N932AE

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

LEFT SUPPORT CORRODED AT BTW FR 60-65. R & R THE SUPPORT IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

STALL WARNING COMPUTER SUPPORT BRACKETS CRACKED. R & R SUPPORT BRACKETS IAW SRM 51-40-02

Part: SPAR — CRACKED (ZONE 300) · airframe 45,809 hrs · 41,328 cycles

BTM OF VRT STA, AFT OF REAR SPAR 3, LWR LH PROFILE CRACKED IN 2 PLACES. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

RIGHT SHEAR TIE CRACKED AT FR 80 BTW S3-5R. R & R SHEAR TIE IAW SRM 51-40-02

Part: PROFILE — CRACKED (ZONE 300) · airframe 45,809 hrs · 41,328 cycles

BOTTOM OF VERTICAL STAB, AFT OF REAR SPAR 3, RT PROFILE CRACKED AT LWR END. REPAIRED IAW ETD 2026-145-934573 AND EO1-55-26-0011

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

FRAME DOUBLER CORRODED AT FR 61 LT. PERFORMED CUTOUT, FABRICATED & REINSTALLED REPAIR DOUBLER IAW SRM 53-31-04.

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

DOUBLER CORRODED BTW FR60-61, BTW LH SILL AND LH DOUBLER. R & R DOUBLER IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

CENTER GUSSET CORRODED AT BTW FR 59-61. R & R THE GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

SHEAR TIE CRACKED AT FR 61, S18-20R. THE SHEAR TIE REMOVED AND INSTALLED IAW SRM 51-40-02, FABRICATED NEW SHEAR TIE IAW ETD2026-415-00784, AND EO1-53-26-0033.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

FR61 FLOOR LEVEL, FRAME DOUBLER CORRODED. REPAIRED IAW SRM 53-31-04.

Part: FIREWALL — CRACKED (APU BAY) · airframe 45,809 hrs · 41,328 cycles

APU FIREWALL CRACKED. REPAIRED IAW SRM 53-32-13 FIG 205

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

ANGLE CRACKED AT FR10 STR 9L. R & R ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FRM 34. REPAIRED IAW ETD2026-145-934095 AND EO1-53-26-0003.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

SHEAR CLIP CRACKED AT FR10 STR 9L. R & R SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (APU FIREWALL) · airframe 45,809 hrs · 41,328 cycles

APU FIREWALL, THREE CRACKED ANGLES. R & R ANGLES IAW SRM M51-40-02.

Part: SHIELD — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

CORROSION UNDERNEATH LT THRUST REVERSER OTBD PYLON FIRESHIELD. REPAIRED IAW EO1-78-26-0009 ANS SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FRM 33. REPAIRED IAW ETD 2026-145-934095 AND EO1-53-26-0003.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

53-2131 RH OMEGA BEAM OB ANGLE CRACKED AT BTW FR48-50. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM OTBD ANGLE CRACKED AT BTW FR47-50. R & R ANGLE IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

CARGO DOOR LIFTING MECHANISM SUPPORT CRACKED AT BTW FR61-62 BTW STR4-5R. RAR SUPPORT IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

CARGO DOOR LIFTING MECHANISM UPPER SUPPORT CRACKED AT BTW FR 67-68 STR4R. RAR SUPPORT IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

SHEAR TIE CRACKED AT FR 58 BTW S15-16L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

STRINGER 21R CORRODED AT BTW FR 50-53. R & R THE STRINGER BETWEEN FRMS 50-53 IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM CRACKED AT FR36. REPAIRED IAW ETD 2025-145-934098 AND EO1-53-26-0001.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

CARGO DOOR LIFTING MECHANISM SUPPORT ANGLE CRACKED AT FR 62 BTW S4 - 5R. R & R THE SUPPORT ANGLE IAW SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

RIGHT OVERWING PANEL 194ER, NR 1 LWR ANGLE CRACKED, YA-1085, RIB1A. REMOVED, FARICATED, AND INSTALLED A NEW ANGLE IAW SRM 57-20-01RE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

53-2132 RH OMEGA BEAM IB ANGLE CRACKED AT BTW FR48-50. R & R ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

SHEAR CLIP CORRODED AT FR 52 BTW STR 20-21R. R & R SHEAR CLIP IAW SRM51-40-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

SHEAR TIE CORRODED AT FR51 BTW S20 - 21R. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE IAW ETD2026-145-000952.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD ANGLE CRACKED AT BTW FR47-50. R & R ANGLE IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,809 hrs · 41,328 cycles

RIGHT SILL CORRODED AT BTW FR 71-73. R & R SILL IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FR23. REPAIRED IAW ETD2025-145-93466 AND EO 1-53-26-0001.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,809 hrs · 41,328 cycles

SHEAR TIE CRACKED AT FR26 BTW S15-16L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AROUND RIVET AT FR 21. REPAIRED IAW ETD2025-145-934066 AND EO1-53-26-0001.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 45,809 hrs · 41,328 cycles

LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AROUND RIVET HEAD AT FR22. REPAIRED IAW ETD 2025-145-934066 AND EO1-53-26-0001.

