N685AE

Part: ENGINE — MAKING METAL (NR 2) · airframe 45,245 hrs · 41,498 cycles

ENGINE 2 SHUTDOWN IN FLIGHT, WITH NO N2 ROTATION DFRL 28OCT24 21:14 PHL MX FOUND FOD IN CORE AND EXHAUST. RAR #2 ENGINE IAW WC 710000 AND OPS CHECKED IAW WC 727000

Part: UNKNOWN — ODOR (ZONE 200) · airframe 45,229 hrs · 41,473 cycles

AT 1'000FT BURNING SMELL IN CABIN AND FLT DECK DISSIPATED APROX. 7 MINUTES LATER FACT 25OCT24 09:07 FLO RAN BOTH PACKS ON APU SEVERAL MINTUES. NO BURNING SMELL NOTED. RAN BOTH ENGINES TO HIGHPOWER WITH CREW. BOTH BLEEDS AND PACKS ON NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2388 SHEAR CLIP CRACKED AT FR80 BTW STR3-5R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2283 SHEAR CLIP CRACKED AT FR80BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 300) · airframe 45,212 hrs · 41,450 cycles

53-2260 VERT STAB, AFT OF REAR SPAR 3, RH SKIN PROFILE CRACKED BTW YH1423 AND YH1932. REPAIRED IAW EO 1-55-24-0577

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2224 SHEAR CLIP CRACKED AT FR48 BTW STR13-14L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLAP TRACK — WORN (ZONE 600) · airframe 45,212 hrs · 41,450 cycles

57-2212 RH WING OB FLAP, IB TRACK WORN. RAR TRACK IAW AMM 57-30-01

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2209 RH OMEGA BEAM CRACKED AT BTW FR59-60 AND FR60-61. REPAIRED IAW EO1-53-24-0508.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2210 LH OMEGA BEAM CRACKED AT BTW FR59-60 AND FR61-61. REPAIRED IAW EO 1-53-24-0580 AND EO 1-53-24-0583

Part: ANGLE — CRACKED (FRM 10) · airframe 45,212 hrs · 41,450 cycles

53-2183 ANGLE CRACKED AT FR10 RH SIDE UNDER WINSHIELD. RAR ANGLE IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2128 ANGLE CRACKED AT TOP OF FR10, UNDER LH SIDE WINDOW. RAR ANGLE IAW SRM 51-40-02

Part: GUSSET — CORRODED · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2188 RH GUSSET CORRODED AT BTW FR59-61. RAR GUSSET IAW SRM 51-40-02

Part: GUSSET — CORRODED · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2190 CORRODED LH GUSSET BTW FR59-61. RAR GUSSET IAW SRM51-40-02

Part: GUSSET — CORRODED · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2188 RH GUSSET BTW FR59-61 IS CORRODED. RAR GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2184 LH SHEAR CLIP CRACKED AT FR10 BTW STR9-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2189 CORROSION ON CTR GUSSET AT BTW FR59-61. FABRICATED REPLACEMENT GUSSET IAW SRM 53-2U-10 AND 51-30-01. RAR GUSSET IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2186 SHEAR CLIP CRACKED AT LH SIDE OF FR58 BTW STR 15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: THRUST REVERSER — CRACKED (RIGHT) · airframe 45,212 hrs · 41,450 cycles

78-2163 RH TR IB SIDE, CRACK AROUND ANCHOR NUT ON THE FRONT BULKHEAD ON THE BEAMS AT THE PRIMARY LOCK. REPAIRED IAW EO1-05-24-0564

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2141 LH OMEGA BEAM #1 CRACKED AT FR21,22,23. REPAIRED IAW EO1-53-24-0581

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2115 CARGO DOOR LWR BEAM FWD SUPPORT ANGLE FITTING CORRODED AT FR65. RAR ANGLE FITTING IAW SRM 51-40-02

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 45,212 hrs · 41,450 cycles

78-2164 RH TR, OB SIDE, CRACK AROUND ANCHOR NUT ON THE FRONT BULKHEAD ON THE BEAMS AT THE PRIMARY LOCK. REPAIRED IAW EO1-53-24-0564

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2118 RH SIDE SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2129 SHEAR CLIP CRACKED AT RH SIDE OF FR16 BTW STR15-16R. RAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2154 SHEAR CLIP CRACKED AT FR73 BTW STR9-10L. RAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2126 RH SIDE SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2119 OMEGA BEAM #2 CRACKED AT FR24 &25, CORROSION ON FR29. REPAIRD IAW ETD2024-145-024776 AND EO1-53-24-0576

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2153 SHEAR CLIP CRACKED AT FR68 BTW STR6-10R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2152 SHEAR CLIP CRACKED AT FR62 BTW STR6-8R. RAR CLIP IAW SRM 51-40-02

Part: BEAM — CRACKED (ZONE 400) · airframe 45,212 hrs · 41,450 cycles

78-2166 CRACK AROUND ANCHOR NUT ON LH TR OB SIDE, FRONT BULKHEAD ON THE BEAMS AT THE PRIMARY LOCK. REPAIRED IAW EO1-05-24-0564A

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2155 SHEAR CLIP CRACKED AT FR66 BTW STR7-9L. RAR SHEAR CLIP IAW EO1-53-24-0629

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,212 hrs · 41,450 cycles

53-2124 SHEAR CLIP CRACKED AT FR26 BTW STR16-17R. RAR CLIP IAW SRM 51-40-02

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2116 CARGO DOOR OPENING L-SHAPE CORRODED AT FR65. REPAIRED IAW EO1-53-24-0584

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2156 SHEAR CLIP CRACKED AT FR67 BTW STR6-7L. RAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2123 RH SIDE SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FRAME — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2125 FR25 RH SIDE CRACKED AT BTW STR15-16R. REPAIRED IAW EO1-53-24-0575

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2117 RH SIDE SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 45,212 hrs · 41,450 cycles

78-2165 LH TR IB SIDE, FRONT BULKHEAD ON THE BEAMS AT THE PRIMAY LOCK, CRACK FOUND AROUND THE ANCHOR NUT. REPAIRED IAW EO1-05-24-0564

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2122 SHEAR CLIP CRACKED AT FR28 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2128 LH OMEGA BEAM #3 CRACKED AT BTW FR31-33. REPAIRED IAW EO 1-53-24-0579

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2120 LH SIDE SHEAR CLIP CRACKED AT FR25 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 5-40-02

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2115 CARGO DOOR OPENING LWR BEAM SUPPORT ANGLE FITTING CORRODED AT FR65. RAR FITTING IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2137 GUSSET BTW LH OMEGA BEAM AND CTR OMEGA BEAM IS CORRODED AT FR16-18. BLENDED, OUT OF LIMITS, RAR GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2130 RH SIDE FR17 BTW STR15-16R SHEAR CLIP CRACKED. RAR CLIP IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,212 hrs · 41,045 cycles

