N661JA

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 46,065 hrs · 40,990 cycles

EMERGENCY LILIGHTS FROM GALLEY TO SEAT 7A ARE INOP. RAR EMERGENCY BATTERY #200 IAW AMM 33-50-04

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 46,056 hrs · 40,978 cycles

BLEED 2 VALVE FAIL DURING T/O ROLL R & R NR 2 BLEED VALVE IAW AMM 36-11-05. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SERVICE AT THIS TIME.

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 46,055 hrs · 40,978 cycles

BLD 2 VLV FAIL DURING T/O ROLL. R & R #2 BLEED VALVE IRW AMM 36-11-05. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SERVICE4 AT THIS TIME

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F041443 SERVICE DOOR AFT SILL CORRODED AT UPPER ATTACHMENT FLANGE. REMOVED AND REPLACE SERVICE DOOR AFT SILL IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F040724 SHEAR CLIP IS CRACKED IN GALLEY AREA AT FRAME 15 BETWEEN STRINGER 15R-16R. REMOVED AND REPLACED SHEAR CLIP IN GALLEY AREA AT FRAME 15 BETWEEN STRINGER 15R-16R IAW EMB 145 SRM 51-40-02.

Part: SKIN SPLICE — CRACKED (ZONE 500) · airframe 44,968 hrs · 39,712 cycles

F040415 LH WING SPLICE 13 CRACKED. REMOVED AND REPLACED LH WING SPLICE 13 IAW EMB 145 SRM 51-40-02 IAW ETD2025-145-905692 REV B AND EO1-57-25-0168

Part: SKIN — MECHANIC ERROR (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F040237 MIS-DRILLED HOLE ON RH AFT DV WINDOW SKIN DURING ACCOMPLISHMENT OF PIEDMONT FCD 1-53-23-0183. REPAIRED MIS-DRILLED HOLE ON THE RH AFT DV WINDOW SKIN IAW EMB ETD-2025-145-906052 AND E01-53-25-0148

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F037450 SERVICE DOOR AIRCRAFT STRUCTURE CUT-OUT AFT LWR SIDE CORRODED. INSTALLED FR 22 REPAIR SECTION BTW STGR 11R-18R, FR 22 SPLICES, AND SHEAR CLIPS AT FR 22 BTW STGR 16R-17R AND 17R-18R IAW EMB 145 SRM 53-00-04 ITEM 17 ETD# ETD2025-145-906465 AND EMB 145 SRM 51-40-02 AND PIEDMONT EO1-53-25-0159.

Part: BULKHEAD — CHAFED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F037449 PILOT SIDE AFT BULKHEAD UPPER OTBD GUIDE PIN HOLE CHAFED. REPAIRED THE PILOT SIDE AFT BULKHEAD UPPER OTBD GUIDE PIN HOLE IAW EMB 145 SRM 53-21-02-RE, ITEM 4, FIGURE 204 AND EO1-53-25-0156

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F037275 SHEAR CLIP IS CRACKED IN GALLEY AREA AT FRAME 16 BETWEEN STRINGER 15R-16R. REMOVED AND REPLACED SHEAR CLIP IN GALLEY AREA AT FRAME 16 BETWEEN STRINGER 15R-16R IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036858 LH #6 FLOOR SILL CORRODED. RAR L/H #6 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036966 PASSENGER DOOR ENTRY FWD FLOORBOARD SUPPORT IS CORRODED. REMOVED AND REPLACED PASSENGER DOOR ENTRY FWD FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F036991 SHEAR CLIP CRACKED AT FR26 BETWEEN STRGS15R-16R. REMOVED AND INSTALLED NEW & SERVICEABLE SHEAR CLIP AT FR26 BETWEEN STRGS15R-16R IAW EMB-145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036776 CARGO DOOR CUTOUT LWR SILL HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR CUTOUT LWR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036818 CENTER FLOOR BEAM WEB CORRODED AT FR38. ACCOMPLISHED REPAIR OF CENTER CROSSBEAM AT FR38 IAW ETD2025-145-906383 AND EO1-53-25-0154

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036861 LH #4 SEAT TRACK GOUGED WITH PITTING CORROSION. RAR LH #4 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,968 hrs · 39,712 cycles

F036843 SHEAR CLIP CRACKED AT FR24 BETWEEN STRGS 16R-17R. REMOVED AND INSTALLED NEW & SERVICEABLE SHEAR CLIP AT FR24 BETWEEN STRGS 16R-17R IAW EMB-145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036857 LH #7 FLOOR SILL CORRODED. RAR LH #7 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F036990 SHEAR CLIP CRACKED AT FR25 BETWEEN STRGS15R-16R. REMOVED AND INSTALLED NEW &SERVICEABLE SHEAR CLIP AT FR25 BETWEEN STRGS15R-16R IAW EMB-145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F036989 SHEAR CLIP CRACKED AT FR24 BETWEEN STRGS15R-16R. REMOVED AND INSTALLED NEW & SERVICEABLE SHEAR CLIP AT FR24 BETWEEN STRGS15R-16R IAW EMB-145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036822 LH FLOOR BEAM LWR FLANGE CORRODED BETWEEN FR33-34. FABRICATED DOUBLER REPAIAR FOR LH FLOOR BEAM LWR FLANAGE, INSTALLED SERVICEABLE DOUBLER REPAIR ON LH FLOOR BEAM LWR FLANGE BETWEEN FR. 33-34 IAW EMB 145 SRM 53-22-10RE, ETD2025-145-905975 AND PIEDMONT EO1-53-25-0149.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F036992 SHEAR CLIP CRACKED AT FR27 BETWEEN STRGS15R-16R. REMOVED AND INSTALLED NEW & SERVICEABLE SHEAR CLIP AT FR27 BETWEEN STRGS15R-16R IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036820 LH CABIN FLOOR SILL #4 CORRODED. RAR L/H #4 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036855 RH #4 FLOOR SILL CORRODED. RAR R/H #4 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,968 hrs · 39,712 cycles

F036839 SHEAR CLIP CRACKED AT FR26 BETWEEN STRGS 16R-17R. INSTALLED NEW & SERVICEABLE SHEAR CLIP AT FR26 BETWEEN STRGS 16R-17R IAW EMB-145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036825 RH CABIN FLOOR SILL #3 CORRODED. RH CABIN FLOOR SILL #3 CORRODED

