N695AE

Part: AHRS — FAULTED · airframe 46,256 hrs · 43,267 cycles

ON DESCENT, INTERMITTENT ELECT BURNING ODOR BY FA JUMPSEAT. ELECT ODOR AT GATE WITH A/C IN EMERG POWER MODE AFTER ENG SHUTDOWN. LT DIST BOX RT, DIST BOX LT AND RT COCKPIT RELAY SUPPORTS NO DEFECTS NOTED. PERFORMED POWER OPS CHECK IAW AMM 24-60-00, PERFORMED PITOT STATIC HEAT, OPS CKD IAW AMM 30-31-00. RAN PACKS ON APU BLEED FOR MORE THAN AN HR, NO DEFECTS NOTED. INSPECTED LT DIST BUS UNDER FA JUMP SEAT, NO DEFECTS NOTED. AHRS 1 INTERMITTENT, AFTER SELECTING ESS PWR AHRS 2 STOPPED WORKING WITH ELECT ODOR AFTER SWITCHING FROM APU TO GPU POWER. FA REPORTS ODOR FWD & MID CABIN. OPS CHECKED MAIN AC GEN SYS & MAIN GEN SWITCHING CIRCUIT IAW AMM 24-31-00. RAN BOTH PACKS ON ENG BLEEDS FOR 10 MINS, NO DEFECTS NOTED. ACFT OK FOR SERVICE

Part: CONTROLLER — FAULTED (ZONE 200) · airframe 45,788 hrs · 42,687 cycles

RAPID DEPRESSURIZATION AT 22,000FT USED CREW OXYGEN MASK TO DESCEND TO 10,000FT AND DIVERTED. R & R DIGITAL PRESSURIZATION CONTROLLER IRT AMM 21-31-04. OPS CHECK IRT 21-31-00. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: PROFILE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2316 CARGO ENTRY FWD T PROFILE CRACKED AT FR66. RAR PROFILE IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2297 ANGLE UNDER RH WINDOW CRACKED AT FR10 STR9R. RAR ANGLE IAW SRM 51-40-02

Part: PROFILE — DAMAGED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2317 CARGO DOOR ENTRANCE AFT T-PROFILE DAMAGED AT FR67. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2321 SHEAR CLIP CRACKED AT FR61 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 800) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2315 CARGO DOOR ENTRY LWR BEAM CORRODED. R & R BEAM IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2296 SHEAR CLIP CRACKED AT FR10 BTW STR9-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2314 SHEAR CLIP CRACKED AT FR72 BTW STR16-17L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BEAM — DAMAGED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2318 LH BEAM OB ANGLE AT FR67 IS DAMAGED. RAR ANGLE IAW SRM 51-40-02. MANUFATURED ANGLE IAW DRAWING 145-25681

Part: ANGLE — CRACKED (ZONE 800) · airframe 45,396 hrs · 42,202 cycles

53-2323 CARGO DOOR AFT MECHANISM FWD ANGLE CRACKED AT BTW STR4-5R. RAR ANGLE IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 800) · airframe 45,396 hrs · 42,202 cycles

53-2324 CARGO DOOR AFT MECHANISM UPPER ANGLE CRACKED AT STR4R. RAR ANGLE IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2320 SHEAR CLIP CRACKED AT FR61 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PLATE — CRACKED (NLG WW) · airframe 45,396 hrs · 42,202 cycles

53-2303 NLG WHEEL WELL UPPER PLATE CRACKED AROUND 2 NUTPLATES. REPAIRED IAW SRM 53-11-10RE FIG 201 (2 LOCATIONS)

Part: SKIN — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2777 SKIN CRACKED AROUN RIVETS (2) AT FR77 BTW STR5-6R AND 3-4R. REPAIRED IAW SRM53-32-01 ITEM 9 FIG 213

Part: SKIN — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2274 EXTERNAL SKIN CRACKED AROUND RIVET AT FR77 BTW STR8-9L. REPAIRED IAW SRM 53-32-01 FIG 213 ITEM 9

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2244 CTR OMEGA BEAM #1 CORRODED AT BTW FR18-23. R & R OMEGA BEAM IAW SRM 51-40-02

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

FWD SIDE OF SERVICE DOOR OPENING, FR20 CORRODED AT FLOOR LEVEL. REPAIRED IAW ETD2025-145-921347 AND SRM 53-00-04RE ITEM 17

Part: SPAR — CRACKED (ZONE 300) · airframe 45,396 hrs · 42,202 cycles

53-2283 BOTTOM VERTICAL STAB, AFT OF SPAR 3, RH LWR PROFILE CRACKED . REPAIRED IAW ETD2025-145-921570 AND EO1-55-25-0192

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2263 SHEAR CLIP CRACKED AT FR59 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2182 RH SILL CORRODED BTW FR18-20. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2173 LH OMEGA BEAM, IB FLANGE CRACKED AT FR22. REPAIRED IAW ETD2025-145-921472 AND EO1-53-25-0185

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2176 LH OMEGA BEAM, FLOOR SUPPORT ANGLE CRACKED AT BTW FR19-20. RAR ANGLE IAW SRM51-40-02

Part: SPLICE ANGLE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2179 LH OMEGA BEAM, IB ANGLE SPLICE CRACKED BTW FWD AND AFT DIGITAL. RAR SPLICE IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2177 CTR GUSSET CORRODED BTW FR18-23. RAR GUSSET IAW SRM 51-40-02

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2183 CTR FUSE I, AFT DIGITAL CORRODED. R & R DIGITAL IAW SRM 51-20-08

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2181 SHEAR CLIP CRACKED AT FR16 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2184 SERVICE DOOR ENTRY, LWR BEAM CORRODED. RAR BEAM IAW SRM 51-40-02-PR

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2180 LH OMEGA BEAM , IB FLANGE CRACKED AT FR23. REPAIRED IAW ETD2025-145-901472 AND EO1-53-25-0185

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2174 LH OMEGA BEAM, IB FLANGE CRACKED AT FR21. REPAIRED IAW ETD2505-145-921972 AND EO 1-53-25-0185

Part: SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2140 RH SILL CORRODED BTW FR23-29. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2150 LH OMEGA BEAM IB FLANGE CRACKED AT FR35. REPAIRED IAW ETD2025-145-921567 AND EO1-53-25-0188

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2137 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2151 LH OMEGA BEAM IB FLANGE CRACKED AT FR24. REPAIRED IAW ETD2025-145-921486 AND EO1-53-25-0186

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2143 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2149 LH OMEGA BEAM IB FLANGE CRACKED AT FR31. REPAIRED IAW ETD2025-145-921567

