N809HK

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,077 hrs · 32,018 cycles

MAIN DOOR HAND RAIL EMERGENCY EXIT LIGHT NR 1 INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 33,636 hrs · 31,567 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,630 hrs · 31,561 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,291 hrs · 30,271 cycles

RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 32,268 hrs · 30,245 cycles

PITCH TRIM MAIN INOPERATIVE EICAS MESSAGE ON CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT, OPS CHECK GOOD.

Part: CONNECTOR — DAMAGED (NLG WOW) · airframe 32,195 hrs · 30,167 cycles

AIR GROUND FAIL EICAS MESSAGE DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED THE NLG WOW PROXIMITY SWITCH CONNECTOR, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,116 hrs · 30,092 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,941 hrs · 29,930 cycles

LEFT AND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,703 hrs · 29,717 cycles

PASSENGER DOOR U-SHAPES CORRODED. MAINTENANCE REPLACED PASSENGER DOOR U-SHAPES.

Part: SILL — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 31,703 hrs · 29,717 cycles

LEFT SILL AFT OF PASSENGER DOOR HAS CORROSION. MAINTNENACE REPLACED LEFT SILL AFT OF PASSENGER DOOR.

Part: CHANNEL — CORRODED (CARGO RAMP) · corrosion level 2 · airframe 31,703 hrs · 29,717 cycles

CARGO RAMP ZEE CHANNEL IS CORRODED. MAINTENANCE REPLACED THE CHANNEL.

Part: CONNECTOR — CORRODED (SPOILERS) · airframe 31,316 hrs · 29,345 cycles

SPOILER FAIL MESSAGE IN FLIGHT, SPOILERS SHOW OPEN ON GROUND. MX REPLACED CONNECTOR AT RT INBD SPOILER PROXIMITY SWITCH, OPS CHECK GOOD.

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 30,801 hrs · 28,870 cycles

DURING POST FLIGHT INSPECTION, THE FLIGHT CREW FOUND THE PASSENGER DOOR HARD TO OPEN. MX INSPECTED AND ADJUSTED THE PASSENGER DOOR LOCKING MECHANISM. DOOR OPS CHECKED GOOD.

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 30,732 hrs · 28,810 cycles

DURING POST FLIGHT INSPECTION, CREW FOUND PASSENGER DOOR HANDLE STUCK. MX INSPECTED AND ADJUSTED THE PASSENGER DOOR LINKAGE. DOOR OPS CHECKED GOOD.

Part: FIXTURE — DEFECTIVE (CABIN) · airframe 30,499 hrs · 28,599 cycles

DURING SCHEDULED MAINTENANCE THE RH OVERWING EMERGENCY EXIT LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT FIXURE. LIGHT OPS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (OVERWING EXIT) · airframe 30,449 hrs · 29,599 cycles

DURING SCHEDULED MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT FIXTURE. LIGHT OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,874 hrs · 27,046 cycles

DURING MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REPLACED BULB IN RIGHT OVERWING LIGHT, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,543 hrs · 26,740 cycles

FLIGHT CREW NOTED THAT EMERGENCY LIGHT STRIP AT 2A IS MISSING. MAINTENANCE DEFERRED MISSING EMERGENCY LIGHT STRIP AT 2A, OPS CHECK GOOD.

Part: SHAFT — OUT OF ALIGNMENT (PAX DOOR) · airframe 27,866 hrs · 26,147 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WON'T OPEN FROM THE INSIDE. MAINTENANCE INSPECTED AND RE-ALIGNED LOCK BOX ACTUATOR SHAFT. DOOR OPS CHECKED GOOD.

Part: ARM — OUT OF ADJUST (PAX DOOR) · airframe 27,859 hrs · 26,142 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED THE AIRCRAFT FOR A FERRY FLIGHT TO STL. MAINTENANCE IN STL INSPECTED AND REMOVED THE PASSENGER DOOR INTERNAL HANDLE AND RE-INDEXED THE STRIKER ARM AND ROLLER. RE-INSTALLED THE INTERNAL HANDLE AND THE DOOR OPS CHECKED GOOD.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 27,778 hrs · 26,070 cycles

DURING CLIMB THE FLIGHT CREW GOT A E1 BLEED LEAK MESSAGE ON EICAS. AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BLEED DUCT O-RINGS AT CONNECTION NR 19. SYSTEM LEAK AND OPS CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 26,786 hrs · 25,189 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED AND LUBRICATED THE PASSENGER DOOR ACTUATING LOCK MECHANISM. DOOR OPS CHECKED GOOD.

Part: AHRS — MALFUNCTIONED (E&E BAY) · airframe 26,697 hrs · 25,112 cycles

DURING CLIMB THE FLIGHT CREW GOT A PITCH COMPARISON ERROR. AIRCRAFT RETURNED TO STL. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 1 AHRS. SYSTEM OPS CHECKED GOOD.

