N906AE

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT OMEGA BEAM CORRODED ON LOWER FLANGE BETWEEN FR 28-29. ACOMPLISHED PERMANENT REPAIR ON LH OMEGA BEAM FLANGE BETWEEN FR28-29 IAW EMB145 SRM 53-22-10RE, ITEM 4, FIG 203, SHEET 2 AND E01-53-25-0423.

Part: SKIN — GOUGED (ZONE 100) · airframe 45,490 hrs · 42,373 cycles

GOUGE UNDER GPU DOOR. REPAIRED DAMAGED UNDER GPU DOOR IAW EMB 145 SRM 53-12-01 ITEM 2 FIG 201. AND EO1-53-25 0424

Part: RIB — CRACKED (ZONE 500) · airframe 45,490 hrs · 42,373 cycles

LEFT WING, UPPER SECTION OF RIB 21 IS CRACKED. INSTALLED DOUBLER AND FILLER ON LH WING UPPER SECTION OF RIB 21. IAW EMB 145 SRM 57-20-07-RE, ITEM 4, FIG. 203, DET. C. AND E01-57-25-0425

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

RIGHT OUTBD FLOOR SILL NR 1 IS CORRODED. R & R RT NR 1 OTBD FLOOR SILL IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,490 hrs · 42,373 cycles

STRINGER 15-16R SHEAR CLIP CRACKED AT FRAME 25. RAR SHEAR CLIP ON FR25 BTWN STGR 15R-16R IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT OUTBD FLOOR SILL #2 IS CORRODED. REMOVED AND REPLACED LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT OMEGA BEAM CENTER FLOORBOARD SUPPORT AND RH SIDE OF BEAM HAS CORROSION BETWEEN FRAMES 24-27. BLENDED OUT CORROSION ON LH OMEGA BEAM CENTER FLOORBOARD SUPPORT AND RH SIDE OF BEAM BETWEEN FRAMES 24-27 IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS AT BLENDED AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-22-10-AD. REPAIRED THE CRACKED AREA LOCATED AT LH OMEGA BEAM AT FR 26 SUPPORT IAW EMB ETD2025-145-931696 REV A AND EO1-53-25-0414.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT UPPER SEAT TRACK #3 HAS CORROSION. RAR LH #3 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT UPPER SEAT TRACK #2 HAS CORROSION. RAR LH UPPER SEAT TRACKS # 2 IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

RIGHT LOWER SEAT TRACK #3 HAS MULTIPLE CORROSION SPOTS. RAR RH LOWER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,409 hrs · 42,373 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT FLOOR SILL NR 4 HAS CORROSION. R & R LT FLOOR SILL NR 4 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

RIGHT FLOOR SILL NR 3 HAS CORROSION. RAR RH FLOOR SILL NR 3 IAW EBM 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT OMEGA BEAM CENTER FLOORBOARD SUPPORT AND RH SIDE OF BEAM HAVE CORROSION BETWEEN FRAMES 28-30. REPAIRED IAW SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT LOWER SEAT TRACK #5 HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED LH LOWER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — GOUGED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

F081061 LH FLOOR SEAT TRACK #2 IS GOUGED AND CORRODED. RAR LH FLOOR SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CARGO SIDEWALL PANELS SUPPORT AT FR 61 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED CARGO SIDEWALL PANELS SUPPORT AT FR. 61 IAWEMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT LOWER SEAT TRACK NR 4 HAS VARIOUS CORROSION SPOTS. R & R LT LOWER SEAT TRACK NR 4 IAW AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT OMEGA BEAM OTBD GUSSET #6 HAS CORROSION. R & R LT OMEGA BEAM OTBD GUSSET #6 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

LEFT UPPER SEAT TRACK NR 5 HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED LT OTBD SEAT TRACK NR 5 IAW AMM 53-01-06.

Part: SEAT TRACK — GOUGED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

F081064 RH FLOOR SEAT TRACK #2 IS GOUGED AND CORRODED. RAR RH INBD FLOOR SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

RIGHT OTBD FLOOR SILL NR 2 IS CORRODED. R & R RT OTBD FLOOR SILL NR 2 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION ON LH OTBD #1 SEAT TRACK. RAR LH OUTB SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION IN GALLEY AREA ON PASSENGER DOOR ENTRY AFT FLOORBOARD SUPPORT. R & R PASSENGER DOOR ENTRY AFT FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION IN GALLEY AREA ON LH OTBD NR 1 FLOOR SILL. R & R LT OUTBOARD NR 1 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION IN GALLEY AREA ON RH DIAMOND GUSSET AT FRAME 22. RAR DIAMOND GUSSET ON RH AT FRAME 22 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION IN GALLEY AREA ON CENTER FWD DIGITAL. ACCOMPLISHED REPAIR OF GALLEY AREA CENTER FWD DIGITAL IAW EMB 145 SRM 53-21-10 ITEM 2 FIGURE 201 SHEET 1.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION ON SERVICE DOOR CENTER SILL. BLENDED CORROSION ON SERVICE DOOR CENTER SILL IAW SRM 51-10-03. UPON FURTHER INVESTIGATION FOUND THE BLENDED AREAS TO BE PREVIOUSLY REPAIRED IAW EMB 145 SRM 53-21-02-RE ITEM 2 FIG. 201. REMAINING THICKNESS OF BLENDED AREAS FOUND TO BE WITHIN LIMITS OF REPAIR APPLICABILITY. APPLIED HYSOL TO BLENDED AREAS OF THE SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-02-RE, ITEM 2 STEPS I ANDO ONLY.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

CORROSION ON SERVICE DOOR AFT FLOOR SILL. R & R SERVICE DOOR AFT FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,490 hrs · 42,373 cycles

BAGGAGE DOOR LOWER INBOARD PROFILE HAS CORROSION AROUND NUTPLATES. RAR BAGGAGE DOOR LOWER INBOARD PROFILE IAW EMB 145 SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 45,490 hrs · 42,373 cycles

FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AT RIVET ON FR 77 BETWEEN STR 6R/7R. INSTALLED SKIN BUSHING FOR REPAIR OF FUSELAGE EXTERNAL SKIN AT RIVET ON FR 77 BETWEEN STR 6R/7R IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213. AND EO1-53-25-0426

Part: SKIN — CHAFED (ZONE 800) · airframe 45,409 hrs · 42,373 cycles

BAGGAGE DOOR INNER SKIN IS CHAFED 2 PLACES AT PREVIOUSLY BLENDED AREA AT HB3 AND VB2. RAR BAGGAGE DOOR INNER SKIN IAW EMB 145 SRM 51-40-02

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 45,490 hrs · 42,373 cycles

VERTICAL STABILIZER LH FWD DRAG ANGLE CRACKED. REMOVED AND REPLACED CRACKED VERTICAL STABILIZER LH FWD DRAG ANGLE IAW EMB145 SRM 51-40-02 AND INFORMATION CONTAINED IN SRM 53-31-01RE, ITEM 11, FIG 219.