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2141 SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRN 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2144 LH OMEGA BEAM CRACKED ON IB FLANGE AT FR26. REPAIRED IAW ETD2025-145-921486 AND EO1-53-25-0186

Part: FIREWALL — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2087 APU FIREWALL CRACKED AT ELECTRICAL CONNECTOR LOCATION. REPAIRED IAW SRM 53-32-13 ITEM 7 FIGURE207

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2097 RH OMEGA BEAM IB ANGLE CRACKED AT BTW FR48-50. RAR ANGLE IAW SRM 51-40-02

Part: STIFFENER — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2102 NLG FWD LH WHEEL STOPPER INTERNAL STIFFENER CRACKED AT ANCHOR NUT. RAR STIFFENER IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 54,396 hrs · 42,202 cycles

53-2106 LH OMEGA BEAM IB ANGLE CRACKED AT FR48-50. RAR ANGLE IAW SRM 53-23-02RE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2107 CTR OMEGA BEAM RH ANGLE CRACKED AT FR46-50. RAR ANGLE IAW SRM 53-23-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2100 LH OMEGA BEAM CRACKED AT FR36. REPAIRED IAW ETD2025-145-921488 AND EO 1-53-25-0189

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2096 RH SILL BTW FR48-52 CORRODED. REPAIRED IAW ETD2025-145-922013 AND SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2104 LH OMEGA BEAM OB ANGLE CRACKED AT FR48-50. RAR ANGLE IAW SRM 53-23-02RE

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2103 LH LWR ANGLE CRACKED AT FLOOR LEVEL OF FR46. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT — CRACKED (APU FIREWALL) · airframe 45,396 hrs · 42,020 cycles

APU FIREWALL LH SIDE LWR APU SUPPORT CRACKED. REPAIRED SUPPORT IAW SRM53-32-13 ITEM 8 FIG 202.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2098 RH OMEGA BEAM OB ANGLE CRACKED AT BTW FR48-50. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,396 hrs · 42,202 cycles

53-2105 CTR OMEGA BEAM LH ANGLE CRACKED AT BTW FR46-50. RAR ANGLE IAW SRM 53-23-02RE

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,396 hrs · 42,202 cycles

53-2099 RH SILL CORRODED BTW FR41-48. RAR SILL IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 45,396 hrs · 42,202 cycles

53-2033 LH WING TO BODY FAIRING, LWR ANGLE SUPPORT #2 FROM FWD IS CRACKED. RAR SUPPORT IN IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2028 RH UPPER SUPPORT WING TO BODY FAIRING CRACKED BTW FR41-42. REPAIRED IAW SRM 53-23-12RE ITEM 3 FIG 202

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2030 RH WING TO BODY FAIRING, LWR ANGLE SUPPORT#4 FRO FWD IS CRACKED. REPAIRED IAW SRM 57-20-01RE ITEM 3 FIG 203,204

Part: HINGE — CRACKED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2037 TOILET WASTE VALVE SUPPORT HINGE CRACKED. RAR HINGE IAW SRM 51-40-02

Part: RIB — CRACKED (ZONE 600 LE) · airframe 45,396 hrs · 42,202 cycles

57-2010 RH LE #2 OB END RIB CRACKED. RAR RIB IAW SRM 51-40-02, ETD2025-145-921063, AND EO1-05-25-0202

Part: ACCESS DOOR — GOUGED (ZONE 100) · airframe 45,396 hrs · 42,202 cycles

53-2014 GOUGE BELOW GPU ACCESS DOOR. REPAIRED IAW SRM 53-12-01 FIG 201

Part: SUPPORT ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 45,396 hrs · 42,202 cycles

53-2029 WING TO BODY FAIRING, RH LWR ANGLE SUPPORT #2 FROM FWD IS CRACKED. RAR SUPPORT IAW SRM 51-20-02

Part: PLATE — BROKEN (THRUST REVERSERS) · airframe 44,718 hrs · 41,460 cycles

E1 REV DISAGREE INFLIGHT. NDIS 695 78-30 0059000 04DEC24 SBY CLOSE. FOUND #100 TR UPPER DOOR O/B KICKER PLATE BROKEN AND MISSING 3 INCH SECTION AND MISSING SUPPOERT BRACKET. REPAIRED IAW EO1-78-24-0707 OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 43,097 hrs · 39,646 cycles

HYD1 LOW QTY MSG IN FLT SERVICED #1 HYD IN REF TO AMM 12-13-01. LEAK CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: WARNING LIGHT — FALSE INDICATION (FUEL DOOR) · airframe 42,860 hrs · 39,368 cycles

FUEL DOOR OPEN INDICATION ON TAKE OFF. CLOSED AND OPENED FUELING DOOR SEVERAL TIMES IRW EMB145 AMM 52-45-02, NO DEFECTS FOUND AT THIS TIME. A/C OK FOR SERVICE. CLEAR MEL 52-3-5

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,987 hrs · 38,363 cycles

10K A/C PRESSURIZATION FAILED (C/W MX PROCEDURE) INSPECTED ALL DOOR RUBBER SEALS. FOUND BAG BAY DOOR SEAL AT LOWER SECTION TO BE MISSING. R&R BAG BAY DOOR SEAL IN REF TO AMM 52-30-02-000/400-801-A. PERFORMED OPS CHECK IN REF TO AMM 21-31-00-700-808-A. OPS CHECK GOOD. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,381 hrs · 37,711 cycles

NR 2 ENG BLEED LEAK INFLIGHT. CMC DISPLAYS AIR COND 2 LEAKAGES WING 2 A/ICE LEAK. FOUND LEAK BY Y-DUCT. R+R'D DUCT + COUPLING IRT AMM 21-60-01. OPS LEAK/ CHECK GOOD. OK FOR SERVICE

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954275 - SERVICE DOOR FWD SILL HAS CORROSION .... REPAIRED SERVICE DOOR FWD SILL CORROSION IAW EO1-05-23-0024.

Part: SKIN — DAMAGED (FRMS 25-26) · airframe 40,974 hrs · 37,250 cycles

EXTERIOR FUSELAGE SKIN BETWEEN FR. 25-26/ STGR. 20L-21L HAS POSSIBLE BURN. REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN FR. 25-26/ STGR. 20L-21L BURN MARK IAW SRM 53-00-01, AND PIEDMONT EO1-05-23-0024.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

GALLEY AREA FWD DIGITAL HAS CORROSION .... REPAIRED GALLEY AREA FWD DIGITAL CORROSION IAW PIEDMONT EO1-05-23-0024.

