N956UW

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 23,173 hrs · 19,153 cycles

R2 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE R2 DOOR ASSIST BOTTLE IAW AMM 52-42-51. OK FOR SERVICE.

Part: DOOR — OUT OF SEQUENCE (MAIN CABIN) · airframe 22,030 hrs · 18,170 cycles

MAIN CABIN DOOR WILL NOT CLOSE AND LOCK. FOUND DOOR OUT OF SEQUENCE. BALANCED MECHANISM IAW 52-10-00. OPS NORMAL. OK FOR SERVICE.

Part: DOUBLER — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. WASTE DOOR CUTOUT INNER DOUBLER HAS EXFOLIATED CORROSION IN SEVERAL SPOTS. REPLACED WASTE DOOR CUTOUT DOUBLER PER DWG 170-65180-445.

Part: RAIL — WORN (FLAP TRACK) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. THICKNESS REDUCTION ON RIGHT WING FLAP TRACK 2A RAIL INBOARD SIDE AT RIB 8. REPLACED RAIL PER AMM 57-54-25-400-801B.

Part: RAIL — WORN (FLAP TRACK) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. THICKNESS REDUCTION ON RIGHT WING FLAP TRACK 2A RAIL OUTBOARD SIDE AT RIB 9A. REPLACED OUTBOARD RAIL PER AMM 57-54-25-400-801B.

Part: FLAP — CHAFED (LT WING) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT WING INBOARD FLAP LOWER INBOARD TRAILING EDGE IS CHAFED. REPAIRED PER EA 275297.

Part: WINDSHIELD — DELAMINATED (COCKPIT)

AIRCRAFT IN BASE MAINTENANCE. FIRST OFFICERS WINDSHIELD IS DELAMINATED AT UPPER LEFT CORNER. PROCURED WINDSHIELD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION (WITH GOUGE) ON FORWARD MAIN CABIN RIGHT HAND SEAT TRACK BEAM AT Y230 AND FR 23. REPLACED SEAT TRACK PER DWG 170-67660-431 AND 170-67120-433.

Part: HINGE FITTING — WORN (RT WING) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 2 PER AMM 57-61-00-000-81.

Part: HINGE FITTING — WORN (RT WING) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 1 PER AMM 57-61-00-000-801.

Part: HINGE FITTING — WORN (RT WING) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 4. PER AMM 57-61-00-000-801.

Part: HINGE FITTING — WORN (RT WING) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 3 PER AMM 57-61-00-000-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR12 AND FR20. REPLACED SEAT TRACK PER 53-00-00-3 REPAIR 3.

Part: SUPPORT — CRACKED (FRAME 12) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND CRACK IN COCKPIT FLOOR STRUCTURE ANGLE BRACKET AT FR12 BL0 #30-076. REPLACED ANGLE BRACKET PER SRM 51-44-01 AND DWG 171-00237-403.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y1100, BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT HAND LATERAL SEAT TRACK HAS CORROSION BETWEEN FR 51 AND FR 56. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 12-23) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN LEFT SEAT TRACK BETWEEN FRAMES 12 AND 23. REPLACED THE SEAT TRACK IAW 53-00-00-3, REP 3, AND DWG 170-67120-469.

Part: SEAT TRACK — CORRODED (FRAMES 19-20) · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE RIGHT LATERAL SEAT TRACK BETWEEN FRAMES 19 AND 20. REPLACED IAW 51-41-01, AND 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y330 BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y380, BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-43-03, AND DRAWING 190-05555-805.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT MAIN CABIN LEFT HAND SEAT TRACK HAS CORROSION AT FR 84, Y-270. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND IN AFT MAIN CABIN RIGHT HAND SEAT TRACK BETWEEN FR 84 AND 85, Y254. REPLACED SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT AT FRAME 16, -Y1220. REPLACED THE FLOOR SUPPORT 53-00-00-3, REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND INBOARD SEAT TRACK BETWEEN FR 34 AND FR 42. REPLACED SEAT TRACK PER DRAWING 190-23017-407.

Part: FLAP TRACK — WORN (LT WING TE FLAP) · airframe 21,405 hrs · 17,674 cycles

WEAR ON THE LEFT WING FLAP TRACK NR 1A. REPLACED THE FLAP TRACK IAW AMM 57-54-25-000-801-B.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 21,405 hrs · 17,674 cycles

CRACKED REAR SPAR BRACKET ON VERTICAL STABILIZER, BETWEEN RIBS 9 AND 10. REPLACED THE BRACKET IAW DRAWING 170-63200-451.

Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON FLOOR PANEL SUPPORT BETWEEN FR90 AND FR89. Y838, IN THE AFT MAIN CABIN ON THE RIGHT HAND SIDE. REPLACE FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (FRAME 12) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN FLOORBEAM ANGLE AT FRAME 12, Y260. REPLACED FLOORBEAM ANGLE IAW DRAWING 170-00810-405.

Part: DOUBLER — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN LEFT FLOOR DOUBLER BETWEEN FRAMES 13 AND 16, BETWEEN Y=-3 AND 09 AND Y=-400E190. REPAIRED IAW 53-00-00-3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT BETWEEN FRAMES 12 AND 13, -Y500. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-413.

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT FRAME 14, Y=+710. REPAIRED IAW SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN LEFT FLOOR SUPPORT AT -Y1140 AND FRAME 16. REPLACED THE FLOOR SUPPORT IAW DWG 170-00816-415.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR DOUBLER AT -Y660 AND FR 19. REPLACED FLOOR DOUBLER 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT AT -Y838, BETWEEN FRAMES 88 AND 90. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-457.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON THE CENTER FLOOR SPLICE IN THE AFT MAIN CABIN. REPLACED FLOOR SPLICE PER E-190 170-65660-447 AT DWG.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND ON THE AFT MAIN CABIN RIGHT GUSSET PLATE AT Y584.2, FRAME 90. REPLACED THE GUSSET PLATE IAW DRAWING 170-6001-825, AND SRM 51-41-02.

Part: WINDOW — SCRATCHED (LEFT) · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT HAND WINDOW 1 IS HAZY AND SCRATCHED. REPLACED WINDOW AND SEAL PER AMM 56-20-00.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR STRUCTURE RIGHT FLOOR SUPPORT AT Y955.2, BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 83-84) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORRODED LEFT FLOOR SUPPORT BETWEEN FRAMES 83 AND 84. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-65600-443, AND SRM 51-41-01.

Part: REINFORCEMENT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORRODED RIGHT REINFORCEMENT STRUCTURE AT FRAME 84. REPLACED THE REINFORCEMENT IAW DWG 190-65140-801.

Part: FLOORBEAM — CRACKED (FRAME 86) · airframe 21,405 hrs · 17,674 cycles

CRACK IN AFT MAIN CABIN FLOORBEAM ANGLE Y685.8 AT FRAME 86. REPLACED THE FLOORBEAM ANGLE IAW DRAWING 170-65660-447, AND SRM 51-41-01.

Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON LEFT HAND FLOOR SPLICE ON THE AFT MAIN CABIN BETWEEN FR87 AND FR88, Y-1100. REPLACED FLOOR SPLICE PER AARD 53-00-00-3 AND 5EA 51-42-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION ON THE AFT MAIN CABIN RIGHT SHEAR PANEL BETWEEN FRAMES 87 AND 88, Y584.42 AND Y914.4. REPLACED THE SHEAR PANEL IAW 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 21,405 hrs · 17,674 cycles

CORROSION FOUND THE ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT AT FRAME 19, Y-1140. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-03 AND 51-40-03.

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 21,287 hrs · 17,582 cycles

RIGHT EMERGENCY EXIT DOOR, VIBRATES AND MAKES A LOUD NOISE DURING TAKE-OFF. REMOVED THE RIGHT EMERGENCY EXIT DOOR, CLEANED THE SEAL AREA AND REINSTALLED EXIT DOOR. PRESSURIZED AIRCRAFT, NO LEAKS NOTED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 21,255 hrs · 17,560 cycles

FLASHLIGHT AT THE FLIGHT ATTENDANT RT AFT STATION, LED DOES NOT FLASH. REPLACED FLASHLIGHT, OPS CHECKED NORMAL.

Part: PIN — DAMAGED (R1 DOOR) · airframe 20,512 hrs · 17,028 cycles

AIRCRAFT WAS NOT GROUNDED. R1 FWD SVC DOOR EMERGENCY EVACUATION SLIDE PACKBOARD AFT ISOLATOR DAMAGE. REPLACED R1 FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE PACKBOARD AFT ISOLATOR PIN J23676-1.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,134 hrs · 16,724 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION HAS BEEN INSTALLED INCORRECTLY AND ONE CANNOT SEE THE STATUS LIGHT INDICATION. REPLACED FLASHLIGHT BATTERY.