Part: UNKNOWN — FUMES (ZONE 200) · airframe 44,966 hrs · 40,293 cycles

SMELLED POSSIBLE FUEL FUMES IN CLOCKPIT DURING APU START FACT 15JUN25 18:20 CLT STARTED APU AT GATE NO FUEL SMELL IN FLIGHT DECK OR CABIN. OK FOR SERVICE

Part: CONTACTOR — LOOSE (ZONE 200) · airframe 44,822 hrs · 40,118 cycles

WHILE DEPLANING SMELLED FUMES IN FLIGHT DECK DETECTED SMOKE AT L/H DISTROBUTION BOX BEHIND CAPTAIN SEAT. REMOVED EBC1 IAW AMM 24-60-03.(842286) R&R'D #100 EBC1 CONTACTOR SUPPORT AS REQ.(231414) INSTALLED NEW EBC1 CONTACTIOR & ASSOCIATED INTERCONNECTION BAR IAW 24-60-03. COMPLETED OP CHECKS IAW AMM 24-65-00. NO DEFECTS NOTED AT THIS TIME

Part: CONTACTOR — OVERHEATED · airframe 43,838 hrs · 39,032 cycles

ODOR ON FLIGHT DECK ON DECENT, BECAMRE STRONGER WHEN APU SELCTED. INSPECTED AND FOUND ODOR TO BE OF A BURNT ELECTRICAL SMELL, VISUALLY INSPECTED LH DISTRIBUTION BOX AND FOUND SEVERAL FUSES AND CONTACTORS K0001 AND K0189 SHOW SIGNS OF OVERHEATING. R&R'D FUSES IAW AMM 20-13-08 AND R&R'D RELAY/CONTACTOR IAW AMM 20-13-08. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,837 hrs · 39,029 cycles

OZONE SMELL ON DECENT IN CABIN AND FLIGHT DECK UPON TOUCHDOWN WITH APU BLEED SELECTED SMELL BECAME STRONG UPON GAT EARRIVAL WHEN DOOR OPEN SMELL PERSIST. FACT 16NOV24 11:00 RIC INSPECTED PACKS, FWD PRESSURIZED BAY, CONTACTORS, RELAY PANELS, RAN ENGINES + APU NO SMELL NOTED OK FOR SERVICE

Part: UNKNOWN — VIBRATION · airframe 42,946 hrs · 37,995 cycles

SUDDEN VIBRATION AND LOUD NOISE DURING CLIMB, DESCENT AND TURNS THAT LASTED APPROX 5 SECONDS WITH GEAR UP AND LOCKED. NOISE OBSERVED FROM NOSE OF A/C. FACT 31MAY24 05:47 PHL VISUALLY INSP'D NLG WHEEL WELL AVIONICS BAY, HELL HOLE, L/H & R/H WHEEL WELL AVIONICS BAYS & RADOME. NO DEFECTS NOTED. PERFORMED MULTIPLE GEAR SWINGS. NO ABNORMAL VIBRATIONS OR NOISE. NO DDEFECTS IN NLG DOORS R/R WORN NOSE WHEEL SPIN BLOCK IAW AMM 32-49-06. AC OK FOR SERVICE AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,946 hrs · 37,995 cycles

RH EMERGENCY EXIT DOOR IDENTIFIER SIGN IS OUT. RAR #5 INVERTER IAW AMM 33-50-11-400-801-A

Part: WIRE — FRAYED (EMERGENCY LIGHT) · airframe 42,420 hrs · 37,414 cycles

EMERGENCY FLOOR STRIP LIGHT WIRES ARE FRAYED AT ROW 8 TO9. R&R'D EMERGENCY FLOOR LIGHT ASSY AT ROW 8-9 IAW AMM33-50-12

Part: UNKNOWN — UNKNOWN (UNKNOWN)

NO.2 ENG SHUT DOWN INFLIGHT AND WOULD NOT RESTART. R/R #200 ENGINE IRT WORKCARD 71-00-00

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,512 hrs · 36,365 cycles

E975872 SSI 53-30-48, CARGO DOOR LOWER SILL FWD EDGE HAS LEVEL 2 CORROSION. : BLENDED CORROSION ON CARGO DOOR LOWER SILL FWD EDGE IAW EMB 145 SRM 51-10-03. HASN’T BEEN PREVIOUSLY BLENDED. REMAINING THICKNESS AT BLENDED AREAS ON CARGO DOOR LOWER SILL FWD EDGE FOUND TO BE BEYOND LIMITS IAW EMB145 SRM 53-31-15AD, ITEM 2. REMOVED CARGO DOOR LOWER SILL IAW EMB-145 SRM 51-40-02.INSTALLED SERVICEABLE CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,512 hrs · 36,365 cycles

E974821 LH UPPER FUSELAGE SKIN IS CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L. CRACK IS APPROX. 3/8” LONG. PERFORMED REPAIR AT L/H UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L IAW EMB 145 SRM 53-31-01 RE ITEM 11 FIG 219 SHEET 1 AND EO1-53-23-0149

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,512 hrs · 36,365 cycles

E974720 MAIN DOOR EXTERIOR SKIN IS GOUGED ON THE AFT LOWER CORNER, ON AND BELOW EXISTING DOUBLE. BLENDED GOUGE ON MAIN DOOR EXTERIOR SKIN ON AFT LOWER CORNER, ON AND BELOW EXISTING DOUBLER IAW EMB 145 SRM 51-10-03 FOUND TO BE ACCEPTED AS IS IAW ETD2023-145-012815 "REV A" AND PIEDMONT EO1-52-23-0136

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 41,070 hrs · 35,926 cycles

PASSENGER STOLE CABIN EMERGENCY FLASHLIGHT FROM ABOVE SEAT 18A. R & R AFT CABIN EMEREGENCY FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD.

