N958UW

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 24,338 hrs · 20,180 cycles

AIRCRAFT WAS NOT GROUNDED: R1, L1, AND R2 DOOR ASSIST BOTTLES LOW PRESSURE. MAINTENANCE SERVICED R1, L1 (SEE AALA201905229024), AND R2 (SEE AALA201905229025) DOOR ASSIST BOTTLES PER AMM 52-12-51.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 24,338 hrs · 20,180 cycles

AIRCRAFT WAS NOT GROUNDED: R1, L1, AND R2 DOOR ASSIST BOTTLES LOW PRESSURE. MAINTENANCE SERVICED R1 (SEE AALA201905229007), L1, AND R2 (SEE AALA201905229025) DOOR ASSIST BOTTLES PER AMM 52-12-51.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 24,338 hrs · 20,180 cycles

AIRCRAFT WAS NOT GROUNDED: R1, L1, AND R2 DOOR ASSIST BOTTLES LOW PRESSURE. MAINTENANCE SERVICED R1 (SEE AALA201905229007), L1 (SEE AALA201905229024), AND R2 DOOR ASSIST BOTTLES PER AMM 52-12-51.

Part: UNKNOWN — MALFUNCTIONED (LE SLAT) · airframe 24,301 hrs · 20,151 cycles

AIRCRAFT WAS GROUNDED: SLAT FAILED UPON SELECTION OF FLAPS 1. ACCOMPLISHED QRH PRECAUTION, SLATS AND FLAPS EXTENDED NORMALLY. MAINTENANCE PERFORMED SLAT OPERATIONAL TEST AFTER RTS TEST PER AMM 27-80-00-710-801-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,727 hrs · 19,687 cycles

LEFT SIDE EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-15/400. OPS CHECKED NORMAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,946 hrs · 19,046 cycles

LEFT OVERWING DOOR LOWER EXIT SIGN DID NOT ILLUMINATE. REPLACED EXIT SIGN ASSEMBLY IAW AMM 33-50-15. OPS CHECKED OK FOR SERVICE.

Part: APU — LEAKING (ZONE 200) · airframe 22,572 hrs · 18,761 cycles

AIRCRAFT WAS GROUNDED. PHL FLT 1889 EN-ROUTE PHL - MCI. AN UNUSUAL ODOR WAS NOTED IN THE AIRCRAFT CABIN SHORTLY AFTER TAKE-OFF. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO PHL WITHOUT FURTHER INCIDENT. REPLACED APU ASSEMBLY PER J/C 43L35249001. OPERATIONS TEST AND LEAK CHECK GOOD. NO MORE ODOR NOTED WHILE RUNNING PACKS OFF OF APU BLEED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 22,456 hrs · 18,682 cycles

L1 EMERGENCY PNEUMATIC ASSEMBLY REQUIRED SERVICING. SERVICED L1 FOWARD PASSENGER DOOR PER WEEKLY CHECK JOBCARD 43C10005002 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 21,863 hrs · 18,214 cycles

LAVATORY SMOKE WARNING DURING FLIGHT. PERFORMED AN OPS TEST OF THE LAVATORY SMOKE DETECTOR IAW AMM 26-14-01-710-801-A/500. NO FAULTS NOTED. OK FOR CONTINUED SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 21,713 hrs · 18,072 cycles

CRACKED RT WING FIXED LEADING EDGE RIB 17 AT YA8551. REPLACED THE RIB IAW DRAWING 191-03203-421, SRM 51-43-03, AND SRM 51-41-01,51-41

Part: WINDOW — CRAZED (PAX CABIN) · airframe 21,713 hrs · 18,072 cycles

LEFT MAIN CABIN PASSENGER NR 1 WINDOW IS CRAZED. REPLACED THE WINDOW IAW AMM 56-20-00.

Part: LAMP — INOPERATIVE (EXIT SIGN) · airframe 21,713 hrs · 18,072 cycles

LEFT AFT ENTRY DOOR EXIT SIGN WITH ONE LED INOPERATIVE. AIRCRAFT WAS GROUNDED. REPLACED EXIT SIGN.

Part: DOUBLER — CORRODED (COCKPIT FLOOR) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON COCKPIT FLOOR STRUCTURE, LEFT DOUBLER. REPAIRED THE FLOOR DOUBLER IAW EA 277336A.

Part: DOUBLER — CORRODED (FRAMES 7-12) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

COCKPIT FLOOR STRUCTURE RIGHT DOUBLER HAS CORROSION BETWEEN FRAMES 7 TO 12, RBL 11 TO RBL 37. REPAIRED IAW 53-10 10-1, REPAR 1, AND EA 277332.

Part: HINGE — WORN (RT WING AILERON) · airframe 21,713 hrs · 18,072 cycles

RIGHT WING AILERON NR 1 HINGE FOUND TO BE WORN AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE IAW AMM 57-61-00-000-801.

Part: HINGE — WORN (RT WING AILERON) · airframe 21,713 hrs · 18,072 cycles

RIGHT WING AILERON NR 2 HINGE FOUND TO BE WORN AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE IAW AMM 57-61-00-000-801.

