIN ENTRANCE DOOR EMERGENCY FLOOD LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD

Part: SKIN — CRACKED (CARGO DOOR) · airframe 43,942 hrs · 39,712 cycles

CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER CORNER-C/A-REPAIRED CARGO DOOR HANDLE CUOUT CRACK AT AFT UPPER CORNER IAW ERS-EM-52MR-936

Part: TRUNNION — CRACKED (RT AFT) · airframe 43,942 hrs · 39,712 cycles

RH AFT UPPER TRUNION CRACKED-C/A-REMOVED AND REPLACED RH AFT UPPER TRUNNION IAW ERS-EM-57MR-1053

Part: FRAME — GOUGED (FRM 70) · airframe 43,942 hrs · 39,712 cycles

FRAME 70 GOUGED BETWEEN STR 13R-12R INSIDE CARGO-C/A-REPAIRED FRAME 70 IAW ERS-EM-53MR-3535

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 43,942 hrs · 39,712 cycles

CENTER SERVICE DOOR SILL CORRODED AROUND 3 AFT RIVETS-C/A-REMOVED AND REPLACED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB145 SRM 51-40-02

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 43,942 hrs · 39,712 cycles

CARGO DOOR SILL CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW EMB 145 SRM 51-40-02

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 43,942 hrs · 39,712 cycles

EMERGENCY LIGHT STRIP #5 HAS BROKEN WIRE-C/A-REMOVED AND REPLACED #5 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.

Part: REPAIR — GOUGED (FRAME 64) · airframe 43,942 hrs · 39,712 cycles

FRAME 64 PREVIOUS REPAIR BETWEEN STR 6R-7R GOUGED-C/A-REMOVED AND REPLACED FRAME 64 PREVIOUS REPAIR IAW ERS-EM-53MR-XXXX

Part: LIGHT — DAMAGED (CABIN) · airframe 43,942 hrs · 39,712 cycles

LH #6 FLOOR PROXIMITY LIGHT DAMAGED-C/A-REMOVED AND REPLACED #6 FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,006 hrs · 38,804 cycles

DURING A PS-1 CHECK, FOUND THE LT EMERGENCY LIGHT ABOVE THE WING INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: ELECTRONIC UNIT — FAILED (MLG) · airframe 42,545 hrs · 38,395 cycles

LANDING GEAR FAILED TO RETRACT; LANDING GEAR LEVER DID NOT UNLOCK WHEN GEAR RETRACTION WAS SELECTED-C/A-REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW AMM TASK 32-32-01. OPS CHECK GOOD IAW AMM TASK 32-30-00. NO FURTHER DEFECTS NOTED.

Part: UPLOCK SENSOR — FAULTED (NLG) · airframe 42,337 hrs · 38,196 cycles

LG/LVR DISAGREE AFTER TAKE OFF, SOUNDED AS THE GEAR RETRACTED BUT DOORS DID NOT CLOSE. TROUBLESHOT IAW FIM 32-32-00-810-802-A, AND AMM 32-63-05-700-802--A. FOUND A FAULT WITH NLG UPLOCK BOX , REMOVED AND REPLACED THE UPLOCK BOX IAW AMM 32-33-07-400-801-A, ALL REQUIRED FUNCTIONAL AND OPERATIONAL CHECKED GOOD.

Part: COVER — OUT OF POSITION (PAX DOOR) · airframe 42,008 hrs · 37,891 cycles

TRIM PIECE ON MAIN DOOR STICKING UP MAKING IT HARD TO OPEN DOOR. REPOSTITION MAIN DOOR TRIM COVER ON SWING ARM OF MAIN CABIN DOORD IAW STANDARD MAINTENANCE PRACTICES. NO FURTHER DEFECTS NOTED.

Part: CLAMP — DAMAGED (PRECOOLER) · airframe 40,674 hrs · 36,674 cycles

PASSING 11,000 BLEED 1 MASTER CAUTION. RAN EPC & AOM1 CHECKLIST AND AFTER A PERIOD OF TIME, LESS THAN 3 MINUTES IT WENT AWAY. WAS IN ICING CONDITIONS WHEN HAPPENED. REMOVED AND REPLACED AFT V- CLAMP ON NR 1 ENGINE PRECOOLER IAW AMM 36-11-04. LEAK CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 40,542 hrs · 36,545 cycles

SMOKE IN THE COCKPIT AT FLT 300 ALL WINDOWS FROSTED ON INSIDE. VAPOR BEGAN COMING INTO COCKPIT AROUND DV WINDOWS. AT FLT 280 CREW NOTICED STRONG SMELL AND SMOKE ODOR IN COCKPIT DECLARED EMERGENCY LANDED LIT. ACCOMPLISHED ETN EM-72-034. NO FAULTS FOUND. FOLLOWED FIM 21-20-00 WITH NO DISCREPANCIES FOUND. FCF FOUND SATISFACTORY.

