N841HK

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 35,815 hrs · 32,219 cycles

AFTER REACHING CRUISE, CREW FELT A BUMP IN THE PRESSURIZATION & CABIN PRESSURE BEGAN TO RISE, DONNED OXYGEN MASKS & PERFORM ALL REQUIRED CHECKLISTS. AN EMERGENCY WAS DECLARED AND DESCENDED TO 10000 FT. CABIN ALTITUDE REACHED 15000 FT & PAX O2 MASKS DEPLOYED. ONCE STABILIZED, DIVERTED & LANDED WITHOUT INCIDENT. FOUND AIR LEAKS AROUND MAIN PAX, SERVICE DOORS AND COCKPIT SIDE WINDOWS SEALS AND REPAIRED. FOUND CONNECTING B-NUTS TO ELECTROPNEUMATIC OUTFLOW VALVE LOOSE AND TIGHTENED. FOUND LEAK BEHIND THE NR 2 STATIC PORT AND CORRECTED. DISCOVERED 1500 FT/MIN LEAK IN ELECTROPNEUMATIC OUTFLOW VALVE. THE VALVE WAS REPLACED . OPS CHECK FLIGHT AND THE PRESSURIZATION SYSTEM CHECKING NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: PLATE — CORRODED (FRAME 14) · corrosion level 2 · airframe 35,533 hrs · 31,917 cycles

FRAME 14 HAS CORROSION. REPLACED FRAME PLATE

Part: PLATE — CORRODED (FRAME 18) · corrosion level 2 · airframe 35,533 hrs · 31,917 cycles

FRAME 18 PLATE HAS CORROSION. MAINTENANCE REPLACED THE FRAME PLATE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,474 hrs · 31,858 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 IS INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 35,474 hrs · 31,858 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN DURING POST FLIGHT. MAINTENANCE CLEANED AND LUBED MAIN DOOR, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 35,274 hrs · 31,692 cycles

LEFT OVERWING EMERGENCY LIGHT NR 5 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT, OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 33,760 hrs · 30,331 cycles

MAIN DOOR DIFFICULT TO OPEN OR CLOSE DURING POST FLIGHT. MAINTENANCE CLEANED AND LUBED MAIN PASSENGER DOOR SEALS, OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — INOPERATIVE (WING) · airframe 33,664 hrs · 30,244 cycles

WING ANTI-ICE FAIL MESSAGE ON EICAS DURING CRUISE, RETURNED TO DEPARTURE. MAINTENANCE REPLACED LT WING ANTI ICE VALVE, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,593 hrs · 30,174 cycles

LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 33,521 hrs · 30,104 cycles

MAIN CABIN DOOR HARD TO OPEN DURING POST FLIGHT. MAINTENANCE INSPECTED AND LUBED MAIN DOOR AND OPS CHECKED GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 32,998 hrs · 29,620 cycles

DURING LANDING, LOSS OF HYDRAULIC FLUID FROM SYSTEM 2, FOLLOWED BY HYD 2 LOW QUANTITY, RUDDER SYS 2 INOPERATIVE, AILERON SYS 2 INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP, OPS AND LEAK CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,751 hrs · 29,379 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 3 IS INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (GALLEY) · airframe 32,751 hrs · 29,379 cycles

CEILING EMERGENCY EXIT LIGHT IN GALLEY IS INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,653 hrs · 29,276 cycles

EMERGENCY LIGHT STRIP AT ROW 3 AND 4 INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT STRIP, OPS CHECKED GOOD.

Part: RIVET — CORRODED (FRAME 33) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

TWO RIVETS HAVE CORROSION ON LOWER FUSELAGE BY FRAME 33. MAINTENANCE REPLACED TWO RIVETS.

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

FORWARD SERVICE DOOR SILL HAS CORROSION. MAINTENANCE REPLACED FORWARD SERVICE DOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

LT OMEGA BEAM HAS CORROSION AT FR20. MAINTENANCE REPLACED LT OMEGA BEAM AT FR20.

Part: CHANNEL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

LOWER SERVICE DOOR CHANNEL, DOOR FRAME HAS CORROSION. MAINTENANCRE REPLACED LOWER SERVICE DOOR FRAME.