Part: DOOR — LACK OF LUBE (R1) · airframe 19,524 hrs · 16,235 cycles

FORWARD R1 DOOR UNABLE TO BE ARMED OR VENT FLAP CLOSED. MAINTENANCE LUBRICATED THE DOOR IAW AMM 52-11-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: POWER UNIT — FAULTY (CABIN) · airframe 19,511 hrs · 16,228 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS OVER CABIN WING EXIT ILLUMINATED AFTER POWER DOWN. REPLACED BATTERY POWER UNIT PER AMM 33-50-01.

Part: DOOR SEAL — OUT OF POSITION (CARGO DOOR) · airframe 19,075 hrs · 15,881 cycles

AIRCRAFT WAS NOT GROUNDED. AIRCRAFT WILL NOT MAINTAIN PROPER PRESSURIZATION AT FT 380 CABIN 9600FT AND CLIMBING,150FT MIN AT 340 CABIN ALTITUDE 8500FT FLUCTUATING + -150 FT PER MIN. FLIGHT ATTENDANT STATES RIGHT CABIN DOOR MAKING NOISE. MAINTENANCE FOUND DEBRIS AND REMOVED DEBRIS FROM R2 DOOR JAM AREA. THEN FOUND THE FORWARD CARGO DOOR SEAL OUT OF THE RETAINER AND REINSTALLED IT. MAINTENANCE PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, STEP 1B FAILS ON ROUTINE CARD 43C20033004. NOT ALL EMER LIGHTS STAY ON FOR 15 MINUTES. CHARGED BATTERY & ACCOMPLISHED FUNCTIONAL CHECK STEP 1B WITH NO DEFECTS BEING NOTED.

Part: SIGN — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT L2 DOOR, THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15 & 33-50-00.

Part: SIGN — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT R2 DOOR, THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15 & 33-50-00.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, MAIN CABIN LT PHOTO LUMINESCENT STRIPS MISSING PIECES & CRACKS, DAMAGED, MORE THAN 10%. REPLACED MAIN CABIN LT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR CUT OUT LOWER BEAM. REPLACED BEAM IAW SRM 51-40-01.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, MAIN CABIN RT PHOTO LUMINESCENT STRIPS MISSING PIECES & CRACKS, DAMAGED MORE THAN 10%. REPLACED MAIN CABIN RT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: SIGN — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT LT OVERWING DOOR THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 53-50-00 & 53-50-15.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT L1 DOOR, THE UPPER EMER EXIT SIGN LENS IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-17.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT R1 DOOR THE UPPER EMER EXIT SIGN LENS IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-17.

Part: SIGN — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT R1 DOOR THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00 & 33-50-15.

Part: SIGN — CRACKED (CABIN) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, AT RIGHT OVERWING DOOR THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00 & 33-50-15.

Part: HINGE FITTING — CORRODED (RT AILERON) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON RT WING AILERON NR 3 HINGE FITTING. REPAIRED HINGE FITTING IAW EA 256079.

Part: HINGE FITTING — CORRODED (RT AILERON) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON RT WING AILERON NR 4 HINGE FITTING. REPAIRED HINGE FITTING IAW EA 256079.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CABIN FLOOR SUPPORT CRACKED ON RADIUS AT FRAME 45 & RBL 10. REPAIRED IAW EA 255839.

Part: LENS — DEFECTIVE (EXTERIOR) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, EXTERNAL EMER LIGHT LENS ON WING TO FUSE FAIRING ACCESS PNL 199EL IS FOGGY. REPLACED EXTERNAL EMER LIGHT LENS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-25-400-802-A.

