N951UW

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 25,926 hrs · 21,598 cycles

AIRCRAFT WAS GROUNDED, NR 2 ENGINE NO LIGHT OFF DURING START. GROUND PERSONAL REPORTED SPARKS FROM ENGINE. REPLACED THE STARTER IAW AMM 80-10-03.

Part: WINDOW — SCRATCHED (MAIN CABIN) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN WINDOW BETWEEN FR 82 AND FR 83, BETWEEN S9L AND S10L IS WORN / SCRATCHED. REPLACED WINDOW PER AMM 56-20-00.

Part: WINDOW — CRAZED (MAIN CABIN) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN WINDOW BETWEEN FR 20 AND FR 21, BETWEEN S9L AND S10L IS WORN / CRAZED. REPLACED WINDOW PER AMM 56-20-00.

Part: FITTING — WORN (RT OVERWING DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: LOWER AFT FITTING IS WORN IN THE RIGHT HAND OVERWING EXIT DOOR CUTOUT. REPLACED FITTING PER AMM 52-21-00 AND 21-31-00.

Part: STOP FITTING — WORN (FWD PAX DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER DOOR CUTOUT DOOR STOP PADS #1, #2 AND #6 ARE WORN. REPLACED DOOR STOP PADS PER AMM 53-10-21 AND 52-11-00.

Part: INDICATOR — DAMAGED (FWD PAX DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER DOOR PNEUMATIC INDICATOR HAS NO FLUID. REMOVED AND REPLACED FORWARD PASSENGER DOOR PNEUMATIC INDICATOR.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT WAS NOT GROUNDED: MAIN CABIN ALL PHOTOLUMINESCENT STRIPS WERE MORE THAN 10% DAMAGED. MAINTENANCE REPLACED PHOTOLUMINESCENT STRIPS PER AMM 33-50-21.

Part: FLOOR SUPPORT — CORRODED (FRAME 88) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT MAIN CABIN RIGHT HAND FLOOR SUPPORT AT FR 88 AND Y= +863.6. REPLACED FLOOR SUPPORT PER SRM 51-41-02.

Part: STOP FITTING — WORN (AFT SERVICE DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT SERVICE DOOR FRAME STOP #8 PAD WORN. REPLACED AFT SERVICE DOOR FRAME STOP #8 PAD PER AMM 53-23-25.

Part: STOP FITTING — WORN (AFT PAX DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER DOOR CUTOUT PRESSURE DOOR STOPS #6, #7 AND #8 WORN. REPLACED DOOR STOPS PER AMM 53-23-21.

Part: STOP FITTING — WORN (FWD SERVICE DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD SERVICE DOOR CUTOUT #1 STOP FITTING PAD IS WORN. REPLACED FORWARD SERVICE DOOR CUTOUT #1 STOP FITTING PAD PER AMM 53-10-25.

Part: DAMPENER — CORRODED (AFT SERVICE DOOR) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT SERVICE DOOR DAMPENER RUSTED, MARKED RJ-041. REPLACED DOOR DAMPENER PER E190 AMM 52-42-27 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SPLICE — CORRODED (FRAME90) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR CENTER SPLICE AT FR 90 AND BL 0. REPLACED SPLICE PER E190 DRAWING 170-86119-005.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN RIGHT HAND SHEAR PANEL BETWEEN FR 87 AND FR 88 AT RBL 914.4. REPLACED SHEAR PANEL PER AARD 53-00-00-3 REPAIR 3.

Part: FITTING — WORN (OVRWG DOOR FRAME) · airframe 25,920 hrs · 21,595 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND OVER WING EXIT DOOR CUT OUT LOWER FORWARD AND AFT FITTINGS WORN. REPLACED FITTINGS PER AMM 52-21-00-820-801-A,

Part: DAMPENER — CORRODED (FWD DOOR) · airframe 25,829 hrs · 21,538 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD DOOR DAMPENER HAD RUST. MAINTENANCE REPLACED DAMPENER PER AMM 52-41-27.

Part: BATTERY — FAULTED (ZONE 200) · airframe 25,829 hrs · 21,513 cycles

AIRCRAFT WAS GROUNDED: EMER BATT FAULT CYAN CAS MSG. REMOVED AND REPLACED MID AIRCRAFT EMERGENCY BATTERY IAW AMM 33-50-01. ***SUPPLEMENTAL ACTION: SECT. 3, TT/TC.***

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,829 hrs · 21,538 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS EMERGENCY LIGHTS ON AMBER CAS MSG IN FLIGHT. QRH COMPLIED WITH, MSG REAPPEARED ON APPROACH TO PHL. MAINTENANCE REMOVED AND REPLACED MID AIRCRAFT EMERGENCY BATTERIES IAW AMM 33-50-01. ALL EMERGENCY LIGHTS WORK GOOD. (SEE SDR # AALA201909109018, AALA201909109019)

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,829 hrs · 21,538 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS EMERGENCY LIGHTS ON AMBER CAS MSG IN FLIGHT. QRH COMPLIED WITH, MSG REAPPEARED ON APPROACH TO PHL. MAINTENANCE REMOVED AND REPLACED MID AIRCRAFT EMERGENCY BATTERIES IAW AMM 33-50-01. ALL EMERGENCY LIGHTS WORK GOOD. (SEE SDR # AALA201909099015, AALA201909109019)