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036860 LH #5 SEAT TRACK GOUGED WITH PITTING CORROSION. RAR LH INBORD #5 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036787 RH CARGO FLOOR SILL CORRODED AT FR 71. RAR CARGO FLOOR SILL AT FRM 71 IAW EMB 145 SRM 51-40-02

Part: SKIN — CHAFED (ZONE 800) · airframe 44,968 hrs · 39,712 cycles

F036371 BAGGAGE DOOR INTERNAL SKIN CHAFED AT FWD LWR CORNER. PERFORMED CUTOUT, FABRICATE REPAIR PART AND INSTALLED SERVICEABLE REPAIR FOR BAGGAGE DOOR INTERNAL SKIN AT LOWER FWD CORNER IAW EMB 145 SRM 52-30-01, ITEM #12, FIGURE 213 AND EO1-52-25-0127

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036377 RH CABIN EMERGENCY ESCAPE HATCH LWR EDGE FRAME CORRODED. REMOVED AND REPLACED RH EMERGENCY ESCAPE HATCH LWR FRAME IAW EMB 145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036379 LH CABIN EMERGENCY ESCAPE HATCH LWR EDGE FRAME CORRODED. REMOVED AND REPLACED L/H CABIN EMERGENCY ESCAPE HATCH LWR EDGE FRAME IAW EMB 145 SRM 51-40-02

Part: YOKE — CRACKED (ZONE 400) · airframe 44,968 hrs · 39,712 cycles

F036162 LH LWR FWD ENGINE YOKE FWD FITTING CRACKED. REPAIRED LH LWR FWD ENGINE YOKE FWD FITTING IAW FCD1-54-21-0015

Part: SKIN — CHAFED (ZONE 400) · airframe 44,968 hrs · 39,712 cycles

F0361458 RH PYLON EXTERNAL SKIN CHAFED UNDER ACCESS PANEL 424DB. REMOVED AND REPLACED DOUBLER ON RH PYLON UNDER ACCESS PANEL 424DB. IAW EMB 145 SRM 51-40-02

Part: RIB — CORRODED (ZONE 400) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F035864 CORROSION ON 4 REINFORCEMENTS ON RH ENGINE UPPER COWLING AT CENTER RIB. REMOVED AND REPLACED 4 CORRODED TRIANGLE GUSSET REINFORCEMENTS ON RH ENGINE UPPER COWLING AT CENTER RIB IAW EMB 145 SRM 51-40-02, 51-20-01

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035591 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 6L-7L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 6L-7L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035589 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 8L-9L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 8L-9L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035593 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 3R-4R. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 3R-4R IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0146.

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035590 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 8L-9L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 8L-9L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035592 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 3L-4L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 3L-4L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035594 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0146

Part: SKIN — CRACKED (ZONE 200) · airframe 44,968 hrs · 39,712 cycles

F035588 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 78 BETWEEN STRINGERS 6L-7L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 78 BETWEEN STRINGERS 6L-7L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.

Part: SPAR — CRACKED (ZONE 500) · airframe 44,968 hrs · 39,712 cycles

F035242 THE LH WING SPAR I LOWER FLANGE AT RIB #9 IS CRACKED. PERFORMED CUTOUT, FABRICATED REPAIR DOUBLER, FILLER, SHIMS, AND SPACERS FOR LH WING SPAR I REPAIR AT RIB 9 IAW EMB 145 SRM 57-20-05 ITEM 2. AND INSTALLED IAW ETD2025-145-905692 REV B AND EO1-57-25-0168

Part: BATTERY — UNSERVICEABLE · airframe 44,964 hrs · 39,710 cycles

REAR SET OF EMERGENCY LIGHTS INOP - SUSPECT NO.4 EMERGENCY LIGHT BATTERY-C/A-REPLACED THE NO.4 EMERGENCY LIGHT BATTERY IAW WORK CARD 33-700-19. ALSO REPLACED THE NO. 4 EMERGENCY LIGHT BATTERY CHARGER (SEE ITEM 2 OF THIS NRWC 661-SGF-07052) OPC GOOD IAW WORK CARD 33-700-17.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 44,653 hrs · 39,391 cycles

FA REPORTED SMOKE COMING FROM UNDER ROW 9/10. TURNED OFF BOTH PACKS AND SMOKE STOPPED *DURING TAXI TO THE GATE* ON APU BLEED NO ODOR NOTICED "TRANSFERRED TO NRWC 661-DFW-06888"-C/A-REF LOG PAGE 4797560 ITEM 2. WHILE PERFORMING ETN TRIAD WORKSCOPE FOUND RECIRCULATION SYSTEM MUFFLER DISCONNECTED. MUFFLER HOSE WAS RECONNECTED IAW EMB 145 AMM 21-24-02. LEAK CHECK GOOD. NO LEAKS NOTED. NO VAPORS, SMELLS OR SMOKE NOTED DURING OPC CHECKS. REF LOG PAGE 4797562 ITEM 2 AND 3 FOR OPC CHECKS OF PACKS SYSTEMS AFTER HOSE WAS RECONNECTED AND OPC OF ENGINES PER ETN-EM-72-034. OPC GOOD NO DEFECTS NOTED AFTER ENGINE RUNS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,461 hrs · 39,203 cycles

DURING PS-1 FOUN RH AND LH OVER THE WING EMERGENCY EXTERIOR LIGHTS INOP.-C/A-REF. NRWC# 661-ORD-06781. REPLACED #4 BATTERY CHARGER ASSY #4 IAW EMB-145 M/M 33-50-04, OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (RH) · airframe 44,112 hrs · 38,812 cycles

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

Part: LAMP — INOPERATIVE (RH) · airframe 43,888 hrs · 38,568 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REPLACED LIGHT LAMP FOR RH OVERWING EMERENCY LIGHT IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: RMU — INOPERATIVE (FLIGHT DECK) · airframe 43,786 hrs · 38,466 cycles

THROUGH 8000' RMU 1 OUT - ELECTRICAL BURNING SMELL IN THE COCKPIT. TROUBLESHOT PER FIM 21-20-00-210-801-A. DETERMINED CAUSE OF SMOKE TO BE THE #1 RMU. PULLED AND OCLLARED #1 RMU CIRCUIT BREAKER. REMOVED AND REPLACED #1 RMU IAW AMM 23-81-01. OPS CHECK GOOD. NO ELECTRICAL BURNING SMELL NOTED. UNCOLLARD AND RESET CIRCUIT BREAKER. OPS CHECK GOOD.