Part: WIRE — BROKEN (MIC JACK) · airframe 41,023 hrs · 35,872 cycles

HIGH SPEED ABORTED TAKEOFF DUE TO HIGH PICH SQUEAL THROUGH BOTH HADSETS ON COM1 HAD TO ABORT TAKEOFF SQUEAL HAPPENED AROUND 80KTS ABORTED TAKEOFF BETWEEN 80-100 KTS NORMAL BRAKING APPLIED PLENTY OF RUNWAY LEFT. FOUND CPTN HAND MIC JACK TO HAVE BROKEN WIRE CONNECTION. REPAIRED CONNECTION IAW SWPM 20-30-00. OPC GOOD IAW 23-51-00

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 40,919 hrs · 35,764 cycles

FA EMERGENCY FLASHLIGHT HOLDER CLIP BROKE-C/A-RAR FLASHLIGHT HOLDER CLIP IAW CMM 25-60-14 OPS CHECK GOOD NO DEFECTS NOTED

Part: LAMP — INOPERATIVE (R16) · airframe 40,686 hrs · 35,505 cycles

ROW 16 CEILING EMERGENCY LIGHT INOP-C/A-RAR ROW 16 CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (SD) · airframe 40,686 hrs · 35,505 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: NONE — DAMAGED (RH) · airframe 40,474 hrs · 35,239 cycles

SUPPLEMENTAL CA FOR AT FLIGHT ADJUST ABOUT TO BEGIN DESCENT FOS OUTER PANE WINDSHELD SHATTERED DECLARED EMERGENCY."TRANSFERRED TO NRWC 932-DFW-05822"-C/A-CA PENDING. REMOVED F/O WINDSHIELD IAW EMB 145 AMM 56-10-01 UP TO STEP J/7.-C/A-REMOVED AND REPLACED FO'S COCKPIT WINDSHIELD IAW EMB 145 AMM 56-10-01. OPERATIONAL CHECK GOOD. TRANSFERRED TO AML PAGE 4735966 ITEM 1.

Part: NONE — NONE · airframe 39,980 hrs · 34,667 cycles

EMERGENCY FLASHLIGHT HOLDER AT FWD PARTION ABOVE FA SEAT ASSY. IS CRACKED-C/A-REPAIRED EMERGENCYFLASHLIGHT HOLDER BRACKET CLAMP IAW CMM 25-60-14

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 39,756 hrs · 34,425 cycles

MAIN CABIN DOOR WILL NOT CLOSE ALL THE WAY.-C/A-LUBRICATED MAIN PAX DOOR FRAME ROLLERS IAW EMB-145 AMM 53-21-02. FOUND SATISFACTORY AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 38,866 hrs · 33,413 cycles

FWD FA EMERGENCY FLASHLIGHT INOP-C/A-RAR FWD FA EMERGENCY FLASHLIGHT IAW EEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,684 hrs · 33,184 cycles

MAIN DOOR SHROUD EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR SHROUD EMERGENCY LIGHT LAMP IN REF TO AMM 33-50-10. OPC GOOD IN REF TO AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,915 hrs · 32,327 cycles

NUMBER 3 CEILING EMERGENCY LIGHT INOP. -C/A-R & R NR 3 CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD.

Part: AOA — FAILED (STALL WARNING) · airframe 37,784 hrs · 32,195 cycles

SPS-1 FAIL IN CLIMB 17,000-FL190 RAN QRH PROCEDURE, SPS 1-2 INOPERABLE MESSAGE. MECH SPS 1 FAILURE EMERGENCY DECLARED. CONTINUED TO ORD. C/A: R & R NR 1 AOA SENSOR, IAW EMB 145 AMM TASK 27-36-01. OPERATIONS CHECK GOOD.

Part: COMPUTER — FAILED (STICK PUSHER) · airframe 37,782 hrs · 32,192 cycles

SPS 1-2 INOPERABLE, STICK PUSHER FAIL, SPS ADVANCED MECHANICAL DECLARED EMERGENCY FLIGHT CONTINUED DTW. C/A: R & R SPC IAW AMM 27-36-02. OPERATIONS CHECK GOOD.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 37,655 hrs · 32,065 cycles

CARGO DOOR FWD LOWER EDGE CORNER HAS 1 NUTPLATE HOLE CORRODED. C/A: ACCOMPLISHED PERMANENT REPAIR ON CARGO DOOR FWD LOWER EDGE CORNER CORRODED NUTPLATE HOLE, IAW EMB 145 SRM 52-30-04.