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,829 hrs · 21,513 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS EMERGENCY LIGHTS ON AMBER CAS MSG IN FLIGHT. QRH COMPLIED WITH, MSG REAPPEARED ON APPROACH TO PHL. MAINTENANCE REMOVED AND REPLACED MID AIRCRAFT EMERGENCY BATTERIES IAW AMM 33-50-01. ALL EMERGENCY LIGHTS WORK GOOD. (SEE SDR # AALA201909099015, AALA201909109018)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 25,829 hrs · 21,513 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHL ON ACCOUNT OF BOTH AFT FLIGHT ATTENDANT OXYGEN MASKS DEPLOYED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED AFT FA O2 BOXES IAW AMM 35-20-05. OPS CK GOOD IAW AMM 35-20-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 25,782 hrs · 21,462 cycles

AIRCRAFT WAS GROUNDED: EMERGENY LIGHT BATTERY FAULT DURING TEST. TWO EMERGENCY LIGHTS AFT OF EXITROW ARE TURNING ON AND OFF DURING TEST. REMOVED AND REPLACED FWD LH EMER BATT PWR UNIT, IAW AMM 33-50-01/400.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 25,502 hrs · 21,199 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLATP TRACK # 1 WORN. REPLACED FLAP TRACK PER EA 294185B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 25,339 hrs · 21,051 cycles

AIRCRAFT NOT GROUNDED: PILOT DECLARED EMERGENCY INBOUND ON ACCOUNT OF POSSIBLE #3 TIRE OR BRAKE DAMAGE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF MAIN BRAKE SYSTEM, OK IAW AMM 32-41-00. NO HISTORY. NO ABNORMAL OR OUT OF RANGE VALUES NOTED.

Part: REGULATOR VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 24,002 hrs · 19,947 cycles

AIRCRAFT WAS GROUNDED. PHL-MHT DURING DESCENT INTO MHT FLIGHT DEVELOPED A PRESSURIZATION ISSUE. CREW DECLARED AN EMERGENCY FOR PRIORITY CLEARANCE AS A PRECAUTION. CABIN NOT PREPPED AND AFR TRUCKS DID NOT RESPOND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ENGINE NR 1 BLEED AIR PRESSURE WAS FLUCTUATING BETWEEN 0-60 PSI AT CLIMB POWER. THE FLIGHT DROPPED DOWN TO FL 150. THEN ENGINE NR 2 BLEED FAIL EICAS MESSAGE, WHICH WAS RESET PER QRH PROCEDURE. REPLACED HIGH PRESSURE REGULATING VALVE AND NACELLE PRESSURE REGULATING VALVE PER AMM 36-11-01/03. LEAK CHECKED PER TASK 36-11-01-790-801- / A/500. CHECK GOOD. THIS SDR IS FOR THE HIGH PRESSURE REGULATING VALVE ON ENGINE NR 1. (SEE CONTROL AALA201810179002 AND AALA201810179003)

Part: REGULATOR VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 24,002 hrs · 19,947 cycles

AIRCRAFT WAS GROUNDED. PHL-MHT. DURING DESCENT INTO MHT FLIGHT DEVELOPED A PRESSURIZATION ISSUE. CREW DECLARED AN EMERGENCY FOR PRIORITY CLEARANCE AS A PRECAUTION. CABIN NOT PREPPED AND AFR TRUCKS DID NOT RESPOND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ENGINE NR 1 BLEED AIR PRESSURE WAS FLUCTUATING BETWEEN 0-60 PSI AT CLIMB POWER. THE FLIGHT DROPPED DOWN TO FL 150. THEN ENGINE NR 2 BLEED FAIL EICAS MESSAGE, WHICH WAS RESET PER QRH PROCEDURE. REPLACED HIGH PRESSURE REGULATING VALVE AND NACELLE PRESSURE REGULATING VALVE PER AMM 36-11-01/03. LEAK CHECKED PER TASK 36-11-01-790-801- / A/500. CHECK GOOD. THIS SDR IS FOR THE NACELLE PRESSURE REGULATING VALVE ON ENGINE NR 1. (SEE CONTROL AALA201810179001 AND AALA201810179003)

Part: REGULATOR VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 24,002 hrs · 19,947 cycles

AIRCRAFT WAS GROUNDED. PHL-MHT. DURING DESCENT INTO MHT FLIGHT DEVELOPED A PRESSURIZATION ISSUE. CREW DECLARED AN EMERGENCY FOR PRIORITY CLEARANCE AS A PRECAUTION. CABIN NOT PREPPED AND AFR TRUCKS DID NOT RESPOND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ENGINE NR 1 BLEED AIR PRESSURE WAS FLUCTUATING BETWEEN 0-60 PSI AT CLIMB POWER. THE FLIGHT DROPPED DOWN TO FL 150. THEN ENGINE NR 2 BLEED FAIL EICAS MESSAGE, WHICH WAS RESET PER QRH PROCEDURE. REPLACED HIGH PRESSURE REGULATING VALVE AND NACELLE PRESSURE REGULATING VALVE PER AMM 36-11-01/03. LEAK CHECKED PER TASK 36-11-01-790-801- / A/500. CHECK GOOD. THIS SDR IS FOR THE NACELLE PRESSURE REGULATING VALVE ON ENGINE NR 2. (SEE CONTROL AALA201810179001 AND AALA201810179002)

Part: SENSOR — DEFECTIVE (RT WING) · airframe 23,993 hrs · 19,941 cycles

WITH THE NR 1 ENGINE BLEED ON MEL, THE NR 2 ENGINE BLEED FAILED IN FLIGHT, AT FL210 IN MODERATE FREEZING RAIN CONDITIONS. THE AIRCRAFT LOST WING ANTI-ICE AND PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO FL 100, THEN TO FL 040 TO AVOID FREEZING PRECIPITATION. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AND 2 BLEED PRESSURE SWITCHES IAW AMM 36-14-02, AND THE SPDA POWER MODULES IAW AMM 42-61-11. ACCOMPLISHED ENGINE RUNS AND ALL CHECKED GOOD.

