N941LT

Part: NONE — NO DISCREPANCY · airframe 44,461 hrs · 40,780 cycles

MULTIPLE BIRDSTRIKES ON AIRCRAFT. CLEANED REMAINS AND PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. REMAINS FOUND IN TAT SENSOR. CLEANED AND PERFORMED OPS CHECK IAW AMM 30-33-00. OPS CHECK GOOD. AC OK FOR SERVICE AT THIS TIME

Part: FILTER — BENT (AIR VALVE)

BLEED 2 OVER TEMP DURING CLIMB THRU 16K FOR ABOUT 5 SECONDS AND MESSAGE CLEARED AND RETURNED AFTER 5 SECONDS ALL DURING CLIMB IN ICEING CONDITIONS FOLLOWED FIM 36-11-00-810-804-1 TO STEP 2 FOUND FAN AIR VALVE FILTER TO BE BENT AND CRIMPED, R&R'D FILTER IAW AMM 36-11-03. OPS AND LEAK CHECKED IAW AMM 36-00-00. OPS CHECK GOOD LEAK CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY LIGHTS) · airframe 42,324 hrs · 38,349 cycles

EMER LT NOT ARMED AND ELEC EMERG ABNORMAL EICAS MESSAGES. FACT 21NOV24 15:08 CLT INSP'D, NO OBVIOUS DEFECTS NOTED. PERFORMED ELECTRICAL RESET AND EMER LIGHT TEST AMM 33-50-00 AND DC ELEC LOAD DISTRIBUTION TEST AMM 24-60-00. ALL TESTS PASSED. GROUND RAN ENGINES WITH NO DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 41,988 hrs · 37,971 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP. FOUND WIRES W717-0003-2 AND W717-0004-20 BROKEN. SPLICED WIRES IAW WM 33-50-50. OPS CHECK GOOD

Part: SKIN — CRACKED (ZONE 100) · airframe 41,803 hrs · 37,740 cycles

E047453 EXTERNAL FUSELAGE SKIN HAS A CRACK AT RH DV WINDOW CUTOUT AFT UPPER CORNER. ACCOMPLIHSED FCD1-53-23-0183 CRACK AT RH DV WINDOW CUTOUT AFT UPPER CORNER DAMAGE

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E047385 CARGO DOOR LOWER INBOARD L-PROFILE CORRODED AT NUTPLATE HOLES. REMOVED AND INSTALLED SERVICEABLE CARGO DOOR LOWER INBOARD L-PROFILE IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046446 CABIN LH LOWER FLOOR BEAM UPPER FLANGE CORRODED FROM FRAMES 28-29. RAR CABIN L/H LOWER FLOOR BEAM UPPER FLANGE (GUSSET) #2 IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046443 CABIN CENTER FLOOR BEAM UPPER FLANGE CORRODED AT FRAME 26. RAR CABIN CENTER FLOOR BEAM UPPER FLANGE (GUSSET) AT FRAME 26 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

CABIN LH #4 OB FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,803 hrs · 37,740 cycles

E046324 SHEER CLIP CRACKED AT FR66 BETWEEN STRGS 9L-8L. : ACCOMPLISHED REPAIR AT FR66 BETWEEN STRGS 9L-8L (SHEAR CLIP) IAW EMB 145 SRM 53-31-04

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046412 CABIN LH #3 OUTBD FLOOR SILL CORRODED. : RAR L/H # 3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046411 CABIN LH #2 OUTBD FLOOR SILL CORRODED. : RAR CABIN L/H # 2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046450 CABIN LH FLOOR BEAM CORRODED AT FRAME 29. ACCOMPLISHED PERMANENT REPAIR ON LH CABIN FLOOR BEAM AT FR 29 IAW EMB145 ETD2024-145-019932 AND EO1-53-24-0455

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046415 CABIN RH #1 OUTBD FLOOR SILL CORRODED. RAR CABIN RH #1 OUTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046416 CABIN RH #2 OUTBD FLOOR SILL CORRODED. : RAR #2 RH OUTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046419 CABIN RH #4 OUTBD FLOOR SILL CORRODED. RAR CABIN RH #4 OUTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046418 CABIN RH #3 OUTBD FLOOR SILL CORRODED. REMOVED AND REPLACED CABIN RH #3 OUTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046414 CABIN LH #5 OUTBD FLOOR SILL CORRODED. RAR LH #5 OUTBD FLOOR SILL IAW EMB145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046316 RH SIDE CABIN UPPER #4 SEAT TRACK IS CORRODED. RAR UPPER RH #4 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046309 LH SIDE CABIN UPPER #3 SEAT TRACK IS CORRODED. : REMOVED AND REPLACED DUE TO CORROSION EXTENSIVE AND BEYOND ALLOWABLE LIMITS ON LH SIDE CABIN UPPER #3 SEAT TRACK IAW EMB 145 SRM 53-00-11/AD

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,803 hrs · 37,740 cycles

E046328 SHEER CLIP CRACKED AT FR73 BETWEEN STRGS 10R-9R. REMOVED & REPLACED SHEER CLIP AT FR73 BETWEEN STRGS 10R-9R IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046219 CABIN LH #7 FLOOR SILL CORRODED. REMOVED AND REPLACED CABIN LH #7 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046317 RH SIDE CABIN UPPER #3 SEAT TRACK IS CORRODED. RAR UPPER RH #3 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046336 SERVICE DOOR LWR AFT CORNER SILL BRACKET CORRODED. RAR SERVICE DOOR LWR AFT CORNER SILL BRACKET IAW EMB 145 SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046342 GALLEY FWD DIGITAL CORRODED AT FR 15 NEAR PAX DOOR CUTOUT. ACCOMPLISHED REPAIR ON GALLEY FWD DIGITAL AT FR. 15 NEAR PAX DOOR CUT OUT IAW PIEDMONT ESR 1-53-24-004 AND PIEDMONT EO1-05-24-0470

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046335 SERVICE DOOR LWR SILL CORRODED AROUD SCREW HOLES. RAR SERVICE DOOR LWR SILL IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 500) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046308 LH SIDE CABIN UPPER #2 SEAT TRACK IS CORRODED. REMOVED AND REPLACED DUE TO CORROSION EXTENSIVE AND BEYOND ALLOWABLE LIMITS ON LH SIDE CABIN UPPER #2 SEAT TRACK IAW EMB 145 SRM 53-00-11/AD

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046221 CABIN RH #6 OUTBD FLOOR SILL CORRODED. RAR CABIN R/H #6 OUTBD FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046341 LH CROSSBEAM AT FR 18 CORRODED. : R & R L/H CROSS BEAM AT FR 18 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046172 RH CARGO FLOOR SILL CORRODED AROUND SCREW HOLES BTWN FR 65-68. RAR RH CARGO FLOOR SILL BTWN FR 65-68 IAW EMB 145 SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046173 LH CARGO FLOOR BEAM GUSSET CORRODED AT FR 65. RAR L/H CRAGO FLOOR BEAM GUSSET AT FR65 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E046168 CARGO DOOR CUTOUT SILL CORRODED. RAR THE CARGO DOOR CUTOUT SILL IAW EMB 145 SRM 51-40-02

Part: RIB — CRACKED (ZONE 500) · airframe 41,803 hrs · 37,740 cycles

E045630 LH WING RIB 21 IS CRACKED. PERFORMED CUTOUT, FABRICATED AND INSTALLED NEW FABRICATED DOUBLER AND FILLER FOR LH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIG 203 AND EO1-57-24-0467

Part: SKIN — DENTED (RUDDER) · airframe 41,803 hrs · 37,740 cycles

E045412 DENT ON RUDDER 2. INSTALLED SERVICABLE DOUBLER AND FILLER FOR REPAIR ON RUDDER 2 IAW EMB 145 ETD2024-145-019254 REV. "B" AND EO1-55-24-0431.