Part: HINGE — WORN (RT WING AILERON) · airframe 21,713 hrs · 18,072 cycles

RIGHT WING AILERON NR 4 HINGE WAS FOUND TO BE WORN AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE IAW AMM 57-61-00-000-801.

Part: HINGE — WORN (RT WING AILERON) · airframe 21,713 hrs · 18,072 cycles

RIGHT WING AILERON NR 3 HINGE WORN AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE IAW AMM 57-61-00-000-801.

Part: DOUBLER — CORRODED (FRAME 11) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE DOUBLER CONNECTOR LOCATED AT FRAME 11, Y=+25.4. REPLACED CONNECTOR IAW DWG 170-13808-001, DWG 170-00825-503, & SRM.

Part: SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE RIGHT SUPPORT LOCATED BETWEEN FRAMES 17 AND 18, WL Z-490, AND Y+1160 Y=+1200. REPLACED THE SUPPORT IAW 53-00-00-3, REPAIR 3, FIG 1.

Part: GUIDE — WORN (LT WING TE FLAP) · airframe 21,713 hrs · 18,072 cycles

LEFT OUTBOARD FLAP, OUTBOARD END GUIDE TRACK HAS WEAR DAMAGE LOCATED RIB 23, STR YA11335. REPLACED GUIDE IAW AMM 57-50-07-000-801A, & 57-50-07-400-801-A/4.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 21,713 hrs · 18,072 cycles

CRACK FOUND ON THE FLOORBEAM ANGLE AT FRAME 12, Y0. REPLACED THE FLOORBEAM ANGLE IAW DWG 170-16131-001, AND 171-00237-403.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 16, AND -Y1140. REPLACED FLOOR SUPPORT IAW DWG 170-21768-403.

Part: SEAT TRACK — CORRODED (FRAMES 65-66) · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON AFT MAIN CABIN RIGHT INBOARD SEAT TRACK CROWN BETWEEN FRAMES 65 AND 66, Y270. REPLACED THE SEAT TRACK IAW DWG 190-25017-415.

Part: SEAT TRACK — CORRODED (FRAMES 12-17) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE SEAT TRACK LOCATED BETWEEEN FRAMES 12 AND 17, Y+276. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3.

Part: ANGLE — CRACKED (FRM 12 FLOORBEAM) · airframe 21,713 hrs · 18,072 cycles

CRACK FOUND ON THE FLOORBEAM ANGLE FR 12. REPLACED THE ANGLE IAW SRM 51-41-01 AND DWG 171-00237-403.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE AFT CABIN MAIN RIGHT SEAT TRACK AT FRAME 84, Y276. REMOVED, AND REPLACED DOUBLER AT RIGHT HAND FLOOR SEAT TRACK IAW SRM 53-23-10, REPAIR 54.

Part: DOUBLER — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE DOUBLER IN THE AFT MAIN CABIN FLOOR AT FRAME 84, Y276. REPLACED THE DOUBLER IAW DWG 190-65294-401, SRM 51-43-04, AND 51-43-0.

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN FLOOR DOUBLER, FRAME 16, Y=-330. REMOVED AND REPLACED FLOOR DOUBLER IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE LEFT FLOOR SUPPORT, FRAME 19, Y-1140. REPLACED THE FLOOR SUPPORT IAW DWG 170-29712-805.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION WAS FOUND ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 12 AND 14, BETWEEN Y980 AND Y1210. REPLACED FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 19 AND 20, -Y1200. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REP 3, AND SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON THE AFT MAIN CABIN FLOOR SHEAR PANEL BETWEEN FRAMES 84 AND 85, Y1194. REPLACED THE SHEAR PANEL IAW DWG 190-65140-801.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORRODSION WAS FOUND ON THE AFT MAIN CABIN FLOOR RIGHT SHEAR PANEL AT FRAME 87 AND 88, BETWEEN Y330 AND Y1140. REPLACED THE SHEAR PANEL IAW 53-00-00-3, REPAIR 3.

Part: REINFORCEMENT — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON AFT MAIN CABIN FLOOR REINFORCEMENT STRUCTURE BETWEEN FRAMES 84 AND 85 BETWEEN Y330 AND Y1194. REPLACED THE REINFORCEMENT IAW DWG 190-65140-801.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 12 AND 13, Y370. REPLACED FLOOR SUPPORT IAW DWG 190-05555-805.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 17 AND 18, Y340. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, & DWG 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,713 hrs · 18,072 cycles

CORROSION FOUND ON AFT MAIN CABIN FLOOR SUPPORT AT FRAME 84, -Y1168. REPLACED FLOOR SUPPORT

Part: LIGHT — MISSING (CABIN) · airframe 21,620 hrs · 18,000 cycles

FIRST ROW EMERGENCY LIGHT STRIP AT THE R1 DOOR FOUND MISSING. INSTALLED THE LIGHT.

Part: WINDOW — CRAZED (COCKPIT) · airframe 21,240 hrs · 17,732 cycles

AIRCRAFT WAS GROUNDED. CRAZED CAPTAIN'S DIRECT VIEW SIDE WINDOW AND UNABLE TO SEE OUT CLEARLY. REPLACED CAPTAINS DIRECT VIEW SIDE WINDOW PER AMM 56-12-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 21,174 hrs · 17,690 cycles

EMERGENCY LIGHT OVER CENTER AISLE NEAR ROW 27 IS INOPERATIVE. SECURED THE CONNECTOR. AIRCRAFT WAS GROUNDED.