Part: ROLLER — STUCK (EMERGENCY EXIT) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, RT OVERWING HATCH FRAME, UPPER ROLLER IS STUCK. REPLACED ROLLER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 20-10-08 & 52-21-00-820-801-A.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON COCKPIT FLOOR STRUCTURE DOUBLER, BETWEEN FRAME 8 & 11 AT LBL 15. REPAIRED DOUBLER IAW EA 255873.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON COCKPIT FLOOR STRUCTURE DOUBLER, BETWEEN FRAME 10 & 12, RBL 12 - 35. REPAIRED DOUBLER IAW EA 255882A.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON COCKPIT FLOOR STRUCTURE, CTR DOUBLER AT FRAME 10, BETWEEN LBL 9 & RBL 9. REPAIRED IAW EA 255876A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON FLOOR PANEL SUPPORT, BETWEEN FRAME 88 & 90 AT RBL 44. REPLACED FLOOR PANEL SUPPORT IAW DWG 170-66000-445, SRM 51-41-02 & 51-42-01.

Part: ROLLER — STUCK (EMERGENCY EXIT) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, LT OVERWING HATCH FRAME, FWD ROLLER IS STUCK. REPLACED ROLLER IAW AMM 20-10-08.

Part: ROLLER — STUCK (EMERGENCY EXIT) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, LT OVERWING HATCH FRAME, UPPER AFT ROLLER STUCK. REPLACED ROLLER IAW AMM 20-10-18.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON SHEAR PANEL, BETWEEN FRAME 84 & 85 AT RBL 48. REPLACED SHEAR PANEL IAW DWG 190-65293-001 & SRM 51-42-04. .

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON RT OVERWING EXIT DOOR CUT OUT STRUCTURE STRIKER PLATE AT FRAME 49 & STRINGER 13R. REPLACED STRIKER PLATE IAW DWG 190-20905-001 & SRM 51-41-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, COCKPIT FLOOR STRUCTURE, ANGLE CLIP CRACKED AT FRAME 12 & LBL 37. REPLACED CLIP IAW SRM 51-40-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON AFT ENTRY FLOOR PANEL SUPPORT AT FRAME 87 & RBL 30. REPLACED SUPPORT IAW SRM 51-41-01.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR, CUT OUT LOWER AFT CORNER SEAL REST. REPLACED SEAL REST IAW AARD 53-00-00-3 REPAIR 3.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR CUT OUT LOWER FWD CORNER SEAL REST AT FRAME 24 & STRINGER 26R. REPLACED SEAL REST IAW AARD 53-00-00-3 REPAIR 3.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR, CUT OUT LOWER CTR SEAL REST, BETWEEN FRAME 25 & 26 AT STRINGER 25R. REPLACED SEAL REST IAW SRM 51-41-01 & AARD 53-00-00-3 REPAIR 3.

Part: MOUNT FITTING — CORRODED (LT AILERON) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON LT AILERON NR 2 MOUNT FITTING BEARING. REPLACED LT AILERON NR 2 MOUNT FITTING IAW AMM 57-61-01-400-801-A.

Part: HINGE FITTING — CORRODED (LT AILERON) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, LT AILERON INBD NR 1 MOUNT FITTING HAS A RUSTED BEARING. REPLACED LT AILERON INBD NR 1 MOUNT FITTING IAW AMM 57-61-01-400-801-A.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON RT SHEAR PANEL, BETWEEN FRAME 87 & 88, +Y304 & +Y1140. REPLACED SHEAR PANEL IAW AARD 53-00-00-3 REPAIR 3 & SRM 51-42-01 & 51-43-03.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 17,112 hrs · 14,129 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 & RBL 30. REPLACED GUSSET IAW DWG 170-65660-447 & SRM 51-41-02.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON SPLICE AT FRAME 90 & BL 0. REPLACED SPLICE IAW DWG 170-65660-447 & SRM 51-40-02 03.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,115 hrs · 14,131 cycles

C3 CHECK, CORROSION ON CTR SHEAR PANEL, BETWEEN FRAME 87 & 88, -Y222 & +Y222. REPLACED SHEAR PANEL IAW AARD 53-00-00-3 REPAIR 3 & SRM 51-42-01 & 51-43-03.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,002 hrs · 14,032 cycles

PILOTS WINDSCREEN CRACKED & DELAMINATION AROUND EDGE OF WINDSCREEN, SOME DELAMINATION OVER 1 INCH WIDE & OVER 12 INCHES LONG. DAMAGE IS ALL AROUND WINDSCREEN EDGES ALONG WITH CRACKS. REPLACED WINDSCREEN IAW AMM 56-11-00.