Part: NUT PLATE — MISSING (RUDDER) · airframe 41,803 hrs · 37,740 cycles

E045410 NUT PLATE ON RUDDER 2 MISSING. INSTALLED SERVICABLE DOUBLER AND FILLER FOR REPAIR ON RUDDER 2 IAW EMB 145 ETD2024-145-019254 REV. "B" AND EO1-55-24-0431.

Part: SUPPORT BRACKET — CRACKED (ZONE 800) · airframe 41,803 hrs · 37,740 cycles

E045329 PASSENGER DOOR INTERNAL HANDLE SUPPORT BRACKET CRACKED. RAR THE PAX DOOR INTERNAL HANDLE SUPPORT BRACKET IAW EMB 145 SRM 51-40-02

Part: RIB — CORRODED (ZONE 400) · corrosion level 2 · airframe 41,803 hrs · 37,740 cycles

E045282 CORROSION ON RH ENGINE UPPER COWLING CENTER RIB REINFORCEMENT 2 EACH. REMOVED AND REPLACED 2 CORRODED CENTER RIB REINFORCEMENTS (TRIANGLE GUSSETS) ON RH UPPER ENGINE COWLING IAW EMB 145 SRM 51-40-02, 51-20-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,746 hrs · 36,541 cycles

RUD SYSTEM 2 INOP EICAS MESSAGE DURING T/O ROLL AT ABOUT 60 KTS. R/R #2 HYD PRESSURE TRANSMITTER IRW AMM 29-30-02 OPS CHECK LEAK CHECK GOOD. PERFORMED HIGH POWER ENG RUN AS REQ OK FOR SERVICE AT THIS TIME

Part: LAMP — INOPERATIVE (LH) · airframe 40,600 hrs · 36,387 cycles

L/H EXTERNAL AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR L/H EXTERNAL AFT OVERWING EMERGENCY LIGHT LAMP, OPC GOOD, IAW AMM 33-50-10

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,488 hrs · 36,275 cycles

LH EXT OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH EXT OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,481 hrs · 36,271 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (OVERWING) · airframe 40,334 hrs · 36,113 cycles

LAMP INOP LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD.

Part: LAMP — ABNORMAL (EMERGENCY LIGHT) · airframe 40,156 hrs · 35,931 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD.

Part: SWITCH — FAULTED (DUCT OVERTEMP) · airframe 40,061 hrs · 35,828 cycles

BLEED 1 OVER TEMP DECLARED EMERGENCY -C/A-RAR PACK 1 DUCT OVERTEMP SWITCH IAW EMB-145 AMM 21-51-09. OPS CHECK GOOD NO DEFECT NOTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,934 hrs · 35,702 cycles

LH OVERWING EXTERIOR EMERGENCY LT INOP-C/A-RAR THE LH OVERWING EXTERIOR EMERGENCY LT LAMP IN REFRENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,915 hrs · 35,682 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK. END.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,824 hrs · 35,572 cycles

R/H OVERWING EMERGENCY EXIT SIGN INOP-C/A-RAR #5 EMERGENCY LIGHT INVERTER, OPC GOOD, IAW AMM 33-50-11

Part: LAMP — INOPERATIVE (LH) · airframe 39,582 hrs · 35,288 cycles

UPPER LH EMERGENCY LIGHT INOP-C/A-RAR UPPER LH EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPC GOOD

Part: LAMP — INOPERATIVE (LH) · airframe 39,314 hrs · 34,966 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RARLH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10 OPS CHECK GOOD

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 38,685 hrs · 34,255 cycles

FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN REFERENCE AML PAGE 4763289, ITEM 1 -C/A-RAR'D FWD FA EMERGENCY FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECK IS GOOD. MEL ITEM RESTORED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 38,674 hrs · 34,247 cycles

FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT HOLDER. M PROCEDURE C/W. MEL AUTH# 030247M-C REF# 25-32MOC# 628765

Part: NONE — NONE · airframe 38,664 hrs · 34,237 cycles

AFT FA EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT FA EMERGENCY FLASHLIGHT. M PROCEDURES C/W. MEL AUTH# 030214M-C REF# 25-32 MOC# 628765

Part: NONE — NONE · airframe 38,466 hrs · 34,017 cycles

AFT CABIN EMERGENCY FLASHLIGHT WILL NOT CHARGE-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD. END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,391 hrs · 33,925 cycles

DURING PS-1 LH AFT EMRGENCY LIGHT INOP-C/A-RAR AFT EMRGENCY LIGHT IAW 33-50-10 OPS CHECK GOOD

Part: NONE — NONE · airframe 38,378 hrs · 33,914 cycles

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

Part: NONE — NONE · airframe 38,378 hrs · 33,914 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 38,306 hrs · 33,839 cycles

FLIGHT ATTENDANT SAYS THAT THE MAIN CABIN DOOR IS ABNORMALLY HARD TO OPEN.-C/A-CLEAN AND LUBRICATE THE MAIN-DOOR FRAME ROLLERS IAW 145 AMM 53-21-02 OPS CHECK GOOD

Part: NONE — NONE · airframe 38,258 hrs · 33,780 cycles

UPPER LH WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED UPPER LH WING EMERGENCY LIHGT LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: NONE — NONE · airframe 38,209 hrs · 33,724 cycles

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

Part: NONE — NONE · airframe 38,150 hrs · 33,655 cycles

DURING PS2 FOUND LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10 OPC GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,937 hrs · 33,415 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 37,935 hrs · 33,411 cycles

LH OVERWING LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: ROLLER — SEIZED (THRUST LEVER) · airframe 37,852 hrs · 33,307 cycles

NO 1 ENGINE THRUST LEVER WILL NOT ADVANCE TO MAX THRUST DECLARED EMERGENCY. CLEANED AND FREED UP ROLLER ON RH POWER LEVER AND SLIDING ROD ASSEMBLY IN THE RH POWER LEVER IAW CMM 76-11-00, AND THEN FRICTION MOVEMENT OF LEVER CHECK GOOD IAW CMM 767-11-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,831 hrs · 33,281 cycles

LH OVERWING LATERAL PANEL EMERGENCY LIGHT IS INOP.-C/A-RAR LH OVERWING LATERAL PANEL EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,780 hrs · 33,227 cycles

LEFT EMERGENCY EXIT LIGHT INOP ON FUSELAGE EXTERIOR-C/A-RAR LEFT WING EMER EXIT LIGHT IAW AMM 33-50-04 OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,754 hrs · 33,201 cycles

ROW 11 EMERGENCY STRIP LIGHT INOP-C/A-RAR #3 EMERGENCY BATTERY IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. RAR EMERGENCY BATTERY CHARGER ASSEMBLY IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPC GOOD END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,754 hrs · 33,201 cycles

ROW 12A OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR ROW 12A OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: LIGHT — NO TEST (CABIN) · airframe 37,708 hrs · 33,146 cycles

DURING PS-1 CHECK, FOUND LH UPPER EMERGENCY LIGHT INOP-C/A-RAR LH UPPER EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,539 hrs · 32,954 cycles

LH EXTERNAL EMERGENCY LIGHT BULB INOP.-C/A-RAR LH EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10 OPS CHECK GOOD.

Part: FRAME — DAMAGED (FRM 67) · airframe 37,439 hrs · 32,842 cycles

FRAME 67 HAS 2EA ELONGATED HOLES AT THE END OF THE FRAME THAT CONNECTS TO CARGO DOOR SILL.-C/A-REPAIRED IAW SRM 53-00-04.