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 26,597 hrs · 25,024 cycles

DURING FLIGHT CREW INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN FROM THE INSIDE. AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE INSPECTED AND ADJUSTED PASSENGER DOOR LINKAGE. DOOR OPS CHECKED GOOD.

Part: CABLE — LOOSE (PAX DOOR) · airframe 26,591 hrs · 25,020 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. AIRCRAFT WAS FERRIED FROM LGA TO STL. MAINTENANCE INSPECTED AND FOUND THE DOOR CABLES LOOSE. MAINTENANCE RE-RIGGED THE PASSENGER DOOR CABLES. DOOR OPS CHECKED GOOD.

Part: WIRE — BROKEN (PAX DOOR) · airframe 26,217 hrs · 24,688 cycles

DURING MAINTENANCE INSPECTION THE PASSENGER DOOR HANDRAIL EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE INSPECTED AND REPAIRED A BROKEN WIRE.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

B-ROW NR 5 SEAT TRACK CORRODED AROUND SCREW HOLES, FR 46-53. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK AT ROW B NR 5 BETWEEN FR 46-53 IAW EMB145 AMM 53-01-06. W/C 2125

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

B-ROW NR 4 SEAT TRACK CORRODED AROUND SCREW HOLES, FR 36-45. INSTALLED NEW SEAT TRACK B NR 4 FROM FR 36-45 IAW EMB145 AMM 53-01-06. W/C 2126

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

B-ROW NR 6 SEAT TRACK CORRODED AROUND SCREW HOLES, FR 54-59. REMOVED AND REPLACED SEAT TRACK B-6 AT FR 54-59 IAW EMB145 AMM 53-01-06. W/C 2124

Part: FITTING — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

(V0XR) FWD GALLEY ALL FOUR SUPPORT FITTINGS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR FITTINGS. W/C 2176

Part: FITTING — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

(V0XR) FWD GALLEY ALL FOUR SUPPORT FITTINGS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR FITTINGS. W/C 2176

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

SEAT TRACK B ROW NR 1 SEAT AT FR 19-24 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK. W/C 2129

Part: FITTING — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

(V0XR) FWD GALLEY ALL FOUR SUPPORT FITTINGS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR FITTINGS. W/C 2176

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

SEAT TRACK A ROW NR 6 SEAT AT FR 53-59 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK. W/C 2134

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK C ROW NR4 CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK B ROW NR2 FR 24-29 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK A ROW NR5 FR 47-53 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK C ROW NR 5 CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK A ROW NR4 FR 36-45 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: ROLLER — CORRODED (RT WING TE FLAP) · airframe 26,114 hrs · 24,597 cycles

FLAP ROLLERS AND PLUNGERS WORN BEYOND LIMITS. R & R (6) FLAP ROLLERS.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK B ROW NR 3 FR 30-35 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK A ROW NR1 CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK A ROW NR3 FR 30-350 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SEAT TRACK C ROW NR1 FR 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CARBON FIBER FLOOR SUPPORT AT FR 20 IS DAMAGED BEYOND LIMITS. R & R SUPPORT.

Part: BUSHING — CORRODED (ATTACH FITTING) · airframe 26,114 hrs · 24,597 cycles

HORIZONTAL ACTUATOR ATTACHMENT HARDWARE IS CORRODED BEYOND LIMITS. R & R (2) BUSHINGS.

Part: BEAM — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RT HAT CHANNEL BEAM AT FR 18 - 25 IS CORRODED BEYOND LIMITS. R & R BEAM.

Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT AFT WING-BODY ATTACHMENT CRACKED. R & R STRIP.

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT OMEGA BEAM AT FR 24 IS DAMAGED BEYOND LIMITS. R & R BEAM.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL AT FR 60-65 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: BUSHING — CORRODED (ATTACH FITTING) · airframe 26,114 hrs · 24,597 cycles

HORIZONTAL ACTUATOR ATTACHMENT HARDWARE IS CORRODED BEYOND LIMITS. R & R (4) BUSHINGS.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CENTER GUSSET AT FR 40-46 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: PROFILE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT INBD PROFILE AT FR 61 IS CORRODED BEYOND LIMITS. R & R PROFILE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CENTER GUSSET AT FR 36-40 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SUPPORT BRACKET — CORRODED (CARGO DOOR) · airframe 26,114 hrs · 24,597 cycles

BAGGAGE COMPARTMENT DOOR ASSIST HANDLE SUPPORT BRACKET CRACKED. R & R SUPPORT.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL AT FR 36-41 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL AT FR 48-52 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL AT FR 41-48 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL AT FR 41-49 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL AT FR 48-52 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT GUSSET AT FR 40-46 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

FWD DIGITAL PLATE FR 14-16 IS CORRODED BEYOND LIMITS. R & R DIGITAL PLATE.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SILL AT RY 780.0 FR 29-35 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL FR 59-60 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: PROFILE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT PROFILE FR 17 - 18 IS CORRODED BEYOND LIMITS. R & R PROFILE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