53-2112 CARGO DOOR LWR BEAM CORRODED BTW FR65-68. RAR BEAM IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2157 SHEAR CLIP CRACKED AT FR62 BTW STR6-8L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: CROSSBEAM — CRACKED (ZONE 100) · airframe 45,212 hrs · 41,850 cycles

53-2113 ON CARGO DOOR LWR BEAM, CROSS BEAM LWR SUPPORT ANGLE CRACKED AT FR66. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2121 LH SIDE SHEAR CLIP CRACKED AT FR26 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,212 hrs · 41,450 cycles

53-2131 SHEAR CLIP CRACKED AT FR22 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FASTENER — LOOSE (T/R DOOR) · airframe 45,212 hrs · 41,450 cycles

53-2114 LOOSE RIVETS ON RH TR LWR DOOR. REPAIRED IAW ETD2024-145-24496 AND EO1-05-24-0564A

Part: RIB — CRACKED (ZONE 500) · airframe 45,212 hrs · 41,450 cycles

57-2061 RH WING AT RIB 9 SLICE XIV CRACKED AT 1 HY-LOK HOLE. REPAIRED IAW EO1-57-24-0600

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,212 hrs · 41,450 cycles

53-2036 RH WING TO FUSE FAIRING LWR ANGLE CRACKED AT BTW FR47-48. RAR ANGLE IAW SRM 51-40-02

Part: CUP — CORRODED (TOILET) · corrosion level 2 · airframe 45,212 hrs · 41,450 cycles

53-2039 TOILET WAST CUP CORRODED. REPAIRED IAW EO1-53-24-0585

Part: RIB — CRACKED (ZONE 500) · airframe 45,212 hrs · 41,450 cycles

57-2062 LH WING AT RIB 9 LWR SPLICE XIV CRACKED AT 3 HI-LOK HOLES. REPAIRED IAW EO1-57-24-0600

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,212 hrs · 41,450 cycles

LH WING TO FUSE FAIRING LWR ANGLE CRACED AT FR47. RAR ANGLE IAW SRM 51-40-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 44,692 hrs · 40,865 cycles

WING A/I FAIL IN ICING WITH WING A/ICE LOW PRESS MESSAGE ON CMC. FACT 14MAY24 09:41 MGM PERFORMED ANTI-ICING SYSTEM OPS CHECK IRT AMM 30-00-00-802-A & 30-00-00-700-803-A. OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

ACCOMPLISH PERMANENT REPAIR OF RUDDER PROTRACTOR MISSING NUTPLATE. REAIRED IAW PIEDMONT EO 1-05-23-0053

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB 145 SRM51-40-02 AND 145-53-0068

Part: NONE — NONE · airframe 42,486 hrs · 38,375 cycles

UNABLE TO PRESSURIZE A/C IN IETHER AUTOMATIC OR MANUAL MODE WITH LIGHT VISIBLE AROUND MAIN PAX DOOR

Part: NONE — NONE · airframe 42,486 hrs · 38,375 cycles

UNABLE TO PRESSURIZE A/C IN IETHER AUTOMATIC OR MANUAL MODE WITH LIGHT VISIBLE AROUND MAIN PAX DOOR

Part: LIGHT — INOPERATIVE (RH) · airframe 41,783 hrs · 37,567 cycles

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

Part: LIGHT — INOPERATIVE (RH FWD WING) · airframe 41,783 hrs · 37,567 cycles

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

Part: PANEL — OPEN (GPU PANEL) · airframe 41,529 hrs · 37,274 cycles

FOA, COMM SIDE PANEL OPEN CREW DECLARED AN EMERGANCY LANDING FOR A OPENED GPU PANEL-C/A-OPENED AND CLOSED PANEL, INSPECTED FOR DAMAGE. NO DEFECTS FOUND.

Part: LAMP — INOPERATIVE (12B) · airframe 41,225 hrs · 36,916 cycles

SEAT 12BC OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LAMP IAM EMB 145 AMM 33-50-07. OPS CHECK GOOD.

Part: NONE — NONE · airframe 40,795 hrs · 36,454 cycles

DIVR TO GRB ACCT E1/2 FUEL IMP BYPASS MESSAGE. EMERGENCY DECLARED FLIGHT CONTINUED -C/A-RAR ENGINE #2 FUEL FILTER IAW RRMM 73-21-10 LEAK CHECK GOOD IAW RRMM 72-00-00

Part: NONE — NONE · airframe 40,792 hrs · 36,449 cycles

#1 ENGINE FWD ENGINE MOUNT YOKE FORK IS CRACKED ON FWD INBD RADIUS. (MAJOR REPAIR)-C/A-COMPLETE: INSTALLED NEW LOWER FWD #1 ENGINE YOKE FORK FITTING IAW ERS-EM-54MR-698

Part: DOOR SILL — CORRODED (FRMS 65-68) · airframe 40,792 hrs · 36,449 cycles

CARGO SILL CORRODED LEVEL 1 CORROSION (MAJOR REPAIR)-C/A-COMPLETE: INSTALLED NEW CARGO DOOR SILL IAW SRM 51-40-02.

Part: NONE — NONE · airframe 40,792 hrs · 36,449 cycles

FRAME 67 IS CRACKED AROUND RIVET HOLES AT STR 18L-C/A-COMPLETE: C/W FRAME 67 SPLICE REPAIR AT STR,18L IAW SRM 53-00-04 ITEM #4 FIG.201.

Part: NONE — NONE · airframe 40,792 hrs · 36,449 cycles

FRAME 66 IS CRACKED AROUND RIVET HOLES AT STR 18 L-C/A-COMPLETE: REPAIRED IAW SRM 53-00-04 ITEM #4 FIG 201.

Part: NONE — NONE · airframe 40,792 hrs · 36,449 cycles

EMERGENCY FLOOR PATH LIGHTING WIRES AT FRAME 49 ARE MISSING CONNECTORS-C/A-COMPLETE:REPLACED EMERGENCY FLOOR LIGHT CONNECTORS AT FRAME 49 IAW EMB SWPM 20-50-01. SEE PS-2 FOR OPC OF EMERGENCY LIGHTING.

Part: NONE — NONE · airframe 40,792 hrs · 36,449 cycles

LH #1 EMERGENCY PROXIMITY LIGHT HAS BROKEN WIRE.-C/A-COMPLETE:INSTALLED NEW LH #1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. REF BOW 359190 FOR OPS CHECK.

Part: NONE — NONE · airframe 40,412 hrs · 36,018 cycles

FA REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN-C/A-CLEANED AND LUBED PAX DOOR ROLLERS. PERFORMED OPS CHECK IAW E145 AMM 25-10-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT ASSY — BROKEN (CABIN) · airframe 40,348 hrs · 35,959 cycles

FWD AND AFT FLASHLIGHT ASSY TABS BROKEN-C/A-RAR FWD AND AFT FLASHLIGHT ASSY IAW ETN -EM-33-059

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,094 hrs · 35,665 cycles

DURING PS-1 CHECK, FOUND ROW 3 GALLEY BULKHEAD EMERGENCY EXIT LIGHT INOP-C/A-RAR EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-50-14. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 39,921 hrs · 35,482 cycles

FA REPORTS MAIN CABIN DOOR HARD TO OPEN. FO HAD TO ASSIST TO OPEN.-C/A-LUBED DOOR ROLLERS AS NEEDED OPS CHECK GOOD IAW EMD 145 AMM 52-10-01.

