N670AE

Part: CRADLE — INOPERATIVE (ZONE 200) · airframe 49,423 hrs · 45,097 cycles

COPILOT EMERGENCY FLASHLIGHT WILL NOT CHARGE FACT 14DEC25 10:16 ROA RAR FLASHLIGHT BASE IRT AMM 33-50-16 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 49,086 hrs · 44,719 cycles

OVHD EMERGENCY LIGHT AT ROW 11 INOPERATIVE. R & R EMERGENCY LIGHT ASSY ON SIDEWALL AT ROW 12 IAW AMM 33-50-14. OPS CK GOOD

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 44,054 hrs · 44,681 cycles

LH PAX EMERGENCY EXIT LATCH LIGHT PANEL INOPERATIVE. R & R PANEL IAW AMM3-50-14.

Part: FAN — FAILED (ZONE 200) · airframe 48,166 hrs · 43,646 cycles

LH SIDE ROW 4 THRU 6 HAD SMOKE. TURNED OFF RECIRC FAN AND SMOKE CLEARED. PERFORMED OPS CHECK OF AIR DISTRIBUTION SYSTEM IRW AMM 21-20-00 RAN PACK 1 AND 2 FOR 1 HOUR NO SMOKE OR SMELLS NOTED. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL LEVER — FAULTED (ZONE 700)

AT 330 ALT LG DISAGREE MESSAGE DISPLAYED. FOLLOWED QRH WOULD NOT CLEAR. TROUBLE SHOT IAW FIM 32-32-00-810-803-A STEPS 1, 2, 9, 22 NO FAULTS FOUND. R&R LANDING GEAR LEVER AS A MAINTENANCE PRECAUTION IAW AMM 32-32-02-04, OPS CHECK GOOD. OKAY FOR SERVICE AT THIS TIME

Part: EXCITER — FAULTED (NR 2 ENGINE) · airframe 53,043 hrs · 51,280 cycles

E2 HUNG START AT 30%N2 ON FADEC A. CREW STOPPED START SEQ WHEN FUEL SMELLED IN A/C. FACT 06DEC24 21:38 PHL R&R E2 LEFT IGNITION EXCITER IAW RRM 74-13-10. STARTED E2 OF BOTH FADECS. OPS CHECK GOOD. NO FUEL SMELL IN A/C WHILE RUNNING ENGINE. OK FOR SERVICE AT THIS TIME.

Part: A/C PACK — ODOR (ZONE 100) · airframe 47,097 hrs · 42,488 cycles

OIL SMELL FROM NO.1 BLEED SYSTEM CLEARS WHEN NO.1 PACK IS SHUT DOWN. FACT 22OCT24 12:50 CLT RAN PACKS ON APU FOR 15 MIN NO OIL SMELL NOTED OK FOR SERVICE AT THIS TIME CLEAR MEL 21-15-2

Part: ACM — FAILED (NR 1) · airframe 46,572 hrs · 41,882 cycles

SMOKE SMELL IN FLIGHT DECK WITH PACK 1 OPERATING. C/W FLT CREW PROCEDURES MEL 12JUL24 C19403 21-15-21 AIR COND PACK N650 AND ABOVE. FACT 12JUL24 DURING OPERATING THE PACK #1 FOUND #100 ACM MAKING SQEAKY/GRADING SOUNDS. R&R #100 ACM IAW AMM 21-51-03 OPS CHECK GOOD. NO BURN/SMOKE SMELL NOTICED. A/C GOOD FOR SERVICE. CLEAR MEL 21-15-2.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,570 hrs · 41,878 cycles

DURING HANDOVER NOTICED STRONG ELECTRICAL BURNING SMELL WITH VISIBLE SMOKE IN COCKPIT. FACT 11JUL24 19:48 LYH T/S ELECTRICAL BURNING SMELL WITH VISIBLE SMOKE. RUN BOTH PACKS WITH APU AND BOTH ENGINE BLEEDS, ALSO RUN IN BOTH AUTOMATIC AND MANUAL MODE. DID VISUAL INSPECTION ON PACK 1, IN NOSE BAY AND COCKPIT. NO BURNING SMELL AND VISIBLE SMOKE TO BE FOUND. OPS CHECK GOOD IAW 21-51-00. AIRCRAFT OKAY FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,459 hrs · 41,754 cycles

STRONG BURNING SMELL IN FLT DECK. RAN PACKS 1 AND 2 FOR SEVERAL HOURS OPENED PACK PANELS 1 AND 2 INSPECTED FOR SIGNS OF BURNING NO SMELL INSPECTED COCKPIT AVIONICS COMPONENTS NO SIGN OF BURNING SMELL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,348 hrs · 41,620 cycles

IN CRUISE LOUD POP FOLLOWED BY LOUD RUSHING AIR SOUND AT ROW 13. FACT 30MAY24 17:20 CLT INSPECTED ECS PACKS, RAM AND DUCTS WHILE A/C PRESSURIED TO 7PSI. NO LEAKS NOTED. PRESSURIED IAW AMM 21-31-00. CND A/C OK FOR SERVICE

Part: SHEAR TIE — CRACKED (FRM 25 S15-16R) · airframe 46,320 hrs · 41,592 cycles

E031785 SHEAR CLIP IS CRACKED AT FRAME 25 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SRM 51-40-02.

Part: REPAIR — CORRODED (FRM 20) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E035316 PREVIOUS REPAIR AT FR 20 CORRODED. REMOVED PREVIOUS CORRODED REPAIR AT FR 20, PERFORMED PERMANENT REPAIR TO LH OMEGA BEAM AT FR 20 IAW PIEDMONT EO1-53-24-0315 AND ETD2024-145-012944

Part: NUT PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E030534 CARGO DOOR STAY ROD STOW BRACKET NUTPLATES HAVE CORRISION. REMOVED AND REPLACED LOWER INBOARD L-PROFILE IAW EMB-145 SRM 51-10-03, SRM 52-30-04 AD, TABLE 101, FIGURE 101, AND SRM 51-40-02

Part: FRAME — CORRODED (FRM 20) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E033874 FRAME 20 CORRODED JUST ABOVE SERVICE DOOR LOWER CENTER SILL.. REMOVED CORRODED FR 20, PREPPED AND INSTALLED SERVICEABLE FR 20 BTW STGR 5R-18R IAW PIEDMONT EO1-53-24-0287, EMB 145 SRM 51-40-02 AND ETD2024-145-011775

Part: SUPPORT RIB — CRACKED (SERVICE DOOR) · airframe 46,320 hrs · 41,592 cycles

E033873 SERVICE DOOR INTERNAL WEB SUPPORT RIB AT STGR 11R CRACKED. REMOVED AND REPLACED SERVICE DOOR INTERNAL WEB SUPPORT RIB AT STGR 11R IAW EMB 145 SRM 51-40-02.