Part: BLEED VALVE — FAULTED (NR 1 ENG)

HSV 1 FAIL ON EICAS DURING T/O ROLL. R & R ENGINE BLEED VALVE 1 IAW AMM 36-11-05. OPS CHECK GOOD,. ACFT IS OK FOR SERVICE

Part: CONTROLLER — FAULTED (ZONE 200) · airframe 45,438 hrs · 42,315 cycles

IN DESCENT FROM 24,000 FT AT SINK RATE OF 4,000 FT/MIN PRESSURIZATION INDICATION WENT INTO RED UNTIL UNDER 10,000 FT AND MANUAL DUMP. PERFORMED OPS CEHCK IRT AMM TASK 21-31-00-700-802-A. OPS CHECK GOOD. R & R DIGITAL CONTROLLER AS A MAINTENANCE PRECAUTION IRT AMM 21-31-01-000/400-801-A. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: OXYGEN MASK — DAMAGED (ZONE 200) · airframe 45,438 hrs · 42,315 cycles

FLIGHT CREW O2 MASKS DO NOT SEAL TO FACE AND MASK MICS INOP FACT 12OCT25 19:19 RIC R+R #100/200 CREW OXYGEN MASKS IAW AMM TASK 35-10-10-000/400-801-A. OPS CHECK GOOD, LEAK CHECK GOOD. OK FOR SERVICE. #1 PN:MC10-02-106 SN:SEO1454 TOTAL TIME: 15436.9, TOTAL CYCLES: 16010, TIME SINCE OH: 14436.9

Part: DUCT — DISCONNECTED (ANTI-ICE VALVE) · airframe 43,966 hrs · 40,644 cycles

WING A/ICE FAIL CAUTION WITH ICE CONDITION A/I INOP WARNING. ALB FOUND #2 WING A/I VALVE DUCT CONNECTION LEAKING AT LEADING EDGE AND #1 PRESSURE REGULATOR VALVE LEAKING R&R O-RING AT LEADING EDGE CONNECTION IAW EMB-145 AMM 57-41-00. R&R #1 PRESSURE REGULATOR VALVE IAW EMB-145 AMM 21-31-05. OPS& LEAK CHECK GOOD FOR BOTH THE LEADING EDGE CONNECTION & THE PRESSURE REGULATOR VALVE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,031 hrs · 38,482 cycles

ATTEMPTED #2 ENGINE START. HUNG AT 30%, ATC ADVISED ENGINE WAS SMOKING BUT CLEARING UP. TAXIED BACK TO GATE ON ENGINE 1. OPERATION REPORTED SMOKE AS WELL AS FUMES UPON AIRCRAFT RETURNING TO GATE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,171 hrs · 37,477 cycles

BURNT RUBBER SMELL IN FLIGHT DECK AND CABIN. INSP COCKPIT NO-DEFECTS NOTED RAN BOTH PACKS ON APU BLD NO BURNING SMELL NOTED GROUND RAN BOTH ENGINES OPS 1&2 SYS AND BOTH PACKS. NO BURNT RUBBER SMELL NOTED A/C OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,164 hrs · 37,469 cycles

00246 PROTRACTOR NUTPLATE MISSING ON TRAIL RUDDER LH SIDE REPLACE WITHIN 5000 FC PER SRM 55-40-01. REPAIRED RUDDER II LH SIDE IAW REPAIR #6 OF SRM 55-40-01,

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,164 hrs · 37,469 cycles

00245 COMPLY WITH PERMANENT REPAIR AT LOCATION FR67 & STR21L WITHIN 1200 FLIGHTCYCLES OR THE NEXT HEAVY CHECK WHICHEVER COMES FIRST AS OF OCTOBER 12, 2022 PER SECTION 5 OF ETD 2022-145-031648 REV A AND SRM1142 53-31-01-RE FINAL ACTION. COMPLIED WITH PERMANENT REPAIR AT LOCATION FR67 AND STR21L IAW EMBRAER ETD2023-145-012958 REV. :/ DATED MAY 23, 2023. THIS CLOSES DMT 35.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,164 hrs · 37,469 cycles

00238 LH AFT SIDE OF AIRCRAFT, JUST FWD OF THE APU WAS HIT BY A MANLIFT, PUTTING A HOLE IN THE AIRCRAFT SKIN, REPAIR REQUIRED. REPAIRED LH SIDE OF AIRCRAFT IAW EMBRAER ETD2023-145-014130

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,164 hrs · 37,469 cycles

00229 CORROSION ON L/H FLOOR SILL BETWEEN FR 36 AND FR41. : REMOVED CORRODED LH FLOOR SILL FR36 AND FR41 AND INSTALLED NEW SERVICEABLE LH FLOOR SILL PN: 145-25800-009 IAW EMB-145 SRM 51-40-02PR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00188 SERVICE DOOR SILL IS CORRODED BETWEEN FRM20 AND FRM22. REPAIRED SERVICE DOOR SILL IAW EMB145LR SRM 53-21-02-RE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00191 LH Y -479 FLOOR BEAM CAP FS X9551-X11990 SEGMENT IS CORRODED. : REMOVED AND REPLACED LH FLOOR CROSSBEAM P/N 145-32636-403 BETWEEN Y -479 AND Y -758 FS 31 EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00192 LH Y -479 FLOOR BEAM CAP FS X7065-X9551 SEGMENT IS CORRODED. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP (GUSSET, FLOOR) PN:145-30633-001 IAW EMB-145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00194 FRM35 LH FLOOR CROSSBEAM IS CORRODED BETWEEN Y -479 AND Y -758. REPAIRED FRM35 LH FLOOR CROSSBEAM Y-479 AND Y-758 IAW ETD2023-145-014599 REV A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00190 LH FLOOR SILL FS X9551-X11990 SEGMENT IS CORRODED. :INSTALLED NEW SERVICEABLE LH FLOOR SILL AT FS X9551-X11990 (STA 9399.0 TO STA 1108.0) IAW EMB 145LR SRM 51-40-02-PR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,164 hrs · 37,469 cycles

00196 CENTER Y 0 FLOOR BEAM CAP FS X9551-X11990 SEGMENT IS CORRODED. REMOVED CORRODED GUSSET AND INSTALLED NEW SERVICEABLE GUSSET (FLOOR BEAM CAP) PN:145-30633-006 IAW EMB-145 SRM 51-40-02PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00195 CENTER Y 0 FLOOR BEAM LH FLANGE IS CORRODED BETWEEN FRM28 AND FRM29. :INSTALLED 1 EA. NEW OMEGA BEAM @ Y0.00 FR. 22 - 29 IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00187 PASSENGER DOOR SILL FLOOR SUPPORT ANGLES BETWEEN FRM16 AND FRM17 ARE CORRODED. : INSTALLED NEW FWD AND AFT PAX DOOR LOWER FLOOR SUPPORT ANGLES BETWEEN FRAME 16 AND FRAME 17 IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,164 hrs · 37,469 cycles

00198 L/H LOWER PYLON SKIN T/E HAS 1EA. DENT ON THE I/B SIDE THAT MEASURES 1" DIA.X 0.008" DEEP. REPAIRED LH LOWER PYLON SKIN T/E 1EA DENT ON THE IB SIDE IAE EMB145 SRM 54-50-01 REPAIR #4

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00189 LH FLOOR SILL FS X7065-X9551 SEGMENT IS CORRODED BETWEEN FRM25 AND FRM27. REMOVED AND REPLACED LH FLOOR SILL BETWEEN FRM25-27 IAW EMB145LR SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00158 CORROSION FOUND ON LH 497.00 FLOOR BEAM BETWEEN FRM 43-45. : INSTALLED NEW SERVICEABLE GUSSET PN:145-30634-005 IAW EMB-145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00154 CORROSION FOUND ON LH FLOOR SILL BETWEEN FRM 48-49. : INSTALLED FLOOR SILL BETWEEN FRM48-49 AND DRILLED UP NEW SERVICEABLE FLOOR SILL PN 145-25800-015 IAW EMB145LR SRM 51-40-02-PR & 51-20-03-PR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00148 BAGGAGE BAY DOOR CUTOUT UPPER BEAM IS CORRODED. REF IPC 53-31-15 ITEM 180. REMOVED DAMAGE BAGGAGE BAY DOOR CUTOUT UPPER BEAM AND REPAIRED IAW EMB ETD2023-145-012972