Part: WIRE HARNESS — DAMAGED (RT MLG BRAKE) · airframe 39,872 hrs · 35,422 cycles

MECHANICAL / LANDING GEAR GND FAIL MSG AFTER TAKEOFF EMERGENCY DECLARED- BRAKE OVERHEAT CAUTION MESSAGE. ERRATIC RT INBOARD - PEGGED AT MAX TEMP -MEL 3203 AUTH 060159DM-C AML 4764592 ITEM 1.-C/A-TROUBLESHOT RH MLG BRAKE TEMP INDICATION HARNESS IAW SWPM 20-20-03. NO TIME TO FIX. UPDATED KVA. MEL CONTINUES. M PROCEDURES RE-COMPLIED WITH.

Part: PROXIMITY SWITCH — FAILED (WOW) · airframe 39,854 hrs · 35,402 cycles

INBOUND DFW LG AIR GRND FAIL CAUTION / DECLARED EMERGENCY- "TRANSFERRED FROM AML PAGE 4764587 ITEM 2-LG AIR/GND FAIL EICAS CAUTION PCESENT AT - FL 180 -> GROUND-C/A-RAR LH AFT WOW PROXIMITY SWITCH IAW AMM 32-63-01.PERFORMED AIR/GROUND OPERATIONAL CHK IAW AMM 32-63-00.OPC GOOD. NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 39,797 hrs · 35,337 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AT GATE CABIN ALT INDICATING 500-C/A-LUBRICATED MAIN CABIN DOOR ROLLERS AND PERFORMED OPS CHECK IAW AMM 52-10-01 OPS CHECK GOOD

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 39,662 hrs · 35,182 cycles

STEERING INOP UPON TAXI RUNWAY WITH LOUD NOISE ABORTED TAKEOFF-C/A-ADJUSTED AND TESTED NWS IAW 32-50-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,528 hrs · 35,028 cycles

AISLE EMERGENCY LIGHT INOP AT ROW 12-C/A-RAR AISLE EMERGENCY LIGHT LAMP AT ROW 12 IAW EMB 145 AMM 33-50-08. OPC GOOD

Part: SLEEVE — DAMAGED (AIR DUCT) · airframe 39,501 hrs · 34,992 cycles

BLEED 2 LEAK IN FLIGHT DECLARED EMERGENCY EQUIPMENT SWAP FLT CONT. -C/A-RAR Y-DUCT, SLEEVES AND CLAMPS AT RH PACK.IAW REF ETN-EM-21-056. PERFORMED OPC IAW AMM EMB 145 21-51-00. OPC GOOD. NO DEFECT NOTED. IN REF WITH 21-60-01.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 39,447 hrs · 34,934 cycles

CABIN DOOR DIFFICULT TO CLOSE-C/A-LUBRICATED MAIN CABIN DOOR IAW EMB145 AMM 53-21-02 OPS CHECK GOOD

Part: PANEL — DAMAGED (PAX DOOR) · airframe 39,180 hrs · 34,660 cycles

THE MAIN PASSENGER DOOR PANEL WITH THE EMERGENCY LIGHT IS DAMAGED. C/A: R & R THE MAIN DOOR EMERGENCY LIGHT PANEL, IAW EMB145 AMM 25-23-04. OPERATIONS CHECK OF EMERGENCY LIGHT GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 38,585 hrs · 34,033 cycles

MAIN CABIN DOOR RED HANDLE DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBRICATED MAIN DOOR STOPS, ROLLERS, AND ASSOCIATED GUIDES AS NECESSARY, MAIN CABIN DOOR OPENS AND CLOSES AND LATCHES SMOOTHLY AND SECURELY IAW AMM 52-18-00

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 38,356 hrs · 33,804 cycles

SUPPLEMENTAL CLIMBING THROUGH FL280 CABIN ALT WAS AT 8900. SHORTLY WENT INTO THE RED RANGE AND POST A CABIN ALT OF 10000 FT. DESCENDED AND CABIN PRESSURE APPEARED TO RETURN TO NORMAL. DEFERRED PRESSURIZATION SYSTEM AUTOMATIC AND MANUAL MODE. M PROCEDURES C/W AUTH 020281DM-C REF 21-19. REACTIVATED SYSTEM IAW AMM 21-31-03-440-801-A. REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE OPS CHECK GOOD IAW AMM 21-31-00 MEL RESTORED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 38,356 hrs · 33,803 cycles

CLIMBING THROUGH FL230, AMBER CABIN ALT READ 8800 AND QUICKLY CLIMBERD TO 10,700 WITH RED AND AURAL WARNING. DESCENDED TO 10,000 FT, RAN QRH, AND MANUAL PRESS STABILIZED CABIN ALT FOR DURATION OF FLT-C/A-REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB-145 AMM 21-31-01. OPS CHECK GOOD

Part: SENSOR — OUT OF ADJUST (MLG WOW) · airframe 37,444 hrs · 32,910 cycles

LG AIR/GND FAIL MSG ON EICAS SHORTLY AFTER TAKE OFF-C/A-FOUND CMC MSG FOR RH & LH MLG WOW SWITCH FAIL, FOUND FWD AND AFT WOW SWITCH GAP OUT OF MAXIMUM LIMIT AT THE LH LG AND ADJUSTED BOTH TO THE MINIMUM GAP IAW EMB145 AMM 32-63-05. PERFORMED OHM AND INSULATION TEST OF HARNESS BETWEEN RH & LH MLG WOW CONNECTORS FOR #1 & #2 SWITCHES AND THE CONNECTORS AT THE LGEU P1763 & P1764 IAW WM 32-61-50 AND SWPM 20-20-03, OPC GOOD NO DEFECTS NOTED. PERFORMED FUNCTIONAL TEST OF THE RH AND LH WOW PROX SWITCHES IAW ETN-EM-32-245, OPC GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 37,390 hrs · 32,861 cycles

FLAP FAIL DURING APPROACH IN FLAP 45 POSITION-C/A-FOLLOWED FIM TASK 27-51-00-810-804-A STEPS 1&2. FAULT REMAINS, FURTHER TROUBLESHOOTING REQUIRED. PERFORMED TROUBLESHOOTING FLAP FAIL REF FIM 27-51-00-810-804-A BLOCK 1. OPS CHECK OF FLAP CONTROL SYSTEM REF EMB 145 AMM 27-51-00-700-801-A. OPS CHECK GOOD. NO EICAS MSG RELATED. A/C OK TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 37,259 hrs · 32,740 cycles