Part: GUSSET — CORRODED (FRAME 20-22) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

CENTER GUSSET HAS CORROSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REPLACED CENTER GUSSET.

Part: SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

CENTER RAMP SUPPORT HAS CORROSION AT FRAME 20. MAINTENANCE REPLACED CENTER RAMP SUPPORT.

Part: HOUSING — CORRODED (LAVATORY) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

LAVATORY DRAIN CUP HOUSING CORRODED. MAINTENANCE REPLACED LAVATORY DRAIN CUP HOUSING.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,653 hrs · 29,276 cycles

CARGO BAY SILL PLATE HAS CORROSION. MAINTENANCE REPLACED CARGO BAY SILL PLATE.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,483 hrs · 29,121 cycles

F/A REPORTED SMOKE AND BURNING ODOR AT ROW 19.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,234 hrs · 27,983 cycles

RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MX REPLACED RIGHT AFT WING/FUSELAGE FAIRING LIGHT AND OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 30,700 hrs · 27,542 cycles

LEFT AFT WING TO FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MX REPLACED FLOOD LIGHT AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,693 hrs · 27,536 cycles

CABIN EMERGENCY LIGHTS 8 AND 14 FOUND INOPERATIVE DURING PREFLIGHT. FERRIED ACFT AND MX REPLACED LIGHTS AND OPS CHECKED GOOD.

Part: SWITCH — CONTAMINATED (EMERGENCY LIGHTS) · airframe 29,713 hrs · 26,686 cycles

AFTER NORMAL AIRCRAFT POWER DOWN SEVERAL EMERGENCY LIGHTS STAYED ON IN THE AFT CABIN, OVERWING EMERGENCY LIGHT AND MAIN CABIN STAIR LIGHTS. MAINTENANCE INSPECTED CLEANED THE EMERGENCY LIGHT SWITCH. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,354 hrs · 26,347 cycles

DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT. SYSTEM OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,500 hrs · 25,595 cycles

DURING PREFLIGHT, THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS SYSTEM WAS LEFT ACTIVE FROM PREVIOUS FLIGHT AND EXTINGUISHED. MAINTENANCE INSPECTED AND FOUND TO BE SAFE FOR ONE-WAY FERRY FLIGHT TO KSTL. IN KSTL, MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES, OPS CHECK GOOD. A/C IS RELEASED FOR FERRY FLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,653 hrs · 22,083 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT ABOVE THE PASSENGER DOOR WAS INOP. MAINTENANCE INSPECTED AND RELAMPED THE EMERGENCY LIGHT ABOVE THE PASSENGER DOOR. SYSTEM OPS CHECKED GOOD.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 24,653 hrs · 22,083 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HANDLE WAS HANGING UP WHEN TRYING TO OPEN FROM THE INSIDE. MAINTENANCE INSPECTED AND FOUND THE PASSENGER DOOR HANDLE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR HANDLE. SYSTEM OPS CHECKED GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 24,635 hrs · 22,067 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHTS AT 17F - 17H, 16C, 16D AND 18A INOP. MAINTENANCE INSPECTED AND RE-SEATED THE CONNECTOR. SYSTEM OPS CHECKED GOOD.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

CARGO ENTRY SILL AT FR 65-68 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1122

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SHEAR CLIP AT FR 65 IS CORRODED BEYOND LIMITS. R & R SHEAR CLIP. W/C 1124

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SHEAR CLIP AT FR 68 STGR 9L-18L IS CORRODED BEYOND LIMITS. R & R SHEAR CLIP. W/C 1125.

Part: SUPPORT — BROKEN (BS 6938) · airframe 24,448 hrs · 21,913 cycles

(V0XR) FLIGHT CABLE STANDOFF SUPPORT BROKEN AT STA 6938. R & R SUPPORT. W/C 1128

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CARGO DOOR CABLE TORSION RODS BRACKET CRACKED. R & R SUPPORT. W/C 2072

Part: SILL — CRACKED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT CARGO FLOOR SILL BETWEEN FR 68-71 IS CRACKED. R & R SILL. W/C 2194

Part: SUPPORT — CRACKED (ZONE 500) · airframe 24,448 hrs · 21,913 cycles

LT UPPER WING TO BODY FAIRING SUPPORT STRIP STA 16143.5-17445.0 IS CRACKED. R & R STRIP. W/C 1054.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SEAT TRACK POS B FR 18-24 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2139.

