N948UW

Part: VALVE — LEAKING (L2 DOOR) · airframe 24,844 hrs · 20,317 cycles

THE AIRCRAFT WAS NOT GROUNDED. L2 DOOR ASSIST FILLING VALVE LEAKING. REPLACED L2 DOOR RESERVOIR FILL VALVE PER AMM 52-12-51. NO LEAKS NOTED.

Part: BLEED VALVE — DEFECTIVE (RT ENGINE) · airframe 24,479 hrs · 20,001 cycles

BLEED 2 SURGING 5 - 75 PSI. CABIN ALTITUDE RATE +600 TO -800 FPM. STOPPED CLIMB AT FL-210. BLEED SURGE CONTINUED THROUGHOUT FINAL APPROACH. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT ENGINE BLEED PRESSURE VALVE IAW AMM 36-11-03. LEAK CHECK AND ENGINE RUN CHECKED GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 24,293 hrs · 19,847 cycles

THE EMERGENCY LIGHT D AND E, INOPERATIVE. R & R THE EMERGENCY LIGHTS IAW AMM 33-50-21. OPS CHECKED NORMAL.

Part: LIGHT — NO TEST (CABIN) · airframe 24,293 hrs · 19,847 cycles

THE EMERGENCY LIGHTS AT D AND E INOPERATIVE. R & R THE EMERGENCY LIHGTS IAW AMM 33-50-21. OPS CHECKED NORMAL.

Part: LIGHT — MISSING (GALLEY) · airframe 23,184 hrs · 18,979 cycles

PHOTOLUMINESCENT STRIP AT FORWARD GALLEY AIRCRAFT RIGHT SIDE MISSING APPROXIMATELY 18 INCH PIECE WHERE MOON MAT MEETS CARPET. PHOTOLUMINESCENT LIGHT STRIP INSTALLED AT FORWARD GALLEY AIRCRAFT RIGHT SIDE PER AMM 33-50-21.

Part: LIGHT — LOOSE (CABIN) · airframe 22,479 hrs · 18,432 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHTS AT SEAT 1D LOOSE. SECURED LIGHT SEGMENT.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 22,396 hrs · 18,377 cycles

R1 DOOR EXIT LIGHT LENS CRACKED. REPLACED EMERGENCY LIGHT LENS.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 22,224 hrs · 18,244 cycles

L2 DOOR SHOWS LOW PRESSURE ON DOOR ASSIST BOTTLE. CHARGED THE L2 DOOR ASSIST BOTTLE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,224 hrs · 18,244 cycles

CABIN CEILING EMERGENCY LIGHT LENS ABOVE ROW 13, MISSING. REPLACED EMERGENCY LIGHT.

Part: DOOR LATCH — NOT SEATED (EMERGENCY EXIT) · airframe 20,914 hrs · 17,177 cycles

RIGHT EMERGENCY DOOR OPEN ILLUMINATED AT NORMAL PRESSURE. MAINTENANCE FOUND OVERWING ESCAPE HATCH LATCH NOT SEATED COMPLETELY. RESEATED HATCH IAW AMM 52-21-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: RIB — CRACKED (LT WING) · airframe 20,911 hrs · 17,176 cycles

CRACK ON LEFT WING RIB 17. REPLACED RIB IAW SRM 51-41-02, 51-43-03, 51-43-04, DRAWING 190-31005-405 AND 190-31249-409 .

Part: SKIN — CRACKED (RT WING LE) · airframe 20,911 hrs · 17,176 cycles

CRACK ON RIGHT WING LEADING EDGE SKIN BETWEEN RIBS 17-23. REPLACED THE SKIN IAW SRM 51-41-02, 51-43-03, 51-42-02, 51-43-04, DRAWINGS 190-31003-405, AND 190-31249-409.

Part: HINGE FITTING — CORRODED (LT AILERON) · airframe 20,911 hrs · 17,176 cycles

LEFT AILERON NR 3 HINGE POINT RUSTED FROM INBOARD END AT BEARING. REPLACED AILERON HINGE IAW 57-61-01.