DURING PS-1 CHECK FOUND EMERGENCY FLOOR PROXIMITY STRIP BETWEEN ROW 8 AND 9 INOP.-C/A-DEFFERRED PER MEL 33-30. AUTH # 100811-C. REMOVED LIGHT STRIP IAW AMM 33-50-12. RESEATED PIN ON QUICK DISCONNECT 9102 IAW SWPM 20-50-01. REINSTALLED LIGHT STRIP IAW 33-50-12. OPC GOOD. MEL ITEM RESTORED

Part: OXYGEN GEN — FAILED (PAX CABIN) · airframe 37,248 hrs · 32,732 cycles

SUPPLEMENTAL PAX O2 MASKS DROPPED-C/A-INSPECTED ALL PASSENDGER O2 MASKS AND RESTOWED MASKS IAW AMM 35-20-04. REMOVED AND REPLACED PASSENGER O2 GENERATORS 1A, 6A, 5A, 8A, 9A, 14A, 13A, 11A, 7A, 17A, 16A, 10A, 15A, 4BC, 5BC, 6BC, 7BC, 8BC, 9BC, 10BC, 11BC, 18BC, 13BC, 12BC, 17BC, 15BC, 16BC, 14BC, IAW EMB 145 AMM 35-20-01. OXYGEN GENERATOR P/N 803000-21 S/N A16110338 (6A); A16110301 (5A); A16110297 (8A); A16110255 (9A); A16110333 (14A); A16110346 (7A); A16110324 (11A); A16110300 (13A); A16110265 (15A); A16110336 (10A); A16110249 (16A); A16110305 (17A); P/N 803000-23 S/N A17021522 (6BC); A17021531 (4BC); A17021520 (7BC); A17021519 (8BC); A17021769 (5BC); A17021514 (9BC); A17021518 (10BC); A17021533 (11BC); A17021521 (18BC); A17021756 (17BC); A17021535 (12BC); A17021523 (13BC); A17021532 (14BC); A17021537 (16BC); A17021516 (15BC)

Part: VALVE — FAILED (LT A/C PACK) · airframe 37,197 hrs · 32,687 cycles

PACK 1 VALVE FAIL-C/A-FLT CREW PLACARD PACK 1 IAW MEL 21-30 AUTH # 100481D-C MOC # 624980. REMOVED AND REPLACED RELAY K0187 IAW EMB AMM 20-13-02-000-801-A AND 20-13-02-400-801-A PER KVA. NO FIX. FOUND PACK 1 OVERTEMP ON CMC. T/S PER FIM 21-51-00-810-823-A. FOUND PACK VALVE TO BE BAD. RAR PACK VALVE IAW EMB AMM 21-51-01-000-801-A AND 21-51-01-400-801-A. OPC LEAK CHECK GOOD AT THIS TIME. MEL RESTORED. END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,960 hrs · 32,495 cycles

SUPPLEMENTAL # 4 FLOOR EMERGENCY LIGHT STRIP INOP. C/A- DEFERRED PER MEL 33-30. REMOVED AND REPLACED #4 EMERG FLOOR STRIP IAW AMM 33-50-12 OPS CHECK GOOD MEL RESTORED.

Part: BRACKET — DAMAGED (COCKPIT) · airframe 36,896 hrs · 32,441 cycles

CRASH AXE BRACKET BEHIND FO SEAT HAS BUTTERFLY. NOT RECEIVING THREAD WORN OUT. UNABLE TO SECURE. SECURED CRASH AXE 1/4 TURN CAM-LOCK IAW STANDARD MAINT PRACTICE. CHECK GOOD

Part: FITTING — CRACKED (FRAME 19) · airframe 36,856 hrs · 32,399 cycles

DURING HMBV INSPECTION, QC FOUND THE MACHINED FITTING CRACKED AT FR 19 STGR 3L. REMOVED AND REPLACED MACHINED FITTING AT FR 19 STGR 3L IAW SRM 51-40-02.

Part: STRINGER SPLICE — CRACKED (FR 14) · airframe 36,856 hrs · 32,399 cycles

DURING HMBV INSPECTION, QC FOUND STGR 6R SPLICE CRACKED AT FR 14. REMOVED AND REPLACED STGR 6R SPLICE AT FR 14 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 65 - 68) · airframe 36,856 hrs · 32,399 cycles

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

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 36,856 hrs · 32,399 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR INBD L ANGLE NUT PLATE HOLES HAVE CORROSION (4EA) -C/A-REMOVED AND REPLACED CARGO DOOR LOWER INBD L ANGLE IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 36,856 hrs · 32,399 cycles

DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT LOWER SHEAR CLIP AT FR 65 CORRODED-C/A-PERFORMED PERMANENT REPAIR ON CARGO CUTOUT LOWER SHEAR CLIP IAW EMB 145 SRM 53-31-04. REPAIR MATERIAL; SHEAR CLIP P/N 145-25175-001.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 36,856 hrs · 32,399 cycles

DURING HMBV INSPECTION, QA FOUND FR 68 SHEAR CLIP CORRODED AT LOWER AFT CORNER OF THE CARGO DOOR CUTOUT-C/A-PERFORMED PERMANENT REPAIR ON FR 68 SHEAR CLIP AT LOWER AFT CORNER OF CARGO DOOR CUTOUT IAW EMB 145 SRM 53-31-04. REPAIR MATERIAL; SHEAR CLIP P/N 145-25369-603.

Part: WIRE — BROKEN (CABIN) · airframe 36,856 hrs · 32,399 cycles

2EA PROX LIGHT WITHOUT ARROWS, 1EA PROX LIGHT WITH ARROWS, AND 1EA OVERWING EXIT PROX LIGHT HAVE BROKEN WIRES. C/A-COMPLETE: REMOVED AND REPLACED 2EA PROX LIGHT WITHOUT ARROWS, 1EA PROX LIGHT WITH ARROWS, AND 1EA OVERWING EXIT PROX LIGHT IAW AMM 33-50-12 SEE NRTC BOW326791 FOR FINAL INSTALL AND OPS CHECKS.

Part: RECEPTACLE — DEFECTIVE (GALLEY) · airframe 36,738 hrs · 32,272 cycles

SUPLEMENTAL WHILE TAXING TO GATE IN DFW CREW NOTICED WARM ELECTRICAL BURNT ELECTRICAL SMELL IN COCKPIT AND AT FA STATION. C/A-UPON ARRIVAL NOTICED NO ABNORMAL SMELL THROUGHOUT ENTIRE CABIN, C/W FIM 25-31-00 810-810A & FIM 21-20-00 810-810A STEPS 1-6,8,14-18. FOUND EVIDENCE OF ARCING @ O/B HOT JUG RECEPTACLE. CONTINUITY WAS INCONSISTANT. DEFERRED IAW MEL 25-50. MTX C/W. REMOVED AND REPLACED OTBD HOT JUG RECEPT IAW CMM 25-32-48. OPC GOOD. MEL ITEM RESTORED.

Part: SIGN — UNSECURE (CABIN) · airframe 36,378 hrs · 31,966 cycles

ILLUMINATED EMERGENCY EXIT SIGN FELL ( OVER ROW 12 ). C/A-REMOVED AND REPLACED EXIT LOCATING SIGN IAW AMM 33-50-15. OPS CHECK GOOD.

