N949UW

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 23,615 hrs · 19,767 cycles

EMERGENCY LIGHT INOPERATIVE AT THE CEILING, ROW 17 IN ISLE. REPLACED THE LIGHT BATTERY PACK IAW AMM 33-50-01, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SEAT TRACK — FOD (CREW SEAT) · airframe 22,812 hrs · 19,089 cycles

FLIGHT CREW SEAT HORIZONTAL ADJUSTMENT WERE INOPERATIVE FOR SEAT TO SLIDE AFT, DURING TAKEOFF. MAINTENANCE REMOVED DEBRIS FROM SEAT TRACK AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 22,222 hrs · 18,589 cycles

FLIGHT ATTENDANT REPORTED AFT GALLEY EXIT LIGHT LENS LOOSE. REPLACED THE AFT GALLEY EXIT LIGHT LENS.

Part: SLIDING WINDOW — DAMAGED (COCKPIT) · airframe 21,992 hrs · 18,397 cycles

UNABLE TO SEE CLEARLY OUT OF THE CAPTAIN'S SLIDING SIDE VIEW WINDOW. REPLACED THE WINDOW IAW AMM #56-12-00/400. ACCOMPLISHED ADJUSTMENT OF LOCKING MECHANISM IAW AMM 56-12-00-820-801A, AND FUNCTIONAL TESTED PRESSURIZATION IAW AMM 21-31-00720-802A-500. AIRCRAFT WAS GROUNDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,112 hrs · 17,625 cycles

STRONG DIRTY SOCKS ODOR AT 3000 FT ON FINAL. ODOR ONLY IN COCKPIT. OXYGEN MASK DONNED AND EMERGENCY DECLARED. ACCOMPLISHED CABIN ODOR JOB CARDS. NO FAULTS FOUND. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,926 hrs · 17,472 cycles

EMERGENCY EXIT LIGHT AT THE L2 DOOR INOPERATIVE. REPLACED THE BATTERY PACK.

Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT) · airframe 20,570 hrs · 17,201 cycles

LEFT SLIDING WINDOW DIFFICULT TO OPEN. HAVE TO PUSH FORWARD ON HANDLE TO BE ABLE TO DEPRESS THE UNLOCK BUTTON. LUBED THE SLIDING WINDOW.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. WEAR ON LEFT WING INBOARD FLAP TRACK INBOARD HALVE AT -Y1830. REPLACED FLAP TRACK PER SRM 57-52-03 AND AMM 57-54-21.

Part: LENS — CRACKED (EXIT SIGN) · airframe 20,523 hrs · 17,156 cycles

AIRCRAFT IN BASE MAINTENANCE. RT OVERWING TOP EMERGENCY EXIT SIGN LENS CRACKED. REPLACED RT OVERWING TOP EMERGENCY EXIT SIGN LENS.

Part: SPAR — WORN (RT WING) · airframe 20,520 hrs · 17,155 cycles

WEAR ON RIGHT WING REAR SPAR NR 3 IN FITTING, BEHIND MAIN LANDING GEAR BETWEEN RIBS 6 AND 7. REPAIRED REAR SPAR IAW SRM 57-50-05.

Part: SIGN — BROKEN (CABIN) · airframe 20,523 hrs · 17,156 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT DOOR LT FUSELAGE, BOTTOM EMERGENCY EXIT SIGN CASE BROKEN. REPLACED AFT DOOR LT FUSELAGE BOTTOM EMERGENCY EXIT SIGN IDENTIFIER.

Part: SIGN — CRACKED (CABIN) · airframe 20,523 hrs · 17,156 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKS IN LT FORWARD ENTRY DOOR BOTTOM EMERGENCY EXIT LIGHT SIGN CASE. REPLACED LT FORWARD ENTRY DOOR BOTTOM EMERGENCY EXIT LIGHT SIGN.

Part: LENS — CRACKED (EXIT SIGN) · airframe 20,523 hrs · 171,456 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKS ON RT OVERWING EMERGENCY EXIT BOTTOM SIGN CASE. REPLACED RT OVERWING EMERGENCY EXIT SIGN IDENTIFIER.