Part: STRINGER — CRACKED (FRM 13 S6R) · airframe 46,320 hrs · 41,592 cycles

E032626 STRINGER 6R IS CRACKED AT FRAME 13. REMOVED AND REPLACED STRINGER 6R AT FRAME 13 IAW EMB145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 46,230 hrs · 41,592 cycles

E032495 FR 20 CROSSBEAM CORRODED AT RH SIDE. : REMOVED AND REPLACED FR 20 CENTER AISLE CROSSBEAM IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032496 GALLEY FWD DIGITAL IS CORRODED AT LH AND CENTER BEAM POSITIONS ON AFT END. REPAIRED GALLEY FWD DIGITAL CORROSION AT LH AND CENTER BEAM POSITIONS ON AFT END IAW PIEDMONT EO1-53-24-0295 AND ETD2024-145-011366

Part: FLOOR SUPPORT — CORRODED (NR 2) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032414 CORROSION ON LH OMEGA BEAM #2 GUSSET. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE L/H OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NR 1) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032410 CORROSION ON CENTER OMEGA BEAM #1 GUSSET. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE CENTER OMEGA BEAM #1 GUSSET IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 62 S7-8R) · airframe 46,320 hrs · 41,592 cycles

E031914 SHEAR CLIP CRACKED AT FR62, BETWEEN STR 08R-07R. RAR SHEAR CLIP AT FR 62, BETWEEN STR 08R-07R IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED (CARGO) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E031897 CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 73 S9-10R) · airframe 46,320 hrs · 41,592 cycles

E031913 SHEAR CLIP CRACKED AT FR73, BETWEEN STR 10R-09R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 73 BETWEEN STRINGERS 10R-09R IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (NR 2) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E031924 CORROSION ON LH #2 OTBD SEAT TRACK. : REMOVED AND REPLACED THE LH #2 OTBD SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (NR 4) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032102 CORROSION ON RH OTBD #4 FLOOR SILL. REMOVED AND REPLACED RH OTBD #4 FLOOR SILL IAW EMB145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 75 S6-7L) · airframe 46,320 hrs · 41,592 cycles

E031911 POSSIBLE SHEAR CLIP CRACKED AT F75, BETWEEN STR 07L-06L. REMOVED CRACKED SHEAR CLIP AT FR 75 BTW 07L-06L, FABRICATED, PREPPED AND INSTALLED SERVICEABLE SHEAR CLIP IAW E01-53-24-0270, EMB 145 SRM 51-40-02, SRM 51-30-01 STEP 2.I

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032068 CORROSION ON LOWER SIDE OF CROSS FLOORBOARD SUPPORT ON LH SIDE IN LAV AREA. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE LOWER SIDE OF CROSS FLOORBOARD SUPPORT ON L/H SIDE IN LAV IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (NR 5) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E032103 CORROSION ON RH OTBD #5 FLOOR SILL. R & R R/H #5 OTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 58 S15-16L) · airframe 46,320 hrs · 41,592 cycles

E031803 SHEAR CLIP IS CRACKED AT FRAME 58 BETWEEN STRINGERS 15L-16L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 58 BETWEEN STRINGERS 15L-16L IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (NR 2) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E031925 CORROSION ON RH #2 OTBD SEAT TRACK. RAR RH #2 OTDB SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: SHEAR TIE — CRACKED (FRM 73 S9-10L) · airframe 46,320 hrs · 41,592 cycles

E031912 SHEAR CLIP CRACKED AT FR73, BETWEEN STR 10L-09L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 73 BETWEEN STRINGERS 10L-09L IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E031925 CORROSION ON RH #2 OTBD SEAT TRACK. RAR RH #2 OTDB SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: SHEAR TIE — CRACKED (FRM 56 S15-16L) · airframe 46,320 hrs · 41,592 cycles

E031804 SHEAR CLIP IS CRACKED AT FRAME 56 BETWEEN STRINGERS 15L-16L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 56 BETWEEN STRINGERS 15L-16L IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 26 S15-16R) · airframe 46,320 hrs · 41,592 cycles

E031786 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 15R AND 16R. : REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 24 S15-16R) · airframe 46,320 hrs · 41,592 cycles

E031784 SHEAR CLIP IS CRACKED AT FRAME 24 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SRM 51-40-02.

Part: RIB — GOUGED (LT WING) · airframe 46,320 hrs · 41,592 cycles

E031190 LH OTBD WING TIP RIB 25 LOWER AND UPPER SURFACE IS SCRATCHED AND GOUGED. REMOVED AND REPLACED LH OTBD WING TIP RIB 25 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 46,320 hrs · 41,592 cycles

E031218 POSSIBLE CRACK ON RH WING RIB 21 UNDER ACCESS PANEL 651CB. PERFORMED PERMANENT REPAIR TO CRACK ON R/H WING RIB 21 UNDER ACCESS PANEL 651CB IAW PIEDMONT EO1-57-24-0314, EMB 145 SRM 57-20-07, ITEM#4, FIGURE 203.

Part: DOOR FRAME — DAMAGED · corrosion level 2 · airframe 46,320 hrs · 41,592 cycles

E031373 SERVICE DOOR AFT FRAME IS CORRODED AT BOTTOM SCREW HOLE PREVIOUSLY BLENDED PAINTED BLUE. PERFORMED FRAME SPLICE REPAIR ON SERVICE DOOR AFT FRAME CUTOUT AND INSTALLED SERVICEABLE LOWER FRAME SECTION (FR22) IAW PIEDMONT EO1-53-24-0285, ETD2024-145-011218 REV A AND EMB 145 SRM 53-00-04 ITEM 17, FIG 209 SHEET 1 AND 2.

Part: DISPLAY — INOPERATIVE (EICAS) · airframe 46,269 hrs · 41,536 cycles

EICAS SCREEN WENT BLANK. FACT 29MAR24 20:52 CLT R/R EICAS DISPLAY IAW AMM 34-22-01 OPS CHK DONE IAW AMM 31-41-00 OPS CHECK GOOD A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN)

BLEED 1 LEAK EICAS MESSAGE DISPLAYED DURING CLIMB IN ICING. FACT: INSPECTED #1 PRECOOLER AREA AND FOUND CRACKED INLET DUCT TO PRECOOLER. R+R #1 PRE-COOLER IAW AMM 36-11-04. INSTALLED PRE-COOLER INLET DUCT IRT AMM 36-11-09. PERFORMED LEAK CHECK/OPS CHECK IAW AMM 36-00-00 OPS CHECK LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,082 hrs · 40,246 cycles

EMERGENCY LIGHTS IN CABIN TURN ON INTERMITTENTLY. ( CAPTAIN SAID ALL CABIN EMERGENCY LIGHTS WOULD TURN AND OFF LIKE HE WAS HITTING HIS SWITCH ) R&R ATTENDANT CONTROL PANEL IAW EMB-145 AMM 25-27-09 OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,875 hrs · 40,016 cycles

BLD 1 VLV CLOSED MSG IN FLIGHT. R&R ENG 1 BLEED VLV IAW AMM 36-11-05. NO FIX. R&R AIR COND. PNUMATIC PANEL IAW AMM 20-13-10. PERFORMED OPS CHECK IAW AMM 36-11-05 ON BOTH ENGINES. OPS AND LEAK CHECK GOOD. OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,873 hrs · 40,015 cycles

HYD 1 LOW QUANTITY DISPLAYED CRZ FACT 01JUL23 13:10 PHL FOUND NO. 1 ENGINE HYD PUMP LEAKING. R/R NO. 1 HYD PUMP IAW EMB 145 MM 29-10-03. OPS CHECK AND LEAK CHECK GOOD.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 44,177 hrs · 39,264 cycles

