N810HK

Part: TRIM SWITCH — INOPERATIVE (PITCH) · airframe 34,626 hrs · 31,421 cycles

PITCH TRIM MAIN INOPERATIVE, FOLLOWED BY BACK UP PITCH TRIM INOPERATIVE, FOLLOWED QRH. BACK UP PITCH TRIM CAME BACK, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED THE PITCH TRIM SWITCH AND RERACKED THE HSCU, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,385 hrs · 31,198 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 DIM. R & R PAX DOOR EMERGENCY LIGHT NR 1. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,385 hrs · 31,198 cycles

RIGHT AFT OVER WING EXTERIOR EMERGENCY FLOOD LIGHT NR 6 INOPERATIVE. R & R RT AFT OVERWING EXTERIOR EMERGENCY FLOOD LIGHT NR 6 BULB. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,012 hrs · 30,861 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,715 hrs · 30,613 cycles

EMERGENCY EXIT LIGHT IN COCKPIT CEILING LIGHT NR 7 IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED LIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,090 hrs · 30,044 cycles

EMERGENCY EXIT LIGHT AT STEP INTO COCKPIT NR 9 IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,920 hrs · 29,880 cycles

CEILING EMERGENCY LIGHT IN GALLEY, NR 8, IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: BULB — INOPERATIVE · airframe 32,889 hrs · 29,855 cycles

CEILING EMERGENCY EXIT LIGHT IN GALLEY, NR 8, IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED BULB, OPS CHECK GOOD.

Part: STOP FITTING — BENT (PAX DOOR STEP) · airframe 32,467 hrs · 29,462 cycles

MAIN DOOR AIRSTAIRS NOT FULLY DEPLOYING DURING POST FLIGHT. MAINTENANCE INSPECTED AND FOUND STEP FOLDOUT BACKSTOP BENT, REPLACED BACKSTOP, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 32,433 hrs · 29,426 cycles

NR 1 EMERGENCY BATTERY WILL NOT CHARGE. MAINTENANCE REPLACED NR 1 EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.

Part: DOOR FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

PASSENGER DOOR FORWARD FRAME CORRODED. MAINTENANCE REPLACED PASSENGER DOOR FORWARD FRAME.

Part: CONTROL ROD — CORRODED (ELEVATOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

ALL 4 ELEVATOR TRIM TAB RODS HAVE CORROSION. MAINTENANCE REPLACED ALL 4 ELEVATOR TRIM TAB CONTROL RODS.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-23) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

CENTER OMEGA BEAM GUSSET FR19-23 IS CORRODED. MAINTENANCE REPLACED CENTER OMEGA BEAM GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

LT OMEGA BEAM LOWER RAMP SUPPORT FR18-19 IS CORRODED. MAINTENANCE REPLACED LT OMEGA BEAM LOWER RAMP SUPPORT.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

AFT PASSENGER DOOR DIGITAL FR17-18 IS CORRODED. MAINTENANCE REPLACED AFT PASSENGER DOOR DIGITAL.

Part: FLOOR SUPPORT — CORRODED (FRAME 18-19) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

CENTER OMEGA BEAM RAMP SUPPORT FR18-19 IS CORRODED. MAINTENANCE REPLACED CENTER OMEGA BEAM RAMP SUPPORT.

Part: DOUBLER — CORRODED (FRAME 61) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

LEFT SIDE DOUBLER ON FRAME 61 IS CORRODED. MAINTENANCE REPLACED LT SIDE DOUBLER.

Part: GUSSET — CORRODED (FRAMES 58-61) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

LEFT BEAM GUSSET AT FRAMES 58-61 IS CORRODED. MAINTENANCE REPLACED LT BEAM GUSSET.

Part: GUSSET — CORRODED (FRAMES 58-61) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

CENTER BEAM GUSSET AT FRAMES 58-61 IS CORRODED. MAINTENANCE REPLACED CENTER BEAM GUSSET.

Part: CHANNEL — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

CARGO DOOR FRAME Z CHANNEL CORRODED. MAINTENANCE REPLACED CARGO DOOR FRAME Z CHANNEL.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

FORWARD U SHAPE AT PASSENGER DOOR HAS CORROSION. MAINTENANCE REPLACED FORWARD U SHAPE AT PASSENGER DOOR.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,433 hrs · 29,426 cycles

AFT U SHAPE AT PASSENGER DOOR HAS CORROSION. MAINTENANCE REPLACED AFT U SHAPE AT PASSENGER DOOR.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 11C) · airframe 32,278 hrs · 29,278 cycles

OXYGEN MASK AT SEAT 11C FELL DOWN DURING TAXI. MAINTENANCE STOWED THE OXYGEN MASK, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,273 hrs · 29,269 cycles

EMERGENCY EXIT SIGN AFT OF OVERWING EMRGENCY EXIT DOOR AT 18D IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,570 hrs · 28,598 cycles

EMERGENCY EXIT LIGHT AT ROW 18D INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,479 hrs · 28,519 cycles

EMERGENCY EXIT LIGHT ON PASSENGER DOOR HAND RAIL IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 30,070 hrs · 27,265 cycles