Part: GIRT BAR — FOD (L2 DOOR SLIDE) · airframe 21,011 hrs · 17,558 cycles

L2 DOOR BINDING, FLIGHT ATTENDANT REPORTED HEARING SOMETHING MECHANICAL OR METAL ON METAL. CLEARED FOD FROM GIRT ENGAGEMENT HOOK.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 20,723 hrs · 17,326 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHT POWER UNIT NR 6 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY POWER SUPPLY UNIT NR 6.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 20,723 hrs · 17,326 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHT POWER UNIT NR 5 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY POWER SUPPLY UNIT NR 5.

Part: POWER UNIT — FAILED (CABIN) · airframe 20,723 hrs · 17,326 cycles

AIRCRAFT WAS GROUNDED. EPLU NR 2 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT POWER UNIT.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 20,723 hrs · 17,326 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHT POWER UNIT 1 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY POWER SUPPLY UNIT NR 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,187 hrs · 16,868 cycles

RIGHT SIDE 5 FEET OF EMERGENCY LIGHT STRIP BY ROWS 1 AND 2, INOPERATIVE. REPLACED THE LIGHT STRIP IAW AMM 33-50-21.

Part: STRAP — UNKNOWN (FLASHLIGHT) · airframe 19,930 hrs · 16,658 cycles

FLIGHT ATTENDANT REPORTED FORWARD CABIN FLASHLIGHT STRAP NEEDS TO BE REPLACED. REPLACED THE STRAP IAW MM 33-51-01.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 19,577 hrs · 16,405 cycles

AIRCRAFT WAS NOT GROUNDED. PHOTO LUMINESCENT STRIP MISSING 1D FROM FIRST SECTION ON THE RIGHT SIDE THAT SUPPOSED TO BE GLUED TO GALLEY FLOOR. MAINTENANCE REPLACED PHOTO LUMINESCENT STRIP AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,719 hrs · 14,883 cycles

RETURNED, ACFT WAS GNDED. CLIMBING THROUGH FL 230, DOOR EMER RT OPEN WARNING. CABIN ALT APPROX 7000 & CLIMBING AT 780 FPM, COULD NOT CONFIRM PRESSURIZATION WAS NORMAL. RETURNED TO FIELD FOR PRECAUTIONARY LANDING. PERFORMED AMM 52-21-02-200-801A OVERWING HATCH INSPECTION. PERFORMED AMM TASK 21-31-00-720-802-A PRESSURIZE TESTED GOOD. ACFT RETURNED TO SERVICE.

Part: FILTER — DIRTY (ZONE 100) · airframe 17,644 hrs · 14,807 cycles

AIRCRAFT WAS NOT GNDED. ON GND, AT GATE WITH APU ON, NOTICED BURNING RUBBER TYPE SMELL WHEN TEMP TURNED UP WARMER THAN FULL COLD. FOUND DUCT, BETWEEN THE H DUCT MIXING CHAMBER & THE GASPER DUCT COMPLETELY DISCONNECTED, DUCT WAS RECONNECTED. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO MORE ODORS BEING NOTED. ALSO FOUND BOTH RECIRCULATION FILTERS DIRTY & REPLACED THEM IAW AMM 21-24-02. SEE AALA201603099004 FOR ADDITIONAL PART.

Part: AIR DUCT — DETACHED (ZONE 100) · airframe 17,644 hrs · 14,807 cycles

AIRCRAFT WAS NOT GNDED. ON GROUND, AT GATE WITH APU ON, NOTICED BURNING RUBBER TYPE SMELL WHEN TEMP TURNED UP WARMER THAN FULL COLD. FOUND DUCT, BETWEEN THE H DUCT MIXING CHAMBER & THE GASPER DUCT COMPLETELY DISCONNECTED. DUCT WAS RE-CONNECTED & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO MORE ODORS BEING NOTED. ALSO FOUND BOTH RECIRCULATION FILTERS DIRTY & REPLACED THEM IAW AMM 21-24-02. SEE AALA 201603099016 FOR ADDITIONAL PART.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. UPPER EMER EXIT SIGN AT R1 DOOR IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 17,253 hrs · 14,468 cycles

UPPER EMERGENCY EXIT SIGN AT L1 DOOR IS CRACKED. R & R THE EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. LOWER EMER EXIT SIGN AT L1 DOOR IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 17,253 hrs · 14,468 cycles

LOWER R1 EXIT IDENTIFIER SIGN IS INOPERATIVE. FOUND CONNECTOR SP0888 NOT PROPERLY SECURED. SECURED SP0888 & PERFORMED OPERATIONAL CHECK IAW AMM 25-23-10, 33-50-15 & 33-50-00 & WM 33-50-50. CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 17,253 hrs · 14,468 cycles