Part: MODULE — DEFECTIVE (BLEED SYS) · airframe 23,993 hrs · 19,941 cycles

WITH THE NR 1 ENGINE BLEED ON MEL, THE NR 2 ENGINE BLEED FAILED IN FLIGHT, AT FL210 IN MODERATE FREEZING RAIN CONDITIONS. THE AIRCRAFT LOST WING ANTI-ICE AND PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO FL 100, THEN TO FL 040 TO AVOID FREEZING PRECIPITATION. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AND 2 BLEED PRESSURE SWITCHES IAW AMM 36-14-02, AND THE SPDA POWER MODULES IAW AMM 42-61-11. ACCOMPLISHED ENGINE RUNS AND ALL CHECKED GOOD.

Part: MODULE — DEFECTIVE (BLEED SYS) · airframe 23,993 hrs · 19,941 cycles

WITH THE NR 1 ENGINE BLEED ON MEL, THE NR 2 ENGINE BLEED FAILED IN FLIGHT, AT FL210 IN MODERATE FREEZING RAIN CONDITIONS. THE AIRCRAFT LOST WING ANTI-ICE AND PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO FL 100, THEN TO FL 040 TO AVOID FREEZING PRECIPITATION. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AND 2 BLEED PRESSURE SWITCHES IAW AMM 36-14-02, AND THE SPDA POWER MODULES IAW AMM 42-61-11. ACCOMPLISHED ENGINE RUNS AND ALL CHECKED GOOD.

Part: SENSOR — FAILED (NR 2 BLEED SYS) · airframe 23,993 hrs · 19,941 cycles

WITH THE NR 1 ENGINE BLEED ON MEL, THE NR 2 ENGINE BLEED FAILED IN FLIGHT, AT FL210 IN MODERATE FREEZING RAIN CONDITIONS. THE AIRCRAFT LOST WING ANTI-ICE AND PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO FL 100, THEN TO FL 040 TO AVOID FREEZING PRECIPITATION. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AND 2 BLEED PRESSURE SWITCHES IAW AMM 36-14-02, AND THE SPDA POWER MODULES IAW AMM 42-61-11. ACCOMPLISHED ENGINE RUNS AND ALL CHECKED GOOD.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 22,573 hrs · 18,809 cycles

FORWARD L1 DOOR EXIT SIGN DAMAGED. REPLACED THE SIGN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,052 hrs · 18,421 cycles

FORWARD FACING EXIT SIGN OVER CENTER AISLE AT ROW 12 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ON. REPLACED EMERGENCY BATTERY PACK NR 3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,052 hrs · 18,421 cycles

AIRCRAFT WAS GROUNDED. FORWARD FACING EXIT SIGN OVER CENTER AISLE AT ROW 12 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ON. REPLACED EMERGENCY BATTERY PACK NR 4.

Part: REGULATOR VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 21,265 hrs · 17,823 cycles

BLEED FAULTS. DIVERTED THE FLIGHT. REPLACED E2 PRESSURE REGULATOR VALVE. AIRCRAFT WAS GROUNDED.

Part: VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 21,264 hrs · 17,822 cycles

DIVERTED AND DECLARED AN EMERGENCY DUE TO BLEED FAULTS. AIRCRAFT WAS GROUNDED. REPLACED THE NR 2 ENGINE FAN AIR VALVE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 20,793 hrs · 17,467 cycles

AIRCRAFT WAS GROUNDED. RIGHT HAND EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE AT GATE WHEN EMERGENCY LIGHT TEST IS ACCOMPLISHED ON FED FLIGHT ATTENDANT PANEL. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-50-01.

Part: RIB — CRACKED (RT WING) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED RIGHT HAND WING FRONT SPAR (LEADING EDGE) RIB 17. REPLACED RIGHT WING LEADING EDGE RIB 17 PER DRAWING 190-31005-409, 190-31267-021 AND SRM'S 51-43-03 AND 51-43-04.

Part: RIB — CRACKED (LT WING) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED LEFT HAND WING FRONT SPAR RIB 17. REPLACED RIB 17 FROM WING LEADING EDGE PER DRAWING 190-31005-409, 190-31267-021 AND 190-31249-409, SRM 51-42-02, 51-41-01, 51-43-03, 51-43-04 AND 51-41-02.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO DOOR CUT-OUT CENTER SEAL REST, NUTPLATE SPACERS, AT STRINGER 22R. REPLACED SEAL REST PER AARD 53-00-00-3 REPAIR 3 FIG 2.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT WING (SPAR 2) LOWER SKIN PANEL FASTENER, JUST OUTBOARD OF DRAIN HOLE AND RIB 10. REPAIRED SKIN PANEL PER EA 506702B.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CAPTAINS DIRECT VISION WINDOW EXTERNAL SURFACE SCUFFED AND HAS A 2 INCH BY 4 INCH AREA OF DELAMINATION AT AFT UPPER CORNER. REPLACED CAPTAINS DIRECT VISION WINDOW PER JOB CARD 43C22156003.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFING ON AFT PASSENGER DOOR CONTROL ROD AT HOISTING ARM FITTING. PERFORMED ADJUSTMENT OF AFT PASSENGER DOOR CONTROL MECHANISM PER AMM 52-12-52-820-801-A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BEARING — SEIZED (SERVICE DOOR) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT WAS GROUNDED. FORWARD AND AFT BEARINGS UNDER FORWARD SERVICE DOOR EXTERIOR HANDLE ARE SEIZED. CLEANED FORWARD SERVICE DOOR AND FORWARD AND AFT BEARINGS UNDER EXTERNAL DOOR HANDLE.