Part: RIB — CRACKED (RT WING) · airframe 20,911 hrs · 17,176 cycles

CRACK ON RIGHT WING RIB 17. REPLACED RIB IAW SRM'S 51-40-02/-03, 51-43-03/-04, 51-42-02, 51-41-01, AND DRAWING 190-13005-405.

Part: INDICATOR — DIRTY (SERVICE DOOR) · airframe 20,911 hrs · 17,176 cycles

FORWARD SERVICE DOOR UPPER AFT ARM - DISARM VISUAL INDICATOR WILL NOT SPRING BACK ALL THE WAY. CLEANED THE INDICATOR IAW AMM 12-22-01 AND AMM SDS 52-41-01.

Part: LINE — FRAYED (ESCAPE HATCH) · airframe 20,911 hrs · 17,176 cycles

FRAYED LEFT OVERWING ESCAPE HATCH LIFE LINE WITH LOOSE STITCHING. REPLACED ESCAPE LINE.

Part: PAD — WORN (DOOR FRAME) · airframe 20,911 hrs · 17,176 cycles

WORN DOOR STOP PAD AT AFT PASSENGER DOOR FUSELAGE FRAME FORWARD UPPER FITTING. REPLACED DOOR STOP PAD IAW AMM 53-23-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND SIDE SEAT TRACK AT Y260 BETWEEN FR 12 AND FR 16. REPLACED SEAT TRACK PER AARD ATA 53-00-00-3, SRM 51-40-02, 51-40-03, 51-41-01, 51-41-03, 51-43-02, AND 51-43-03.

Part: SUPPORT FITTING — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON FORWARD MAIN CABIN GALLEY SUPPORT FITTING AT Y260 BETWEEN FRAMES 13 AND 14. REPLACED THE SUPPORT FITTING IAW DRAWING 170-00822-413.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON RIGHT AFT MAIN CABIN SHEAR PANEL Y650 AND Y970, AND BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW DWG 53-00-00-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON LEFT FORWARD MAIN CABIN FLOOR SUPPORT -Y1120, BETWEEN FRAMES 12 AND 20. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, 51-40-03, AND DWG 170-00822-413.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1193.8 AND FR 16. REPLACED FLOOR SUPPORT PER SRM 51-43-03, 51-40-02/03, AND 51-23-04/05/06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN FLOOR SUPPORT AT Y304.88 BETWEEN FR 17 AND FR 18. REPLACED FLOOR SUPPORT PER SRM'S 51-75-16, 51-41-02, 51-43-04 AND 51-40-02.

Part: CROSSBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON FORWARD CABIN FLOORBEAM AT FRAME 14 BETWEEN Y280 AND Y820. REPAIRED THE FLOORBEAM IAW SRM 53-00-10.

Part: SUPPORT FITTING — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON RIGHT AFT CABIN GALLEY SUPPORT FITTING AT Y194 BETWEEN FRAMES 87 AND 88. REPLACED THE SUPPORT FITTING IAW SRM 51-43-03, AND SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT MAIN CABIN SEAT TRACK AT -Y250 BETWEEN FR 84 AND FR 85. REPAIRED SEAT TRACK PER SRM 53-23-10 REPAIR 54.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT MAIN CABIN LONGITUDINAL BEAM AT Y250 BETWEEN FR 86 AND FR 87. REPAIRED BEAM PER SRM 53-23-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT MAIN CABIN FLOOR SUPPORT AT -Y1150 AND FR84. REPLACED FLOOR SUPPORT PER SRM 51-41-01 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y380 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-02, SRM 51-41-01 AND DRAWING 170-00822-413.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND SEAT TRACK AT -Y260 BETWEEN FR 16 AND FR 20. REPLACED SEAT TRACK PER AARD 53-00-00-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1092 AND FR 19. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 51-43-01.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON AFT MAIN CABIN CENTER SHEAR PANEL BETWEEN FRAMES 87 AND 88. REPLACED SHEAR PANEL IAW AARD 53-00-00-3, REPAIR 3, SRM 51-40-02, 51-40-03, AND 51-42-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-21) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT AT -Y121, BETWEEN FRAMES 19 AND 21. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-01 AND DRAWING 170-00822-413.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON LEFT AFT MAIN CABIN FLOOR SUPPORT AT -Y997, FRAME 90. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, AND 51-43-03.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON AFT MAIN CABIN LEFT SHEAR PANEL AT -Y920 BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW 53-00-00-3, REPAIR 3, SRM 51-40-02, AND 51-42-01/-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,911 hrs · 17,176 cycles

CORROSION ON RIGHT FLOOR SUPPORT AT Y1016, BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, SRM 51-43-04 AND 53-00-00-3, REPAIR 3.