AFT CABIN CEILING EMERGENCY LIGHT IS INOPERATIVE. FOUND P2939 CONNECTOR TO AFT CABIN CEILING EMERGENCY LIGHT NOT SECURED PROPERLY. SECURED P2939 & PERFORMED OPERATIONAL CHECK IAW SWPM 20-52-00 & AMM 33-50-00. CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. UPPER EMER EXIT SIGN AT R2 DOOR IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. LOWER EMER EXIT SIGN AT L2 DOOR IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. LOWER EMER EXIT SIGN AT RT OVERWING EXIT IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 17,248 hrs · 14,466 cycles

DURING ACCOMPLISHMENT OF EO 5713P144, THE RT WING, LOWER SKIN WAS FOUND CRACKED AT THE FASTENER HOLE, NEXT TO & OTBD OF THE DRAIN HOLE AT SPAR 2 & RIB 10. REPAIRED SKIN IAW EA 256428.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. LOWER EMER EXIT SIGN AT R2 DOOR IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,253 hrs · 14,468 cycles

AIRCRAFT WAS IN BASE MX. EMER EXIT SIGN AT ROW 2AC UPPER ON MONUMENT IS CRACKED. R & R EMER EXIT SIGN LENS IAW AMM 33-50-15, 33-50-17 & 33-50-00-710-801-A 500. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,248 hrs · 14,466 cycles

MAIN CABIN AFT RT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY IS LOW. R & R CABIN AFT RT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-01.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MAINTENANCE. MAIN CABIN LT PHOTO LUMINESCENT STRIPS ARE CRACKED & POOR CONDITIONS, MORE THAN 10% DAMAGED. REPLACED LT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: GROUND WIRE — KINKED (CABIN) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT LT WTB FAIRING UPPER EMER LIGHT GND WIRE KINKED, CONDUCTOR EXPOSED. REPLACED GND WIRE & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 20-41-20 & 33-50-00.

Part: LIGHT — CRACKED (CABIN) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. MAIN CABIN RT PHOTO LUMINESCENT STRIPS ARE CRACKED & POOR CONDITION, MORE THAN 10% DAMAGED. REPLACED RT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: BRACKET — CORRODED (FRAMES 77-80) · airframe 17,248 hrs · 14,466 cycles

FIVE EACH NUT SUPPORT BRACKETS ATTACHED TO AFT CARGO LOWER SILL BEAM, BETWEEN FRAME 77 - 80, HAVE CORROSION ON FACE AT SURROUND STRUCTURE CUT OUT 96-22. R & R FIVE EACH NUT SUPPORT BRACKETS IAW SRM 51-41-01 & DWG 120-85513-845.

Part: BRACKET — CORRODED (FRAMES 24-27) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON BRACKET, BETWEEN FRAME 24 & 27 AT Z-1550. REPLACED BRACKET IAW SRM 51-41-01 & DWG 170-67080-461.

Part: BRACKET — CORRODED (FRAMES 77-80) · airframe 17,248 hrs · 14,466 cycles

FIVE EACH NUT SUPPORT BRACKETS ATTACHED TO AFT CARGO LOWER SILL BEAM, BETWEEN FRAME 77 - 80, HAVE CORROSION ON FACE AT SURROUND STRUCTURE CUT OUT 96 - 22. R & R FIVE EACH NUT SUPPORT BRACKETS IAW SRM 51-41-01 & DWG 120-85513-845.

Part: BRACKET — CORRODED (FRAMES 24-27) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON BRACKET, BETWEEN FRAME 24 & 27 AT Z-1550. REPLACED BRACKET IAW SRM 51-41-01 & DWG 170-67080-461.

Part: BRACKET — CORRODED (FRAMES 77-80) · airframe 17,248 hrs · 14,466 cycles

FIVE EACH NUT SUPPORT BRACKETS ATTACHED TO AFT CARGO LOWER SILL BEAM, BETWEEN FRAME 77 - 80, HAVE CORROSION ON FACE AT SURROUND STRUCTURE CUT OUT 96 - 22. R & R FIVE EACH NUT SUPPORT BRACKETS IAW MM 51-41-01 & DWG 120-85513-845.

Part: BRACKET — CORRODED (FRAMES 24-27) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON BRACKET, BETWEEN FRAME 24 & 27, AT Z-1550. REPLACED BRACKET IAW SRM 51-41-01 & DWG 170-67080-461.

Part: BRACKET — CORRODED (FRAMES 77-80) · airframe 17,248 hrs · 14,466 cycles

FIVE EACH NUT SUPPORT BRACKETS ATTACHED TO AFT CARGO LOWER SILL BEAM, BETWEEN FRAME 77 - 80, HAVE CORROSION ON FACE AT SURROUND STRUCTURE CUT OUT 96 - 22. R & R FIVE EACH NUT SUPPORT BRACKETS IAW SRM 51-41-01 & DWG 120-85513-845.

Part: BRACKET — CORRODED (FRAMES 77-80) · airframe 17,248 hrs · 14,466 cycles

FIVE EACH NUT SUPPORT BRACKETS ATTACHED TO AFT CARGO LOWER SILL BEAM, BETWEEN FRAME 77 - 80, HAVE CORROSION ON FACE AT SURROUND STRUCTURE CUT OUT 96 - 22. R & R FIVE EACH NUT SUPPORT BRACKETS IAW SRM 51-41-01 & DWG 120-85513-845.