Part: CONTROL MODULE — FAULTY (BRAKE SYSTEM) · airframe 16,483 hrs · 13,623 cycles

FLIGHT 549 EN-ROUTE, AFTER GEAR DOWN, EICAS STATUS MSGS, BRAKE LT FAULT & BRAKE RT FAULT. RAN NORMAL CHECK LIST, DECLARED EMER, 2ND APPROACH GEAR DOWN, MSGS DISAPPEARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. R & R MAIN BRAKE CONTROL MODULE INBD MAU2 SBT NR 16 IAW MM PROCEDURE & REF 32-41-07. OPERATIONS CHECKED NORMAL.

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 16,434 hrs · 13,584 cycles

FLIGHT 1776 EN-ROUTE, GEAR WILL NOT RETRACT, NO EICAS MSGS. GEAR HANDLE WOULD NOT MOVE. THE FLIGHT RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. VERIFIED PROBLEM DURING GEAR RETRACTION TEST AMM 32-33-00. R & R LG SELECT HANDLE AMM 32-33-01. GEAR RETRACTION TEST SATISFACTORY SEVERAL TIMES. ACCOMPLISHED INSPECTION.

Part: SIGN — BROKEN (CABIN) · airframe 16,056 hrs · 13,237 cycles

FORWARD LT EXIT IDENTIFICATION SIGN BROKEN. REPLACED THE FWD LT LIGHT EXIT IDENTIFICATION SIGN.

Part: LIGHT — LOOSE (CABIN) · airframe 15,972 hrs · 13,191 cycles

FLOOR MOUNTED EMERGENCY LIGHTING STRIP BY SEATS 1D & 1F PEELED UP. SECURED STRIP AS REQUIRED.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,790 hrs · 13,042 cycles

FLOOR PANEL 252DRF ADJACENT R2 DOOR SPONGY. R & R FLOOR PANEL 252DRF IAW MM 53-01-39 400.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 14,676 hrs · 12,162 cycles

FOREIGN SMELL IN COCKPIT & CABIN REPORTED. THE DECISION WAS MADE TO RETURN TO FIELD. THE PILOTS DONNED THE OXYGEN MASKS & DECLARED AN EMER. THE FLIGHT LANDED WITHOUT INCIDENT. NO CABIN ODOR FOUND AT EACH INDIVIDUAL PACK. NO 90 DAY HISTORY, OK FOR SERVICE.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,117 hrs · 11,637 cycles

LT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUTS LOOSE FOR BOTH ENGS, IN BOTH INBD & OTBD POSITIONS. RE-TORQUED PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUTS FOR BOTH ENGS, IN BOTH POSITIONS & APPLIED THE APPROPRIATE SAFETIES.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,117 hrs · 11,637 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 14,117 hrs · 11,637 cycles

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

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,117 hrs · 11,637 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: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 13,383 hrs · 11,016 cycles

FLIGHT 1703, BOS-PHL, THE FLIGHT HAD A SLAT FAIL INDICATION ON APPROACH IN PHL. THE CAPTAIN DECLARED AN EMERGENCY & THE FLIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED A RESET AT THE GATE.

Part: ACM — FAILED (RIGHT) · airframe 11,201 hrs · 9,455 cycles

FLIGHT 2135, AFTER TAKEOFF A STRONG SULFUR ODOR WENT THROUGH AIRCRAFT. AFTER ABOUT 10 MINUTES ODOR DISSIPATED. F/A REPORTED STRONG VIBRATION UNDER ROW 2. WHEN RECIRCULATION FAN TURNED OFF VIBRATION DID NOT GO AWAY. MAINTENANCE ISOLATED ODOR TO NR 2 A/C PACK. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE. OPS AND LEAK CHECKED OKAY.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,160 hrs · 9,406 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FR17 CROSSBEAM AT LBL 7. REPLACED CROSSBEAM AT FR17, LBL 7 IAW EMBRAER 190 SRM II 51-23-04/1, 05/1, 06/1.