Part: CRADLE — CRACKED (FLASHLIGHT ASSY) · airframe 39,771 hrs · 35,847 cycles

AFT F/A FLASHLIGHT BASE CRACKED. REMOVED AND REPLACED THE FLASHLIGHT BASE IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,634 hrs · 35,706 cycles

EMERGENCY LIGHT NOT WORKING. REPAIRED WIRE W192-8830-22 IAW SWPM 20-21-00. OPS CHECKED GOOD IAW WC 33-700-17.

Part: ELEC CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 39,634 hrs · 35,706 cycles

CEILING PANEL 233BLC EMERGENCY LIGHT NOT WORKING. ON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR NOT CONNECTED. CONNECTED IAW SWPM 20-50-00. OPS CHECKED GOOD IAW WC 33-700-17.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,634 hrs · 35,706 cycles

EMERGENCY EXIT LIGHT CONNECTION AT FLOOR AT ROW 12 HAS BROKEN CONNECTOR. REPAIRED THE BROKEN WIRE IAW SWPM 20-50-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,634 hrs · 35,706 cycles

EMERGENCY LIGHT NOT WORKING. R & R THE BATTERY PACK AND POWER SUPPLY IAW WC 33-700-19. OPS CHECKED GOOD IAW WC 33-700-17.

Part: SKIN — DENTED (FRAME 4) · airframe 39,634 hrs · 35,706 cycles

DENT WITH POSSIBLE LIGHTNING STRIKE JUST FWD FRAMNE 4 BETWTEEN STRINGER 14 AND 15L. REPAIRED IAW ERS-EM-53MR-2352.

Part: BRACKET — CRACKED (FRAME 19) · airframe 39,634 hrs · 35,706 cycles

STRINGER 13L BRACKET AT FRAME 19 CRACKED. REPAIRED THE BRACKET IAW ERS-EM-53MR-2361.

Part: TRUNNION — CRACKED (LT MLG) · airframe 39,634 hrs · 35,706 cycles

LEFT AFT UPPER MLG TRUNION CRACKED. REMOVED AND REPLACED THE TRUNNION IAW ERS-EM-57MR-717.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 39,634 hrs · 35,706 cycles

OMEGA BEAM CORRODED UNDER CROSBEAM AT FRAME 59. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2350.

Part: DOOR FRAME — CORRODED (CARGO) · airframe 39,634 hrs · 35,706 cycles

CARGO DOOR LOWER FRAME ANGLE CORRODED AT NUTPLATE HOLES. BLENDED OUT THE CORROSION IAW SRM 51-10-03.

Part: SKIN — DENTED (FRAMES 71-72) · airframe 39,634 hrs · 35,706 cycles

REAR FUSELAGE SKIN DENTED BETWEEN FRAMES 71 AND 72, STRINGERS 21L AND 21R. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53DF-946 PART D.

Part: FRAME — CORRODED (FRM 65) · airframe 39,634 hrs · 35,706 cycles

CORROSION ON FRAME 65 AROUND NUTPLATE JUST FWD OF CARGO DOOR FWD TRACK LOWER END. PERFORMED REPAIR ON THE FRAME IAW ERS-EM-53MR-2351.

Part: BOOT — DAMAGED (SPEED BRAKE) · airframe 39,634 hrs · 35,706 cycles

LEFT NR 3 SPEED BRAKE PROXIMITY SWITCH PROTECTIVE BOOT DAMAGED. REPLACED THE PROTECTIVE BOOT IAW AMM 27-63-04. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FRAME 75) · airframe 39,634 hrs · 35,706 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R. CRACK IS APPROX. 3/8" LONG, PERFORMED A REPAIR IAW SRM 53-31-01 AND 51-40-02.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 39,002 hrs · 35,136 cycles

HYD SYS 1 QTY SHOWS HALF SCALE AND CREEPING LOWER. STILL IN GREEN RANGE INFLIGHT. VERY LITTLE HYDRAULIC DEMAND. DURING TROUBLESHOOTING FOUND LT MLG ACTUATOR LEAKING. R & R LT MLG ACTUATOR IAW AMM 323308. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,939 hrs · 35,071 cycles