Part: LENS — CRACKED (CABIN) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT WAS GROUNDED. MAIN CABIN AFT LOWER CEILING PANEL EMERGENCY EXIT LIGHT LENS COVER CRACKED AT 253GLC. REPLACED MAIN CABIN AFT LOWER CEILING PNL EMERGENCY EXIT LIGHT LENS COVER.

Part: LENS — CRACKED (CABIN) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT WAS GROUNDED. MAIN CABIN AFT LOWER CEILING PANEL EMERGENCY EXIT LIGHT LENS COVER CRACKED AT 254CRC AND 253GLC. REPLACED MAIN CABIN AFT LOWER CEILING PANEL EMERGENCY EXIT LIGHT LENS COVER.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 19 AND -Y1092. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-413, AND SRM 51-43-03.

Part: SEAT TRACK — CORRODED (FRAMES 83-85) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON THE AFT MAIN CABIN SEAT TRACK AT -Y266 BETWEEN FRAMES 83 AND 85. REPLACED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT MAIN CABIN CROSSBEAM UPPER FLANGE SURFACE AT Y196 AND FR 84. REPAIRED CROSSBEAM PER SRM 53-23-10.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN SHEAR PLATE AT -Y330 AND FR 16. REPLACED SHEAR PLATE PER AARD 53-00-00-3 REPAIR 3, SRM 51-10-03 AND 51-12-01.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND INBOARD FLAP INBOARD SUPPORT FITTING. REPLACED FITTING PER SRM 51-43-03.

Part: ROLLER — SEIZED (LT OVERWING EXIT) · airframe 20,766 hrs · 17,454 cycles

LEFT OVERWING EXIT, AFT TOP BEARING IS SIEZED TO PIN ON FRAME. REPLACED THE ROLLER IAW AMM 20-10-08/400.

Part: CHANNEL — CORRODED (FRAME 27) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON FORWARD CARGO DOOR CUTOUT, LOWER SILL HAT CHANNEL AT FRAME 27. REPLACED THE HAT CHANNEL IAW SRM 51-41-01, 51-23-05, AND 51-23-06.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION WAS FOUND ON AFT MAIN CABIN SPLICE AT FRAME 90 AND -Y100. REPLACED THE SPLICE IAW DRAWING 170-660-445, AND SRM 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN SEAT TRACK AT Y304 BETWEEN FR 13 AND FR 14. REPLACED SEAT TRACK PER AARD 53-00-00-3 REP 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y304 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-03, 51-75-16, AND DRAWING 170-00822-503.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT -Y863 BETWEEN FR 89 AND FR 90. REPLACED PANEL SUPPORT PER DWG 170-6600-457.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1168 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-04, 51-402, AND 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y330 BETWEEN FR 12 AND FR 13. REPLACED FLOOR SUPPORT PER AARD 53-10-00-2 REP 2, SRM 51-43-03, 51-43-04 AND 51-41-01.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FORWARD LAVATORY DRAIN-DUCT BRACKET AT -Y1105 AND FR 13. REPAIRED BRACKET PER DRAWING 170-03967-803.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FORWARD MAIN CABIN LONGITUDINAL FLOOR SUPPORT AT Y330.2 BETWEEN FR 17 AND FR 18. REPLACED FLOOR SUPPORT PER DRAWING 170-00822-503, SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON VERTICAL STABILIZER REAR SPAR (ZV4269) BETWEEN RIBS 9-10. REPLACED RIB PER DRAWING 190-63400-419.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN SHEAR PLATE AT Y965 BETWEEN FR 13 AND FR 14. REPLACED SHEAR PLATE PER SRM 51-42-02 AND AARD 53-00-00-3 REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN SEAT TRACK AT Y266 BETWEEN FR 83 AND FR 85. REPAIRED SEAT TRACK PER SRM 53-23-10 REPAIR 54 AND SRM 53-23-10 AD54.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT Y863 AND FR 89. REPLACED FLOOR SUPPORT PER AARD 53-00-00, SWPM 20-67-00, SRM 51-10-03, 51-12-01, 51-75-16, 51-41-01, 51-41-02, 51-23-04, 51-23-05 AND 51-23-06.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION / SCRATCHES ON AFT MAIN CABIN RIGHT HAND SHEAR PANEL BETWEEN Y355 AND Y939, BETWEEN FR 87 AND FR 88. REPLACED SHEAR PANEL PER AARD 53-00-00, SRM 51-42-03 AND 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,766 hrs · 17,454 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT, -Y965 BETWEEN FRAMES 87 & 88. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-42-02, AND DRAWING 170-66000-445.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 19,826 hrs · 16,799 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS SLIDING WINDOW HAS BUBBLES IN DIRECT LINE OF SIGHT. REMOVED AND REPLACED FIRST OFFICERS SLIDING WINDOW PER AMM 56-12-00.