Part: BRACKET — CORRODED (FRAMES 24-27) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON BRACKET, BETWEEN FRAME 24 & 27, AT Z-1550. REPLACED BRACKET IAW SRM 51-41-01 & DWG 170-67080-461.

Part: BRACKET — CORRODED (FRAMES 24-27) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON BRACKET, BETWEEN FRAME 24 & 27, AT Z-1550. REPLACED BRACKET IAW SRM 51-41-01 & DWG 170-67080-461.

Part: LENS — CRACKED (EXTERIOR) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. AFT RT WTB FAIRING, UPPER EMER LIGHT LENS CRACKED. REPLACED AFT RT WTB FAIRING, UPPER EMER LIGHT IAW AMM 33-50-25. OPERATIONAL CHECKED GOOD.

Part: WIRE — DAMAGED (ZONE 100) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. WIRE W101-14702-12, NEAR EICC, HAS ARCING DAMAGE. REPAIRED WIRE W101-14702-12 IAW SWPM 20-41-20. OPERATIONS CHECKED GOOD IAW AMM 24-36-00.

Part: LENS — CRACKED (EXTERIOR) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. AFT LT WTB FAIRING, LOWER EMER LIGHT LENS CRACKED. REPLACED AFT LT WTB FAIRING, LOWER EMER LIGHT IAW AMM 33-50-25. OPERATIONAL CHECKED GOOD.

Part: SPLICE PLATE — DAMAGED (E/E BAY DOOR) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. FWD AVIONICS HATCH LT UPPER GUSSET & SPLICE PLATE FOUND WITH ARCING DAMAGE. REMOVED, FABRICATED & INSTALLED LT UPPER GUSSET & SPLICE PLATE ON FWD AVIONICS DOOR IAW SRM 52-43-00 FIG 05 51-41-01.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MAINTENANCE. VERTICAL STABILIZER RIB CRACKED, BETWEEN RIB 9 & 10. REPLACED RIB IAW SRM 51-41-02, 51-41-01 & DWG 190-63830-401.

Part: ROLLER — SEIZED (FUSELAGE) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. RT OVERWING EXIT DOOR CUT OUT, UPPER AFT LATCH ROLLER SEIZED. R & R RT OVERWING EXIT DOOR CUT OUT, UPPER AFT LATCH ROLLER IAW AMM 53-22-11-212-801-A.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT DOOR, CUT OUT LOWER AFT CORNER SEAL REST AT FRAME 27 & STRINGER 26R. REPLACED SEAL REST IAW AARD 53-00-00-3 REPAIR 3 SRM 51-40-02.

Part: PLATE — MISINSTALLED (PAX DOOR) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. FWD PAX DOOR FAILS EES MECHANISM IN EMER CONFIGURATION OPERATIONAL CHECK. DOOR DOES NOT FULLY OPEN. FOUND CONTROL PLATE INCORRECTLY INSTALLED & STRIKER IN DIS-ARMED POSITION, CORRECTLY INSTALLED CONTROL PLATE IN THE PLATE GUIDE & STRIKER. OPERATIONS CHECKED GOOD RECHARGED PNEUMATIC ASSEMBLY AT FWD PAX DOOR IAW AMM 52-11-53.

Part: PAN — CORRODED (FUSELAGE) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. CORROSION ON WASTE WATER PAN, BOX ASSEMBLY, BETWEEN FRAME 88 & 89, STRINGER 28R & 29R. REPLACED WASTE WATER PAN, BOX ASSEMBLY, IAW EO 5313P246.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MX. CORROSION ON CABIN FLOOR STRUCTURE, CTR SHEAR PANEL, BETWEEN FRAME 87 & 88. REPLACED SHEAR PANEL IAW SRM 51-41-02 & 51-43-04.

Part: SEAL REST — CORRODED (FRAMES 77-78) · airframe 17,248 hrs · 14,466 cycles

CORROSION ON AFT CARGO DOOR CUT OUT LOWER FWD CORNER SEAL REST, BETWEEN FRAME 77 & 78 AT STRINGER 26R. REPLACED SEAL REST IAW SRM 51-40-02 & AARP 53-00-00-03 REPAIR 3.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 17,248 hrs · 14,466 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT SIDE SHEAR PLATE, BETWEEN FRAME 87 & 88 AT -Y1020. REPLACED SHEAR PLATE IAW AARD 53-00-00-3 REPAIR 3.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

L1 EMERGENCY PNEUMATIC BOTTLE HAS LOW PRESSURE. SERVICED L1 DOOR EMERGENCY PNEUMATIC ASSEMBLY AS REQUIRED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST)

L2 EMERGENCY PNEUMATIC BOTTLE HAS LOW PRESSURE. SERVICED L2 DOOR EMERGENCY PNEUMATIC ASSEMBLY AS REQUIRED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,598 hrs · 13,017 cycles

FORWARD FLIGHT ATTENDANTS FLASHLIGHT. REPLACED BATTERY AS REQUIRED. OPERATIONAL CHECK IS NORMAL.