OMEGA BEAM REPAIR AT LY 479.0 FR 20 IS CORRODED BEYOND LIMITS. R & R REPAIRED BEAM.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT GUSSET FR 36-41 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

GUSSET AT Y0.0 FR 24-29 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT GUSSET FR 46-52 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

GUSSET AT Y0.0 FR 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: PROFILE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT PROFILE FR 16 INBD OF PAX DOOR CORRODED BEYOND LIMITS. R & R PROFILE.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CARGO DOOR TORSION BAR FWD BRACKET CRACKED. R & R SUPPORT ASSY.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT GUSSET FR 53-59 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

HORSESHOE SHAPED GUSSET FR 16-18 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL FR 53-59 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT FWD GUSSET FR 19-23 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SUPPORT BEAMS AT Y0.0 AND RY 479.0 CORRODED BEYOND LIMITS. R & R BEAM.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL FR 59-60 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

FLOOR SUPPORT ANGLE AT Y0.0 FR 18-20 IS CORRODED BEYOND LIMITS. R & R ANGLE.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT SILL FR 60-65 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

GUSSET AT LY 479.00 FR 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL FR 36-41 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT CTR GUSSET FR 46-52 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SHAPE AT LY-479.0 FR 16 IS CORRODED BEYOND LIMITS. R & R SHAPE.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 26,114 hrs · 24,597 cycles

RT AFT WHEEL WELL BULKHEAD CRACKED. R & R RIB.

Part: PROFILE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT PROFILE AT FR 22 LY-479.0 - OTBD LT SILL IS CORRODED BEYOND LIMITS. R & R PROFILE.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT SILL FWD OF SERVICE DOOR AT FR 18-20 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CENTER GUSSET AT FR 18 - 23 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: PARTITION — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RIGHT LOWER PARTITION IS CORRODED BEYOND LIMITS. R & R PARTITIAN.

Part: STRUCTURE — BROKEN (WNG-BDY FAIRING) · airframe 26,114 hrs · 24,597 cycles

LEFT PAX EXHAUST DUCT ON BODY FAIRING BROKEN. R & R GRATE ASSY.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SILL CORRODED AT LY 780.0 FR 24-29. R & R SILL AT FRAME 24-29 AND LY 780.0, LH.

Part: SHROUD — WORN (LT WING TE FLAP) · airframe 26,114 hrs · 24,597 cycles

LT OTBD FLAP INBD AND OTBD FLAP DRIVERS ARE WORN OUT. R & R LT OTBD FLAP INBD AND O/D FLAP DRIVER SHROUDS IAW AMM 25-50-00. (PN'S 145-68246-001 AND 145-68249-001).

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

AFT WHEEL WELL BULKHEAD LT SIDE CRACKED ON BOTTOM. R & R AFT WHEEL WELL BULKHEAD LT SIDE AND INSTALLED FASTENERS WET WITH SEALANT IAW SRM 51-40-02, 51-10-02, AND 51-40-09.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SERVICE DOOR SILL IS CORRODED OUT OF LIMITS. R & R SERVICE DOOR SILL IAW SRM 51-10-02, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

CENTER HAT CHANNEL BEAM AT FR 18-25 IS CORRODED OUT OF LIMITS. REMOVED, LOCATED, DRILLED AND REPLACED CTR OMEGA BEAM IAW SRM 51-40-07 AND 51-40-00.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

BOTH DOUBLERS AT FR 20 AND 22 RY 479.0 ARE CORRODED BEYOND LIMITS. REMOVED LOCATED, DRILLED, AND REPLACED 2 EA DOUBLERS IAW SRM 51-40-00 AND 51-40-07.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RT SILL AFT OF SERVICE DOOR AT FR 22-23 IS CORRODED BEYOND LIMITS. R & R RT SILL AFT OF SERVICE DOOR AT FR 22-23 IAW SRM 51-40-02.

Part: PROFILE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LEFT OTBD PROFILE AT FR 61 IS CORRODED OUT OF LIMITS. R & R LT OTBD PROFILE AT FR 61 IAW SRM 51-10-02, 51-40-02, 51-21-04, 51-21-05.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LT SILL AT FR 18-23 IS CORRODED OUT OF LIMITS. R & R LT SILL AT FR 18-23 IAW SRM 51-40-02, 51-20-03, 51-10-02.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

LT SILL AT FR 53-59 IS CORRODED OUT OF LIMITS. R & R LT SILL AT FR 53-59 IAW SRM 51-10-02, 51-40-02, 51-20-03.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RT SILL FR 24-29 CORRODED BEYOND LIMITS. R & R RT SILL AT FR 24-29 IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

"U" CHANNELS UNDER PASSENGER DOOR THRESHOLD ARE CORRODED BEYOND LIMITS. R & R "U" CHANNELS WITH NEW PARTS (PN'S 145-24131-009 AND -011) IAW SRM 51-10-02, 51-40-02, 51-20-03.