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,165 hrs · 37,469 cycles

00157 CORROSION FOUND ON LH FLOOR SILL BETWEEN FRM 39-45. INSTALLED NEW FLOOR SILL P/N 145-25800-613 AT FRM 42 - FRM 46 IAW EMB145LR SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,133 hrs · 37,429 cycles

LH OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATT CHARGER ASSY/ WITH RETAINING HARDWARE, AND REMOVED AND REPLACED BATTERY PACK IAW WC 33-70-19 AT POSITION 400

Part: SEAL — LEAKING (PAX DOOR) · airframe 40,572 hrs · 36,817 cycles

LOUD WHISTILING NOISE FROM MAIN CABIN DOOR ABOVE 10000 FEET. ON INSPECTION FOUND 2 SMALL GAPS IN THE SEALANT OF THE MAIN DOOR FRAME RUBBER SEAL. APPLIED RTV-157 TO THE AFFECTED AREAS PER SRM 51-20-01-PR. PERFORMED PRESSURE CHECK OF AIRCRAFT AND NO LEAKS WERE FOUND. AIR CRAFT OK FOR SERVICE. CLEAR MEL 21-12-3

Part: NONE — NONE · airframe 40,071 hrs · 36,233 cycles

PDIS 906 36-12 2480401 12SEP22 CLT CLOSE EXHAUST FUMES WHEN PACK 1 OPERATING ON APU BLEED FACT 13SEP22 02:13 MDT INSPECTED AND FOUND C/P AT APU BLEED VALVE CONNECTED. RAN APU BLEED AND BOTH PACKS FOR 20 MINS. NO EXHAUST SMELL NOTED AND NO HISTORY IN 30 DAYS. OK FOR SERVICE.

Part: NONE — NONE · airframe 39,253 hrs · 35,284 cycles

PDIS 906 23-40 2632231 01APR22 CLT CLOSE SQUELCH FROM INTERPHONE DURING FLIGHT DECK TO FLIGHT DECK AND FLIGHT DECK TO CABIN COMMUNICATION. FACT 01APR22 17:13 CLT PERFORMED PASSENGER ADDRESS AND CABIN INTERPHONE SYS OPS CHECK IAW AMM 23-31-00-700-801-A OPS CHECK GOOD OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 37,366 hrs · 33,279 cycles

PDIS 906 21-00 2318501 07APR21 CLT CLOSE LIGHT BURNING OIL SMELL WITH BLEEDS ON. DISIPATED SOON AFTER TAKEOFF. STRONGER NUMBER 2 PACK FACT 07APR21 13:28 CLT OPERATED BOTH PACKS WITH APU BLEED NO SMELL NOTED INCOCKPIT OR CABIN. OPERATED BOTH PACKS OF EACH ENGINE INDIVIDUALLY WITH NO SMELLS NOTED IN COCKPIT OR CABIN. BLEED AND PACK SYSTEMS OPERATE NORMALLY AT THIS TIME. A/C OK FOR SERVICE.

Part: STRUCTURE — CORRODED (LAV DUMP VALVE) · corrosion level 2 · airframe 36,812 hrs · 32,688 cycles

EXTERNAL LAV DUMP VALVE BUCKET CORRODED AT VALVE MARKED. INSTALLED SERVICEABLE LAV BUCKET, IAW EMB 145 SRM 51-40-02. SEE TASKS AND WIPS FOR DETAILS.

Part: SKIN — CRACKED (FRAME 79) · airframe 36,812 hrs · 32,688 cycles

RT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 79. INSTALLED SERVICEABLE RIVET AND REPAIR SKIN BUSHING AT FR 79 BETWEEN STR 3R-4R, IAW EO1-53-20-0406.

Part: SKIN — CRACKED (FRAME 79) · airframe 36,812 hrs · 32,688 cycles

LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 4 EA FR 79. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 78, IAW PIEDMONT EO1-53-20-0407. 2 LOCATIONS WERE FOUND NOT TO BE CRACKED.

Part: HOUSING — WORN (HORIZONTAL STAB) · airframe 36,812 hrs · 32,688 cycles

HORIZONTAL STAB BUSHING HOUSING 2 WORN. R & R 2 HORIZONTAL STAB BUSHINGS, IAW EO1-55-20-0400.

Part: FRAME — CRACKED (FRM 25) · airframe 36,812 hrs · 32,688 cycles

FR 25 IS CRACKED BETWEEN STR 16R-15R. PERFORMED SPLICE REPAIR OF FR 25 LOWER FRAME SECTION AND U-SHAPED DOUBLER, IAW EMB 145 SRM 53-00-04 ITEM 4 FIG 201 AND EO1-53-20-0397.

Part: SKIN — CRACKED (FRAME 77) · airframe 36,812 hrs · 32,688 cycles

RT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 5 EA FR 77. INSTALLED SERVICEABLE RIVET AND REPAIR SKIN BUSHING AT FR 77 BETWEEN STR 8R-9R, IAW EO1-53-20-0406. SEE WIPS AND TASKS FOR DETAILS.

Part: SKIN — CRACKED (FRAME 77) · airframe 36,812 hrs · 32,688 cycles

LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 77. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 77, IAW PIEDMONT EO1-53-20-0407.

Part: FRAME — GOUGED (FRM 68) · airframe 36,812 hrs · 32,688 cycles

FR 68 RT SIDE HAS MULTIPLE GOUGES ON FWD SIDE AT NUTPLATES. REPAIRED FR 68 RT SIDE HAS MULTIPLE GOUGES ON FWD SIDE AT NUTPLATES, IAW PIEDMONT EO-1-05-20-0410 AND EO1-53-20-0390. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 36,812 hrs · 32,688 cycles

BAGGAGE DOOR CUTOUT SHEAR CLIP AT FR 65 CORRODED AT LOWER END. PERFORMED REPAIR AT BAGGAGE DOOR CUTOUT SHEAR CLIP AT FR 65 AT LOWER END, IAW EO1-53-20-0398.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · corrosion level 2 · airframe 36,812 hrs · 32,688 cycles

LEFT OMEGA BEAM HAS CORROSION BETWEEN FRAME, 58 AND FRAME 59. PERFORMED REPAIR OF LT OMEGA BEAM BETWEEN FRAME 58 AND FRAME 59, IAW E01-53-20-0399.