CABIN EMERGENCY EXIT LOCATING SIGN AFT SIDE INOPERATIVE. REMOVED CABIN EMERGENCY EXIT LOCATING SIGN, REATTACHED WIRES AND REINSTALLED SIGN ASSY IAW AMM 33-50-15. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,482 hrs · 33,728 cycles

FLOOR EMER PROXIMITY LIGHTING STRIP AT ROWS 8 & 9 INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 37,482 hrs · 33,728 cycles

FLOOR EMER LIGHTING STRIP AT SEAT ROWS 6 & 7 HAS WIRES BROKEN OFF. R & R EMER FLOOR PROXIMITY LIGHT STRIP AT ROWS 6 & 7 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: DE-ICE VALVE — FAILED (WING) · airframe 36,416 hrs · 32,755 cycles

DURING THE ICE PROTECTION TEST, PNEUMATIC IN FLIGHT, THE LOCAL WING LIGHT DID NOT ILLUMINATE. 15 SECONDS INTO THE TEST EICAS DISPLAYED WING ANTI-ICE FAIL CAUTION MSG. TRANSFERRED TO NRWC 649-DFW-02152. R & R RELAYS K0528 & K0361. R & R NR 1 & 2 WING ANTI-ICE VLVS. OPERATIONS CHECKED GOOD AMM 20-13-02, 30-11-01 & 30-00-00. NO MSGS ON CMC. LT WING DE-ICE PN 10006491 & SN 200001059.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 36,377 hrs · 32,719 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FITTING — CRACKED (TE FLAP) · airframe 35,242 hrs · 31,806 cycles

INBOARD FLAP FITTING CRACKED. REPAIRED INBD FLAP FITTING IAW ERS-EM-57MR-320.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 35,123 hrs · 31,695 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

LEFT AFT FUSELAGE SKIN AT FRAME 75 STRINGER 2 UPPER & LOWER AREA HAS CRACKS MARKED. ACCOMPLISHED REPAIR OF LT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-789.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

FRAME 65 SHEAR CLIP AT CARGO DOOR CUT OUT CORRODED. SATISFACTORILY ACCOMPLISHED EM-53MR-1129.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

FRAME 68 SHEAR CLIP AT CARGO DOOR CUT OUT CORRODED. REPAIRED IAW EM-53MR-1129 PART B.

Part: SPAR — CRACKED (LT WING) · airframe 34,999 hrs · 31,565 cycles

LEFT WING SPAR 3 HARNESS HOLE IS CRACKED. COMPLETED INSTALLATION OF REPAIR DOUBLER ON LT WING SPAR 3 IAW ERS-EM-57MR-248. FOUND DURING EO EM-5700-662.

Part: RIB — GOUGED (LT WING) · airframe 34,999 hrs · 31,565 cycles

RIB OTBD OF LT WING STUB RIB II & FWD OF LT MLG WW GOUGED. R & R IAW SRM 51-40-02.

Part: WIRE — CRUSHED (CABIN) · airframe 34,999 hrs · 31,565 cycles

TWO WIRES CRUSHED FRAME 25 BETWEEN STRINGERS 15L - 16L. REPAIRED TWO WIRES W192-8680-22 & W192-8681-22 IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: FRAME — CHAFED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

FRAME 65 IS CHAFED ON RT SIDE. INSTALLED L DOUBLER ON FRAME 65 RT SIDE IAW ETD2014-145-076830.

Part: MOUNT — CRACKED (LT ENGINE) · airframe 34,999 hrs · 31,565 cycles

LEFT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IS CRACKED. REPLACED LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO EM-54MR-386.

Part: WIRE HARNESS — CHAFED (RT ENGINE) · airframe 34,999 hrs · 31,565 cycles

RIGHT ENG GREEN HARNESS CHAFING ON THE FIRE EXTINGUISHING TUBE AFT & ABOVE THE ATS. PERFORMED REPAIR IAW RR MM 70-00-00-300-804.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,999 hrs · 31,565 cycles

THE MOST AFT EMER FLOOR LIGHT STRIP CONNECTORS BROKEN ON ACFT SIDE. REPLACED IAW EMB-145 SWPM 20-21-00. SEE BOW164458 FOR OPERATIONS CHECK.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,999 hrs · 31,565 cycles

