N654AE

Part: CABIN PRESSURE — NO DISCREPANCY · airframe 53,278 hrs · 49,878 cycles

CAB ALT AND CAB RATE SHOWING ZERO. OPS CHECKED PER AMM 21-31-00 NO DEFECTS NOTED

Part: DAU — CHATTERING (ZONE 100)

DURING APPR AT 10000 LOST BOTH FUEL QTY IND INTERMITTENTLY. IND RETURNED AFTER LANDING. FACT 03FEB25 19:51 PHL R/R FWD AND AFT DAU IAW AMM 31-41-01 OPS CHECK GOOD. FUEL QTY SHOWS NO DASHES C/W AMM 28-41-00 TO INSPECT 28-41-00 NO DEFECTS FOUND OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 51,541 hrs · 47,921 cycles

STRONG ODOR NOTICED IN DESCENT AROUND 2,000FT IN THE FLIGHT DECK AND CABIN. FACT 21OCT24 04:25 MDT C/W FIM TASK 21-20-00-810-803A. NO DEFECTS FOUND. INSPECT BOTH ENGINES INTERNALLY AND EXTERNALLY, NO LEAKS NOTED. ENG 1 AND 2 AND APU OILS FOUND TO BE PROPERLY SECURED. INSPECTED FOR HYDRAULIC LEAKS UNDER CABIN FLOOR, NO LEAKS FOIUND. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 400) · airframe 51,353 hrs · 47,708 cycles

BLD 1 LEAK MSG DISPLAYED DURING DECENT. RAN UP #100 ENGINE AND INSPECTED BLEED AIR VALVE AND PACK ON #100 SIDE INSPECTED DUCTING NO LEAKS FOUND. COMPLIED WITH AIR BLEED SYSTEM OPERATIONAL TEST IAW AMM 36-00-00-700-803-A OPS CHECK GOOD. NO BLEED LEAK MESSAGES APPEAR.

Part: SWITCH — WARNING LIGHT (GUST LOCK) · airframe 50,241 hrs · 46,512 cycles

GUST LOCK ILLUMINATED AT PWR APPLICATION ON TAKE OFF. ELECTRO-MECHANICAL GUST LOCK SYSTEM. R & R SWITCHES IAW MM 27-71-14-05, RIGGED NEW SWITCHES IAW MM 27-71-14-05. SWITCHES S0657 AND S0659. OPS CK GOOD CLEAR MEL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E007209 THE RH ENGINE PYLON FORWARD YOKE UPPER FLANGE HAS VISIBLE DAMAGE. : REPAIRED THE RH ENGINE PYLON FORWARD YOKE UPPER FLANGE VISIBLE DAMAGE INSIDE THE HOLE WHERE THE FASTENER WAS REMOVED FOR INSPECTION IAW PIEDMONT EO1-54-23-0382

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E005137 NO REPAIR INFO FOUND FOR EXTERNAL FUSELAGE REPAIR DOUBLER AND TRIPLER BETWEEN FR 17/20 STR 18L/20L. REPAIRED EXISTING EXTERNAL FUSELAGE REPAIR DOUBLER AND DOUBLER/TRIPLER BTW FR17-20 AND BTW STR 18L-20L IAW PIEDMONT EO1-53-23-0390 AND ETD2023-145-027868 REV A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E005159 NO REPAIR INFO FOUND FOR EXTERNAL FUSELAGE REPAIR DOUBLER AT FR 26 BETWEEN STR 20L/21R. PERFORMED CUTOUT AND RE-ACCOMPLISHED DOUBLER REPAIR ON EXTERNAL FUSELAGE AT FR 26 BETWEEN STR 20L/21R IAW ETD2023-145-027841 AND EO1-53-23-0367

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E005157 NO REPAIR INFO FOUND FOR FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 29/30 STR 15R/17R. : RE-ACCOMPLISHED FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 29/30 STR 15R/17R IAW ETD2023-145-021114 AND EO1-53-23-0363

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E004729 LH BANANA PANEL IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE LH BANANA PANEL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E004750 R/H LAV FLOOR BEAM CORROSION FOUND TO EXTEND TO NUT PLATE HOLE ON OMEGA BEAM. REPAIRED R/H LAV FLOOR BEAM CORROSION AT NUTPLATE HOLE ON OMEGA BEAM IAW EO1-53-23-0351.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004502 ACCOMPLISH PERMANENT REPAIR FOR FCD1-53-23-0180 FUSELAGE WINDSHIELD PILLAR REINFORCEMENT, LH SIDE. ACCOMPLISHED PERMANENT REPAIR FOR FCD1-53-23-0180 FUSELAGE WINDSHIELD PILLAR REINFORCEMENT, LH SIDE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004503 ACCOMPLISH FCD1-53-23-0183 FUSELAGE FWD REINFORCEMENT FOR LH AND RH SIDE DV WINDOW CUTOUT. ACCOMPLISHED FCD1-53-23-0183 FUSELAGE FWD REINFORCEMENT FOR LH AND RH SIDE DV WINDOW CUTOUT. RECEIVED EO1-53-23-0375 ACCEPTING DEVIATION OF LH AND RH UPPER AFT DOUBLERS. RECEIVED PIEDMONT EO1-05-23-0377 ACCEPTING THE USE OF PLASTIC FILLERS IN REPAIR AREA.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004302 PREVIOUSLY BLENDED AREA BTW FR 28-29 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. CUTOUT DAMAGE, AND PERFORMED DOUBLER REPAIR OF PREVIOUSLY BLENDED AREA BTW FR 28-29 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE IAW EDT2023-145-026709 AND EO1-53-23-0359

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004250 LH WING RIB 21 HAS A POSSIBLE CRACK AT UPPER FLANGE. REPAIRED LH WING RIB 21 CRACK AT UPPER FLANGE IAW PIEDMONT EO1-57-23-0379

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004296 PREVIOUSLY BLENDED AREA AT FR 27 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. : CUT OUT DAMAGE, AND PERFORMED DOUBLER REPAIR ON PREVIOUSLY BLENDED AREA FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE AT FR 27 STGR 5R IAW ETD2023-145-026709 AND EO1-53-23-0359

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,487 hrs · 46,069 cycles

E004444 LH OMEGA BEAM CORRODED AT FR29 AT CROSSBEAM. REPAIR CORROSION ON LH OMEGA BEAM AT FR29 AT CROSSBEAM IAW PIEDMONT EO1-53-23-0353

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E004294 PREVIOUSLY BLENDED AREA AT FR 26 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. CUT OUT DAMAGE, AND PERFORMED DOUBLER REPAIR ON PREVIOUSLY BLENDED AREA FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE AT FR 26 STGR 5R IAW ETD2023-145-026709 AND EO1-53-23-0359