Part: DOOR SILL — CORRODED · airframe 36,812 hrs · 32,688 cycles

53-20-10 SERVICE DOOR CENTER SILL IS CORRODED. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR CENTER SILL, IAW EMB145 SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 79) · airframe 36,812 hrs · 32,688 cycles

LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 79. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 79, IAW PIEDMONT EO1-53-20-0407.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,622 hrs · 32,478 cycles

PETROLEUM BASED FUMES PRESENT WHEN RUNNING PACKS FROM APU. MAINTENANCE. RESET C/B'S. INSPECTED APU FOUND OIL LEVEL GOOD AND NO OIL OR FUEL LEAKS. RAN APU FOR 1 HOUR WITH APU BLEED AND BOTH PACJKS ON, NO PETROLEUM BASED FUMES NOTED IN CABIN OR COCKPIT. OK FOR SERVCIE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 35,959 hrs · 31,701 cycles

CHO RAMP CONTROL WAS ADVISED BY THE CREW THAT THEY HAD SMOKE IN THE FLIGHT DECK DURING TAXI AND THEY CALLED CFR. ADVISED MOCC OF THE POTENTIAL SITUATION, AND THEY ADVISED THAT THEY WERE O THE PHONE WITH THE CA AND IT WAS MERELY A BAGGAGE COMPARTMENT FIRE TEST LIGHT WHICH REMAINED ILLUMINATED. THE FLIGHT ATTENDANT CONFIRMED THAT THERE WAS NO SMOKE OR FIRE PER HER REQUIRED CHECKS. MOCC HAD THE CREW HOLD THE TEST SWITCH FOR 3 SECONDS AND THE FIRE TEST LIGHT EXTINGUISHED.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 35,638 hrs · 31,327 cycles

PDIS 906 36-21 2082641 02NOV19 BUF CLOSE BLEED 1 LEAK EICAS MSG IN FLIGHT DURING ICING CONDIT IONS. FACT 03NOV19 06:34 BUF PERFORMED OPS CHECK OF BLD SYS FAILED BLD 1 VLV FAIL . RNR BLD VLV 1 PERFORMED OPS CHECK OF BLDS SYS OPS CHECK GOOD IAW AMM 36-00-00 AND 36-11-05 OK FOR SERV ICE. NO FURTHER LEAKS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,622 hrs · 31,308 cycles

BLD 1 LK WARNING INFLT....FIX: GND RAN ENGINE FOR 30 MINUTES W/ BLEED PRESS ON. OPS CK BLEED SYS IAW 76-00-00-700-801A. CND. OPS CHECK GOOD

Part: BLEED VALVE — LEAKING (LT ENGINE) · airframe 35,577 hrs · 31,264 cycles

PDIS 906 36-11 1898991 20OCT19 ALB CLOSE BLD 1 LEAK INDICATED IN FLT FACT 20OCT19 11:18 ALB FOUND BLEED LEAK AT LH ENGINE BLEED VALVE CLEANED MA TING FLANGES RETORQUED BAND CLAMPS IAW EMB 145 AMM 3 6-11-05 R&R CLAMP AT PRECOOLER IAW EMB 145 AMM 36-11 -04 OPS AND LEAK CHECK GOOD IAW EMB 145 AMM 36-00-00 , OK FOR SERVICE

Part: FAN — FAULTED (RECIRCULATION) · airframe 35,512 hrs · 31,187 cycles

ELECTRICAL ODOR FLT DECK AND CABIN AT LANDING. AIR COND PACKS MEL,D MX ISOLATED TO PACK #1. NOTE: 10OCT19 INSP & FOUND #1 RECIR FAN AT FAULT. R&RD FAN PER 21-24-01-04. OPERATED BLEEDS. OPS & LK CHECK GOOD. NO ODOR DETECTED.(MDT)

Part: UNKNOWN — ODOR · airframe 35,460 hrs · 31,121 cycles

APU HAD A STRONG OIL BURNING ODOR WITH BLEED SELECTED. RAN PACK 1 AND 2 FOR 30 MIN WITH APU BLEED ON. COULD NOT DUPLICATE THE ODOR.

Part: UNKNOWN — SMOKE (CABIN) · airframe 35,336 hrs · 30,969 cycles

PDIS 906 05-50 1898563 09SEP19 RDU ASSGN IN CRUISE FLIGHT BURNING SMELL NOTED IN FLT DECK AND CABIN W/ NOTED VISIBLE SMOKE IN CABIN (REPORTED BY F/A) SMELL AND SMOKE DISSIPATED UPON DESCENDING WITH PACK 2 OVHT EICAS MSG PRESENT AFTER LANDING. AIRCRAFT IS CURRENTLY IN WORK PER MOCC.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,336 hrs · 30,969 cycles

PDIS 906 05-50 1898561 08SEP19 CLT CLOSE ELECTRICAL SMELL IN FLIGHT DECK FACT 08SEP19 22:55 CLT INSPECTED BEHIND RELAY PANELS, CHECKED ENGINE INTAKES. RAN BOTH PACKS. NO ELECTRICAL SMELL NOTED. UPON FURTHER INSPECTION, FOUND OIL SMELL PRESENT INTERMITTENTLY WITH PACK 1 RUNNING. SEE SEQ 2 FOR PACK MEL.

Part: ACM — FAILED (AC BAY) · airframe 34,306 hrs · 29,799 cycles

PDIS 906 21-50 1875141 01MAR19 ROC CLOSE PACK 1 OVER HEAT CAUTION MESSAGE DISPLAYED FOLLOWED BY BURNING SMELL IN CABIN AND FLIGHT DECK. FA REPORTS A HAZE. CYCLED PACK 3 TIMES. SMELL IS ONLY ASSOCIATED WITH PACK 1. FACT 01MAR19 19:07 ROC MX INSP NR 1 PACK AND T/S IAW FIM 21-20-00-810-801-A. FOUND NR 1 PACK ACM FAILED. SEE SEQ 2 BELOW FOR MEL OF NR 1 PACK.

Part: ACM — FAILED (AC BAY) · airframe 34,306 hrs · 29,799 cycles

PDIS 906 1-50 1875142 01MAR19 ROC CLOSE DURING T/S OF LP187514-1 FOUND NR 1 PACK ACM FAILED. MEL 01MAR19 17:59 ROC C06015 21-13-2 AIR CONDITONING PACK N650 & ABOVE FACT 02MAR19 07:26 MDT R&R NR 1 PACK ACM REF 21-51-03 OPS CK GOOD OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,306 hrs · 29,799 cycles

PDIS 906 21-50 1875143 01MAR19 MDT CLOSE PACK 2 OVR HEAT CAUTION MSG DISPLAYED ON GROUND. 25445 00 VAG FACT 02MAR19 07:49 MDT RAN PACK NR 2 IN MANUAL & AUTO FOR 15 MINUTES, CND OVERHEAT MSG, OK FOR SVC AT THIS TIME.

Part: INVERTER — FAULTY (CABIN) · airframe 34,183 hrs · 29,644 cycles

EMERGENCY LIGHTS INOP AT 1A AND 2A AT FLOOR. TROUBLESHOT AND FOUND GALLEY CEILING INVERTER PS 8501 TO BE AT FAULT. (SHORT SIGNED). R&R EMERGENCY LIGHTS INVERTER ASSY AS REQ. OPS CK GOOD.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 34,104 hrs · 29,553 cycles

NDIS 906 33-20 0006990 18JAN19 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS FLICKERING. FACT 18JAN19 10:36 SBY R&R LIGHT BULB AT SAID LOCATION AND RE-SECURED THE COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,104 hrs · 29,553 cycles

NDIS 906 33-20 0007020 18JAN19 SBY CLOSE MOST FWD FLOOR EMERGENCY LIGHT STRIP IS INOP. FACT 18JAN19 10:40 SBY R& R MOST FWD LIGHT STRIP IAW AMM TASK NUMBERS 33-50-12-00-801-A AND 33-50-12-400-801-A.