AFT EXT RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT ESPU IAW W/C 33-700-19, AFT EXTERIOR RT OVERWING EMERGENCY LIGHT OPS CHECK BAD IAW 33-700-17 REF. ITEM #2

Part: UPLOCK — FAULTED (NLG) · airframe 43,957 hrs · 39,041 cycles

ON DEPARTURE WHEN LANDING GEAR SELECTED UP THE NOSEWHEEL ONCE RETRACTED KEPT MAKING A NOISE SIMILAR TO A PISTON RAPIDLY FIRING FOR 45 SECONDS APPROX- FOLLOWED BY A WARNING CAUTION LIGHT WITH NO EICAS ALERT - NO TRANSITORY LIGHTS NOTED DURING GEAR RETRACTION. TRANSFERRED TO NRWC 670-ORD-06133. DECLARED EMERGENCY-C/A-RAR NLG UPLOCK BOX IAW EMB 145 AMM 32-33-07 OPS CHECK FUNCTIONAL LEAK CHECK GOOD SEE NRWC 670-ORD-06133 FOR ADDITIONAL WORK PERFORMED

Part: NONE — NONE · airframe 43,857 hrs · 38,936 cycles

WING ANTI ICE/PACK 2 BLEED FAIL. ICING CONDS INTO YUL. RETURN TO ORD. EMERGENCY DECLARED. NOT OVR WT LNDNG. FLT CONT WHILE T/S PACK 2 FAIL AND OVERHEAT (REF NRWC# 670-ORD-06037) FOUND #2 RECIRC FAN MUFFLER BLOWN/DAMAGED-C/A-RAR #2RECIRCULATION FAN MUFFLER IAW EMB 145 AMM 21-24-02. LEAK CHECK GOOD.

Part: NONE — UNSERVICEABLE (AFT CABIN) · airframe 43,823 hrs · 38,903 cycles

AFT EMERGENCY FLASHLIGHT HOLDER IS BROKEN AND LIGHT IS NOT CHARGING CORRECTLY-C/A-REPLACED AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 145 MM 33-50-16. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (RH) · airframe 43,594 hrs · 38,632 cycles

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

Part: SIGN — INOPERATIVE (AFT GALLEY) · airframe 43,574 hrs · 38,606 cycles

EMERGENCY EXIT LOCATING SIGN LIGHT INOP ON G2-C/A-RAR EMERGENCY EXIT LOCATING SIGN ON G2 IAW AMM 33-50-14 OPS CHECK GOOD.

Part: NONE — INOPERATIVE (#4) · airframe 43,532 hrs · 38,557 cycles

PERFORMING PS-1 EXTERIOR WALK AROUND FOUND BOTH OVER WING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY BATTERY PACK POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD OF L/H OVERWING LIGHT

Part: LAMP — INOPERATIVE (RH) · airframe 43,532 hrs · 38,557 cycles

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

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 43,468 hrs · 38,490 cycles

EMERGENCY EXIT LIGHT IN FRONT OF PAX SEAT 3BC INOP-C/A-RAR EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD.

Part: BRAKE ASSY — SMOKE (RH) · airframe 43,348 hrs · 38,378 cycles

SMOKE ON MLG. NITROGEN BASED FIRE EXTINGUISHER SPRAYED ON MLG. WHILE TAXIING IN TO PARK AFTER FLIGHT, GOUND OBSERVED A LOT OF SMOKE FROM RIGHT MAIN TIRE AREA. THEY ADVISED US WHILE WE WERE DISEMBARKING PASSENGERS. GROUND OPS APPLIED NITROGEN BASED FIRE EXTINGUISHER TO THE AREA AND SMOKING HAD CEASED BY THE TIME FIRE TRUCKS ARRIVED. RED FLUID OBSERVED AROUND BASE OF TIRE AND ON TIRE-C/A-#4 MLG BRAKE REQUIRES REPLACEMENT DUE TO CONTAMINATION.RAR #4 BRAKE IAW ENVOY MTX WC 32-600-14TS TO LEAK NEAR #3 BRAKE TOP BLEED FITTING. RAR #3 BRAKE IAW ENVOY MTX WC 32-600-14

Part: EICAS — FAULTY (COCKPIT) · airframe 43,333 hrs · 38,361 cycles

AT ROTATION EICAS MSG AIR-GROUND FAIL E1 E2 REV DISAGREE EMERGENCY DECLARED. -C/A- RAR W019 HARNESS & NLG WOW SWITCH IAW SWPM 20-21-01, AMM 32-00-03, AND AMM 32-63-05. OPS CHECK GOOD. REF NRWC'S 670-ORD-05800 THRU 05801 FOR SUPPORTING ACTION

Part: NONE — NONE · airframe 43,027 hrs · 38,016 cycles

SUPPLEMENTAL C/A FOR MECH. NO1 BLEED OVERHEAT /DIVR MCI . BLEED 1 OVERTEMP POSTED WHEN SWITCHING FROM APU BLEED TO ENGINE BLEEDS ABOUT 17,000 FT ALSO HAD A BURNING SMELL CLOSED ENG 1 BLEED PER QRH AND MESSAGE AND SMELL WENT AWAY.-C/A- RAR LH ACM. C/W ETN-EM-72-034. NO DISCREPANCIES NOTED.C/W N670 PRELIMINARY TRIAD WORK SCOPE 4-28-22. FOUND LH ACM SEIZED. NO CRACKED / DAMAGED / MISSING BLADES OR ROTOR CONTACT NOTED. SEE LGPG 4865479/2 FOR LH ACM RAR

Part: NONE — INOPERATIVE (G2) · airframe 43,024 hrs · 38,013 cycles

EMERGENCY LIGHT ON G2 INOP-C/A-RAR EMERGENCY LIGHT ON G2 IAW AMM 33-50-14 OPS CHECK GOOD.

Part: NONE — INOPERATIVE (AFT) · airframe 42,958 hrs · 37,941 cycles

AFT FA EMERGENCY LIGHT DOES NOT CHARGE-C/A-RAR AFT FA EMERGENCY LIGHT AND BATTERY IAW ETN-EM-33-059 OPS CHECK GOOD

Part: NONE — NONE · airframe 42,849 hrs · 37,835 cycles

SEAT 3B EMERGENCY EXIT PLACARD LIGHT INOP-C/A-RAR BATTERY POWER SUPPLY 2 AND BATTERY 2 IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 42,465 hrs · 37,403 cycles

FWD CABIN EMERGENCY LIGHT INOP-C/A-RAR FWD CABIN EMERGENCY BATTERY CHARGER ASSY AND BATTERY IAW ENVOY W/C 33-700-19. OPC GOOD. END.

Part: NONE — NONE · airframe 42,230 hrs · 37,139 cycles

ON CLIMB ABOVE 10000FT LOW CABIN PRESSURE EICAS MSG. CABIN ALT READ 11800FT. PRESSURIZATION ISSUES DECLARED EMERGENC.-C/A-RE-SET MANUAL PRESSURE CONTROL KNOB AND C/W AUTO AND MANUAL PRESSURIZATION SYSTEMS OPC IAW EMB 145 AMM 21-31-00. FOUND SATISFACTORY AT THIS TIME.

