N832HK

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 37,034 hrs · 33,666 cycles

UNCONTROLLABLE CABIN PRESSURIZATION IN FLIGHT - BOTH IN AUTO & MANUAL MODES.

Part: SUPPORT — CORRODED (FRAME 23) · airframe 35,229 hrs · 32,147 cycles

CTR OMEGA BEAM AT FR 23 HAS CORROSION. REMOVED AND REPLACED CTR OMEGA BEAM AT FR 23

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-25) · corrosion level 2 · airframe 35,229 hrs · 32,147 cycles

CORROSION ON CABIN FLOORBOARD SUPPORT SILL REMOVED AND REPLACED AFEECTED PART

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 35,229 hrs · 32,147 cycles

SHEAR CLIP IS CRACKED AT FR 72 STR 17L. REMOVED AND REPLACED SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 35,229 hrs · 32,147 cycles

SHEAR CLIP IS CRACKED AT FR 72 STR 16L. REMOVED AND REPLACED SHEAR CLIP.

Part: GUSSET — CORRODED (FRAMES 18-21) · airframe 35,229 hrs · 32,147 cycles

CTR GUSSET HAS CORROSION FROM FR18- FR 21. REMOVED AND REPLACED THE CTR GUSSET.

Part: FLOORBOARD — CORRODED (FRAME 20) · airframe 25,229 hrs · 32,147 cycles

ANGLE ON FLOOR BOARD AT FR 20 HAS CORROSION.... REMOVED AND REPLACED ANGLE...

Part: MOUNT — GOUGED (APU) · airframe 35,229 hrs · 32,147 cycles

APU LOWER RT MOUNT WAS GOUGED TOP SIDE. REMOVED AND REPLACED APU LOWER RT MOUNT....

Part: STRUCTURE — CRACKED (FRAME 15) · airframe 25,229 hrs · 32,147 cycles

FWD CTR DIGITAL IS CRACKED AT FRAME 15... REPAIRED WITH FILLER AND DOUBLER IAW SRM 53-21-10

Part: BRACKET — DAMAGED (CARGO RAMP) · airframe 35,229 hrs · 32,147 cycles

CARGO RAMP FWD SUPPORT LOWER BRACKET HAS DAMAGED RIVETS. FOUND CARGO RAMP FWD LOWER BRACKET TO BE CRACKED. REMOVED AND REPLACED THE BRACKET.

Part: BEAM — CORRODED (FRAME 20) · airframe 25,229 hrs · 32,147 cycles

PREVIOUS REPAIR ON L/H OMEGA BEAM AT FR 20 HAS CORROSION.... REMOVED AND FABRICATED NEW AND INSTALLED IAW SRM 53-21-10

Part: SKIN — DENTED (FRAMES 75-76) · airframe 35,229 hrs · 32,147 cycles

FUSELAGE DENT BETWEEN FR. 75-76 STR.11L-12L DAMAGED SKIN REMOVED AND REPAIR DOUBLER FABRICATED AND INSTALLED

Part: CLAMP — BROKEN (ZONE 400) · airframe 34,295 hrs · 40,221 cycles

ON CLIMBOUT AND ACFT CONFIGURED FOR FULL THRUST, BLEED 1 LOW TEMP IN ICING CONDITIONS. FOUND BROKEN CLAMP ON NR 1 FAN AIR VALVE, R&R CLAMP AND SWAPPED NR 1 AND NR 2 FAN AIR VALVES OPS TEST GOOD. JUMPED RELAYS I21/I22 FOR BLEED OPS CHECK, AFTER SWAPPING FAN AIR VALVES AND REPLACING NR 1 SIDE CLAMP TO FAN AIR VALVE. TEMP INDICATION WERE IN THE GREEN. OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 32,548 hrs · 29,811 cycles

ELECTRICAL BURNING ODOR AT THE LIGHT AT ROW 7. OPEN

Part: WIRE HARNESS — FAILED (CABIN LIGHT) · airframe 32,548 hrs · 29,811 cycles

DISABLED LIGHT AND BALLAST AT ROW 7. R & R HARNESS ASSY AT ROW 7.