Part: SILL — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

RT SILL FWD OF SERVICE DOOR AT FR 18-20 IS CORRODED OUT OF LIMITS. R & R SILL AT FR 18-20 IAW SRM 51-10-02, 51-20-03, 51-40-02.

Part: ANGLE — CORRODED (ZONE 100) · airframe 26,114 hrs · 24,597 cycles

SCALLOPED ANGLE AT FR 24 AND Y 0.0 IS CORRODED BEYOND LIMITS. R & R ANGLE AT FR 24 AND Y 0.0 TO RY 780.0 IAW SRM 51-10-02, 51-20-03 AND 51-40-02.

Part: SILL — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

SILL LY 780.0 AT FR 29-35 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

LEFT GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

RIGHT GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

CENTER GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: GUSSET — CORRODED (ZONE 100) · airframe 23,114 hrs · 24,597 cycles

LEFT L/E NR3 OTBD COMPOSITE BROKEN. R & R GUSSET.

Part: ANGLE — CRACKED (ZONE 600) · airframe 26,114 hrs · 24,597 cycles

RT NR 3 BOTTOM WING-BODY ANGLE CRACKED. R & R ANGLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,950 hrs · 24,458 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCT EXIT LIGHT BY THE GALLEY DOOR WAS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 25,607 hrs · 24,132 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT IN THE COCKPIT WAS INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE EMERGENCY FLOOD LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD.

Part: FUEL NOZZLE — DIRTY (APU) · airframe 25,536 hrs · 24,063 cycles

DURING DESCENT THE FLIGHT CREW REPORTED FUEL SMELL IN THE COCKPIT COMING FROM THE APU BLEED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED APU FUEL NOZZLES. SYSTEM OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 25,500 hrs · 24,023 cycles

DURING FLIGHT THE FLIGHT CREW GOT A RUDDER SYSTEM 1 AND 2 INOP INDICATION. AIRCRAFT RETURNED FROM FLIGHT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RUDDER NR 2 PRESSURE SWITCH. SYSTEM OPS CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (MAIN DOOR) · airframe 24,258 hrs · 22,842 cycles

DURING THE GROUND HANDLING, THE CREW REPORTED THAT THE MAIN DOOR MECHANISM HAD BECOME INCREASINGLY DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBED THE DOOR HANDLE MECHANISM AND THE DOOR SEAL. FOLLOW ON OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,245 hrs · 22,826 cycles

WHILE IN CLIMB, THE CREW REPORTED A STRONG SMELL OF FUEL WITH PACKS RUNNING ON APU BLEED AFTER TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE APU BLEED SYSTEM WITH NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,243 hrs · 22,824 cycles

DURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE MID CABIN CEILING EMERGENCY LIGHT AS BEING INOPERATIVE. PRIOR TO FLIGHT, MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. FOLLOW-ON OPERATIONAL CHECK OF THE LIGHTS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,212 hrs · 22,796 cycles

PRIOR TO FLIGHT, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT STRIP AS BEING INOPERATIVE. MAINTENANCE RE-SECURED THE CONNECTOR TO THE LIGHT ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.

Part: CONNECTOR — WORN (LT MLG) · airframe 24,116 hrs · 22,705 cycles

DURING TAKEOFF CLIMB, THE CREW REPORTED RECEIVING A LANDING GEAR AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE CONNECTION ON THE LT MAIN LANDING GEAR AT THE FORWARD WOW SWITCH. OPS CHECK OF THE EXTENSION AND RETRACTION SYSTEM WAS GOOD FOLLOWING THE REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,805 hrs · 22,401 cycles

DURING THE PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE SERVICE DOOR AS BEING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 23,589 hrs · 22,209 cycles

CREW REPORTED THE MAIN PITCH TRIM TO BE INOPERATIVE DURING CRUISE FLIGHT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT IAW AMM PROCEDURES. PITCH TRIM OPERATIONALLY CHECKED GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 22,998 hrs · 21,665 cycles

CREW REPORTED A STRONG FUEL SMELL FROM THE APU BLEED AFTER TAKEOFF THAT WENT AWAY AFTER SWITCHING TO THE ENGINE BLEED SYSTEM. MAINTENANCE INSPECTED THE AIRCRAFT AND DEFERRED THE APU IAW EMB145 MEL PROCEDURES.

Part: BALLAST — OVERHEATED (CABIN) · airframe 22,760 hrs · 21,440 cycles

AT CRUISE ALTITUDE, THE CREW REPORTED A BURNING PLASTIC SMELL IN THE AREA OF SEAT 2A (GALLEY AREA). UPON INSPECTION BY MAINTENANCE, THE LIGHT BALLAST WAS FOUND TO BE OVERHEATING. MAINTENANCE REMOVED POWER TO THE LIGHT ASSEMBLY AND DEFERRED THE LIGHT BALLAST AS PER THE NEF PROGRAM.