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E003942 EXTERNAL SKIN, THERE ARE 2 PREVIOUS LIGHTNING STRIKE BLENDS AT FR24-25, ON STGR 20L-21L. CUT OUT 2 PREVIOUS LIGHTNING STRIKE BLENDS, AND PERFORMED DOUBLER REPAIR AT CENTER FUSELAGE II, EXTERNAL SKIN, AT FR24-25, ON STGR 20L-21L IAW ETD2023-145-026517, AND EO1-53-23-0348.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E003712 FR65 SHEAR CLIP AT CARGO DOOR CUTOUT HAS CORROSION. : REPAIRED CORRODED FR 65 SHEAR CLIP AT CARGO DOOR CUTOUT IAW PIEDMONT EO1-53-23-0352

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E003551 FOUND RH VERTICAL STABILIZER SPHERICAL BEARING HOUSING BORE OUT OF LIMITS. ENLARGED RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOUSING TO THE FIRST OVER SIZE IAW PIEDMONT EO1-55-23-0378.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E003545 RUDDER 2 HAS TWO LIGHTNING STRIKE HOLES AFT OF LOWER CENTER HINGE FITTING. CUT OUT DAMAGE, PERFORMED DOUBLER REPAIR ON RUDDER 2 AT TWO LIGHTNING STRIKE HOLES AFT OF LOWER CENTER HINGE FITTING IAW ETD2023-145-026628 REV A AND EO1-55-23-0371

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E003269 PAX DOOR ENTRENCE AFT FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOORBOARD SUPPORT IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E003213 LAV CENTER BEAM GUSSET HAS CORROSION. : RAR LAV CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E003228 CABIN L/H #2 FLOORBOARD SUPPORT HAS CORROSION. : REMOVED AND REPLACED CABIN L/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E003068 CARGO L/H FWD FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND INSTALLED NEW L/H FWD FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E003274 SERVICE DOOR AFT SILL HAS CORROSION. : RAR SERVICE DOOR AFT SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,847 hrs · 46,069 cycles

E003268 PAX DOOR ENTRENCE FWD FLOORBOARD SUPPORT HAS CORROSION. REMOVED & REPLACED PAX DOOR ENTRANCE FWD FLOORBOARD SUPPORT IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E002398 PAX DOOR HANDLE BRACKET SUPPORT CRACKED AT UPPER NUT PLATE. RAR PAX DOOR HANDLE BRACKET SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E001596 CARGO DOOR INTERNAL SKIN HAS NUMEROUS CHAFE SPOTS. BLENDED NUMEROUS CHAFE SPOTS (3 EA) ON CARGO DOOR INTERNAL SKIN IAW EMB 145 SRM 51-10-03. 2 BLENDED AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 52-30-01AD. REPAIRED CARGO DOOR INTERNAL SKIN CHAFE SPOT OUT OF LIMITS IAW PIEDMONT EO1-52-23-0395 AND EMB 145 SRM 52-30-01RE ITEM 12, FIG 213

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E001274 EXTERNAL SKIN, THERE IS A LIGHTENING STRIKE AT FR29-30, ON STGR 19R-18R. PERFORMED CUT OUT AND DOUBLER REPAIR OF LIGHTNING STRIKE ON CENTER FUSELAGE II, EXTERNAL SKIN, AT FR29-30, ON STGR 19R-18R. IAW ETD2023-145-027308 AND EO1-53-23-0350

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E001277 EXTERNAL SKIN, THERE ARE 2 LIGHTENING STRIKES AT FR28-29 , STGR 19R-18R. OF THE 2 LIGHTNING STRIKES CENTER FUSELAGE II, EXTERNAL SKIN, AT FR28-29 , STGR 19R-18R 1(FWD) WAS REPAIRED BY DRILL AND RIVET/WASHER INSTALL IAW EMB 145 SRM 53-00-01RE ITEM 2B, AN 1 (AFT) WAS REPAIRED BY CUTOUT AND DOUBLER REPAIR BOTH IAW ETD2023-145-027308 AND EO1-53-23-0350

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E001091 EXTERIOR SKIN, THERE IS A LIGHTENING STRIKE AT ON FR 20, STGR 19R-20R. CUT OUT DAMAGE, PERFORMED DOUBLER REPAIR ON CENTER FUSELAGE 1, EXTERIOR SKIN, LIGHTENING STRIKE AT ON FR 20, STGR 19R-20R IAW ETD2023-145-026716 AND EO1-53-23-0347

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,847 hrs · 46,069 cycles

E000706 CARGO DOOR, THERE ARE SMALL PAINT SCRATCHES AT VARIOUS LOCATIONS. REPAIRED SMALL SCRATCHES ON CARGO DOOR AT VARIOUS LOCATIONS IAW PIEDMONT EO1-52-23-0349

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,108 hrs · 45,241 cycles

T/O ABORTED AT ABOUT 100KTS DUE TO GUSTLOCK CAUTION ILLUMINATED FOR ABOUT 10 SECONDS FACT 05MAY23 01:50 PHL PERFORMED GUST LOCK OPS CHECK PER AMM 27-71-00 OPS CHECK GOOD, NO ACTION TAKEN AT THIS TIME AS NO FAULT WAS RECORDED DURING THE OPS CHECK. CLEAR MEL 27-11 MEL 05MAY23 16:22 PHL C12509 27-11 ELECTRO-MECHANICAL GUST LOCK SYSTEM

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,904 hrs · 44,985 cycles

FLIGHT ATTENDANT UPPER EXIT SIGN INOP. FACT: R&R'D EMERGENCY BATTERY IAW W/C 33-70-19

Part: NONE — NONE · airframe 47,232 hrs · 43,065 cycles

654 21-51 2495471 23MAR22 FWA CLOSE ON T/O ROLL PACK 1 OVERHEAT MESSAGE DISPLAYED EXTINGUISHED AFTER THRUST LEVER WAS RETARDED. IN MANUAL MODE. FACT 23MAR22 03:18 MDT INSPECTED #1 PACK & FOUND BOTH SLEEVES AT Y-DUCT AFT OF THE DUAL TEMP CONTROL VALVE LEAKING.INSTALLED NEW SLEEVES PER AMM 21-60-01.OPERATED #1 PACK WITH ENGINE BLEEDS AT TAKE OFF POWER OPS & LEAK CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 46,330 hrs · 42,040 cycles

A/C EXPERIENCED SMOKE ON FLIGHT DECK AND IN CABIN DURING TAKE OFF. MXT INSP NO.1 AND NO.2 ENGINE INLETS FOR DEBRIS OR DAMAGE, NONE FOUND. ALSO GROUND RAN NO.1 AND NO.2 ENGINES ALTERNATING BETWEEN BLD 1 AND BLEED 2 NO SMOKE AND OR SMELL PRESENT, ALSO PERFORMED PACK 1 AND PACK 2 GVI, NO DAMAGE NOTED OK FOR SERVICE.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

SSI 53-20-13 CORROSION ON SERVICE DOOR CENTER SILL....REPAIRED CORROSION ON SERVICE DOOR CENTER SILL IAW PIEDMONT EO1-53-21-0086

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 45,563 hrs · 41,203 cycles

RH REAR FUSELAGE II SKIN PREVIOUS REPAIR DOUBLER, JUST FWD OF 312AR HAS TOOLING MARKS, INCORRECTLY INSTALLED RIVETS, AND A MISSING RIVET....RE-ACCOMPLISHED RH REAR FUSELAGE II SKIN DOUBLER IAW PIEDMONT EO1-53-21-0079.