MAIN PITCH TRIM FAILED IN FLIGHT DURING DESCENT. MADE EMERGENCY LANDING, MAINTENANCE REPLACED HORIZONTAL STABALIZER CONTROL UNIT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,062 hrs · 27,256 cycles

CEILING EMERGENCY LIGHT AT ROW 18 IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: FIRE DETECTOR — FALSE INDICATION (APU BAY) · airframe 29,876 hrs · 27,102 cycles

APU FIRE MESSAGE DISPLAYED ON EICAS DURING DESCENT. MAINTENANCE PERFORMED FIRE DETECTION TEST, OPS CHECKED GOOD. PERFORMED GVI OF APU, NO FIRE DETECTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,843 hrs · 27,067 cycles

AISLE FLOOD LIGHT 16B INOPERATIVE. REPLACED BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,626 hrs · 26,884 cycles

CEILING EMERGENCY LIGHT AT ROW 12, AFT SIDE IS INOPERATIVE. MX REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,552 hrs · 26,822 cycles

AFT CEILING EMERGENCY EXIT SIGN AT ROW 12 INOPERATIVE. MX REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,188 hrs · 26,502 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MX REPLACED BULB AND OPS CHECKED GOOD.

Part: DOOR — DIRTY (MAIN PAX) · airframe 23,976 hrs · 21,865 cycles

PASSENGER DOOR HARD TO CLOSE AND DOOR OPEN INDICATION WHEN DOOR IS CLOSED. MX CLEANED AND INSPECTED PASSENGER DOOR. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,019 hrs · 26,360 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 3 INOPERATIVE. MX INSPECTED AND REPLACED BULB AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,351 hrs · 25,731 cycles

DURING SCHEDULED MAINTENANCE THE AFT CABIN FLASHLIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT. SYSTEM OPS CHECKED GOOD.

Part: BALLAST — BURNED (CABIN) · airframe 26,893 hrs · 24,422 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED A BURNING ODOR IN THE PASSENGER COMPARTMENT. MAINTENANCE INSPECTED AND FOUND THE SMELL COMING FROM THE BALLAST FOR THE OVERHEAD LIGHT AT SEAT 9A. THE BALLAST WAS DISCONNECTED AND THE LIGHT WAS DEFFERED PER MEL 33-20-00-2.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 24,535 hrs · 22,271 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND C/W ADJUSTMENT/TEST OF THE PASSENGER DOOR. OPS CHECKED GOOD. INCOMING FLIGHT CREW ALSO CHECKED THE PASSENGER DOOR AND HAD NO ISSUES WITH THE DOOR.

Part: STAND OFF — BROKEN (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) ELEVATOR CABLE LH INBOARD STANDOFF CRACKED AT FR 24, STA. 7324. REMOVED AND REPLACED SUPPORT. W/C 1147

Part: PROFILE — CORRODED (PAX DOOR) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX DOOR FWD LOWER CORNER CORRODED. REMOVED AND REPLACED PROFILE. W/C 8012

Part: STAND OFF — BROKEN (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) ELEVATOR CABLE OUTBOARD STANDOFF BROKEN AT FR 23, STA 6930. REMOVED AND REPLACED SUPPORT. W/C 1146

Part: DOOR — CRACKED (LT MLG) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT NR 2 AUX MAIN LANDING GEAR DOOR CRACKED. REMOVED AND REPLACED AUX MAIN LANDING GEAR DOOR. W/C 7002

Part: DOOR — CORRODED (LT MLG) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT MAIN LANDING GEAR DOOR CORRODED. REMOVED AND REPLACED STRUCTURE IN MAIN LANDING GEAR DOOR. W/C 8011

Part: FLAP TRACK — DAMAGED (TE FLAP) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT INBOARD FLAP TRACK DAMAGED. REMOVED AND REPLACED FLAP TRACK. W/C 5079.

Part: FLAP TRACK — DAMAGED (TE FLAP) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT OUTBOARD FLAP TRACK DAMAGED. REMOVED AND REPLACED FLAP TRACK. W/C 5078.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

RIGHT BEAM STOP SIGN DOUBLER AT FR 25 CRACKED. REMOVED AND REPLACED DOUBLER. W/C 1088

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX SEAT TRACK POSITION C AT STA 17913.2 - 20230.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2142

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION B AT STA. 15506.5 - 17913.2 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2136

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

TENSION SUPPORT BRACKET CRACKED AT FR 61-62. REMOVED AND REPLACED SUPPORT. W/C 1085

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION B AT BS 12176.2 - 15506.5 IS CORRODED ON SEAT TRACK AND UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2135

Part: DUCT — DAMAGED (CABIN AIR) · airframe 24,195 hrs · 21,948 cycles

AIR CONDITIONING DUCT AT FR 15 DAMAGED. REMOVED AND REPLACED DUCT. W/C 1115

Part: SILL — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

RIGHT SILL AT FR 41-48 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 2113

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION B AT STA. 7324.0 - 9814.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2133

Part: STRIP — CRACKED (RT WING) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT INBOARD LEADING EDGE WING-BODY ATTACHMENT IS CRACKED. REMOVED AND REPLACED RIB STRIP. W/C 6039