Part: FRAME — DAMAGED (FRM 66) · airframe 37,439 hrs · 32,842 cycles

FRAME 66 HAS 2EA ELONGATED HOLES AT THE END OF THE FRAME THAT CONNECTS TO CARGO DOOR SILL.-C/A-INSTALLED NEW FRAME SECTION AND SPLICE AT FR 66 IAW SRM 53-00-04 FIG 201.

Part: FLOOR SUPPORT — CRACKED (FRMS 66-67) · airframe 37,439 hrs · 32,842 cycles

CARGO DOOR SILL FLOOR SUPPORT ANGLES AT FRAME 66 AND 67 ARE CRACKED. -C/A-RAR CARGO DOOR SILL SUPPORT ANGLES AT FRAME 66 AND 67 IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRM 75 S1-3R) · airframe 37,439 hrs · 32,842 cycles

R/H FUSELAGE SKIN HAS A CRACK APROX 1/2 INCH LONG AT FR 75 BETWEEN STRS 1R AND 3R-C/A-REPAIRED RH FUSELAGE SKIN AT FR75 BETWEEN STR 1R AND 3R IAW SRM 53-31-01. ENTERED INTO DT # DT-EM-53-1367 AND DTEM-53-1368.

Part: SKIN — CRACKED (FRM 77 S4L) · airframe 37,439 hrs · 32,842 cycles

FUSELAGE SKIN HAS 6 CRACKS AT FR 77, 1ST RIVET UP FROM STR 4L. (1/32" LONG). FUSELAGE SKIN HAS 6 CRACKS AT FR 77, 1ST RIVET DOWN FROM STR 4L. (1/32" LONG). FUSELAGE SKIN HAS 2 CRACKS AT FR 77, 1ST RIVET UP FROM STR 6L. (1/32" LONG).. FUSELAGE SKIN HAS 1 CRACK AT FR 77, 1ST RIVET DOWN FROM STR 6L. (1/32" LONG). FUSELAGE SKIN HAS 4 CRACKS AT FR 77, 1ST RIVET DOWN FROM STR 8L. (1/16 LONG).-C/A-C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01.

Part: BUSHING — WORN (LT AILERON) · airframe 37,439 hrs · 32,842 cycles

LH AILERON OUTBD PCA BUSHINGS WORN. (MAJOR REPAIR)-C/A-RAR LH AILERON PCA FITTING IAW EO EM-27MR-112.

Part: SKIN — CRACKED (FRM 77 S3R) · airframe 37,439 hrs · 32,842 cycles

FUSELAGE SKIN IS CRACKED AT FR 77, 5TH RIVET DOWN FROM STR 3R. (1/16"LONG) - FUSELAGE SKIN IS CRACKED AT FR 77, 1ST RIVET DOWN FROM STR 4R. (1/16"LONG-C/A-C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01.

Part: ATTACH BRACKET — CRACKED (CARGO DOOR) · airframe 37,439 hrs · 32,842 cycles

CARGO DOOR LIFTING MECHANISM FORWARD ATTACH BRACKET IS CRACKED. -C/A-RAR BRACKET IAW SRM 51-40-02.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 36,987 hrs · 32,391 cycles

CREW REPORTS FWD F/A FLASHLIGHT HOLDER BROKEN. C/A: R & R FWD F/A FLASHLIGHT HOLDER, IAW AMM 33-50-16-04. OPERATIONS CHECK GOOD, IAW AMM 33-51-01.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,574 hrs · 31,956 cycles

MAIN ENTRY EMERGENCY EXIT PLACARD SIGN INOPERABLE. C/A: R & R INVERTER NR 1, IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPERATIONS CHECK GOOD.

Part: SEAL — LEAKING (SERVICE DOOR) · airframe 35,652 hrs · 31,100 cycles

SHORTLY AFTER TAKE OFF AT 240KTS THE F/A ADVISED THAT LOUD AIR NOISE AND VIBRATION COMMING FROM THE SERVICE DOOR. SLOWING THE AIRPLANE LESSENED THE NOISE AND VIBRATION-C/A-REMOVED STACK OF BLUE SECURITY STICKERS FROM SERVICE DOOR SEAL. CLEANED DOOR SEAL AS REQUIRED. PERFORMED FUNTIONAL CHECK AND INTEGRITY CHECK OF DOOR COMPONENTS IAW EMB 145MM 52-43-03. PERFORMED PRESSURIZATION CK OF A/C IAW EMB 145MM 21-31-00. OPS CK GOOD NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,606 hrs · 31,051 cycles

DURING PS-1 CHECK FOUND EXTERNAL LH EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED EXTERNAL LH EMERGENCY LIGHT ASSY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,024 hrs · 30,520 cycles

AFT AILE EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED AFT AILE EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801 AND 33-50-08-400-801 OPS CHECK GOOD

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,538 hrs · 30,077 cycles

FA REPORTS MAIN CABIN DOOR STICKING AND DIFFICULT TO OPEN. C/A-LUBED THE MAIN CABIN DOOR ADJUSTMENT AND TEST OK. REF AMM 52-10-01.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 34,312 hrs · 29,857 cycles

MAIN CABIN DOOR WAS JAMED FOR A FEW MINUTES WHEN FA TRIED TO OPEN. C/A-CLEANED AND LUBED DOOR ROLLERS DOOR OP CK GOOD IAW AMM 52-10-01 NO FURTHER DEFECTS NOTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 34,127 hrs · 29,618 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN/CLOSE, FOUND MAIN DOOR TO HAVE RECENTLY INSTALLED STOPS, ROLLERS, ETC. LUBRICATED AS NECESSARY. DOOR OPENS/CLOSES AND LATCHES SMOOTHLY AND SECURELY IAW AMM 52-18-00.

Part: DOOR SILL — DAMAGED (FRAMES 20-22) · airframe 33,744 hrs · 29,245 cycles

SERVICE DOOR SILL FROM FRAME 20 RT TO 22 RT AT FLOOR LEVEL HAS AREAS OF CORROSION. -C/A-REPAIRED SERVICE DOOR SILL FROM 20-22 RT AT FLOOR LEVEL IAW SRM 53-21-02.

Part: FITTING — CHAFED (LT AILERON) · airframe 33,744 hrs · 29,245 cycles

LH AILERON DAMPNER FITTING HAS CHAFING MARKS ON THE INSIDES OF TH FITTING. LH AILERON FITTING TO PCA HAS (2EA) INBD MIGRATED HAT BUSHINGS. -C/A-REMOVED AND REPLACED LH AILERON DAMPNER FITTING IAW EO-EM-27MR-112. RAR'D PCA ATTACH FITTING (INCLUDES HAT BUSHINGS) ON LH AILERON IAW EO-EM-27MR-112. FITTING P/N 145-69382-609

Part: BUSHING — MIGRATED (RT AILERON) · airframe 33,744 hrs · 29,245 cycles

RH AILERON DAMPER FITTING HAD MIGRATED HAT BUSHING. RAR RH AILERON DAMPER FITTING IAW EO- EM-27MR-112.