Part: LINE — NOT REPORTED (NR 1 FAN CONTROL) · airframe 32,458 hrs · 29,737 cycles

BLEED 1 OVERTEMP EICAS MESSAGE AFTER TAKEOFF. R & R THE NR 1 FAN AIR CONTROL THERMOSTAT LINE. OPS CHECKED GOOD.

Part: COVER — MISSING (VALVE) · airframe 30,277 hrs · 27,873 cycles

ACFT FAILED TO PRESSURIZE IN BOTH AUTO & MANUAL MODE. FOUND GROUND CONNECTION VALVE COVER MISSING, REPLACED COVER IAW AMM 21-22-04, PERFORMED PRESSURIZATION CHECK IAW AMM 21-31-00, OPS CHECKED GOOD.

Part: LIGHT — SHORTED (LT OVERWING) · airframe 29,402 hrs · 27,166 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. FOUND LT OVERWING EMERGENCY LIGHT TO BE SHORTED TO GROUND. R & R LT EXTERNAL OVERWING LIGHT ASSY. OPS CHECK GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 29,193 hrs · 26,998 cycles

MOST FORWARD SECTION OF EMERGENCY LIGHTING IS NOT SERCURE TO FLOOR. RESECURED LOOSE EMERGENCY LIGHT.

Part: SOCKET — BURNED (CABIN LIGHT) · airframe 28,931 hrs · 26,782 cycles

BURNING ODOR IN CABIN. FOUND BURNED LIGHT SOCKET AT ROW 17 AND 18A. DEACTIVATED BULB AND REMOVED CONNECTOR.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 28,649 hrs · 26,544 cycles

AUTO PRESSURIZATION LOSING PRESSURE, SWITCHED TO MANUAL MODE, MANUAL MODE WAS HARD TO CONTROL. OPEN

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,552 hrs · 25,606 cycles

FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,261 hrs · 25,343 cycles

PASSENGER DOOR EMERGENCY EXIT FLOOD LIGHT NR 3 INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 27,114 hrs · 25,211 cycles

MAIN PASSENGER DOOR DIFFICULT TO OPEN DURING POST FLIGHT. MAINTENANCE INSPECTED AND CLEANED AND LUBRICATED MAIN DOOR ROLLERS, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,929 hrs · 25,037 cycles

PASSENGER DOOR ENTRANCE EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,841 hrs · 24,955 cycles

PASSENGER DOOR DIFFICULT TO OPEN DURING POST FLIGHT. MAINTENANCE LUBED DOOR AND ADJUSTED INTERNAL HANDLE, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,798 hrs · 24,901 cycles

RIGHT EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 26,744 hrs · 24,856 cycles

MAIN ENTRANCE F/A FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,739 hrs · 24,850 cycles

RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 26,723 hrs · 24,838 cycles

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

Part: ANTENNA — FAILED (VOR) · airframe 26,554 hrs · 24,686 cycles

NR 1 AND 2 VOR LOCALIZERS VERY ERRATIC WITH FULL DEFLECTIONS L/R NEAR LANDING MINIMUMS. MAINTENANCE INSPECTED AND REPLACED LT VOR ANTENNA, OPS CHECK GOOD.

Part: BLEED VALVE — FAILED (NR 2) · airframe 26,499 hrs · 24,639 cycles

NR 2 BLEED VALVE FAILED DURING CLIMB AND RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE HIGH STAGE VALVE, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

CENTER OMEGA BEAM AT FR 59 HAS CORROSION AROUND FASTENER HOLE. MAINTENANCE REPAIRED CENTER OMEGA BEAM.

Part: ANGLE — CORRODED (FRAME 20) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

CENTER RAMP ANGLE CORRODED AT FR 20. MAINTENANCE REPLACED CENTER RAMP ANGLE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

AFT SERVICE DOOR SILL CORRODED. MAINTENANCE REPLACED AFT SERVICE DOOR SILL.