Part: A/C PACK — MALFUNCTIONED (NR 1) · airframe 22,352 hrs · 21,054 cycles

FLT 7928 - CHS - PAC NR 1 OVERLOAD MESSAGE. MAINTENANCE DEFERRED NR 1 PAC.

Part: CONNECTOR — LOOSE (CABIN) · airframe 22,195 hrs · 20,911 cycles

EMERGENCY LIGHT FLOOR STRIP AT ROW 1 INOPERATIVE. MAINTENANCE RESTORED THE CONNECTION TO THE LIGHT STRIP. THE EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 22,062 hrs · 20,797 cycles

DURING INSP, MX DISCOVERED THAT THE OVERHEAD EMERGENCY LIGHT AT ROW 7 TO BE INOPERATIVE. MX REMOVED AND REPLACED THE CONNECTOR PLUG AT THE LIGHT ASSY IAW MM PROCEDURES. OPS CHECK OF THE LIGHTS WAS SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,029 hrs · 17,928 cycles

FLT 7907 - CVG - MAINTENANCE DEFERRED AIRSTAIRS LIGHT PER EMB 145 MEL PROCEDURE.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 21,557 hrs · 20,352 cycles

FLT 7888 - ORD - NR 1 ENGINE T/R DISAGREE MESSAGE ON TAKEOFF. MAINTENANCE DEFERRED NR 1 THRUST REVERSER IAW EMB 145 MEL PROCEDURE.

Part: THRUST REVERSER — MALFUNCTIONED (NR 1) · airframe 21,481 hrs · 20,287 cycles

FLT 5530 - STL - NR 1 ENG THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED NR 1 THRUST REVERSER PER EMB 154 MEL PROCEDURE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,462 hrs · 20,270 cycles

FLT 7934 - ORD - EMERGENCY LIGHT INOP AT SERVICE DOOR, FLOOD LIGHT. MAINTENANCE REMOVED AND REPLACED BULBS IAW EMB 145 AMM OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 21,239 hrs · 20,063 cycles

NR 1 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE DEFERRED NR 1 THRUST REVERSE IAW MEL PROCEDURES.

Part: SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 21,354 hrs · 20,172 cycles

NR 1 TR DISAGREE ON T/O. MX DEFERRED IAW MEL MX PROCEEDURE. MX CLEARED DMI, RESHIMMED UPPER OTBD STOW SWITCH IAW AMM MX PROCEEDURE.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 21,354 hrs · 20,172 cycles

NR 1 T/R DISAGREE ON T/O. MAINT DEFERRED T/R IAW MEL MX PROCEDURE.

Part: THRUST REVERSER — UNWANTED DEPLOY (NR 1 ENGINE) · airframe 21,354 hrs · 20,172 cycles

NR 1 THRUST REVERSER DEPLOYED ON TAKEOFF. NR 1 THRUST REVERSER PLACED ON DEFERRAL IAW MEL MX PROCEDURE.

Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 21,346 hrs · 20,166 cycles

EMERGENCY LIGHT ON STAIRS INOP. DEFER EXTERNAL EMERGENCY LIGHT ON AIRSTAIRS PER MX MEL PROCEDURE.

Part: LIGHT — OUT OF ADJUST (COCKPIT) · airframe 21,287 hrs · 20,109 cycles

DURING PRE FLIGHT INSPECTION, THE COCKPIT ENTRY EMERGENCY LIGHT WAS FOUND TO INOPERATIVE. MAINTENANCE ADJUSTED THE LIGHT ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.

Part: CABLE — WORN (PAX DOOR) · airframe 21,171 hrs · 19,998 cycles

PASSENGER DOOR WOULD NOT OPEN FROM INSIDE THE AIRCRAFT (NO PASSENGERS ONBOARD). MAINTENANCE REMOVED AND REPLACED THE INNER PASSENGER DOOR HANDLE CABLE. DOOR OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 21,122 hrs · 19,960 cycles

DURING CLIMB FROM TAKEOFF, CREW RECEIVED AN AIR/GROUND FAIL MESSAGE ON THE EICAS AND GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND FOUND THAT THE LT MLG WOW PROXIMITY SENSOR REQUIRED ADJUSTMENT. ADJUSTMENT WAS MADE AND LANDING GEAR SYSTEM, OPS CHECKED GOOD.