Part: FRAME — CORRODED (FRM 22) · airframe 33,744 hrs · 29,245 cycles

FRAME 22 RT CORRODED AT FLOOR LEVEL. C/W REPAIR OF FR 22R IAW SRM 53-00-04RE AND 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 33,744 hrs · 29,245 cycles

NUMEROUS SPOTS OF CORROSION ON CARGO SILL BETWEEN FRAMES 65 TO 68. -C/A-C/W RAR OF CARGO DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 33,744 hrs · 29,245 cycles

BAGGAGE DOOR MECHANISM FORWARD SUPPORT IS CRACKED. INSTALLED NEW SUPPORT IAW SRM 51-10-02.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 33,744 hrs · 29,245 cycles

FRAME 68 SHEAR CLIP BETWEEN STR 7L AND 8L HAS 1 CRACK. ( 1,5 INCH TOTAL CRACK LENGTH) -C/A-INSTALLED FR68 SHEAR CLIP IAW SRM 51-40-02

Part: INTERCOSTAL — CRACKED (NLG AREA) · airframe 33,744 hrs · 29,245 cycles

NLG FORWARD INTERCOSTAL CRACKED-C/A-REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 33,744 hrs · 29,245 cycles

FRAME 73 SHEAR CLIP AT STRINGER 10L HAS 2 CRACKS. (1.5 INCH TOTAL CRACK LENGTH)-C/A-REPLACED SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CRACKED (FRAME 68) · airframe 33,744 hrs · 29,245 cycles

CARGO DOOR HOLD OPEN SUPPORT REINFORCEMENT AT FRAME 68 STRINGER 15L HAS 2 CRACKS. (1 INCH IN LENGTH TOTAL)-C/A-REPLACED SUPPORT REINFORCEMENT IAW SRM 51-40-02

Part: LIGHT — DAMAGED (CABIN) · airframe 33,744 hrs · 29,245 cycles

FOUND FLOOR EMERGENCY LIGHT STRIPS SIDEWALL ASSEMBLIES CRACKED, CHIPPED AND BROKEN BROKEN. C/A-COMPLETE:RAR FLOOR EMERGENCY LIGHT STRIPS IAW AMM 33-50-12.

Part: CONNECTOR — BROKEN (CABIN) · airframe 33,744 hrs · 29,245 cycles

FOUND LAST:LT FLOOR PROXIMITY EMERGENCY LIGHT (CLOSES TO THE LAV DOOR) HAS A BROKEN CONNECTOR. C/A-COMPLETE:REPLACED FLOOR PROX EMERGENCY LIGHT CONNECTOR IAW SWPM 20-21-00.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 33,744 hrs · 29,245 cycles

LT FLOOR PROXIMITY EMERGENCY LIGHT (IN THE FLOOR) AT FRM54. CONNECTOR WILL NOT CONNECT WITH THE PROX LIGHT CONNECTOR. C/A-COMPLETE: REPLACED LT FLOOR PROX EMERGENCY LIGHT @ FR54 IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 33,744 hrs · 29,245 cycles

LT FLOOR PROXIMITY EMERGENCY LIGHT WIRE BROKEN AT FRM54. C/A-COMPLETE: REPAIRED LT FLOOR PROXIMITY EMERGENCY LIGHT WIRE IAW SWPM 20-21-00.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 33,663 hrs · 29,167 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. C/A-RAR SERVICE DOOR EMERGENCY DOOR LIGHT LAMP IAW 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,643 hrs · 29,147 cycles

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

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WING) · airframe 33,581 hrs · 29,088 cycles

WG A/ICE FAIL DURING PNEUMATIC TEST AIRBORNE. RECEIVED CMC MESSAGE WING 2 ANTI-ICE LEAK INSPECTED NR 2 ACM AREA AND WING ROOT FOR LEAKS NO LEAKS NOTED PERFORMED. OPS CHECK OF ANTI-ICING SYSTEM IAW AMM 30-00-00 OPS CK OK.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 33,138 hrs · 28,704 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-10 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,059 hrs · 28,618 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LAMP IN LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10-000-801-A

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 32,939 hrs · 28,486 cycles

LT OVERWING AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING AFT EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: CONDITIONER — FAILED (FUEL SYSTEM) · airframe 32,762 hrs · 28,317 cycles

UPON DEPARTURE THE RIGHT WING FUEL INDICATION WENT TO 0. FOUND REFUEL/DEFUEL PANEL SWITCH IN "BATTERY" POSITION UPON AIRCRAFT ARRIVAL CONFIGURED NORMALLY IAW AMM 12-11-01. TROUBLESHOT IAW FIM TASK 28-41-00-810-845-A WITH NO FAULTS FOUND, REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW AMM 28-41-01-000-801-A & 28-41-01-400-801-A. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,714 hrs · 28,267 cycles

FORWARD CABIN FLASHLIGHT NOT WORKING. -C/A-FOUND FLASHLIGHT TO BE BAD. REPLACED FLASHLIGHT IAW AMM 33-50-16. NO FURTHER DEFECTS NOTED. FLASHLIGHT OPERATES NORMALLY NOW.

Part: FLAP — OUT OF ADJUST (DOOR) · airframe 32,702 hrs · 28,259 cycles

MAIN SERVICE HAD VERY LOUD SQUEEL AFTER T/O FROM TOP OF DOOR. MAIN SERVICE DOOR INDICATED CLOSED ON MFD "TRANSFERRED TO NRWC 941-SGF-03683" JP678019-C/A-UPON INSP FOUND SIGNIFICANT GAP BETWEEN MAIN DOOR FAME AND FOLDING FLAP WHEN DOOR IS SHUT. PERFORMED MAIN DOOR FOLDING FLAP ADJUSTMENT. OPC GOOD PER AMM 52-18-00. FNC FOR CABIN LEAKAGE TEST GOOD PER AMM 21-31-00.

Part: CONTROLLER — LACK OF LUBE (BRAKE SYSTEM) · airframe 32,492 hrs · 28,067 cycles

CREW REPORTED PARKING BRAKE VERY DIFFICULT TO ENGAGE. LUBRICATED PARKING BRAKE CONTROL IAW AMM 32-44-10. OPS CHK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 32,424 hrs · 28,028 cycles

CARGO SMOKE INDICATION DURING FLIGHT, CARGO EXTINGUISHER DISCHARGED IAW AOM. INSPECTED THE CARGO BAY AND FOUND NO EVIDENCE OF SMOKE. REMOVED AND REPLACED THE SMOKE DETECTORS IAW AMM 26-15-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,266 hrs · 27,866 cycles

FOUND LT REAR EXTERNAL EMERGENCY LIGHT TO BE INOP. REPLACED LIGHT IAW AMM 33-50-10. OPS CHECK GOOD IAW AMM 33-50-00. NO FURTHER DEFECT NOTED.

Part: CONTROL UNIT — FAULTY (SPOILER SYS) · airframe 32,180 hrs · 27,800 cycles

INBND JAN DECLARED EMRG FOR SPOILERON FAIL IN FLIGHT. INTERROGATED CMC AND FOUND FAULT CODE GND SPLR ENG CKT FAULT AND SPBK LEVER SW/RELAY FAIL. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW AMM-27-63-02. OPCK GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 31,293 hrs · 26,883 cycles

FWD CABIN FLASHLIGHT CRADLE CRACKED. REMOVED AND REPLACED FWD CABIN FLASHLIGHT CRADLE ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A OPS CHECK GOOD AT THIS TIME END.