Part: FRAME — DENTED (CARGO DOOR) · airframe 37,655 hrs · 32,065 cycles

CARGO DOOR LOWER OUTER FRAME DENT. C/A: R & R CARGO DOOR LOWER OUTER PROFILE, IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 64-68) · airframe 37,655 hrs · 32,065 cycles

SSI 53-30-48-CARGO DOOR CUTOUT STRUCTURE FLOOR SILL CORRODED. C/A: REMOVED AND REPLACED CARGO DOOR CUTOUT FLOOR SILL, IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 145-25480-603.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,655 hrs · 32,065 cycles

FLOOR PROX LIGHTS NR 1, 2 AND 3 ARE INOPERABLE. C/A COMPLETE: R & R NR 2 EMERGENCY BATTERY POWER SUPPLY, IAW EMB-145 AMM 33-50-04 AND ENVOY W/C 33-700-19, OPERATIONS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,655 hrs · 32,065 cycles

EMERGENCY LIGHT STRIP NR 3 IS DISCOLORED. C/A COMPLETE: R & R EMERGENCY LIGHT STRIP NR 3, IAW EMB 145 AMM 33-50-12. TRANSFERED OPC OF LIGHT STRIP NR 3 TO BOW349189.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 37,546 hrs · 31,948 cycles

MOST AFT EMERGENCY AISLE CEILING LIGHT INOPERABLE. C/A: INSTALLED NEW AISLE CEILING LIGHT, IAW EMB 145 AMM 33-60-08. OPERATIONAL CHECK IS GOOD.

Part: MUFFLER — DISCONNECTED (RECIRC FAN) · airframe 37,065 hrs · 31,494 cycles

FO FELT LOUD SLAMMING NOISE HEARD THRU CABIN, FA REPORTS SMOKE IN CABIN AND OVERHEATING ELEC SMELL, 2 MINS LATER GEN 3 FAIL, GEN2-3 OFF BUS AUTOPILOT FAIL. T/S PERFORMED PER TECH SUPPORT WORKSCOPE AND AML 4602372/2 FOR INSPECTION FINDINGS AND RESECURRING OF BLOWN DUCT. NO FURTHER DEFECTS OR SMOKE NOTED AT THIS TIME, A/C OK FOR SERVICE. PERFORMED CMC DOWNLOAD IAW CMC DOWNLOAD W/C 45-900-00. C/W FIM TASK 21-20-00-810-801-A AS PER WORK SCOPE. OPS CHECK GOOD FOR ALL GENERATORS IAW AMM 24-31-00. PERFORMED GVI OF LT & RT RELAY PANELS AS REQUESTED IN WORK SCOPE NO DEFECTS NOTED. C/W GVI OF LT & RT ELECTRICAL DISTRIBUTION BOXES NO DEFECTS NOTED. WHEN NR 1 PACK OPERATED, FOUND VAPOR IN CABIN FROM NR 1 RECIRC FAN MUFFLER BEING DISCONNECTED. RESECURED MUFFLER IAW AMM 21-20-03. NO LEAKS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,447 hrs · 30,947 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EMERGENCY LAMP IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME. END.

Part: SKIN — DAMAGED (LT NACELLE) · airframe 35,983 hrs · 30,499 cycles

LH COWL DMG FOUND DURG PRE FLIGHT.DAMAGE #1: LH LWR COWL 14.5" OTBD OF OIL SERV DOOR BOTTOM EDGE. PUNCTURE DUE TO BOLT ON CLAMP ON BLD TUBE BTWN ATS AND ATS VLV WITH CRACKS. CRACK L 1.5" WITH 2 LATERAL CRACKS OF 0.5" AND 0.25" FOR TOTAL W 0.75". PROTRUSION DEPTH H= 0.029". AT 6 O'CLOCK POSTION. REF NRWC 932-CMH-03929 FOR CLAMP REPOSITION.-C/A-DEFERRED PER ERS-EM-54DF-802 TDMI AUTHORIZATION NUMBER 932T5460. PERFORMED LH COWL SKIN WITH PUNCTURE AND CRACK RECURRING INSPECTION IAW ERS-EM-54DF-802 PTC TDMI REMAINS OPEN. PERFORMED LH LOWER COWLING SKIN WITH DENT AND SCRATCH RECURRING INSPECTION IAW ERS-EM-54DF-801 PTB TDMI REMAINS OPEN. C/W ERS-EM-54DF-802 PTB AS REQUIRED BY TDMI 932T5460. NO DEFECTS NOTED AT THIS TIME. C/W PERMANENT REPAIR IAW ERS# ERS-EM-54DF-802 PART D & C/W PERMANENT REPAIR IAW ERS# ERS-EM-54DF-801 PART C. TDMI ITEM RESTORED.