Part: HOLDER — BROKEN (FWD FLASHLIGHT) · airframe 43,428 hrs · 38,072 cycles

FA FWD FLASHLIGHT HOLDER BROKEN. RAR FWD FA FLASHLIGHT IAW EMB 145 AMM 33-50-16 . OPS CHECK GOOD M PROCEDURES REVERSED MEL ITEM RESTORED

Part: NONE — NONE · airframe 43,185 hrs · 37,780 cycles

RH SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP-C/A-REMOVED AND REPLACED RH SIDE EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM 33-50-10. DID NOT FIX. REFERENCE NRWC 661-ORD-06175 FOR REMOVAL AND REPLACEMENT OF #4 EMERGENCY LIGHTING BATTERY AND CHARGER. OPS CHECK GOOD

Part: NONE — NONE · airframe 43,185 hrs · 37,780 cycles

LH SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP-C/A-REMOVED AND REPLACED LH SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT LAMP IAW EMB145 AMM 33-50-10. DID NOT FIX. REMOVED AND REPLACED #4 EMERGENCY LIGHTING BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECK GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 42,121 hrs · 36,545 cycles

LH WING LOWER SKIN HAS CRACK ON TRAILING EDGE AT OUTBD END OF INBD FLAP SHROUD HINE PIN. -C/A-REPAIRED LH WING LOWER SKIN ERS-EM-57MR-1318.

Part: FLOOR SUPPORT — CORRODED (FRM 18) · airframe 42,121 hrs · 36,545 cycles

(SSI) RH OMEAGA BEAM IS CORRODED AT NUTPLATES HOLE JUST AFT OF FRAME 18. -C/A-REPAIRED IAW ERS-EM-53MR-4362.

Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 42,121 hrs · 36,545 cycles

#2 ENGINE FORWARD LOWER ENGINE MOUNT LUG CRACKED IN FORWARD INBOARD RAIUS. VERIFIED WITH HFEC. -C/A-REPAIRED #2 ENGINE FORWARD LOWER ENGINE YOKE IAW ERS-EM-54MR-698.

Part: ATTACH ANGLE — CRACKED (WNG-BODY FAIRING) · airframe 42,121 hrs · 36,545 cycles

RH LATERAL WING-TO-FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED BETWEEN FR 48-49. -C/A-REPAIRED RH LATERAL WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE BETWEEN FRAME 48 AND 49 IAW SRM 53-23-12 FIGURE 202

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 42,121 hrs · 36,545 cycles

FWD FLIGHT ATT EMERGENCY FLASH LIGHT HOLDER BROKEN-C/A-COMPLETE:REMOVED AND REPLACED FLASHLIGHT ASSY IAW AMM 33-50-16 OPS CK GOOD

Part: SEAL — WORN (EMERGENCY LIGHT) · airframe 42,121 hrs · 36,545 cycles

LEFT AND RIGHT OVERWING EMERGENCY EXIT SIGN SEAL IS WORN AND TORN..-C/A-COMPLETE:SEAL RAR IAW EMB-145 AMM 52-21-01 AND ETN-EM-52-069. SEE BOW 356061 FOR TEST FOR CABIN LEAKAGE.

Part: CRADLE — BROKEN (C/P FLASHLIGHT) · airframe 41,831 hrs · 36,216 cycles

FLT DECK FA EMERGENCY FLASHLIGHT HOLDER CA FLASH LIGHT HOLDER CLAMP BROKEN MEL 2532 - AUTH# 04-141M-C REF LOGPAGE 4689409 ITEM 1-C/A-RAR CA FLIGHT DECK ATTENDANT EMERGENCY FLASHLIGH ASSY IAW EMB AMM 33-50-16. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 BLEED SYS) · airframe 40,140 hrs · 34,545 cycles

IN CLIMB BLD 1 LEAK EICAS WARNING MESSAGE IN ICING CONDITIONS-C/A-RETORQUED VBAND CLAMPS ON #1 ENG. PRECOOLER IAW AMM 20-10-10 AND AMM 36-11-04. PERFORMED AIR BLEED SYS. OPS CHECK IAW AMM 36-00-00. OPS CHECK GOOD. PERFORMED ICE/RAIN PROT. OPS CHECK IAW AMM 30-00-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 40,110 hrs · 34,526 cycles

BRAKE DEGRADED CAUTION MESSAGE ON EICAS AFTER LOWERING GEAR ON FINAL. BRAKING WAS NOTICEABLY LESS EFFECTIVE.-C/A-REMOVED AND REPLACED NO3 WHEEL SPEED XDUCER AND CLEANED CONNECTION IAW AMM 32-41-03 OPS CHECK GOOD IAW AMM 32-41-00 OPS CHECK GOOD AT THIS TIME.

Part: WIRE — BROKEN (FLASHLIGHT ASSY) · airframe 40,005 hrs · 34,420 cycles

MEL 25-53 AUTH #010760-C ORIG LG PG 4452721 ITEM #2 FWD FA FLASHLIGHT NOT CHARGING-C/A-T/S AND FOUND BROKEN WIRE IN FLASHLIGHT HARNESS. REPAIRED WIRE IAW SWPM 20-21-00 OPC GOOD IAW EMB AMM 33-51-01 MEL RESTORED

Part: WARNING MESSAGE — FALSE INDICATION (NR 1 BLEED SYS) · airframe 39,979 hrs · 34,396 cycles

BLD 1 LEAK IN FLIGHT-C/A-TROUBLESHOT PER FIM TASK 36-20-00-810-801-A & PERFORMED OPC OF THE AIR BLEED SYSTEM PER AMM 36-00-00-700-803. ALL CHECKS GOOD. CND FAULT AT THIS TIME. A/C HISTORY SHOWS NO CURRENT/RECENT FAULT. A/C OK FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 39,651 hrs · 34,049 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPC GOOD

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 38,279 hrs · 32,838 cycles

AFTER REMOVAL OF RT LAV FLOOR GUSSET FOUND 2EA. NUTPLATE HOLES ON UNDERLYING HAT BEAM TO BE CRACKED. C/A-COMPLIED WITH REPAIR IAW ERS-EM-53MR-3755.

Part: ATTACH FITTING — EXCESS PLAY (RT AILERON) · airframe 38,279 hrs · 32,838 cycles

RIGHT AILERON PCA ATTACH FITTING, ALL HAT BUSHINGS HAVE PLAY. C/A-REMOVED AND REPLACED RIGHT AILERON PCA ATTACH FITTING IAW EO EM-27MR-112.