Part: GUSSET — CORRODED (FRAME 22) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

CENTER GUSSET CORRODED AT FRAME 22. MAINTENANCE REPLACED CENTER GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

RT OMEGA BEAM CORRODED AT FRAME 23. MAINTENANCE REPLACED RT OMEGA BEAM.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

FORWARD SERVICE DOOR SILL CORRODED. MAINTENACE REPLACED FORWARD SERVICE DOOR SILL.

Part: CHANNEL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

SERVICE DOOR CHANNEL CORRODED. MAINTENANCE REPLACED SERVICE DOOR CHANNEL.

Part: DOUBLER — CORRODED (FRAME 20) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

DOUBLER ON RT OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE REPLACED DOUBLER.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

LEFT FLOOR SUPPORT AT FRAME 59 CORRODED. MAINTENANCE REPLACED LT FLOOR SUPPORT.

Part: CHANNEL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 34,361 hrs · 30,502 cycles

CARGO DOOR ZEE CHANNEL CORRODED. MAINTENANCE REPLACED CARGO DOOR ZEE CHANNEL.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 26,378 hrs · 24,531 cycles

DURING POST FLIGHT, THE MAIN PASSENGER DOOR IS HARD TO OPEN. MAINTENANCE LUBRICATED PASSENGER DOOR AND OPS CHECK GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 26,104 hrs · 24,255 cycles

MAIN PASSENGER DOOR HARD TO OPEN DURING POST FLIGHT. MAINTENANCE INSPECTED AND LUBRICATED MAIN DOOR LOCKING MECHANISM, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 26,076 hrs · 24,231 cycles

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

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 25,759 hrs · 23,931 cycles

CEILING EMERGENCY EXIT LIGHT IN GALLEY IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT IN THE GALLEY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,016 hrs · 23,239 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,980 hrs · 23,205 cycles

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

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 24,783 hrs · 23,032 cycles

PASSENGER DOOR IS DIFFICULT TO OPEN DURING POST FLIGHT. MAINTENANCE INSPECTED AND LUBED PASSENGER DOOR SEAL, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,706 hrs · 22,966 cycles

LEFT AFT WING TO FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED FLOOD LIGHT, OPS CHECKED GOOD.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 24,697 hrs · 22,959 cycles

UNCOMMANDED NR 1 ENGINE SHUTDOWN DURING CLIMB. ALL OTHER ENGINE INDICATIONS WERE NORMAL AND ENGINE NR 1 EXCEEDENCE MESSAGE WAS DISPLAYED ON EICAS AFTER SHUTDOWN.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 24,696 hrs · 22,957 cycles

DURING POST FLIGHT INSPECTION, CREW FOUND PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED, CLEANED AND LUBED PASSENGER DOOR, OPS CHECKED GOOD.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 23,950 hrs · 22,319 cycles

MAIN PASSENGER DOOR IS HARD TO OPEN. MX ADJUSTED ROLLERS AND CABLES, OPS CHECK GOOD.

Part: DOOR — DIRTY (MAIN PAX) · airframe 23,920 hrs · 22,291 cycles

PASSENGER DOOR HARD TO OPEN. MX CLEANED AND OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 23,401 hrs · 21,837 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW FOUND THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND THE DOOR SEAL WAS CLEANED AND LUBED. DOOR OPS CHECKED GOOD.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 23,245 hrs · 21,703 cycles

DURING POST FLIGHT INSPECT THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR LINKAGE. THE DOOR OPS CHECK GOOD.

Part: SKIN — DENTED (ZONE 200)

DENT IN FUSELAGE SKIN BETWEEN FRAMES 56 AND 57, 1.4" BELOW STRINGER 12L, 1.1" AFT OF FRAME 56. REPAIRED DENT IAW SRM 53-24-01, TYPE A, FIG 208, SHEET 3.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 22,826 hrs · 21,308 cycles

DURING CLIMB THE FLIGHT CREW GOT A BLEED 2 VALVE FAIL MESSAGE FOLLOWED BY A WING ANTI-ICE FAIL MESSAGE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 HIGH STAGE PRESSURE SWITCH AND THE NR 2 BLEED VALVE. SYSTEM OPS CHECKED GOOD.