Part: SUPPORT — DAMAGED (FRM 26 S15-16R) · airframe 45,563 hrs · 41,203 cycles

FRAME 26 HAS ELONGATED HOLES AT FLOOR SILL ATTACH POINT BETWEEN STR 15R-16R REPAIRED FRAME 26 ELONGATED HOLES AT FLOOR SILL ATTACH POINT BETWEEN STR 15R-16R IAW PIEDMONT EO1-53-21-0085

Part: SUPPORT — DAMAGED (FRM 24 S15-16R) · airframe 45,563 hrs · 41,203 cycles

FRAME 24 HAS ELONGATED HOLES AT FLOOR SILL ATTACH POINT BETWEEN STR 15R-16R...REPAIRED FRAME 24 ELONGATED HOLES AT FLOOR SILL ATTACH POINT BETWEEN STR 15R-16R IAW PIEDMONT EO1-53-21-0084.

Part: FITTING — WORN (RUDDER) · airframe 45,563 hrs · 41,203 cycles

UPPER RUDDER ACTUATOR TO RUDDER 1 HINGE FITTING IS WORN....REPAIRED UPPER RUDDER ACTUATOR TO RUDDER 1 HINGE FITTING IAW EO1-55-21-0077.

Part: WEB — CORRODED (CARGO DOOR) · airframe 45,563 hrs · 41,203 cycles

SSI 52-30-08 CORROSION ON BAGGAGE DOOR WEBBING 2 EACH MARKED....ACCOMPLISHED 2 REPAIRS OF CARGO DOOR INNER WEB AT LOWER FWD AREA IAW EMB-145 SRM 52-30-01 RE ITEM 12 AND EO1-52-21-0076.

Part: BEAM — CORRODED (FRM 23) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

SSI 53-20-11 CORROSION ON RH BEAM AT FRAME 23....ACCOMPLISHED REPAIR ON RH BEAM AT FR23 IAW EMB 145 SRM 53-21-10 ITEM 6 FIGURE 205 AND EO1-53-21-0081

Part: SHEAR TIE — CORRODED (FRM 65) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

SSI 53-30-48, CARGO DOOR CUTOUT SHEAR CLIP AT FRAME 65 HAS CORROSION ON LOWER END MARKED....REPAIRED REPAIR AT FR 65 BETWEEN STR 15-18L IAW SRM 53-31-04RE ITEM 4, FIG 212 AND EO1-53-21-0074

Part: SHEAR TIE — CORRODED (FRM 68) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

SSI 53-30-48, CARGO DOOR CUTOUT SHEAR CLIP AT FRAME 68 HAS CORROSION ON LOWER END MARKED. REPAIRED CARGO DOOR CUTOUT SHEAR CLIP AT FRAME 68 ON LOWER END IAW EMB145 SRM 53-31-04RE ITEM 4D AND EO1-53--21-0073.

Part: ATTACH BRACKET — GOUGED (FUSELAGE) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

PILOT'S BULKHEAD OTBD UPPER ATTACHMENT REPAIRED BRACKET IS GOUGED. REPAIRED PILOT'S BULKHEAD OUTBOARD UPPER ATTACHMENT BRACKET IAW EO1-53-21-0068.

Part: CROSSBEAM — CORRODED (FRM 44) · corrosion level 2 · airframe 45,563 hrs · 41,203 cycles

SSI 53-20-11 LH OMEGA BEAM CORRODED AROUND CROSS BEAM AT FR 44....REPAIRED LH OMEGA BEAM AROUND CROSS BEAM AT FR 44 IAW EMB145 SRM 53-00-10, AND PIEDMONT EO1-53-21-0067.

Part: PEDAL — LOOSE (RUDDER) · airframe 45,534 hrs · 41,178 cycles

ON TAKEOFF ROLL AIRCRAFT VEERED HARD TO THE RIGHT LEFT HAND RUDDER PEDAL IS ACTUATING THE LEFT BRAKES. CREW REPORTED ABORTED AT 10 KNOTS. PERFORMED OPS CHECK FOR MAIN BRAKE SYS IAW AMM 32-41-00 AND RUDDER SYS CHECK IAW AMM 27-25-00. BOTH CHECKS ARE SATISFACTORY, NO DEFECTS NOTED. INSP'D RUDDER PEDAL AREA FOUND A LOOSE AIR DUCT ON PILOTS SIDE. SECURED DUCT ON BRACKET. PERFORMED TAXI CHECK, RUDDER AND BRAKE SYS OPS NORMAL. OPS CHECK GOOD. OK FOR

Part: GUST LOCK — MALFUNCTIONED (NOT REPORTED) · airframe 45,430 hrs · 41,067 cycles

GUST LOCK WOULD NOT UNLOCK THEN THE GUST LOCK WOULD NOT LOCK. PERFORMED OPERATIONAL CHECK, IAW AMM 27-71-00. OPERATIONS CHECK GOOD. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (GUST LOCK) · airframe 45,057 hrs · 40,642 cycles

GUST LOCK LIGHT ILLUMINATED DURING TAKE OFF ROLL. MAINTENANCE: PERFORMED OPS CHECK OF GUST LOCK MECHANISM IAW AMM TASK 27-70-00-700-802-A. OPS CHECK GOOD. LIGHT ILLUMINATED NORMALLY. OK FOR SERVICE AT THIS TIME. CLEARS MEL 27-11.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 44,945 hrs · 40,515 cycles

AIRCRAFT PULLED TO LEFT DURING TAKEOFF ROLL WITH LEFT BRAKE TEMPS READING HIGH. INSP'D ALL 4 BRAKES IAW AMM 32-49-03-06, NO DEFECTS FOUND. PERFORMED HIGH SPEED TAXI WITH CREW. OPS NORMAL, NO DEFECTS NOTED. PERFORMED SECOND HIGH SPEED TAXI. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,375 hrs · 39,862 cycles