Part: WASHER — MISINSTALLED (PROXIMITY SWITCH) · airframe 33,844 hrs · 29,237 cycles

PDIS 906 32-61 2044661 29NOV18 RIC CLOSE LG AIR/GROUND FAIL ON DEPARTURE. FACT 29NOV18 14:26 RIC INSP AND FOUND NLG WOW PROX SW LOCK WASHER TO BE INORRECTLY INSTALLED ON TOP OF THE BRACKET CAUSING THE SW CLEARANCE TO BE WRONG. REMOVED NLG WOW PROX SW AND REINSTALLED WITH LOCK WASHER IN THE CORRECT LOCATION. VERFIED GAP ADJ. IN REF TO AMM 32-63-05-700-803-A. REF AMM 32-63-02-400-801-A/400 AND 32-63-02-100-801-A/400 FOR NLG WOW SW REMOVAL AND INSTALLATION. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 33,179 hrs · 28,463 cycles

BRAKE DEGRADED EICAS MESSAGE, ON T/O ROLL. T/O ABORTED. BLED ALL FOUR BRAKES AND TESTED WHEEL SPEED TRANSDUCERS AND BRAKES. CND. REF 32-41-00.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 33,143 hrs · 28,419 cycles

BRAKE DEGRADED MSG ON AND OFF 5 TIMESDURING TAXI OUT WITH NO CMC MESSAGES, ONLY WHEN APPLYING BRAKES. RT I/B BRAKE APPEARS HOTTER THAN THE REST. BLED ALL BRAKES. PERFORMED TAXI CHECK. LEAK AND OPS CHECK GOOD. NO EICAS MESSAGES. NO OTHER DEFECTS NOTED. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,052 hrs · 28,317 cycles

LOWER EMERGENCY LIGHT WON'T ILLUMINATE AT THE SERVICE DOOR AREA. R & R LOWER THE EMERGENCY LIGHT IAW AMM 33-50-13-000/400-801-A, OK FOR SERVICE.

Part: WIRE — NOT SEATED (EMERGENCY LIGHT) · airframe 33,052 hrs · 28,317 cycles

EMERGENCY LIGHT STRIP AT ROW 1 WOULD NOT ILLUMINATE. SEATED THE WIRES IN THE LIGHT. OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 33,004 hrs · 28,253 cycles

DURING CLIMB, THE FIRST OFFICER NOTICED THE CABIN PRESSURE CLIMBING, SWITCHED TO MANUAL CONTROL, AND LEVELED OFF AT FL 228. STARTED QRH MEMORY ITEMS FOR RAPID DEPRESSURE, NO EICAS MESSAGES NOTED. INITIATED RAPID DEPRESSURE PROCEEDURE, DUE TO PUTTING CONTROL IN MANUAL AND CABIN ALTITUDE. R & R THE MANUAL CONTROLLER IAW AMM 21-31-02. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT/CABIN) · airframe 32,986 hrs · 28,231 cycles

SMOKE IN CABIN AND FLT DECK AT 24,000 FT, LASTED FOR APPROXIMATELY 5 MINUTES THEN DISSIPATED. DURING TAXI, THE NR 2 PACK2 OVERHEAT MESSAGE. ELECTRICAL BURNING ODOR AT ROW 8-11 IN CABIN.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,884 hrs · 28,109 cycles

EMREGENCY EXIT SIGN ABOVE THE SERVICE DOOR DID NOT ILLUMINATE. R & R THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD

Part: TUBE — DISCONNECTED (ANTI-ICE SYS) · airframe 32,657 hrs · 27,873 cycles

WING ANTI-ICE FAILED EICAS. PERFORMED A VISUAL INSPECTION OF ALL WING ANTI-ICE COMPONENTS AND ATTACHING LINES, AND FOUND THE LOW PRESSURE TRANSDUCER DAMPER TUBE ASSY TO WING ANTI-ICE DUCT WAS NOT CONNECTED TO WING ANTI-ICE DUCT, ATTACHED THE TUBE ASSY TO WING ANTI-ICE DUCT IAW AMM 30-11-08, LEAK AND OPS CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (FRAME 50) · airframe 32,656 hrs · 27,871 cycles

LEFT UPPER ATTACH ANGLE FOR OVERWING LATERAL PANEL IS CRACKED AT FUSELAGE FRAME 50. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.

Part: ATTACH ANGLE — CRACKED (FRAMES 47-48) · airframe 32,656 hrs · 27,871 cycles

RIGHT LOWER ATTACH ANGLE FOR THE OVERWING PANEL IS CRACKED BETWEEN FUSELAGE FRAMES 47 AND 48. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, AND ETN -EM-53-142.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,656 hrs · 27,871 cycles

THE EMERGENCY CEILING LIGHT IN PANEL 243DLC IS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-08.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 32,426 hrs · 27,662 cycles

LAV SMOKE EICAS MESSAGE DURING CLIMB OUT THROUGH 12,000 FT SMOKE ALARM DID SOUND. INSP LAV NO EVIDENCE OF SMOKE OR ODOR. PERFORMED ENGINE, APU & PACK RUN W/CREW, NO DEFECTS NOTED. DETERMINED TO BE LAV SMOKE DETECTION SYSTEM. DEFERRED LAV SMOKE DET SYSTEM. NO ASSOCIATED CMC MESSAGES. M PROCEDURES C/W. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-14-01-000-801 AND 26-14-01-400-801 OPS CHECK GOOD MEL RESTORED. LAV SMOKE DETECTOR P/N AML 4195403-1 S/N FTA719-01.

Part: CONTROL PANEL — FAILED (PITCH TRIM) · airframe 32,392 hrs · 27,624 cycles

PITCH TRIM MAIN SYSTEM CUTOUT INOPERATIVE IN FLIGHT. REMOVED AND REPLACED TRIM CONTROL PANEL IAW AMM 20-15-10. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERENCY LIGHT) · airframe 32,299 hrs · 27,548 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMPS IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. NO FAULT FOUND.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 30,792 hrs · 26,150 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10 , OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 28,762 hrs · 24,308 cycles

NUMBER 1 HYD QTY LOW INFLIGHT. SERVICED NR 1 HYD SYS IAW AMM 12-13-01. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,718 hrs · 24,264 cycles

AFT OVERHEAD EMER LIGHT INOPERATIVE. R & R AFT OVERHEAD EMER LIGHT IAW AMM TASK 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 28,592 hrs · 24,169 cycles

LAVATORY DETECTOR HORN FOR SMOKE ACTIVATED CLIMBING THROUGH 12,000. FLIGHT ATTENDANT INVESTIGATED LAV FOR SMOKE & FIRE, DID NOT FIND ANY EVIDENCE OF FIRE OR SMOKE. CLIMBING THROUGH 20,000 FT ECAC LAV SMOKE WARNING. FOLLOWED QRH FOR LAV SMOKE & LAV DETECTOR RESET & TESTED. MONITORED LAV REMAINDER OF FLIGHT, LAV SMOKE WARNING EXTINGUISHED AFTER ABOUT 1 MIN. INSPECTED LAV FOR ANY OBVIOUS DEFECTS, NO EVIDENCE OF FIRE OR SMOKE NOTED. PERFORMED LAV SMOKE DETECTION SYS. OPERATIONS CHECKED WITH NO DEFECTS NOTED IAW AMM 26-14-00. PERFORMED ENG SMOKE & ODOR TROUBLESHOOTING SUPPLEMENT ETN EM-72-034 WITH NO DEFECTS NOTED. OK FOR SERVICE AT THIS TIME.