Part: ROLLER — DEFECTIVE (PAX DOOR) · airframe 21,946 hrs · 20,517 cycles

PASSENGER DOOR HARD TO OPEN DURING POST FLIGHT. MAINTENANCE INSPECTED AND DOOR SECURES AND SEALS PROPERLY FOR A ONE TIME FERRY FLIGHT TO KSTL. MAINTENANCE REPLACED 2 AIRFRAME ROLLERS AND OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,878 hrs · 20,454 cycles

DURING CRUISE, THE PACK NR 2 OVERLOAD MSG APPEARED, PACK NR 2 VALVE CLOSED. THE CREW RETURNED A/C TO STL. MAINTENANCE PERFORMED OPS CHECK OF PACK NR 2, OPS CHECK GOOD.

Part: VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 21,878 hrs · 20,454 cycles

DURING CRUISE, BLEED NR 1 OVERTEMP APPEARED. THE CREW RETURNED THE A/C TO STL. MAINTENANCE INSPECTED AND REPLACED NR 1 FAN AIR VALVE, OPS CHECK GOOD.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 21,378 hrs · 20,000 cycles

CREW REPORTED A SMOKE SMELL COMING FROM OVERHEAD LIGHT BALLAST AT ROW 2, DURING CRUISE. AFTER MAKING ITS SCHEDULE LANDING, MAINTENANCE INSPECTED AND DEFERRED THE CABIN LIGHTING AT ROWS 3 AND 4.

Part: LIGHT — LOOSE (CABIN) · airframe 21,322 hrs · 19,956 cycles

EMERGENCY FLOOR LIGHT PHOTO ILLUMINESCENT STRIP LOOSE AT GALLEY. MAINTENANCE RE-SECURED EMERGENCY FLOOR LIGHT PHOTO ILLUMINESCENT STRIP, OPS CHECK GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (RT MLG) · airframe 21,292 hrs · 19,929 cycles

AFTER TAKEOFF IN KSTL, THE AIRCRAFT HAD A LANDING GEAR AIR GND FAIL MSG ON EICAS. THE CREW RETURNED THE AIRCRAFT TO KSTL FOR AN UNSCHEDULED LANDING. MAINTENANCE INSPECTED AND FOUND THE RIGHT MLG WOW PROX SWITCH OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED WOW PROX SWITCH AND OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,238 hrs · 19,883 cycles

CREW REPORTED A "FLAP OVERSPEED" WARNING IN FLIGHT WITH FLAPS AT 45 DEGREES AND AT A SPEED OF 155 KNOTS, IN DESCENT. MAINTENANCE INSPECTED AND FOUND NO INSPECTION IS REQUIRED FOR THIS DISCREPANCY PER THE EMB AMM, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (E&E BAY) · airframe 20,773 hrs · 19,444 cycles

ON APPROACH TO IAH THE FLIGHT CREW GOT "115 VAC FAIL" MESSAGE ON EICAS. DUE TO WIND SHEAR CONDITIONS THE AIRCRAFT DIVERTED TO BTR. MAINTENANCE INSPECTED AND RESET THE 115 VAC SYSTEM, CLEANED ELECTRICAL CONNECTOR AND SYSTEM OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 19,696 hrs · 18,476 cycles

DURING TAXI THE FLIGHT CREW GOT A LAVATORY SMOKE DETECTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESET THE LAVATORY SMOKE DETECTION SYSTEM. THE SYSTEM OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 18,692 hrs · 17,535 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBRICATED THE PASSENGER DOOR FRAME ROLLER. DOOR OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 18,662 hrs · 17,506 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY FLOOR LIGHT STRIP LOOSE AT THE GALLEY. MAINTENANCE INSPECTED AND SECURED THE EMERGENCY GLOW STRIP. SYSTEM OPS CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (COCKPIT) · airframe 18,557 hrs · 17,402 cycles

DURING FLIGHT THE FLIGHT CREW REPORTED THE AMBER WEATHER CAPTION ON THE MFD AND RADAR WAS NOT PAINTING ANY RETURNS. AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPECTED AND OPS CHECKED THE SYSTEM. OPS CHECKED GOOD.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 18,440 hrs · 17,296 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE FLOOR STRIP EMERGENCY LIGHTING INOP AT 12A. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE EMERGENCY LIGHTING SYSTEM INVERTER. SYSTEM OPS CHECKED GOOD.