Part: A/C PACK — SEIZED (NR 2) · airframe 35,917 hrs · 30,455 cycles

ON DESCENT SMELLED ELECTRICAL BURNING SMELL NO SMOKE FA SMELLED ALSO IN CABIN-C/A-PAX ON AND OF ON LH ENGINE RH ENG APU COULD NOT DUPLICATE INSPECTED FWD AVIONICS BAY NO SMELL RECIRCULATION FAN ON NO SMELL ALL COCKPIT EQUIPMENT LIGHTS CBS NO SEMLL COULD NOT DUPLICATE. C/W FIM TASK 21-20-00-810-801-A. PERFORMED ETN-EM-72-034 UNABLE TO COMPLETE DUE TO PACK 2 OVERHEAT, NO OTHER DEFECTS NOTED. FOUND NR 2 PACK SEIZED. COMPLIED WITH EO EM-2100-048. COMPLIED WITH ETN-EM-72-034.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 35,670 hrs · 30,276 cycles

REJECTED TAKE-OFF AT 90 KNOTS DUE TO STRONG ELECTRICAL BURN SMELL IN THE FLIGHT DECK. C/A-FOUND FWD ELEC BAY LT RECIRC FAN INOP. REMOVED AND REPLACED FAN IAW AMM 21-26-02. OPS CK GOOD. PERFORMED ETN-EM-72-034. ODOR WAS NOTICEABLE AT STEP 8 AT MAX POWER SETTING. REMOVED AND REPLACED PACK 1 DUAL CONTROL VALVE IAW AMM 21-60-01. OPS CK GOOD. PERFORMED ETN-EM-72-034. NO NOTICEABLE SMELLS. ACFT OK FOR SERVICE. VALVE DUAL TORQUE MOTOR P/N C143123-6 S/N 97101304.

Part: ACM — FAILED (LEFT) · airframe 35,450 hrs · 30,082 cycles

DURING CRUISE, A BRIEF BURNING ODOR FOLLOWED BY REPORTS OF A BANGING SOUND FROM ROWS 8-9-10, AFTER LANDING, CABIN GOT VERY HOT, NO PRESSURIZATION ISSUES WERE NOTED. TROUBLESHOT IAW ETN-EM-72-034 AND EO-EM-2100-048. R & R THE NR 1 ACM IAW AMM-21-51-03. OPS AND LEAK CHECKED GOOD IAW AMM 21-51-00. REMOVED AND REPLACED HEAT EXCHANGER IAW AMM 21-51-02 OPS CHECKED IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD. ACFT GOOD FOR SERVICE.

Part: SPRING — DEFECTIVE (SERVICE PANEL) · airframe 34,917 hrs · 29,637 cycles

SUPPLEMENTAL GROUND SERVICE PANEL OPENED INFLIGHT. SPRING ON PANEL INOP AND DENT IN FUSELAGE. C/A-DEFFERED EXT POWER CONNECTION ACCESS DOOR AUTH# 050533CDL-D. INSTALLED NEW GROUND SERVICE PANEL IAW SRM 51-40-02. CDL ITEM RESTORED. REPAIRED SKIN GOUGE WITH SMALL HOLE BELOW GPU DOOR IAW SRM 53-12-01. PERFORMED INSPECTION TO VERIFY FABRICATED PART CONFORMS TO DESIGNED DATA, AND PART IS IN A CONDITION FOR SAFE OPERATIONS.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLAPS) · airframe 34,798 hrs · 29,510 cycles

TAKE-OFF CONFIG WARNING DISPLAYED ON EICAS AT APPROXIMATELY 90 KNOTS ABORTED TAKE-OFF. FLAPS WAS INDICATING GREEN DASH WHILE EXITING RUNWAY W/ HANDLE SELECTED TO 9.-C/A-RAR FECU IAW EMB-145 AMM 27-53-02. OPC FOUND SATISFACTORY AT THIS TIME. NO HIGH ENERGY STOP INSP REQUIRED AT THIS TIME IAW EMB-145 AMM 05-50-16.

Part: A/C PACK — OVERHEATED (AC BAY) · airframe 34,058 hrs · 28,894 cycles

PACK 1 OVERHEAT 3 TIMES WITH A SMELL. C/A-REMOVED AND REPLACED NR 1 PACK IAW AMM 21-51-03. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,216 hrs · 28,169 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY FLASHLIGHT AND FLASHLIGHT BATTERY IN REFERENCE WITH AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD. FLASHLIGHT BATTERY P/N P2-01-1003-001.

Part: SKIN — CANNING (FUSELAGE) · airframe 32,732 hrs · 27,719 cycles

RT CENTRAL FUSELAGE I LOWER SKIN DENTS PERMANENT REPAIR ERS-EM-53DF-2832 PTC. ERS-EM-53DF-2832 WAS NO LONGER REQUIRED DUE TO OIL CANNING. ACCOMPLISHED PERMANENT REPAIR IAW ERS-EM-53MR-3304.

Part: SKIN — SCRATCHED (PAX DOOR) · airframe 32,732 hrs · 27,719 cycles

PAX DOOR EXTERNAL SKIN HAD SEVERAL SCRATCHES ALONG THE TRAILING EGDE. INSTALLED A FILLER, DOUBLER AND EDGE SEALED THE REPAIR IAW SRM 52-10-01, FIG 204.

Part: FLOOR SUPPORT — CRACKED (FR 50) · airframe 32,732 hrs · 27,719 cycles

LEFT OMEGA BEAM SUPPORT WAS CRACKED ON THE AFT INBD SIDE AT FRAME 50. PERFORMED A REPAIR IAW SRM 53-23-02.

Part: BRACKET — CORRODED (WASTE VALVE) · airframe 32,732 hrs · 27,719 cycles

TOILET WASTE VALVE SUPPORT HAD MINOR CORROSION BENEATH LANYARD FOR FILL CAP. REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT IAW SRM 51-40-02.