Part: COVER — BROKEN (ZONE 800) · airframe 15,030 hrs · 12,595 cycles

R 1 DOOR EMER EXIT LIGHT COVER BROKEN. REPLACED R1 DOOR EMER EXIT LIGHT COVER.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,988 hrs · 10,718 cycles

THE RT PYLON LOWER LINK OTBD & INBD FITTING SHEAR PIN LOCKNUTS LOOSE. RE-TORQUED THE RT PYLON LOWER LINK OTBD & INBD FITTING SHEAR PIN LOCKNUTS & APPLIED THE APPROPRIATE SAFETIES.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (PAX DOOR) · airframe 13,856 hrs · 11,482 cycles

LEFT FWD PAX DOOR EMERGENCY PNEUMATIC ASSEMBLY REQUIRES SERVICING. SERVICED LT FWD PAX DOOR EMERGENCY PNEUMATIC ASSEMBLY TO 2450 PSI.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 13,770 hrs · 11,419 cycles

PHL L2 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR ASSIST BOTTLE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - CABIN CROSS BEAM CORRODED AT FR 14 FROM RBL 20 INCHES TO RBL 30 INCHES. REPAIRED CROSS BEAM IAW EA 505262.

Part: LENS — DAMAGED (CABIN) · airframe 11,356 hrs · 9,586 cycles

EMERGENCY EXIT LIGHT LENS ON CEILING PANEL 228 ARC DAMAGED WHERE MARKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON CEILING PANEL 228 ARC IAW EMB190 AMM 33-21-01.

Part: LIGHT — BROKEN (CABIN) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - PANEL 254CRC EMERGENCY EXIT LIGHT BROKEN WHERE MARKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT 254CRC IAW EMB190 AMM 33-21-01.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - CORROSION ON FORWARD CARGO DOOR BEAM AT FR24, 4 INCHES AFT, S26R, RBL15. REPLACED FORWARD CARGO DOOR BEAM AT FR24, 4 INCHES AFT, S26R, RBL15 IAW EMBRAER SRM II 51-43-03, 51-43-04, 51-41-02 & 51-43-03.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET BETWEEN FR85 TO FR86, LBL 11. REPLACED UPPER SHEET BETWEEN FR85 TO FR86, LBL 11 IAW EMBRAER SRM II 51-41-02, 51-42-02, 51-23-04, 51-23-05 & 51-23-06.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET AT FR85, RBL 11. REPLACED UPPER SHEET AT FR85, RBL 11 IAW EMBRAER SRM II 51-43-03, 51-41-01, 51-40-02, 51-23-04, 51-23-05 & 51-23-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT FLOOR SILL BETWEEN FR12 TO FR14 & BETWEEN RBL 40 TO RBL 52. REPLACED RIGHT FLOOR SILL BETWEEN FR12 TO FR14 & BETWEEN RBL 40 TO RBL 52 IAW EMBRAER SRM II 51-41-02, 51-43-04, 51-40-03, 51-23-04, 51-23-05 & 51-23-06.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON PANEL MOUNT AT FR17, LBL 22. REPLACED PANEL MOUNT AT FR17, LBL 22 IAW EMBRAER SRM II 51-41-01, 51-23-04, 51-23-05 & 51-23-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR80, RBL 20. REPLACED GUSSET AT FR80, RBL20 IAW EMBRAER SRM II 51-41-02, 51-23-04, 51-23-05 & 51-23-06.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - CORROSION ON AFT CARGO LOWER BEAM BETWEEN FR80 TO FR84, RBL 54. REPLACED AFT CARGO LOWER BEAM BETWEEN FR80 TO FR84, RBL 54 IAW EMBRAER SRM II 51-40-02, 51-41-02, 51-43-01 & 51-23-10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT FLOORBEAM AT FR86, LBL 11. REPAIRED LEFT FLOORBEAM AT FR86, LBL 11 IAW EMBRAER SRM II 53-23-01, 51-23-04, 51-23-05 & 51-23-06.