EMERGENCY LIGHT STRIP EXTRUSIONS NR 1, 2, 3, 4, 6, 7 & 8 ARE DAMAGED. REPLACED EMER LIGHT STRIP EXTRUSIONS IAW AMM 33-50-12. SEE BOW 164458 FOR FINAL INSTALL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

RIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND 3 FASTENERS ON FRAME 78 BELOW VERTICAL STAB. ACCOMPLISHED REPAIR OF RT FUSELAGE EXTERNAL SKIN AROUND 3 FASTENERS ON FRAME 78 BELOW VERTICAL STAB IAW ERS-EM-5300-735.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

RIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER ON FRAME 77 BELOW VERTICAL STAB. ACCOMPLISHED REPAIR OF RT FUSELAGE EXTERNAL SKIN AROUND 1 FASTENER ON FRAME 77 BELOW VERTICAL STAB IAW ERS-EM-5300-735.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

LEFT BEAM OTBD SUPPORT IS CRACKED AT FRAME 47. R & R FWD BEAM SUPPORT SECTION IAW SRM 53-23-02.

Part: CHARGER — BENT (FLASHLIGHT) · airframe 34,999 hrs · 31,565 cycles

PILOTS COCKPIT & CABIN PARTITION FLASHLIGHT CHARGER IS BENT. R & R PILOTS COCKPIT & CABIN PARTITION FLASHLIGHT CHARGER IAW EMB 145 AMM 33-50-16. OPERATIONAL CHECKED GOOD.

Part: TUBE — CHAFED (LT ENGINE) · airframe 34,999 hrs · 31,565 cycles

LEFT ENG FIRE EXTINGUISHING DISCHARGE TUBE IS CHAFED AT AFT OTBD END OF ENG. REPAIRED THE LT ENG FIRE EXTINGUISHING DISCHARGE TUBE, AT AFT OTBD END OF ENG IAW AMM 20-10-03.

Part: LIGHT — BROKEN (CABIN) · airframe 34,999 hrs · 31,565 cycles

NUMBER 8 EMER LIGHT STRIP IS BROKEN. R & R NR 8 EMER LIGHT STRIP IAW EMB 145 AMM 33-50-12. SEE BOW164458 FOR FINAL INSTALL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,999 hrs · 31,565 cycles

RIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER ON FRAME 79 BELOW VERTICAL STAB. ACCOMPLISHED REPAIR OF RT FUSELAGE EXTERNAL SKIN AROUND 1 FASTENER ON FRAME 79 BELOW VERTICAL STAB IAW ERS-EM-5300-735.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,916 hrs · 31,493 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL 25-53. ALL M PROCEDURES COMPLIED WITH. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL RESTORED PLACARDS REMOVED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 34,536 hrs · 31,130 cycles

FIRST OFFICERS FLASHLIGHT HOLDER BROKEN. FOUND DAMAGED WIRE & MADE REPAIR IAW AMM20-21-00. R & R FIRST OFFICERS FLASHLIGHT & CRADLE IAW AMM33-50-16. OPERATIONS CHECKED GOOD.

Part: ENGINE — ODOR (LEFT) · airframe 33,906 hrs · 30,599 cycles

ELECTRICAL BURNING ODOR & HAZE IN COCKPIT & FWD PART OF CABIN. R & R LT ENGINE IAW 71-000-00. OPS CHECKED GOOD. NO FURTHER ODOR NOTICED.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 33,649 hrs · 30,397 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 33,644 hrs · 30,390 cycles

ON FLIGHT 2768 LANDING GEAR RETRACT FAIL. ACFT WAS REMOVED FROM SERVICE. FOUND NLG WOW SWITCH HARNESS DAMAGED & INOPERATIVE. R & R HARNESS IAW AMM 32-20-01-841-001-A00 8 & AMM 32-20-01-842-001-A00 8.

Part: UNKNOWN — ODOR · airframe 33,601 hrs · 30,349 cycles

VERY STRONG SMELL, LIKE OIL, DURING DECENT FROM 13,000 TO 10,000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,416 hrs · 30,212 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IN SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,114 hrs · 29,968 cycles

LEFT FWD EXTERNAL EMERGENCY LAMP INOPERATIVE. R & R LT FWD EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-07-000-801-A & 33-50-07-400-801-A, OPERATIONS GOOD.