Part: DOOR — UNSECURE (ZONE 800 - DOORS) · airframe 20,862 hrs · 17,143 cycles

DURING CLIMBOUT, RECEIVED OPEN MESSAGE AT FORWARD SERVICE DOOR SERVICE. APPROXIMATELY 15000 FEET AND DISAPPEARED ABOUT10000 FEET. PRESSURIZATION APPEARED NORMAL, NO HISSING SOUNDS OBSERVED. MAINTENANCE PERFORMED TROUBLE SHOOTING PER FIM 52-41-00-810-803-A. INSPECTED SERVICE DOOR ACTUATING AND LOCK MECHANISMS. MEASURED RIGGING OF DOOR WARNING SENSOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FLAP SYSTEM — MALFUNCTIONED (SLAT/FLAPS) · airframe 20,721 hrs · 17,050 cycles

DURING APPROACH, RECEIVED SLAT FAIL ANNUNCIATION ON EICAS. ACCOMPLISHED CHECKLIST ITEMS, DECLARED AN EMERGENCY, LANDED FLAPS 2 WITH NO INCIDENT. MAINTENANCE PERFORMED RESET OF FLAP / SLAT SYSTEM IAW AMM 27-00-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,398 hrs · 15,906 cycles

AIRCRAFT WAS NOT GNDED. OVERHEAD EMER LIGHT AT CEILING PANEL NR 3 FAILS TO ILLUMINATE. REPLACED RT FRONT EMER LIGHTING POWER UNIT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-01.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 19,119 hrs · 15,671 cycles

AIRCRAFT WAS GNDED. UPON ACFT POWER UP RECEIVED EMER LIGHT BATTERY FAULT EICAS MSG. ACCOMPLISHED FIM 33-50-00 & FOUND LT MID EMER LIGHT POWER UNIT BAD. REPLACED IAW AMM 33-50-01. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,671 hrs · 15,232 cycles

AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT FLASHLIGHT IS NOT BLINKING. REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,649 hrs · 15,206 cycles

ACFT WAS GNDED. ON CLIMB THE CREW REPORTED A BURNING RUBBER ODOR IN THE CABIN. THE CREW DECLARED AN EMER & RETURNED, WHERE THE ACFT LANDED SAFELY WITH NO FURTHER INCIDENTS. PERFORMED TROUBLESHOOTING IAW JC 43L00021001, 43L00072001, & FIM TASK 21-20-00-810-801-A. NO ODORS NOTED, NO ADVERSE CONDITIONS NOTED. OPERATED BOTH PACKS INDIVIDUALLY & TOGETHER WITH ENG 1 - 2, & APU, NO ODORS NOTED AT THIS TIME. UNABLE TO DUPLICATE COMPLAINT. ACFT WAS RETURNED TO SERVICE.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 18,008 hrs · 14,664 cycles

FLIGHT 1794, OVERHEAD EXIT SIGN IN MID CABIN IS MISSING. LOCATED EXIT SIGN BEHIND COACH SEAT. INSTALLED SIGN & OPERATIONS CHECKED GOOD.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 17,693 hrs · 14,375 cycles

FLIGHT 2150, CAPTAINS WINDSHIELD AN AREA OF DELAMINATION AT LOWER RIGHT CORNER NEAR WINDSHIELD HEAT POINTS. REPLACED CAPTAINS WINDSHIELD IAW AMM 56-11-00.

Part: FIRE BOTTLE — EMPTY (AFT LAVATORY) · airframe 17,033 hrs · 13,818 cycles

AFT LAVATORY FIRE EXTINGUISHER BOTTLE EMPTY. R & R LAV FIRE EXTINGUISHER BOTTLE.