Part: SKIN — CRACKED (FRM 49 S4-5R) · airframe 40,974 hrs · 37,250 cycles

E953561 - POSSIBLE CRACKS AROUND 3 RIVETS ON FRAME 79 BETWEEN STRINGERS 4R – 9R. FURTHER INVESTIGATION FOUND ONLY ONE CRACKED AREA AT RIVET. REPAIRED FUSELAGE SKIN BY REMOVING CRACK AND INSTALLING A BUSHING ON FRAME 79 AT FASTENER BETWEEN STRINGERS 4R – 5R IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213, AND EO1-53-23-0017.

Part: NONE — NONE (NONE) · airframe 40,974 hrs · 37,250 cycles

POSSIBLE INCORRECT REPAIR BETWEEN FRAME 78–80 STRINGER 12L-14L .... RE-ACCOMPLISHED REPAIR BETWEEN FRAME 78–80 STRINGER 12L-14L IAW EO1-53-23-0007.

Part: GUSSET — CORRODED (FRMS 37-39) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954135 - CENTER BEAM GUSSET HAS CORROSION BETWEEN FRAMES 37 AND 39 .... RAR CENTER BEAM GUSSET AT FRAMES 37 AND 39 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954131 - L/H #3 CABIN FLOORBOARD SUPPORT HAS CORROSION .... REMOVED CORRODED L/H #3 CABIN FLOORBOARD SUPPORT AND INSTALLED SERVICEABLE FLOORBOARD SUPPORT

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954132 - R/H #3 CABIN FLOORBOARD SUPPORT HAS CORROSION .... REMOVED AND REPLACED R/H #3 CABIN FLOORBOARD SUPPORT (FLOOR SILL) IAW EMB-145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,974 hrs · 37,250 cycles

E954284 - PAX DOOR ENTRANCE AFT FLOOR BOARD SUPPORT HAS CORROSION ..... REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: BUSHING — MIGRATED (RUDDER HINGE) · airframe 40,974 hrs · 37,250 cycles

RUDDER I LWR CENTER HINGE FITTING BOTH UPPER HAT BUSHINGS MIGRATED. REPAIRED RUDDER I LWR CENTER HINGE FITTING BOTH UPPER HAT BUSHINGS MIGRATED IAW EO1-55-23-0010

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954284 - PAX DOOR ENTRANCE AFT FLOOR BOARD SUPPORT HAS CORROSION ..... REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02. ORIG SUBMISSION DATE: 1/30/2023

Part: FLOORBEAM — CORRODED (FRM 18) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954281 - GALLEY AREA CROSS MEMBER AT FRAME 18 HAS CORROSION .... REMOVED AND REPLACED GALLEY AREA CROSSBEAM AT FR 18 IAW EMB 145 SRM 51-40-02 AND PIEDMONT BULLETIN 53-3 R1

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954134 - L/H #4 CABIN FLOORBOARD SUPPORT HAS CORROSION .... RAR SERVICEABLE L/H #4 CABIN FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954138 - R/H #5 CABIN FLOORBOARD SUPPORT HAS CORROSION .... RAR R/H #5 CABIN FLOORBOARD SUPPORT IAW EMB 145 SRM 51-20-03 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954139 - L/H #5 CABIN FLOORBOARD SUPPORT HAS CORROSION .... REMOVED CORRODED L/H #5 CABIN FLOORBOARD SUPPORT, PREPPED AND INSTALLED SERVICEABLE L/H #5 CABIN FLOORBOARD SUPPORT IAW EMB 145 SRM 51-20-03, EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 40,974 hrs · 37,250 cycles

E954129 - L/H #2 CABIN FLOORBOARD SUPPORT HAS CORROSION .... REMOVED AND REPLACED L/H #2 CABIN FLOORBOARD SUPPORT (FLOOR SILL) IAW EMB-145 SRM 51-40-02

Part: SKIN — CHAFED (LT NACELLE) · airframe 40,974 hrs · 37,250 cycles

LEFT PYLON SKIN CHAFED INSIDE 414DB. REPAIRED L/H PYLON SKIN CHAFE INSIDE 414DB IAW EO1-53-23-0006.

Part: SKIN — CHAFED (LT NACELLE) · airframe 40,974 hrs · 37,250 cycles

LT PYLON SKIN CHAFED INSIDE 414DB. REPAIRED LT PYLON SKIN CHAFE INSIDE 414DB IAW EO1-53-23-0006.

Part: ACM — UNSERVICEABLE · airframe 37,996 hrs · 33,835 cycles

SMOKE SMELL IN FLIGHT DECK AND CABIN, WITH PACK 1 ON, AND SHORTLY AFTER CABIN TEMPERATURE INCREASED RAPIDLY. (CREW REPORTED SMELL IMPROVED BEFORE GETTING STARTED WITH QRH AND TURNING OFF RECIRCE FAN). MAINTENANCE: UPON FURTHER INSPECTION FOUND AIR CYCLE MACHINE TO BE UNSERVICEABLE REMOVED AIR CYCLE MACHINE IAW AMM 21-51-03. INSTALLED ACM IAW AMM 21-51-03-400-801-A R&R HEAT EXCHANGER IAW AMM 21-51-02 OPS CHECK AND LEAK CHECK GOOD OK FOR SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 37,410 hrs · 33,205 cycles

AFTER GEAR SELECTED UP GEAR SHOWED UP AND LOCKED GEAR DOORS REMAINED OPEN, CYCLED GEAR. HANDLE DISAGREE MESSAGE DISPLAYED WITH RELEVANT CAUTIONS.FOLLOWED FIM TASK 32-32-00-810-803-A, BLOCK 17. R & R LANDING GEAR CONTROL LEVER, IAW 32-32-02-000-801-A/400. OPERATIONS CHECK GOOD.

Part: SOLENOID VALVE — MALFUNCTIONED (NLG DOORS) · airframe 37,408 hrs · 33,203 cycles

AFTER GEAR SELECTED UP, NOSE GEAR DOORS REMAINED OPEN. EXTENDED GEAR NORMALY, AND RETURNED TO FIELD. R & R NLG-DOOR SOLENOID VALVE, IAW AMM 32-33-02-000/400-801-A. LEAK CHECK GOOD. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OKAY FOR SERVICE.

Part: POTENTIOMETER — OUT OF RIG (FEEDBACK UNIT) · airframe 37,065 hrs · 32,783 cycles

A/C VEERS TO THE LEFT WITH T/O THRUST IS SET WITH FULL RIGHT PEDAL DEFLECTION. MAINTENANCE: RERIGGED FEEDBACK UNIT POT PER AMM 32-50-00-700-802-A SUB TASK 720-002-A OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: SKIN — CRACKED (FRAME 79) · airframe 37,060 hrs · 32,779 cycles

RH SIDE FUSELAGE FRAME 79 HAS POSSIBLE SKIN CRACKS AROUND 1 FASTENER. MAINTENANCE: REPAIRED IAW EO1-53-20-0244.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 37,060 hrs · 32,779 cycles

CARGO DOOR LOWER SILL IS CORRODED. MAINTENANCE: REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB145 SRM 51-40-02.