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHT) · airframe 32,722 hrs · 29,657 cycles

MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. FOUND THE GROUND WIRE FOR THE LIGHT ASSY LOOSE. SECURED GROUND WIRE IAW SWPM 20-13-05. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,403 hrs · 29,410 cycles

CREW REPORTED A BIRD STRIKE AT 12,000 FT, ON LT NOSE. A 6 INCH HOLE IN THE NOSE. ACFT REMOVED FROM SERVICE. REMOVED FUSELAGE SKIN AT FRAMES 1A TO 3 LT IAW SRM 51-40-02. REPLACED SKIN PANEL AND FRAME 2 ON LT FOWARD FUSELAGE 1 IAW SRM 51-40-02. ACFT RETURNED TO SERVICE.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 32,104 hrs · 29,154 cycles

DURING B INSPECTION, FOUND RT EMERGENCY MARKING SIGN ASSY BY OVERWING DOOR INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R AC/DC INVERTER NR 5 IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: COFFEEMAKER — SHORTED (GALLEY) · airframe 30,515 hrs · 27,927 cycles

ON FLIGHT 4326 THE CREW REPORTED ON TAXI OUT THEY NOTICED AN ELECTRICAL BURNING SMELL AND THE FLIGHT ATTENDANT ADVISED SHE SAW A MIST COMING FROM THE BULKHEAD IN FRONT OF ROW 3. THE CREW PERFORMED THE CABIN/COCKPIT FIRE/FUMES CHECKLIST AND TOLD THE GROUND THEY NEEDED TO RETURN TO THE GATE WITH CRASH, FIRE AND RESCUE TO MEET THEM. THE FIRE TEAM FOUND NO PROBLEM. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE INSPECTED AND FOUND PINS ON HOT JUG SHORTED. REMOVED AND REPLACED HOT JUG. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,383 hrs · 27,821 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 1 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,383 hrs · 27,821 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 4 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,383 hrs · 27,821 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 3 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 30,196 hrs · 27,669 cycles

AFT SCREW HOLE ON BOTTOM EDGE OF PAX DOOR IS CORRODED. REPAIRED AFT SCREW HOLE CORRODED AREA ON BOTTOM EDGE OF PAX DOOR IAW AEA EO-EM-52MR-331.

Part: LIGHT — CRACKED (CABIN) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE LEFT NR 1, 5 AND 6 PROXIMITY LIGHT FLOOR SIDEWALL ASSEMBLIES CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 5 AND 6 PROXIMITY LIGHT FLOOR SIDEWALL ASSEMBLIES IAW EMB AMM 33-50-2.1.(3) AND 3.I.(1). THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE LEFT OMEGA BEAM GUSSET CORRODED BETWEEN FRAMES 19-24. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED WITH SERVICEABLE GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE RIGHT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON THE RIGHT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE RIGHT FLOORBEAM DIAMOND GUSSET CORRODED AT FRAME 22. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM DIAMOND GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE RIGHT FLOORBEAM DIAMOND GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM DIAMOND GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06, AND EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE LEFT FLOOR SILL IS CORRODED BETWEEN FRAMES 61-65. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOOR SILL BETWEEN FRAMES 61-65 IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,240 hrs · 27,700 cycles

DURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE LEFT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON LEFT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,474 hrs · 27,117 cycles

DURING B INSPECTION, FOUND BOTH LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT LIGHT ASSEMBLY LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 28,576 hrs · 26,390 cycles

ON FLIGHT 4111 THE CREW REPORTED THAT ON THE DESCENT BELOW 20,000 FT AND BELOW 250 KT SELECTED FLAP 9 DEGREES AND RECEIVED A FLAP FAIL MESSAGE ON EICAS. FLAP LOCKED AT 8 DEGREES. FOLLOWED AOM VOL FLAP FAIL CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM TASK 27-51-00-810-804A. RESET FLAP SYSTEM. PERFORMED OPERATIONAL CHECK OF FLAP CONTROL SYSTEM. THE OPERATIONAL CHECK WAS GOOD - IAW AMM 27-51-00-700-801 A/501. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (FIRE DETECTOR) · airframe 28,576 hrs · 26,390 cycles

DURING MAINTENANCE INSPECTION UNSUCCESSFUL FIRE DETECTION SYSTEM TEST BAGGAGE EXTG BUTTON AND BAGGAGE SMOKE ON EICAS WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED CONNECTOR TO BOTH 1/2 FIRE DETECTORS. PERFORMED OPERATIONAL CHECK OF BAGGAGE FIRE DETECTION IAW EMB 145 MM 26-15-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,695 hrs · 25,741 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY CHARGE NR 4. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 26,823 hrs · 25,066 cycles

PAX DOOR HARD TO OPEN. ADJUSTED MAIN DOOR IAW EMB 145 AMM 52-18-00, OPS CHECK GOOD.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 26,823 hrs · 25,066 cycles

PAX DOOR HARD TO OPEN. ADJUSTED MAIN DOOR IAW AMM 52-18-00 OPS CHECKED GOOD.