Part: FIRE BOTTLE — LOW PRESSURE (FWD LAVATORY) · airframe 17,033 hrs · 13,818 cycles

FORWARD LAVATORY FIRE EXTINGUISHER BOTTLE LOW WEIGHT. R & R FWD LAVATORY FIRE EXTINGUISHER BOTTLE.

Part: SEAL — LEAKING (NLG STRUT) · airframe 16,552 hrs · 13,427 cycles

EN-ROUTE, UPON RAISING GEAR GOT EICAS MSG, LG WOW SYS FAIL. DECLARED AN EMER & RETURNED TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED NLG SHOCK STRUT SEALS. ACCOMPLISHED A LG EXTENSION & RETRACTION SYS TEST, TESTED OK.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,300 hrs · 13,259 cycles

C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS ARE CRACKED & DAMAGED MORE THAN 10%. R & R AT MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: PIN — BACKED OUT (CABIN) · airframe 16,299 hrs · 13,259 cycles

C3 CHECK, EMER LIGHT EXIT SIGN AT FWD CLOSET AFT WALL IS INOPERATIVE. CHECKED FOR VOLTAGE AT LIGHT CONNECTOR, NO VOLTAGE. TROUBLE SHOT, FOUND PIN ON CONNECTOR J2477 RECEDED, INSERTED PIN. OPERATIONS CHECK GOOD ON EMER LIGHT EXIT SIGN AT FWD CLOSET AFT WALL IAW WM 33-50-50 & AMM 33-50-00-710-801A-A.

Part: LENS — CRACKED (EXIT SIGN) · airframe 16,304 hrs · 13,259 cycles

C3 CHECK, LOWER EMER EXIT SIGN AT R2 DOOR HAS A CRACKED LENS. REPLACED LOWER EMER EXIT SIGN. PERFORMED OPERATIONS CHECK, CHECKED GOOD IAW AMM 33-50-15-000-801, 33-50-15-400-801 & 33-50-00-710-801.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 86 TO 87, Z=-490MM & BETWEEN Y=+275MM TO Y=-275MM. REPLACED SHEAR PANEL IAW SRM 51-42-01 & 53-23-10.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 86 TO 87, Z=-490MM & BETWEEN Y=+275MM TO Y=+833MM. REPLACED SHEAR PANEL IAW SRM 51-42-01 & 53-23-10.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 86 TO 87, Z=-490MM & BETWEEN Y=-275MM TO Y=-833MM. REPLACED SHEAR PANEL IAW SRM 51-42-01 & 53-23-10.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90, Z=-490, Y=+625MM. REPLACED GUSSET IAW SRM 53-30-10 & 51-41-02.

Part: UPPER SHEET — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON UPPER SHEET BETWEEN FRAME 85 & 86, Z=-490, Y=+275MM. REPLACED UPPER SHEET IAW SRM 51-10-03, 53-23-10, 51-40-03, 51-43-01 & 51-41-01.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, CORROSION ON SEAL REST BETWEEN FRAME 78 TO 79, STRINGER 25R, Z=-1550, Y=+650MM. REPLACED CTR SEAL REST IAW SRM 53-23-11, 51-10-03, 51-23-05 & 51-41-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,297 hrs · 13,258 cycles

C3 CHECK, FWD CARGO DOOR CUT OUT LOWER SILL BEAM IS CORRODED BETWEEN FRAME 24 & 27. R & R BEAM IAW SRM 51-43-02.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 15,402 hrs · 12,490 cycles

THE LT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT LOOSE. ACCOMPLISHED A RE-TORQUE OF THE LT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT & APPLIED THE APPROPRIATE SAFETIES.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,402 hrs · 12,490 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON OTBD 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 15,402 hrs · 12,490 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 (RT PYLON) · airframe 15,402 hrs · 12,490 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: DIAPHRAGM — DEFECTIVE (PAX DOOR) · airframe 15,372 hrs · 12,447 cycles

AFT LT PAX DOOR ASSIST BOTTLE PRESS READS 0 PSI. R & R AFT LT DOOR PNEUMATIC ASSEMBLY DIAPHRAGM & SERVICED PNEUMATIC DOOR ASSEMBLY.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 14,429 hrs · 11,717 cycles