Part: LENS — CRACKED (EXIT SIGN) · airframe 20,523 hrs · 17,156 cycles

AIRCRAFT IN BASE MAINTENANCE. LT FUSELAGE AFT DOOR, TOP EMERGENCY EXIT SIGN LENS CRACKED. REPLACED LT FUSELAGE AFT DOOR TOP EMERGENCY EXIT SIGN.

Part: FITTING — LOOSE (CRGO DOOR LATCH) · airframe 20,520 hrs · 17,155 cycles

BRASS SLEEVE SPINS ON LATCH PIN AT FORWARD CARGO DOOR CUTOUT, FORWARD AND AFT DOOR LATCH FITTINGS. REPLACED THE LATCH FITTING IAW AMM 53-21-29.

Part: LENS — CRACKED (EXIT SIGN) · airframe 20,523 hrs · 17,156 cycles

AIRCRAFT IN BASE MAINTENANCE. LT FORWARD ENTRY DOOR EMERGENCY EXIT TOP SIGN LENS CRACKED. REPLACED LT FORWARD ENTRY DOOR EMERGENCY EXIT SIGN.

Part: FITTING — FROZEN (CRGO DOOR LATCH) · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. FROZEN (DOES NOT SPIN ) LATCH PIN ON FORWARD CARGO DOOR CUTOUT, THIRD DOOR LATCH FITTING FROM THE FRONT. REPLACED LATCH FITTING IAW AMM 53-21-29.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN INBOARD SEAT TRACK CROWN AT -Y276 BETWEEN FR 20 AND FR 23. REPAIRED SEAT TRACK PER SRM 53-00-10 AND EA 268427.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON RIGHT AFT MAIN CABIN SHEAR TIE AT FRAME 88 BETWEEN STRINGERS 25 AND 27L. REPLACED THE SHEAR TIE IAW DRAWING 170-65900-441, SRM 51-41-01, 51-41-02, 51-43-03, AND 51-40-06.

Part: SEAT TRACK — CORRODED (FRAMES 12-15) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON RIGHT FORWARD MAIN CABIN SEAT TRACK AT Y276 BETWEEN FRAMES 12 AND 15. REPLACED SEAT TRACK IAW 53-00-00-3, REP 3, SRM 51-41-01, AND 51-43-03.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 20,520 hrs · 17,155 cycles

CRACK ON FLIGHT DECK FLOORBEAM ANGLE AT FRAME 12.REPLACED FLOORBEAM ANGLE IAW DWG 171-00237-403.

Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON LEFT AFT MAIN CABIN DIVIDER SUPPORT AT -Y360 AND FRAME 84. REPLACED DIVIDER SUPPORT IAW DRAWING 170-65600-439.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT MAIN CABIN CENTRAL SEAT TRACK AT FR.84 AND Y280. REMOVED AND REPLACED PREVIOUS REPAIR REPLACEMENT SECTION OF SEAT TRACK PER DWG 170-66000-441, E190 SRM 51-43-01, 51-43-02, 51-43-03 AND 53-00-10 REPAIR 51.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT AT -Y1150 AND FRAME 84. REPLACED FLOOR SUPPORT IAW DRAWING 170-66000-445.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN SEAT TRACK AT -Y276 BETWEEN FR 16 AND FR 20. REPLACED SEAT TRACK PER AARD 53-00-00 REP 3, SRM 51-43-01 AND 51-43-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04, AND DRAWING 170-00822-413.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON AFT MAIN CABIN LEFT CENTRAL SEAT TRACK AT -Y280 AND FRAME 84. REPAIRED THE SEAT TRACK IAW SRM 51-00-10, REPAIR 51.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND LATERAL SEAT TRACK AT Y1270 BETWEEN FR19 AND FR20. REPLACED SEAT TRACK PER SRM 51-41-01, 51-41-02, 51-43-03 AND DRAWING 170-17900-801.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FORWARD FLOOR SILL BETWEEN FR 16 AND FR 12, BETWEEN -Y1149 AND -Y1257. REPLACED FLOOR SILL PER AARD 53-00-00-3 REP 3, SRM 51-41-02 AND 51-43-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR DOUBLER AT -Y310 AND FR16. REPLACED FLOOR DOUBLER PER AARD 53-00-00-3 REPAIR 3 AND SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1140 AND FR 16. REPLACED FLOOR SUPPORT PER SRM 51-43-01.