Part: UPLOCK — FAILED (NLG) · airframe 31,207 hrs · 26,797 cycles

LOUD RHYTHIMIC BANGING NOISE FROM NOSE WHEEL AREA AFTER RETRACTING GEAR ON TAKE OFF. GEAR INDICATED UP. NOISE WENT AWAY AFTER GEAR WAS DOWN. NO RELATED NLG CMC MESSAGES. REMOVED AND REPLACED NLG UPLOCK BOX IAW AMM 32-33-07. LANDING GEAR NORMAL AND EMERGENCY RETRACTION/EXTENSION CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,167 hrs · 26,759 cycles

LT AND RT OVERWING EXTERNAL LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 15271.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,167 hrs · 26,759 cycles

LT AND RT OVERWING EXTERNAL LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED LT AND RT OVERWING EXTERNAL LAMPS IAW AMM 33-50-10. OPS CHECK FAILED. CHARGER ASSY BATTER P/N BA5-0933-901 S/N C01638.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,117 hrs · 26,720 cycles

DURING A CHECK, FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY NR 4 IAW AMM 33-50-04. OPS CHECKED GOOD. NO DEFECTS NOTICED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,967 hrs · 26,577 cycles

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

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,967 hrs · 26,577 cycles

BOTH RT AND LT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R THE NR 4 POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04-000-801-A, AND 33-50-04-400-801-A, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,895 hrs · 26,510 cycles

SERVICE DOOR EMERGENCY LT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LAMP IN REFERENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FURTHER DISCREPANCIES FOUND. END.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,895 hrs · 26,510 cycles

BOTH EXTERIOR OVERWING EMERGENCY LTS INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY BATTERY AND POWER SUPPLY IAW ENVOY W/C 33-700-19 AND 33-700-17 OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 12701

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,890 hrs · 26,505 cycles

FOUND AFT EXTERIOR RH EMERGENCY LIGHT TO BE INOP DURING PS-1 CHECK-C/A-REMOVED AND REPLACED #4 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04-04. OPS CHECK GOOD

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,695 hrs · 26,341 cycles

LT AND RT AFT OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY AND CHARGER IAW WORKCARD 33-700-19 OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 19592.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 29,795 hrs · 25,359 cycles

EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. INSPECTED THE POWER SUPPLY AND FOUND THE BATTERY TO HAVE BECOME DISSCONNECTED. CONNECTED THE BATTERY, AND OPS CHECKED GOOD. WORK DONE IAW AMM 33-50-04-400-802-A. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 29,758 hrs · 25,316 cycles

NR 2 ENGINE SPOOLED DOWN AT GATE, ENGINE OUT EICAS CAUTION MESSAGE. START STOP SELECTOR WAS IN RUN POSITION AT THAT TIME. COMPLIED WITH FIM TASK 72-00-00-810-815 , FIM TASK 72-00-00-810-809 AND PERFORMED OPERATIONAL TEST OF ENGINE AT MAXIMUM POWER IAW MM 72-00-00, NO DEFECTS NOTED. PERFORMED DFDR DOWNLOAD, NO EVENTS NOTED. AIRCRAFT OKAY FOR RETURN TO SERVICE. PERFORMED NR 2 ENGINE STATIC CHECK IAW AMM 72-00-00, NO DEFECTS NOTED. PERFORMED GVI OF RH ENGINE SCAVENGE, AND OIL TANK CHIP DETECTOR IAW AMM 79-37-10, NO DEFECTS NOTED. ACCOMPLISHED RT ENGINE SCAVENGE AND OIL TANK CHIP DETECTORS LEAK CHECK IAW MM 72-00-00, NO LEAKS NOTED. PERFORMED NR 2 ENGINE RUN IAW FIM 79-37-00-810-805. OP CHECKED GOOD IAW FIM AT THIS TIME. ENGINE OKAY TO RETURN TO SERVICE

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,753 hrs · 25,312 cycles

FLASHLIGHT ABOVE FA JUMPSEAT DOEN NOT WORK. REPLACED THE FLASHLIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,600 hrs · 25,178 cycles

RT EXTERIOR FUSELAGE FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM 33-50-04 OPC GOOD. LIGHT EMERGENCY P/N 30-2510-3. BATTERY CHARGER ASSY P/N 11-0049 S/N 24446.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,317 hrs · 24,946 cycles

AFT LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD IAW AMM 33-50-10

Part: THERMOSTAT — FAILED (NR 1 ENGINE) · airframe 29,172 hrs · 24,793 cycles

BLEED NR 1 OVERTEMP DURING CLIMB OUT OF 5,000FT. REMOVED AND REPLACED THE 1 ENGINE FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. OPS CHECKED GOOD.

Part: ECU — FAILED (TE FLAPS) · airframe 28,803 hrs · 24,465 cycles

FLAP LOW SPEED EICAS MSG FOLLOWED BY SPS ADVANCED MSG. WHEN FLAPS SELECTED ON APPROACH IN ICING CONDITIONS. DECLARED EMERGENCY.-C/A-DEFERRED FLAP CHANNEL 2, "M" PROCEDURE C/W.MEL 27-9 AUTH 120375DM-B MOC 607038. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW EMB AMM 27-53-02. OPS CHECK DONE IAW EMB AMM 27-53-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED. REFERENCE NRWC 941-ORD-02782

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,759 hrs · 24,423 cycles

DURING OPERATION CHECK OF THE EMERGENCY LIGHTING SYSTEM, FOUND CEILING PANEL 253BLC AFT EMERGENCY EXIT LOCATOR SIGN INOP. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED CEILING PANEL 253BLC AFT EMERGENCY EXIT LOCATOR SIGN DC TO AC INVERTER 4 IAW AMM 33-50-11. OPERATIONAL CHECK GOOD. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,759 hrs · 24,423 cycles

DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, FOUND PAX DOOR EMERGENCY LIGHT INOP. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND THE FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER AT FR78 LT BETWEEN STGR 5L-6L. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. INSTALLED BUSHING ON FUSELAGE EXTERNAL SKIN AT FR 78 LT SIDE BETWEEN STGR 5L-6L IAW SRM 53-32-01RE SECTION 9 AND ETN-EM-53-194 AND EM-53-276. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND CRACKS AROUND ONE FASTENER AT FR 78 BETWEEN STGR'S 5R AND 6R. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR BY INSTALLING A BUSHING ON RT FUSELAGE EXTERNAL SKIN AT FR 78 BETWEEN STGR 5R AND 6R IAW SRM 53-32-01RE SECTION 9 AND ETN EM-53-194 AND EM-53-276. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND CRACKS AROUND ONE FASTENER AT FR 77 BETWEEN STGR 3R AND 4R. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR BY INSTALLING A BUSHING ON FR 77 BETWEEN STGR 3R AND 4R IAW SRM 53-32-01RE SECTION 9 AND ETN EM-53-194 AND EM-53-276. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND CRACKS AROUND NUT PLATE HOLES ON LAV LT FLOORBEAM, ONE AT FR 59 AND ONE AT FR 61. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REPAIRED CRACKS AT NUT PLATE HOLES AT FR 59 AND FR 61 ON LAV LT FLOORBEAM IAW SRM 53-24-10RE SECTION 3. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. (REPAIR MATERIALS: 2 DOUBLERS AL 2024 T3 0.063)

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND CORROSION ON THE CENTER HAT BEAM AT FR 20. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED CENTER HAT BEAM BETWEEN FR16 AND FR23 IAW SRM 51-40-02 AND 51-40-03. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. (REPAIR PART 145-21713-605)

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QA FOUND CORROSION ON CARGO DOOR STRUCTURE UPPER NUT PLATE HOLES. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED CARGO DOOR STRUCTURE UPPER NUT PLATE PROFILE IAW SRM 51-40-02. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. (REPAIR PART 145-31544-601 )

Part: FITTING — CRACKED (LT ENGINE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QC FOUND LT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED LT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. (REPLACEMENT FITTING PN 145-29426-004)

Part: FITTING — CRACKED (RT ENGINE) · airframe 28,759 hrs · 24,423 cycles

DURING IMBV INSPECTION, QC FOUND RT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED RT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. (REPLACEMENT FITTING PN 145-29426-003)

Part: MOUNT — CRACKED (RT ENGINE) · airframe 28,759 hrs · 24,423 cycles

RT ENGINE FWD ENGINE MOUNT HAS POSSIBLE CRACK. REMOVED AND REPLACED RT ENGINE FWD LWR ENGINE MOUNT YOKE IAW EO EM-54MR-386.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,759 hrs · 24,423 cycles