Part: DOOR SEAL — DAMAGED (SERVICE DOOR) · airframe 26,606 hrs · 24,876 cycles

ON FLIGHT 3268 DURING CLIMB THE CREW REPORTED THE SERVICE DOOR SQUEAL AND A LOSS OF PRESSURIZATION. THE FLIGHT ATTENDANT REPORTED THAT HE COULD SEE DAYLIGHT. THE CREW ELECTED TO DIVERT TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. UPON INSPECTION FOUND AT LEAST 1/4 INCH GAP IN SEAL IN THE UPPER LEFT CORNER. DETERMINED THE AIR WAS RUSHING OUT LIKE A VACUUM CLEANER. GAP WAS SIZE OF AN INDEX FINGER. REPAIRED SERVICE DOOR AIR FRAME SEAL IAW EMB-145 AMM 52-00-04. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,155 hrs · 24,540 cycles

ON FLIGHT 4366 THE CREW REPORTED THE LEFT WING AFT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB PER EMB -145-AMM -33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 25,206 hrs · 23,814 cycles

DURING MAINTENACE BASE VISIT INSPECTION FOUND THE LEFT FORWARD VERTICAL STABILIZER FUSELAGE ATTACH ANGLE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD VERTICAL STABILIZER ATTACH ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 25,206 hrs · 23,814 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUIND FRAME 64 RIGHT UPPER INBOARD FACE DAMAGED. AIRCRAFT REMOVED FROM SERVICE. COMPLETED REPAIR TO FRAME 64 IAW EO EM-53MR-1709. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — DAMAGED (RT WING) · airframe 25,206 hrs · 23,814 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUIND THE RIGHT WING RIB 25 DAMAGED UNDER THE FLUX VALVE SUPPORT BRACKET. AIRCRAFT REMOVED FROM SERVICE. COMPLETED REPAIR TO FRAME 64 IAW EO EM-53MR-1709. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 25,206 hrs · 23,814 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RT FRAME 70 HAS TOOLING MARKS BETWEEN STRINGER 11 AND 12 RT. AIRCRAFT REMOVED FROM SERVICE. COMPLETED REPAIR TO RIB 25 RIGHT WING TIP IAW EO EM-57MR-515. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,014 hrs · 22,878 cycles

ON FLIGHT 3231 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE FORWARD LEFT OZONE. THE CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. WORK CARD 05-200-00 HAS BEEN COMPLIED WITH, NO DAMAGE WAS FOUND. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 23,849 hrs · 22,746 cycles

ON FLIGHT 2813 DURING THE CLIMB THE CREW RECEIVED A CARGO SMOKE INDICATION ON EICAS. THE CREW FOLLOWED THE AIRCRAFT OPERATIONS MANUAL AND RETURNED TO DFW. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT SMOKE DETECTOR IN C4 IAW EMB 145 AMM 26-15-01 AND THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 26-15-00. REMOVED AND REPLACED THE CARGO FIRE BOTTLE IAW EMB AMM 26-23-01. REMOVED AND REPLACED THE CARGO METERING FIRE BOTTLE IAW EMB 145 AMM 26-23-01. ALL OF THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 23,659 hrs · 22,585 cycles

ON FLIGHT 4014 DURING THE CLIMB THE CREW REPORTED SMOKE AND ELECTRICAL BURNING ODOR IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING FOUND NR 1 PACK AIR CONDITIONING UNIT INOPERABLE. REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE IAW EMB 145 AMM 21-51-03. THE OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,225 hrs · 20,532 cycles

ON PS CHECK AFT MOST FLOOR PROXIMITY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED PROX LIGHT STRIP. OPS CHECK GOOD. ACFT RETURN TO SERVICE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 19,770 hrs · 19,308 cycles

ON FLIGHT 3609 CREW REPORTED HYDRAULIC SYSTEM 2 LOW QUANTITY THEN HYDRAULIC SYSTEM 2 PUMP FAIL AND HYDRAULIC SYS 2 FAIL MESSAGE ON EICAS. CREW DECLARED A EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 HYDRAULIC PUMP PER EMB AMM 29-10-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — ODOR (COCKPIT) · airframe 17,101 hrs · 16,901 cycles

FO DISPLAY UNIT FLICKERED OFF THEN ON THEN EMITTED STRONG ELECTRICAL ODOR WHICH WAS NOTICED BY PASSENGERS IN THE CABIN. REPLACED DISPLAY UNIT.