Part: FRAME — CRACKED (FRM 10) · airframe 38,279 hrs · 32,838 cycles

PILOTS SIDE UPPER FRAME #10 HAS APPROX. A 2" CRACK. -C/A-INSTALLED NEW LH FRAME 10 SECTION IAW SRM 51-40-02.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 38,279 hrs · 32,838 cycles

LEFT AILERON PCA FITTING ON AILERON, INBOARD 2 LUGS, HAVE MIGRATING BUSHINGS.-C/A-REMOVED AND REPLACED LEFT AILERON PCA ATTACH FITTING IAW EO EM-27MR-112.

Part: ATTACH FITTING — EXCESS PLAY (RT AILERON) · airframe 38,279 hrs · 32,838 cycles

RIGHT AILERON DAMPER FITTING HAT BUSHING HAS PLAY IN FITTING. C/A-REMOVED AND REPLACED RT AILERON DAMPER ATTACH FITTING IAW EO EM-27MR-112.

Part: FRAME — CRACKED (FRM 10) · airframe 38,279 hrs · 32,838 cycles

FO'S SIDE UPPER FRAME #10 HAS APPROX. A 2" CRACK.-C/A-RE-EVALUATED AND FOUND UPPER FRAME 10 SEGMENT P/N 145-02409-002 TO FIT TH U-CHANNEL SPLICE PROPERLY. INSTALLED THE NEW FRAME 10 UPPER SEGMENT IAW SRM 51-40-02.

Part: CROSSBEAM — CRACKED (NLG UPLOCK BOX) · airframe 38,279 hrs · 32,838 cycles

NLG UPLOCK BOX, AFT CROSSBEAM IS CRACKED. CRACK IS ON THE LH SIDE, OTBD OF THE UPLOCK BOX. -C/A-INSTALLED NEW NLG UPLOCK BOX AFT CROSSBEAM IAW SRM-51-40-02.

Part: ANGLE — CRACKED (WNG-BODY FAIRING) · airframe 38,279 hrs · 32,838 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING AFT ATTACH ANGLE ON WING HAS 1/4" CRACK ON THE AFT END. -C/A-CUT OUT DAMAGED SECTION AND INSTALLED SERVICEABLE SECTION OF ATTACH ANGLE IAW ETN-EM-53-142.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 38,279 hrs · 32,838 cycles

RH SHEARCLIP AT FRAME 80 BETWEEN STRINGERS 4R AND 5R HAS A 3/8 INCH CRACK.-C/A-REMOVED AND REPLACED RH SHEARCLIP AT FRAME 80 BETWEEN STR 4R-5R IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (HOLD OPEN ROD) · airframe 38,279 hrs · 32,838 cycles

BRACKET ON FR 68 FOR BAGGAGE DOOR HOLD OPEN ROD SUPPORT IS CRACKED.-C/A-REMOVED AND REPLACED SUPPORT BRACKET ON FRAME 68 FOR BAGGAGE DOOR HOLD OPEN SUPPORT ROD BRACKET IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 46) · airframe 38,279 hrs · 32,838 cycles

FRAME SUPPORT FOR FRAME 46 AT STR 15R IS CRACKED.-C/A-RAR FRAME SUPPORT BRACKET AT FRAME 46 IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 77) · airframe 38,279 hrs · 32,838 cycles

FUSELAGE SKIN HAS A CRACK INDICATION .250 INCHES IN LENGTH 1 RIVET ABOVE STRINGER 6L AT FRAME 77. -C/A-REPAIRED FUSELAGE SKIN AT FRAME 77 IAW SRM 53-32-01.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 38,279 hrs · 32,838 cycles

LH SHEAR CLIP AT FRAME 80 BETWEEN STRINGERS 4L AND 5L HAS A 3/8 INCH CRACK.-C/A-INSTALLED NEW LH SHEARCLIP AT FRAME 80 BETWEEN STRINGER 4L AND 5L IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 77) · airframe 38,279 hrs · 32,838 cycles

FUSELAGE SKIN HAS A CRACK INDICATION .125 INCHES IN LENGTH 1 RIVET BELOW STRINGER 6L AT FRAME 77 -C/A-EVALUATED WITH HFEC FOUND NO CRACK. RESTORED SURFACE PROTECTION IAW CPM 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,279 hrs · 32,838 cycles

LT OMEGA BEAM CORRODED AT FRAME 29. C/A-REPAIRED LT OMEGA BEAM AT FR 29 IAW ERS-53MR-3756.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 38,279 hrs · 32,838 cycles

CENTER SERVICE DOOR SILL IS CORRODED.-C/A-INSTALLED NEW CENTER SERVICE DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — CRACKED (CABIN) · airframe 38,279 hrs · 32,838 cycles

CABIN PROXIMITY LIGHT STRIPS (LT) NR 8,6,4,3,2 AND 1 ARE CRACKED. C/A-COMPLETE:RAR CABIN PROXIMITY LIGHT STRIPS EXTRUSIONS LT NR 8,6,4,3,2,1 IAW AMM 33-50-12 (REF NRWC E705441 FOR OPS TEST)

Part: LIGHT — DAMAGED (CABIN) · airframe 38,279 hrs · 32,838 cycles

BOTH AFT EMERGENCY FLOOR LIGHTING EXTRUSIONS IN LAV AREA DAMAGED. C/A-COMPLETE:INSTALLED NEW LT AND RT AFT EMERGENCY FLOOR LIGHTING EXTRUSIONS IN LAV AREA IAW AMM 53-01-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,279 hrs · 32,838 cycles

NR 3 EMERGENCY FLOOR PATH LIGHT STRIP IS INOP. C/A-COMPLETE: REMOVED AND REPLACED NR 3 FLOOR PATH LIGHT STRIP IAW AMM 33-50-12 (REF NRWC E705441 FOR OPERATIONAL TEST)

Part: TRIM SWITCH — DEFECTIVE (COCKPIT) · airframe 37,775 hrs · 32,373 cycles

PTRIM MAIN INOP AFTER TAKEOFF WITH THRUST IN DETENT. C/A-FOLLOWING FIM TASK 27-43-00-810-801-A C/W STEP NR 1 AND PITCH TRIM SYSTEM FAILED WITH PTRM CPT SW FAIL MESSAGE ON THE EICAS, FOLLOWING FIM TASK 27-43-00-810-816-A REMOVED AND REPLACED PILOT CONTROL YOKE PITCH TRIM SWITCH IAW 27-40-03, MAIN PITCH TRIM SYSTEM OPS CHECK GOOD IAW AMM 27-40-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,727 hrs · 32,325 cycles