Part: RELAY — FAILED (SMOKE WARNING) · airframe 36,367 hrs · 31,952 cycles

DURING APU/BAGGAGE FIRE AND SMOKE TEST CARGO LIGHT FAILED TO ILLUMINATE. C/A-REFER WORK PERFORMED ON TURNOVER THIS NRWC. RAR RELAY K0438 IAW SWPM 20-13-03. DID NOT FIX. RAR RELAY K0625 IAW SWPM 20-13-03. DID NOT FIX. RAR RELAY K0630 IAW SWPM 20-13-03. OPS CHECK GOOD IAW AMM 26-10-00. SLEEVE P/N D-103-31; SPLICE BUTT P/N D436-37; RELAY P/N M83536/6-022M; RELAY 4 PDT P/N M83536/31-6002P.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 35,980 hrs · 31,601 cycles

REF ITEM1 CREW REPORTED HEAT LIKE ELECTRICAL SMELL. C/A-PERFORMED INSPECTION OF LT AND RT RELAY PANELS NO SMELLS NOTED IAW AMM 20-13-03. INSPECTED FLASHLIGHTS NO SMELL AND NO SMELLS FROM DISPLAYS NO DEFECTS NOTED RAN BOTH PACKS NO SMELLS NOTED INSPECTED FWD AVIONICS BAY FOUND RECIRC FAN INOP. DEFERRED AED REF MEL 25-57AUTH 030304-A. FOUND AED MISSING REPLACED AED IAW EMB-GN-25-074 NO FURTHER DISCREPANCIES NOTED MEL ITEM RESTORED. PERFORMED ICE DETECTOR OPS CHECK IAW AMM 30-80-00 OPS CHECK GOOD NO MESSAGES NOTED. PERFORMED W/S HEAT OPS CHECK IAW AMM 30-42-00 OPS CHECK GOOD NO MESSAGES NOTED.

Part: LIGHT — DAMAGED (EXTERIOR) · airframe 35,762 hrs · 31,380 cycles

RT FUSELAGE EMERGENCY LIGHT DAMAGED. C/A-REMOVED AND REPLACED RT FUSELAGE EMERGENCY LIGHT ASSY. REF. AMM 33-50-10. OPS CHECK GOOD.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 35,288 hrs · 30,861 cycles

BAGGAGE SMOKE WARNING LIGHT WILL NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED RELAY KO629 IAW AMM 20-13-02. OPS CHECK FAILED. REMOVED AND REPLACE FIRE PANEL IAW MM 26-00-01. OPS CK OK.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 35,071 hrs · 30,711 cycles

SERVICED DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-000-801-A. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,982 hrs · 30,623 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-09-000-801 AND 33-50-09-400-801 OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (NOSE) · airframe 34,347 hrs · 30,042 cycles

AFTER TAKEOFF, A LOUD BANGING SOUND WAS HEARD AND FELT ON THE LEFT FORWARD SIDE OF THE NOSE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. NORMAL LANDING. INSPECTED IAW 51-10-02, NO AREAS OF DAMAGE FOUND, THE DOOR OPERATED NORMAL.

Part: SMOKE DETECTOR — NO TEST (AFT CARGO) · airframe 34,288 hrs · 29,992 cycles

CARGO FIRE LIGHT INDICATOR NOT WORKING. DOES NOT TEST. REMOVED & REPLACED THE AFT CARGO AFT SMOKE DETECTOR IAW 26-15-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,283 hrs · 29,986 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-000-801-A. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (TE FLAPS) · airframe 33,997 hrs · 29,695 cycles

FLAPS FAILED AT 45 WHEN SELECTED TO 45 DURING APPROACH. PERFORMED FIM 27-51-00-810-804-A, FOUND TO BE TRANSITORY CONDITION. PERFORMED AN OPS CHECK OF FLAP SYSTEM IAW AMM 27-51-00 OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 33,703 hrs · 29,411 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. CLEANED AND LUBED THE MAIN DOOR ROLLERS AND CATCHES IAW AMM 52-21-02. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,213 hrs · 28,989 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (SPOILER SYS) · airframe 32,898 hrs · 28,634 cycles

AT 14000 FT MSL SPOILER FAIL EICAS MESSAGE AND OPEN SPOILER INDICATION. FA REPORTED NO PANELS DEPLOYED & AIRCRAFT DID NOT FEEL AS IF THEY WERE DEPLOYED MESSAGE WENT AWAY AT 300' MSL. TROUBLESHOT CMC MESSASGE OTBD SPOILER FAIL IAW FIM 27-63-00-810-807-A. FOUND THE RT OTBD PROXIMITY SENSOR TO BE BAD. REMOVED AND REPLACED THE RT OTBD PROXIMITY SENSOR IAW AMM 27-63-04. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: ROLLER — BINDING (PAX DOOR) · airframe 32,831 hrs · 28,568 cycles

FA REPORTED THE MAIN DOOR VERY HARD TO OPERATE. PERFORMED MAIN DOOR FRAME ROLLERS SERVICE IAW AMM 53-21-02. OPS CHECKED GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,754 hrs · 28,505 cycles

AFT EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY CEILING LIGHT LAMP. OPS CHECKED GOOD IAW AMM 33-50-08.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,340 hrs · 28,132 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE IAW PS-1 INSPECTION. R & R THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,219 hrs · 28,025 cycles

SERVICE DOOR EXTERNAL 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: STRUCTURE — CORRODED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

EXTERNAL SIDE OF LAV BUCKET CORRODED AT DRAIN VALVE AFT UPPER CORNER. REMOVED AND INSTALLED NEW SERVICEABLE LAV BUCKET IAW SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

STRINGER 2L CRACKED AT FASTENER HOLE AFT OF FR 75. REPAIRED STRINGER 2L CRACK AT FASTENER HOLE AT FR75 IAW ERS-EM-53MR-2683.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

FRAME 73 CRACKED AT STRINGER 16R-17R. REPAIRED FR 73 AT STRINGER 16R-17R IAW SRM 53-31-04.

Part: PROFILE — CORRODED (SERVICE DOOR) · airframe 32,028 hrs · 27,854 cycles

SERVICE DOOR CORRODED AROUND LOWER NUTPLATE HOLES. REPAIRED SERVICE DOOR LOWER PROFILE IAW ERS-EM-52MR-739.