Part: O-RING — WORN (NLG) · airframe 21,116 hrs · 19,949 cycles

DURING CLIMB, CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAKING O-RING ON THE NLG SERVICING PORT. THE O-RING WAS REPLACED, NLG WAS SERVICED, AND AN OPERATIONAL CHECK OF THE EXTENSION AND RETRACTION SYSTEM WAS PERFORMED. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,937 hrs · 19,791 cycles

DURING PRE FLIGHT INSPECTION THE OVERHEAD EMERGECNY EXIT LIGHT AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,872 hrs · 19,732 cycles

POST FLIGHT, SMOKE COULD BE SEEN COMING FROM THE READING LIGHT AT SEAT 12A. MAINTENANCE REMOVED THE BULB FROM THE LIGHT ASSEMBLY AND DEFERRED THE LIGHT ASSEMBLY.

Part: UNKNOWN — SMOKE (CABIN) · airframe 19,616 hrs · 18,571 cycles

FLT 8061 -ORD- SMOKE IN THE CABIN. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AIRCRAFT LIGHTING AND THE BLEED AIR SYSTEM WITH NO DEFECTS NOTED.

Part: TERMINAL — BROKEN (CABIN) · airframe 19,559 hrs · 18,514 cycles

PRE FLT 5511 - STL - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE INSPECTED AND FOUND A BROKEN TERMINAL END. TERMINAL WAS REPAIRED AND THE SYSTEM, OPS CHECKED GOOD.

Part: UPLOCK — MALFUNCTIONED (LT MLG) · airframe 19,481 hrs · 18,433 cycles

FLT 5502 - STL - YAW DURING LANDING GEAR EXTENSION. LEFT MAIN INDICATED IN TRANSIT FOLLOWED BY A LANDING GEAR DISAGREE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE LT MLG UPLOCK BOX. SYSTEM OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 19,361 hrs · 18,319 cycles

PRE FLT 7969 - STL - OVERWING EMERGENCY EXIT LIGHTS AND FLOOR STRIP LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY. A SUCCESSFUL OPERATIONAL CHECK OF THE SYSTEM WAS COMPLETED AFTERWARDS.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 19,197 hrs · 18,174 cycles

PRE FLT NR 7982 - IAD - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR AT THE LIGHT ASSEMBLY. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,991 hrs · 17,987 cycles

POST FLT NR 3501 - PIT - MAIN DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT, OPS CHECK GOOD AT THIS TIME.

Part: SEAL — LEAKING (BLEED AIR SYS) · airframe 18,936 hrs · 17,940 cycles

FLT NR 8092 - ROC - BLEED LEAK 1 MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED BLEED AIR SEAL AT AFT FUSELAGE LOWER FAIRING, PERFORMED ENGINE GROUND RUN, NO LEAKS NOTED, NO LEAK MESSAGE NOTED.

Part: O-RING — BLOWN (BLEED AIR SYS) · airframe 18,933 hrs · 17,938 cycles

FLT NR 7927 - ROC - NR 1 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED CROSS BLEED TUBE COUPLING O-RINGS, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,780 hrs · 17,798 cycles

PRE FLT NR 3558 - PIT - AIRSTAIR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT AND OPS CHECK GOOD.

Part: INVERTER — NO TEST (EMERGENCY LIGHT) · airframe 17,939 hrs · 17,057 cycles

POST FLT NR 5561 - STL - EMERGENCY LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED NR 5 EMERGENCY INVERTER, SYSTEM CHECKS GOOD.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 17,698 hrs · 16,835 cycles

FLT NR 5469 - STL - VISIBLE SMOKE IN COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE APU OIL WAS OVERSERVICED. MAINTENANCE DRAINED THE OIL AND OPS CHECKED THE BLEED SYSTEM. OPS CHECKED GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYS) · airframe 17,525 hrs · 16,663 cycles

FLT NR 5565 - STL - LEFT INBOARD BRAKE DRAGGING DURING TAXI. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE AND THE NR 2 BRAKE. OPERATIONAL CHECK GOOD.

Part: GROUND WIRE — LOOSE (CABIN) · airframe 17,442 hrs · 16,588 cycles

PRE FLT NR 5517 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE FOUND GROUND WIRE LOOSE, SECURED GROUND WIRE AND LIGHT STRIP OPS NORMAL.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 17,399 hrs · 16,551 cycles

POST FLT NR 5524-STL-PAX DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED DOOR FRAME AND INSPECTED MAIN PAX DOOR .

Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE) · airframe 16,583 hrs · 15,785 cycles

PRE FLT NR 5462 - STL - ENGINE 1 FIRE DETECTION FAIL IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR LOOP. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 16,550 hrs · 15,760 cycles

PRE FLT NR 5566 - RIC - FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY IAW MM PROCEDURES.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 16,533 hrs · 15,744 cycles

PRE FLT NR 5579 - STL - EMERGENCY LIGHTS WILL NOT ILLUMINATE AFTER BEING LEFT ON WITH AIRCRAFT POWER OFF. MAINTENANCE RESET THE EMERGENCY LIGHT POWER FOLLOWED BY REMOVING AND REPLACING THE EMERGENCY LIGHT POWER SUPPLIES. OPS CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL PROTECTION) · airframe 16,454 hrs · 15,673 cycles

FLT NR 5450 - STL - SPS 2 FAIL ON EICAS ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REINSTALLED THE STALL PROTECTION COMPUTER, ALIGNED THE AOA VANES TO MATCH AND PERFORMED A STALL PROTECTION TEST. SYSTEM CHECKED GOOD.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 16,196 hrs · 15,427 cycles

FLT NR 5511-STL-LANDING GEAR WOULD NOT RETRACT. LG/LEVER DISAGREE RAN CHECKLIST AND RETURNED TO STL. MAINTENANCE REMOVED AND REPLACED NOSE GEAR WOW PROXIMITY SWITCH. PERFORMED GEAR SWING WITH NO DEFECTS NOTED.