Part: NONE — NONE · airframe 42,205 hrs · 37,114 cycles

FLT DECK/ATTENDANT EMERGENCY FLASHLIGHT/HOLDER AFT FA FLASHLIGHT MISSING MEL 2532 - AUTH# 11-312M-C REPAIR REPAIR-C/A-RAR AFT CABIN FA EMERGENCY FLASHLIGHT IAW ETN-EM-33-059, MEL RESTORED, OPS CHECK GOOD

Part: NONE — NONE · airframe 42,197 hrs · 37,104 cycles

FA EMERGENCY FLASH LIGHT MISSING AFT CABIN-C/A-FLIGHT CREW PLACARDED AFT CABIN EMERGENCY FLASHLIGHT M PROCEDURES C/W AUTH# 110312M-C REF# 25-32 MOC# 206396

Part: NONE — NONE · airframe 42,110 hrs · 37,004 cycles

FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR FA EMERGENCY FLASHLIGHT AND HOLDER IAW ETN-EN-33-059. OPS CHECK GOOD.

Part: NONE — NONE · airframe 42,063 hrs · 36,946 cycles

AIR INTERRUPTED BACK TO ORD WITH A CABIN PRESSURIZATION ISSUE. CABIN ALTITUDE HIGH ON DEPARTURE DECLARED EMERGENCY.-C/A-CONFIRMED MEL 21-22 MAINT PROCEDURE HAVE BEN REV. PERFORMED PRESSURATION CONTROL SYSTEM OPS CHECK IN MANUAL M/M TASK 21-31-00-700-801A AND PRESSURATION CONTROL SYSTEM FUNCTIONAL TEST IN AUTO MOD IAW TASK 21-31-00-700-802A OPS CHECK GOOD

Part: NONE — NONE · airframe 41,972 hrs · 36,849 cycles

LG/ LEVER DISAGREE MASTER WARNING ON CLIMBOUT WITH LG / LEVER UP. RIGHT MLG INDICATED IN TRANSIT, THEN RED. LEFT MAIN GEAR AND NOSE NORMAL INDICATIONS.-C/A-PERFORMED T/S OF LG/LEVER DISAGREE IAW FIM 32-32-00-810-803. FOUND ONE CMC MESSAGE, LGEU AIR GROUND FAIL PRESENT. PERFOMED OPERATIONAL CHECK OF LANDING GEAR EXTENSION/RETRACTION IAW 145 AMM 32-30-00. RAR LGEU IAW 145 AMM 32-32-01. NO DEFECTS NOTED.

Part: NONE — NONE · airframe 41,971 hrs · 36,848 cycles

EMERGENCY FLOOR STRIPS #6, #7 AND #8 TURN ON INTERMTTENTLY-C/A-RAR #4 EMER LIGHT BATTERY IAW AMM 33-50-04 AND RAR #4 EMER BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK FAIL. REMOVED #6 INVERTER IAW AMM 33-50-11

Part: NONE — NONE · airframe 41,909 hrs · 36,777 cycles

BACK HALF OF FLOOR PROXIMITY EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY CHARGER AND BATTERY IAW AMM 33-50-04. OPS CHECK GOOD.

Part: NONE — NONE · airframe 41,909 hrs · 36,777 cycles

CANNED RH OVER WING EXTERIOR EMERGENCY LIGHT ASSY. (P/N 30-2510-3, S/S PT17781) FOR RON AIRCRAFT N698CB.-C/A-COMPLETE:INSTALLED NEW RH OVER WING EMERGENCY LIGHT ASSY IAW AMM 33-50-10.

Part: NONE — NONE · airframe 41,909 hrs · 36,777 cycles

LH AISLE EMERGENCY FLOOR LIGHT EXTRUSIONS AT ROWS 1-3, 7-10 AND 10-12 ARE BENT, DEFORMED OR BROKEN.-C/A-COMPLETE:REMOVED AND REPLACED L/H AISLE EMERGENCY FLOOR LIGHT EXTRUSIONS AT ROWS 1-3, 7-10 AND 10-12 IAW AMM 33-50-12. REF NRWC E 879845 FOR OPS CHECK.

Part: NONE — NONE · airframe 41,909 hrs · 36,777 cycles

#3 EMERGENCY LIGHT STRIP WIRING IS DAMAGED.-C/A-COMPLETE:REMOVED AND REPLACED L/H #3 EMERGENCY STRIP IAW AMM 33-50-12. REF BOW 358069 FOR OPS CHECK.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 41,661 hrs · 36,493 cycles

REAR CABIN EMERGECNY FLASHLIGHT MISSING.MEL 25-32 ORIGINAL AML PAGE 4538182 ITEM-C/A-INSTALLED NEW EMERGENCYFLASHLIGHT IN REF. TO AMM TASK 33-50-16. MEL IS RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,495 hrs · 36,292 cycles

RT OVERWING EMERGENCY LIGHT INOP. R & R RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. END.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,375 hrs · 36,151 cycles

BOTH EXTERNAL SIDE CENTER FAIRING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY BATTERY AND CHARGER IAW ENVOY MTX WC 33-700-19. OPC GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 41,281 hrs · 36,045 cycles

ABOVE DOOR EMERGENCY LIGHT BY THE SERVICE DOOR IS INOP-C/A-TROUBLESHOT EMERGENCY LIGHT, FOUND BAD INVERTER. RAR SERVICE DOOR ABOVE DOOR FRAME EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD, NO DEFECTS NOTED

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,080 hrs · 35,824 cycles

BOTH FLOOR EMERGENCY EXIT LIGHTS INOP-C/A-RAR #5 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW EMB AMM 33-50-11

Part: UNKNOWN — ODOR (ROW 12) · airframe 41,054 hrs · 35,796 cycles

FLIGHT ATTENDENT REPORTED BURNING SMELL NEAR ROW 12 SMELL WENT AWAY IN 5 MINUTES-C/A-COMPLIED WITH FIM TASK 21-20-00-810-801-A UP TO STEP 12

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,781 hrs · 35,505 cycles

RT EMERGENCY EXIT DOOR EXIT SIGN INOPERABLE. C/A: R & R NR 3 BATTERY PACK, IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. R & R BATTERY POWER SUPPLY, IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. OPERATIONS CHECK GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 40,303 hrs · 35,043 cycles

SEAT 12A EMERGENCY EXIT SIGN INOP. RESET ELECTRICAL CONNECTION ON INVERTER 4 IN REFERENCE WITH AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPS CHECKED GOOD.