Part: FLOOR SUPPORT — CRACKED (FRAME 85) · airframe 20,520 hrs · 17,155 cycles

CRACK FOUND ON THE AFT MAIN CABIN FLOOR SUPPORT, -Y730 AND FRAME 85. REPLACED FLOOR SUPPORT IAW DRAWING 170-65660-441.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN BEAM AT Y381 BETWEEN FR 12 AND FR 13. REPLACED BEAM PER DRAWING 170-00822-503.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOORBEAM AT Y308 BETWEEN FR 17 AND FR 18. REPLACED FLOORBEAM PER SRM 51-40-02, SRM 51-43-03 AND DRAWING 170-00822-413.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON RIGHT FORWARD MAIN CABIN FORWARD FLOOR SUPPORT, BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW 53-00-00, SRM 51-41-02, 51-43-04, AND 51-40-02.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION LEFT FORWARD MAIN CABIN AFT FLOOR DOUBLER BETWEEN -Y304 AND -Y850, FRAMES 19 AND 20.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 17 AND 20. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, SRM 51-41-02, 51-40-02, AND 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 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, 51-43-03 AND DRAWING 170-00822-505.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT MAIN CABIN DIVIDER SUPPORT AT -Y990 AND FR 84. REPLACED DIVIDER SUPPORT PER SRM'S 51-40-02, 51-43-03 AND DRAWING 170-65600-441.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON AFT MAIN CABIN SPLICE, -Y550 AND FRAME 90. REPLACED SPLICE IAW SRM 51-23-01, AND DWG 170-65660-447

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT MAIN CABIN FLOOR SUPPORT AT Y910 AND FR 89. REPLACED FLOOR SUPPORT PER SRM'S 51-41-02, 51-42-01, 51-43-01, 51-40-02 AND AARD 53-00-00-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT MAIN CABIN FLOOR SUPPORT AT -Y750 AND FR 90. REPLACED FLOOR SUPPORT PER AARD 53-00-00-3 REPAIR 3, SRM'S 51-41-01, 51-41-02, 51-42-01 AND 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN FLOOR SUPPORT AT Y737 AND FR 15. REPLACED FLOOR SUPPORT PER SRM'S 51-41-01, 51-40-02 AND DRAWING 170-21768-407.

Part: MOUNT FITTING — CRACKED (HORIZ STAB) · airframe 20,520 hrs · 17,155 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND ELEVATOR INBOARD PCU MOUNT FITTING AT HORIZONTAL SPAR 3. REPLACED MOUNT FITTING PER DRAWING 190-09152-405, SRM 51-40-02, 51-40-03 AND 51-43-03.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,520 hrs · 17,155 cycles

CORROSION ON LEFT AFT MAIN CABIN SHEAR PANEL AT -Y920 BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW 53-00-00-3, REPAIR 3.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,442 hrs · 17,102 cycles

EMERGENCY LIGHT INOPERATIVE IN COCKPIT. CHARGED THE BATTERIES IAW AMM 33-50-01.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 19,717 hrs · 16,522 cycles

R1 DOOR ASSIST BOTTLE BELOW LIMITS. SERVICED THE ASSIST BOTTLE IAW AMM 5212-51.

Part: KNOB — LOOSE (EXIT SIGN) · airframe 18,946 hrs · 15,828 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT KNOB ON PAX SIGNS PANEL IS LOOSE. SECURED LOOSE EMER LIGHT KNOB SET SCREW & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: LENS — SATURATED (EXTERIOR LIGHT) · airframe 18,889 hrs · 15,768 cycles

AIRCRAFT WAS NOT GNDED. LT AFT EXTERIOR EMER LIGHT LENS SHOWS WATER. DRAINED WATER FROM AFT LT EMER LIGHT, RESEALED LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-25.