Part: CONTROLLER — DEFECTIVE (WINDOW HEAT) · airframe 18,286 hrs · 15,311 cycles

AIRCRAFT WAS GNDED. FIRST OFFICERS DIRECT VIEW WINDSHIELD, LT CORNER DELAMINATED WITH INDICATION OF ARCING ALONG BUS BAR & HEATING ELEMENTS. REPLACED IAW AMM 56-11-00-000-801-A, 400-801-A & THE WINDOW HEAT CONTROLLER NR 2 IAW AMM 30-42-01-000-801-A & 400-801. ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK. SEE AALA201601079002 FOR ADDITIONAL PART INFORMATION.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 18,286 hrs · 15,311 cycles

AIRCRAFT WAS GNDED. FIRST OFFICER DIRECT VIEW WINDSHIELD, LT CORNER DELAMINATED WITH INDICATION OF ARCING ALONG BUS BAR & HEATING ELEMENTS. REPLACED FIRST OFFICER WINDSHIELD IAW AMM 56-11-00-000-801-A, 400-801-A & THE WINDOW HEAT CONTROLLER NR 2 IAW AMM 30-42-01-000-801-A, 400-801. ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK. SEE AALA201601079009 FOR ADDITIONAL PART INFORMATION.

Part: EXCITER — DEFECTIVE (APU) · airframe 18,267 hrs · 15,291 cycles

AIRCRAFT WAS GNDED. AT GATE WITH APU ON, FUMES & FUEL ODOR SMELT THROUGHOUT COCKPIT & CABIN. TROUBLE SHOT IAW FIM 4910421, FOUND APU EXCITER FAULT. REPLACED APU EXCITER. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 49-41-01.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 17,424 hrs · 14,488 cycles

FLIGHT CREW REPORTED HEARING A POSSIBLE AIR LEAK FROM THE CTR WINDSHIELD AREA. FOUND A LOCK FASTENER RIVET MISSING FROM THE CAPTAINS WINDSHIELD, 5TH ONE UP FROM THE INBD LOWER CORNER. REPLACED THE WINDSHIELD IAW AMM 56-11-00-000-8941A400.

Part: MODULE — FAULTY (CABIN) · airframe 17,043 hrs · 14,115 cycles

FLIGHT 1827, EN-ROUTE EMER LIGHTS CAME ON DURING TAXI. EMER LIGHT BATTERY FAULT. THE FLIGHT RETURNED TO GATE. REPLACED THE PAX SIGNS PANEL, NO HELP. REPLACED THE GENERIC I/O MODULE MAU 2 SLOT 9 & 10. OK FOR SERVICE.

Part: LENS — BROKEN (EXIT SIGN) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, R1 DOOR LOWER EMER EXIT SIGN LENS IS BROKEN. REPLACED R1 DOOR LOWER EMER EXIT SIGN IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LENS — BROKEN (EXIT SIGN) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, RT OVERWING LOWER EMER EXIT SIGN LENS IS BROKEN. REPLACED RT OVERWING LOWER EMER EXIT SIGN LENS IAW AMM 33-50-15-000-801-A & 33-50-15-400-801-A. OPERATIONAL TEST GOOD IAW AMM 33-50-00-710-801-A.

Part: LENS — BROKEN (EXIT SIGN) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, L2 DOOR LOWER EMER EXIT SIGN LENS IS BROKEN. REPLACED L2 DOOR LOWER EMER EXIT SIGN IAW AMM 33-50-15-000-801-A & 33-50-15-400-801-A. OPERATIONAL TEST GOOD IAW AMM 33-50-00-710-801-A.

Part: LENS — BROKEN (EXIT SIGN) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, FWD LAVATORY EMER EXIT SIGN LENS IS BROKEN. REPLACED FWD LAVATORY EMER EXIT SIGN IAW AMM 33-50-15-000-801-A & 33-50-15-400-801-A. OPERATIONAL TEST GOOD IAW AMM 33-50-00-710-801-A.

Part: LENS — SATURATED (EXTERIOR LIGHT) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, LOWER EXTERNAL EMER LIGHT LENS AT BOTTOM LT SIDE OF THE AFT FUSELAGE WING TO BODY FAIRING HAS WATER INTRUSION. REMOVED, INSPECTED & REINSTALLED THE LOWER EXTERNAL EMER LIGHT LENS WITH NEW SEALANT ON LT WING TO BODY FAIRING IAW AMM 33-50-25-000-802-A & AMM 33-50-25-400-802A STEPS 1F 1 J & K.

Part: LIGHT — CRACKED (EXTERIOR) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, LOWER EMER LIGHT IS CRACKED, 093-03, AT THE LT WING TO BODY FAIRING 199ML. REPLACED LOWER EMER LIGHT AT LT WING TO BODY FAIRING 199ML. GOOD OPERATIONAL CHECKS IAW AMM 33-50-25-000-802-A, AMM 33-50-25-400-802A & AMM 33-50-25-710-801A.

Part: LENS — BROKEN (EXIT SIGN) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, R1 DOOR UPPER EMER EXIT SIGN LENS IS BROKEN. REPLACED R1 DOOR UPPER EMER EXIT SIGN LENS IAW AMM 33-50-15.

Part: GLOWSTRIP — DAMAGED (CABIN)

C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS HAS MORE THAN 10% DAMAGE. REPLACED IAW AMM 33-50-21.

Part: FITTING — BROKEN (ZONE 800) · airframe 16,397 hrs · 13,550 cycles

C3 CHECK, L2 DOOR FWD GIRT BAR FITTING, THE FLAP SPRING IS BROKEN. R & R L2 DOOR FWD GIRT BAR FITTING ASSEMBLY IAW AMM 53-23-21-400-804-A.