Part: DUCT — CRACKED (ZONE 200) · airframe 15,917 hrs · 15,861 cycles

NUMBER 1 BLEED LEAK OCCURRED CLIMBING THROUGH 13,000 FEET, RETURNED TO ORD. REMOVED AND REPLACED T-DUCT BEHIND LEFT SIDE WALL IAW EMB 36-11-09. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT FORWARD LOWER CABIN SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT FORWARD CABIN SEAT TRACK BETWEEN FRAME 18 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT FORWARD LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 30 TO 50. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION ON LEFT LOWER CABIN SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION FOUND ON RIGHT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAMES 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 51-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 18 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,572 hrs · 15,709 cycles

CORRISION FOUND ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAMES 30 TO 35. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 30 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,742 hrs · 15,709 cycles

CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 30 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: LEVER — STUCK (COCKPIT)

ORD - FLT 4138 - FLAPS WERE STUCK AT 9 DEGREES NO ASSOCIATED EICAS MESSAGES OR ALERTS. CREW ELECTED TO RETURN. REPLACED FLAP SELECTOR LEVER IAW EMB AMM 27-53-03. OPS CHECK GOOD. NO OVERWEIGHT LANDING INSPECTION REQUIRED. VERT SPEED WAS LESS THAN 6 FPS. TRANSFERRED TO AML PAGE 2101443 PER 145 AMM 5-50-15. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (SPOILERS)

SPOILER FAIL MESSAGE ON EICAS DURING TAKEOFF ROLL. FOLLOWED FIM TASK 27-63-00-810-802 SYSTEM OPS CHECK GOOD AS PER AMM 27-63-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

EVV - FLT 4304 - OVERWING AISLE EMERGENCY EXIT SIGN FAILS TO ILLUMINATE. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FRAME 20)

PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PART. FABRICATED A FILLER, EXTERNAL ANGLE, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)

Part: FLOORBEAM — CORRODED (GALLEY)

THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED FORWARD DIGITAL. INSTALLED NEW DIGITAL IAW SRM. (K)

Part: SKIN — DENTED (FR 72, 74)

AIRCRAFT ARRIVED FOR REPAIR OF A DENT WITH A SCRATCH BETWEEN FRAMES 72 AND 74 AND STRINGERS14L AND 15L. REMOVED THE DAMAGE BY MAKING A CUT OUT. FABRICATED AN EXTERNAQL DOUBLER AND FILLER. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (GALLEY)

THE RT CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED RT CENTER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K)

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

PIT - FLT 4297 - DURING PREFLIGHT, CREW REPORTED THE FORWARD CENTER OVERWING EXIT SIGN TO BE INOPERATIVE. MAINTENANCE REPLACED SIGN ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SIGN — INOPERATIVE (OVERWING)

CREW NOTED WHEN DOING CABIN PREFLIGHT THE FORWARD CENTER OVERWING EXIT SIGN INOPERATIVE. REPLACED SIGN ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - FLT 3762 - FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (FWD CABIN)

ORF - FLT 4524 - AMBER FLOOR PROXIMITY LIGHT AT SERVICE DOOR FAILS TO ILLUMINATE. REPLACED SERVICE DOOR FLOOR EMERGENCY LIGHT STRIP ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

OMA - FLT 4079 - DURING PREFLIGHT, CREW REPORTED THAT SOME CABIN FLOOR PROXIMITY EMERGENCY LIGHTS AFT OF OVERWING EXITS DID NOT ILLUMINATE. AIRCRAFT WAS FERRIED TO ORD FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY AND INVERTER ASSEMBLY P/N 67343 IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (NR 4)

FLIGHT ATTENDANTS REPORTS REAR HALF OF EMERGENCY FLOOR EGRESS LIGHTS STAYS ON FOR 1-2 SECONDS AND THEN DIMS COMPLETELY DURING TEST. REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CMH - FLT 4401 - CRWE REPORTED THE EMERGENCY CABIN LIGHTS IN THE LAST THREE ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL MODULE — FAILED (EMERGENCY LIGHT)