Part: LIGHT — BROKEN (CABIN) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - PHOTO LUMINESCENT INDICATOR STRIP LIGHT BROKEN AT L5 POSITION. REPLACED LEFT LIGHT STRIP IAW EMBRAER 1 90 AMM 33-50-21-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOUBLER AT FR19 BETWEEN LBL 13 TO LBL 22. REPLACED DOUBLER AT FR19 BETWEEN LBL 13 TO LBL 22 IAW EMBRAER SRM II 51-43-04, 51-41-02, 51-23-04, 51-23-05 & 51-23-06.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR MOUNT AT FR18, LBL 25. REPLACED FLOOR MOUNT AT FR18, LBL 25 IAW EMBRAER SRM II 51-41-01, 51-40-03, 51-43-01, 51-23-04, 51-23-05 & 51-23-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET PLATE AT FR90, LBL 11. REPLACED GUSSET PLATE AT FR90, LBL 11 IAW EMBRAER SRM II 51-41-02, 51-23-04, 51-23-05 & 51-23-06.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON PANEL MOUNT AT FR17, RBL 22. REPLACED PANEL MOUNT AT FR17, RBL 22 IAW EMBRAER SRM II 51-40-03, 51-41-01, 51-23-04, 51-23-05 & 51-23-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT FR84 BETWEEN RBL 11 TO RBL 45. REPLACED SILL PLATE AT FR84 BETWEEN RBL 11 TO RBL 45 IAW EMBRAER SRM II 51-41-02, 51-43-01, 51-43-02 & 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET PLATE AT FR90, RBL 11. REPLACED GUSSET PLATE AT FR90, RBL 11 IAW EMBRAER SRM II 51-41-02, 51-23-04, 51-23-05 & 51-23-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SEAT TRACK BEAM AT FR14, RBL 11. REPLACED RIGHT SEAT TRACK BEAM AT FR14, RBL 11 IAW EMBRAER SRM II 51-41-02, 51-43-01, 51-43-02 & 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL AT FR87, RBL 11 INCHES TO RBL 40 INCHES. REPLACED SHEAR PANEL AT FR87, RBL 11 INCHES TO RBL 40 INCHES IAW EMBRAER SRM II 51-42-01, 51-23-04, 51-23-05 & 51-23-06.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CENTER SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN LBL 11 & RBL 11. REPLACED CENTER SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN LBL 11 & RBL 11 IAW EMBRAER SRM II 51-40-02, 51-42-01, 51-23-04, 51-23-05 & 51-23-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT FLOOR SILL AT L1 DOOR AT FR16, LBL 50. REPLACED LEFT FLOOR SILL AT L1 DOOR AT FR16, LBL 50 IAW EMBRAER SRM II 51-41-02, 51-43-02, 51-23-04, 51-43-04 & 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR15, RBL 27. REPLACED FLOOR SUPPORT AT FR15, RBL 27 IAW EMBRAER SRM II 51-41-07, 51-23-04, 51-23-05 & 51-23-06.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD FRAME DOUBLER AT FR16 BETWEEN LBL 11 TO LBL 40. REPLACED FORWARD FRAME DOUBLER AT FR16 BETWEEN LBL 11 TO LBL 40 IAW EMBRAER SRM II 51-41-02, 51-40-02, 51-40-04 & 51-23-04.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON PANEL SUPPORT AT FR87 AT RBL 25. REPLACED PANEL SUPPORT AT FR87 AT RBL 25 IAW EMBRAER SRM II 51-40-03, 51-41-01 & 51-21-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHEAR PANEL AT FR87 BETWEEN LBL 11 TO LBL 30. REPLACED LEFT SHEAR PANEL AT FR87 BETWEEN LBL 11 TO LBL 30 IAW EMBRAER 190 SRM II 51-42-03, 51-23-04, 51-23-05 & 51-23-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - CORROSION ON LEFT SEAT TRACK BEAM AT FR16, LBL 11. REPLACED LEFT SEAT TRACK BEAM AT FR16, LBL 11 IAW EMBRAER SRM II 51-41-01, 51-41-02, 51-43-03, 51-43-04, 51-23-04, 51-23-05 & 51-23-06.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - PHOTO LUMINESCENT INDICATOR STRIP BROKEN AT L6 POSITION. REPLACED LEFT NR 6 LIGHT STRIP IAW EMBRAER 190 AMM 33-50-21-04.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SUPPORT AT FR87, LBL 30. REPLACED SUPPORT AT FR87, LBL 30 IAW EMBRAER SRM II 51-41-01, 51-40-02, 51-23-03, 51-23-04, 51-23-05 &, 51-23-06.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - CRACK ON SUPPORT AT FR85, RBL 30. REPLACED SUPPORT AT FR85, RBL 30 IAW EMBRAER SRM II 51-41-01 & 51-21-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SUPPORT AT FR86, LBL 30. REPLACED SUPPORT AT FR86, LBL 30 IAW EMBRAER 190 SRM II 51-40-02 & 51-23-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WAIST BOX DOUBLER AT FR89, RBL 11. REPLACED WAIST BOX DOUBLER AT FR89, RBL 11 IAW EMBRAER SRM II 51-43-02, 51-40-03, 51-23-04 & 51-23-05.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,356 hrs · 9,586 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SUPPORT AT FR86, RBL 30. REPLACED SUPPORT AT FR86, RBL30 IAW EMBRAER 190 SRM II 51-40-02 & 51-23-04.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (SERVICE DOOR) · airframe 10,089 hrs · 8,590 cycles

AFT SERVICE DOOR PNEUMATIC ASSEMBLY (DOOR ASSIST) REQUIRE SERVICING. MAINTENANCE SERVICED AFT SERVICE DOOR PNEUMATIC ASSEMBLY.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (SERVICE DOOR) · airframe 10,089 hrs · 8,590 cycles

FORWARD SERVICE DOOR PNEUMATIC ASSEMBLY (DOOR ASSIST) REQUIRE SERVICING. MAINTENANCE SERVICED FWD SERVICE DOOR PNEUMATIC ASSEMBLY.