Part: ROLLER — FROZEN (EMERGENCY EXIT)

RIGHT OVERWING ESCAPE HATCH CUT OUT AFT UPPER ROLLER IS FROZEN, IS NOT MOVING 093-12. REPLACED AFT UPPER ROLLER AT RT OVERWING HATCH CUT OUT IAW AMM 20-10-08.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 16,396 hrs · 13,550 cycles

C3 CHECK, UPON REMOVAL OF AFT ENTRY FLOOR PANELS, LIGHT CORROSION FOUND ON FLOOR GUSSET PLATE AT FRAME 89, Y+579.88. R & R GUSSET PLATE AT MAIN CABIN FLOOR STRUCTURE IAW SRM 51-41-02 PAGE 1 TO 7. DIMENSIONS OF CORROSION ARE L=2 INCHES, W=4 INCHES & D=.008 INCHES.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,396 hrs · 13,550 cycles

C3 CHECK, UPON REMOVAL OF AFT ENTRY FLOOR PANELS, CORROSION WAS DISCOVERED ON CTR SHEAR PANEL, BETWEEN FRAME 86 & 87, Y +275 TO Y -275. THE CORROSION MEASURED L=1.2 INCHES, W=.900 INCHES & D=.012 INCHES. R & R CTR SHEAR PANEL AT MAIN CABIN IAW SRM PART II 51-42-01 PAGE 1 TO 6.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 16,396 hrs · 13,550 cycles

C3 CHECK, LT WING LOWER SKIN PANEL FASTENER HOLE CRACKED JUST OTBD OF DRAIN HOLE & RIB 10. REPAIRED LT WING LOWER SKIN PANEL IAW EA 506702.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,188 hrs · 12,482 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 15,188 hrs · 12,482 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 15,188 hrs · 12,482 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,188 hrs · 12,482 cycles

THE RT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT LOOSE & THE BUSHING MIGRATED. RE-TORQUED THE LOCKNUT & APPLIED THE APPROPRIATE SAFETIES.

Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 13,677 hrs · 11,333 cycles

SLAT FAIL MESSAGE ON EICAS AFTER EXTENDING SLAT/FLAP HANDLE TO "1". MAINTENANCE REPLACED LT OTBD SLAT 3-4 SKEW SENSOR AND HARNESS.

Part: SLIDE — FAULTY (CABIN) · airframe 12,024 hrs · 10,074 cycles

FUNCTIONAL EVACUATION SLIDE TEST NEEDS ACCOMPLISHED PER JC 43T20025001. MAINTENANCE ACCOMPLISHED TEST PER JC 43T20025001 AND SLIDE DEPLOYMENT FAILED. THE DOOR STALLED BEFORE OPENING ALL THE WAY. MAINTENANCE REPLACED THE SLIDE.

Part: GUIDE — DIRTY (L1 DOOR) · airframe 11,246 hrs · 9,453 cycles

THE 1L DOOR VENT FLAP HANDLE NOT CLOSING PROPERLY. MAINTENANCE CHECKED PAX ENTRY DOOR 1L CONDITION, NO DEFECTS FOUND. CLEANED AND LUBED DOOR GUIDES, CAM FOLLOWERS AND DOOR BOX ASSEMBLY. CHECKED OPERATION AND LIGHT INDICATION, SYSTEM NORMAL.

Part: SPRING — DEFECTIVE (L1 DOOR) · airframe 11,196 hrs · 9,398 cycles

1L DOOR ARMING LEVER STICKS AND GRINDS WHEN LOWERING TO ARMING POSITION. MAINTENANCE REPLACED ASSIST SPRING FROM FWD PAX DOOR VENT FLAP VISUAL LOCK INDICATOR. OPERATIONAL CHECK IS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 11,116 hrs · 9,339 cycles

A F/A JUMP SEAT EMERGENCY ENTRY LIGHT BROKE. MAINTENANCE SECURED EMERGENCY LIGHT ASSEMBLY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN SEAT TRACK CORRODED BETWEEN FR 13 AND FR 19 AT Y -273, Z -490. REMOVED AND REPLACED SEAT TRACK IAW EMBRAER DRAWING 170-00822-413 AND TR 190-5300-11-0563A.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE GUSSET CORRODED AT FR 16, Y -1170, Z -490. REMOVED AND RELACED GUSSET IAW TR-190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM UPPER SHEET CORRODED BETWEEN FR 85 AND FR 86, Y 273, Z-490. REMOVED AND REPLACED UPPER SHEET IAW TR 190-5300-11-0563.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM SPLICE PLATE CORRODED AT FR 87, Y 273, Z -490. REMOVED AND REPLACED SPLICE PLATE IAW E190 SRM 51-23-06, 51-43-01 & 51-40-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE GUSSET CORRODED AT FR 90, Y 625, Z -490. REMOVED AND RELACED GUSSET IAW EMBRAER DRAWING 170-60001-825.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - SILL PLATE CORRODED BETWEEN FR 12 AND FR 14 AT Y 1380, Z -490. REMOVED AND REPLACED SILL PLATE IAW E190 SRM 51-40-00 AND TR 190-5300-11-0563A.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR INTERCOSTAL GUSSET PLATE CORRODED AT FR90, Y 273, Z -490. REMOVED AND REPLACED GUSSET PLATE IAW EMBRAER DRAWING 170-60001-825.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM UPPER SHEET CORRODED BETWEEN FR 85 AND FR 86, Y-273, Z-490. REMOVED AND REPLACED UPPER SHEET IAW TR 190-5300-11-0563.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOOR SUPPORT PLATE CORRODED AT FR 84, Y 273, Z -490. REMOVED AND REPLACED SUPPORT PLATE IAW E190 SRM PART 2 51-40-02, 51-23-04, 51-41-02 & 51-42-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR DOUBLER CORRODED AT FR 16, Z -490 BETWEEN Y -276 & Y -913. REMOVED AND REPLACED FLOOR DOUBLER IAW TR 190-5300-11-0562A.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE SPLICE PLATE CORRODED AT FR 90, Y -243, Z -490. REMOVED AND REPLACED SPLICE PLATE IAW EMBRAER DRAWING 170-60001-825, SHEET 8 AND E190 SRM 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR DOUBLER CORRODED AT FR 19, Z -490 BETWEEN Y -863 AND Y -276. REMOVED AND REPLACED FLOOR DOUBLER IAW TR 190-5300-11-0563.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM SHEAR PANEL CORRODED BETWEEN FR 87 AND FR 88, BETWEEN Y 273 AND Y 1175. REMOVED AND REPLACED SHEAR PANEL IAW TR 190-5300-11-0563, EMBRAER DRAWING 170-66000-439 AND E190 SRM 51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM CORRODED AT FR 86 + 6 IN, Y -273 & Z -490. REMOVED AND REPLACED BEAM IAW TR 190-5300-11-0563, E190 SRM 51-40-02 AND EMBRAER DRAWING 170-85509-841.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOORBEAM SHEAR PANEL CORRODED BETWEEN FR 87 AND FR 88 FROM Y -273 AND Y -1175. REMOVED AND REPLACED SHEAR PANEL IAW TR 190-5300-11-0563 AND EMBRAER ERJ 190-100 IGW SRM 53-23-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE FLOOR SUPPORT PLATE CORRODED AT FR 28, Y 1310, Z -490. REMOVED AND REPLACED PLATE IAW EMBRAER DRAWING 170-66000-439A AND E190 SRM SRM 51-41-01/02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOORBEAM CORRODED BETWEEN FR 14 AND FR 17 AT Y 273, Z -490. REMOVED AND REPLACED FLOORBEAM IAW EMBRAER DRAWINGS 170-14790-803 & 170-0822-413 AND TR 190-5300-11-0563.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - FLOOR STRUCTURE SPLICE PLATE CORRODED AT FR 89, Y -273 & Z-490. REMOVED AND REPLACED SPLICE PLATE IAW TR 190-5300-11-0563 AND E190 SRM 51-40-06.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE SHEAR PANEL CORRODED AT FR 87, BETWEEN Y -273 AND Y 273, Z -490. REMOVED AND REPLACED SHEAR PANEL IAW TR190-5300-11-0563.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,688 hrs · 8,948 cycles