Part: FRAME — CRACKED (FRAME 73) · airframe 37,060 hrs · 32,779 cycles

FR 73 IS CRACKED BETWEEN STR 17R-16R. MAINTENANCE: REMOVED AND INSTALLED NEW LOWER SECTION OF FRAME 73 IAW EMB 145 SRM 51-40-02.

Part: WEB — GOUGED (CARGO DOOR) · airframe 37,060 hrs · 32,779 cycles

CARGO DOOR INTERNAL WEBBING IS GOUGED IN 5 AREA'S. MAINTENANCE: REPAIRED CARGO DOOR INTERNAL WEBBING GOUGED IN 4 AREAS IAW EMB145 SRM 52-30-01, AND 1 AREA REPAIRED IAW PIEDMONT EO1-52-20-0240.

Part: SKIN — CRACKED (FRAME 77) · airframe 37,060 hrs · 32,779 cycles

LH SIDE FUSELAGE FRAME 77 HAS POSSIBLE SKIN CRACKS AROUND 3 FASTENERS. REPAIRED THE FUSELAGE EXTERNAL SKIN AT FR 77 STGR 3L AND 6L IAW SRM 53-32-01 RE ITEM 9.

Part: YOKE — CRACKED (LT PYLON) · airframe 37,060 hrs · 32,779 cycles

LH PYLON LOWER FWD ENGINE YOKE FITTING IS CRACKED. MAINTENANCE: REMOVED AND REPLACED LH PYLON LOWER FWD ENGINE YOKE FITTING IAW EO1-54-20-0235.

Part: YOKE — CRACKED (LT ENGINE) · airframe 37,060 hrs · 32,779 cycles

LH PYLON LOWER FWD ENGINE YOKE FITTING IS CRACKED. MAINTENANCE: REMOVED AND REPLACED LH PYLON LOWER FWD ENGINE YOKE FITTING IAW EO1-54-20-0235. UNIQUE CONTROL NUMBER HNAA2020062900180 WAS ENTERED IN ERROR. THIS IS THE CORRECTED ONE LISTED ABOVE.

Part: NUT PLATE — MISSING (RUDDER) · airframe 37,060 hrs · 32,779 cycles

ACCOMPLISH PERMANENT REPAIR OF RUDDER II PROTRACTOR NUTPLATE MISSING AND NUTPLATE ATTACHING FASTENER HOLES ELONGATED. MAINTENANCE: PERFORMED CUT-OUT AT NUTPLATE ON RUDDER II AND FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ETD2020-145-019643.

Part: STRINGER — CRACKED (FRAME 75) · airframe 37,060 hrs · 32,779 cycles

STR 2L IS CRACKED AT FR 75. MAINTENANCE: REPAIRED IAW EO1-53-20-0238.

Part: RIB — CRACKED (RT WING) · airframe 37,060 hrs · 32,779 cycles

RH WING RIB 21 IS CRACKED INSIDE PANEL 651CB. MAINTENANCE: REPAIRED RH WING RIB 21 INSIDE PANEL 651CB IAW EMB 145 SRM 57-20-07 AND EO1-57-20-0242.

Part: FLOORBEAM — CORRODED (FRAME 61) · airframe 37,060 hrs · 32,779 cycles

LH LAV FLOOR BEAM CORRODED UNDER GUSSET AT AFT NUTPLATE HOLE, FWD OF FR 61. MAINTENANCE: REPAIRED LH LAV FLOOR BEAM CORROSION UNDER GUSSET AT AFT NUTPLATE HOLE, FWD OF FR 61 IAW PIEDMONT EO1-53-20-0234.

Part: STRUCTURE — CORRODED (LAVATORY) · airframe 37,060 hrs · 32,779 cycles

LAV DUMP BUCKET CORRODED. MAINTENANCE: REMOVED AND REPLACED LAV BUCKET IAW SRM 51-40-02.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 36,963 hrs · 32,666 cycles

LANDING GEAR DID NOT RETRACT ON T/O. LG/LEVER DIS, EICAS WARNING. PERFORMED QRH, GEAR RETRACTED NORMALLY. PER QRH, GEAR THEN EXTENDED NORMALLY, NORMAL LANDING MADE. MAINTENANCE: PERFORMED GEAR SWING IN EF TO AMM 32-30-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: ENGINE — UNKNOWN (NR 2) · airframe 36,896 hrs · 32,581 cycles

THROUGH 200FT E2 ROLL BACK WITH E2 OUT AFTER HEARING THUMP FROM #2 SIDE. NOTED E2 OIL PSI IN YELLOW PRIOR TO EVENT....FIX: ENGINE R&R IN PROGRESS PHL

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 36,762 hrs · 32,432 cycles

LANDING GEAR LEVER DISAGREE MESSAGE DISPLAYED. PERFORMED GEAR SWING NO DEFECTS NOTED OK FOR SERVICE.

Part: CONTROLLER — DEFECTIVE (WINDOW HEAT) · airframe 36,031 hrs · 31,598 cycles

PDIS 695 05-50 1904473 14SEP19 CLT CLOSE REOCCURING ELECTRICAL ODOR OBSERVED MULTIPLE TIMES IN FLIGHT DECK. FACT 14SEP19 16:39 CLT T/S AND FOUND FO'S W/S HEAT DRAWING EXCESSIVE CURRENT. INSPECTED W/S CONNECTIONS AND CONTACTORS, NO DEFECTS NOTED. R+R FO'S W/S HEAT CONTROLLER. OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,905 hrs · 31,455 cycles

EMERGENCY PATH LIGHT SECTION 7 INOP. R&R EMERGENCY PATH LIGHT SECTION 7 IAW AMM 33-50-12-04. OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,756 hrs · 30,156 cycles

PDIS 695 52-30 1721522 03JAN19 PHL ASSGN ABORTED TAKEOFF DUE TO BAG DOOR WARNING INDICATION ON EICAS. MX VERIFIED DOOR OPS NORM AND IS CLOSED AND LATCHED. MEL 03JAN19 14:36 PHL C00319 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING.