Part: NUT PLATE — BROKEN (LIGHT HOUSING) · airframe 39,973 hrs · 34,691 cycles

RH OVERWING EMERGENCY LIGHT HOUSING HAS 1EA NUTPLATE BROKEN-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT HOUSING IAW EMB 145 AMM 33-50-10. OPS CK GOOD

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,973 hrs · 34,691 cycles

LH/RH OVERWING EXTERIOR EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY HOLDER AND BATTERY PACK IAW EMB 145 AMM 33-50-04. OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 11652

Part: FAN — MALFUNCTIONED (NR 1) · airframe 39,761 hrs · 34,504 cycles

ON ARRIVAL ELECTRICAL FUMES FOR ABOUT 3-5 MIN BEFORE CLEARING.-C/A-REMOVED AND REPLACED #1 RECIRC. FAN IAW AMM 145 21-24-01. OPS CHECK GOOD NO ELECTRCAL FUMES NOTED. FOUND RECIRC. #1 FAN NEARLY SIEZED COMPLETELY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,428 hrs · 34,188 cycles

PER PS-1, FOUND LH FUSELAGE EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH FUSELAGE EMERGENCY LIGHTBULB IAW EMB 145 AMM 33-50-10

Part: CONNECTOR — BURNED (HOT WATER POT) · airframe 39,319 hrs · 34,099 cycles

AT 26000 FT STRONG ELECTRICAL BURNING SMELL ON FLIGHT DECK AND ENTIRE CABIN, FOLLOWING FIM 25-31-00-810-810-A, FIM 21-20-00-810-801-A AND ETM-EM-72-034. FOUND THE RT HOT JUG CONNECTOR BURNED. REMOVED AND REPLACED RT HOT JUG CONNECTOR IAW CMM 25-32-62, OPS CHECKED GOOD.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 37,950 hrs · 32,973 cycles

BAGGAGE DOOR AFT TORSION BAR MECHANISM CENTER SUPPORT BRACKET IS CRACKED. -C/A-REMOVED AND REPLACED BAGGAGE DOOR AFT TORSION BAR MECHANISM CENTER SUPPORT BRAKET IAW SRM 51-40-02.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 37,950 hrs · 32,973 cycles

CARGO DOOR CUTOUT SILL IS CORRODED. -C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: CROSSBEAM — CRACKED (NLG) · airframe 37,950 hrs · 32,973 cycles

CROSSMEMBER ON THE AFT SIDE OF NLG UPLOCK BOX HAS A 1 1/2" CRACK.-C/A-REPLACED CROSSMEMBER ON AFT SIDE OF NLG UPLOCK BOX IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 37,950 hrs · 32,973 cycles

PAX DOOR INNER HANDLE LOCK BOX SUPPORT IS CRACKED. -C/A-REMOVED AND REPLACED PAX DOOR INNER HANDLE LOCK BOX SUPPORT BRACKET IAW SRM 51-42-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 37,950 hrs · 32,973 cycles

BAGGAGE DOOR AFT TORSION BAR SUPPORT BRACKET APPEARS TO BE CRACKED.-C/A-REMOVED AND REPLACED BAGGAGE DOOR AFT TORSION BAR SUPPORT BRACKET IAW SRM 51-40-02

Part: CHANNEL — CRACKED (FRAMES 47 - 48) · airframe 37,950 hrs · 32,973 cycles

R/H HAT BEAM SUPPORT IS CRACKED BETWEEN FRS 47 AND 48. -C/A-INSTALLED NEW R/H SUPPORT IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 37,950 hrs · 32,973 cycles

LEFT UPPER WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR 3 HAS A 3/4' CRACK. C/A-REMOVED AND FABRICATED NEW SECTION OF DAMAGED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR III IAW ETN-EM-53-142. 53-142.

Part: BRACKET — CRACKED (FRAME 61) · airframe 37,950 hrs · 32,973 cycles

FWD TORSION BAR BRACKET AT FRAME 61 FOR CARGO DOOR HAS A 1/8" CRACK. -C/A-REMOVED AND REPLACED FWD TORSION BAR BRACKET AT FRAME 61 IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 37,950 hrs · 32,973 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR 3 HAS 2 CRACKS. (APPROX. 1" AND 2" IN LENGTH). C/A-RAR DAMAGED SECTION RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR III IAW ETN-EM-53-142.

Part: LIGHT — DAMAGED (LAVATORY) · airframe 37,950 hrs · 32,973 cycles

AFT LH AND RH EMERGENCY FLOOR LIGHTING EXTRUSIONS IN LAV AREA DAMAGED-C/A-COMPLETE:AFT LH AND RH EMERGENCY FLOOR LIGHTING EXTRUSIONS ARE INSTALLED IN LAV AREA IAW AMM 33-50-12

Part: HANDLE — LOOSE (PAX DOOR) · airframe 36,698 hrs · 31,854 cycles

FLIGHT ATTENDANT HAVING HARD TIME OPENING AND CLOSING MAIN CABIN DOOR-C/A-FOUND MAIN CABIN DOOR UNABLE TO BE OPENED FROM INSIDE THE PLANE. DURING INSPECTION OF THE DOOR FOUND THE HANDLE LOOSE. RESECURED DOOR HANDLE IAW EMB145 AMM 52-18-05. OPPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 35,760 hrs · 30,972 cycles

MAIN DOOR HARD TO OPEN & CLOSE. CLEANED AND LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 52-18-00, OPS CHECKED GOOD.

Part: ROLLER — MALFUNCTIONED (PAX DOOR) · airframe 35,622 hrs · 30,838 cycles

FA ADVISED THE MAIN DOOR IS DIFFICULT TO OPEN. REMOVED AND REPLACED LOWER AFT MAIN DOOR ROLLER IAW EMB AMM 53-21-02 PERFORMED ADJUSTMENT OF LOWER AFT MAIN DOOR ROLLER IAW AMM 52-18-00. OPS CHECKED GOOD.

Part: FIRE WARNING — ILLUMINATED (CARGO) · airframe 35,441 hrs · 30,703 cycles

ACTIVATED THE CARGO FIRE BOTTLES DUE TO A CARGO SMOKE EPC. REMOVED AND REPLACED BOTH CARGO COMPARTMENT FIRE BOTTLES AND FWD AND AFT SMOKE DETECTORS IAW AMM 26-23-01, AND AMM 26-15-01, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 34,505 hrs · 29,865 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT CABIN FLASHLIGHT IAW EMB 145 AMM 33-50-16 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (CABIN LIGHTS) · airframe 34,403 hrs · 29,768 cycles

PAX CEILING LIGHT AT SEAT 3A INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-21-06, OP CHECKED GOOD.

Part: FRAME — CRACKED (FRM 67) · airframe 32,956 hrs · 28,590 cycles

LOWER END OF FRAME 67, FOUND CRACKED. REPAIRED THE FRAME IAW ERS-EM-53MR-2628, PART B.

Part: FRAME — CRACKED (FRM 66) · airframe 32,956 hrs · 28,590 cycles

LOWER END OF FRAME 66 CRACKED. REPAIRED THE FRAME IAW ERS-EM-53MR-2628, PART A.

Part: FRAME — CRACKED (FRM 73) · airframe 32,956 hrs · 28,590 cycles

FRAME 73 CRACKED AT STRINGER 17R. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-20-03, 51-40-02 AND ERS-EM-53MR-2639 R1, PART C.

Part: HANDLE — MISINSTALLED (PAX DOOR) · airframe 31,983 hrs · 27,709 cycles

F A UNABLE TO OPEN MAIN CABIN DOOR. FOUND MAIN PAX DOOR HANDLE INSTALLED INCORRECTLY. REMOVED AND REPLACED IAW MM 52-18-05. FUNCTIONAL CHECKED GOOD IAW MM 52-18-00-820-801 A .

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,867 hrs · 27,622 cycles

FA REPORTED MAIN CABIN DOOR DIFICULT TO OPEN. LUBRICATED ROLLERS IAW AMM 53-21-02. OPS CHECKED GOOD.