Part: CABLE — DEFECTIVE (L2 DOOR) · airframe 18,833 hrs · 15,712 cycles

AIRCRAFT IN BASE MX. WHEN REPLACING THE EMER EVACUATION SLIDE MECHANISM FLEX CABLE ON THE L2 DOOR, MX FOUND THE LOWER LOCK NUT FROZEN TO CABLE SHAFT ON THE REPLACEMENT FLEX CABLE. THE DEFECTIVE FLEX CABLE WAS RETURNED TO STORES AS BAD FROM STOCK & A SERVICEABLE FLEX CABLE WAS INSTALLED IN ITS PLACE.

Part: LIGHT — CRACKED (CABIN) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, EMER LIGHT HAS A CRACK AT LOWER RT SIDE, BELOW INBD FLAP. REPLACED & PERFORMED OPERATIONS CHECK ON AFT EMER LIGHT AT LOWER RT SIDE, BELOW INBD FLAP IAW AMM 33-50-25.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, MAIN CABIN PHOTO LUMINESCENT STRIPS HAVE MORE THAN 10% DAMAGED. REPLACED PHOTO LUMINESCENT STRIPS AT MAIN CABIN IAW AMM 33-50-21-400-801-A.

Part: LENS — CRACKED (EXIT SIGN) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, ON THE R2 DOOR THE LOWER EMER LIGHT EXIT SIGN LENS IS CRACKED. REPLACED EMER EXIT IDENTIFIER SIGN LIGHT IN IAW AMM 33-50-15-000-801-A & 33-50-15-400-801-A. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00-710-801-A.

Part: LENS — CRACKED (EXTERIOR) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, LT WING TO FUSELAGE PANEL 1932AL HAS A CRACKED LIGHT LENS, OFF ACFT PART. REPLACED EXTERNAL EMER LIGHT ASSEMBLY ON LT WING IAW AMM 33-50-25-400-802-A. PERFORMED OPERATIONS CHECK IAW AMM 33-50-25-710-801-A.

Part: LENS — CRACKED (EXIT SIGN) · airframe 15,824 hrs · 13,123 cycles

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

Part: SIGN — CRACKED (CABIN) · airframe 15,824 hrs · 13,123 cycles

R1 LOWER EMER EXIT SIGN IS CRACKED. REPLACED EMER EXIT SIGN, LOWER, AT R1 DOOR IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: PANEL — CORRODED (FUSELAGE) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 87 TO 88, Z=-490MM & BETWEEN Y=+275 TO Y=+833. REPLACED SHEAR PANEL IAW SRM 53-23-10, 51-23-05 & 51-42-01.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, CRACK IN VERTICAL STABILIZER RIB AT RIB 9 & 10 TE BETWEEN FRAME 98 TO 99, ZV=4353.20MM & Y=0. ACCOMPLISHED REPLACEMENT OF RIB 9 AT VERTICAL STABILIZER REAR SPAR IAW SRM PART II 51-41-01 PARA 6 & 51-41-02 PARA 6.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 15,824 hrs · 13,123 cycles

AFTER OPENING L2 PAX DOOR, EMER SLIDE FELL OUT OF ITS SOFT COVER ONTO THE DOOR STAND. REPLACED L2 PAX DOOR EMER SLIDE IAW AMM 25-65-01-020-002-A.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 Z=-490MM & Y=+609MM. REPLACED GUSSET IAW SRM 51-40-02 & 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 86 TO 87, Z=-275MM & Y=+275MM. REPLACED SHEAR PANEL IAW SRM 51-40-02 PAGE 1 TO 4 & SRM 51-42-01.

Part: SKIN — BULGED (FUSELAGE) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK 2 EACH INCOMING, EXISTING, REPAIRS ON FUSELAGE SKIN ARE BULGING BETWEEN FRAME 6 TO 7 & STRINGER 20R TO 21R. REMOVED 2 EACH INCOMING, EXISTING, REPAIR DOUBLERS ON FUSELAGE SKIN. INSPECTED & REPAIRED FUSELAGE SKIN IAW SRM 51-41-01, 51-41-02. ACCOMPLISHED REPAIR IAW EA 506715. WORKED IN CONJUNCTION WITH SDR 2015011200017.