Part: ATTACH ANGLE — BROKEN (LT WING) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT LOWER NR 4 WING FAIRING ATTACHMENT ANGLE IS BROKEN. REMOVED AND REPLACED ANGLE. W/C 5064

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION B AT BS 17913.2 - 20230.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2137

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION B AT STA. 9814.0 - 12176.2 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2134

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION A AT STA. 12176.2 - 15506.5 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2129

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

PAX SEAT TRACK POSITION C AT STA. 9814.0 - 12176.2 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2139

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX SEAT TRACK POSITION C AT STA 12176.2 - 1506.5 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2140

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FR 49 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 2117

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 65-68 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 2125

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 29-35 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 1091

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 36-41 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 2112

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 53-59 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 1103

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FR 60-65 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 1107

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT GUSSET AT FR 47-52 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED GUSSET. W/C 2116

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FR 53-59 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 1100

Part: PROFILE — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT PROFILE AT FR 17-18 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED PROFILE. W/C 1062

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX SEAT TRACK AT POS B STA 4154.5-7324.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2132

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX SEAT TRACK AT POS C STA 15506.5-17913.2 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2138

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) PAX SEAT TRACK AT POS C STA 7324.0-9814.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK. W/C 2138

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FR 19-23 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. W/C 1072

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT GUSSET AT FRAME 23-29 IS CORRODED OUT OF LIMITS. REPLACED CORRODED RT GUSSET AT FRAME WITH NEW PART IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 1095

Part: GUSSET — CRACKED (ZONE 600) · airframe 24,195 hrs · 21,948 cycles

OUTBOARD SPLICE CRACKED ON R/H OUTB/D WING LEADING EDGE 3. REMOVED AND REPLACED THE GUSSET SPLICE BETWEEN LEADING EDGE III AND THE WING TIP IAW AMM 20-10-01. W/C 6016

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) CENTER GUSSET AT FRAME 59-61 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED GUSSET AT FRAME 59-60 CENTER IAW EMB145 SRM 51-40-02. W/C 1098

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) PASSENGER SEAT TRACK POSITION 'A' AT STATION 7324.0 - 9814.0 IS CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK POSITION 'A' AT STATION 7324.0 - 9814.0 IAW EMB145 AMM 53-01-06. W/C 2127

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'A' AT STATION 15506.5 - 17913.2 CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED PASSENGER SEAT TRACK POSITION 'A' AT STA 15506.5 - 17913.2 IAW AMM 53-10-06. W/C 2130

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'D' AT STA 15506.5 - 17913.2 CORRODED ON SEAT TRACK SURFACE AND UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK 'D' AT STA 15506.5 TO 17913.2 IAW AMM 53-01-06.W/C 2146

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT GUSSET AT FRAME 53-59 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED LT GUSSET AT FRAME 53-59 IAW EMB145 SRM 51-40-02, 51-10-02, 51-40-09, AND 51-20-01. W/C 1101

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

SILL ON LT AT FRAME 42 REQUIRES REPLACEMENT DUE TO CORROSION. SILL ON LT AT FRAME 42 DRILLED UP AND REPLACED IAW SRM 51-10-02 AND 51-40-02. W/C 2118

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

CENTER GUSSET AT FRAMES 39-46 REQUIRES REPLACEMENT DUE TO CORROSION. REPLACED CORRODED CENTER GUSSET AT FRAME 39-46 WITH NEW PART IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 2121

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'D' AT STATION 17913.2 - 20230.0 HAS CORRODED SURFACES AND UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK 'D' AT STA 17913.2 TO 20230.0 IAW EMB145 AMM 53-01-06. W/C 2147

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) PASSENGER SEAT TRACK POSITION 'D' AT STA 12176.2 - 15506.5 CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK 'D' AT STA 12176.2 TO 15506.5 IAW EMB145 AMM 53-01-06. W/C 2145

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) SERVICE DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB145 SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 1070

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FRAME 23-29 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED LT SILL AT FRAME 23-29 IAW EMB145 SRM 51-40-02 AND 51-10-02. W/C 1096

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) PASSENGER SEAT TRACK POSITION 'A' AT STA 9814.0 - 12176.2 CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK AT POSITION 'A' AT STA 9814.0 - 12176.2 IAW EMB145 AMM 53-01-06. W/C 2128

Part: SEAT TRACK — CORRODED (BS 4154.5-7324) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK AT POSITION A, STA 4154.5 - 7324.0 CORRODED UNDER SCREW HEADS. R & R SEAT TRACK 'A' AT STATION 4154.5 TO 7324.0 IAW AMM 53-01-06.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

LEFT GUSSET AT FRAMES 39-46 CORRODED BEYOND LIMITS. REMOVED AND REPLACED LT GUSSET AT FRAME 39-46 IAW SRM 51-20-3, 51-10-02, AND 51-40-02. W/C 2120

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

SILL ON LT FROM FRAME 36-41 REQUIRES REPLACEMENT DUE TO CORROSION. SILL ON LT FROM FRAME 36-41 REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. W/C 2119

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'D' AT STATION 7324.0 - 9814.0 CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED PASSENGER SEAT TRACK AT 7324.0 - 9814.0 IAW EMB145 AMM 53-01-06. W/C 2143