A3 CHECK, WHEN ACCOMPLISHING JOB CARD NUMBER 43C22025001 FOUND FIRST OFFICER`S FIXED WINDSHIELD DELAMINATED, CRACKED & BURNED ALONG UPPER & LOWER EDGES. REPLACED FIRST OFFICER`S WINDSHIELD IAW AMM 56-11-00-400-801-A. OPERATIONS & LEAK CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,813 hrs · 11,272 cycles

EMERGENCY LIGHTS EXIT SIGN ON AFT WALL OF FORWARD CLOSET INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT POWER UNIT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,813 hrs · 11,272 cycles

EMERGENCY EXIT LIGHT AT RT OVERWING EXIT INOPERATIVE. MX R & R NR 3 EMERGENCY LIGHT POWER UNIT.

Part: LIGHT — BROKEN (ZONE 200) · airframe 13,813 hrs · 11,272 cycles

EMERGENCY EXIT LIGHT AT L1 DOOR BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT.

Part: SEAT — OUT OF ADJUST (COCKPIT) · airframe 13,181 hrs · 10,796 cycles

CAPTAINS SEAT WILL NOT LOCK IN POSITION TO ALLOW IT TO SLIDE FORWARD AND AFT. MX PERFORMED ADJUSTMENT/TEST, OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,249 hrs · 9,342 cycles

AFT EMERGENCY FLASHLIGHT BATTERIES LOW. MAINTENANCE REMOVED AND REPLACED BATTERIES AS REQUIRED. OPERATIONAL CHECK OKAY FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,249 hrs · 9,342 cycles

FORWARD EMERGENCY FLASHLIGHT BATTERIES LOW. MAINTENANCE REMOVED AND REPLACED BATTERIES AS REQUIRED. OPERATIONAL CHECK OKAY FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 10,932 hrs · 9,040 cycles

LGA FLT 2117 BOS-LGA DIRTY/MUSTY OIL SMELL DURING TAXI, TAKEOFF, CRUISE, DESCENT, TAXI-IN. DRAINED NR 1 ENGINE OIL TANK. RAN PACKS, WITH AIR SOURCE FROM THE APU AND ENGINES NR 1 & 2. NO ODOR DETECTED. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: BELLCRANK — OUT OF ADJUST (R1 DOOR) · airframe 10,908 hrs · 9,010 cycles

PHL - 1R DOOR VERY DIFFICULT TO ARM. PERFORMED ADJUSTMENT/TEST OF R1 SERVICE DOOR ARMING. FOUND LOWER BELLCRANK FINGER SLIGHTLY OUT OF ADJUST. RE-ADJUST PER ALL X-DIMENSION AND W-DIMENSION. BELLCRANK OPERATION NORMAL. FUNCTIONAL TEST OF ARMING /DISARMING EVAC SLIDE GOOD.

Part: ACTUATOR — INOPERATIVE (PITCH TRIM) · airframe 10,861 hrs · 8,978 cycles

FLIGHT 1811, FLIGHT CREW REPORTED CAPTAIN'S PITCH TRIM INOPERATIVE. FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONAL STABILIZER ACTUATOR CONTROL ELECTRONICS