Part: SKIN — BULGED (FUSELAGE) · airframe 15,824 hrs · 13,123 cycles

C3 CHECK 2 EACH INCOMING, EXISTING, REPAIRS ON FUSELAGE SKIN ARE BULGING BETWEEN FRAME 6 TO 7 & STRINGER 20R TO 21R. REMOVED 2 EACH INCOMING, EXISTING, REPAIR DOUBLERS ON FUSELAGE SKIN. INSPECTED & REPAIRED FUSELAGE SKIN IAW SRM 51-41-01, 51-41-02 & ACCOMPLISHED REPAIR IAW EA 506715. WORKED IN CONJUNCTION WITH SDR 201501130001.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,847 hrs · 12,259 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 14,847 hrs · 12,259 cycles

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

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 14,064 hrs · 11,619 cycles

FLT 2033, PHL-BOS. WHILE PREPARING TO LAND THE CREW NOTED THAT THE LE DEVICES DID NOT MOVE FROM THEIR POSITION AS COMMANDED IN PREPARATION FOR THE APPROACH. THE CREW EXECUTED A GO AROUND ABOVE 1500 FEET & WERE ABLE TO CLEAR THE DISAGREEMENT. THE FLIGHT LANDED UNEVENTFULLY & TAXIED TO THE GATE. R & R THE SLAT FLAP CONTROL LEVER.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (L1 DOOR) · airframe 13,443 hrs · 11,169 cycles

L1 DOOR WILL NOT CLOSE OR LATCH. MAINTENANCE REPLACED FWD PASS ENTRANCE DOOR DIAPHRAGM AND SERVICED PNEUMATIC ASSEMBLY. OPENED AND CLOSED DOOR, OPS CHECKED NORMAL.

Part: ROD — BROKEN (L2 DOOR) · airframe 13,233 hrs · 11,037 cycles

CREW REPORTS L2 DOOR HARD TO OPEN AND CLOSE. MAINTENANCE FOUND BROKEN FORWARD AND AFT COUNTERBALANCE RODS ON BELLCRANK, R & R.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 12,678 hrs · 10,629 cycles

CEILING EXIT SIGN AT EMERGENCY EXIT ROW ACFT FWD IS MISSING. MX REINSTALLED EXIT SIGN AT EMERGENCY ROW, CHECKS OK.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,665 hrs · 10,624 cycles

FRONT LENS COVER ON MID-CABIN CEILING EMERGENCY EXIT LIGHT IS MISSING. SECURED LENS, OK FOR SERVICE.

Part: RAMP — LACK OF LUBE (L1 DOOR) · airframe 12,499 hrs · 10,503 cycles

L1 DOOR (MAIN ENTRY DOOR) DIFFICULT TO OPEN BY AGENT. MX LUBED FWD (L1) DOOR COMMAND RAMPS. OPS CHECKS OK.

Part: ROLLER — DIRTY (L1 DOOR) · airframe 12,399 hrs · 10,409 cycles

AT GATE ARRIVAL AGENT HAD DIFFICULTY OPENING 1L DOOR. MX CLEANED & LUBED DOOR ROLLERS. OK FOR SERVICE.

Part: PNEUMATIC SYSTEM — LOW (PAX DOOR) · airframe 11,363 hrs · 9,627 cycles

AFT PASSENGER DOOR PNEUMATIC ASSEMBLY NEEDS SERVICING. MAINTENANCE SERVICED THE AFT PASSENGER DOOR PNEUMATIC ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (ENTRY DOOR) · airframe 10,852 hrs · 9,263 cycles

LEFT AFT ENTRY DOOR PNEUMATIC BOTTLE LOW. MAINTENANCE SERVICED DOOR BOTTLE.