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 24,195 hrs · 21,948 cycles

LEFT BOTTOM THRUST REVERSER FRAME CRACKED. REMOVED AND REPLACED LT LOWER THRUST REVERSER FWD FRAME WET WITH SEALANT IAW SRM 51-40-02. W/C 4034

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'D' AT STA 9814.0 - 12176.2 CORRODED UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK 'D' AT STA 9814.0 TO 12176.2 IAW EMB145 AMM 53-01-06. W/C 2144

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

CENTER GUSSET FROM FRAMES 36-40-REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AND REPLACED CENTER GUSSET AT FRAME 36-40 IAW EMB145 SRM 51-40-02 AND 51-40-02. W/C 2123

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT GUSSET AT FRAME 29-35 CORRODED OUT OF LIMITS. REPLACED CORRODED RT GUSSET AT FRAME 29-35 WITH NEW PART IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 1090

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT GUSSET AT FRAME 29-35 CORRODED OUT OF LIMITS. REMOVED AND REPLACED LT GUSSET AT FRAME 29-35 IAW EMB145 SRM 51-40-02 AND 51-10-02. W/C 1089

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

PASSENGER SEAT TRACK POSITION 'A' AT STA 17913.2 - 20230.0 HAS CORROSION UNDER SCREW HEADS. REMOVED AND REPLACED SEAT TRACK 'A' AT STA 17913.2 TO 20230.0 IAW EMB145 AMM 53-01-06. W/C 2131

Part: ATTACH ANGLE — CRACKED (NR 3) · airframe 24,195 hrs · 21,948 cycles

NR 3 LT LOWER FAIRING ATTACH ANGLE BROKEN. (WING FAIRING). REMOVED AND REPLACED NR 3 LT LOWER FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5063

Part: ATTACH ANGLE — CRACKED (ZONE 500) · airframe 24,195 hrs · 21,948 cycles

LEFT LOWER FWD FAIRING ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED LT LOWER FWD FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5068

Part: ATTACH ANGLE — CRACKED (NR 3) · airframe 24,195 hrs · 21,948 cycles

NR 3 LT UPPER WING FAIRING ATTACH ANGLE IS BROKEN. REMOVED AND REPLACED L/H WING - BODY FAIRING STRIP NR 3 IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5065

Part: ATTACH ANGLE — CRACKED (NR 2) · airframe 24,195 hrs · 21,948 cycles

NR 2 LT LOWER WING TO FUSELAGE FAIRING ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED NR 2 LT LOWER FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5062

Part: SUPPORT — DAMAGED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

FRAME 25 RT BEAM SUPPORT HAS PREVIOUS BAD HOLE DRILLED. REMOVED AND REPLACED R/H BEAM SUPPORT AT FRAME 25 IAW EMB145 SRM 51-40-02 AND 51-10-02. W/C 1138

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

CENTER GUSSET AT FRAME 19-23 IS CORRODED. REMOVED AND REPLACED CENTER GUSSET AT FRAME 19-23 IAW SRM 51-40-02 AND 51-20-03. W/C 1065

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) CENTER GUSSET FROM FRAMES 47-52 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AND REPLACED CENTER GUSSET FROM FRAMES 47-52 IAW EMB145 SRM 51-20-03, 51-10-02, AND 51-40-02. W/C 2115

Part: STRIP — CRACKED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT WING-BODY FAIRING STRIP NR 4 BACK HAS CRACK. REMOVED AND REPLACED LT WING-BODY FAIRING STRIP NR 4 IAW EMB145 SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2061

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) CENTER OMEGA BEAM AT Y 0.0 BETWEEN FRAMES 17-24 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED OMEGA BEAM AT Y 0.0 BETWEEN FRAMES 17-24 IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 1117

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT GUSSET AT FRAME 53-59 CORRODED OUT OF LIMITS. REMOVED AND REPLACED GUSSET AT FRAME 53-59 IAW EMB145 SRM 51-40-02, 51-10-02, AND 51-20-03. W/C 1102

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT BEAM AT FRAME 18-24 IS CORRODED. RT BEAM AT FRAME 18-24 REMOVED AND REPLACED PER EMB145 SRM 51-10-02, 51-20-03, 51-40-02, 51-21-04, AND 51-20-01. W/C 1066

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

LEFT PROFILE AT FRAME 22 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED L/H PROFILE AT FRAME 22 IAW SRM 51-40-02 AND 51-10-02. W/C 1075

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) FLOORBOARD ANGLES ON IB LT BEAM AT FRAME 18-19 ARE CORRODED. REMOVED AND REPLACED PROFILES (P/N'S 145-21718-005 AND 145-21718-007) ON IB LT BEAM AT FRAME 18-19 IAW EMB145 SRM 51-20-03, 51-10-02, 51-40-02, AND 51-20-01. W/C 1061

Part: STRIP — CRACKED (WG-BDY FAIRING) · airframe 24,195 hrs · 21,948 cycles

RT UPPER WING-BODY FAIRING STRIP, NR 2 BACK IS CRACKED. REMOVED AND REPLACED RT UPPER WING-BODY STRIP NR 2 IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2056