Part: ACCUMULATOR — LOW (R2 DOOR) · airframe 9,979 hrs · 8,495 cycles

R2 DOOR ASSIST PNEUMATIC ASSEMBLY REQUIRES SERVICING. MAINTENANCE SERVICED R2 DOOR ASSIST PNEUMATIC ACCUMULTOR. NO FURTHER DEFECTS NOTED.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (SERVICE DOOR) · airframe 9,502 hrs · 8,065 cycles

AFT SERVICE DOOR PNEUMATIC ASSEMBLY PRESSURE LOW. MAINTENANCE SERVICED THE PNEUMATIC ASSEMBLY OF RIGHT AFT SERVICE DOOR.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 8,936 hrs · 7,526 cycles

R2 DOOR BOTTLE NEEDS SERVICED. MAINTENANCE SERVICED THE DOOR BOTTLE PER AMM 52-11-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,744 hrs · 6,603 cycles

BOS - FOUND NR 2 CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED FRONT RIGHT EMERGENCY LIGHT PSU. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,483 hrs · 6,353 cycles

LGA - R1 DOOR EMERGENCY EXIT RED LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT RED LIGHT ASSEMBLY IAW E-190 AMM 33-50-00 OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

BOS - THE R2 DOOR ASSIST BOTTLE BELOW PRESSURE. MAINTENANCE SERVICED THE R2 DOOR ASSIST BOTTLE PER AMM 52-41-51.

Part: ALTIMETER — FAILED (COCKPIT)

FLIGHT 1845, PVD-PHL - ON CLIMBOUT OF PVD THE CREW RECEIVED EICAS MESSAGES "YAW DAMPER OFF","1 RADAR ALTIMETER FAILED", THEN A CONTINUOUS SOUNDING OF THE LANDING GEAR AURAL WARNING HORN. THE CREW RECYCLED THE LANDING GEAR AT 4,000FT WITH NO POSITIVE RESULTS. THE CREW ELECTED TO RETURN TO PVD AND THE FLIGHT LANDING WAS UNEVENTFUL. MAINTENANCE MEL'D THE RADAR ALTIMETER 1 AND THE FLIGHT WILL DEPART TO PHL. PERFORMED FIM TASK 21-11-00-811-88F-A, SYSTEM CHECK IS NORMAL. THE NR 1 RADAR ALTIMETER WAS REMOVED AND REPLACED AS A PRECAUTION. THE MEL WAS REMOVED.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - THE RIGHT AFT PASSENGER DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED THE RIGHT AFT PASSENGER DOOR IAW AMM 52-12-51.

Part: DISC — PUNCTURED (R1 DOOR)

BOS - WHILE PERFORMING THE WEEKLY CHECK MAINTENANCE PERSONNEL FOUND THE PNEUMATIC DOOR ASSEMBLY DISC PUNCTURED ON THE R1 DOOR. MAINTENANCE REMOVED AND REPLACED THE DISC DIAPHRAGM ON THE R1 DOOR AND SERVICED AS REQUIRED PER AMM 52-41-51.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (CABIN PRESSURE)

BOS - THE LEFT AFT CABIN DOOR EMERGENCY PNUEMATIC ASSEMBLY PRESSURE IS LOW. MAINTENANCE SERVICED THE EMERGENCY PNUEMATIC ASSEMBLY PER AMM 52-12-51.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AIRCRAFT RIGHT AFT DOES NOT FLASH RED. UNABLE TO TELL IF IT IS CHARGING. MAINTENANCE REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - THE R2 PASSENGER DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE PER AMM 52-12-51-03.

Part: INDICATOR — FAULTY (DOOR)

PHL - THE AFT LEFT DOOR IS DIFFICULT TO ARM AND WHEN DISARMED, THE HANDLES APPEAR TO BE IN A LOWER POSITION THAN THE OTHER DOOR HANDLES. REMOVED AND REPLACED THE VISUAL LOCK INDICATOR ASSEMBLY.

Part: SENSOR — FAULTY (LE SLAT)

FLIGHT 9198, PHL-CLT - FLIGHT WAS A POSITION FERRY FLIGHT TO CLT. INBOUND THE CREW DECLARED AN EMERGENCY WHILE ON APPROACH TO LANDING FOR FLAPS 1, RECEIVED SLATS 0 FLAP 1 MESSAGE. THE CREW PERFORMED QRH PROCEDURE; LANDED WITH SLATS 0, FLAPS 2. BRAKES WERE USED NO MORE THAN FOR NORMAL LANDING DUE TO LIGHT WEIGHT AIRCRAFT AND LONG RUNWAY. MAINTENANCE REPLACED RIGHT SLAT 2-3 SKEW SENSOR FOR OPEN CIRCUIT CONDITION. ALSO FOUND INTERMITTENT WIRING IN RIGHT 2-3 SLAT HARNESS AND REPLACED THE HARNESS.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

CLT - THE FORWARD EMERGENCY BREAKAWAY FLASHLIGHT DOES NOT BLINK RED. MAINTENANCE REPLACED THE BATTERY, OPERATIONAL CHECK IS NORMAL.

Part: DIAPHRAGM — FAULTY (L1 DOOR)

DCA - THE L1 DOOR PNEUMATIC ASSEMBLY PRESSURE IS LOW. MAINTENANCE REMOVED AND REPLACED THE DIAPHRAGM.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

BDL - THE R2 DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED THE BOTTLE TO 2250 PSI.

Part: SIGN — INOPERATIVE (CABIN)

PHL - THE R1 DOOR EXIT IDENTIFIER SIGN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR EXIT IDENTIFIER SIGN.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

RIC - THE FORWARD EMERGENCY FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT BATTERY AND STRAP.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

PIT - R2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED THE R2 DOOR ASSIST BOTTLE.