DURING TAXI IN EMERGENCY LIGHT NOT ARMED MSG APPEARED ON EICAS NUMEROUS TIMES. R/R CONTROL MODULE ASSEMBLY, OPS CHECK GOOD. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT STRIP IS INOPERATIVE. LIGHT STRIP PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE INVERTOR ASSEMBLY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY EXIT LIGHT AT SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR FOR THE EXIT LIGHT TO BE DIRTY. THE CONNECTOR WAS CLEANED AND RESECURED. OPS CHECK OF EMERGENCY LIGHTS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TERMINAL BLOCK — DAMAGED (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY LIGHT NOT ARMED LIGHT ILLUMINATED DURING FLIGHT WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE GROUND BLOCK, GROUND JUNCTION, IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — INOPERATIVE (COCKPIT)

CREW REPORTED AN EMERGENCY LIGHT NO ARMED MESSAGE ON EICAS WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOOR)

DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTER 51-40-02 AND CPM 51-21-04, 51-21-05, 51-21-06, 51-61-00. (M)

Part: ODOR — DETECTED (COCKPIT)

ORD - FLT 4334 - CREW REPORTED A RUBBER ODOR IN MAIN CABIN AND COCKPIT IN FLIGHT. SHUT OFF GASPER AND RECIRCULATION FANS AND ODOR DECREASED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED GROUND OPERATIONAL CHECK OF APU AND AIRCRAFT BLEED SYSTEMS AND DETECTED NO ODOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)

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

ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LEFT OMEGA BEAM IAW EMB145 SRM 53-21-10 AND 51-40-02. (M)

Part: CAP — CORRODED (LT MLG) · corrosion level 3

ABI - THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM. LEFT AFT BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB 145 AMM 32-10-01-801-A. (M)

Part: CAP — CORRODED (RT MLG) · corrosion level 2

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27713. RIGHT AFT BEARING CAP CORRODED/PITTED. REMOVED AND REPLACED RIGHT MLG SWIVEL CAP, IAW EMB AMM 32-10-01-000-801-1 AND 32-10-01-400-801-A. (M)

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

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA CROSSBEAM AND PROFILE CORRODED. REMOVED AND REPLACED CROSSBEAM AND PROFILE IAW EMB SRM 51-40-02. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27707. GALLEY CENTER BEAM CORRODED AT FRAME 20. CENTER BEAM AT FRAME REPAIRED IAW EMB GST-3729/01. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 3

THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM. GALLEY AFT GUSSET CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-01. (M)

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

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA AT FRAME 20. REMOVED CORROSION. FABRICATED A DOUBLER AND INSTALLED IAW EMB 145 (SRM 145/1142 CHAPTER 53 REV 15) 53-21-10 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY FORWARD GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND CORROSION ON THE GALLEY CENTER OMEGA BEAM AT FRAME 20. REMOVED CORROSION. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER AND INSTALLED IAW EMBRAER GST-3729/01, PARA 5 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA CENTER BEAM GUSSET CORRODED. REMOVED AND REPLACED GUSSET IAW EMB 145 51-40-02 AND 51-40-06. (M)

Part: CONTROL UNIT — FAILED (HORIZ STAB)

ORD - FLT 4406 - DURING CLIMB-OUT, CREW NOTED ON EICAS PITCH TRIM 1 FAIL. NOTE YOKE SWITCHES DID NOT WORK BUT THE BACK UP TRIM DID. AIRCRAFT RETURNED TO ORD SAFELY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE REMOVED AND REPLACED HSCU IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ABI - FLT 9735 - THE FLIGHT CREW ABORTED TAKEOFF DUE TO BOTH THRUST REVERSER DISAGREE INDICATION. SERVICED NOSE STRUT IAW AMM. OPS CHECK GOOD. (M)

Part: INDICATOR — ILLUMINATED (ENGINE)

ABI - FLT 9735 - THE FLIGHT CREW ABORTED TAKEOFF DUE TO BOTH THRUST REVERSER DISAGREE INDICATION. (M)

Part: LEVER — INOPERATIVE (COCKPIT) · airframe 1,085 hrs · 1,155 cycles

AZO - FLT 4369 - DURING LANDING GEAR RETRACTION, CREW HEARD A NOISE THAT SOUNDED LIKE THE NOSE LANDING GEAR DOORS DID NOT CLOSE. NO VISIBLE DAMAGE NOTED ON POST-FLIGHT WALKAROUND. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB MM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)