FLOOR PROX LIGHTING STRIP NR 4 INOP. C/A-REMOVED AND REPLACED FLOOR PROX LIGHTING STRIP NR 4, OPC GOOD, IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,315 hrs · 31,924 cycles

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

Part: LIGHT — INOPERATIVE (SEAT 1A) · airframe 36,851 hrs · 31,462 cycles

CEILING LIGHTS AT SEAT 1A INOPERATIVE. REMOVED AND REPLACED THE LIGHTS IAW AMM 33-21-06. OPS CHECKED GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 36,397 hrs · 31,016 cycles

ON TAXI OUT CA WINDSHIELD SHATTERED, RETURNED TO GATE "TRANSFERRED TO NRWC 661-ORD-03688". INSTALLED LT WINDSHIELD IAW AMM 56-10-01. LEAK CHECK AND PRESSURIZATION GOOD. RE-TORQUE AFTER PRESSURIZATION COMPLETED.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 35,966 hrs · 30,628 cycles

MAIN DOOR HANDLE BROKEN. SECURED MAIN DOOR HANDLE IAW AMM 52-18-07.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,446 hrs · 30,192 cycles

GALLEY AND FLOOR EMERGENCY LIGHTS FROM ROW 7 FORWARD, INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND CHARGER IAW WC 33-700-19. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,212 hrs · 29,957 cycles

EMERGENCY FLOOR LIGHT STRIP #1 INOP.-C/A-REMOVED AND REPLACED #2 INVERTER IAW EMB 145 AMM 33-50-11 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 35,122 hrs · 29,876 cycles

FWD FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. R & R THE EMERGENCY LIGHT IAW 33-50-12, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,726 hrs · 29,480 cycles

FWD CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 6 INVERTER FOR THE FWD CEILING EMERGENCY EXIT LIGHT IAW AMM 33-50-11, OPS CHECKED GOOD.

Part: SKIN — CRACKED (FRAME 75) · airframe 33,288 hrs · 28,213 cycles

LEFT UPPER FUSELAGE SKIN CRACKED ON FRAME 75 STRINGER 2L. REPAIRED IAW SRM 53-31-01-RE ITEM 11 FIG. 219 SHEET 1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 33,288 hrs · 28,213 cycles

FWD CARGO DOOR STOP FITTING, CRACKED AT LOWER CORNER. REMOVED AND REPLACED FWD CARGO DOOR STOP FITTING IAW SRM 51-40-02

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 33,288 hrs · 28,213 cycles

THE NR 1 EMERGENCY LIGHT STRIP WIRES BROKE OFF THE BACK. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,288 hrs · 28,213 cycles

RT CABIN FLOOR EMERGENCY LIGHT EXTRUSIONS NR 3, 5, 6, AND 7 DAMAGED. REMOVED AND REPLACED THE LIGHTS IAW AMM 33-50-12

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 33,288 hrs · 28,213 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT BASE HAS INTERMITTENT OPERATION. REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT BASE IAW AMM 33-50-16.

Part: BULB — OUT OF POSITION (EMERGENCY LIGHT) · airframe 32,290 hrs · 27,304 cycles

LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REPOSITIONED THE LIGHT BULB AND OPS CHECK IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,202 hrs · 27,226 cycles

ROW 17, EMERGENCY CEILING LIGHT INOPERATIVE. R & R ROW 17 EMERGENCY CEILING LIGHT BULB IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A, OPS GOOD.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 31,883 hrs · 26,965 cycles

ON TAKEOFF AT GEAR RETRACTION GOT LG LEVER DISAGREE WARNING WITH GEAR INDICATION SHOWING DOWN. R & R LGEU IAW AMM 32-30-00. FOUND EMER EXTENSION TOGGLE SWITCH OUT OF NORMAL POSITION, SWITCH WAS RESTOWED. CYCLED GEAR IAW AMM 32-30-00. OPERATIONS CHECKED GOOD IAW NRWC 661-ORD-02683. PERFORMED OPERATIONAL CHECK OF EXTENSION & RETRACTION SYS IAW AMM 32-30-00-700-801-A. NO DEFECT NOTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 31,607 hrs · 26,700 cycles

AT GATE ON APU GEN & PACK 2 NOTICED BURNING SMELL IN FLIGHT DECK & FOUND PRESS SPIKE & CONTROLLER DISPLAYED WENT BLANK, NO DISPLAY. ALSO NOTICED CB F8 POPPED. OPENED DV WINDOWS TO RELIEVE CABIN PRESS. REMOVED DIGITAL CONTROLLER & FOUND TO SMELL BURNT DIS-CONNECTED CONNECTOR & FOUND CB F8 STAYS IN. INSTALLED DIGITAL PRESSURIZATION CONTROLLER CONNECTED CONNECTOR CB F8 POPS. REF AMM 21-31-01. R & R DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHECKED GOOD IAW AMM 21-31-00.

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 31,600 hrs · 26,693 cycles

DURING LANDING WHEN PUT GEAR DOWN GOT CAUTION MSG, LG AIR & GND FAIL. PERFORMED GO AROUND, DURING GO AROUND MSG CLEARED ITSELF & LANDED UNEVENTFULLY. R & R LT NLG ACTUATOR DOOR IAW AMM 32-20-05. OPERATIONS CHECKED GOOD.

Part: PITOT SYSTEM — CONTAMINATED (NR 2) · airframe 31,039 hrs · 26,188 cycles

SPS ADVANCE MSG ON EICAS & ADC 2 FAILED. CLEARED NR 2 PITOT MAST DRAIN HOLES, DRAINED & PURGED NR 2 PITOT SYS, NR 2 PITOT CHECKED OK IAW AMM CH 34-13-00. NR 1 & 2 ADC OPERATIONS CHECKED OK IAW AMM CH 34-15-00. SPS OPERATION CHECKED OK IAW AMM CH 27-36-00.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 30,115 hrs · 25,323 cycles

AT FL 370 BOTH PRESERVED IAS MESSAGE. CAPTAIN`S PFD INDICATES 239 KIAS .74 MACH, FIRST OFFICER`S SIDE INDICATES 250 KIAS .77 MACH, STANDBY SHOWS 248 KIAS. ALSO GET SPS ADVANCED ON EICAS. BACK TO NORMAL DESCENDING THRU FL 200. DRAINED WATER FROM PITOT 1 - 2 SYSTEM DRAINS. PERFORMED OPERATIONAL TEST OF THE ADC SYSTEM IAW AMM 34-13-00 & 34-15-00 WITH NO FAULTS NOTED.