C2 CHECK - CABIN FLOOR STRUCTURE GUSSET CORRODED BETWEEN FR 12 AND FR 16 AT Y -1170, Z -490. REMOVED AND RELACED GUSSET IAW TR-190-5300-11-0563.

Part: ACM — CONTAMINATED (AC BAY) · airframe 10,141 hrs · 8,456 cycles

FLIGHT 1634 - THE FLIGHT ATTENDANT REPORTED A SMOKE SMELL IN THE CABIN DURING APPROACH AND PACK 2 FAIL DURING TAXI IN. MAINTENANCE REPLACED THE NR 2 AIR CYCLE MACHINE. ALSO REPLACED THE NR 2 DUAL HEAT EXCHANGER AND NR 2 DUAL HEAT EXCHANGER INLET DUCT DUE TO CONTAMINATION. OPERATIONAL CHECK IS GOOD, NO LEAKS NOTED AND NO ODORS DURING OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,532 hrs · 7,977 cycles

BOS - AFT LEFT ENTRY EMERGENCY LIGHT INOP. ACCOMPLISHED REPLACEMENT OF LIGHT ASSEMBLY.

Part: SENSOR — MALFUNCTIONED (LT WING) · airframe 8,401 hrs · 7,076 cycles

FLIGHT 751, PHL-BOS - UPON SELECTING "FLAPS 1" EICAS HAD NUMEROUS FAULTS/WARNINGS: SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, AOA LIMIT FAULT, AND STALL PROTECTION FAULT. THE CREW WAS UNABLE TO CLEAR THE FAULTS, DECLARED AND EMERGENCY, AND LANDED WITHOUT INCIDENT. ON TAXI IN, ALSO RECEIVED FLIGHT CONTROL NO DISPATCH. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SKEW SENSORS IAW EO2711P167 AND EA 200310. OPERATIONAL CHECKS SATISFACTORY FOR SERVICE IAW TASK 27-83-01-710-801.

Part: SENSOR — MALFUNCTIONED (LT WING) · airframe 8,401 hrs · 7,076 cycles

FLIGHT 751, PHL-BOS - UPON SELECTING "FLAPS 1" EICAS HAD NUMEROUS FAULTS/WARNINGS: SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, AOA LIMIT FAULT, AND STALL PROTECTION FAULT. THE CREW WAS UNABLE TO CLEAR THE FAULTS, DECLARED AND EMERGENCY, AND LANDED WITHOUT INCIDENT. ON TAXI IN, ALSO RECEIVED FLIGHT CONTROL NO DISPATCH. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SKEW SENSORS IAW EO2711P167 AND EA 200310. OPERATIONAL CHECKS SATISFACTORY FOR SERVICE IAW TASK 27-83-01-710-801.

Part: SENSOR — MALFUNCTIONED (RT WING) · airframe 8,401 hrs · 7,076 cycles

FLIGHT 751, PHL-BOS - UPON SELECTING "FLAPS 1" EICAS HAD NUMEROUS FAULTS/WARNINGS: SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, AOA LIMIT FAULT, AND STALL PROTECTION FAULT. THE CREW WAS UNABLE TO CLEAR THE FAULTS, DECLARED AND EMERGENCY, AND LANDED WITHOUT INCIDENT. ON TAXI IN ALSO RECEIVED FLIGHT CONTROL NR DISPATCH. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SKEW SENSORS IAW EO2711P167 AND EA 200310. OPERATIONAL CHECKS SATISFACTORY FOR SERVICE IAW TASK 27-83-01-710-801.