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) DOUBLERS AT FRAMES 20 AND 22 ON THE RT BEAM ARE CORRODED. REMOVED AND REPLACED DOUBLERS AT FRAMES 20 AND 22 IAW EMB145 SRM 51-40-02 AND 51-10-02. W/C 1067

Part: PARTITION — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

RIGHT PARTITION AT FRAME 61 IS CORRODED OUT OF LIMITS. REPLACED CORRODED RT PARTITION AT FRAME 61 WITH NEW PART IAW SRM 51-10-02 AND 51-40-02. W/C 1084

Part: STRIP — CRACKED (WG-BDY FAIRING) · airframe 24,195 hrs · 21,948 cycles

RT UPPER WING-BODY FAIRING STRIP, NR 4 BACK IS CRACKED. REMOVED AND REPLACED RT UPPER WING-BODY FAIRING FAIRING STRIP IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2057

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

BEAM AT FRAME 20 IS CORRODED OUT OF LIMITS. REMOVED OLD REPAIR, FABRICATED NEW REPAIR AND REPLACED IAW SRM 53-00-10, 51-20-03, 51-40-02, 51-30-01, 51-20-01, AND CPM 51-21-04, 51-20-05. W/C 1076

Part: SILL — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

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

Part: SILL — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

RT SILL AT FR 23-29 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

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

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,195 hrs · 21,948 cycles

RT PROFILE AT FR 61 IS CORRODED BEYOND LIMITS. R & R PROFILE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

LT SILL AT FRAME 59-60 IS CORRODED OUT OF LIMITS. R & R LT SILL AT FRAME 59-60 IAW SRM 51-10-02, 51-40-02, AND 51-20-03.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) U-SHAPE ANGLES AT PASSENGER DOOR REQUIRE REPLACEMENT DUE TO CORROSION. U-SHAPE ANGLES PN'S 145-24131-009 AND 145-24131-011 AT PASSENGER DOOR REPLACED PER EMB145 SRM 51-20-03, 51-40-02, AND CPM 51-21-04.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT GUSSET AT FRAME 59-61 CORRODED OUT OF LIMITS. REMOVED AND REPLACED R/H GUSSET AT FR 59-61 AS REQUIRED IAW EMB145 SRM 51-10-02, 51-21-04, 51-21-05 AND 51-20-01. W/C 1097

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) HORSESHOE DIGITAL PLATE AT FRAME 16-18 HAS CORROSION. REMOVED AND REPLACED HORSESHOE AT FRAME 16-18 IAW EMB145 SRM 51-20-03, AND 51-40-02. W/C 1063

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

SCALLOPED ANGLE AT FRAME 23 IS CORRODED OUT OF LIMITS. REPLACED CORRODED SCALLOPED ANGLE AT FRAME 23 WITH NEW PART IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 1105

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

LEFT GUSSET FROM FRAMES 36-40 REQUIRES REPLACEMENT DUE TO CORROSION. REPLACED LT GUSSET FROM FRAMES 36-40PER EMB145 SRM 51-10-02, 51-40-02, 51-40-01, 51-40-09. W/C 2122

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

LEFT GUSSET AT FRAME 23-29 CORRODED OUT OF LIMITS. REPLACED CORRODED LT GUSSET AT FRAME 23-29 WITH NEW PART IAW SRM 51-10-02 AND 51-40-02. W/C 1094

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

(V0XR) FORWARD DIGITAL PLATE AT FRAME 14-16 HAS CORROSION. REPLACED CORRODED FORWARD DIGITAL AT FRAME 14-16 WITH NEW PART IAW EMB145 SRM 51-10-02 AND 51-40-02. W/C 1064.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,195 hrs · 21,948 cycles

ANGLE ON RT RY 780.0 AT FRAME 23 IS CORRODED OUT OF LIMITS. REPLACED CORRODED ANGLE ON RT RY 780.0 AND FRAME 23 WITH NEW PART IAW SRM 51-10-02 AND 51-40-02. W/C 1093

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT SILL AT FR 29-35 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 1087

Part: PROFILE — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT PROFILE AT 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE. W/C 1113

Part: PARTITION — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT PARTITIAN AT FR 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PARTITIAN. W/C 1083

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 48-52 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 2114

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AFT OF SERVICE DOOR AT FR 22-23 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 1059

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AT FR 68-71 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 2124

Part: SPLICE — CRACKED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) DIGITAL SPLICE ON INBOARD SIDE OF LT OMEGA BEAN BETWEEN FR 16-17 IS CRACKED. REMOVED AND REPLACED SHAPE. W/C 1118

Part: SILL — CORRODED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT SILL AFT OF SERVICE DOOR AT FR 18-20 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 1060

Part: RIB — CRACKED (LT WING) · airframe 24,195 hrs · 21,948 cycles

(V0XR) LT WING END RIB CRACKED. REMOVED AND REPLACED WEB. W/C 5064

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 24,195 hrs · 21,948 cycles

(V0XR) RT INBOARD WING LEADING EDGE TO FWD BODY FAIRING GUSSET MISS-DRILLED. REMOVED AND REPLACE GUSSET. W/C 6033,

Part: DUCT — LOOSE (ANTI-ICE SYS) · airframe 24,131 hrs · 21,884 cycles

DURING CLIMB THE FLIGHT CREW GOT A WING A/ICE FAIL MESSAGE IN ICING CONDITIONS. AIRCRAFT MADE A RETURN FLIGHT TO IAD. MAINTENANCE INSPECTED AND FOUND A LOOSE DUCT. THE DUCT WAS RE-SECURED. ANTI-ICE SYSTEM OPS CHECK WAS PERFORMED AND SYSTEM OPS CHECKED GOOD.