Part: SEAL — DAMAGED (CABIN DOOR) · airframe 31,838 hrs · 27,604 cycles

F/A STATED THE MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE. R & R PASSENGER DOOR FRAME SEAL AND ADJUSTED PASSENGER DOOR IAW NRWC 670-DFW-02612.

Part: DOOR SEAL — LACK OF LUBE (CABIN DOOR) · airframe 31,800 hrs · 27,568 cycles

F/A ADVISES MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. LUBRICATED MAIN ENTRANCE DOOR RUBBER SEAL IAW AMM 52-18-04, OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 31,498 hrs · 27,293 cycles

F/A REPORTS THAT MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. LUBRICATED DOOR ROLLER IAW ETN-EM-52-061, NO FURTHER DEFECTS NOTED.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 31,484 hrs · 27,279 cycles

F/A ADVISED MAIN DOOR HARD TO OPEN. LUBRICATED MAIN DOOR ACTUATING AND LOCKING MECHANISM IAW AMM-52-18-00, OPS CHECK SATISFACTORY.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 30,733 hrs · 26,611 cycles

FIRST OFFICERS AIRSPEED INDICATOR UNRELIABLE, APPEARS TO BE BLOCKED, ACTING LIKE ALTIMETER BECAME UNBLOCKED DESCENDING THRU FL 320. DRAINED PITOT STATIC SYS IAW AMM 34-13-00. OPERATIONS CHECKED ADC IAW 34-15-00. OPERATIONS CHECKED GOOD.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 30,274 hrs · 26,224 cycles

GOT IAS COMPARATOR ALERT ON BOTH PFD'S DURING DESCENT FROM FL 310. FIRST OFFICERS IAS WAS EQUAL TO THE STBY ISIS IAS. DURING DESCENT THE CAPTAINS IAS WAS INDICATING SLOWER AT AN INCREASING DIFFERENCE TO 100 KNTS. SELECTED ADC ON CAPTAINS REVERSIONARY PANEL WHICH RESOLVED IAS DIFFERENCE. SUSPECT CAPTAINS PITOT BLOCKAGE. CLEARED NR 1 PITOT MAST DRAIN PORTS, DRAINED NR 1 PITOT WATER TRAP & PURGED MOISTURE. NUMBER 1 PITOT LCK OK IAW AMM CH 34-13-00, ADC 1 & 2. OPERATIONS CHECKED OK IAW AMM CH 34-15-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,111 hrs · 26,089 cycles

CAPTAINS FLASHLIGHT INOPERATIVE, MEL 25-53. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: DOOR — JAMMED (CABIN) · airframe 29,780 hrs · 25,783 cycles

MAIN PAX DOOR JAMMED, HANDLE MOVES A FEW INCHES, THE TWO RAMP PERSONNEL PULLED DOOR TO OPEN FROM OUTSIDE. REINSTALLED MAIN DOOR INTERNAL ACTUATING HANDLE IAW AMM 52-18-05. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (PITOT HEAT) · airframe 29,464 hrs · 25,468 cycles

PITOT FROZEN & ASI WAS SPORADIC ABOVE FL 280, DECLARED EMER. PERFORMED PITOT & STATIC PROBE HEATING OPERATIONS TEST IAW AMM 30-31-00. CHECK PASSES. AT 360 FIRST OFFICERS IAS 10 KT FASTER AT 370, CAPTAINS IAS 250, STBY 240, FIRST OFFICERS 240 FLASHING IAS FOLLOWED BY SPS ADV ON DES TO 280, SEEMED LIKE IT CORRECTED. PERFORMED ADC SYS OPERATIONS TEST & FUNCTION CHECK IAW AMM 34-15-00, CHECKS PASS. READINGS IN LIMITS, NO SPLITS IN AIRSPEED NOTED DURING CHECK. NO FAULTS NOTED OUTLINED IN FIM 27-36-00 FOR SPS ADVANCED. STALL PROTECTION OPERATIONS TEST PASSED AMM 27-36-00.

Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 29,080 hrs · 25,111 cycles

MAIN CABIN DOOR HARD TO OPEN & CLOSE. SERVICED MAIN CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 29,022 hrs · 25,061 cycles

MAIN DOOR DIFFICULT TO OPEN. LUBRICATE FWD UPPER PAX MAIN DOOR ROLLER IAW MM 53-21-02. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR — STIFF (CABIN) · airframe 28,993 hrs · 25,029 cycles

FLIGHT ATTENDANT REPORTS MAIN DOOR VERY DIFFICULT TO OPEN. DEFERRED REF FMR IAW TN-EM-52-029.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,087 hrs · 24,277 cycles

DAMAGE LOCATED ON LAP SEAM & APPROX 4 INCHES BELOW SEAM BELOW 2ND RT WINDOW RT FUSELAGE. REMOVED LIGHTNING DAMAGED AREAS, INSTALLED DOUBLER & FILLERS IAW ERS-EM-53MR-1026.

Part: PROFILE — CRACKED (COCKPIT) · airframe 27,979 hrs · 24,176 cycles

DURING IMBV INSPECTION, QA FOUND THE COCKPIT UNDER FLOOR ACCESS HATCH 123BL CRACKED AT THE HINGE PIN RECEIVER. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON THE COCKPIT UNDER FLOOR ACCESS HATCH 123BL IAW ERS-EM-52MR-261. REPAIR MATERIALS INTERNAL L PROFILE 2024-T3 0.040 INCHES.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,979 hrs · 24,176 cycles

GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE, LT & RT SUPPORTS, CRACKED AT LT FLOORBEAM. R & R GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE, LT & RT SUPPORTS, AT LT FLOORBEAM IAW SRM 51-40-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,979 hrs · 24,176 cycles

THE CONNECTOR FOR THE AFT MOST EMER EXIT AISLE LIGHT STRIP IS BROKEN. R & R CONNECTOR FOR THE AFT MOST EMER EXIT AISLE LIGHT STRIP IAW SWPM 20-21-00 STEP 5. CPRIMPER SN EA041205, TURRET SN 7859, STRIPPER SN 6853.

Part: WIRE — DAMAGED (CABIN) · airframe 27,979 hrs · 24,176 cycles

EMERGENCY LIGHT ON SERVICE DOOR IS INOPERATIVE. SPLICED WIRE W716-0008-20 IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,979 hrs · 24,176 cycles

GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE LT SUPPORT CRACKED AT CTR FLOORBEAM. R & R GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE LT SUPPORT AT CTR FLOORBEAM IAW SRM 51-40-02.