Part: LINKAGE — BINDING (PAX DOOR) · airframe 17,818 hrs · 16,693 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR. DOOR OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,669 hrs · 16,561 cycles

DURING PRE-FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CHECKED GOOD.

Part: ATTACH FITTING — CRACKED (WG-BDY FAIRING) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT WING TO BODY FAIRING UPPER AFT STRIP IS CRACKED. R & R STIP. W/C 6010

Part: ATTACH FITTING — CRACKED (WING TO BODY) · airframe 17,578 hrs · 16,480 cycles

(V0XR) LT WING TO BODY FAIRING ATTACHMENT STRIP AT STA 17445.0 - 16143.5 IS CRACKED. REMOVED AND REPLACED STIP. W/C 5063

Part: ATTACH FITTING — CRACKED (WG-BDY FAIRING) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT UPPER WING TO BODY FAIRING ATTACHMENT STRIP AT STA 16143.0 - 14967.0 IS CRACKED. R & R STIP. W/C 6009

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) SEAT TRACK POSITION B BETWEEN FRAME 19-24 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2172

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RIGHT SILL SERVICE DOOR AT FRAME 19-20 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1084

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) CENTER FLOOR GUSSET AT FRAME 36-40 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2153

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) LT SILL AT FRAME 19-23L IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1077

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) SILL AT FRAME 36-42L IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1073

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) SERVICE DOOR SILL IS CORRODED BEYOND LIMITS. R & R SERVICE SILL. W/C 1074

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) GUSSET AT FRAME 17-18 Y0.0 - LY 479.0 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1087.

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) LT SILL AT FRAME 60-65S CORRODED OUT OF LIMITS. R & R ANGLE. W/C 2108

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) FWD DIGITAL PLATE AT FRAME 14-16 IS CORRODED OUT OF LIMITS. R & R DIGITAL PLATE. W/C 1086

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) LT GUSSET AT FRAME 59-61 LY-479.0S CORRODED OUT OF LIMITS. R & R ANGLE. W/C 2109

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) SUPPORT ANGLES AT FRAME 19-23 LY 0.0 IS CORRODED OUT OF LIMITS. R & R ANGLE. W/C 1116

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) CTR GUSSET AT FRAME 59-61 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1089

Part: DOUBLER — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) DOUBLER AT RY 479.0, FRAME 20-22 IS CORRODED OUT OF LIMITS. R & R DOUBLER. W/C 1083

Part: SILL — CORRODED (ZONE 800) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT SILL AT SERVICE DOOR AT FRAME 22-23 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1075

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT OMEGA BEAM AT RY 479.0 FRAME 19-25 IS CORRODED OUT OF LIMITS. R & R BEAM. W/C 1082

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT GUSSET AT FRAME 59-61 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1090

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) CTR GUSSET AT FRAME 19-23 Y0.0 IS CORRODED OUT OF LIMITS. R & R CTR GUSSET. W/C 1081

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) LT GUSSET FROM FRAME 23-29 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1058

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) GUSSET FROM FRAME 39-46 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1069

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) SCALLOPED ANGLE AT FRAME 23 BETWEEN CTR BEAM AND SILL IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1055.