Part: PIVOT — CONTAMINATED · airframe 30,016 hrs · 25,249 cycles

AT 370FT, ADC 1 IAS WAS READING +/- 20 KNOTS & ALTITUDE WAS +/- HIGH SPEED AUROL WARNING PRESENT. SELECTED ADC 2 ISIS & ADC 2 READ SAME INFO. INSPECTED PITOT DRAINS FOR MOISTURE, NONE FOUND. INSPECTED PITOT TUBES & STATIC PORTS, NO DEFECTS NOTED. FOUND WATER IN PITOT STATIC DRAIN AND REMOVED IAW MM 34-13-00. PERFORMED FUNCTIONAL CHECK OF ADC 1, NO FAULTS FOUND IAW MM 34-15-00.

Part: TIRE — SEPARATED (NR 3) · airframe 29,891 hrs · 25,148 cycles

ON POST FLIGHT FOUND THAT A LARGE PIECE OF NR 3 TIRE HAD SEPARATED. R & R NR 3 TIRE IAW WC 32-700-11.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,823 hrs · 25,089 cycles

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

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 29,790 hrs · 25,060 cycles

AFTER TAKEOFF PASSING THROUGH APPROX 25000 FT CABIN RATE INCREASED DRAMATICALLY & CABIN WAS NOT PRESSURIZING, AUTO CONTROLLER WAS NOT RESPONSIVE & DISPLAY SHOWED 48102 IN WINDOW. UNABLE TO CHANGE LANDING ELEVATION. SEE LOG PAGE 3796251 FOR MORE INFO. DEFERRED THE PRESSURIZATION CONTROL SYS, AUTOMATIC & MANUAL MODE IAW MEL 21-18. MX PROCEDURE COMPLIED WITH. R & R ELECTRO PNEUMATIC OUTFLOW VLV IAW AMM 21-31-03. OPERATIONS CHECKED SATISFACTORY. THIS RESTORED MEL 21-18.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 29,727 hrs · 25,003 cycles

ENGINE OIL SMELL IN COCKPIT, ONLY DURING TOP OF DESCENT TO LANDING, CABIN OK. TRANSFERRED TO NRWC 661-ORD-02242. COMPLIED WITH RR FIM 72-00-00-810-814 OBSERVED FAULT, OIL OR UEL SMELL, HAZE IN THE CABIN & ETN EM-72-034 ENG ODOR EVENT. TROUBLESHOOTING DISCREPANCY TRANSFERRED TO AML 3806131 ITEM 1. REF AML 3806129 NR 1 ENG OIL SMELL IN COCKPIT ONLY. DETERMINED TO BE FROM ENG NR 1. ENG 1 REQUIRES CHANGE. R&R NR 1 ENG IAW WC 71-000-00. OPERATIONS & LEAK CHECKED GOOD, NO DEFECTS NOTED. ENG ACC FIRE DETECTOR PN 3601133500230C90M, SN 217282. COMPLIED WITH DECONTAMINATION OF AIR CONDITIONING SYS IAW AMM 21-20-00, NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,126 hrs · 24,458 cycles

AFT CABIN FLASHLIGHT UP WON’T STAY ON. REPLACED AFT CABIN FLASHLIGHT IAW 25-60-11. FLASHLIGHT B-07-0011-500 INTERCHANGE WITH B-07-0011-501.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 28,798 hrs · 24,144 cycles

EMERGENCY LIGHT COMES ON IN ARM POSITION. POWERED DOWN ACFT POWER & BACK UP IAW 20-40-01. EMER LIGHTS OPERATIONS CHECKED GOOD.

Part: GROUND STUD — DIRTY (CABIN) · airframe 28,798 hrs · 24,144 cycles

AFTER ARMING EMER LIGHTS, APPROX 1 MIN, EMER LIGHTS CAME ON. CYCLED BOTH FLIGHT ATTENDANT & COCKPIT SWITCHES, EMER LIGHTS CAME BACK ON FM ARMED MODE. TRANSFERRED TO NRWC 661-MIA-02045. FOUND GS8008 DIRTY & INHIBIT GND SIGNAL. CLEANED GND STUD GS8008, GOT GOOD GND SIGNAL. EMER LIGHTS OPERATIONS CHECKED NORMALLY IAW AMM 33-50-00.

Part: TAT PROBE — INOPERATIVE (NR 1) · airframe 28,761 hrs · 24,115 cycles

TAT 1 HEAT INOPERATIVE IN FLIGHT. TRANSFERRED TO NRWC 661-CVG-02040.

Part: SENSOR — FAILED (NR 2 BRAKE) · airframe 28,686 hrs · 24,057 cycles

MEL 32-3, LOG PAGE 3678350 2 INBD BRAKE OVERHEAT. R & R NR 2 BRAKE TEMP SENSOR IAW AMM 32-47-01. OPERATIONS CHECKED GOOD AT THIS TIME. MEL RESTORED.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 28,504 hrs · 23,898 cycles

EMERGENCY LIGHTS AT OVERWING EXITS & FLOOR PROXIMITY LIGHT STRIPS NR 4 & 5 DO NOT TURN OFF WHEN SWITCH IS TURNED OFF. R & R BATTERY HOLDER & BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04, OPERATIONALLY CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,504 hrs · 23,898 cycles

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

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,504 hrs · 23,898 cycles

FOUND NR 2 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 2 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,504 hrs · 23,898 cycles

FOUND NR 8 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 8 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,504 hrs · 23,898 cycles

FRAME 68 SHEAR CLIP CORRODED AT LOWER END AT CARGO DOOR FRAME. REPAIRED IAW EO EM-53MR-1129 PART B.

Part: TERMINAL — BROKEN (CABIN) · airframe 28,504 hrs · 23,898 cycles

LEFT NR 4 EMER LIGHT STRIP HAS BROKEN TERMINAL. REPLACED THE LT NR 4 EMER LIGHT STRIP TERMINAL IAW SWPM 20-00-03 PAGE 69.