Part: ROLLER — LACK OF LUBE (DOOR FRAME) · airframe 27,032 hrs · 23,383 cycles

FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN. LUBRICATED MAIN CABIN DOOR ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: MASK — BROKEN (CABIN) · airframe 26,857 hrs · 23,224 cycles

FLIGHT ATTENDANT REPORTS DEMO O2 MASK IS BROKEN, NEEDS REPLACEMENT. REPLACED FLIGHT ATTENDANT O2 DEMO MASK AS REQUIRED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,779 hrs · 23,153 cycles

FORWARD CABIN FLASHLIGHT HOLDER BROKEN. R & R FWD CABIN FLASHLIGHT ASSEMBLY IAW MM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,502 hrs · 22,906 cycles

FWD CEILING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-08, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,464 hrs · 22,873 cycles

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

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,464 hrs · 22,873 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,464 hrs · 22,873 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,402 hrs · 22,808 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY EMERGENCY LIGHT & BATTERY CHARGER ASSEMBLY IAW WC 33-700-19, OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,357 hrs · 22,761 cycles

LEFT EXTERNAL OVERWING EMERGENCY LAMP INOPERATIVE. R & R LT EXTERNAL OVERWING LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, NO FIX. R & R NR 4 EMERGENCY BATTERY & CHARGER ASSEMBLY IAW WC 33-700-19, NO FIX. TROUBLE SHOT HARNESS USING WM 33-50-50 NO FAULTS FOUND, SUSPECT FAULT IN NEW CHARGER. R & R NR 4 CHARGER TWICE MORE UNTIL GOOD PART FOUND. OPERATIONS CHECKED WC 33-700-17 GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,626 hrs · 22,181 cycles

CABIN FWD FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARDED IAW MEL 2553 AUTH 010277C MOC 135181. R & R FWD CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16 STEPS 2 J 1 & 3 I 4. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,340 hrs · 21,962 cycles

CAPTAIN'S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,269 hrs · 21,084 cycles

THE CREW REPORTED CAPTAIN’S FLASHLIGHT WAS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE FLASHLIGHT. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 24,234 hrs · 21,058 cycles

CREW REPORTED MAIN PASSENGER DOOR WAS HARD TO OPEN. ACFT REMOVED FROM SERVICE. CLEANED AND LUBED UPPER DOOR ROLLERS AND EXT DOOR LOCKING CAMS. THE OPS CHECK WAS WITHIN LIMITS IAW AMM 52-18-00. THE ACFT WAS RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 24,212 hrs · 21,040 cycles

DURING MX INSPECTION, FOUND FRAME 19 CHAFED AT STRINGER 3R. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR IAW AEA EO-EM-53MR-2152. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 24,236 hrs · 21,059 cycles

DURING B INSPECTION, FOUND EMERGENCY EXIT SIGN INOPERATIVE. ACFT REMOVED FROM SERVICE. CONNECTED SP9009 AND SP9010 AS REQUIRED. OPS CHECKED GOOD AMM 33-50-00. ACFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,236 hrs · 21,059 cycles

DURING MX INSPECTION, FOUND RT LAV GUSSET CORRODED. ACFT REMOVED FROM SERVICE. R & R GUSSET IAW SRM 51-40-02 AND 51-40-09. ACFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,236 hrs · 21,059 cycles

DURING MX INSPECTION FOUND THE NR 5 EMERGENCY LIGHT STRIP TO HAVE BROKEN WIRES. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,236 hrs · 21,059 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY PROXIMITY LIGHT STRIP NR 7 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 24,236 hrs · 21,059 cycles

DURING MX INSPECTION, FOUND THE NR 4 EMERGENCY LIGHT CRACKED PLASTIC COVER. ACFT REMOVED FROM SERVICE. R & R LIGHT COVER IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 24,212 hrs · 21,040 cycles

LOWER END OF SHEAR TIE AT FR 65 CORRODED. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 24,236 hrs · 21,059 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR CENTER SILL CORRODED. ACFT REMOVED FROM SERVICE. R & R CENTER SILL IAW SRM 51-40-02. ACFT RETURNED TO SERVICE.

Part: TRUNNION — CORRODED (NLG) · airframe 24,212 hrs · 21,040 cycles

LEFT NLG TRUNNION CORRODED. R & R LT NLG TRUNNION IAW EO-EM-53MR-1623 01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,236 hrs · 21,059 cycles

DURING MX INSP FOUND THE EMERGENCY PROXIMITY LIGHT STRIP NR 8 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW SWPM 20-00-03 AND WM 91-10-02. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (CABIN) · airframe 22,946 hrs · 20,029 cycles

DURING MAINTENANCE FOUND THE NR 1, 2, 3 & 4 EMERGENCY BATTERIES REQUIRED REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE #1, 2, 3 & 4 EMERGENCY BATTERIES IAW EMB-145 AMM 33-50-04. SERIAL NUMBER 1 105211, SERIAL NUMBER 2 68819, SERIAL NUMBER 370993, SERIAL NUMBER 4 115005. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,240 hrs · 19,486 cycles

DURING B INPSECTION FOUND THE OVERHEAD AFT 12A CEILING EMERGENCY IDENTIFIER SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY EXIT SIGN. FOUND SIGN GOOD TESTED INVERTER FOUND TO BE BAD. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT INVERTER IAW EMB AMM TASK: 33-50-11-000-801-A, AND 33-50-11-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — NO INDICATION (FIRE DETECTION) · airframe 21,758 hrs · 19,108 cycles

FLIGHT 2858, DURING FIRE TEST, CARGO EXTINGUISHER LIGHT DID NOT ILLUMINATE. AIRCRAFT REMOVE FROM SERVICE. UNABLE TO DUPLICATE, OPS CHECKED OK IAW AMM 26-15-00. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 21,563 hrs · 18,967 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HOLDER NOT HOLDING FLASHLIGHT PROPERLY TO ALLOW IT TO CHARGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BASE AT FLIGHT ATTENDANT'S SEAT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,481 hrs · 18,901 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FIRST OFFICER’S FLASHLIGHT RECEPTACLE BASE BROKE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT RECEPTACLE BASE IAW W/C 33-700-20. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 21,388 hrs · 18,832 cycles

ON FLIGHT 2965 THE CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — UNSERVICEABLE (BLEED AIR SYS) · airframe 20,814 hrs · 18,360 cycles

ON FLIGHT 3263 THE CREW REPORTED AN ENGINE 1 FIRE MESSAGE ON EICAS JUST AFTER TAKEOFF. NO OTHER ENGINE INDICATION WAS OBSERVED. THE CREW RAN THE EMERGENCY CHECKLIST. ENGINE 1 FIRE INDICATION ON EICAS WENT AWAY. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. LANDING WAS UNDER MAX LANDING WEIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE BLEED TUBE ON LEFT ENGINE PYLON TO OCSP IAW MM 36-10-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL MODULE — FAULTY (FIRE WARNING) · airframe 20,496 hrs · 18,102 cycles

ON FLIGHT 4201 THE CREW REPORTED THAT ON CLIMBOUT AT 8000 FEET THEY RECEIVED A LEFT ENGINE FIRE WARNING. REDUCED POWER AND MESSAGE CLEARED. SHUTDOWN E-1 AS PRECAUTIONARY ITEM BUT THE BOTTLE WAS NOT BLOWN. RETURNED TO FIELD AND LANDED OVERWEIGHT. RATE OF DESCENT AT LANDING WAS LESS THAN 300 FPM. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW EMB 145 FIM 26-11-00 FOUND NR 1 ENGINE CONTROL MODULE FAULTY PER FIM. REMOVED AND REPLACED NR 1 ENGINE CONTROL MODULE IAW EMB AMM 26-11-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 20,334 hrs · 17,980 cycles

FLIGHT 4344, FLIGHT ATTENDANT REPORTED THE ORANGE STRIP EMERGENCY LIGHT INSTALLED IN WRONG LOCATION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT TO CORRECT POSITION IAW AMM 33-50-12. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 20,269 hrs · 17,932 cycles