MID CENTER CEILING AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID CENTER CEILING AFT EMERGENCY LIGHT NR 4 INVERTER. OPERATIONAL CHECK GOOD IAW AMM 33-50-11, 33-50-00

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,560 hrs · 24,232 cycles

WIRE ON EMERGENCY FLOOR LIGHT STRIP BROKEN AT ROW 6A. R & R EMERGENCY FLOOR LIGHT STRIP AT ROW 6A IAW AMM 33-50-12 OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,529 hrs · 24,202 cycles

FWD EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHTING SYSTEM POWER SUPPLY NR 1 IAW WC 33-700-19. OPS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,451 hrs · 24,133 cycles

MAIN PASSENGER DOOR EXTERNAL EMERGENCY LIGHT FAILS TO ILLUMINATE. CLEANED GROUND ON EMERGENCY LIGHT ON PAX DOOR IAW STANDARD PRACTICES, OPS CHECK GOOD. MEL RESTORED.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 27,941 hrs · 23,661 cycles

ON APPROACH, EICAS INDICATED LAV SMOKE, F/A NOTIFIED BY ALARM, LAV SMOKE, RAN TO LAVATORY, SAW PASSENGER EXITING LAV, F/A SMELLED SWEET VAPOR IN LAV. NO OTHER SIGN OF ODOR OR SMOKE. TRANSFERRED TO NRWC 941-DFW-02571. R & R LAV SMOKE DETECTOR SENSOR IAW AMM 26-14-01. OPS GOOD IAW AMM 26-14-00-700-803-A. NO EVIDENCE OF SMOKE NOTED AT THIS TIME. REF NRWC 941-DFW-02572 FOR ADDITIONAL WORK DONE.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 27,791 hrs · 23,513 cycles

EMERGENCY LIGHTS ON AFTER BATTERIES OFF WITH EMER LIGHTS SWITCH IN OFF POSITION. SHUT OFF GPU & REBOOTED ACFT APU, EMER LIGHTS WENT OFF AFTER SHUTTING OFF ALL ACFT POWER. OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 27,741 hrs · 23,462 cycles

DESCENT LOSS OF AIRSPEED INDICATIONS ON FIRST OFFICERS PFD. PERFORMED OPERATIONAL CHECK OF AIR DATA COMPUTER SYS IAW AMM 34-15-00. OPERATIONS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (CARGO DOOR) · airframe 27,663 hrs · 23,386 cycles

DURING ROLL AT APPROX 90 KTS EICAS BAGGAGE DOOR OPEN MSG. CLEARED DURING ABORT. FLIGHT CREW PLACARDED BAGGAGE DOOR WARNING SYS MEL 52-05. R&R BAGGAGE DOOR WARNING REAR MICRO SWITCH. OPERATIONS CHECKED GOOD IAW AMM 52-76-01. MEL ITEM RESTORED.

Part: CONNECTOR — LOOSE (ELECTRICAL SYS) · airframe 27,505 hrs · 23,239 cycles

AFTER TAKEOFF, ELEC EMER ABNORM, ON EICAS. ACCOMPLISHED THE CHECKLIST & LANDED AT AIRPORT. ELEC EMER ABNORM, MSG REMAINED ON THROUGHOUT FLIGHT. EMER LIGHT NOT ARMED, MSG ALSO ON FOR FLIGHT. BOTH MSGS CAME ON AFTER TAKEOFF. TIGHTENED CONNECTOR P1153, BATTERY 1 RELAY BOX, 4 QUARTER URNS, P1143 3 QUARTER URNS, BACKUP BATTERY RELAY BOX. DC ELEC DISTRIBUTION LOAD CHECKS ARE GOOD IAW MM 24-60-00. NO RECENT GRIPES. EMER LIGHTS OPERATIONS CHECKED GOOD IAW AMM 33-50-00. MSG NEVER SHOWED ON GND.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,498 hrs · 23,233 cycles

EXTERNAL OVERWING EMER LIGHTS INOPERATIVE. TROUBLE SHOT IAW FIM TASK 33-50-00-810-804-A. FOUND NR 4 BATTERY & CHARGER TO BE BAD. R & R NR 4 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME ENDS. EMER LIGHT BATTERY, PN 2013-1A & SN 108110.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,282 hrs · 23,023 cycles

LEFT & RIGHT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 11448.

Part: CHARGER — FAILED (CABIN) · airframe 27,155 hrs · 22,913 cycles

LEFT & RIGHT EXTERIOR OVERWING EMER LIGHTS FAILED TO ILLUMINATE. R & R NR 4 EMER LIGHT CHARGER ASSEMBLY & BATTERY ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED IAW AMM 33-50-0. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A & SN 125752.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,051 hrs · 22,814 cycles

OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 17641.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,891 hrs · 22,672 cycles

FIRST OFFICERS FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 26,330 hrs · 22,189 cycles

ON APPROACH CREW RECEIVED SPOILER FAIL MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & LANDED WITHOUT INCIDENT. PERFORMED SPOILER SYS OPS CHECK IAW AMM 27-63-01. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,129 hrs · 21,007 cycles

SEAT 12A OVERWING EMER LIGHT INOPERATIVE. R & R OVERWING EMER LIGHT LAMP AT SEAT 12A IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,727 hrs · 20,671 cycles

BIRD STRIKE DAMAGE TO RT FWD FUSELAGE I SKINS. REPAIRED BIRD STRIKE DAMAGE TO RT FWD FUSELAGE I IAW ERS-EM-53MR-1014 PART B. FWD FUSELAGE UPPER PN 145-50543-401.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,727 hrs · 20,671 cycles

BIRD STRIKE DAMAGE TO LT FWD FUSELAGE I SKINS. REPAIRED LT FWD FUSELAGE I BIRD STRIKE DAMAGE IAW ERS-EM-53MR-1014 PART A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,727 hrs · 20,671 cycles

BIRD STRIKE DAMAGE TO LT FWD FUSELAGE I SKINS. REPAIRED LT FWD FUSELAGE I BIRD STRIKE DAMAGE IAW ERS-EM-53MR-1014 PART A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,727 hrs · 20,670 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R LIGHT LAMP IAW AMM 33-50-06. OPERATIONALLY CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,727 hrs · 20,670 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06. OPERATIONS CHECKED GOOD.

Part: ECU — FAILED (TE FLAP) · airframe 24,336 hrs · 20,353 cycles

ON APPROACH AT MLI SELECTED FLAPS 45 DEGREES THE FLAP TOOK A LONG TIME TO COME DOWN. AFTER THEY GOT TO 40 DEGREES GOT FLAP LOW SPEED MSG. 50 FT BEFORE LANDING GOT FLAP FAIL MSG. ELECTED TO LAND INDICATED 45 DEGREES. R & R FECU IAW AMM 27-53-02. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,314 hrs · 20,337 cycles

WITH FLAP LEVER SET TO 45 DEGREES & EICAS FLAP INDICATION AT 45 RECEIVED FLAP FAIL CAUTION ON EICAS. FOUND TO BE TRANSITORY CONDITION IAW FIM 27-51-00-810-808-A. OPERATIONS CHECK FLAPS IAW AMM 27-51-00. OPERATIONS CHECK MSG CLEARED. OK FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 24,312 hrs · 20,335 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,213 hrs · 20,261 cycles

FLAP LOW SPEED MSG ON EICAS ON APPROACH. RAN FLAPS THRU REACH DENT COMPLIED WITH OPERATIONS CHECK IAW AMM 27-51-00. OPERATIONS CHECK COMPLETED. NO DEFECTS OR MSGS NOTED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 24,180 hrs · 20,230 cycles

DURING MBV INSPECTION QA FOUND FRAME 65 SHEAR CLIP CORRODED AT LOWER FWD CORNER OF CARGO DOOR CUT OUT & CHAFE BETWEEN STRINGER 14L & 15L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FRAME 65 SHEAR CLIP IAW ERS-EM-53MR-787. SHEAR CLIP 145-25178-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,180 hrs · 20,230 cycles

DURING MBV INSPECTION, QA FOUND LT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-788. REPAIR MATERIALS FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .063 & ANGLE FILLER 2024T3 .032.