Part: LIGHT — BROKEN (CABIN) · airframe 28,504 hrs · 23,898 cycles

LEFT NR 8 EMER LIGHT STRIP EXTRUSION IS BROKE & CRACKED. R & R NR 8 EMER LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW 167569 FOR OPERATIONAL CHECK OF EMER LIGHT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,504 hrs · 23,898 cycles

FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT RIVET ON FRAME 79 BETWEEN STRINGER 5L & 6L. REPAIRED FUSELAGE EXTERNAL SKIN ON FRAME 79 BETWEEN STRINGERS 5L - 6L IAW ERS-EM-5300-835.

Part: LIGHT — BROKEN (CABIN) · airframe 28,504 hrs · 23,898 cycles

LEFT NR 2 EMER LIGHT STRIP EXTRUSION IS CRACKED & BROKE. R & R NR 2 EMER LIGHT STRIP IAW AMM 33-50-12. SEE BOW 167569 FOR OPERATIONAL CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,504 hrs · 23,898 cycles

FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT RIVET ON FRAME 78 BETWEEN STRINGER 5L & 6L. REPAIRED FUSELAGE EXTERNAL SKIN ON FRAME 78 BETWEEN STRINGERS 5L & 6L IAW ERS-EM-5300-835.

Part: SENSOR — FAULTY (BRAKE SYSTEM) · airframe 28,280 hrs · 23,738 cycles

RIGHT INBD BRAKE TEMP ERRATIC. ABORTED TAKEOFF FOR BRAKE OVERHEAT PREVIOUS WRITE UP 3637162. R & R BRAKE TEMP SENSOR IAW AMM 32-47-01.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 28,213 hrs · 23,673 cycles

AIRSPEED INDICATORS ALL 3 STOPPED WORKING, FROZE AT FL370. ON DESCENT WENT AS LOW AS 70 KNOTS, SEEMED TO BE WORKING AS ALTIMETERS. STANDBY SEEMED TO CLEAR FIRST FOLLOWED BY CAPTAIN`S SIDE AT FL 290, THEN FIRST OFFICER`S SIDE AT FL 250. DRAINED PITOT LINES IAW AM 34-13-00 & PERFORMED ADC SYS OPERATIONAL TEST IAW AMM 34-15-00. OPERATIONS CHECKED OK.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 26,245 hrs · 22,082 cycles

ON FLIGHT 3584 CREW REPORTED BAGGAGE OKE WARNING EICAS. EPC BAGGAGE EXTINGUISHER DEPLOY & DECLARED EMERGENCY. R & R SMOKE DETECTOR IAW AMM 26-15-01, OPERATIONS CHECKED GOOD.

Part: CRADLE — DAMAGED (CKPT FLASHLIGHT) · airframe 25,947 hrs · 21,858 cycles

CAPTAIN`S FLASHLIGHT WILL NOT CLIP INTO CHARGER HOLDER. R & R FLASHLIGHT CRADLE BRACKET IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,614 hrs · 24,614 cycles

THE CREW REPORTED WHEN EMERGENCY LIGHTS ARE TURNED OFF WITH BATTRIES ON. CENTER FLOOR STRIP AND WITH BATTERIES OFF AS WELL LIGHTS ONLY, GO OFF WITH EMERGENCY LIGHTS IN ARM. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND POWER SUPPLY IAW AMM 33-50-04. THE OPS CHECK WAS GOOD IAW AMM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 24,527 hrs · 20,724 cycles

ON FLIGHT 2939 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED EXTERNAL HANDLE IAW PART TASK 52-18-00-640-00-640-001-A00. OPENED AND CLOSED GOOD IAW EMB145 AMM 52-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,283 hrs · 20,522 cycles

ON FLIGHT 3332 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — OUT OF ADJUST (EMERGENCY EXIT) · airframe 24,060 hrs · 20,342 cycles

DURING B INSPECTION FOUND RIGHT OVERWING EMERGENCY EXIT HATCH LINER BINDING WITH OPENING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RIGHT & LEFT EMERGENCY EXIT DOORS FOUND TO BE IN SWAPPED POSITIONS. REMOVED AND REINSTALLED IN CORRECT POSIITION. ADJUSTED AND TIGHTENED LINER BRACKET ON LEFT EMERGENCY EXIT LINING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — WORN (PAX DOOR) · airframe 24,060 hrs · 20,342 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR SEAL WORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW EMB 145 AMM 52-18-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,060 hrs · 20,342 cycles

DURING B INSPECTION FOUND THE NR 4, 7 AND 8 EMERGENCY LIGHT STRIP TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4, 7 AND 8 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FAULTY (CABIN) · airframe 23,847 hrs · 20,173 cycles

ON FLIGHT 4313 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS ON ICU WILL NOT GO OFF. THE CREW WAS UNABLE TO COMMUNICATE WITH FLIGHT ATTENDANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AURAL WARNING UNIT IAW EMB-145 AMM 31-51-01. PERFORMED OPERATIONAL CHECK OF PASSENGER ADDRESS & CABIN INTERPHONE SYSTEM IAW EMB-145 AMM 23-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — DEFECTIVE (SPOILER)

AT 37000 FT SPOILER OPEN MSG, UNCOMMANDED T/S IAW EMB FIM TASK 27-63-00-810-806. REMOVED AND REPLACED LEFT SPOILER PROXIMITY SENSOR INBOARD IAW EMB AMM 27-63-04. REMOVED AND REPLACED PROXIMITY SENSOR CONNECTOR P1167 IAW EMB SWPM 20-50-00. OPS CHECK GOOD IAW EMB AMM 27-63-01.

Part: BRACKET — BROKEN (FLASHLIGHT)

AFT FLASHLIGHT BROKEN BRACKET. REPLACED AFT FLASHLIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 23,404 hrs · 19,800 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT IAW 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,908 hrs · 19,426 cycles

DURING B INSPECTION FOUND THE CABIN CEILING FORWARD FACING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHT DC/AC INVERTER 6 IAW EMB145 AMM TASK 33-50-11-000-801-A AND 33-50-11-400-801-A. PERFORMED EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK IAW W/C 33-700-17. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,793 hrs · 19,340 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR ENTRY EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR ENTRY EMERGENCY LIGHT IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHT) · airframe 22,442 hrs · 19,076 cycles

DURING B INSPECTION, FOUND THE EMERGENCY EXIT SIGN AT THE FORWARD CABIN CEILING, FORWARD FACING, LAMP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED EMERGENCY EXIT SIGN IAW AMM 33-50-15-000-801-A. FOUND CORROSION ON ELECTRICAL PINS, CLEANED ELECTRICAL PINS AND REINSTALLED ELECTRICAL PINS AND FORWARD FACING AISLE EMERGENCY EXIT SIGN IAW AMM 33-50-15-400-801-A. OPS CHECKED GOOD IAW AMM 33-50-15-710-001-A00. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,416 hrs · 19,056 cycles