ON FLIGHT 9804 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT ASSEMBLY IAW 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — CORRODED (LT MLG) · airframe 20,120 hrs · 17,802 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT MAIN LANDING GEAR DOWNLOCK PROXIMITY SWITCHES TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR DOWNLOCK PROXIMITY SWITCHES IAW EMB 145 AMM TASKS 32-61-02-000-801-A & 32-61-02-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,048 hrs · 17,757 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,875 hrs · 17,641 cycles

DURING MAINTENANCE VISIT, FOUND EMERGENCY LIGHT DAMAGED AT FLOORBOARD 261BF. ACFT REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT IAW AMM 33-50-12. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,875 hrs · 17,641 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 5 LEFT FLOOR PROXIMITY STRIP LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 LEFT FLOOR PROXIMITY LIGHT IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — LOOSE (FLASHLIGHT) · airframe 19,432 hrs · 17,305 cycles

FOR FLIGHT 4100 THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT CHARGING INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED LOOSE CONNECTION OF BATTERY. NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (TE FLAP) · airframe 18,982 hrs · 16,959 cycles

ON FLIGHT 2731 THE CREW REPORTED, RECEIVED A FLAP FAIL INDICATION ON EICAS UPON SELECTING FLAP UP ON CLIMBOUT. THE FLAPS DID NOT RETRACT, RECEIVED FLAP FAIL INDICATION. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND FLAP DRIVE CONNECTOR P1108 DISCONNECTED. RECONNECTED THE SAME. DISCONNECTED PLUG P1102 PER MEL 27-9, COMPLETED FLAP OPERATIONAL CHECK PER EMB AMM 27-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,943 hrs · 16,933 cycles

FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE RIGHT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 AC/DC INVERTER IAW EMB 145 AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,014 hrs · 16,223 cycles

DURING MAINTENANCE BASE VISIT FOUND LEFT EXTERIOR FORWARD EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERIOR FORWARD EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 17,600 hrs · 15,906 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHTING STRIP WIRE BROKEN AT ROW 18 SEAT A AND B. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROW 18 A AND B IAW EMB 145 AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 16,974 hrs · 15,438 cycles

ON FLIGHT 2791 DURING THE CLIMB THE CREW REPORTED, WHEN RETRACTING THE GEAR HAD NO IN TRANSIT INDICATION. THE LANDING GEAR DID NOT RETRACT ON THE FIRST ATTEMPT. ON THE SECOND ATTEMPT NO DISAGREEMENT INDICATED. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02. THE OPERATIONAL CHECK WAS GOOD, GEAR SWING GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE ASSY — MALFUNCTIONED (NR 3) · airframe 16,810 hrs · 15,315 cycles

FOR FLIGHT 2963 ON TAXI INTO THE RAMP AT DFW THE CREW REPORTED A BRAKE OVER TEMPERATURE INDICATION ON THE RIGHT INBOARD BRAKE. ANOTHER AIRCRAFT REPORTED THERE WAS FIRE ON THE RIGHT MAIN TIRE. AN EMERGENCY EVACUATION WAS PERFORMED THROUGH THE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BRAKE P/N-OFF 21707-1 S/N 3693. REMOVED AND REPLACED THE NR 3 MAIN TIRE P/N OFF 3641 S/N 2177. REMOVED AND REPLACED THE NR 4 MAIN TIRE P/N OFF 31641 S/N 0064. REMOVED AND REPLACED THE NR 3 BRAKE TEMPERATURE SENSOR P/N OFF 0132AFU-1 S/N E5666. INSPECTION REVEALED NO EVIDENCE OF FIRE. PERFORMED OVERHEATED WHEEL INSP OF NR 3 MAIN LANDING GEAR WHEEL IAW AMM 5-50-14, NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 16,517 hrs · 15,080 cycles

ON FLIGHT 2738 AFTER TAKEOFF SELECTED GEAR UP THE CREW REPORTED, GOT NO RETRACT AFTER 10 SECONDS. THE CREW RECEIVED LANDING /DISAGREE MESSAGE. THE CREW PERFORMED AIRCRAFT OPERATIONS MANUAL PROCEDURES. THE GEAR WOULD STILL NOT COME UP. RETURNED TO GSP NO OTHER PROBLEMS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR LEVER IAW EMB AMM 32-32-02. THE OPERATIONAL CHECK OF LANDING GEAR EXTENSION/RETRACTION’S WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PCU — FAULTY (RUDDER) · airframe 16,068 hrs · 14,740 cycles

ON FLIGHT 3788 DURING DESCENT THE FIRST OFFICER REPORTED THE PEDALS FELT LOOSE AND ON FINAL APPROACH THE RUDDER PEDALS EXHIBITED A BUFFETING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER POWER CONTROL UNIT IAW EMB 27-22-03-00-801A & EMB AMM 27-22-03-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 14,900 hrs · 13,830 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT THE FOURTH ROW EMERGENCY LIGHT STRIP FROM FORWARD AFT HAS BROKEN WIRE, FOUND DURING AILERON TENSION CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT STRIP ASSEMBLY IAW EMB MM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 200) · airframe 9,594 hrs · 9,079 cycles

DURING INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE TWO SMALL AREAS CORRODED BEYOND MANUAL LIMITS. REMOVED CORROSION IAW EMB SRM PERFORMED EDDY CURRENT WITH NO REJECTABLE INDICATIONS. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 9,594 hrs · 9,079 cycles

DURING INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE TWO SMALL AREAS CORRODED BEYOND MANUAL LIMITS. REMOVED CORROSION IAW EMB SRM PERFORMED EDDY CURRENT WITH NO REJECT ABLE INDICATIONS. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE)

THE FUSELAGE SKIN WAS FOUND TO HAVE A DENT BETWEEN FRAMES 64-65 AND STRINGERS 19L AND 20L. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SEAT — OUT OF TRACK (COCKPIT)

ORD - FLT 4395 - CREW REPORTED THE FIRST OFFICERS SEAT WAS INOPERATIVE AND WAS OUT OF ITS TRACK. MAINTENANCE INSPECTED THE SEAT AND FOUND NO DEFECTS. SEAT WAS REINSTALLED IN ITS SEAT TRACKS IAW EMB MM. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PIA - FLT 4102 - ON PREFLIGHT CHECK, THREE EMERGENCY FLOOR LIGHT STRIPS COME ON FOR 3 SECONDS THEN GO OUT. REPLACED EMERGENCY LIGHTING BATTERY PACKS NR 2/3/4 IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. NR 1 P/N 2013BR S/N B1641 NR 2 2012BR S/N 1560, NR 3 2012BR S/N 1614. (M)

Part: SKIN PANEL — DAMAGED (FUSELAGE)

SAW - FOUND LIGHTNING STRIKE DAMAGE ON RIGHT SIDE OF FUSELAGE BETWEEN FRAMES 25 AND 26 AT STRINGER 18A. REPAIRED LIGHTNING STRIKE DAMAGE AREA WITH A CUT OUT AND DOUBLER PATCH IAW SRM 53-22-01 FIG 304 SHEET 3. AIRCRAFT WAS RETURNED TO SERVICE. (M)