Part: FRAME — CHAFED (SERVICE DOOR) · airframe 32,028 hrs · 27,854 cycles

SERVICE DOOR FWD FRAME WEB PAINT DAMAGED BTW NR 3 AND NR 5 STOP. REPAIRED SERVICE DOOR FWD FRAME WEB CHAFE BTW NR 3 AND NR 5 STOP IAW ERS-EM-52MR-738.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

LT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 AFT OF FRAME ABOVE 2L AND FIRST FASTENER BELOW STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 IAW SRM 53-31-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

RT REAR FUSELAGE I SKIN CRACK AT FRAME 75, AND STRINGER 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 AND STR 2R IAW SRM 53-31-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

LT UPPER FUSELAGE SKIN CRACKED IN 2 PLACES, CRACK 1 IS JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX 1/2" LONG, CRACK 2 IS AT THE FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, ALL CRACK ENDS ARE MARKED. REPAIRED LT FUSELAGE CRACK JUST AFT FR 75 ABOVE STR 2L IAW SRM 53-31-01 ITEM 11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,028 hrs · 27,854 cycles

RT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK IS APPROX 1/4" LONG. REPAIRED CRACK ON RT SIDE OF FUSELAGE AFT OF FR75 ABOVE STR 2R IAW SRM 53-31-01 ITEM 11.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 27,473 hrs · 23,274 cycles

LT AND RT OVERWING LIGHTS INOPERATIVE. R & R FUSE ON THE BATTERY POWER SUPPLY. OPS CHECK GOOD

Part: SKIN — DENTED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

DENT APPROXIMATELY 4 INCHES LONG, ON FUSELAGE APPROX 1 FOOT AFT OF THE SERVICE DOOR AT FRAME 22R & STRINGER 11R. REPAIRED DENT WITH DOUBLER REPAIR IAW SRM 51-21-01 FIG 202 & SRM 53-21-01.

Part: BRACKET — CRACKED (ACCESS DOOR) · airframe 27,470 hrs · 23,272 cycles

CRACK AROUND RIVET SECURING THE PIP PIN BRACKET IN PLACE ON THE ACCESS DOOR 272DR. REPAIRED IAW ERS-EM-52MR-281.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

FRAME CLIP CRACKED .5 INCHES AT FRAME 80 BETWEEN STRINGERS 6L - 7L. R & R CRACKED FRAME CLIP WITH NEW IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,473 hrs · 23,274 cycles

CARGO DOOR CUP SUPPORT AT FRAME 68 IS CRACKED AT THE LOWER LOCK FASTENER. CRACK IS .25 INCHES LONG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

RIGHT OMEGA BEAM INBD ATTACH ANGLE CRACKED BETWEEN FRAMES 47 & 48. REPAIRED RT OMEGA BEAM INBD ATTACH ANGLE BETWEEN FRAMES 47 & 48. BRACKET PN 140-04214-609 IAW SRM 53-23-02.

Part: SUPPORT — CRACKED (LT PYLON) · airframe 27,470 hrs · 23,272 cycles

LEFT PYLON PRE-COOLER FWD BRACKET SUPPORT ASSEMBLY IS CRACKED. R & R LT PYLON PRE-COOLER FWD BRACKET SUPPORT ASSEMBLY IAW SRM 51-40-02 & ETN EM-54-056.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,470 hrs · 23,272 cycles

RIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 1/2" ON THE PREVIOUS REPAIR OF THE LE. RT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1" ON THE PREVIOUS REPAIR OF THE TE. INSTALLED NEW ANGLES IAW ETN-EM-53?142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

LEFT HAND OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 2 INCHES ON PREVIOUS REPAIR OF THE LE. LEFT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 INCH ON THE PREVIOUS REPAIR OF THE TE. REPAIRED LT LOWER OVERWING TO FUSELAGE LOWER ANGLE NR 1 IAW ETN-EM-53-142. REF E433596 FOR LEAK CHECK.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

LEFT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IS CRACKED 3/8 INCH ON THE TE. COMPLIED WITH REPAIR OF LT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IAW ETN-EM-53-142.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 27,470 hrs · 23,272 cycles

PASSENGER DOOR BRACKET THAT INNER HANDLE TORQUE BOX MOUNTS TO HAS TWO 1/4 INCH CRACKS IN THE AFT UPPER CORNER. REPAIRED PAX DOOR BRACKET THAT INNER HANDLE TORQUE BOX MOUNT TO IAW EO-EM-52MR-250.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,470 hrs · 23,272 cycles

RIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IS CRACKED 3/8 INCHES ON THE FWD EDGE & 2 1/2 INCHES ON THE TE. R & R RT OVERWING LOWER ANGLE NR 2 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

RIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 1/2" ON THE PREVIOUS REPAIR OF THE LE. INSTALLED NEW ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,470 hrs · 23,272 cycles

RIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 3 IS CRACKED COMPLETELY IN HALF. BRACKET IS APPROX 5 INCHES LONG. R & R RT OVERWING LOWER ANGLE NR 3 IAW ETN-EM-53-142R2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

FRAME CLIP 68 IS CRACKED BETWEEN STRINGER 6L & 7L. CRACK IS 1 INCH IN LENGTH. R & R SHEAR CLIP IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

LEFT OVERWING TO FUSELAGE LOWER ANGLE NR 1 IS CRACKED 2 INCHES ON THE PREVIOUS REPAIR OF THE LE. REPAIRED IAW ETN-EM-53-142. REF E433596 FOR LEAK CHECK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

LEFT OVERWING TO FUSELAGE LOWER ANGLE NR 1 IS CRACKED 1 INCH ON THE PREVIOUS REPAIR OF THE TE. REPAIRED IAW ETN-EM-53-142. REF E433596 FOR LEAK CHECK.

Part: HINGE — CRACKED (TE FLAP) · airframe 27,470 hrs · 23,272 cycles

LEFT WING OTBD FLAP SHROUD HINGE IS CRACKED. R & R LT WING OTBD FLAP SHROUD HINGE IAW AMM 57-56-01 & SRM 51-40-02.

Part: RIVET — LOOSE (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

LEFT OVERWING TO FUSELAGE UPPER ANGLE ATTACHMENT BRACKET HAS ALL 4 RIVETS LOOSE BETWEEN FRAMES 48 - 49. R & R LOOSE RIVETS IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,470 hrs · 23,272 cycles

FOUND THE FLOOR EMER LIGHT INOPERATIVE AT THE LAVATORY DOOR. R & R FLOOR EMER LIGHT STRIP BY LAVATORY DOOR IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 27,470 hrs · 23,272 cycles

FLOOR PROXIMITY LIGHT STRIP NR 7 HAS A BROKEN WIRE. REPLACED SP9113 & SP9114 ON FLOOR PROXIMITY LIGHT STRIP NR 7 IAW SWPM 20-21-00. SEE BOW178339 FOR OPERATIONS CHECK.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 27,470 hrs · 23,272 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. SHOWS CHARGING BUT FLASHLIGHT ITSELF DOESN'T WORK. R & R RECHARGEABLE BATTERY PACK IN FLASHLIGHT IAW CMM 25-60-11. FLASHLIGHT ILLUMINATES.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

FRAME CLIP 65 IS CRACKED BETWEEN STRINGERS 7L & 8L. CRACK IS 1.5 INCHES IN LENGTH. FABRICATED & INSTALLED SHEAR CLIP AT FRAME 65 IAW ERS EM-5300-1070 & SRM 51-40-02.