Part: UPPER SHEET — CORRODED (FUSELAGE) · airframe 11,158 hrs · 9,405 cycles

C2 CHECK - CORROSION ON UPPER SHEET BETWEEN FR85 & FR86, RBL 10.748. REPLACED UPPER SHEET BETWEEN FR85 & FR86, RBL 10.748 IAW EMBRAER 190 SRM II 51-41-01, 51-43-03, 51-23-05 & 51-23-06.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,158 hrs · 9,405 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT FR16, LBL 48. REPLACED SILL PLATE AT FR16, LBL 48 IAW EMBRAER 190 SRM II 51-23-04, 51-23-05, 51-23-06, 51-41-01, 51-41-02 & 51-43-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR DOUBLER AT FR16 BETWEEN LBL 25 TO LBL 36. REPLACED FLOOR DOUBLER AT FR16 BETWEEN LBL 25 TO LBL 36 IAW EMBRAER 190 SRM II 51-23-04, 51-23-05, 51-23-06, 51-41-01, 51-41-02 & 51-43-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON REINFORCING PLATE AT FR84, RBL 12. REPLACED REINFORCING PLATE AT FR84, RBL 12 IAW EMBRAER 190 SRM II 51-41-02, 51-41-03, 51-23-04 & 51-23-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SEAT TRACK BETWEEN FR12 & FR18, RBL10.75. REPLACED SEAT TRACK BETWEEN FR12 & FR18, RBL 10.75 IAW EMBRAER 190 SRM II 51-40-02, 51-43-02, 51-43-01 & 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON SHEAR PANEL AT FR87, RBL 10.748. REPLACED SHEAR PANEL AT FR87, RBL 10.748 IAW EMBRAER 190 SRM II 51-42-01, 51-42-02, 51-10-03, 51-23-05 & 51-23-06.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON FORWARD CARGO COMPARTMENT FORWARD FINGER DOUBLER AT FR20, RBL 42. REPLACED DOUBLER AT FR20, RBL 42 IAW EMBRAER 190 SRM II 51-41-00, 51-43-04, 51-40-02/04.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CLIP AT FR16, RBL 28.25. REPLACED CLIP AT FR16, RBL28.25 IAW EMBRAER 190 SRM II 53-10-10, 51-41-00, 51-41-01, 51-23-05 & 51-23-06.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON GUSSET PLATE AT FR90, LBL 21. REPLACED GUSSET PLATE AT FR90, LBL 21 IAW EMBRAER 190 SRM II 51-41-02, 51-40-02 & 51-23-04.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CLIP AT FR18, LBL 29.5. REPLACED CLIP AT FR18, LBL 29.5 IAW EMBRAER 190 SRM II 51-40-02, 51-41-01, 51-23-04 & 51-23-05, 51-23-06, & 51-21-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON WASTE PAN DOUBLER BETWEEN FR88 TO FR89. REPLACED WASTE PAN DOUBLER BETWEEN FR88 TO FR89 IAW EMBRAER 190 SRM II 51-43-02, 51-23-06 & 51-23-05.

Part: UPPER SHEET — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON UPPER SHEET BETWEEN FR85 TO FR86, RBL10.748. REPLACED UPPER SHEET BETWEEN FR85 TO FR86, RBL 10.748 IAW EMBRAER 190 SRM II 51-43-03, 51-10-02, 51-40-02 & 51-43-0.

Part: PANEL — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON SHEAR PANEL AT FR87 BETWEEN RBL 21 TO RBL 22. REPLACED SHEAR PANEL AT FR87 BETWEEN RBL 21 TO RBL 22 IAW EMBRAER 190 SRM II 51-42-01, 51-42-02, 51-10-13 & 51-40-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR16 TO FR19, LBL 10.75. REPLACED SEAT TRACK BETWEEN FR16 TO FR19, LBL 10.75 IAW EMBRAER 190 SRM II 51-40-01, 51-41-02, 51-43-03 & 51-43-04.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON INTERCOSTAL BETWEEN FR88 TO FR89, RBL10.748. REPLACED INTERCOSTAL BETWEEN FR88 TO FR89, RBL10.748 IAW EMBRAER 190 SRM II 51-41-02, 51-40-02, 51-23-04 & 51-41-01.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FR12 TO FR14, RBL 38. REPLACED SILL PLATE BETWEEN FR12 TO FR14, RBL 38 IAW EMBRAER 190 SRM II, 51-40-04, 51-43-04 & 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON SHEAR PANEL AT FR87 BETWEEN LBL 21 TO LBL 32. REPLACED SHEAR PANEL AT FR87 BETWEEN LBL 21 TO LBL 32 IAW EMBRAER 190 SRM II 51-42-01, 51-42-02 & 51-23-06.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON GUSSET PLATE AT FR90, RBL 20. REPLACED GUSSET PLATE AT FR90, RBL 20 IAW EMBRAER 190 SRM 51-41-02 & 51-23-04/05.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - CORROSION ON GUSSET PLATE AT FR90, RBL 10.748. REPLACED GUSSET PLATE AT FR90, RBL 10.748 IAW EMBRAER 190 SRM II 51-41-02, 51-40-02 & 51-23-04.