Part: PROFILE — CRACKED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) FWD LOWER CORNER OF CARGO FLOOR IS DAMAGED. R & R PROFILE. W/C 8011

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) LT SILL AT FR 36-41 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1078.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CORRECTION SEAT TRACK POS A FR 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2146

Part: STRIP — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

RIGHT UPPER WING TO BODY FAIRING STRIP BETWEEN STA 16143.5 - 17445.0 IS CRACKED. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

GUSSET AT FR 59-62 RY 479.0 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SUPPORT ANGLE AT FR 20 FROM Y0.0 IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1098

Part: DOUBLER — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

DOUBLERS AT FR 20 - 22 FROM RY479.0 IS CORRODED BEYOND LIMITS. R & R DOUBLERS.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SEAT TRACK POS D AT FR 47-52 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

LEFT FWD OMEGA BEAM AT FR 14-23 IS CORRODED BEYOND LIMITS. R & R BEAM.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SEAT TRACK POS D AT FR 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: PARTITION — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

LT LOWER PARTITIAN AT FR 61 IS CORRODED BEYOND LIMITS. R & R PARTITIAN.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SUPPORT ANGLE AT FR 19 - 20 FROM Y0.0 IS CORRODED BEYOND LIMITS. R & R ANGLE.

Part: BRACKET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

WING TO BODY FAIRING BRACKET BETWEEN FR 48-49 IS CRACKED. R & R STRIP.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

RIGHT SILL FR 65 - 68 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

AFT SILL AT FR 22-23 FROM RY780.0 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

LEFT GUSSET AT FR 20 - 24 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POS B AT FR 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

PROFILE AT FR 17 - 18 FROM LY780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POS D AT FR 36-47 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POS B AT FR 52-60 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

RIGHT SILL AT FR 61-65 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

RT HAT BEAM AT FR 58-62 IS CORRODED BEYOND LIMITS. R & R BEAM HAT.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

SEAT TRACK POS C AT FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: ANGLE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SCALLOPED ANGLE AT FR 18 RY 780.0 TO LY 479.0 IS CORRODED BEYOND LIMITS. R & R DOUBLER.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POSITION A FR 36-47 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) FWD DIGITAL AT FR 14-16 AT RY 780.0 TO RY780.0 IS CORRODED OUT OF LIMITS. R & R DIGITAL.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CTR HAT CHANNEL BEAM SUPPORT FR 14 Y0.0 IS CORRODED OUT OF LIMITS. R & R SUPPORT.

Part: BRACKET — BROKEN (ZONE 800) · airframe 24,448 hrs · 21,913 cycles

(V0XR) UPLOCK BRACKET FOR CARGO DOOR BROKEN. R & R BRACKET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CTR GUSSET FR 20-23 AT Y0.0 IS CORRODED OUT OF LIMITS. R & R GUSSET.

Part: ATTACH ANGLE — CRACKED (LT WING ATTACH) · airframe 24,448 hrs · 21,913 cycles

(V0XR) LT LOWER FWD WING ATTACHMENT ANGLE CRACKED. R & R ATTACHMENT ANGLE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CTR GUSSET AT FR 23-29 IS CORRODED OUT OF LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT SILL FR 48-52 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POSITION B FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT BEAM DOUBLER AT FR 18 IS CORRODED BEYOND LIMITS. R & R DOUBLER.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT SILL FR 36-41 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT SILL AT FR 41-48 IS CORRODED OUT OF LIMITS. R & R RT SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) FWD SILL FR 19-20 AT RY 780.0 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SEAT TRACK POSITION A FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) CTR OMEGA BEAM AT FR 17-25 AT Y0.0 IS CORRODED OUT OF LIMITS. R & R OMEGA BEAM.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) OMEGA CTR BEAM FR 14-18 IS CORRODED OUT OF LIMITS. R & R OMEGA CTR BEAM.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT WINGTIP TO WING L/E GUSSET IS CRACKED. R & R GUSSET.