Part: MECHANISM — OUT OF SEQUENCE (L2 DOOR) · airframe 10,756 hrs · 9,178 cycles

L2 GALLEY DOOR WILL NOT OPEN FROM OUTSIDE. MAINTENANCE RE-CONFIGURED DOOR TO PROPER SEQUENCE, DOOR OPENS AND CLOSES NORMAL.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - LEVEL 2 SURFACE CORROSION ON LEFT FLOOR PANEL ATTACH FITTING AT FR17, Z-490, Y745. REPLACED LEFT FLOOR PANEL ATTACH FITTING AT FR17, Z-490, Y745 IAW EA 203158.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOOR SUPPORT ATTACH FITTING CORRODED AT FR 18, Y -745, Z -490. REMOVED AND REPLACED FITTING IAW E190 SRM 53-21-10 AND SRM 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM SHEAR PANEL CORRODED BETWEEN FR 87 AND FR 88 AT Z -490. REMOVED AND REPLACED SHEAR PANEL IAW TR 190-5300-11-0563A.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM GUSSET CORRODED AT FR 90, Y -95, Z -490. REMOVED AND REPLACED GUSSET IAW E190 SRM 51-41-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM SHEAR PANEL CORRODED BETWEEN FR 87 AND FR 88 FROM Y +273 TO Y -273 AT Z -490. REMOVED AND REPLACED SHEAR PANEL IAW TR 190-5300-11-0563 AND E190 SRM 51-40-00 & SRM 51-40-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM GUSSET CORRODED AT FR 89, Y 252, Z -490. REMOVED AND REPLACED GUSSET IAW TR190-5300-11-0563 AND E190 SRM 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOOR STRUCTURE UPPER SHEET CORRODED BETWEEN FR 85 AND FR 86 AT Y -273, Z -490. REMOVED AND REPLACED UPPER SHEET IAW TR190-5300-11-0563 AND E190 SRM 51-40-06 & 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM SHEAR PANEL CORRODED BETWEEN FR 87 AND FR 88 AT Y -273, Z -490. REMOVED AND REPLACED SHEAR PANEL IAW TR 190-5300-11-0563 AND E190 SRM 51-40-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM GUSSET CORRODED AT FR 90, Y 273, Z -490. REMOVED AND REPLACED GUSSET IAW E190 SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM UPPER SHEET CORRODED BETWEEN FR 85 AND FR 86 AT Y 273, Z -490. REMOVED AND REPLACED UPPER SHEET IAW TR 190-5300-11-0563 AND E190 SRM 51-41-01 & SRM 51-43-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR84 TO FR85, Z-490, -Y273. REPAIRED SEAT TRACK BETWEEN FR84 TO FR85, Z-490, -Y273 IAW EA 203083.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM GUSSET CORRODED AT FR 90, Y -507, Z -490. REMOVED AND REPLACED GUSSET IAW E190 SRM 51-41-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM GUSSET CORRODED AT FR 90, Y -273, Z -490. REMOVED AND REPLACED GUSSET IAW E190 SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 87 AND FR 89 AT Y -273, Z -490. REMOVED AND REPLACED FLOORBEAM IAW TR190-5300-11-0563 AND E190 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 86 AND FR 88 AT Y +273, Z -490. REMOVED AND REPLACED FLOORBEAM IAW TR 190-5300-11-0563 AND E190 SRM CHAPTER 51 STANDARD PRACTICES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR84 TO FR85, Z-490, Y273. REPAIRED SEAT TRACK BETWEEN FR84 TO FR85, Z-490, Y273 IAW EA 203084.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 12 AND FR 20.5 AT Y 273, Z -490. REMOVED AND REPLACED FLOORBEAM IAW TR 190-5300-11-0563A AND E190 SRM 51-40-004.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM CORRODED BETWEEN FR 12 AND FR 20.5 AT Y -273, Z -490. REMOVED AND REPLACED BEAM IAW TR 190-5300-11-0563A AND E190 SRM 51-43-013.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOOR SILL CORRODED BETWEEN FR 12 AND FR 14 FROM Y1060 TO Y1380 AT Z -490. REMOVED AND REPLACED SILL IAW E190 SRM 51-43-02 AND 51-41-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,388 hrs · 8,882 cycles