Part: LANDING GEAR — FALSE INDICATION · airframe 34,615 hrs · 29,990 cycles

PDIS 695 32-61 1864742 06DEC18 PHL CLOSE L/G DISAGREE AFTER GEAR WAS RETRACTED. QRH C/W AND MESSAGE EXTINGUISHED. RETURNED TO PHL FACT 06DEC18 18:07 PHL PERFORMED L/G RETRACT/EXTENSION OPS CHECK. OPS GOOD AFTER 10 PLUS CYCLES PER AMM 32-30-00. PERFORMED PROX. SWITCH FUNCTIONAL CHECK OF L/G PER AMM 32-63-05. NO DEFECTS OR EICAS MESSAGES NOTED, OK FOR SERVICE.

Part: SCREW — MISSING (STOP BRACKET) · airframe 34,543 hrs · 29,902 cycles

NDIS 695 52-10 0008280 21NOV18 MDT CLOSE MAIN CABIN ENTRANCE DOOR FWD LOWER DOOR STOP BRACKET HAS 3 SCREWS MISSING FACT 21NOV18 09:58 MDT INSTALLED 3 SCREWS, WASHERS AND NUTS TO FWD LOWER DO OR STOP MOUNTING BRACKET ON MAIN DOOR IRT EMB145 MM 52-18-00

Part: NONE — NONE (NONE) · airframe 34,453 hrs · 29,788 cycles

PDIS 695 05-50 1614951 06NOV18 PWM CLOSE SEVERE TURBULENCE ENCOUNTERED AT 29K FT. WITH A/C CLIMB AND THEN PITCH DOWN. FACT 06NOV18 21:50 PWM C/W SEVERE TURBULENCE INSP. PER AMM 05-50-27. NO DISCREPANCIES NOTED, OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (NR 3 PITOT) · airframe 33,993 hrs · 29,266 cycles

PITOT 3 INOPERATIVE EICAS MESSAGE ILLUMINATED DURING THE NR 1 ENGINE START. CREW FOUND THE CIRCUIT BREAKER TRIPPED. PERFORMED A NR 3 PITOT HEATING OPS CHECK IAW AMM 30-31-00. OPS CHECKED GOOD. GROUND RAN THE ACFT, NO PITOT MESSAGES OR DEFECTS NOTED. INSPECTED RELAYS K0058 AND K0060, NO DEFECTS NOTED. OK FOR SERVICE.

Part: DAU — FAILED (NR 2) · airframe 32,892 hrs · 28,036 cycles

PERFORMED ANTI ICE TEST DURING FLIGHT TEST, FAILED WITH THE NR 1 PACK BLEED VALVE. MULTIPLE OTHER ANTI ICE SYSTEM CAUTION MESSAGES. PERFORMED TEST AGAIN, TEST FAILED WITH SAME RESULTS. R & R THE NR 2 DAU IAW AMM 31-41-01.

Part: WIRE — BROKEN (ANTI ICE SYS) · airframe 32,854 hrs · 27,994 cycles

DURING DESCENT. AFTER ENTERING ICE CONDITION, STAB ANTI ICE FAILED, WING ANTI ICE FAIL AND ICE CONDITION. ANTI ICE INOPERATIVE. REMOVED, CLEANED AND SWAPPED NR 1 AND NR 2 FAN AIR CONTROL THERMOSTATS. R & R IAW AMM 36-11-06-000-802A. OPS AND LEAK CHECKED GOOD. REPAIRED BROKEN WIRE IN OVERHEAD ANTI ICE PANEL

Part: ATTACH ANGLE — CRACKED · airframe 32,793 hrs · 27,942 cycles

RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE NR 2 HAS A 1.5 INCH CRACK ON THE AFT END. REMOVED AND REPACED THE ATTACH ANGLE IAW SRM 51-40-02

Part: ATTACH ANGLE — CRACKED (FRAMES 48-49) · airframe 32,793 hrs · 27,942 cycles

RIGHT WING TO FUSELAGE UPPER ATTACH ANGLE APPEARS TO HAVE A ONE INCH CRACK BY THE RIVET BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 32,793 hrs · 27,942 cycles

SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 16L AND 17L IS CRACKED. -INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED · airframe 32,793 hrs · 27,942 cycles

LEFT WING TO FUSELAGE LOWER ATTACH ANGLE NR 1 IS CRACKED ON THE AFT END APPROXIMATELY ONE INCH LONG. REPAIRED THE ATTACH ANGLE IAW SRM 57-20-01 AND ETN EM-53-142

Part: ATTACH ANGLE — CRACKED · airframe 32,793 hrs · 27,942 cycles

LT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED ON THE FWD END. REPAIRED IAW SRM 57-20-01, AND ETN EM-53-142

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 32,793 hrs · 27,942 cycles

SHEAR TIE AT FRAME 72 BETWEEN STRINGERS 16L AND 17L IS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 32,793 hrs · 27,942 cycles

CARGO DOOR UPPER CABLE WHEEL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 32,793 hrs · 27,942 cycles

CARGO DOOR CENTER WHEEL CABLE SUPPORT BRACKET IS CRACKED IN TWO PLACES. REMOVED AND REPLACED CENTER CABLE WHEEL SUPPORT BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 32,793 hrs · 27,942 cycles

CARGO DOOR FORWARD TORSION BAR SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02.

Part: BUSHING — LOOSE (PCA FITTING) · airframe 32,793 hrs · 27,942 cycles

RIGHT AILERON OTBD PCA ATTACH FITTING ON THE AILERON HAS A BUSHING THAT IS LOOSE IN THE FITTING. R & R THE AILERON PCA FITTING IAW EO EM-27MR-112.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,793 hrs · 27,942 cycles

EMERGENCY LIGHT STRIP AT FLOOR BOARD 251FF IS DAMAGED-C/A-COMPLETE:RAR EMERGENCY LIGHT STRIP AT FLOOR BOARD 251FF IAW EMB 145 AMM 33-50-12 SEE NRWC # BOW263117 FOR OPT'S CHECK

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,712 hrs · 27,857 cycles

EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT CHARGER ASSEMBLY AND BATTERY IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,529 hrs · 27,684 cycles

LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW WIRING MANUAL 33-50-50 AND FOUND THE NR 4 BATTERY AND CHARGER BAD. R & R THE 4 BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,363 hrs · 27,550 cycles

BOTH LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE FUSE IN THE NR 4 BPSU IAW CMM 26-60-03. OPS TEST OF EXTERIOR OVERWING EMERGENCY LIGHTS CHECKS OK IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,109 hrs · 27,326 cycles

FLOOR EMERGENGY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: INVERTER — DEFECTIVE (CABIN) · airframe 30,479 hrs · 25,791 cycles

DURING PS-2, FOUND EMERGENCY LIGHT STRIP FROM ROW 3A TO 7A VERY DIM. R&R DC/AC INVERTER NR 2 IAW AMM 33-50-11. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,965 hrs · 25,344 cycles

RIGHT FWD WING EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 29,938 hrs · 25,321 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW 33-50-16. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,733 hrs · 24,195 cycles

CAPTAINS FLASHLIGHT STOPPED WORKING ON POSTFLIGHT. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16-4.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 28,654 hrs · 24,116 cycles

LOUD WHISTLING NOISE FROM MAIN CABIN DOOR, STARTED ABOVE FL 220 TO FL 340. THE WHISTLING WAS LOUD AT FL 220 BUT NOT AS QUIET. AT FL 340. ALL PRESSURE INDICATIONS IN COCKPIT READ NORMAL. CLEANED MAN DOOR SEAL & PERFORMED LEAK CHECK IAW AMM 21-31-00 NO SEALS TORN. ACFT OK FOR SERVICE.