Part: SOCKET — DIRTY (CABIN) · airframe 23,242 hrs · 21,035 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW FOUND THE MAIN PASSENGER DOOR EMERGENCY LIGHT VERY DIM. MAINTENANCE INSPECTED AND CLEANED THE LIGHT BULB SOCKET AND RELAMPED THE MAIN PASSENGER DOOR EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD.

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 23,020 hrs · 20,823 cycles

DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HANDLE WILL NOT CLOSE FLUSH. MAINTENANCE INSPECTED AND ADJUSTED THE INNER DOOR HANDLE. DOOR OPS CHECKED GOOD.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 22,232 hrs · 20,104 cycles

DURING CRUISE, THE CREW REPORTED AN ELECTRICAL SMELL IN THE CABIN AND SUSPECTED THAT IT WAS FROM THE COFFEEMAKER. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT BALLAST AT ROW 1 TO BE THE CAUSE OF THE ODOR. THE LIGHT BULB WAS REMOVED AND THE BALLAST DEFERRED PER THE EMB145 MEL.

Part: CABLE — LACK OF LUBE (CABIN DOOR) · airframe 22,041 hrs · 19,918 cycles

DURING DE-PLANE, THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBED THE DOOR CABLES AND HANDLE. FOLLOW ON OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: DOOR — OUT OF ADJUST (PAX DOOR) · airframe 22,032 hrs · 19,908 cycles

THE CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. PRIOR TO THE NEXT SCHEDULED FLIGHT, MAINTENANCE ADJUSTED THE PASSENGER DOOR IAW AMM PROCEDURES. NO ADDITIONAL DEFECTS NOTED.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 21,900 hrs · 19,790 cycles

DURING THE GROUND HANDLING OPERATION, THE FLIGHT ATTENDANT REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR OPERATING LINKAGE AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE DOOR.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 21,879 hrs · 19,766 cycles

CREW REPORTED RECEIVING A NR 2 ADC FAIL AND AUTOPILOT FAIL MESSAGE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ADC AND PERFORMED A OPERATIONAL CHECK OF THE ADC AND THE AUTOPILOT SYSTEM IAW THE AMM PROCEDURES. BOTH SYSTEMS OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING SCHEDULED MAINTENANCE, THE FORWARD CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-SECURED A LOOSE CONNECTION AT THE LIGHT ASSEMBLY. THE FOLLOW-ON OPERATIONAL CHECK WAS GOOD.

Part: O-RING — WORN (BLEED AIR SYS) · airframe 21,494 hrs · 19,422 cycles

CREW REPORTED RECEIVING A NR 1 BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE REPLACED THE LEFT ENGINE PRE COOLER DUCT TY-WRAPS AND BLEED O-RINGS IN THE CARGO BAY UNDERNEATH THE FLOOR PANELS. OPS CHECKED AND LEAK CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,208 hrs · 19,179 cycles

DURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF EMERGENCY LIGHTS AS BEING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 20,552 hrs · 18,614 cycles

DURING TAKEOFF CLIMB, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAULT ON THE EICAS AND THE GEAR HANDLE WOULD NOT MOVE TO A GEAR UP POSITION. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LOWER PROXIMITY SWITCHES TO BE OUT OF ADJUSTMENT. ADJUSTMENTS WERE MADE AND THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM OPERATIONALLY CHECKED GOOD.

Part: BRAKE ASSY — OVERTEMP (LT MLG) · airframe 20,442 hrs · 18,506 cycles

FLT 8057 - ORD - BRAKE OVERTEMP MESSAGE ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE.

Part: CONNECTOR — CORRODED (NLG) · airframe 20,311 hrs · 18,395 cycles

CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS AFTER TAKEOFF AND THAT THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND REPLACED THE NLG WEIGHT ON WHEELS SWITCH AND CONNECTOR. SUBSEQUENT OPERATIONAL CHECK OF THE SYSTEM PROVED A GOOD CORRECTIVE ACTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,124 hrs · 18,241 cycles

PRE FLT NR 8018-STL-OVERHEAD AISLE EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED THE BULB AT THE EMERGENCY LIGHT SIGN. OPS CHECKED GOOD IAW AMM PROCEDURES.

Part: CONNECTOR — DIRTY (FECU) · airframe 19,118 hrs · 17,389 cycles

THE CREW RECEIVED A FLAP FAIL MESSAGE ON THE EICAS. MAINTENANCE CLEANED AND RE-SECURED THE CONNECTOR TO THE FECU, INSPECTED WIRES, AND PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM WITH NO DEFECTS NOTED.