Part: DOOR — DENTED (CABIN) · airframe 24,180 hrs · 20,230 cycles

TRANSFERRED FROM LGPG 3513285 TDMI 941T5210. PERFORM PERMANENT REPAIR TO DENT ON MAIN DOOR 6 INCHES DOWN FROM GRAB HANDLE & 9 1/2 INCHES IN FROM AFT EDGE AT NEXT MBV. TRANSFERRED TO NRTC E404243. RE-CONTOURED DENT ON MAIN PAX DOOR IAW ERS-EM-52DF-179. TDMI RESTORED. SEE NRTC E404243 FOR DETAILS.

Part: DOOR — DENTED (CABIN) · airframe 24,180 hrs · 20,230 cycles

ERS-EM-52DF-179 PART D MAIN DOOR DENT PERMANENT REPAIR. CONTOURED MAIN DOOR DENT IAW ERS-EM-53DF-179 PART D. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,180 hrs · 20,230 cycles

LEFT OVERWING PANEL UPPER FUSELAGE SUPPORT CRACKED BETWEEN FRAME 41 & 42. REPAIRED IAW SRM 53-23-12. SEE TURNOVER FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,180 hrs · 20,230 cycles

CABIN LT FLOORBEAM INBD SUPPORT CRACKED AT AFT END. R & R CABIN LT FLOORBEAM INBD SUPPORT IAW SRM 53-23-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,180 hrs · 20,230 cycles

FLOOR PROXIMITY LIGHT STRIP CONNECTOR NR 5 BROKEN INSIDE CABIN. REPAIRED FLOOR PROXIMITY LIGHT STRIP CONNECTOR NR 5 IAW SWPM 20-21-00 STEP 5. SEE NRTC E409709 FOR OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 23,426 hrs · 19,638 cycles

RIGHT AFT OVERWING EMER LIGHT INOPERATIVE. R & R RT AFT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: DETECTION SYS — MALFUNCTIONED · airframe 23,320 hrs · 19,554 cycles

ICE DETECTORS DID NOT DETECT ICE WITH VISIBLE ICE ON AIRFRAME. PERFORMED ICE DETECTION SYS OPS TEST IAW AMM 30-80-00. OPS CHECKED GOOD.

Part: PITOT SYSTEM — CONTAMINATED (P1) · airframe 23,320 hrs · 19,554 cycles

CAPTAIN`S AIRSPEED DIVERGE BY ABOUT 80KTS LOWER THAN ISIS & FIRST OFFICER`S AIRSPEED. DRAINED P1 PITOT DRAIN. OPERATIONS CHECKED OK IAW AMM CH 34-13-00. THIS ACFT REMAINS RVSM ELIGIBLE & ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATION.

Part: FLAP — MALFUNCTIONED (WING) · airframe 23,301 hrs · 19,536 cycles

DURING APPROACH TRANSITIONING TO FLAPS 45 RECEIVED EICAS MSG FLAP FAIL, FLAPS INDICATE 39 ON EICAS. RESET FLAPS IAW FIM 27-51-00. PERFORMED OPERATIONS CHECK IAW AMM 27-51-00 OPERATIONS CHECKED GOOD.

Part: ROD — DAMAGED (DOOR GATE) · airframe 21,828 hrs · 18,375 cycles

MAIN CABIN DOOR WAS BOUND SHUT. MAINTENANCE HAD TO OPEN. R & R MAIN DOOR FLAP ACTUATING ROD. OPS CHECK GOOD IAW AMM 52-18-02, RII: 680941.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,395 hrs · 18,013 cycles

FLOOR EMERGENCY EXIT LIGHT AT SEAT ROW 10+11 IS INOPERATIVE. R & R NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,395 hrs · 18,013 cycles

FLOOR EMERGENCY EXIT LIGHT AT SEAT ROW 8 - 9 INOPERATIVE. R & R LIGHT IAW AMM 33-50-13. ACFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 21,291 hrs · 17,928 cycles

F/A REPORTS MAIN DOOR HARD TO OPEN/CLOSE. CLEANED & LUBBED MAIN DOOR ROLLERS IAW MM 52-18-05. OPS CK OF DOOR GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,170 hrs · 17,821 cycles

WHEN GPU POWER WAS REMOVED FROM ACFT, EMERGENCY LIGHTS ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. RECHARGED EMERGENCY BATTERIES IAW CMM 25-60-03 FOR 3.5 HRS AND OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECKED GOOD NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 20,289 hrs · 17,099 cycles

ON FLIGHT 4369 THE CREW REPORTED THEY RECEIVED A LAV SMOKE EMERGENCY INDICATION ON INITIAL CLIMB. THE CREW COMPLETED MEMORY ITEMS, EPC AND AOM VOL 1 PROCEDURES. AN EMERGENCY WAS DECLARED AND AN IMMEDIATE RETURN TO LANDING WAS MADE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE FLIGHT ATTENDANT REPORTED NO VISIABLE INDICATION OF FIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAV SMOKE SENSOR. THE OPERATIONAL CHECK WAS GOOD IAW AMM 26-14-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDSET — DEFECTIVE (CABIN) · airframe 19,948 hrs · 16,833 cycles

ON FLIGHT 3359 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS ON THE HANDSET BOTH LIGHTS REMAIN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT HANDSET PER AMM 23-31-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,852 hrs · 16,752 cycles

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

Part: STRIP — WRONG PART (CASBIN) · airframe 19,762 hrs · 16,679 cycles

ON FLIGHT 2703 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING STRIP NEAR OVERWING EXIT WAS THE WRONG SIZE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP PER EMB AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,704 hrs · 16,636 cycles

DURING B INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIP INOPERABLE AT SEAT 10A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP AT 10A IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,618 hrs · 16,563 cycles

DURING B INSPECTION FOUND THE GALLEY AFT DIAMOND GUSSETT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY AFT DIAMOND GUSSETT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 19,618 hrs · 16,563 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIP WIRE ON AIRCRAFT SIDE AT CENTER AISLE FLOORBOARD 251FF BROKEN. REPAIRED THE FLOOR EMERGENCY LIGHT STRIP WIRE ON AIRCRAFT SIDE AT CENTER AISLE FLOORBOARD 251FF IAW EMB145 WM 20-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,618 hrs · 16,563 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LAMP IAW EMB145 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,618 hrs · 16,563 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR CENTER FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER FLOOR SILL IAW EMB SRM 51-40-02, CPM 51-21-04, CPM 51-21-05, CPM 51-21-06, AEA ETN-EM-51-016R2, ETN-EM-51-075 AND ETN-GN-51-091R2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,618 hrs · 16,563 cycles

DURING B INSPECTION FOUND THE GALLEY FORWARD DIAMOND GUSSETT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY FORWARD DIAMOND GUSSETT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 19,618 hrs · 16,563 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 5 AND 6 CONNECTORS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE EMERGENCY LIGHT STRIP NR 5 AND 6 CONNECTORS IAW EMB 145 SWPM 20-21-00 AND 20-00-03. PERFORMED OPERATIONAL CHECK IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (FLASHLIGHT) · airframe 19,397 hrs · 16,395 cycles