Part: CLAMP — FAILED (BLEED AIR) · airframe 28,530 hrs · 24,005 cycles

BLEED LEAK ENG NR 1 CLIMBING OUT THROUGH 2000 FT. R & R LT ENG PYLON BLEED VALVE V CLAMP NEXT TO FIREWALL DUE TO LEAKAGE IAW AMM 20-10-02. OPERATIONS CHECKED IAW AMM 36-00-00. OPERATIONS CHECKED OK. NO LEAKS NOTED.

Part: DUCT — DETACHED (AC BAY) · airframe 28,529 hrs · 24,004 cycles

BLEED 1 LEAK CLIMBING THROUGH 3000 FEET. LANDED UNDER WT 43000 LBS. TRANSFERRED TO NRWC 695-MIA-02360. DOWNLOADED CMC IAW-AMM-45-45-00 & NO FADEC OVERTEMP FOUND. RE-CONNECTED LT RAM AIR DUCT IAW-AMM-21-25-01. PERFORMED BLEED SYS 1 & 2 OPERATIONAL CHECK AT CRUISE POWER FOR 15 MINUTES IAW-AMM-36-00-00-860-801-A. NO BLEED LEAKS NOTED. SEE NRWC 695-MIA-02360 FOR CORRECTIVE ACTION.

Part: SKIN — DENTED (LT WING) · airframe 28,514 hrs · 23,991 cycles

LEFT LE NR 1, 511 IS DENTED 54" FROM THE INBD EDGE. COMPLETED REPAIR IAW ERS-EM-57MR-547.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,514 hrs · 23,991 cycles

LEFT AFT FUSELAGE SKIN SHOWS ADVERSE SCREEN INDICATIONS DURING HFEC. THREE PLACES AT FRAME 75, BETWEEN STRINGERS 1L & 3L. REPAIRED LT AFT FUSELAGE SKIN IAW ERS-EM-53MR-1751.

Part: FITTING — WORN (LT AILERON) · airframe 28,514 hrs · 23,991 cycles

LEFT PCA TO AILERON ATTACH LUG BUSHINGS ARE MIGRATED. LT DAMPNER TO AILERON ATTACH LUG BUSHING REQUIRES REPLACEMENT, SEIZED TO BOLT. R & R PCA FITTING IAW EO EM-27MR-112. REPLACED DAMPER FITTING IAW EO EM-27MR-112. FITTING PN 145-69382-609.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 28,514 hrs · 23,991 cycles

RIGHT AILERON PCA TO AILERON INBD ATTACHMENT, OTBD HAT BUSHING MIGRATING. REPLACED PCA FITTING IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,514 hrs · 23,991 cycles

AFT CARGO DOOR SILL CORRODED. COMPLETED INSTALLATION OF CARGO DOOR SILL IAW SRM 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 28,514 hrs · 23,991 cycles

CARGO DOOR SUPPORT ROD HOLDER BRACKET IS CRACKED ON THE BACK SIDE. COMPLETED REPLACEMENT OF CARGO DOOR SUPPORT ROD HOLDER BRACKET ASSEMBLY IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,514 hrs · 23,991 cycles

LEFT WING TO FUSELAGE, LOWER ATTACH ANGLE IS CRACKED AT FRAME 47. R & R LT WING TO FUSELAGE, LOWER ATTACH ANGLE AT FRAME 47 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,514 hrs · 23,991 cycles

RIGHT WING TO FUSELAGE, LOWER ATTACH ANGLE IS CRACKED, BETWEEN FRAMES 47 & 48. R & R RT WING TO FUSELAGE LOWER ATTACH ANGLE IAW ETN-EM-53-142 R1.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,514 hrs · 23,991 cycles

RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. REPAIRED RT WING TO FUSELAGE LOWER ATTACH ANGLE AT FRAME 46 IAW ETN-EM-53-142R2. REFERENCE NRTC E479870 FOR LEAK CHECK OF FASTENERS.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,514 hrs · 23,991 cycles

LEFT WING TO FUSELAGE, LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. NEW ANGLE INSTALLED IAW ETN-EM-53-142.

Part: CONNECTOR — MISSING (CABIN) · airframe 28,514 hrs · 23,991 cycles

AFT EMER FLOOR LIGHT IS MISSING BOTH WIRE CONNECTORS. ACFT SIDE. REPLACED BOTH EMER LIGHT CONNECTORS IAW SWPM 20-21-00, OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,514 hrs · 23,991 cycles

LEFT & RT OVERWING EMER LIGHTS INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM 33-50-04.

Part: WIRE — BROKEN (CABIN) · airframe 28,514 hrs · 23,991 cycles

NUMBER 3 EMER FLOOR LIGHT HAS 2 BROKEN WIRES AT FLOOR LEVEL. REPAIRED WIRING IAW SWPM 20-21-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,402 hrs · 23,893 cycles

BACK FLASHLIGHT NOT CHARGING. R & R FLIGHT ATTENDANT REAR FLASHLIGHT BATTERY & CHECKED OK IAW MM 25-60-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,198 hrs · 23,725 cycles

LEFT OVERWING EXTERIOR EMER LIGHT FAILS TO ILLUMINATE. R & R NR 4 EMER BATTERY SUPPLY & CHARGER IAW WC 33-700-19. OPERATIONAL CHECKED GOOD.

Part: ACM — SEIZED (NR 2) · airframe 27,963 hrs · 23,509 cycles

COCKPIT & CABIN FILLED WITH SMOKE AT FL 240. NR 2 PACK INOPERATIVE DUE TO SEIZED ACM. PERFORMED TASK IAW FIM 21-20-00 & ETN-EM-72-034. R & R NR 2 PACK ACM IAW AMM 21-51-03. LEAK & OPS CHECKED GOOD.