Part: SLIDE — FAILED (R1 DOOR) · airframe 11,156 hrs · 9,403 cycles

C2 CHECK - R1 DOOR EVACUATION SLIDE FAILED TO FULLY OPEN THE DOOR DURING A SCHEDULED FUNCTIONAL TEST PER STEP ON TASK CARD 43T20025001. REPLACED R1 DOOR EVACUATION SLIDE IAW JOB CARD 43L00025001.

Part: SEAT — BROKEN (COCKPIT) · airframe 11,002 hrs · 9,137 cycles

FIRST OFFICER'S CHAIR WILL NOT LOCK AND ON LANDING SLID FREE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SEAT ASSEMBLY.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 10,332 hrs · 8,831 cycles

FLIGHT 880, IAH-PHL - ON APPROACH THE CAPTAIN SAW A LARGE BIRD FLASH BY HIS LEFT WINDOW. IMMEDIATELY THEREAFTER, THE LEFT ENGINE SHUT DOWN AND THE CREW EXPERIENCED SEVERAL EICAS FAULTS. AN EMERGENCY WAS DECLARED AND AS LANDING FLAPS WERE SELECTED THE AIRCRAFT INDICATED SLAT FAIL AND SPOILER FAULT MESSAGES ON EICAS. THE CAPTAIN BROKE OFF INITIAL APPROACH AND REQUESTED A 15 MILE FINAL FOR A NO SLAT AND FLAP 2 LANDING. THE AIRCRAFT LANDED AND TAXIED TO THE GATE. UPON INSPECTION EVIDENCE OF A BIRD STRIKE ON THE LEFT ENGINE AND ON THE LEADING EDGE OF THE LEFT WING. MAINTENANCE REPLACED THE LEFT ENGINE. ALSO THE LEFT WING SLAT PANEL SECTION 3 AND LEFT NR 3 SLAT SKEW SENSOR.

Part: GLOWSTRIP — DEFECTIVE (CABIN) · airframe 9,836 hrs · 8,324 cycles

EMERGENCY FLOOR LIGHTING STRIP COMING APART, AIRCRAFT LEFT, REAR OF FIRST CLASS. MAINTENANCE RE-INSTALLED PHOTOLUMINESCENT ESCAPE ROUTE STRIP. NO DEFECTS NOTED.

Part: COVER — MISSING (EXIT SIGN) · airframe 7,557 hrs · 6,428 cycles

PHL - EMERGENCY EXIT SIGN AT ROW 12 PLASTIC COVER IS MISSING. MAINTENANCE INSTALLED FORWARD LENS OVERWING EMERGENCY IDENTIFIER LIGHT ASSEMBLY AND SECURED. OPERATIONAL CHECK IS NORMAL.

Part: SEAT — DEFECTIVE (COCKPIT)

BOS - THE FIRST OFFICER SEAT WILL NOT LOCK IN PLACE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S SEAT, CLEANED THE SEAT TRACK AND PISTONS. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED.

Part: ROLLER — LACK OF LUBE (R1 DOOR)

LGA - THE R1 CABIN DOOR ESCAPE SLIDE ARMING LEVER BINDS AND IS DIFFICULT TO MOVE. MAINTENANCE LUBED THE LOWER ROLLERS. OPERATIONALLY CHECKS OK.

Part: LIGHT — FAILED (EVAC SLIDE) · airframe 5,844 hrs · 4,889 cycles

PIT - C1 - EEL - EMERGENCY LIGHTS FAILED TO FUNCTION DURING FORWARD SERVICE DOOR SLIDE SCHEDULED DEPLOYMENT. SLIDE DEPLOYED OK. REPLACED FORWARD SERVICE DOOR SLIDE IAW JOB CARD 43T20025001.