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) ANGLE ON FRAME 23 RY780.0 POSITION CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1054

Part: FRAME — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) REPAIR AT FROM FRAME 20 IS CORRODED BEYOND LIMITS. R & R REPAIR. W/C 1076

Part: PROFILE — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) FLOOR SUPPORT ANGLE AT FRAME 19-20 LY 4790. IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE. W/C 1085

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) LT SILL FROM FRAME 23-29 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1057

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) FLOOR SUPPORT AT FRAME 19-20 IS CORRODED BEYOND LIMITS. R & R SUPPORT. W/C 1080

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(VOXR) SILL FROM FRAME 24-29 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 1056

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT SILL AT FRAME 41-48 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1067

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,578 hrs · 16,480 cycles

(V0XR) PAX DOOR ANGLE IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1078

Part: MOUNT — CORRODED (GALLEY) · airframe 17,578 hrs · 16,480 cycles

(V0XR) FWD GALLEY INBD MOUNTS ARE CORRODED BEYOND LIMITS. R & R FITTINGS. W/C 2085

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs

(V0XR) LT SILL AT FRAME 41-48 IS CORRODED BEYOND LIMITS. R & R LT SILL. W/C 1066.

Part: ANGLE — CORRODED (ZONE 600) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT WING LOWER WING TO FAIRING ATTACHMENT BRACKET IS CRACKED. R & R ANGLE. W/C 6008

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR)LT GUSSET AT FRAME 39-41 IS CORRODED BEYOND LIMITS. R & R LY GUSSET. W/C 1068

Part: SILL — CORRODED (ZONE 100) · airframe 17,578 hrs · 16,480 cycles

(V0XR) RT SILL AT FRAME 36-41 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1072

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,578 hrs · 16,480 cycles

(V0XR) PAX DOOR ANGLE IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1078

Part: STRIP — LOOSE (CABIN) · airframe 16,756 hrs · 15,692 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT STRIP LOOSE AT ROW 2A. MAINTENANCE INSPECTED AND RE-SECURED THE LIGHT STRIP. SYSTEM OPS CHECKED GOOD.

Part: DOOR — BINDING (CABIN) · airframe 16,725 hrs · 15,664 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. INSPECTED AND SERVICED THE PASSENGER DOOR. DOOR OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 16,725 hrs · 15,664 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY FLOOR LIGHT STRIP LOOSE. MAINTENANCE INSPECTED AND RE-SECURED LIGHTS.

Part: SEAL — DIRTY (PAX DOOR) · airframe 16,689 hrs · 15,634 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED, CLEANED AND LUBED THE DOOR SEAL. DOOR OPS CHECKED GOOD.

Part: SEAL — DEFECTIVE (PAX DOOR) · airframe 16,637 hrs · 15,589 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND DRILLED PRESSURIZATION HOLE IN PASSENGER DOOR SEAL. PASSENGER DOOR OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 16,630 hrs · 15,581 cycles

FLIGHT CREW REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR. DOOR OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 16,626 hrs · 15,575 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR SEAL AND ROLLERS. DOOR OPS CHECKED GOOD.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 16,622 hrs · 15,570 cycles

FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED FORWARD AND AFT ROLLERS. DOOR OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 16,618 hrs · 15,565 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED, CLEANED AND LUBED THE PASSENGER DOOR. OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 16,611 hrs · 15,559 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR HANDLE CATCHES HALFWAY THROUGH CYCLE. MAINTENANCE INSPECTED AND LUBRICATED PASSENGER DOOR SEAL. DOOR OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 16,611 hrs · 15,559 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR SEAL. DOOR OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 16,466 hrs · 15,429 cycles

DURING POST FLIGHT THE FLIGHT CREW REPORTED THE ESCAPE PATH LIGHTING STRIP LOOSE. MAINTENANCE INSPECTED AND RE-SECURED THE ESCAPE PATH LIGHTING STRIP. SYSTEM OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,016 hrs · 14,991 cycles

DURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THE LEFT OVERWING EXIT IDENTIFIER AS BEING INOPERATIVE. PRIOR TO FLIGHT, MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND FOUND THE CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RECONNECTED AND THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 14,805 hrs · 13,865 cycles

DURING INSPECTION, MAINTENANCE REPORTED THAT THE RIGHT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,804 hrs · 13,865 cycles

DURING THE PRE FLIGHT INSPECTION, MAINTENANCE FOUND THE RIGHT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE EMERGENCY LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,405 hrs · 13,493 cycles