Part: ANGLE — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) SCALLOPED ANGLE FR 23 AT Y0.0 TO RY 780.0 IS CORRODED OUT OF LIMITS. R & R ANGLE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

GUSSET ON CTR BEAM AT FR 41-46 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) HORSHOE DIGITAL FR 17-18 FROM LY 479.0 TO Y0.0 IS CORRODED OUT OF LIMITS. R & R DIGITAL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) GUSSET ON CTR BEAM AT FR 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) LT SILL FR 41-48 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) GUSSET ON CENTER BEAM AT FR 36-41 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) GUSSET AT Y0 FRAME 59-62 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) RT SILL FRAME 29-35 IS CORRODED BEYOND LIMITS. R & R RT SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) LT SILL FRAME 61-65 IS CORRODED BEYOND LIMITS. R & R LT SILL.

Part: SUPPORT ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 31,473 hrs · 30,775 cycles

(V0XR) LOWER LT WING TO BODY FAIRING SUPPORT ANGLE IS CRACKED. R & R LT ANGLE.

Part: ANGLE — CRACKED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) SHAPE U ANGLE ON PASSENGER DOOR ENTRY CORRODED BEYOND LIMITS. R & R ANGLE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) GUSSET AT LY479.0 FRAME 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) SILL AT LY780.0 FRAME 19-24 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SUPPORT ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 31,473 hrs · 30,775 cycles

(V0XR) LOWER RT WING TO BODY FAIRING SUPPORT ANGLE IS CRACKED. R & R RT ANGLE.

Part: ANGLE — CRACKED (ZONE 100) · airframe 31,473 hrs · 30,775 cycles

(V0XR) SHAPE U ANGLE ON PASSENGER DOOR ENTRY CORRODED BEYOND LIMITS. R & R ANGLE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) LT GUSSET FROM FRAMES 23-29 ARE CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) RT SILL FROM FRAMES 24-29 ARE CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,448 hrs · 21,913 cycles

(V0XR) LT SILL FROM FRAMES 23-29 ARE CORRODED BEYOND LIMITS. R & R GUSSET.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 24,312 hrs · 21,806 cycles

DURING FLIGHT THE CAPT WINDSHIELD STARTED TO DELAMINATE IN FLIGHT WITH WATER FREEZING AND EXPANDING BETWEEN PLYS. AIRCRAFT RETURNED FROM FLIGHT. MAINTENANCE INSPECTED THE WINSHIELD AND REMOVED AND REPLACED THE CAPT WINDSHEILD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,251 hrs · 21,747 cycles

THE CREW REPORTED THAT THE REAR AISLE FLOOD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD FOLLOWING REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,551 hrs · 21,106 cycles

DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT AT ROW 13 WAS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULB. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,542 hrs · 21,100 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT 16D WAS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,145 hrs · 20,735 cycles

DURING PRE-FLIGHT THE FLIGHT CREW REPORTED SEVERAL EMERGENCY LIGHTS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. SYSTEM OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 23,074 hrs · 20,670 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED SEVERAL EMERGENCY EXIT LIGHTS DID NOT WORK. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY NR 3. SYSTEM OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,011 hrs · 20,618 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED SEVERAL FLOOR STRIP EMERGENCY LIGHTS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 22,926 hrs · 20,529 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT VARIOUS EMERGENCY LIGHTS NOT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT FOR A FERRY FLIGHT TO STL. MAINTENANCE IN STL INSPECTED AND REMOVED AND REPLACED A BULB FROM THE OVERHEAD EMERGENCY LIGHT AND NR 2 AND 3 POWER SUPPLIERS. SYSTEM OPS CHECKED GOOD.

Part: CONNECTOR — DEFECTIVE (RT MLG) · airframe 22,756 hrs · 20,380 cycles

DURING CLIMB CREW RECEIVED A LANDING GEAR AIR/GRN FAIL MESSAGE. MAINTENANCE INSPECTED AND REPAIRED RT MLG FWD WOW SWITCH CONNECTOR. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LT MLG) · airframe 22,710 hrs · 20,335 cycles

DURING THE FLIGHT, THE CREW REPORTED RECEIVING A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE LT MLG AFT PROXIMITY SWITCH AND RELAYS K0353 & K0453 IAW AMM PROCEDURES. FOLLOW ON OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM WAS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,348 hrs · 20,001 cycles

DURING CLIMB, THE CREW RECEIVED AN AIR/GND FAIL MESSAGE ON THE EICAS AND THAT THE GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM WITH NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,249 hrs · 19,913 cycles

DURING THE PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANT AS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 20,803 hrs · 18,601 cycles

DURING PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY AS PER MAINTENANCE MANUAL PROCEDURES. SYSTEM OPS CHECKED GOOD.