C2 CHECK - MAIN CABIN FLOORBEAM SILL PLATE CORRODED BETWEEN FR 12 AND FR 16 FROM Y-1205 TO Y -1380 AT Z -490. REMOVED AND REPLACED SILL PLATE IAW E190 SRM 51-41-02 AND 51-43-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,430 hrs · 8,915 cycles

BOS - EMERGENCY LIGHT ABOVE R1 DOOR INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 9,401 hrs · 7,991 cycles

LGA - EMERGENCY LIGHT RED EXIT SIGN DOOR 2L INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: MECHANISM — OUT OF ADJUST (DOOR)

PHL - LEFT AFT EXIT DOOR WILL NOT CLOSE PROPERLY. ADJUSTED LEFT AFT DOOR AFT HOISTING MECHANISM. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 8,745 hrs · 7,485 cycles

BOS - RIGHT AFT CABIN F/A EMERGENCY FLASHLIGHT BATTERY DEAD. MAINTENANCE REPLACED FLASHLIGHT BATTERY PACK IAW AMM 25-60.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 8,509 hrs · 7,303 cycles

BOS - L1 PASSENGER ENTRY DOOR AND R1 SERVICE DOOR REQUIRE SERVICING. MAINTENANCE SERVICED L1 PASSENGER DOOR PER AMM 52-11-51-03 AND SERVICED R1 SERVICE DOOR PER 52-41-51-03.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 8,509 hrs · 7,303 cycles

BOS - L1 PASSENGER ENTRY DOOR AND R1 SERVICE DOOR REQUIRE SERVICING. MAINTENANCE SERVICED L1 PASSENGER DOOR PER AMM 52-11-51-03 AND SERVICED R1 SERVICE DOOR PER 52-41-51-03.

Part: ACM — CONTAMINATED (AC BAY)

FLIGHT 2119, BOS-LGA - THE FLIGHT ATTENDANTS ADVISED THE CAPTAIN OF A STRONG FUEL (KEROSENE) ODOR THROUGHOUT THE CABIN PASSING THROUGH 10,000FT. THE PASSENGERS AND FLIGHT ATTENDANTS REPORTED A FUEL VAPOR IN THE AIR. MAINTENANCE FOUND THE RIGHT ACM AND HEAT EXCHANGERS CONTAMINATED WITH COFFEE GRINDS. THE ODOR IN THE PACK CONSISTANT WITH THE CABIN ODOR. THE RIGHT AIR CYCLE MACHINE AND THE RIGHT HEAT EXCHANGER WERE REMOVED AND REPLACED. SATISFACTORY OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED.

Part: HEAT EXCHANGER — CONTAMINATED (AC BAY)

FLIGHT 2119, BOS-LGA - THE FLIGHT ATTENDANTS ADVISED THE CAPTAIN OF A STRONG FUEL (KEROSENE) ODOR THROUGHOUT THE CABIN PASSING THROUGH 10,000FT. THE PASSENGERS AND FLIGHT ATTENDANTS REPORTED A FUEL VAPOR IN THE AIR. MAINTENANCE FOUND THE RIGHT ACM AND HEAT EXCHANGERS CONTAMINATED WITH COFFEE GRINDS. THE ODOR IN THE PACK CONSISTANT WITH THE CABIN ODOR. THE RIGHT AIR CYCLE MACHINE AND THE RIGHT HEAT EXCHANGER WERE REMOVED AND REPLACED. SATISFACTORY OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

BOS - THE L2 PASSENGER DOOR ASSIST BOTTLE IS BELOW LIMITS. MAINTENANCE SERVICED THE L2 DOOR ASSIST BOTTLE PER 52-41-51.