TERMINATING CREW REPORTS STRONG ODOR CAUSING COUGH. LASTED TO 1000FT(HAPPEN DURING TAKEOFF. CREW GROUND RAN AIRCRAFT OPERATING BOTH ENGINES AND APU USING BOTH BLEED SYSTEMS. NO SMELLS OR ODORS NOTED. AIRCRAFT OK FOR SERVICE. -PCS- A/C DOWN FROM LAST NITE FOR STRONG ODOR ON TAKE-OFF FROM PHL, TERMINATING CREW STATED THEY HAD THE SMELL LAST 3 FLTS, SENT ALB MECHS ON ROADTRIP, ORIGINATING CAPT GND RUN A/C W/CONTRACT MAINT AND ALB MECHS NO ODOR OR SMELL NOTED. HISTORY: NONE WORK COMPLETE, CAPT SENT ACARS AFTER LEAVING BUF NO SMELL AFTER TAKE-OFF, CREATED FOR MIR PURPOSE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,375 hrs · 39,862 cycles

MAINTENANCE FOUND FWD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED #200 EMERGENCY BATTERY AND POWERSUPPLY IN REFERANCE TO W/C 33-70-19. OPTS CHECK GOOD. OK FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,771 hrs · 39,172 cycles

NDIS 654 33-50 0010340 27SEP19 SBY CLOSE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE FACT 27SEP19 15:06 SBY REMOVED AND REINSTALLED EMERGENCY EXIT SIGN CORRECTL Y. LIGHT ILLUMINATES. OPS CHECK GOOD.

Part: AMPLIFIER — INOPERATIVE (EMERGENCY COMMS) · airframe 43,406 hrs · 34,793 cycles

ABSENCE OF EMERGENCY COMMUNICATIONS BETWEEN PILOT AND FLIGHT ATTENDANT... REMOVED AND REPLACED PUBLIC ADDRESS AMPLIFIER IAW AMM TASK 23-31-01-000/400-801 -A

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,538 hrs · 37,740 cycles

NDIS 654 33-51 0005530 19FEB19 RIC CLOSE TWO EMERGENCY SERVICE DOOR LIGHTS WILL NOT ILLUMINATE AND ROWS 1-7 EMERGENCY FLOOR PROXIMITY LIGHTS WILL NOT ILLUMINATE FACT 19FEB19 06:54 RIC REMOVED #2 EMERGENCY LIGHT BATTERY. INSPECTED BATTERY PINS. REINSTALLED #2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD AT THIS TIME. WORK DONE IN REF TO AMM 33-50-04-000/400-801-A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,538 hrs · 37,740 cycles

NDIS 654 33-51 0005550 19FEB19 RIC CLOSE FWD FUSELAGE RH EMERGENCY LIGHT WILL NOT ILLUMINATE FACT 19FEB19 07:10 RIC REMOVED #2 EMERGENCY LIGHT BATTERY. INSPECTED BATTER Y PINS. REINSTALLED #2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD AT THIS TIME. WORK DONE IN REF TO AMM 33- 50-04-000/400-801-A.

Part: BATTERY — NOT SEATED (EMERGENCY LIGHTS) · airframe 42,217 hrs · 37,384 cycles

DIS 654 33-51 0003990 16DEC18 SBY CLOSE EMERGENCY LIGHT ABOVE F/A SEAT INOP 31253 00 BAD FACT 16DEC18 10:20 SBY RESEATED #1 BATTERY BEHIND COAT CLOSET. RESECURED PANELS

Part: TRUNNION — CRACKED (RT MLG) · airframe 41,541 hrs · 36,582 cycles

RIGHT MLG AFT UPPER TRUNNION WAS CRACKED, JUST OTBD OF THE BEARING, IN THE RADIUS. REMOVED AND REPLACED THE RT MLG AFT TRUNNION IAW ERS-EM-57MR-996.

Part: TRUNNION — CRACKED (LT MLG) · airframe 41,541 hrs · 36,582 cycles

LEFT MLG AFT UPPER TRUNNION WAS CRACKED JUST OTBD OF THE BEARING. REMOVED AND REPLACED THE LT MLG AFT TRUNNION IAW ERS-EM-57MR-995.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,541 hrs · 36,582 cycles

EMERGENCY LIGHT STRIP NR 8 WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 41,364 hrs · 36,423 cycles

SPOILERS FAILED ON APPROACH, AT APPROXIMATELY 800 FT AGL. COMPLIED WITH QRH PROCEDURES. TROUBLESHOT THE GROUND SPOILER AIR/GROUND CKT FAULT IAW FIM 27-63-00-810-811-A. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW AMM 27-63-02. OPS CHECKED IAW AMM 27-63-01. OPS CHECKED GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 40,773 hrs · 35,827 cycles

DURING CLIMB, AT APPROXIMATELY 3000 FT, A LOUD AUDIBLE BANG WITH VIOLENT YAW OF AIRCRAFT NOSE. NR 2 ENGINE OIL QUANTITY SHOWED 11 ATS AND THE NR 2 ENGINE PRESSURE INDICATED 0. RAN ASSOCIATED CHECKLIST AND DUE TO LOUD BANG AND ZERO OIL PRESSURE DECIDED NOT TO RESTART THE ENGINE. INSPECTED THE ENGINE AND FOUND DEBRIS IN THE INLET OF THE ENGINE CORE AND HPC WOULD NOT ROTATE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,722 hrs · 35,773 cycles

EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT IS INOPERATIVE. REMOVED AND REPLACED THE SIGN, OPS TESTED GOOD IAW AMM 33-50-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 40,398 hrs · 35,516 cycles

EMERGENCY LIGHTS #4,5 FLOOR PROX. LIGHTS AND ALL OVERWING EMERGENCY EXIT INTERI0R EMERGENCY LIGHTS WILLL NOT ILLUMINATE.-C/A-T/S IAW WM 33-50-50 REMOVED FLOOR PANEL 251JF IAW AMM 53-01-02 AND FOUND ELECT. CONNECTOR P8031 COMPLETELY DISCONNECTED. FROM #3 BATTERY CHARGER AND BATTERY RE-SECURED ELECT. CONNECTOR P8031 AND ALL EMERGENCY LIGHTS OPS CK GOOD IAW AMM 33-50-00. RE-INSTALLED FLOOR PANEL 251JF IAW AMM 53-01-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,302 hrs · 35,420 cycles