Part: SEAL — LEAKING (BLEED AIR SYS)

FLIGHT 935, PIT - PHL - ON FINAL APPROACH INTO PHL THE CREW EXPERIENCED A FIRE WARNING FOR NR 2 ENGINE AND DECLARED AN EMERGENCY. AS CREW WAS GOING THRU THE CHECKLIST THE WARNING EXTINGUISHED ITSELF. FIRE EXTINGUISHERS WERE NOT DEPLOYED. THE RIGHT ENGINE BLEED VALVE UPPER CLAMP WAS FOUND LEAKING, REPLACED SEALS PER AMM 36-11-03-790-801A, AND LEAKED CHECKED NORMAL. COMPLETED THRUST REVERSER INNER SLEEVE FIRE INSPECTION PER 78-31-22-210-803A AND FIRE ZONE INSPECTION PER 71-30-01-212-801A. INSPECTED AREA THERMO BLANKETS PER 78-32-00-200-801/800. REMOVED DEBRIS FROM RIGHT LOWER THRUST REVERSER AND CLEANED AREA. COMPLETE OPERATIONAL CHECK OF THE FIRE WARNING AND OVERHEAT PER 26-11-00-05. CLOSED AND SECURED THE THRUST REVERSER AND FAN COWLS.

Part: SEAL — LEAKING (BLEED AIR SYS)

FLIGHT 935, PIT - PHL - ON FINAL APPROACH INTO PHL THE CREW EXPERIENCED A FIRE WARNING FOR NR 2 ENGINE AND DECLARED AN EMERGENCY. AS CREW WAS GOING THRU THE CHECKLIST THE WARNING EXTINGUISHED ITSELF. FIRE EXTINGUISHERS WERE NOT DEPLOYED. THE RIGHT ENGINE BLEED VALVE UPPER CLAMP WAS FOUND LEAKING. REPLACED SEALS PER AMM 36-11-03-790-801A, AND LEAKED CHECKED NORMAL. COMPLETED THRUST REVERSER INNER SLEEVE FIRE INSPECTION PER 78-31-22-210-803A AND FIRE ZONE INSPECTION PER 71-30-01-212-801A. INSPECTED AREA THERMO BLANKETS PER 78-32-00-200-801/800. REMOVED DEBRIS FROM RIGHT LOWER THRUST REVERSER AND CLEANED AREA. COMPLETE OPERATIONAL CHECK OF THE FIRE WARNING AND OVERHEAT PER 26-11-00-05. CLOSED AND SECURED THE THRUST REVERSER AND FAN COWLS.

Part: GIRT BAR — JAMMED (EVAC SLIDE)

BOS - DUE TO THE GIRT BAR JAMMED IN MECHANISM IN THE FLOOR OF THE L1 DOOR THE SLIDE NEEDS REPLACED. MAINTENANCE REPLACED THE L1 DOOR SLIDE AND THE L1 DOOR ASSIST BOTTLE PNEUMATIC DIAPHRAGM. THE ASSIST BOTTLE WAS SERVICED TO PRESSURE AND THE ARMING AND DISARMING LINKAGE WERE INSPECTED WITH NO DEFECTS WERE NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

CLT - THE AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT CHARGER INDICATOR INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT.

Part: POWER CABLE — OUT OF POSITION (COCKPIT)

CLT - THE CAPTAIN'S SEAT FWD AND AFT LOCKING MECHANISM IS INOPERATIVE. THE SEAT MOVES FORWARD AND AFT FREELY. MAINTENANCE - THE ELECTRIC POWER CORD WAS FOUND CAUGHT UP UNDER THE LATCH. OPERATIONAL TEST OF SEAT IS SATISFACTORY.

Part: ENGINE — CONTAMINATED (NR 2)

FLIGHT 1711, CLT-ORF - APPROXIMATELY 100 FEET AFTER TAKEOFF THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT THERE WAS SMOKE/FUMES IN THE AFT GALLEY. THE CAPTAIN REQUESTED TO RETURN TO CLT AND THE EMERGENCY EQUIPMENT STAND BY. THE CAPTAIN STATED THE SMOKE AND FUMES DISSIPATED PRIOR TO LANDING AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE NOTICED THE NR 2 ENGINE HAS AN ODOR OF DE-ICING FLUID. THERE WAS ALSO A FAINT ODOR OF DE-ICING FLUID IN THE CABIN. MAINTENANCE PERSONNEL RAN BOTH ENGINES, BOTH PACKS AND PRESSURIZED THE CABIN. AFTER APPROXIMATELY 30 MINUTES THE ODOR CLEARED.