CREW REPORTED THAT THE RIGHT OVERWING EMERGENCY EXIT LIGHT AS BEING INOPERATIVE. MAINTENANCE DEFERRED THE RIGHT OVERWING EMERGENCY EXIT LIGHT IAW MEL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,646 hrs · 12,807 cycles

PRE FLT 8043 - RIC - CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESET THE POWER TO THE EMERGENCY LIGHTING SYSTEM. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,646 hrs · 12,807 cycles

PRE FLT 8043 - RIC - EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE DURING FUNCTIONAL CHECK. MAINTENANCE RESET THE POWER TO THE EMERGENCY LIGHTING SYSTEM IAW AMM PROCEDURES FOR FUNCTIONAL CHECK OF THE LIGHTS. NO OTHER DEFECTS NOTED.

Part: DOOR — BINDS (PAX DOOR) · airframe 13,213 hrs · 12,442 cycles

POST FLT 7914 - ORD - F/A REPORTED THAT THE MAIN PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE DOOR AND FOUND NO DEFECTS WITH ITS OPERATION. THE PROBLEM COULD NOT BE DUPLICATED.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 13,181 hrs · 12,414 cycles

POST FLT 8024 - IAD - MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBED THE PAX DOOR ASSEMBLY. OPS CHECKED GOOD.

Part: DOOR — DIRTY (PAX DOOR)

FLT 7987 - RIC - PASSENGER DOOR DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE CLEANED AND LUBED THE PASSENGER DOOR. OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 13,119 hrs · 12,352 cycles

POST FLT 7886 - IAD - MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE DOOR SEAL. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 13,074 hrs · 12,311 cycles

POST FLT 7983 - IAD - MAIN PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE MAIN PASSENGER DOOR ROLLER PINS AND PERFORMED AN OPERATIONAL CHECK OF THE DOOR. NO DEFECTS NOTED.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 13,057 hrs · 12,292 cycles

FLT 7930 - ORD - HYD 1 SYSTEM QUANTITY APPEARS LOW. MAINTENANCE FOUND NR 1 HYD SYSTEM LOW. SERVICED SYSTEM IAW EMB 145 AMM PROCEDURE, OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 13,047 hrs · 12,284 cycles

POST FLT 7886 - IAD - FLIGHT ATTENDANT REPORTED THAT THE MAIN PASSENGER DOOR IS VERY HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND HINGES. OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: DOOR — BINDS (MAIN DOOR) · airframe 13,038 hrs · 12,277 cycles

POST FLT 8069 - IAD - MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE DOOR WITH NO DEFECTS NOTED.

Part: STOP FITTING — LOOSE (CABIN DOOR) · airframe 13,038 hrs · 12,277 cycles

POST FLT 7892 - IAD - MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND FOUND THE TOP DOOR STOP PAD ON FORWARD SIDE OF THE DOOR LOOSE. THE PAD WAS ADJUSTED, TIGHTENED AND THE LATCHES LUBED. DOOR OPS CHECKED GOOD.

Part: STRIP — LOOSE (CABIN) · airframe 12,780 hrs · 12,045 cycles

EMERGENY FLOOR LIGHT STRIP LOOSE AT 1A. LIGHT STRIP RESECURED IAW AMM MX PROCEEDURES.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,208 hrs · 11,554 cycles

DURING PRE FLIGHT INSPECTION, EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE LIGHT ASSEMBLY. LIGHT OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN/GALLEY)

EMERGENCY LIGHT STRIP AT GALLEY NOT SECURE. MAINT RESECURED THE LOOSE EMERGENCY LIGHT STRIP. OPS CHECKED GOOD. (K)

Part: TIRE — SEPARATED (RT MLG) · airframe 11,675 hrs · 11,051 cycles

FLT 7949 -DEN- CREW REPORTED FEELING VIBRATION AS GEAR WAS RETRACTED AND A FLAP FAIL MESSAGE AT 9 DEGREES. IN ADDITION, ON LANDING THE NR 1 BRAKE TEMP INDICATION SHOWED AN OVERHEAT. MAINTENANCE INSPECTED AND FOUND THE NR 2 MLG WHEEL`S TREAD SEPARATED. MAINTENANCE REMOVED AND REPLACED THE RT MLG WHEEL ASSEMBLIES AND THE NR 1 BRAKE ASSEMBLY. AN OPERATIONAL CHECK OF THE FLAP SYSTEM WAS GOOD. (S)

Part: UNKNOWN — SMOKE (CABIN) · airframe 10,319 hrs · 9,853 cycles

FLT NR 7948 - LGA - CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF ALL AIRCRAFT SYSTEMS WITH NO DEFECTS OR ODOR OF SMOKE. COULD NOT DUPLICATE THE CREW'S DISCREPANCY.