12 B/C EMERGENCY LIGHT UPPER INOPERATIVE. R & R THE LAMP IAW AMM 33-50-08-000-801, AND 33-50-08-400. OPS CHECKED GOOD.

Part: ROLLER — STIFF (PAX DOOR) · airframe 39,862 hrs · 34,943 cycles

FA REPORTED THAT THE CABIN DOOR WAS DIFFICULT TO OPEN. FOUND THE DOOR ROLLERS STIFF, LUBRICATED THE ROLLERS. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,564 hrs · 34,691 cycles

NR 4 EMERGENCY FLOOR PROXIMITY LIGHT WIRING IS DAMAGED. R & R THE NR 4 EMERGENCY FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (ANTI ICE SYSTEM) · airframe 39,468 hrs · 34,593 cycles

ANTI-ICE SYSTEM IS ACTIVATING IN FLIGHT WHEN NOT IN ICING CONDITIONS. PERFORMED AN OPS CHECK OF ICE DETECTION SYSTEM IAW AMM 30-80-00. OPS TESTED OK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 38,952 hrs · 34,124 cycles

ELECTRICAL BURNING ODOR DURING APPROACH. NO SMOKE PRESENT. TROUBLESHOT IAW ETN EM 72-034, NO ODOR NOTED. THE CREW DETECTED THE ODOR. CHECKED FWD AVIONICS, BATTERY BAY, FWD HYD BAY, INSTRUMENT PANEL, REAR COCKPIT PANEL AND EMERGENCY FLASHLIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,869 hrs · 34,045 cycles

SERVICED DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPS CHECK GOOD AT THIS TIME END.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,858 hrs · 34,033 cycles

EMERGENCY EXIT LIGHT JUST AFT OF THE LT EMERGENCY EXIT HATCH INOPERATIVE. INSTALLED A NEW EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY IAW 33-700-19, OPS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 37,348 hrs · 32,653 cycles

CARGO DOOR SILL CORRODED. REMOVED AND REPALCED CARGO DOOR SILL IAW SRM 51-40-02

Part: SKIN — CRACKED (FRAME 75) · airframe 37,348 hrs · 32,653 cycles

LEFT AFT FUSELAGE FRAME 75 SKIN CRACKED BELOW STRINGER 2L. REPAIRED THE SKIN IAW ERS-EM-53MR-2159

Part: SKIN — CRACKED (FRAME 75) · airframe 37,348 hrs · 32,653 cycles

RT AFT FUSELAGE, FRAME 75 SKIN CRACKED BELOW STR 2R. REPAIRED THE SKIN IAW ERS-EM-53MR-2162

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 37,338 hrs · 32,644 cycles

EMERGENCY LIGHT STRIP FEMALE CONNECTOR IS DAMAGED. REPAIRED EMERGENCY LIGHT STRIP FEMALE CONNECTOR IAW SPWM 20-21-00, OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,190 hrs · 32,516 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT ASSEMBLY IAW AMM 33-50-10-000-801 & 33-50-10-400-801. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,983 hrs · 32,352 cycles

RIGHT LOWER EMER LIGHT INOPERATIVE. R & R RT EXTERNAL LOWER EMER LIGHT IAW AMM 33-50-10-000-801 & 33-50-10-400-801. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,915 hrs · 32,290 cycles

SERVICE DOOR EMER EXIT LIGHT IN DOOR HINGE TRIM COVER INOPERATIVE. R & R SERVICE DOOR EMER EXIT LIGHT LAMP IN DOOR HINGE TRIM COVER IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: HINGE — LACK OF LUBE (CABIN DOOR) · airframe 36,866 hrs · 32,251 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LUBED MAIN CABIN DOOR FLAP HINGE. OPERATIONAL CHECKED GOOD IAW AMM 52-10-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,736 hrs · 32,130 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. REPLACED SERVICE DOOR EMER LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A.

Part: SWITCH — MALFUNCTIONED (BLEED AIR SYS) · airframe 36,653 hrs · 32,042 cycles

DURING CLIMB OUT, BLD 1 VLV CLSD ADVISORY MSG ON EICAS. UNABLE TO OPEN BLD VLV OUT TO ORD UPON REDUCING THRUST LEVERS, MSG EXTINGUISHED. R & R NR 1 BLEED PUSH BUTTON SWITCH IAW MM 20-13-04. OPERATIONS CHECKED GOOD.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 36,360 hrs · 31,771 cycles

UPON RETRACTING GEAR AFTER TAKEOFF, GEAR INDICATION TURNED AMBER, FOLLOWED BY RED WITH A LG & LEVER DISAGREE WARNING MSG. THIS REMAINED UNTIL BUMPING LEVER TO CONFIRM ITS POSITION, UPON WHICH GEAR RETRACTED. FOR CORRECTIVE ACTION REF LOG PAGE 3871528 ITEM 1 FOR R & R OF LG LEVER ASSEMBLY & OPERATIONS CHECKS. R & R LG CONTROL LEVER IAW MM 32-32-02. OPERATIONS CHECKED GOOD IAW AMM 32-30-00.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 36,352 hrs · 31,765 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: PUMP — UNKNOWN (NR 1 ENGINE) · airframe 36,332 hrs · 31,748 cycles

TAKEOFF 1, AFTER THRUST WAS SET, RECEIVED AN E1 FUEL LOW PRESSURE EICAS MSG, WITH ASSOCIATED RELAYS CLICKING CYCLING THE FUEL PUMPS. NR 1 ENG WAS ON PUMP C. ABORT BELOW 80 KTS HIGH SPEED. E1 FUEL LOW PRESS WITH PUMP 1C SELECTED. 1C FUEL PUMP & LOW PRESS WARNING OPERATIONS CHECKED GOOD IAW AMM 28-45-00.

Part: DOOR SEAL — LACK OF LUBE (PAX DOOR) · airframe 35,693 hrs · 31,169 cycles

MAIN PAX DOOR HARD TO OPERATE. INSPECTED & LUBED MAIN DOOR RUBBER SEAL & FRAME RUBBER SEAL IAW AMM 52-18-00. NO DEFECT NOTED.

Part: DUCT — LOOSE (AC BAY) · airframe 35,519 hrs · 31,012 cycles

FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, NO SMELL. TURNED PACK 1 OFF, SMOKE DISAPPEARED. FOUND SMOKE TO BE AIR CONDITION CONDENSATION, CAUSE OF LOOSE DUCT FROM PACK TO RECIRC FAN. R & R DUCT TO NR 1 RECIRC FAN IAW AMM 21-20-04. PERFORMED AIR CONDITION OPERATIONS CHECK, FOUND WORKING GOOD NO SMOKE NOTED AT THIS TIME IAW 21-51-00.