DURING B INSPECTION, FOUND THE MID-CABIN FORWARD FACING EMERGENCY EXIT SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TY BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,275 hrs · 18,941 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 22,033 hrs · 18,762 cycles

DURING B INSPECTIONS, FOUND THE CEILING AISLE FORWARD FACING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. FOUND CONNECTOR LOOSE. CONNECTED IAW AMM 33-50-15. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTTLE VALVE — FAILED (BRAKES)

ON FLIGHT 2991, THE CREW REPORTED NR 1 HYDRAULIC QUANTITY LOW INFLIGHT AFTER 1.5 HRS IN FLIGHT. THE MESSAGE CAME ON DURING DESCENT. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AND NR 4 BRAKE SHUTTLE VALVE PER EMB-145 MM 32-49-07. THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,352 hrs · 18,218 cycles

DURING B-INSPECTION FOUND THE FORWARD CEILING OVERWING EXIT SIGN WILL NOT STAY ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — BROKEN (ANTI-ICE SYSTEM) · airframe 19,906 hrs · 17,153 cycles

ON FLIGHT 3515 THE CREW REPORTED A STABILIZER ANTI ICE FAIL MESSAGE IN FLIGHT WHILE ENTERING INTO ICING CONDITIONS. THE CREW ELECTED TO RETURN BACK TO MIA. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND BROKEN INPUT FLOW TUBE TO MANIFOLD ASSEMBLY. REMOVED AND REPLACED INPUT FLOW TUBE IAW EMB 145 AMM 30-12-14. PERFORMED OPERATIONAL CHECK IAW 30-00-00. NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 19,850 hrs · 17,102 cycles

ON FLIGHT 3967 AFTER TAKEOFF AT APPROXIMATELY 500 FEET THE CREW RECEIVED A " MAIN PTRIM INOP " EICAS MESSAGE. THE CAPTAIN’S AND THE FIRST OFFICER’S PITCH TRIM SWITCHES DID NOT OPERATE. THE CREW RETURNED AND THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT IAW EMB-145 AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (RUDDER) · airframe 19,314 hrs · 16,683 cycles

ON FLIGHT 2761 THE CREW REPORTED, ABORTED THE TAKEOFF ROLL DUE TO NO RUDDER CONTROL. THE FIRST OFFICER PRESSED THE QUICK DISCONNECT BUTTON AND CONTROL WAS REGAINED. THE AIRCRAFT WAS REMOVED FROM SERVICE. NO MESSAGE ON THE CENTRAL MAINTENANCE COMPUTER, THE AUTOPILOT AND YAW TRIM CHECKS WERE GOOD IAW AMM 22-11-00 AND AMM 27-24-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,232 hrs · 16,619 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR CUTOUT REINFORCING STRUCTURE HAS CORROSION ON AFT SIDE AROUND LOWER NUT PLATE HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LOWER NUT PLATE HOLE CORROSION IAW AE EO-EM-53MR-1814. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 19,160 hrs · 16,568 cycles

ON FLIGHT 2936 THE CREW REPORTED THE PASSENGER DOOR HANDLE JAMS DURING OPERATING CYCLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED THE INTERNAL ACTUATING HANDLE IAW EMB 145 AMM 52-18-05. A FUNCTIONAL CHECK WAS PERFORMED AND NO DEFECTS WERE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,938 hrs · 15,608 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING LAMP IAW 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — FAULTY (CABIN) · airframe 17,902 hrs · 15,579 cycles

ON FLIGHT 4255 DURING THE CLIMB WHEN REACHED FLIGHT LEVEL 340 THE CREW DETECTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT AND CABIN. THE APU WAS NOT ON. THE AIRCRAFT WAS DE-ICED PRIOR TO FLIGHT. THE CAPTAIN DECLARED AN EMERGENCY. THE CREW DONNED OXYGEN MASK AND DIVERTED INTO IAD. THERE WAS NO SMOKE PRESENT. CRASH, FIRE AND RESUCE WERE CALLED. THE AIRCRAFT LANDED WITHOUT INCIDENT. CRASH, FIRE AND RESUCE FOUND NO EVIDENCE OF FIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE NR 1 RECIRCULATION FAN MAKING A LOUD NOISE. REMOVED AND REPLACED THE NR 1 FAN IAW 21-24-01. FOUND NR 2 RECIRCULATION FAN SYSTEM MUFFLER TORN. REMOVED AND REPLACED NR 2 RECIRCULATION FAN SYSTEM MUFFLER IAW AMM 21-24-02. THE OPERATIONAL CHECK WAS GOOD USING APU AND ENGINES AS A PNEUMATIC SOURCE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 15,930 hrs · 14,007 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FIRST OFFICERS EMERGENCY FLASHLIGHT TO BE DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS EMERGENCY FLASHLIGHT AND CHARGER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 15,176 hrs · 13,400 cycles

DURING MAINTENANCE INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS FLICKER ON/OFF INTERMITTENTLY WITH POWER OFF AND EMERGENCY LIGHT SWITCH NOT ARMED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 EMERGENCY POWER SUPPLY UNIT ASSEMBLY. OPERATIONAL CHECK WAS NORMAL IAW AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER SYSTEM) · airframe 10,256 hrs · 9,109 cycles

AIR TURN BACK FOR RUDDER SYSTEM 2 INOP MESSAGE. AIRCRAFT WAS BEING REPOSITIONED TO XNA. REMOVED AND REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM27-73-04. LEAK AND OPS CHECK GOOD IAW AMM 27-23-00. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED (FLIGHT DECK) · airframe 8,981 hrs · 8,064 cycles

RECEIVED EMERGENCY ARM LIGHT MESSAGE FOLLOWED BY ELECTRICAL ABNORMAL MESSAGE, DIVERTED TO MEM. REMOVED AND REPLACED POWER DISTRIBUTION BOX AND CONTROL RELAY IAW EMB AMM 24-13-02 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE)

ALL PRESSURIZATION INDICATIONS ON EICAS SHOWED FAILED. RESET SYSTEM AND PERFORMED OPERATIONAL CHECK, IAW EMB AMM 21-31-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FS 20)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 1435/1142 REV 30, CHAPTER 53-00-10. (M)