Part: WIRE — BROKEN (CABIN) · airframe 28,279 hrs · 23,871 cycles

NUMBER 1 EMER LIGHT STRIP HAS ONE EACH BROKEN WIRE. R & R NR 1 EMER LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,272 hrs · 23,866 cycles

RIGHT RVSM AREA HAS DAMAGE, DENT, BETWEEN FRAME 12A & 13, JUST BELOW & AFT OF OXYGEN SERVICE PANEL. REPAIRED DAMAGE, BETWEEN FRAME 12A & 13, JUST BELOW & AFT OF OXYGEN SERVICE PANEL IAW SRM 53-00-22.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,272 hrs · 23,866 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1951.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 28,272 hrs · 23,866 cycles

RIGHT FWD EXTERIOR EMER LIGHT WIRE HARNESS IS BROKEN ABOUT A FOOT FROM CONNECTOR P8560. REPAIRED RT FWD INSPECTION LIGHT WIRE HARNESS IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 28,272 hrs · 23,866 cycles

NUMBER 1 EMER LIGHT STRIPS HAS ONE EACH BROKEN WIRE. R & R NR 1 EMER LIGHT STRIPS IAW AMM 33-50-12, OPERATIONS CHECKED GOOD. SEE TASK & WIPS FOR DETAILS.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,173 hrs · 23,774 cycles

AFT FLASHLIGHT CRADLE BROKEN. R & R AFT FLASHLIGHT ASSEMBLY IAW MM 33-50-16.

Part: BATTERY — NOT SEATED (CABIN) · airframe 27,520 hrs · 23,141 cycles

COCKPIT STEP EMER EXIT IDENTIFIER WILL NOT ILLUMINATE. TRANSFERRED TO NRWC 906-CMH-02348. PERFORMED RESET OF EMER BATTERY POWER SUPPLY AT POSITION 1 IAW CMM 25-60-03. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 27,358 hrs · 22,997 cycles

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

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,534 hrs · 22,259 cycles

CAPTAINS FLASHLIGHT IS INOPERATIVE. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,007 hrs · 21,802 cycles

CAPTAINS FLASHLIGHT NEEDS TO BE REPLACED. REPLACED IAW MM 33-50-16. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 25,748 hrs · 21,563 cycles

CLIMBING OUT OF 10,000 FT ACFT WOULD NOT PRESSURIZE. CABIN ALT ON EICAS WENT TO RED 10,000. ACCOMPLISHED PRESSURIZATION OF ACFT WITH BOTH PACKS IAW ITEM 3 OF THIS LOG PAGE. NO FAULTS FOUND IAW AMM-21-31-00.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 25,536 hrs · 21,351 cycles

FLIGHT ATTENDANT ADVISES AFT FLASHLIGHT HOUSING IS DAMAGED. R & R AFT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,213 hrs · 21,060 cycles

WITH EMER LIGHT SWITCH IN ARM POSITION EMER LIGHTS ON FROM ROW 12 TOWARDS BACK. PREVIOUS WRITE UP PG 3688619. R & R NR 4 BATTERY POWER SUPPLY & BATTERY PACK IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A SN 66556.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,854 hrs · 20,756 cycles

CENTER CEILING EMER LIGHT INOPERATIVE. R & R CTR CEILING EMER LIGHT IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 24,846 hrs · 20,748 cycles

PARKING BRAKE ON LIGHT IS INOPERATIVE. FOUND CB FOR PARKING BRAKE OUT. RESET & OPERATIONS CHECKED PARKING BRAKE IAW AMM 32-43-00. OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 24,468 hrs · 20,455 cycles

DURING CLIMB OUT PTRIM BACKUP INOPERATIVE WARNING ILLUMINATED ON EICAS. R & R HSCU IAW AMM 27-40-01, OPERATIONS CHECKED GOOD.

Part: TRIM SWITCH — DIRTY (HORIZ STAB) · airframe 24,466 hrs · 20,452 cycles

PTRIM BACKUP INOPERATIVE MSG ON EICAS. CLEANED BACKUP PTRIM SWITCHES IAW AMM 27 40 04. OPERATIONS CHECKED OK.

Part: BONDING STRAP — CORRODED (LT WING) · airframe 24,009 hrs · 20,020 cycles

LEFT WINGTIP BONDING STRAP CORRODED. REPAIRED LT WINGTIP BONDING STRAP IAW AEA ERS-EM-5700-127.

Part: BONDING STRAP — CORRODED (RT WING) · airframe 24,009 hrs · 20,020 cycles

RIGHT WINGTIP BONDING STRAP CORRODED. REPAIRED RT WINGTIP BONDING STRAP IAW AEA ERS-EM-5700-127.

Part: COVER — DAMAGED (CABIN) · airframe 24,009 hrs · 20,020 cycles

8 EACH EMERGENCY LIGHT PROXIMITY STRIP COVER PANELS DAMAGED. R & R 8 EACH EMERGENCY PROXIMITY LIGHT STRIP COVER PANELS AS REQUIRED. SEE BOW 152362 FOR INSTALLATION OF EMERGENCY PROXIMITY LIGHT STRIPS.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,009 hrs · 20,020 cycles

EMERGENCY PROXIMITY LIGHT STRIPS NR 2, NR 3 & NR 7 DAMAGED. R & R NR 2, NR 3 & 7 EMERGENCY PROXIMITY LIGHT STRIPS AS REQUIRED. SEE BOW 152362 FOR INSTALLATION OF LIGHT STRIPS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,009 hrs · 20,020 cycles

RIGHT EMERGENCY EXIT EMERGENCY WHITE LIGHT INOPERATIVE. R & R RT EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-07, CHECKED GOOD.

Part: PANEL — FAILED (EMERGENCY LIGHT) · airframe 23,877 hrs · 19,908 cycles

MEL 33-1 AUTH 030475-C ORIG AML 3016803 EMERGENCY LIGHT OVERHEAD PANEL BACK LIGHTING INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT PANEL IAW AMM 20-13-10, OPERATIONS CHECKED GOOD IAW AMM 33-12-00 & 33-50-00, MEL ITEM RESTORED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,339 hrs · 19,495 cycles

LEFT OVERWING LARGE EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. R & R NR 4 DC AC INVERTER IAW 145 AMM 33-50-14, OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,260 hrs · 19,434 cycles

UPPER EMERGENCY LIGHT EXIT SIGN AT LT EMERGENCY EXIT OVERWING HATCH FAILS TO ILLUMINATE. R & R NR 4 INVERTER IAW AMM 33-50-11, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 22,762 hrs · 19,030 cycles

CAPTAIN`S FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW AMM IAW 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 22,596 hrs · 18,897 cycles

FWD EMGERGENCY FLASHLIGHT MISSING. REPLACED FWD EMG FLASHLIGHT AS REQUIRED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,203 hrs · 18,562 cycles

FIRST FLOOR EMERGENCY LIGHT INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: INVERTER — UNSERVICEABLE (EMGERGENCY LIGHT) · airframe 22,203 hrs · 18,562 cycles

FIRST FLOOR EMERGENCY LIGHT STRIP IS INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (CARGO DOOR) · airframe 22,091 hrs · 18,469 cycles

CREW REPORTED AT 8000 FT DURING CLIMB, RECEIVED A "BAGGAGE DOOR OPEN" ON EICAS MESSAGE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ACFT LANDED WITHOUT INCIDENT. ON THE RETURN FOR LANDING EICAS MESSAGE AND DOOR OPEN INDICATION WENT AWAY AT 200 FT. ACFT REMOVED FROM SERVICE. R & R ACTUATOR LEVER ON CARGO DOOR SWITCH IAW AMM 52-76-01. OPS TESTED GOOD. ACFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 22,069 hrs · 18,448 cycles

THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT HOLDER WAS BROKEN. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT HOLDER IAW AMM 25-60-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 21,951 hrs · 18,342 cycles

THE CREW REPORTED THE FLASHLIGHT HOLDER IN THE REAR WAS BROKEN. THE FLASHLIGHT WORKS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFT CABIN FLASH LIGHT AND BASE IAW AMM 33-51-01. THE OPS TEST WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 21,719 hrs · 18,149 cycles

DURING MAINTENANCE INSPECTION, FOUND F/A FLASHLIGHT SWITCH INTERMITENT, LIGHT IS DIM. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT, OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 21,324 hrs · 17,832 cycles

ON FLIGHT 4200 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT CRADLE IAW EMB-145 M/M 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 21,091 hrs · 17,646 cycles

FLIGHT 4103. CREW REPORTED THAT AFTER TAKEOFF, RECEIVED AN EICAS LAV SMOKE WARNING MESSAGE. DECLARED AN EMERGENCY AND COMPLETED AOM VOL 1 PROCEDURES AND RETURNED TO DEPARTURE. MESSAGE EXTINGUISHED ON APPROACH. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE CARBON SEAL ASSEMBLY IAW MM 72-25-25, NO SMOKE WARNINGS, BURNING ODORS OR OIL LEAKAGE NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 20,943 hrs · 17,524 cycles

ON FLIGHT 3672 THE CREW REPORTED THAT AT CRUISE ALTITUDE FL 270 IN SMOOTH CONDITIONS THEY RECEIVED A HYD SYSTEM 1 LOW FLUID QUANTITY INDICATION. THE CREW MONITORED THE QUANTITY AND OBSERVED THAT FLUID GOING DOWN CONTINUOUSLY. THE CREW NOTIFIED DISPATCH WHEN IT BECAME APPARENT THEY WOULD LOOSE ALL FLUID. THE DIVERTED TO TLH AS HYD PRESSURE WAS DECREASING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 1 EDP IAW EMB 145AMM 29-10-03. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,878 hrs · 16,666 cycles

DURING B INSPECTION FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY OVERHEAD SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (AILERON) · airframe 19,585 hrs · 16,410 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT AILERON SURFACE DAMPER FITTING DAMAGED DURING AILERON REMOVAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING IAW E.O. EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAPPER VALVE — FAILED (LT WING) · airframe 19,584 hrs · 16,409 cycles

ON FLIGHT 3981, THE CREW REPORTED A POSSIBLE FUEL LEAK FROM CAPTAIN’S SIDE WING APPROX 3 FEET FROM TIP OF WING. THE FLIGHT ATTENDANT REPORTED A "SIGNIFICANT" AMOUNT OF FLUID LEAKAGE. LEAK STOPPED APPROX 7 MILES FROM LANDING. 100 LB FUEL IMBALANCE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING OUTER MOST FLAPPER VALVE IAW EMB 145 AMM 28-11-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 18,640 hrs · 15,672 cycles

DURING B-INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT IAW AMM TASKS 33-50-05-000-801-A AND 33-50-05-400-801-A; BULB-- NO FIX. PART NUMBER 1317. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY AND CHARGER IAW AE WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 18,541 hrs · 15,589 cycles

DURING B-INSPECTION FOUND EMERGENCY LIGHT SYSTEM NR 1 TO BE INOPERATIVE DURING PS-2 CHECK INSPECTION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT SYSTEM NR 1 BATTERY AND CHARGER ASSY IAW W/C 33-700-19, OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,464 hrs · 15,527 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT INOPERABLE. THE CEILING LIGHT AT ROW 3 WAS ALSO INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT IAW EMB AMM 33-50-10 STEPS 2L1-4 AND 3K1-4. PART NUMBER 1317. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT AT ROW 3 IAW EMB AMM 33-50-08 STEPS 2J1-2 AND 3(I)1-2. PART NUMBER 1317. REMOVED AND REPLACED THE NR 1 BATTERY AND EMERGENCY POWER SUPPLY UNIT IAW WORK J CARD 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW WORK CARD 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,380 hrs · 15,461 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD, OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY AND CHARGER IAW EMB 145 W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,260 hrs · 15,380 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD EMERGENCY LIGHT AT THE LEFT WING/FUSELAGE IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY POWER SUPPLY ASSEMBLY IAW EBM 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,868 hrs · 15,103 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIPS 2 & 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 3 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,748 hrs · 15,008 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY NR 1 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY NR 1 IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,677 hrs · 14,958 cycles

FOR FLIGHT 2789 MAINTENANCE FOUND THE COCKPIT FLOOD LIGHT AND 1ST AISLE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 EMERGENCY POWER SUPPLY UNIT CHARGER ASSEMBLY AND BATTERY IAW EM AMM 33-50-0. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,583 hrs · 14,875 cycles

DURING MAINTENANCE BASE VISIT FOUND EMERGENCY LIGHT POWER SUPPLY NR 1 NOT WORKING PROPERLY, HAS MULTIPLE EMERGENCY LIGHTS OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND NR 1 EMERGENCY BATTERY. ALL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 17,575 hrs · 14,871 cycles

ON FLIGHT 2783 THE CREW REPORTED THAT DURING CRUISE FLIGHT AT FLIGHT LEVEL 370 THEY RECEIVED AN EICAS MESSAGE "SPOILER FAIL" DISPLAYED AND SPOILER INDICATOR SHOWED OPEN. PER FLIGHT ATTENDANT VISUAL INSPECTION THEY APPEARED CLOSED. THE CREW DECLARED AN EMERGENCY AND HAD AN UNEVENTFUL LANDING AT THEIR DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB 145 MM 27-63-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,593 hrs · 13,356 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY STRIP NEXT TO THE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP NEXT TO EMERGENCY EXIT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — MALFUNCTIONED (CABIN DOOR) · airframe 15,030 hrs · 12,925 cycles

ON FLIGHT 3921 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO SECURE CLOSED. IT INDICATED CLOSED BUT THE EXTERIOR HANDLE HAS TO BE FORCED TO THE FLUSH POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED THE MAIN CABIN DOOR FRAME ROLLERS IAW EMB145 AMM 53-21-02. NO PARTS WERE REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,617 hrs · 12,640 cycles

DURING MAINTENANCE INSPECTION FOR FLIGHT 9810 THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND NOT TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP OF THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WHEEL — VIBRATION (NLG) · airframe 14,111 hrs · 12,237 cycles

ON FLIGHT 3670 THE CREW REPORTED EXCESSIVE NOSE WHEEL SHIMMY UPON LANDING AND ON TAXI TO THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE ASSEMBLY IAW WORK CARD 32-700-17. REMOVED AND REPLACED NR 3 AND NR 4 TIRES IAW 32-700-11. AS A PRECAUTION REMOVED AND INSTALLED THERMAL TEMPERATURE SWITCH BY LEFT DUAL TEMP CONTROL VALVE IAW EMB-145 AMM 36-20-00. THE OPERATIONAL CHECK WAS GOOD.