Part: BATTERY — DISCHARGED (CABIN)

BOS - THE AFT LEFT EMERGENCY EXIT MARKER NOT ILLUMINATED DURING TEST. MAINTENANCE REMOVED AND REPLACED NR 5 BATTERY POWER UNIT. PERFORMED A SATISFACTORY OPERATIONAL TEST.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DCA - EMERGENCY LIGHT AT 7TH CEILING PANEL FROM FRONT OF AIRCRAFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DCA - CEILING EMERGENCY LIGHT NEAR CLASS DIVIDER INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (ENTRY DOOR)

ATL - THE AFT LEFT ENTRY DOOR PNEUMATIC ASSEMBLY CHARGE IS LOW. MAINTENANCE SERVICED THE PNEUMATIC ASSEMBLY AT THE AFT LEFT ENTRY DOOR.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (PAX DOOR)

ATL - THE FORWARD PASSENGER ENTRY DOOR PNEUMATIC ASSEMBLY CHARGE IS LOW. MAINTENANCE SERVICED THE PNEUMATIC ASSEMBLY AT THE FORWARD PASSENGER ENTRY DOOR.

Part: DOOR — LACK OF LUBE

BOS - THE LEFT REAR DOOR DIFFICULT TO OPEN BY THE CATERER AND FLIGHT ATTENDANT. THE MISALIGNMENT OF THE DOOR CAUSED PAINT TO BE REMOVED FROM THE FRAME OF AIRCRAFT DOORWAY IN TWO PLACES. MAINTENANCE OPERATED THE DOOR NUMEROUS TIMES, ALIGNMENT IS SATISFACTORY. LUBED THE DOOR GUIDES AND OPERATIONAL CHECKED.

Part: MOUNT FITTING — CRACKED (CARGO BAY) · airframe 5,288 hrs · 4,296 cycles

PHL - MAJOR REPAIR - CRACK AT BASE OF AFT CARGO DOOR FITTING AFT MOUNT HOLES. REPLACED AFT CARGO DOOR AFT MOUNT FITTING IAW E190 AMM 53-23-29.

Part: ENGINE — BIRD INGESTION (NR 1)

FLIGHT 1467, PIT-PHL - FOLLOWING TAKEOFF AT APPROXIMATELY 1500 FEET, AIRCRAFT INGESTED A BIRD INTO THE NR 1 ENGINE. THE COCKPIT INDICATIONS SHOWED ENGINE VIBRATION AFTER THE BIRD STRIKE. THE CREW PULLED THE NR 1 ENGINE TO IDLE, DECLARED AN EMERGENCY, AND RETURNED TO PIT. THE FLIGHT MADE A NORMAL APPROACH AND LANDING, AND THERE WERE NO FURTHER INCIDENTS REPORTED. MAINTENANCE ACCOMPLISHED A BIRD STRIKE INSPECTION PER JPC 43L00005001 AND FOUND THE NR 1 ENGINE DAMAGED BEYOND LIMITS. THE NR 1 ENGINE WAS REPLACED PER JPC43L40071001. THE AIRCRAFT IS SATISFACTORY FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (L1 DOOR)

PHL - DURING OPERATIONAL CHECK OF ESCAPE SLIDE L1 DOOR THE SLIDE FAILED TO OPERATE PROPERLY. THE DOOR ASSIST FAILED TO OPEN L1 DOOR FOR SLIDE DEPLOYMENT. MAINTENANCE REPLACED THE L1 DOOR PNEUMATIC ACTUATOR ASSEMBLY.

Part: LOCK — DEFECTIVE (PAX DOOR)

FLIGHT 1701, ATL-CLT - AFTER TAKEOFF WHEN CLIMBING TO 10,000 FEET THE CREW RECEIVED AN EICAS INDICATION SHOWING THE FORWARD PASSENGER DOOR WAS NOT LOCKED. THE CAPTAIN COMPLIED WITH HIS QRH WHICH DIRECTED HIM TO LAND AT THE NEAREST AIRPORT. HE DECLARED AND EMERGENCY AND RETURNED TO ATL. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE VISUAL INDICATOR LOCK ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

ATL - L2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED AS REQUIRED.

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR)

CLT - THE LEFT AFT ENTRY DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED THE LEFT ENTRY DOOR ASSIST BOTTLE.

Part: MODULE — INOPERATIVE

FLIGHT 1092 - PHL-RDU: CREW RECEIVED EICAS MESSAGE "AVNX MAU 3 FAIL". THE AIRCRAFT RETURNED TO PHL PER THE QRH PROCEDURE. MAINTENANCE REMOVED AND REPLACED THE NIC/PROC MODULE FIVE.