Part: ROLLER — LACK OF LUBE (DOOR) · airframe 35,416 hrs · 30,933 cycles

FLIGHT ATTENDANT REPORTS THAT THE MAIN DOOR IS DIFFICULT TO OPEN & CLOSE. LUBRICATED MAIN DOOR FRAME ROLLERS & ACTUATED DOOR OPEN & CLOSE PROPERLY IAW AMM 52-18-00.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 35,353 hrs · 30,872 cycles

MAIN CABIN DOOR DIFFICULT TO OPERATE. CLEANED & LUBED DOOR ROLLERS IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 34,856 hrs · 30,442 cycles

FLIGHT ATTENDANTS FWD FLASHLIGHT HOLDER BROKEN. REMOVED FWD FLIGHT ATTENDANTS FLASHLIGHT HOLDER. INSTALLED SERVICEABLE FLASHLIGHT & FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD & MEL RESTORED.

Part: SEAL — FAILED (WINDSHIELD) · airframe 33,995 hrs · 29,688 cycles

AFTER TAKEOFF HEARD A NOISE FROM TOP CENTER WINDSHIELD AREA, RETURN TO LAND. PERFORMED PERMANENT REPAIR OF CAPTAIN`S WINDSHIELD FILLET SEAL IAW SRM 52-20-01.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS) · airframe 33,963 hrs · 29,652 cycles

BLEED 1 OVER TEMP WARNING DURING CLIMB THROUGH 8000 FT ICING CONDITIONS, BLEED TEMP POINTER WAS IN RED RANGE SAT-10 TAT-1C. R & R NR 1 FAN AIR THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,897 hrs · 29,569 cycles

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

Part: POTENTIOMETER — FAILED (NLG STEERING) · airframe 33,880 hrs · 29,552 cycles

WHEN PARKING IN THE 32R PAD IN A LT TURN FULL TILLER THE NOSE WHEEL, STEER INOPERATIVE, MSG ON THE EICAS, NEVER RELEASED PRESS FROM TILLER HANDLE. R & R NLG FEEDBACK UNIT, POTENTIOMETER, IAW AMM 32-50-07. OPERATIONS CHECKED GOOD FOR FEEDBACK POT R & R, BUT DID NOT CURE ORIGINAL DISCREPANCY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,839 hrs · 29,522 cycles

NUMBER 2 FLOOR PROXIMITY LIGHT STRIP WILL NOT ILLUMINATE. R & R NR 2 CABIN FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,839 hrs · 29,522 cycles

EMERGENCY LIGHTING NR 2 BATTERY NOT CHARGING. R & R NR 2 BATTERY POWER SUPPLY IAW AMM 33-50-04.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

LEFT CTR I SKIN HAS TOOLING MARK AT FRAME 20, STRINGER 3L. PERFORMED REPAIR TO LT CTR I SKIN AT FRAME 20 STRINGER 3L IAW ERS-EM-53MR-873 R1.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE I SKIN. R & R LT CTR FUSELAGE I SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 53-21-01, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

ELONGATED HOLES ON RT ELEVATOR TE TIP & LOWER SKIN. PERFORMED CUT OUT, FABRICATED & INSTALLED DOUBLER FILLER ON RT ELEVATOR TE TIP LOWER SKIN IAW ERS-EM-55MR-199.

Part: SPAR — DAMAGED (RT HORIZ STAB) · airframe 33,839 hrs · 29,522 cycles

RIGHT STAB SPAR II 58% CTL FRAMING HAVE DAMAGED HOLES NEAR ROOT. REPAIRED 5 DAMAGED HOLES AT RT STAB SPAR II & 58% CTL FRAMING BY OVERSIZING HOLES & INSTALLING BUSHINGS IAW ERS-EM-55MR-196.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACED RT STAB UPPER SKIN. R & R RT STABILIZER TOP SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06 SRM 55-10-01 SI & ETN-EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

TOOLING MARK ON OTBD SIDE OF LT ELEVATOR UPPER CTR SKIN. REPAIRED TOOLING MARK ON OTBD SIDE OF LT ELEVATOR UPPER CTR SKIN AREA IAW ERS-EM-55MR-188.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I TOP FWD SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 53-31-01, ETN-EM-51-118 & ETN-EM-53-266.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OTBD UPPER SKIN TIP. R & R RT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN-EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE I. R & R RT CTR FUSELAGE I SKIN IAW SRM 53-21-01-SI, 51-20-01 03, 51-40-02 03 06 08, ETN-EM-53-262 & ETN-EM-51-118.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN CROWN. R & R FWD FUSELAGE II SKIN CROWN IAW SRM 51-20-01 03, 51-40-02 03 04 06 08, 53-12-01, ETN EM-53-206 & EM-51-118.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I SKIN LT AFT. R & R FWD FUSELAGE I SKIN LT AFT IAW SRM 53-11-01, 51-20-01 03, 51-40-02 03/06/08 & ETN-EM-53-235 & ETN-EM-51-118.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, SRM 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, SRM 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II LT SKIN. R & R CTR FUSELAGE II LT SKIN IAW SRM 53-22-01, 51-20-01 03 & 51-40-020 3/06/08 & ETN-EM-53-263 & ETN-EM-51-118.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I SKIN LT FWD. R & R FWD FUSELAGE I LT FWD SKIN IAW SRM 53-11-01, 51-40-02 03 06 08, ETN-EM-53-235 & ETN-EM-51-11.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02, SRM 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, SRM 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I SKIN RT FWD. R & R FWD FUSELAGE I RT FWD SKIN IAW SRM 53-11-01, 51-40-02 03 06 08, ETN- EM-53-235 & ETN-EM-51-118.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R LT STABILIZER TOP SKIN IAW SRM 51-40-02, SRM 55-10-01 & ETN EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II TOP SKIN. R & R CTR FUSELAGE II SKIN TOP IAW SRM 51-20-01 03, 51-40-02 03 04 06 08, 53-22-01 SI & ETNS EM 51-118 & EM-53-263.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OUTER LE. R & R RT ELEVATOR OUTER LE IAW SRM 51-40-02, 51-20-01, 51-20-02, 51-40-06, 55-20-01, ETN EM-55-073 & ERS-EM-5500-178.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I SKIN RT AFT. R & R FWD FUSELAGE I SKIN RT AFT IAW SRM 53-11-01, 51-20-01/03, 51-40-02 03/06/08 & ETN-EM-53-235 & ETN-EM-51-118.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 53-24-01, 51-20-01 03, 51-40--02/03/06/08 & ETN'S EM-51-118 & EM-53-265.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN WIPER. R & R FWD FUSELAGE II SKIN WIPER PANEL IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 53-12-01 ETN-EM-51-118 & ETN-EM-53-206.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OUTER LE. R & R LT ELEVATOR OUTER LE IAW SRM 51-40-02, SRM 55-20-01 & ETN EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 33,839 hrs · 29,522 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, SRM 55-20-01 & ETN EM 55-073.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,476 hrs · 29,238 cycles