Part: FRAME — CORRODED (FRM 22) · airframe 32,732 hrs · 27,719 cycles

FRAME 22 CORRODED AT PREVIOUS BLEND JUST BELOW THE SERVICE DOOR CUTOUT AFT LOWER DOOR STOP . ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-3311.

Part: STRINGER — CHAFED (FRAMES 20-21) · airframe 32,732 hrs · 27,719 cycles

STRINGER 2L WAS CHAFED BETWEEN FRAMES 20 AND 21. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-3312.

Part: LIGHT — CRACKED (CABIN) · airframe 32,732 hrs · 27,719 cycles

NR 7 FLOOR EMERGENCY LIGHT STRIP WAS CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 32,553 hrs · 27,527 cycles

DENT BETWEEN FR 05 AND FR 03 BETWEEN STRINGERS 3L AND 4L LENGTH 4.5", WIDTH 6.5"AND DEPTH .125". REPAIRED IAW ERS-EM-53MR-3256 PART A REF AML PAGE 4250380 ITEM 1.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,540 hrs · 27,513 cycles

LEFT AND RIGHT OVER WING EMERGENCY LIGHTS ARE OFF. REMOVED AND REPLACED THE NR 4 BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,416 hrs · 27,404 cycles

REAR CEILING EMERGENCY LIGHT INOPERATIVE. PERFORMED FIM 33-50-00. REMOVED AND REPLACED THE NR 4 INVERTOR IAW AMM 33-50-11. OPS CHECKED GOOD IAW AMM 33-50-00. NO FUTHER DEFECTS NOTED. INVERTOR P/N 7824-1

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,370 hrs · 27,371 cycles

FLASHLIGHT ABOVE FA JUMPSEAT NOT WORKING. REMOVED AND REPLACED FA FLASH LIGHT IAW AMM 33-50-16. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 31,830 hrs · 26,876 cycles

FOUND RT OVERWING EMERGENCY LIGHT TO BE INOP DURING PS-1 CHECK. R&R RT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07-04. OPS CHECK GOOD.

Part: FAN — ODOR (RECIRCULATION) · airframe 30,951 hrs · 26,120 cycles

BURNING ODOR ENCOUNTERED DURING DESCENT FOR ABOUT 30 SECONDS, BEGAN TO FADE AFTER RECIRCULATION BUTTON WAS RELEASED. INSPECTED COCKPIT RECIRCULATION FAN AND FOUND THE FAN TO HAVE AN ELECTRICAL ODOR. R & R THE COCKPIT RECIRCULATION FAN, OPS CHECKED GOOD IAW AMM 21-24-01.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,239 hrs · 25,441 cycles

CENTER AISLE CEILING EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REINSTALLED CENTER AFT CEILING EMERGENCY EXIT SIGN IAW AMM 33-50-15 AND 33-50-00 OPS CHECK GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 30,116 hrs · 25,327 cycles

AFT CEILING EMERGENCY EXIT SIGN INOPERATIVE. PERFORMED OPS CHECK ON AFT CEILING EMERGENCY EXIT SIGN IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 29,018 hrs · 24,269 cycles

MAIN FLIGHT DISPLAY DOES NOT DISPLAY WX RADAR IMAGE WITH WX SELECTED ON. RESET NR 1 MAIN FLIGHT DISPLAY. OPS CHECKED GOOD IAW MM 34-22-00

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,500 hrs · 23,811 cycles

GALLEY CEILING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-26-04. OPS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,196 hrs · 23,511 cycles

CARGO DOOR CTR SILL CORRODED AT FRAME 66. REPAIRED CARGO DOOR CTR SILL IAW SRM 51-40-02 & SRM 51-20-01.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 28,196 hrs · 23,511 cycles

SERVICE DOOR LOWER AFT CORNER DENTED. PERFORMED PERMANENT REPAIR ON SERVICE DOOR AFT CORNER IAW ERS-EM-52MR-531.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,196 hrs · 23,511 cycles

SIX EACH LIGHTNING STRIKES. REPAIR AT FRAME 10 - 12, STRINGER 20R - 21R. PERFORMED PERMANENT REPAIR OF SIX EACH LIGHTNING STRIKES IAW ERS-EM-53MR-2016.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,196 hrs · 23,511 cycles

POSSIBLE CRACK AROUND RIVET AT FRAME 78, BETWEEN STRINGER 6R - 7R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN IAW SRM 53-32-01 REPAIR TYPE B.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 28,196 hrs · 23,511 cycles

CARGO DOOR CUT OUT UPPER FRAME HAS CORROSION AFT OF FRAME 65. REPAIRED CARGO DOOR UPPER FRAME IAW SRM 51-14-02 & 51-10-03.