Part: CRADLE — MELTED (FLASHLIGHT) · airframe 27,788 hrs · 23,354 cycles

FORWARD CABIN EMER FLASHLIGHT CRADLE IS STARTING TO MELT AT CAPACITOR. R & R FWD CABIN FLASHLIGHT CRADLE ASSEMBLY IAW WC 33-700-20.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 27,788 hrs · 23,354 cycles

AFT CABIN FLASHLIGHT CRADLE WIRING FLATTENED & KINKED. R & R AFT CABIN FLASHLIGHT CRADLE ASSEMBLY IAW WC 33-700-20.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,717 hrs · 23,292 cycles

LEFT & RIGHT TOP OF THE WING EMER LIGHT WILL NOT COME ON. R & R EMER LIGHTING POWER SUPPLY NR 4 IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 & SN C01230.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,632 hrs · 23,215 cycles

LEFT WING EXTERIOR EMER EXIT LIGHT BELOW WING HATCH INOPERATIVE. R & R LT WING EXTERIOR EMER EXIT LIGHT BULB BELOW WING HATCH IAW AMM 33-50-10. OPERATIONAL CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,958 hrs · 22,536 cycles

REAR CABIN FLASHLIGHT DOES NOT WORK. R & R REAR CABIN FLASHLIGHT ASSEMBLY IAW MM 33-50-16.

Part: ACM — FAILED (AC BAY) · airframe 26,840 hrs · 22,422 cycles

AFTER E1 START, SMELLED A BURNT RUBBER SMELL & CABIN FILLED WITH A LIGHT WHITE HAZE. APU ON WITH PACK 2, NO PROBLEM, E1 ON PACK 2 WE BEGAN TO SMELL A BURNT SMELL & HAZE. TROUBLE SHOT & FOUND NR 2 PACK ACM LOCK UP. R & R NR 2 PACK ACM IAW AMM 21-51-03. OPERATIONS CHECKED GOOD. NO ODOR OR SMELL DETECTED AT THIS TIME.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR) · airframe 26,277 hrs · 21,941 cycles

COCKPIT DOOR SLIDING LATCH HARD TO MOVE. LUBRICATED COCKPIT DOOR SLIDING LATCH IAW AMM SMP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,235 hrs · 21,897 cycles

CAPTAIN EMER FLASHLIGHT RED LIGHT DOESN'T STAY ON. R & R CAPTAIN EMER FLASHLIGHT ASSEMBLY. OPERATIONS TESTED OK IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,170 hrs · 21,830 cycles

DURING PS 1 CHECK FOUND EXTERIOR EMER LIGHT LOCATED ON SIDE OF FUSELAGE NEXT TO THE LE OF THE LT WING INOPERATIVE. R & R LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,944 hrs · 21,633 cycles

EMERGENCY FLOOR LIGHT STRIP INOPERATIVE IN CTR OF CABIN. R & R EMER LIGHT DC & AC INVERTER NR 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,201 hrs · 21,027 cycles

FORWARD CABIN AFT GALLEY EXIT SIGN INOPERATIVE. PERFORMED TROUBLESHOOTING, FOUND CONNECTOR P8530 DISCONNECTED AT NR 2 EMER LIGHT BATTERY ASSEMBLY. SECURED CONNECTOR IAW WM CHAPTER 20-50-00, OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 25,002 hrs · 20,856 cycles

AIRCRAFT AVIONICS LT ON BY REPOSITION CREW. WHEN ARRIVING TO ACFT ELEC SMOKE SMELL IN COCKPIT & PFD NR 2 CB POPPED. R & R NR 5 DU IAW AMM 34-22-01. OPERATIONS CHECKED GOOD. ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATIONS. BEZEL UNIT PN 7014331921 SN 04065596.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND THE SERVICE DOOR CTR SILL HAS CORROSION AROUND THE NUT PLATES. REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT CARBON CROSS BEAM OF FRAME 59. REPAIRED DAMAGED CENTER OMEGA BEAM AS REQD IAW EO EM-53MR-1518.

Part: FITTING — CORRODED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND CARGO DOOR FWD SHEAR CLIP AT FRAME 65 HAS CORROSION JUST ABOVE CARGO SILL. COMPLETED REPAIR TO FR 65 SHEAR CLIP IAW SRM 53-31-04, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND LT OMEGA BEAM SUPPORT OTBD FLANGE CRACKED AT FRAME 47. REPAIRED LT OMEGA BEAM SUPPORTS IAW SRM 53-23-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND LT OMEGA BEAM CORRODED AT THE CARBON CROSS BEAM OF FRAME 59. REPAIRED DAMAGED LT OMEGA BEAM AS REQD IAW EO EM-53MR-1518.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,101 hrs · 20,136 cycles

DURING MBV INSPECTION FOUND RT OMEGA BEAM SUPPORT INBD FLANGE IS CRACKED AT FRAME 47. REPLACED RT OMEGA BEAM SUPPORT, INBOARD FLANGE IAW SM 53-23-02.

Part: LIGHT — CRACKED (CABIN) · airframe 24,101 hrs · 20,136 cycles

FLOOR PROXIMITY LIGHT EXTRUSION NR 4 CRACKED. R & R NR 4 FLOOR PROXIMITY LIGHT EXTRUSION IAW AMM 33-50-12.

Part: LIGHT — CRACKED (CABIN) · airframe 24,101 hrs · 20,136 cycles

NUMBER 2 FLOOR PROXIMITY EMERGENCY LIGHT IS CRACKED. R & R NR 2 FLOOR PROXIMITY EMERGENCY LIGHT IAW AMM 33-50-12.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 24,101 hrs · 20,136 cycles

COPILOT’S WINDSHIELD INTERIOR FRAME IS CORRODED. INSPECTED & FOUND COPILOT’S WINDSHIELD INTERIOR FRAME CORROSION TO BE OUT OF LIMITS. IAW NRWC E359210 FOR NEW PART INFORMATION & NRWC E358855 FOR NEW WINDSHIELD INSTALLATION.