Part: SENSOR — MALFUNCTIONED (RT WING) · airframe 8,401 hrs · 7,076 cycles

FLIGHT 751, PHL-BOS - UPON SELECTING "FLAPS 1" EICAS HAD NUMEROUS FAULTS/WARNINGS: SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, AOA LIMIT FAULT, AND STALL PROTECTION FAULT. THE CREW WAS UNABLE TO CLEAR THE FAULTS, DECLARED AND EMERGENCY, AND LANDED WITHOUT INCIDENT. ON TAXI IN, ALSO RECEIVED FLIGHT CONTROL NO DISPATCH. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SKEW SENSORS IAW EO2711P167 AND EA 200310. OPERATIONAL CHECKS SATISFACTORY FOR SERVICE IAW TASK 27-83-01-710-801.

Part: TOILET — ODIFEROUS (LAVATORY)

PHL - EXCESSIVE URINE ODOR IN COCKPIT. MAINTENANCE REPLACED THE FORWARD LAV TOILET. PERFORMED A SATISFACTORY OPERATIONAL CHECK AND CLEANED WASTE MATERIAL AS REQUIRED.

Part: GEARBOX — MALFUNCTIONED (TE FLAP)

FLIGHT 2028, DCA-BOS - AT 20,000FT THE CREW RECEIVED A SLAT/FLAP FAIL MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY WITH THE TOWER. AFTER PERFORMING QRH PROCEDURES THE LIGHT WAS EXTINGUISHED. THE CAPTAIN CANCELLED THE EMERGENCY AND THE FLIGHT LANDED NORMALLY.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

BOS - THE L2 DOOR ASSIST BOTTLE IS BELOW WEEKLY CHECK MINIMUM PRESSURE. MAINTENANCE SERVICED THE L2 DOOR ASSIST BOTTLE TO CORRECT PRESSURE PER MM 52-12-51-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

PHL - THE AFT FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLASHLIGHT, BATTERY AND SEAL. OPERATIONAL CHECK IS GOOD.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 860, MHT - PHL - PACK 2 FAILED ON APPROACH TO PHL. RESET IAW QRH, THE FLIGHT ATTENDANT REPORTED BURNING SMELL IN CABIN. MAINTENANCE TROUBLESHOT PER FIM 21-51-00-810-823A. RAN PACK SYSTEM FOR 45 MINUTES WITH NO DUCT DAMAGE FOUND AND NO UNUSUAL ODOR THROUGHOUT THE CABIN OR COCKPIT DETECTED. OPERATIONAL CHECK IS GOOD.

Part: BOTTLE — LOW (L2 DOOR)

BOS - THE L2 PASSENGER DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE PER AMM 52-12-51-03.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

BOS - THE L2 DOOR ASSIST BOTTLE REQUIRED SERVICING. MAINTENANCE SERVICED THE L2 DOOR ASSIST BOTTLE PER AMM 52-12-51.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

ATL - THE AFT LEFT SERVICE DOOR PNEUMATIC ASSIST BOTTLE CHARGE LOW. MAINTENANCE SERVICED THE AFT LEFT SERVICE DOOR PNEUMATIC ASSEMBLY AS PER AMM 52-120-51-03.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

ATL - THE FORWARD ENTRY L1 DOOR PNEUMATIC ASSIST BOTTLE CHARGE LOW. MAINTENANCE SERVICED THE FORWARD ENTRY L1 DOOR PNEUMATIC ASSEMBLY AS PER AMM 52-120-51-03.

Part: DIAPHRAGM — DAMAGED (L1 DOOR)

BOS - L1 ENTRY DOOR ASSIST BOTTLE DEPLETED. MAINTENANCE REPLACED THE L1 DOOR ASSIST BOTTLE DIAPHRAGM PER MM 52-11-53, SERVICED BOTTLE, AND LEAK CHECKED.

Part: ACTUATOR — LEAKING (NR 3)

FLIGHT 906, MSY-PHL - WHILE ON APPROACH TO PHL AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF SYSTEM 1 HYDRAULIC QUANTITY AND PRESSURE. MAINTENANCE REPLACED THE NR 3 MFS ACTUATOR DUE TO LEAKING. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND PRESSURE RETURN CASE DRAIN FILTERS WERE ALSO REPLACED.

Part: SUPPORT BRACKET — CRACKED (AILERON CONTROL) · airframe 3,516 hrs · 2,804 cycles

PIT - MAJOR REPAIR / ALTERATION, RIGHT AILERON CONTROL SUPPORT BRACKET CRACKED. REPAIRED RIGHT AILERON CONTROL SUPPORT BRACKET AND ACCOMPLISHED MODIFICATION OF THE AILERON SUPPORT FITTING IAW US AIRWAYS EA 112416 AND PROTO TYPE EO 5308P198 PART B.

Part: GEARBOX — INOPERATIVE (TE FLAPS)

FLIGHT 1649, RDU-PHL - THE FLAPS FAILED TO EXTEND PAST 2. THE CREW DECLARED AN EMERGENCY AND DID A GO AROUND. THE FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE FLAP POWER DRIVE GEARBOX.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

PIT FLT 1557 EN ROUTE PIT TO CLT. AT FL 290, RECEIVED EICAS MESSAGE "FWD CABIN DOOR OPEN" PRESSURIZATION WAS NORMAL. HOWEVER, ONLY PARTIAL GREEN DOOR LOCK INDICATION. FOLLOWED QRH PROCEDURES AND RETURNED TO FIELD PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. AIRCRAFT CURRENTLY ON MEL. (A)