SEAT 14 FLOOR PROX EMER LIGHT INOPERATIVE. R & R SEAT 14 FLOOR EMER PROX LIGHT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,871 hrs · 28,749 cycles

FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT IS INOPERATIVE. CHARGING CRADLE WORKS OK. R & R FWD CABIN FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,517 hrs · 28,478 cycles

NR 1 FLOOR EMERGENCY LITE STRIP NOT WORKING DURING TEST. R & R NR 1 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — DAMAGED (CABIN) · airframe 32,517 hrs · 28,478 cycles

NR 4 EMERGENCY LIGHT STRIP WIRE INSULATION TORN. REPAIRED USING HEAT SHRINK RNF-100-1/8-WH & RNF-100-3/16-WH IAW SWPM 20-21-00 STEP 7.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 32,517 hrs · 28,478 cycles

LEFT EMERGENCY LIGHT ON FWD BELLY PANEL WIRES AT CONNECTOR DAMAGED. REPAIRED W122-8276-22 & W122-8277-22N AT CONNECTOR P8561 WITH TERMINAL ENDS M39029 56-351 IAW SWPM 20-00-03 PAGE 31 & SWPM 20-50-01 STEP 2 - 4.

Part: WIRE — DAMAGED (CABIN) · airframe 32,517 hrs · 28,478 cycles

NR 2 EMERGENCY LIGHT STRIP WIRE INSULATION TORN. REPAIRED USING HEAT SHRINK RNF-100-1/8-WH & RNF-100-3/16-WH IAW SWPM 20-21-00 STEP 7.

Part: WIRE — DAMAGED (CABIN) · airframe 32,517 hrs · 28,478 cycles

FORWARD CABIN FLOOR PROXIMITY LIGHT STRIP WIRES, ACFT SIDE, DAMAGED. REPAIRED W 192-8630-22 & W192-8631-22 AT SPLICES SP9019 & SP9020 WITH TERMINAL ENDS M39029 32-248 & M39029 31-229 IAW SWPM 20-00-03 PAGE 65.

Part: RELAY — FAILED (LANDING GEAR) · airframe 32,463 hrs · 28,427 cycles

LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. R & R RELAYS K0352, K0353 & K0453 IAW AMM 20-13-02. PERFORMED NUMEROUS EXTENSION & RETRACTION SYS OPERATIONAL CHECKS IAW AMM 32-30-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — MALFUNCTIONED (CABIN) · airframe 32,327 hrs · 28,328 cycles

DURING PS2 CHECK FOUND AFT FLASHLIGHT TO BE MALFUNCTIONING. R & R AFT FLASHLIGHT IAW AMM 33-50-16, OPERATION GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,180 hrs · 28,208 cycles

AFT CABIN FLASHLIGHT HOLDER BROKEN. R & R AFT CABIN FLASHLIGHT HOLDER IAW EMB AMM 33-50-16.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,702 hrs · 27,856 cycles

MOST FWD EMERGENCY FLOOR STRIP INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY & CHARGER. OPERATIONS CHECKED GOOD IAW EMB AMM 33-50-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,458 hrs · 27,659 cycles

SEVERAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. R & R NR 2 BATTERY IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 31,253 hrs · 27,493 cycles

CAPTAIN`S FLASHLIGHT RED CHARGING LIGHT IS INTERMITTENT. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,133 hrs · 27,395 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,874 hrs · 27,185 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 30,864 hrs · 27,176 cycles

MAIN CABIN DOOR LEVER HARD TO MOVE. LUBED ROLLER IAW REF AMM 20-30-02. OPS CHECKED GOOD

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,534 hrs · 26,157 cycles

ON FLIGHT 3265 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN/CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN PAX DOOR & PERFORMED ADJUSTMENT TEST IAW EMB AMM 52-10-01 AND ETN # EM 52-029 DOOR MAX LOAD MEASURED 43 LBS IN LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,386 hrs · 26,056 cycles

ON FLIGHT 2755 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 29,348 hrs · 26,030 cycles

ON FLIGHT 2900 THE CREW REPORTED THE NOSE WHEEL STEERING WAS INTERMITTENT DURING TAXI AT HIGH SPEED. DURING LANDING IT TOOK MORE FORCE TO MOVE TILLER THAN NORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. TAXI AIRCRAFT FOR CHECKING NOSE WHEEL STEERING IAW EMB 145 32-50-00 AMM. THE OPERATIONAL CHECK WAS GOOD, COULD NOT DUPLICATE PROBLEM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 29,048 hrs · 25,795 cycles

ON FLIGHT 2849 THE CREW REPORTED THAT ON TAKEOFF THE FIRST OFFICER TRIED TO TRIM AND RECEIVED PTRIM MAIN INOP. FOLLOWING THE CHECKLISTS THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR IAW EMB AMM 27-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,903 hrs · 25,679 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT SIGN ABOVE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ILLUMINATION EMERGENCY LIGHT IAW EMB 140 AMM 33-50-13. EXIT MARKER MAIN DOOR PART NUMBER:7444-1. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER IAW EMB 140 AMM 33-50-11. THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,882 hrs · 25,666 cycles

DURING MAINTENANCE CHECK FOUND THE FORWARD RIGHT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD RIGHT EMERGENCY LIGHT IAW EMB-145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — LOOSE (ACM) · airframe 28,095 hrs · 25,013 cycles

FLIGHT 3498, CREW REPORTED THAT AT FLIGHT LEVEL 250 PACK 1-2 VALVE CLOSED. STARTED TO CLIMB, WERE UNABLE TO RESET PACK 1 CABIN REACHED 4400 AT FL 200 PACK 1 TURNED BACK ON. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK AT LEFT AIR CIRCULATION MACHINE AIR OUTLET, SECURED CLAMP AND CHECK SYSTEM ON LT SIDE IAW 21-51-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,893 hrs · 24,811 cycles

DURING B INSPECTION, FOUND ROW 4 AND 5 FLOOR EMERGENCY PROXIMITY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,913 hrs · 24,824 cycles

DURING MAINTENANCE INSPECTION, FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 27,872 hrs · 24,791 cycles

SHEAR TIE FR 65 CORRODED. R & R SHEAR TIE AT FR 65 IAW EO EM-53MR-1129.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,872 hrs · 24,791 cycles

FRAME 20 IS CORRODED BEYOND LIMITS. REPAIRED.