Part: TRIGGER — DAMAGED (PAX DOOR) · airframe 10,821 hrs · 8,956 cycles

C2 CHECK - AFT PASSENGER DOOR, PNEUMATIC DOOR ASSIST TRIGGER ASSEMBLY DAMAGED. REMOVED AND REPLACED DAMAGED PNEUMATIC ASSEMBLY IAW E190 AMM PART 2, 52-12-51.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR FRAME DOUBLER AT FR90, Z-490, Y625. REPLACED FLOOR FRAME DOUBLER AT FR90, Z-490, Y625 IAW ERJ 190 SRM PART 2, 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SILL BETWEEN FR12 TO FR16, Z-490, Y-1380. REPLACED FLOOR SILL BETWEEN FR12 TO FR16, Z-490, Y-1380 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT ANGLE AT FR16, Z-290, Y715. REPLACED FLOOR SUPPORT ANGLE AT FR16, Z-290, Y715 IAW E190 SRM 53-10-1 FIGURE 76 ITEM 60.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK AT FR84, WL-490, Y273. REPLACED SEAT TRACK AT FR84, WL-490, Y273 IAW E190 SRM 53-00-10 REPAIR 51P AND EA 202717.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, Z490, Y273. REPLACED GUSSET AT FR90, Z490, Y273 IAW ERJ 190 SRM PART 2, 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR84 TO FR89, Z-490, Y273. REPLACED SEAT TRACK BETWEEN FR84 TO FR89, Z-490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563 AND DRAWING 170-65660-439.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR84, Z-490, BETWEEN Y273 TO Y1310. REPLACED FLOOR SUPPORT AT FR84, Z-490, BETWEEN Y273 TO Y1310 IAW E190 SRM 51 PART 2 AND DRAWING 190-65140-801.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, Z490, -Y505. REPLACED GUSSET AT FR90, Z490, -Y505 IAW ERJ 190 SRM PART 2, 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR14 TO FR18, Z-490, Y273. REPLACED SEAT TRACK BETWEEN FR14 TO FR18, Z-490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563 AND E190 SRM 51-41-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88, Z-490, BETWEEN Y273 TO Y-273. REPLACED IAW TYPICAL REPAIR 190-5300-11-0563.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, Z490, -Y273. REPLACED GUSSET AT FR90, Z490, -Y273 IAW ERJ 190 SRM PART 2, 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR16 TO FR19, Z-490, Y-273. REPLACED SEAT TRACK BETWEEN FR16 TO FR19, Z-490, Y-273 IAW E190 SRM-51-43-01 AND TYPICAL REPAIR 190-5300-11-0563.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR84 TO FR86, Z-490, Y-273. REPLACED SEAT TRACK BETWEEN FR84 TO FR86, Z-490, Y-273 IAW E190 SRM 51-41-01, SRM 51-43-03.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB SPLICE BETWEEN FR87 TO FR88, Z-490, Y-1175. REPLACED WEB SPLICE BETWEEN FR87 TO FR88, Z-490, Y-1175 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOUBLER BETWEEN FR19 TO FR20, Z-490, Y-273. REPLACED DOUBLER BETWEEN FR19 TO FR20, Z-490, Y-273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y273 TO -Y1175. REPLACED WEB BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y273 TO -Y1175 IAW ERJ 190 SRM 51-42-03 & 51-23-00.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB BETWEEN FR12 TO FR14, Z-490, Y1100. REPLACED IAW E190 SRM 53-10-10 AND TYPICAL REPAIR 190-5300-11-0563.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR DOUBLER BETWEEN FR12 TO FR16, Z-490, Y-273. REPLACED FLOOR DOUBLER BETWEEN FR12 TO FR16, Z-490, Y-273 IAW TYPICAL REPAIR 190-5300-11-0563 AND E190 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,752 hrs · 8,900 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB BETWEEN FR87 TO FR88, Z-490 & BETWEEN Y273 TO Y1175. REPLACED WEB BETWEEN FR87 TO FR88, Z-490 & BETWEEN Y273 TO Y1175 IAW ERJ 190 SRM 51-40-02 & 51-42-01.

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 9,642 hrs · 7,950 cycles

PHL - THE FIRST OFFICERS SEAT WILL NOT LOCK IN TRACK. MAINTENANCE CLEANED AND LUBRICATED THE FIRST OFFICER'S SEAT TRACK. OPERATIONAL CHECK IS NORMAL.

Part: AIR FILTER — DIRTY (CABIN) · airframe 8,903 hrs · 7,360 cycles

FLIGHT 1467, PHL - ATL - DURING NORMAL APPROACH PROCEDURES TO FINAL AT ATL BOTH FLIGHT ATTENDANTS REPORTED THEY BECAME DIZZY AND HAD TO USE OXYGEN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RECIRCULATION AIR FILTER. ACCOMPLISHED A HIGH POWER ENGINE RUN WITH NO ODORS NOTED.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 8,761 hrs · 7,240 cycles

BOS - FOUND RIGHT AFT PASSENGER DOOR EMERGENCY PNEUMATIC AT 900 PSI. SERVICED RIGHT AFT PASSENGER DOOR EMERGENCY PNEUMATIC IAW E190 AMM 52-12-51. NO DEFECTS NOTED.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