Part: VALVE — CLOSED (NR 1 PACK) · airframe 18,639 hrs · 16,985 cycles

DURING CRUISE, PACK 1 VALVE CLOSED UNCOMMANDED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE NR 1 PACK SYSTEM WITH NO DEFECTS NOTED.

Part: O-RING — DEFECTIVE (NR 2 ENGINE)

DURING CLIMB, CREW SHUTDOWN THE NR 2 ENGINE IN FLIGHT DUE TO LOW OIL AND LOW OIL AND LOW OIL PRESSURE. MAINTENANCE INSPECTED THE ENGINE AND FOUND A BAD O-RING AT THE NR4 GENERATOR. THE O-RING WAS REPLACED AND LEAK CHECK OF THE NR 2 ENGINE DID NOT PRODUCE ANY OTHER LEAKS. (K)

Part: LIGHT — LOOSE (CABIN) · airframe 18,337 hrs · 16,716 cycles

PRE FLT 7945 -SGF- EMERGENCY LIGHT STRIP CAME LOOSE FROM THE FLOOR. MAINTENANCE DEFERRED THE APPLICABLE LIGHT STRIP IAW MEL PROCEDURES. (S)

Part: LIGHT — LOOSE (CABIN) · airframe 16,884 hrs · 15,531 cycles

POST FLT NR 8019 - STL - FLOOR PROXIMITY LIGHT LOOSE. MAINTENANCE INSPECTED AND FOUND SAID STRIP CAME LOOSE, RESECURED LIGHT STRIP, CHECKS GOOD.

Part: PROXIMITY SWITCH — DIRTY (LANDING GEAR) · airframe 16,150 hrs · 14,903 cycles

FLT 7981 - ROA - LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS AFTER TAKEOFF AND LANDING GEAR LEVER WOULD NOT MOVE UP WITHOUT USING THE DOWN LOCK RELEASE BUTTON. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM THE LANDING GEAR PROXIMITY SWITCHES. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (AUTO THRUST SYS) · airframe 16,106 hrs · 14,866 cycles

FLT NR 8087 - DEN - AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM RED WARNING ON TAKEOFF. MAINTENANCE PERFORMED EMB SP-22 REFERENCE ENGINE EXCEEDANCE MESSAGE, OPS CHECK GOOD.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 15,992 hrs · 14,768 cycles

PRE FLT NR 8043 - RIC - RIGHTHAND OVERWING EXIT EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY EXIT SIGN INVERTER, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,927 hrs · 14,709 cycles

PRE FLT 5495 - STL - EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE RESECURED A LOOSE CONNECTION TO THE LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,917 hrs · 14,704 cycles

PRE FLT 7901 - ORD - EMERGENCY EXIT LIGHT AT RIGHT HAND OVERWING EXIT IDENTIFIER INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY.

Part: CONTROL VALVE — FAULTY (BRAKE SYSTEM) · airframe 15,733 hrs · 14,546 cycles

FLT NR 8022 - IAD - BRAKE OUTBOARD INOP MESSAGE ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE FUNCTIONAL CHECK GOOD AT THIS TIME.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 15,654 hrs · 14,482 cycles

POST FLT NR 8087 - IAD - RIGHTHAND OVERWING EXIT IDENTIFIER LIGHT INOP. MAINTENANCE RESEATED CONNECTOR ON EMERGENCY LIGHT, OPS CHECK GOOD.

Part: LIGHT — LOOSE (RT OVERWING) · airframe 15,466 hrs · 14,331 cycles

POST FLT NR 8090 - IAD - EMERGENCY LIGHT AT RIGHT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE ADJUSTED EMERGENCY EXIT LIGHT AT RIGHT SIDE OVERWING EXIT. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,447 hrs · 14,312 cycles

PRE FLT NR 8065 - ORD - EMERGENCY LIGHT RIGHTHAND OVERWING EXIT MARKER INOP. MAINTENANCE SECURED CONNECTOR ON LIGHT ASSY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,327 hrs · 14,218 cycles

PRE FLT NR 3542 - STL - AISLE FLOOD LIGHT, FLOOR STRIP EMERGENCY LIGHT INOP. MAINTENANCE OPS CHECK, REMOVED AND REPLACED LAMP, CHECK NORMAL.

Part: CONNECTOR — DIRTY (CABIN) · airframe 15,324 hrs · 14,216 cycles

PRE FLT NR 7912 - IAD - EMERGENCY LIGHT AT RIGHT HAND OVERWING EXIT IDENTIFIER IS INOP. MAINTENANCE CLEANED CONNECTORS FOR EMERGENCY LIGHT, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,261 hrs · 14,174 cycles

PRE FLT NR 8059 - RIC - EMERGENCY LIGHT INOP, LEFT EMERGENCY DOOR FLOOD LIGHT. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD.