Part: DOOR — CORRODED (CARGO BAY) · airframe 28,196 hrs · 23,511 cycles

BAGGAGE DOOR CORROSION AROUND NUTPLATE HOLE, FWD LOWER. REPAIRED BAGGAGE DOOR CORROSION AROUND NUTPLATE HOLE IAW ERS-EM-52MR-513.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,196 hrs · 23,511 cycles

SERVICE DOOR ENTRANCE SILL CORRODED. REPAIRED SERVICE DOOR ENTRANCE SILL IAW SRM 53-21-02 ITEM 2 FIG 201.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 27,899 hrs · 23,236 cycles

AFT FLASHLIGHT BASE DAMAGED. R & R AFT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,741 hrs · 23,086 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16-000-801 & 33-50-16-400-801. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,090 hrs · 22,447 cycles

CABIN CEILING AT ROW 12, AFT EMER EXIT LIGHT INOPERATIVE. R & R CABIN CEILING AFT EMER EXIT, LOCATING LIGHT AT ROW 12. OPERATIONS CHECKED GOOD IAW AMM 33-50-15.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,310 hrs · 21,753 cycles

CAPTAIN FLASHLIGHT CRADLE BROKEN. R & R CRADLE IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,283 hrs · 21,730 cycles

AFT CABIN EMER CEILING LIGHT INOPERATIVE. R & R AFT CABIN EMER CEILING LIGHT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,278 hrs · 21,725 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR VERY HARD TO OPERATE. INSPECTED MAIN CABIN DOOR & FOUND UPPER FWD ROLLER VERY DRY. LUBRICATED ALL FOUR ROLLERS & COMPLIED WITH AN OPERATIONS CHECK IAW AMM 52-10-01. DOOR OPERATING NORMAL.

Part: CONTROL PANEL — FAILED (WEATHER RADAR) · airframe 26,098 hrs · 21,562 cycles

CAPTAIN'S WEATHER RADAR ON MFD DOES NOT WORK. R & R WX RADAR CTL IAW AMM 34-42-02. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 26,002 hrs · 21,486 cycles

DURING PS 2 INSPECTION FOUND AFT OVERHEAD WING EXIT LOCATING SIGN INTERMITTENT. R & R NR 3 EMER LIGHTING SYS POWER SUPPLY IAW WC 33-700-19. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 13699.

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 24,827 hrs · 20,339 cycles

ON CLIMB OUT PASSING THROUGH FL200 DURING ICE PNEUMATIC TEST EICAS & MASTER WARNING WE1 BLEED OVERTEMP AT APPROX 50 SECONDS DURING TEST. SECURED TEST BLEED TEMP BACK TO NORMAL RANGE DIVERT DUE TO ICING COND EN ROUTE. R & R LT FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECKED GOOD IAW AMM 36-00-00-700-803-A. DURING ANTI-ICE TEST GOT BLEED 1 OVERTEMP WARNING ABOUT 40 SECONDS INTO TEST. R & R FAN AIR VLV LT IAW AMM 36-11-03 PN 8166101 SN 200007177. R & R LT TEMP SENSOR PN 81662413 SN 2005010514 IAW AMM 36-20-01. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 24,545 hrs · 20,065 cycles

CEILING EXIT SIGN NEAR GALLEY IS INOPERATIVE. FOUND WIRE BROKEN ABOVE RT GALLEY BETWEEN CONNECTOR P8525 NAD SP9008. REPAIRED WIRE IAW SWPM 20-21-00 & WM 33-50-50. OPERATION CHECKED GOOD IAW AMM 33-50-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,019 hrs · 19,575 cycles

EMERGENCY PROXIMITY LIGHTS NR 1, 2, 3 & FWD LOWER SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT INVERTER NR 2 & NR 3 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 24,019 hrs · 19,575 cycles

NR 4 & NR 6 EMERGENCY PROXIMITY LIGHT STRIP HAS DAMAGED WIRES. R & R NR 4 & NR 6 EMERGENCY PROXIMITY LIGHT STRIP AS REQUIRED.

Part: WIRE — BROKEN (CABIN) · airframe 24,019 hrs · 19,575 cycles

NR 8 EMERGENCY PROXIMITY LIGHT STRIP WIRES BROKEN. R & R NR 8 EMERGENCY PROXIMITY LIGHT STRIP AS REQUIRED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,019 hrs · 19,575 cycles

EMERGENCY PROXIMITY LIGHTS AFT OF EMERGENCY EXIT INOPERATIVE. R & R NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 23,778 hrs · 19,360 cycles

FLIGHT ATTENDANT`S FLASHLIGHT WILL NOT CHARGE UNLESS ITS PUSHED & HELD IN. R & R FLIGHT ATTENDANT`S FLASHLIGHT ASSEMBLY IAW AMM 33-51-01, OPERATIONS CHECKED GOOD.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 23,265 hrs · 18,920 cycles

CAPTAIN`S FLASHLIGHT IS LOOSE IN THE CRADLE & HARD TO KEEP CHARGING. DEFERRED IAW MEL 25-53 AUTH 121495 C CAT C M ACTION. REMOVED AND REPLACED CAPTS FLASHLIGHT HOLDER IAW AMM 25-50-16 OPS CHECK GOOD.