BOS - BOTH LEFT AND RIGHT AFT SERVICE DOOR ASSIST BOTTLES LOW PRESSURE. MAINTENANCE SERVICED BOTH LEFT AND RIGHT SERVICE DOOR ASSIST BOTTLES PER AMM 52-12-51-03.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

BOS - BOTH LEFT AND RIGHT AFT SERVICE DOOR ASSIST BOTTLES LOW PRESSURE. MAINTENANCE SERVICED BOTH LEFT AND RIGHT SERVICE DOOR ASSIST BOTTLES PER AMM 52-12-51-03.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

BOS - THE RIGHT FORWARD SERVICE DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED THE RIGHT FORWARD SERVICE DOOR ASSIST BOTTLE PER AMM 52-11-51-03.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOS - THE FORWARD FIRST CLASS CENTER EMERGENCY LIGHT IS OUT. MAINTENANCE REPLACED THE FORWARD POWER SUPPLY. OPERATIONAL CHECK IS GOOD.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - THE RIGHT FORWARD PASSENGER DOOR EMERGENCY PNEUMATIC ASSEMBLY BOTTLE IS LOW. MAINTENANCE SERVICED THE PASSENGER DOOR ASSIST BOTTLE PER AMM 52-11-51.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - THE LEFT AFT PASSENGER DOOR EMERGENCY PNEUMATIC ASSEMBLY BOTTLE IS LOW. MAINTENANCE SERVICED THE PASSENGER DOOR ASSIST BOTTLE PER AMM 52-11-51.

Part: POWER UNIT — INOPERATIVE (CABIN)

BOS - AFT RIGHT BOTTOM EMERGENCY LIGHT INOPERATIVE ON R2 DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER UNIT. OPS CHECK IS NORMAL.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

BOS - THE R2 DOOR BOTTLE NEEDS SERVICE. MAINTENANCE SERVICED THE BOTTLE PER AMM 52-12-51.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (R2 DOOR)

BOS - THE R2 PASSENGER DOOR REQUIRES PNEUMATIC SERVICE. MAINTENANCE SERVICED THE R2 DOOR PNEUMATIC ASSEMBLY PER AMM 52-11-51.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (R2 DOOR)

LGA - THE R2 DOOR PNEUMATIC ASSEMBLY NEEDS SERVICING. MAINTENANCE SERVICED THE R2 DOOR PNEUMATIC ASSEMBLY.

Part: STRIKER — INOPERATIVE (L1 DOOR)

PIT - DURING THE EVACUATION SLIDE FUNCTIONAL TEST THE L1 DOOR ONLY PARTIALLY OPENED, COULD NOT OPEN OR CLOSE UNTIL THE ASSIST BOTTLE WAS DRAINED. MAINTENANCE REMOVED AND REPLACED THE STRIKER ASSEMBLY. PER CMM 52-11-51, THE DOOR ASSIST OPERATIONAL CHECK IS SATISFACTORY.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE FORWARD LEFT WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER UNIT.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR)

ATL - L2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED THE L2 DOOR EMERGENCY ACCUMULATOR.

Part: SLIDE — LOOSE (L1 DOOR)

CLT THE L1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND PARTIALLY DEPLOYED. MX FOUND THE PRIMARY RELEASE PIN WAS FREED, AND THE SLIDE DROPPED TO THE JETWAY. MX REPLACED THE L1 DOOR EMERGENCY ESCAPE SLIDE.

Part: BRACKET — BENT (L1 DOOR)

CLT THE L1 DOOR PNEUMATIC ASSIST STRIKER BRACKET WAS FOUND BENT. MX REPLACED THE L1 DOOR PNEUMATIC ASSIST ASSEMBLY. OK FOR SERVICE.

Part: SLIDE — COLLAPSED (L1 DOOR)

CLT THE REPLACEMENT SLIDE FOR THE L1 DOOR WAS FOUND COMING APART. MX RETURNED THE DISCREPANT SLIDE TO STOCK AND INSTALLED NEW SLIDE. OK FOR SERVICE.