ON FLIGHT 4224 THE CREW REPORTED THE CAPTAIN'S COCKPIT FLASHLIGHT WAS NOT CHARGING AND THE LIGHT WAS DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S COCKPIT EMERGENCY FLASHLIGHT BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW DME CMM 25-60-11 TASK 4. & 5. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 19,152 hrs · 4,111 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT MISSING. FLASHLIGHT INSTALLED IAW STAND MAINTENANCE PRACTICES MEL ITEM RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOOT — UNSERVICEABLE (SPOILER) · airframe 19,071 hrs · 16,142 cycles

ON FLIGHT 4291 THE CREW REPORTED, RECEIVED A "SPOILER FAIL" MESSAGE IN FLIGHT WHILE THRUST LEVERS AT FLIGHT IDLE FLAPS 9 DEGREES SPEED BRAKE HANDLE CLOSED. AIRSPEED AT 180 KTL-GEAR UP- WENT AROUND ON APPROACH. AT THRUST LEVERS ADVANCED SPOILER FAIL SELF CANCELLED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED INBOARD SPOILER PROXIMITY SWITCHES WITH GSE 212, NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK IAW EMB AMM 27-63-01. NO DEFECTS NOTED. REMOVED AND REPLACED THE HEAT SHRINK BOOT (90 DEGREES). THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 19,028 hrs · 16,103 cycles

ON FLIGHT 4159 THE CREW REPORTED THE FLIGHT ATTENDANT REAR FLASHLIGHT HOLDER WAS NOT HOLDING THE FLASHLIGHT SECURELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT F/A FLASHLIGHT ASSEMBLY PER EMB M/M 33-50-16. THE OPERATIONAL CHECK WAS GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 18,746 hrs · 15,866 cycles

FLIGHT 3578, CREW REPORTED THE CRADLE FOR CAPTAINS FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,482 hrs · 15,648 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING AFT EXT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING AFT EXIT EMERGENCY LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,011 hrs · 15,286 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OVER THE WING EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,923 hrs · 15,216 cycles

DURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CABIN FLASHLIGHT AND BATTERY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — CORRODED (BRAKE TEMP) · airframe 17,528 hrs · 14,890 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 MAIN LANDING GEAR BRAKE TEMPERATURE SENSOR SEVERELY CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 MAIN LANDING GEAR BRAKE TEMPERATURE SENSOR DUE TO CORROSION IAW EMB AMM 32-47-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,188 hrs · 14,635 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 8 AND 11 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND NR 3 BATTERY CHARGER INOPERABLE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,176 hrs · 14,626 cycles

ON FLIGHT 4110 THE CREW REPORTED THAT ON SHUTDOWN AT THE GATE THE EMERGENCY LIGHT STRIP BETWEEN ROW 8 AND ROW 11 DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK AS REQUIRED IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,525 hrs · 14,153 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 2 EMERGENCY LIGHTING SYSTEM FAILED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING SYSTEM BATTERY NR 2 IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 16,018 hrs · 13,725 cycles

ON FLIGHT 4032 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT FAILED TO TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB MM 33-50-16-000-801-A & EMB MM 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — UNSERVICEABLE (NR 1) · airframe 15,774 hrs · 13,535 cycles

ON FLIGHT 4084 THE CREW REPORTED THAT WHILE CLIMBING THROUGH 7500 FEET HEARD A LOUD BOOM. ENGINE 1 AUTO SHUT DOWN AND WITH ENGINE 1 OUT AND ASSOICATED EICAS MESSAGES THE CREW DECLARED AN EMERGENCY. THE CREW RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NO FIRE, SMOKE OR FUMES WERE REPORTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW EMB WC 71-000-00. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 12,740 hrs · 11,262 cycles

FOR FLIGHT 2853 DURING MAINTENANCE CHECK FOUND THE EMERGENCY LIGHTS FROM NR 2 BATTERY DIM AND DRAINING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY POWER SUPPLY UNIT CHARGER IAW W/C 33-700-19 THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAULTY (BRAKE SYS) · airframe 12,745 hrs · 11,267 cycles

FOR FLIGHT 3336 DURING TAXI THE CREW REPORTED A BRAKE DEGRADE MESSAGE ILLUMINATED FOLLOWED BY A FIRM BRAKE GRABBING ON THE RIGHT SIDE. THE MESSAGE EXTINGUISHED 2 SECONDS LATER. THE AIRCRAFT RETURNED TO THE BLOCK AND WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT IAW AMM 32-41-00. REMOVED AND REPLACED NR 1 WHEEL SPEED TRANSDUCER IAW EMB 145 AMM 32-41-03. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,704 hrs · 11,229 cycles

ON FLIGHT 3448 DURING TAXI THE CREW REPORTED THE FIRST STRIP OF EMERGENCY FLOOR LIGHT ILLUMINATED WHEN EMERGENCY LIGHT SWITCH WAS ARMED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 2 POWER SUPPLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — UNSERVICEABLE (NR 1 AGB) · airframe 7,391 hrs · 6,704 cycles

ON FLIGHT 3738, DURING TAKEOFF CREW REPORTED STRONG BURNING OIL SMELL ON CLIMB-OUT, PACKS ON, BLEEDS ON. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE AGB BREATHER CARBON SEAL IAW 72-63-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — FAILED (NR 2) · airframe 7,321 hrs · 6,656 cycles

ON FLIGHT 3386, OPERATIONS CALLED MOC AND REPORTED FOD FOUND ON RUNWAY FROM TIRE DEBRIS AFTER FLIGHT 3386 DEPARTED FROM THE RUNWAY. SOC INFORMED CREW OF POSSIBLE TIRE DAMAGE IN FLIGHT. AIRCRAFT PERFORMED FLYBY AT DFW AND LANDED WITH THE NR 2 MAIN TIRE BLOWN, FLAPS WERE DAMAGED AND NO OTHER PROBLEMS NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 TIRE, REMOVED AND REPLACED E1 FAN BY-PASS VANES, E1 CONTAINMENT RING. TEMPORARY REPAIRED FLAP. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 4,948 hrs · 4,575 cycles

EMERGENCY LIGHTS AFT OF ROW ONE WILL NOT EXTINGUISH, OVERWING EMERGENCY LIGHTS ALSO ILLUMINATED. REMOVED AND REPLACED NUMBER FOUR EMERGENCY BATTERY PACK AND CHARGER IAW EMB AMM 35-50-04 AND 33-50-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 4,929 hrs · 4,546 cycles

DENT AT FRAMES 66 AND 67 AT STRINGER 14R. REPAIRED DENT IAW AMERICAN EAGLE ENGINEERING ORDER EM-53MR-785. RETURNED AIRCRAFT TO SERVICE.

Part: BLEED AIR SYS — LEAKING (NR 2 ENGINE) · airframe 4,516 hrs · 4,197 cycles

LAVATORY SMOKE WARNING MESSAGE ON TAKEOFF WHEN PACKS SELECTED ON, EMERGENCY DECLARED. RETURNED TO ORD. REMOVED AND REPLACED NR 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: CARBON SEAL — FAILED (ENGINE) · airframe 4,184 hrs · 3,882 cycles

LAVATORY SMOKE MESSAGE WITH A BLUE HAZE IN THE CABIN ON CLIMB-OUT, DECLARED EMERGENCY, RETURNED TO ORD. REMOVED AND REPLACED ZERO CARBON SEAL NUMBER 2.

Part: STRUCTURE — GROUND DAMAGE (PAX DOOR)

AIRCRAFT WAS STRUCK BY JETBRIDGE CAUSING DAMAGE TO PASSENGER ENTRY DOOR. AIRCRAFT WAS FERRIED TO MAINTENANCE. DOOR REPAIRED WITH AN EXTERNAL DOUBLER AT DAMAGE CORNER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)