Part: AHRS — INOPERATIVE (NR 1) · airframe 8,573 hrs · 7,439 cycles

ON FLIGHT 3794, CREW REPORTED THEY HAD AHARS 1 INOPERATIVE IN FLIGHT AND DESCENDED OUT OF RVSM BECAUSE THAT MESSAGE MAKES THE AUTO PILOT INOPERATIVE. DID NOT HAVE ENOUGH FUEL AT FL280 TO MAKE IT TO DFW REMOVED AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 AHRS UNIT PER AMM 34-21-01. OPERATIONAL CHECKED GOOD ALSO DEFERRED RVSM 34-50 DUE TO REPLACEMENT OF AHRS. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER) · airframe 6,947 hrs · 6,172 cycles

NOTIFIED BY CREW VIA GRD LINE. ABORTED T/O AT LOW SPEED DUE TO RUD SYS 1 FAIL EICAS MSG. THE MESSAGE WENT AWAY AFTER FOLLOWING CHECK LIST. PERFORMED FIM OF RUDDER SYS INOP ON EICAS PER EMB 145 FIM 27-22-00-810. PERFORMED TEST OF RUDDER PER EMB 145 MM 27-23-00 NO DEFECTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO SERVICE

Part: INVERTER — FAILED (EMERGENCY LIGHT) · airframe 5,762 hrs · 5,085 cycles

EMERGENCY LIGHT INOPERATIVE AT EXIT ROW, FERRIED TO ORD. REMOVED AND REPLACED INVERTER IAW EMB AMM 33-50-11. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 5,667 hrs · 4,993 cycles

FOUND EXIT ROW OVERHEAD SIGN WILL NOT TEST. REPAIRED BROKEN WIRE IAW EMB AWM 20-21-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,946 hrs · 4,378 cycles

LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,946 hrs · 4,378 cycles

DENT FOUND BETWEEN FRAMES 27 AND 28 AND STRINGERS 17L AND 18L. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER. CLEANED AND TREATED SURFACE IAW EMB SRM 53-22-01. RETURNED AIRCRAFT TO SERVICE.

Part: ACM — SMOKE (NR 1)

CREW REPORTED BURNING SMELL IN COCKPIT JUST PRIOR TO PUSH BACK. REPLACED NR 1 AIR CYCLE MACHINE (ACM) IAW AMM. AC RETURNED TO SERVICE. (K)

Part: CARBON SEAL — LEAKING (RT ENGINE)

CREW REPORTED SMOKE AND FUMES IN CABIN. FOUND OIL LEAKING FROM NR 2 ENGINE CARBON SEAL. REPLACED NR 2 ENGINE IAW WC. OPS CHECK GOOD, AC RETURNED TO SERVICE. (SW21200504808) (K)

Part: SKIN — DAMAGED (HORIZ STAB)

LEFT HAND HORIZONTAL STABILIZER FORWARD SPAR HAS TWO OVERSIZED HOLES, UPPER SKIN PANEL. PERFORMED AN NDT INSPECTION, NO DEFECTS NOTED. INSTALLED FASTENERS WET, DONE IAW MFG SRM.

Part: FAIRING — CHAFED (RT NACELLE)

DURING INSPECTION OF AIRCRAFT, FOUND RIGHT INBOARD NACELLE FILLET FAIRING CHAFED. BLENDED OUT CHAFE. FABRICATED AND INSTALLED DOUBLER IAW SAAB 340 SRM 54-10-10 AND STANDARD SRM PRACTICES. (M)

Part: FRAME — DENTED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND TWO DENTS ON CARGO FRAME 677. REFORMED FRAME. PERFORMED A NDT INSPECTION OF THE FRAME AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE. INSTALLED NEW FRAME IAW SAAB 340 REPAIR STATEMENT 340SDS003569, PARA 9, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND PREVIOUSLY REPAIRED GALLEY FLOOR FRAME 258 CORRODED. FABRICATED AND REPLACED DOUBLER, FILLER, AND TWO TRIPLERS IAW SAAB 340 SRM 53-70-30 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN HMBV INSPECTION OF AIRCRAFT, FOUND GALLEY FLOOR FRAME 272 CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, A FILLER, AND A SHIM. WORK DONE IAW SAAB 340 SRM 53-70-30 AND STANDARD SRM PRACTICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING AN HMBV INSPECTION OF AIRCRAFT, FOUND CABIN SEAT TRACK 18.3L FORWARD NEAR KICK PLATE CORRODED BEYOND SRM LIMITS. REMOVED SECTION OF CORRODED SEAT TRACK. INSTALLED IAW SAAB 340 SRM AND STANDARD SRM PRACTICES. (M)

Part: SOCKET — INOPERATIVE (CABIN)

JFK - FLT 5023 - CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THE SOCKET FOR THE LIGHT OVER THE PASSENGER DOOR. OPERATIONAL HECK AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FUSE — INOPERATIVE (CABIN)

DFW - FLT 3765 - FOUND CREW REPORTED OVERHEAD EMERGENCY LIGHT AT 11A TO BE INOPERATIVE. MAINTENANCE REPLACED FUSE 76LN IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3613 - FOUND FLOOR PROXIMITY LIGHT AT SEAT POSITION 4B IS INOPERATIVE. PUT ON MEL AT THIS TIME. (M)

Part: SOCKET — DAMAGED (CABIN)

DFW - FLIGHT 3342 - EMERGENCY FLOOR LIGHTING INOPERATIVE AT 7BC AND 14 BC. REMOVED AND REPLACED SOCKET AT 7BC AND REPLACED LIGHT BULB AT 14BC IAW SAAB AMM 33-50-20. REF LOG PGE NR 1264790. (M)

Part: BULB — INOPERATIVE (CABIN)

DFW - FLT 3509 - FLOOR PROXIMTIY EMERGENCY LIGHT AT 9B IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB IAW SAAB MM 33-50-20. OPERATIONAL CHECK GOOD IAW SAAB MM 33-50-00. (M)

Part: LAMP — INOPERATIVE (CABIN) · airframe 14,142 hrs · 16,255 cycles

DFW - FLT 3838 - EMERGENCY FLOOR LIGHT BETWEEN ROWS 5 AND 6 IS OUT. C/A - REMOVED AND REPLACED FLOOR PROXIMITY LIGHT AT ROWS 5 AND 6 IAW SAAB AMM 33-50-10. OPS CHECKED GOOD. (X)

Part: LIGHT — FAILED (CABIN)

DFW - FLT 3577 - FLOOR PROX EMERGENCY LIGHT INOPERATIVE SEAT 4A. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DFW - FLT 3304 - FLOOR PROXIMITY LIGHT AT 9B DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M)

Part: SKIN — DENTED (BS 351-363)

ABI - TWO DENTS FOUND AFT OF RT ICE SHIELD BETWEEN STA'S 363 AND 351, STR LINE 1615 AND 1616. RECONTOURED BOTH DENTS. PERFORMED EDDY CURRENT INSP OF RECONTOURED AREA. NO DEFECTS NOTED. FABBED 2 REPAIR DOUBLERS .050 INCH THICK. DIMENSIONS OF 14 INCH BY 5.5 INCH AND SECOND 12 INCHES BY 4.5 INCHES. CONTOURED TO FIT FUSELAGE. APPLIED ALODINE AND EPOXY PRIMER TO DOUBLERS. FAY SEALED REPAIR DOUBLERS AND ATTACHED TO ACFT WITH FASTENERS. FILLET SEALED REPAIR EDGES AND APPLIED SURFACE TOPCOAT. WORK DONE IAW SAAB 340 SRM 53-70-10 PG 217 AND STD SRM PRINCIPALS. ACFT OK FOR SERVICE. (X)

Part: BULB — FAILED (ROW 10)

SBP - DURING PS-2 INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 10B/C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)