Part: BRACKET — CRACKED (ACCESS DOOR) · airframe 27,470 hrs · 23,272 cycles

CRACK AROUND RIVET SECURING THE PIP PIN BRACKET IN PLACE ON ACCESS DOOR 272DR. REPAIRED IAW ERS-EM-52MR-281.

Part: FITTING — WORN (LT AILERON) · airframe 27,470 hrs · 23,272 cycles

LEFT AILERON DAMPER FITTING, ON AILERON, HAS EXCESSIVE PLAY WITH HAT BUSHINGS. WEAR APPEARS ON FITTING & NOT HAT BUSHINGS. REF NRWC E433425 FOR R & R OF HAT BUSHINGS. REPLACED FITTING IAW EO EM-27MR-112.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

AFT BELLY FAIRING ATTACH ANGLE IS CRACKED, LOCATED FWD LT ATTACH POINT JUST INBD OF FLAP. REPAIRED AFT BELLY FAIRING ATTACH ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,470 hrs · 23,272 cycles

RIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 INCH ON THE PREVIOUS REPAIR OF THE TE. INSTALLED NEW ANGLE IAW ETN-EM-53-142.

Part: CONTROL UNIT — FAULTY (TE FLAP) · airframe 24,782 hrs · 20,967 cycles

FLAP LOW SPEED EIAC DURING APPROACH. R & R FECU IAW AMM 27-53-07, OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,637 hrs · 20,862 cycles

LEFT & RT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. R & R NR 4 EMERGENCY BATTERY CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-19.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 23,972 hrs · 20,325 cycles

F/O FLASHLIGHT HOLDER BROKEN. R & R F/O FLASHLIGHT HOLDER IAW AMM 33-50-16; OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,737 hrs · 20,163 cycles

NR 5 FLOOR EMERGENCY LIGHT NOT WORKING. R & R NR 5 EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 23,487 hrs · 19,934 cycles

DURING MBV INSPECTION, FOUND BAGGAGE DOOR SILL IS CORRODED BETWEEN FRAMES 65 & 66. R & R BAGGAGE DOOR SILL IAW SRM 51-40-02.

Part: FRAME — DAMAGED · airframe 23,487 hrs · 19,934 cycles

FRAME 27 HAS AN ELONGATED HOLE AT S15R FLOOR SUPPORT. REPAIRED FRAME 27 AT S15R IAW SRM 53-00-04.

Part: FRAME — DAMAGED · airframe 23,487 hrs · 19,934 cycles

FRAME 26 HAS AN ELONGATED HOLE AT S15R, REPAIRED FRAME 26 AT S15R IAW SRM 53-00-04.

Part: LUG — GOUGED (RT AILERON) · airframe 23,487 hrs · 19,934 cycles

DURING MBV INSPECTION FOUND RT AILERON PCA ATTACHMENT OTBD LUG IS GOUGED. R & R RT AILERON PCA FITTING IAW AMERICAN EAGLE EO EM-27MR-112.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,289 hrs · 19,767 cycles

THE F/A REPORTED THE FWD FLASHLIGHT WAS INOPERABLE. THE RED LED LIGHT DID NOT WORK. THE ACFT WAS REMOVED FROM SERVICE. R & R FLASHLIGHT REF AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 23,236 hrs · 19,726 cycles

DURING CLIMB AT 13,000 FT, RECEIVED A BAGGAGE SMOKE MESSAGE ON EICAS AND BAGGAGE EXTINGUISHER LIGHT ILLUMINATED. DEPLOYED EXTINGUISHER BOTTLE IAW EPC. BAGGAGE SMOKE WARNING WENT AWAY AND BAGGAGE EXT INOPERATIVE ON EICAS. NO SIGNS OF SMOKE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF BAGGAGE COMPARTMENT SMOKE DETECTOR, NO DAMAGE NOTED AND PERFORMED BAGGAGE FIRE EXT SYS OPC IAW AMM 26-23-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — BROKEN (CABIN) · airframe 22,847 hrs · 19,410 cycles

FLIGHT 3386. FLIGHT ATTENDANT REPORTED THE FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 22,547 hrs · 19,162 cycles

FLIGHT 4132, CREW REPORTED JUST AFTER VR, FUMES AND HAZE BECAME EVIDENT IN COCKPIT. BY APPROX. 500FT, FLIGHT ATTENDANT CHIMMED AND NOTIFIED CREW OF SMOKE IN CABIN. EICAS LAVATORY SMOKE WARNING ILLUMINATED. EMERGENCY PROCDURES PERFORMED PER AOM - 1. FLIGHT ATTENDANT INSPECTED FOR FIRE/SMOKE IN THE LAV & CARGO AREA. AN OVERWEIGHT LANDING WAS NOT MADE. THE JET HAD EXPERIENCED A DE-ICING/ANTI-ICING EVOLUTION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW 71-000-00. OPS & LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 22,538 hrs · 19,154 cycles

ON FLIGHT 4126 THE CREW REPORTED LAV SMOKE ON EICAS, RAN CHECKLIST, LIGHT ON AFTER FLIGHT ATTENDANT TEST. LIGHT OUT ABOUT 2 MIN LATE ON BASE FOR RETURN LANDING. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR CYCLE MACHINE AND HEAT EXCHANGER REF NRWC 685-ORD-01248. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,438 hrs · 19,078 cycles

DURING B INSPECTION FOUND THE LEFT & RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LAMPS IAW AMM 33-50-07. PART # 1317 AND 30-2510-3. NO FIX. REMOVED AND REPLACED THE NR 4 CHARGER ASSEMBLY AND BATTERY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECKS WERE GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 21,352 hrs · 18,206 cycles

ON FLIGHT 2990 THE CREW REPORTED SMOKE COMING FROM LOWER PEDESTAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DIGITAL CONTROLLER BURN OUT AND REPLACED IAW EMB 145 AMM 21-31-01. REMOVED AND REPLACED THE AUTO PRESS DIGITAL CONTROLLER IAW EMB 145 AMM# 21-31-01. RAN PACKS AND NO SMOKE OR SMELL NOTED IN THE COCKPIT AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,509 hrs · 17,498 cycles

DURING B INSPECTION, FOUND THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD PER AE WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — BROKEN (AFT FLASHLIGHT) · airframe 20,486 hrs · 17,479 cycles

ON FLIGHT 2910, THE FLIGHT ATTENDANT REPORTED THE AFT FLASH LIGHT SWITCH WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASH LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL LIGHT CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,083 hrs · 17,167 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT BULB IAW 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — LOOSE (CABIN) · airframe 20,048 hrs · 17,135 cycles

FLIGHT 4143, CREW REPORTED AFT FLASHLIGHT TO BE VERY LOOSE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 4,143 hrs · 17,135 cycles

FLIGHT 4143, CREW REPORTED CABIN FLOOR EMERGENCY LIGHT COMING OFF FLOOR. AIRCRAFT REMOVED FROM SERVICE. SECURED LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,774 hrs · 16,901 cycles