Part: WIRE — LOOSE (CABIN) · airframe 20,683 hrs · 18,494 cycles

PRE FLT 8010 - STL - DURING PRE FLT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW 12 WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE WIRE TO THE LIGHT ASSEMBLY. OPERATIONAL CHECK OF THE LIGHTS AFTER THE REPAIR CHECKED GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 20,491 hrs · 18,324 cycles

DURING PRE-FLIGHT AT SYR, EMERGENCY LIGHT AT 18B INOP. MAINTENANCE CLEANED CONNECTOR AT LIGHT ASSEMBLY.

Part: WARNING SYSTEM — MALFUNCTIONED (CARGO DOOR) · airframe 20,236 hrs · 18,094 cycles

FLT 7912 - IAD - CREW RECEIVED A CARGO DOOR OPEN INDICATION ON THE EICAS DURING CLIMB. MAINTENANCE INSPECTED AND FOUND THE DOOR TO BE SECURELY CLOSED. THE DOOR INDICATION WAS DEFERRED PER MEL PROCEDURES.

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING PRE-FLIGHT INSPECTION, FA NOTICED SMOKE AT ROW 8C SIDEWALL LIGHTS. MAINT DEFERRED LIGHT AT 8C SIDEWALL IAW MEL PROCEDURES. (K)

Part: CONNECTOR — LOOSE (CABIN) · airframe 18,340 hrs · 16,361 cycles

PRE FLT NR 7889 MKE CABIN EMERGENCY LIGHT INOPERATIVE. MX RESEATED THE CONNECTOR AT THE LIGHT ASSEMBLY. OPS CHECKED AS PER AMM PROCEDURES.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 17,527 hrs · 15,637 cycles

PRE FLT 794 - RIC - EMERGENCY LIGHT OUT AT OVERHEAD EXIT INDICATOR. MAINTENANCE RESEATED THE CONNECTOR AT THE EMERGENCY LIGHT INVERTER. SYSTEM OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 17,203 hrs · 15,354 cycles

DURING SCHEDULED MAINTENANCE - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,010 hrs · 15,175 cycles

PRE FLT 7908 - IAD - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,994 hrs · 15,159 cycles

PRE FLT 7959 - ROC - OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE AFFECTED LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: WIRE — LOOSE (CABIN) · airframe 16,421 hrs · 14,657 cycles

PRE FLT NR 8058 - ORD - EMERGENCY LIGHT AFT SIDE AFT CEILING EXIT LOCATOR INOP. MAINTENANCE SECURED LOOSE WIRES, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 15,486 hrs · 13,812 cycles

PRE FLT NR 8021 - IAD - EMERGENCY LIGHT AT COCKPIT DOOR INOP. MAINTENANCE REMOVED AND REPLACED LAMP CHECK GOOD.

Part: WIRE HARNESS — FAULTY (NR 2 ENGINE) · airframe 14,700 hrs · 13,079 cycles

PRE FLT 8010 - STL - ENGINE 2 NO DISPATCH. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE INTERNAL YELLOW B-HARNESS, NO FAULTS AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (MLG) · airframe 14,699 hrs · 13,078 cycles

FLT 7904 - IAD - L/G AIR/GROUND FAIL MESSAGE, WITH AURAL WARNING. MAINTENANCE INSPECTED AND TESTED WOW SWITCHES CHECKS GOOD. PERFORMED WOW ADJUSTMENT, OPS CHECK GOOD. NO FURTHER MESSAGE.