Part: PROXIMITY SWITCH — CONTAMINATED (SPOILER) · airframe 10,125 hrs · 9,668 cycles

FLT 7948 - IAD - CREW REPORTED A SPOILER FAIL MESSAGE ON THE EICAS. SPOILERS WERE INDICATED AS BEING OPEN. NO CONTROLLABILITY ISSUES REPORTED BY CREW. MAINTENANCE REMOVED GREASE RESIDUE FROM THE LT SPOILER PROX SWITCH. OPS CHECKED GOOD.

Part: PUMP — FAILED (NR 1) · airframe 8,287 hrs · 7,925 cycles

FLT NR 7901 - IAD - ELECTRIC HYDRAULIC PUMP NR 1 FAIL AFTER PUSHBACK. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRICAL HYDRAULIC PUMP, OPS CHECK GOOD.

Part: CARBON SEAL — LEAKING (NR 1 GENERATOR) · airframe 8,182 hrs · 7,817 cycles

FLT NR 8012-ORD-ENGINE NR 1 LOW OIL PRESSURE EICAS MESSAGE ENGINE NR 1 QUANITY LOW. MAINTENANCE REMOVED AND REPLACED NR 1 GENERATOR CARBON SEAL. NO LEAKS NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 8,039 hrs · 7,677 cycles

PRE FLT 7911 - MSN - EMERGENCY LIGHT ON PLUG DOOR HINGE IS OUT. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 7,955 hrs · 7,597 cycles

POST FLT NR 7950 - IAD - PHOTO ILLUMINESCENT STRIP CAME LOOSE AROUND ROW 10. MAINTENANCE SECURED STRIP, CHECK GOOD.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 7,704 hrs · 7,342 cycles

FLT NR 8024 - PVD - FO DV WINDOW WOULD NOT COMPLETELY CLOSE, ABORTED T/O AT 40-50KTS. MAINTENANCE INSPECTED THE WINDOW AREA FOR POSIBLE DEBRIS. INSPECTED WINDOW AND ASSOCIATED LINK. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,402 hrs · 7,037 cycles

PRE FLT NR 8035 - MDT - EMERGENCY LIGHTS INOP IN FWD CABIN. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 7,381 hrs · 7,015 cycles

PRE FLT NR 7983 - IAD - EMERGENCY LIGHTS INOP IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY FOR THESE LIGHTS.

Part: LIGHT — LOOSE (CABIN) · airframe 5,038 hrs · 4,743 cycles

PRE-FLIGHT 7994 - RIC - ESCAPE PATH LIGHTING NEXT TO GALLEY LOOSE. MAINTENANCE RESECURED LIGHT STRIP.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 1,007 hrs · 901 cycles

ORD - BAGGAGE DOOR WARNING CAME ON AT 35,600 FT. MAINTENANCE PLACED DOOR WARNING SYSTEM ON DEFERRAL PER MEL.

Part: LINE — LOOSE (PRESS CONTROLLER) · airframe 185 hrs · 162 cycles

AUTO AND MANUAL PRESSURIZATION INOP. MAINTENANCE SECURED LOOSE LINE IN PRESSURIZATION CONTROLLER.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 161 hrs · 141 cycles

8000-STL- LEFT ELECTRIC HYDRAULIC PUMP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRIC HYD PUMP.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 5,429 hrs · 4,696 cycles

RIC- ANGLE OF ATTACK NR 1 FAIL INDICATION. MAINTENANCE RERACKED STALL PROTECTION COMPUTER.