DURING B-INSPECTION FOUND BOTH AFT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY AND POWER SUPPLY IAW AMM 33-50-04, OPERTIONAL WAS CHECK GOOD. NO DEFECTS NOTED. THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,486 hrs · 16,687 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 1 AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB, THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 19,486 hrs · 16,687 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT EMERGENCY LIGHT IS INOPERABLE. THE AIRCAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY NR 4 IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,486 hrs · 16,687 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD WING/FUSELAGE LIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD WING FUSELAGE LIGHT ASSY IAW EMB AMM 33-50-10 2M2 AND 3L2 AND THE NR 1 BATTERY AND BATTERY CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,456 hrs · 16,662 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT SIDE FORWARD FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — CUT (CABIN) · airframe 19,420 hrs · 16,638 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AFT FLOOR EMERGENCY LIGHT STRIP WIRE CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED AFT FLOOR EMERGENCY LIGHT STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,420 hrs · 16,638 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE NR 3 EMERGENCY FLOOR LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY FLOOR LIGHT STRIP IN REF TO TASK #'S 33-50-12-000-801-A AND 33-50-12-400-801-A, NO OTHER DEFECTS NOTED AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,414 hrs · 16,633 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD WING/FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE BATTERY POWER CHARGER IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 18,987 hrs · 16,346 cycles

ON FLIGHT 3527 DURING DESCENT THE CREW REPORTED THAT A FAIL PRESENTED ON EICAS WHEN FLAP LEVER SET TO 9 DEGREES. THE FLAPS REMAINED AT 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PNS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB145 AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,948 hrs · 16,317 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM HAS SIDE CORROSION FRETTING AND CORROSION AROUND THE NUTPLATE BETWEEN FRAMES 19-24. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM IAW SRM 53-21-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 18,948 hrs · 16,317 cycles

DURING MAINTENANCE INSPECTION FOUND CARGO DOOR SILL WITH SEVERAL SPOTS OF CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,437 hrs · 15,932 cycles

RT FWD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT FWD FAIRING EXTERIOR EMERGENCY LIGHT BULB IAW EMB 145 AMM 33050-10, OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 18,302 hrs · 14,843 cycles

ON FLIGHT 2804 THE CREW REPORTED THAT AFTER GATE ARRIVAL THE FIRST OFFICER OBSERVED SMOKE COMING OUT OF THE NR 1 ENGINE INTAKE AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE NR 1 RUNUP AND NO DEFECTS NOTED, NO SMOKE NOTED FROM INTAKE OR EXHAUST AREA IAW REMOVED AND REPLACED MM 72-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LANDING GEAR) · airframe 17,162 hrs · 14,986 cycles

ON FLIGHT 4067 THE CREW REPORTED THAT UPON TAKEOFF "LG AIR GROUND FAIL' APPEARED ON EICAS. THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO RIC. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH 32-63-02. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR NR 1 DOWNLOCK PROXIMITY SWITCH IAW AMM 32-61-02. THE OPERATIONAL CHECK WAS GOOD. EXTENSION RETRACTION CHECKS WERE GOOD IAW AMM 32-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,020 hrs · 14,870 cycles

A BAGGAGE TUG STRUCK THE AIRCRAFT ON RAMP WHICH RESULTED IN A HOLE AT THE CENTER FUSELAGE II BETWEEN FRAME 24 & 25 AND STRINGER 12L-13L. ALSO NOTICED A DENT BETWEEN JUNCTION 3 AND FRAME 24. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR TO CENTER FUSELAGE II LEFT HAND FUSELAGE SKIN IAW EO# EM-53MR-1762. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,840 hrs · 14,732 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR HINGING ARM EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR HINGING ARM EMERGENCY LIGHT. THE OPERATIONAL CHECK OF THE LIGHT ASSEMBLY WAS GOOD IAW EMBRAER 145 AMM 33-50-10. THE AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 20,088 hrs · 18,095 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY LIGHT PROXIMITY STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CONNECTOR IAW140 WM PART T 20-50-00. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,156 hrs · 14,215 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD EXIT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXIT EMERGENCY LIGHT IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,129 hrs · 14,190 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR OVERHEAD EMERGENCY LAMP IAW EMB145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,129 hrs · 14,190 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR EMERGENCY LIGHT ON THE DOOR FRAME TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09-00-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPRING — DEFECTIVE (COCKPIT) · airframe 16,083 hrs · 14,159 cycles

FOR FLIGHT 4340 DURING TAXI THE CREW REPORTED THE CAPTAIN’S LEFT BRAKE PEDAL BOTTOMED OUT WITH NO RESISTANCE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S LEFT BRAKE FEEL SPRING, EMB 145 AMM 27-21-03. THE BRAKES CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,446 hrs · 12,795 cycles

ON FLIGHT 4182 THE CREW REPORTED A STRONG BURNING ODOR ON THE TAKEOFF ROLL AT 80-90 KNOTS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER ETN EM-72-034 R4, AND COULD NOT DUPLICATE THE ODOR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INOPERATIVE (CABIN) · airframe 14,393 hrs · 12,754 cycles

DURING THE PREFLIGHT INSPECTION FOR FLIGHT 3817 DURING THE FLIGHT CONTROL CHECK, FOUND THAT THE ELEVATOR APPEARED TO BE BINDING DURING MID-TRAVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE STICK PUSHER ACTUATOR IAW AMM 27-36-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,362 hrs · 12,727 cycles

DURING A PS-2 INSPECTION FOUND THE AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB PER EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,118 hrs · 12,529 cycles

DURING MAINTENANCE BASE HEAVY CHECK FOUND THE CARGO DOOR SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMBRAER SRM 51-40-02. THE CORROSION IS NOT A LEVEL 2, BUT WAS DENOTED AS A MAJOR REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 9,563 hrs · 8,588 cycles

DURING A IMBV INSPECTION, THE CARGO DOOR CUT OUT CENTER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED CENTER SILL. OBTAINED NEW SILL, POSITIONED AND DRILLED FOR FASTENERS. CLEANED, ALODINED AND PRIMED FASTENER HOLES AND INSTALLED IAW EMBRAER SRM (SRM 145-1142 REV 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: TRIM SYSTEM — INOPERATIVE (MAIN PITCH) · airframe 8,264 hrs · 7,571 cycles

AIRCRAFT RETURNED TO FIELD FOR MAIN PITCH TRIM INOP. RESET SYSTEM AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (ZONE 100) · airframe 6,724 hrs · 6,309 cycles

MAIN PITCH TRIM FAILURE WARNING MESSAGE DURING CLIMB, RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB AMM 27-40-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: PRINTER — OVERHEATED (COCKPIT)

ORD - FLT 4378 - ELECTRICAL SMOKE AND HAZE IN COCKPIT. ELECTRICAL SMOKE HAZE FOUND TO BE OVERHEATED ACARS PRINTER. REMOVED AND REPLACED ACARS PRINTER, IAW EMB AMM 23-22-03. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM)

ORD - FLT 4228 - ON LANDING ROLL OUT, BRAKES GRABBED AND THEN HAD POOR BRAKING ABILITY. REPLACED BRAKE CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)