Part: SWITCH — SHORTED (RT MLG WOW) · airframe 14,660 hrs · 13,039 cycles

FLT 8022 - STL - LANDING GEAR AIR/GROUND FAIL, NO TRIM, LANDING GEAR NOT DOWN MESSAGES. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR WOW PROX SWITCH, AFT SIDE, SYSTEM CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,551 hrs · 12,939 cycles

POST FLT NR 8045 - STL - FLOOR PROXIMITY LIGHT EMERGENCY FLOOR STRIP LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FORWARD LIGHT BULBS ABOVE 1A, OPS CHECK GOOD. PERFORMED OPS CHECK ON FLOOR PROX LIGHT, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 14,403 hrs · 12,790 cycles

PRE FLT NR 8046 - IAD - FWD EMERGENCY LIGHT STRIP FLOOR PROXIMITY LIGHT INOP. MAINTENANCE CLEANED CONNECTOR ON FWD STRIP.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 14,291 hrs · 12,685 cycles

FLT NR 8023 - IAD - AUTO PILOT FAIL FOLLOWED BY RUDDER SYS 1-2 INOP MESSAGE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RELAYS K0775, K0111, AND K0363. THE NR 1 AND NR 2 RUDDER LOW PRESSURE SWITCHES WERE REMOVED AND REPLACE ALSO.

Part: HANDSET — ODOR · airframe 14,126 hrs · 12,529 cycles

FLT NR 7918-IAD-ELECTRICAL BURNING ODOR THROUGHOUT CABIN AND COCKPIT. MAINTENANCE REMOVED AND REPLACE THE FORWARD FLIGHT ATTENDANT HANDSET.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 14,060 hrs · 12,460 cycles

PRE FLIGHT NR 8006 - RIC - EMERGENCY LIGHT OVER SEAT 12BC INOP. MAINTENANCE REMOVED AND REPLACED THE BULB.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 13,377 hrs · 11,798 cycles

FLT NR 7982 -IAD - LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINTENANCE ACCOMPLISHED AN AIR/GROUND SYSTEM TEST. NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 13,086 hrs · 11,521 cycles

FLT 7965 - ORD - BAG DOOR WARNING ILLUMINATED IN FLIGHT. MAINTENANCE DEFERRED THE INDICATION SYSTEM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,657 hrs · 11,123 cycles

PRE FLIGHT 8092 - ORD - EMERGENCY LIGHT SYSTEM INOP. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM AND FOUND THE NR 2 EMERGENCY LIGHT POWER SUPPLY CONNECTOR LOOSE. OPS CHECKED GOOD AFTERWARDS.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 12,218 hrs · 10,729 cycles

FLT NR 7955 - IAD - EXTREMELY LOUD AIR NOISE COMING FROM MAIN CABIN DOOR. AIRCRAFT DID NOT PRESSURIZE NORMALLY. CABIN WOULD CLIMB 900 FPM, LEVEL OFF AND THEN CLIMB RAPIDLY AGAIN. FLIGHT ATTENDANT REPORTED THAT 2 DOOR CLOSED AND LOCKED INDICATORS WERE NO LONGER ALIGNED. MAINTENANCE CLEANED AND INSPECTED THE MAIN DOOR SEAL, STOPS AND ALIGNMENT MARKS. FOUND DEBRIS IN THE SEAL AREA. RESET PRESSURIZATION CONTROLLER AND CABIN PRESSURIZATION ACQUISITION MODULE CIRCUIT BREAKERS. PRESSURIZATION OPS CHECKED GOOD.

Part: DOWNLOCK SWITCH — FAILED (MLG) · airframe 11,246 hrs · 9,780 cycles

FLT 8000 - IAD - LANDING GEAR AIR/GROUND FAULT. MAINTENANCE REMOVED AND REPLACED THE DOWNLOCK PROXIMITY SWITCH AND CONNECTOR.

Part: CONTROL UNIT — FAILED (MLG) · airframe 11,245 hrs · 9,778 cycles

FLT 8042 - IAD - LANDING GEAR AIR/GROUND FAILURE AFTER TAKEOFF. MAINTENANCE REPLACED THE LANDING GEAR CONTROL UNIT.

Part: SOLENOID VALVE — FAILED (MLG) · airframe 10,582 hrs · 9,108 cycles

FLT 7984 - IAD - LOUD BANGING NOISE AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SOLENOID VALVE.

Part: TILLER — BROKEN (NLG STEERING) · airframe 10,171 hrs · 8,709 cycles

FLT 8077 - ROA - NOSEWHEEL STEERING WILL NOT ENGAGE WITH THE TILLER. MAINTENANCE REMOVED AND REPLACED THE HANDWHEEL. OPS CHECKED GOOD.