Part: HOLDER — BROKEN (COCKPIT) · airframe 26,578 hrs · 23,794 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 26,306 hrs · 23,612 cycles

FOR FLIGHT 2805 DURING PRE-FLIGHT INSPECTION THE CAPTAINS FLASHLIGHT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CAPTAINS FLASHLIGHT AND PLACED IN CHARGING CRADLE AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,042 hrs · 23,436 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY POWER SUPPLY NR 4 AND THE EMERGENCY CHARGER ASSEMBLY NR 4 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY AND THE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04 IAW AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,901 hrs · 23,330 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY LIGHTS NR 6, 7, 8 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (NR 2 BRAKE) · airframe 25,383 hrs · 22,941 cycles

FOR FLIGHT 2932 THE GROUND CREW REPORTED THE LEFT MAIN GEAR SMOKING AND HYDRAULIC FLUID LEAK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BRAKE O-RING AT THE FORWARD END OF BRAKE HOSE IAW CMM 32-40-01. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,627 hrs · 21,701 cycles

WHILE PERFORMING MAINTENANCE FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB ON FORWARD RIGHT WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,874 hrs · 21,144 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT NR 3 EMERGENCY FLOOR PROXIMITY LIGHTING STRIPS TO BE INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMBRAER AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW EMBRAER AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (ANTI-ICE SYS) · airframe 21,150 hrs · 19,789 cycles

ON FLIGHT 3236 DURING CRUISE THE CREW REPORTED A STABILIZER ANTI ICE FAIL MESSAGE ON EICAS IN ICING CONDITIONS. THE CREW COULD NOT RESTORE OPERATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COMMAND RELAY FOR THE STABILIZER ANTI ICE IAW 30-10-51. OPERATIONAL CHECK WAS GOOD IAW AMM 30-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,883 hrs · 17,868 cycles

ON FLIGHT 4300, CREW REPORTED A ELECTRICAL BURNING ODOR FOR SHORT DURATION DURING CLIMB-OUT. ODOR CONFINED TO COCKPIT AND WAS NOTED BY CAPT AND F/O. NO VISIBLE SMOKE AND NO SYSTEM ANOMALIES. AIRCRAFT REMOVED FROM SERVICE. CHECKED COCKPIT LIGHTING-CONTROLS, CIRCUIT BREAKERS PANELS AND DISTRIBUTION BOXES. PERFORMED HI POWER RUN CHECKED BOTH PACKS ON APU AND USING ENGINE BLEEDS. CHECKED ANTI ICE SYSTEM AND WINDSHIELD HEAT, CHECKED AVIONICS FANS FOR OPERATION AND DEBRIS. ALL SYSTEMS CHECKED GOOD AND NO ELECTRICAL ODOR NOTICED. NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,283 hrs · 17,360 cycles

ON FLIGHT 3631, CREW REPORTED PRESS LOSS ON DECENT. COULD NOT MAINTAIN PRESS, EXECUTED EMERGENCY DECENT AND DEPLOYED O2 MASK. F/A REPORTED SMOKE ODOR DURING DECENT, THEY DIVERTED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01 AND CPAM IAW AMM 21-32-01. REMOVED AND REPLACED O2 MASKS. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,921 hrs · 17,028 cycles

DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BY CROSSMEMBER AT FRAME 24-25. REPAIRED RIGHT OMEGA BEAM IAW SRM 53-00-10 FIGURE 203. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON FLIGHT 4123 CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. ACFT REMOVED FROM SERVICE C/A. R&R NR 1 BATTERY PACK. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

ON FLIGHT 4272, MAINTENANCE REPORTED EMERGENCY EXIT SIGN OVER FLIGHT ATTENDANTS JUMP SEAT, CEILING LIGHT BY GALLEY AND LIGHT BY STEP UP TO FLIGHT DECK INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY (HOLDER AND ELECTRONIC ASSY) NR 1 IAW EMB AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: UNKNOWN — UNKNOWN (NLG) · airframe 18,196 hrs · 17,998 cycles

RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE, RETURNED TO DFW. RESERVICED NOSE LANDING GEAR IAW EMB AMM 32-20-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (RT MLG) · airframe 14,608 hrs · 14,036 cycles

LOUD CLUNKING NOISE HEARD ON CLIMB-OUT, DIVERTED TO ABI. INSPECTED BOTH RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCHES HARNESS WITH NO DEFECTS NOTED. REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCHES IAW EMB AMM 32-61-01. OPERATIONAL CHECK GOOD IAW AMM 32-63-05. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,086 hrs · 12,806 cycles

FOUND CARGO ENTRANCE SILL CORRODED. REMOVED AND REPLACED SILL, CLEANED AND TREATED IAW EMB SRM 51-20-03 AND 51-21-04. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — INOPERATIVE (AIR COND SYS)

AFTER ENGINE STARTS, AND RESELECTING BOTH PACKS ON, IMMEDIATELY GOT SMOKE IN THE COCKPIT. REPLACED LT AIRCYCLE MACHINE AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: BRAKE — SEIZED (RT MLG)

DURING LANDING CREW REPORTED BRAKES PULL TO RIGHT. DURING ROLL OUT, REPORTED THUMPING ON RT SIDE OF AIRCRAFT. MAINTENANCE REPORTED THAT BOTH NR 3 AND 4 BRAKES WERE SEIZED. REPLACED BOTH RT MLG WHEEL AND TIRE ASSEMBLIES AND BOTH BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: BRAKE — SEIZED (RT MLG)

DURING LANDING, CREW REPORTED BRAKES PULL TO RIGHT. DURING ROLL OUT, REPORTED THUMPING ON RT SIDE OF AIRCRAFT. MAINTENANCE REPORTED THAT BOTH NR 3 AND NR 4 BRAKES WERE SEIZED. REPLACED BOTH RT MLG WHEEL AND TIRE ASSEMBLIES AND BOTH BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 8,730 hrs · 8,423 cycles

DURING AN INSPECTION THE HOLDING STRINGER AT FRAME 50 AND STRINGER 13L WAS FOUND TO HAVE ONE DAMAGED HI-LOCK HOLE. REMOVED DAMAGED HOLDING STRINGER. INSTALLED NEW FASTENER IAW SRM. (SW21200502478) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,423 hrs · 8,730 cycles

DURING AN MBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502478) (K)

Part: SILL — CORRODED (SERVICE DOOR) · airframe 8,423 hrs · 8,730 cycles

DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL. INSTALLED NEW SILL IAW SRM. (SW2120050478) (K)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, REV 20) 53-24-02, AND STANDARD SRM PRACTICES. (M)