Part: WIRE — BROKEN (CABIN) · airframe 24,101 hrs · 20,136 cycles

NUMBER 6 FLOOR PROXIMITY EMERGENCY LIGHT HAS BROKEN WIRES. R & R NR 6 FLOOR PROXIMITY EMERGENCY LIGHT IAW AMM 33-50-12.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,993 hrs · 20,056 cycles

ON FLIGHT 3531 CREW REPORTED DURING APU START ALL ELECTRONICS & RELAYS WERE CLICKING ON & OFF & THERE WAS A BURNING SMELL. AFTER DE SELECTING THE GPU THE SMELL WENT AWAY GPU SHOWED 28.4 VOLTS. THE ACFT WAS REMOVED FROM SERVICE. POWERED ACFT ELEC SYS DOWN & INSPECTED ELEC COMPARTMENT BY DVI & FOR BURNING SMELL, NONE WAS NOTED. RE-SET ELEC POWER & STARTED APU SYSTEMS, OPERATING NORMAL IAW AMM 24-31-00. THE ACFT RETURN TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 23,969 hrs · 20,044 cycles

FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR IS VERY HARD TO OPEN. CLEANED & LUBRICATED MAIN DOOR, FOUND NO PROBLEMS AT THIS TIME IAW AMM 52-10-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,073 hrs · 19,329 cycles

ENTIRE PLANE SMELLS LIKE A BAD LAVATORY. R & R TOILET SHROUD FOR GENERAL VISUAL INSPECTION IAW AMM 25-40-04. DID NOT VIEW ANY POSS. LEAKS, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,999 hrs · 19,264 cycles

CAPTAIN`S EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 21,980 hrs · 18,467 cycles

FLIGHT 3358, CAPTAIN’S FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED COCKPIT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 21,922 hrs · 18,433 cycles

ON FLIGHT 3289 THE CREW REPORTED THAT A TIRE BLEW ON TAXI OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 TIRE WHEEL ASSY IAW WORKCARD 32-700-11 AND REMOVED AND REPLACED NR 1 BRAKE ASSY IAW WORKCARD 32-600-01. OPS CHECK GOOD NO LEAK NOTED. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 20,995 hrs · 17,740 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN FELL OUT AND HANGING BY ELECTRICITY WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED ASSEMBLY LIGHT IAW MM33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 20,963 hrs · 17,710 cycles

FOR FLIGHT 3526 THE FLIGHT ATTENDANT REPORTED THE EMERGENCY EXIT SIGN BY SEAT 1A CAME OFF- IT NEEDS TO BE RE-SECURED. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED THE EMERGENCY EXIT SIGN BY SEAT 1A IAW EMB 145 AMM 20-12-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — LOOSE (CABIN) · airframe 20,929 hrs · 17,682 cycles

ON FLIGHT 3979 THE CREW REPORTED THE EXIT SIGN WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED EXIT SIGN. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS GOOD IAW EMB 145 AMM 33-50-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — LOOSE (AC BAY) · airframe 19,741 hrs · 16,799 cycles

ON FLIGHT 3464 THE CREW REPORTED THAT WHEN FLYING THE AIRCRAFT THROUGH MEDIUM TO HEAVY PRECIPITATION THE CREW NOTICED AN ODOR IN THE COCKPIT THAT SEEMED LIKE A MILDEW. IT WENT AWAY AFTER EXITING PRECIPITATION. THE ODOR WAS ONLY NOTICED IN THE COCKPIT NOT IN CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED LEFT PACK DUCT IAW EMB-145 AMM 21-20-04. THE OPERATIONAL CHECK WAS GOOD. NO MILDEW ODOR NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 19,667 hrs · 16,731 cycles

DURING B INSPECTIONS, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE BULB IN SOCKET, SECURED BULB AS PER MM 33-50-09. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 19,555 hrs · 16,637 cycles

DURING B INSPECTION, FOUND THE NR 3 AND NR 4 PROXIMITY LIGHT WIRING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 AND NR 4 FLOOR PROXIMITY STRIPS IAW EMB145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,555 hrs · 16,637 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,555 hrs · 16,637 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT NR 1 AND NR 7 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT NR 1 AND NR 7 IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 19,434 hrs · 16,535 cycles

ON FLIGHT 4160 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND UPPER ROLLERS HITTING TRACKS. ADJUSTED ROLLERS IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — OVERHEATED (CABIN) · airframe 17,257 hrs · 14,597 cycles

ON FLIGHT 3348 THE CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE SHOWS SIGNS OF OVERHEATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,210 hrs · 14,125 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD EXIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW EMB AMM 33-50-10. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. THE EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 16,071 hrs · 14,022 cycles

DURING MAINTENANCE FOR FLIGHT 4061 THE FORWARD FLIGHT ATTENDANT’S FLASHLIGHT ASSEMBLY WAS FOUND TO BE BROKEN. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT IAW 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 15,208 hrs · 13,332 cycles

ON FLIGHT 2827 DURING TAKEOFF THE CREW REPORTED, AIR CONDITIONING SMOKE IN THE COCKPIT. THE CAPTAIN ELECTED TO ABORT THE TAKEOFF. THE CREW PERFORMED CHECK LIST PROCDURES AND RETURNED TO THE GATE. NO FURTHER ANOMALIES; NO SMOKE NOTED DURING TAXI. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECKS AND LEAK CHECKS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. PER THE TEAR DOWN REPORT THE NUMBER 4 CARBON SEAL WAS FOUND TO BE FAULTY

Part: UNKNOWN — ODOR (CABIN) · airframe 14,343 hrs · 12,637 cycles

ON FLIGHT 3543 DURING CRUISE THE CREW REPORTED PASSENGERS AT SEATS 2BC-5BC INDICATED AN ODOR OF BURNING RUBBER AT 37000 FEET. THE CREW DESCENDED TO 25000 AND TURNED OFF PACK 2 AND THE ODOR WENT AWAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE HAD THE CREW RUN BOTH ENGINE AND PACKS AND COULD NOT DUPLICATE THE ODOR. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (FIRE CONTROL) · airframe 13,357 hrs · 11,868 cycles

THE CREW FOR FLIGHT 4133, NOTIFIED MOC WHEN ON THE GATE IN MIA THAT DURING FLIGHT THEY RECEIVED AN INTERMITTENT E2 FIRE DETECT FAIL MESSAGE ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 FIRE CONTROL MODULE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,037 hrs · 11,604 cycles

DURING P2-2 INSPECTION FOUND THE LEFT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FROM THE LEFT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE)

DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW EMB SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (S)

Part: ENGINE — LEAKING (RIGHT) · airframe 6,798 hrs · 5,903 cycles

LAVATORY SMOKE WARNING WITH SMOKE IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORKCARD 72-000-00. LEAK AND OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REMOVED CORRODED AREA BY PERFORMING A CUTOUT, FABRICATE A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145-1142 REV 34, CHAPTER 53-00-10 AND CPM, CPM-145/1132 REV 13 CHAPTERS 51-21-04, 51-21-05 AND 51-21-06. AIRCRAFT RETURNED TO SERVICE. (M)