Part: CONTROL CABLE — WORN (AILERONS) · airframe 16,167 hrs · 15,404 cycles

DURING A FLEET WIDE INSPECTION OF THE AILERON CONTROL CABLES, THE RT AILERON CONTROL CABLE WAS FOUND TO BE WORN AT THE POINT WHERE IT TRANSITIONS FROM THE PRESSURIZED VESSEL TO THE WING ROOT (PRESSURE SEAL). MAINTENANCE REMOVED AND REPLACED THE CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,977 hrs · 15,239 cycles

PRE FLIGHT 5575 - STL - EMERGENCY LIGHTS DIM AT ROWS 8 - 12. MAINTENANCE REPLACED THE ESCAPE PATH LIGHTING STRIP.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 15,799 hrs · 15,089 cycles

FLT 5458 - OUTBD BRAKE INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE.

Part: HANDLE — MALFUNCTIONED (PX DOOR) · airframe 15,151 hrs · 14,486 cycles

PRE FLIGHT NR 5578 - TUL - LT FWD PASSENGER DOOR WILL NOT CLOSE AND LOCK WITH THE OUTSIDE HANDLE. MAINTENANCE REMOVED AND REPLACED THE DOOR HANDLE.

Part: ODOR — DETECTED (CABIN) · airframe 14,845 hrs · 14,218 cycles

FLT NR 5562 - OKC - CREW REPORTED BURNING SMELL FROM OVERHEAD, ROW 16, RIGHT SIDE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE LIGHTING SYSTEM. NO DEFECTS NOTED. COULD NOT DUPLICATE.

Part: AIRSTAIR — INOPERATIVE (PAX DOOR) · airframe 14,752 hrs · 14,141 cycles

PRE-FLIGHT 5564 - OKC - MAIN DOOR STEPS WILL NOT COME DOWN. MAINTENANCE REMOVED AND REPLACED THE STEP ACTUATING ARM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,266 hrs · 13,739 cycles

PRE-FLIGHT INSPECTION -STL - EMERGENCY LIGHT STRIP OUT IN ONE SECTION. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY LIGHT STRIP.

Part: COMPUTER — MALFUNCTIONED · airframe 14,014 hrs · 13,513 cycles

FLT 3571 - PIT - AT 20 KTS ON TAKEOFF ROLL RECEIVED CHECK IC 2 CAUTION MESSAGE ON EICAS. MAINTENANCE RERACKED IC 600 CPU.

Part: DAU — INOPERATIVE (NR 2) · airframe 13,226 hrs · 12,801 cycles

FLT 3535 - PIT - SPS NR 2 INOP AND DAU NR 2 WARNING MESSAGE DISPLAYED ON EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 DAU AND OPS CHECKED GOOD.

Part: DAU — MALFUNCTIONED (NR 2) · airframe 11,554 hrs · 11,201 cycles

AVP - NR 2 GENERATOR OVERLOAD, ICE DETECT FAIL, YAW DAMPENER FAIL, AND APU BLEED LEAK MESSAGE. MAINTENANCE DEFERRED AUTO PILOT MEL 22-10-00, APU PER MEL 28-22-01 AND GROUND RAN NR 2 ENGINE. REMOVED AND REPLACED DAU.

Part: O-RING — LEAKING (CABIN AIR) · airframe 10,742 hrs · 10,346 cycles

3515 - PIT- DURING TAXI NR 2 LEAD LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT O-RING IN DISTRIBUTION DUCT AFT AVIONICS BAY.

Part: DUCT — LOOSE (NR 1 ENGINE) · airframe 10,631 hrs · 10,230 cycles

ERI - BLEED AIR LEAK INDICATION NR 1 ENGINE. MAINTENANCE RE-SECURED BLEED AIR DUCT.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 10,626 hrs · 10,224 cycles

PIT - MAIN DOOR OPEN MESSAGE ON TAKEOFF ROLL. MAINTENANCE PLACED DOOR INDICATING ON DEFERRAL PER MEL.

Part: SWITCH — INOPERATIVE (BLEED VALVE) · airframe 10,389 hrs · 9,983 cycles

UNABLE TO CROSS START - CROSS BLEED VALVE WOULD NOT OPEN. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH.