Part: FLASHLIGHT ASSY — OVERHEATED (AFT CABIN) · airframe 21,952 hrs · 17,839 cycles

DURING MX INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE HAS SIGNS OF OVER HEATING. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (VHF) · airframe 21,846 hrs · 17,752 cycles

THE CREW REPORTED COMM 1.2.3 WAS WEAK/UNREADABLE WITH C & R INTERMITTENT, COM 1 WEAKER THAN COM 2 WITH CONSTANT STATIC. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. TESTED COMM 1, 2, 3 IAW AMM 23-12-00, FOUND NO STATIC ON ALL 3 SYS, FOUND SYS 2 AND 3 WORKING GOOD, NO MX ON 2 AND 3 COMM, FOUND COMM NR 1 WEAK. R & R ICU NR 1 IAW AMM 23-00-01 AND R & R NR 1 RMU IAW AMM 23-81-01. RADIO MANAGEMENT UNIT, INTEGRATED COMMS UNIT VHF. THE OPS CHECK WAS GOOD NR 1 COMM IAW AMM 23-12-00 AND THE OPS CHECK WAS GOOD RMU IAW AMM 23 81 00. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,081 hrs · 16,382 cycles

DURING B INSPECTION FOUND THE LEFT AND RIGHT OVER WING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULBS -NO FIX. TROUBLESHOT THE NR 4 BATTERY POWER SUPPLY. REMOVED AND REPLACED THE NR 4 BATTERY AND POWER SUPPLY IAW W/C 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,609 hrs · 16,009 cycles

DURING B INSPECTION, FOUND THE FORWARD AISLE EMERGENCY EXIT SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. FOUND BREAK IN WIRE W192-8584-22. REPAIRED WIRE BY BUTT SPLICING IAW WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,517 hrs · 15,932 cycles

DURING MAINTENANCE INSPECTION, FOUND A DENT IN THE LEFT FORWARD FUSELAGE AT FRAME 2 AND STRINGER 15 LEFT. REPAIRED IAW EO EM 53MR-1686 PART C. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,518 hrs · 15,932 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 58-59 CROSSBEAM. REPAIRED LT OMEGA BEAM IAW EO EM-53MR-1518, PART A.

Part: COFFEEMAKER — NOT SEATED (GALLEY) · airframe 18,792 hrs · 15,344 cycles

ON FLIGHT 4236 THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR. WHEN SHE TURNED THE HOT JUG OFF THE ODOR WENT AWAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND HOT JUG NOT FULLY SEATED INTO O/B POSITION. REMOVED AND REPLACED THE HOT JUG AS REQUIRED. NO FURTHER ODOR NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 18,770 hrs · 15,326 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE CAPTAIN’S FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABIN PRESSURE — FALSE INDICATION · airframe 18,633 hrs · 15,212 cycles

FLIGHT 4050, CREW REPORTED THAT AT 34,000 FT CABIN ALTITIUDE WAS AT 300 FT AND RISING QUICKLY WITH A DIFFENTAL PRESSURE OF 6.8 PSI. PRESSURE STABILIZED AT A CABIN ALTITUDE OF APPROXIMATELY 12,700FT AFTER A RAPID DESCENT TO 10K. DECLARED AN EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK IAW AMM 21-31-00 AND OPS CHECK OF PRESSURIZATION CONTROL SYSTEM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (CABIN) · airframe 17,957 hrs · 14,720 cycles

DURING PS-2 INSPECTION FOUND THE FLASHLIGHT ABOVE FLIGHT ATTENDANT SEAT HAS BROKEN HOLSTER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT AND CRADLE IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STARTER — BROKEN (NR 2 ENGINE) · airframe 14,766 hrs · 12,352 cycles

FOR FLIGHT 3936 THE CREW REPORTED THAT THE NUMBER 2 ENGINE FAILED TO START TWICE AND A LOT OF SMOKE CAME FROM THE ENGINE. THERE WAS NO ROTATION. CRASH, FIRE AND RESCUE WAS CALLED. THE AIRCRAFT WAS TOWED TO THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 AIR TURBINE STARTER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 6,459 hrs · 5,692 cycles

EN ROUTE TO PIA CREW GOT 'LAV SMOKE' ON EICAS. SOME SMOKE NOTED IN GALLEY. NO OTHER SMOKE NOTED. REMOVED AND REPLACED ENGINE 2 ZERO-CARBON SEAL IAW RRMM 72-25-25-000-801 AND 72-25-25-400-801-A. NO FURTHER OIL LEAK NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LAVATORY — WARNING LIGHT (FUSELAGE)

FLT 3665 - TUL - LAVATORY SMOKE DETECTOR LIGHT AND FAINT SMELL IN GALLEY AREA. TROUBLESHOT IAW EMB 145 FIM 21-20-00-810-801. COULD NOT DUPLICATE. A/C OK FOR SERVICE. PERFORMED ENGINE RUNS AND LEAK CHECK. (M)

Part: WARNING MESSAGE — ACTIVATED (LAVATORY)

AFTER TAKEOFF LAVATORY SMOKE WARNING AND EICAS MESSAGE. EMERGENCY DECLARED. NORMAL LANDING AND NOT OVERWEIGHT. CREW INSPECTED LAVATORY FOR SMOKE NO PHYSICAL SMOKE FOUND. REPLACED NR 2 ENGINE AND PERFORMED A SUCCESSFUL FCF. ENGINE P/N OFF/ON AE3007A1, S/N OFF CAE 312810, S/N ON CAE 311496. AIRCRAFT RETURNED TO SERVICE. (M)