Part: SHOULDER BELT — INOPERATIVE (COCKPIT) · airframe 8,795 hrs · 8,352 cycles

FIRST OFFICERS SHOULDER HARNESS WILL NOT RETRACT OR EXTEND. MAINTENANCE REMOVED AND REPLACED SHOULDER HARNESS.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 8,442 hrs · 7,976 cycles

5324-RIC- PITCH TRIM NR 2 FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT.

Part: O-RING — LEAKING (BLEED SYSTEM) · airframe 7,924 hrs · 7,409 cycles

5286 DTW DURING TAKE-OFF NR 1 BLEED LEAK LIGHT CAME ON. MAINTENANCE DEFERRED PER MEL 49-52-2, SUBSEQUENTLY CLEARING DMI BY REPLACING O-RING IN LEFT BLEED LINE.

Part: O-RING — LEAKING (BLEED AIR) · airframe 7,522 hrs · 6,964 cycles

PIT- LT BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT LT BLEED LINE COUPLING.

Part: O-RING — BROKEN (HYD PUMP) · airframe 7,474 hrs · 6,912 cycles

ELM - RIGHT ENGINE LOW OIL PRESSURE, SHUT DOWN ENGINE IN FLIGHT, EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SHAFT O-RING, LEAK CHECK OK.

Part: PUMP — MALFUNCTIONED · airframe 7,474 hrs · 6,912 cycles

5272-ECM- RIGHT HAND HYDRAULIC PUMP PRESSURE FOLLOWS THROTTLE MOVEMENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP, OPS AND LK CH OK.

Part: COMPUTER — INOPERATIVE · airframe 7,086 hrs · 6,491 cycles

5256-PIT- STALL PROTECTION SYSTEM WARNING INDICATION.MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION COMPUTER, OPS CK OK.

Part: CONTROL UNIT — FAILED · airframe 6,770 hrs · 6,150 cycles

5324-RIC- UPON DESCENT INTO PIT PITCH TRIM 1&2 FAILED. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, OPS CK OK.

Part: O-RING — LEAKING (BLEED AIR) · airframe 6,187 hrs · 5,538 cycles

5251-RIC- CREW REPORTED NR 2 BLEED LEAK WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED DUCT SEAL, LEAK AND OPS CHECK OK.

Part: VANE — INOPERATIVE · airframe 5,742 hrs · 5,075 cycles

5251-RIC- ADVISORY SYSTEM REPORTED STALL PROTECTION SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED THE #1 AOA VANE.

Part: VANE — INOPERATIVE · airframe 5,435 hrs · 4,765 cycles

5270-PIT- CREW ALERT MESSAGE "AOA #1 INOP”. MAINTENANCE REMOVED AND REPLACED THE #1 ANGLE OF ATTACK VANE, OPS CK OK.

Part: CONTROL VALVE — FAILED (A/C BAY) · airframe 5,323 hrs · 4,645 cycles

5324-PIT- CREW REPORTED NR 2 PAC OVERLOAD WARNING MESSAGE DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED DUAL TEMP CONTROL VALVE, OP CHECK OK.

Part: SENSOR — MALFUNCTIONED · airframe 5,220 hrs · 4,541 cycles

5318-PIT- RIGHT INBOARD BRAKE OVER TEMP INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD BRAKE TEMP SENSOR, OPS CK OK.

Part: DUCT — CRACKED · airframe 4,471 hrs · 3,795 cycles

5275-PIT-RIGHT ENGINE AUTO TAKEOFF THRUST CONTROL SYSTEM WARNING ON TAKE OFF ROLL. MAINTENANCE DEFERRED PER MEL 73-22-02. CLEARED DMI - REMOVED AND REPLACED THE RIGHT HAND ANTI-ICE BLEED DUCT.

Part: TIRE — FAILED (LT/RT MAIN) · airframe 4,032 hrs · 3,384 cycles

5266-PIT-UPON LANDING IN MEM, ALL FOUR MAIN TIRES FAILED. M,AINTENANCE INSPECTED AND REPLACED ALL FOUR MAIN TIRES, PERFORMED OPERATIONAL CHECK, SYSTEMS CHECKED GOOD. PERFORMED CMC MAINTENANCE DOWNLOAD, NO FAULTS FOUND.

Part: ENGINE — OVERHEATED (RIGHT) · airframe 1,634 hrs · 1,311 cycles

6232-CLE- RIGHT ENGINE ITT HIGH. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE.

Part: HANDLE — BENT (PAX DOOR) · airframe 1,126 hrs · 868 cycles

FLT 6259 - BOS, PASSENGER CREW ENTRY DOOR SQUEALS IN FLIGHT. MAINTENANCE INSPECTED, FOUND PASSENGER DOOR HANDLE BENT. MAINTENANCE INSPECTED DOOR AND REPLACED PASSENGER DOOR HANDLE.