Part: INVERTER — UNKNOWN (CABIN) · airframe 15,231 hrs · 14,151 cycles

PRE FLT NR 5535 - STL - EMERGENCY EXIT LIGHT INOP AT ROW 12. MAINTENANCE REMOVED AND REPLACED NR 6 INVERTER. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (NR 1 ENGINE) · airframe 15,212 hrs · 14,138 cycles

FLT NR 5587 - STL - NO FUEL FLOW ON NR 1 ENGINE DURING START. MAINTENANCE RESEATED CONNECTOR TO FADEC 1A & 1B. OPS CHECK GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 15,190 hrs · 14,120 cycles

PRE FLT NR 7877 - STL - EMERGENCY LIGHT WIRE LOOSE ON HANDRAIL. MAINTENANCE RESECURED PAX DOOR EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 15,007 hrs · 13,966 cycles

PRE FLT NR 5519 - STL - AFT CEILING EMERGENCY EXIT IDENTIFIER INOP. MAINTENANCE RESEATED A LOOSE CONNECTOR AT THE SUBJECT LIGHT ASSEMBLY.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,819 hrs · 13,829 cycles

PRE FLT NR 5475 - STL - EMERGENCY LIGHT AT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE RESECURED A LOOSE CONNECTOR. LIGHTS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,810 hrs · 13,824 cycles

PRE FLT NR 5593 -STL- EMERGENCY EXIT LIGHT ABOVE ROW 12 INOP. MAINTENANCE RESEATED THE CONNECTION ON THE LIGHT ASSEMBLY.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 14,634 hrs · 13,701 cycles

FLT NR 5587 - STL - CREW REPORTED ELECTRICAL BURNING ODOR IN CABIN. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL MODULE ASSEMBLY.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,570 hrs · 13,655 cycles

PRE FLT NR 5574 - STL - EXIT SIGN IN MIDDLE OF AISLE IS INOP. MAINTENANCE CYCLED POWER TO THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,543 hrs · 13,637 cycles

PRE FLT 5563 - STL - EMERGENCY LIGHT INOP. MAINTENANCE RECYCLED THE POWER TO THE EMERGENCY LIGHT SYSTEM. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 14,460 hrs · 13,575 cycles

PRE FLT 5510 - STL - EMERGENCY CEILING LIGHT INOP AT OVERWING EXITS. MAINTENANCE OPS CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED.

Part: BEARING — WORN (TE FLAP) · airframe 14,286 hrs · 13,439 cycles

FLT NR 7938 - STL - AIRCRAFT BUFFETING IN FLIGHT, INSPECTED ON GROUND AND FOUND LEFT INBOARD FLAP BEARING LOOSE. MAINTENANCE REMOVED AND REPLACED THE LT OB FLAP INBOARD ROLLER BEARING.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,235 hrs · 13,395 cycles

PRE FLIGHT 8029 - RIC - EMERGENCY LIGHT OVER ROW 12 OUT. MAINTENANCE RESECURED CONNECTOR TO THE LIGHT ASSEMBLY OVER ROW 12.

Part: CONNECTOR — DIRTY (CABIN) · airframe 14,179 hrs · 13,348 cycles

PRE FLIGHT NR 7954 - IAD - EMERGENCY LIGHT INOP. MAINTENANCE CLEANED THE CONNECTION ON THE RIGHT SIDE EMERGENCY LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: WIRE — LOOSE (CABIN) · airframe 14,143 hrs · 13,320 cycles

PRE FLIGHT NR 8025 - STL - EMERGENCY EXIT LIGHT ON WALL ON C&D SIDE NOT WORKING PROPERLY. MAINTENANCE RESECURED WIRES ON EMERGENCY EXIT LIGHT ON WALL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,091 hrs · 13,268 cycles

PRE FLIGHT 7961 - IAD - EXIT SIGN AT MID CABIN INOP. MAINTENANCE ADJUSTED EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,871 hrs · 13,075 cycles

MX - STL - EMERGENCY LIGHTS IN ENTRY WAY INOP. RELAMPED FWR OVERHEAD EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,767 hrs · 12,986 cycles

PRE FLIGHT 7975 - RIC - CREW REPORTED EMERGENCY LIGHT OUT AT ROW 12. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FAULTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,685 hrs · 12,902 cycles

PRE FLIGHT 7950 - ALB - EMERGENCY LIGHT OVERHEAD AT ROW 12. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.

Part: SWITCH — ACTIVATED (CABIN) · airframe 13,488 hrs · 12,716 cycles

PRE FLIGHT NR 8023-IAD-EMERGENCY LIGHTS OUT IN CABIN. MAINTENANCE RESET LIGHT SWITCH.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 11,364 hrs · 12,606 cycles

MX EMERGENCY EXIT SIGN AT ROW 12 INOP. RESECURED BULB.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 13,316 hrs · 12,556 cycles

MX - SAT EMERGENCY LIGHT STRIP AFT, INOP. RE-SECURED LIGHTING STRIP WIRING.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 12,584 hrs · 11,909 cycles

MX INSPECTION - STL - MAINTENANCE FOUND THE EMERGENCY FLOOR STRIP AT ROW 12, LOWER EXIT SIGN, AND STRIP AT 4A INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND REPAIRED A BROKEN WIRE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,356 hrs · 11,687 cycles

PREFLIGHT - STL - EMERGENCY LIGHT AT EXIT DOOR OUT AT ROW 12. MAINTENANCE REMOVED AND REPLACED THE BULB.

Part: LANDING GEAR — MALFUNCTIONED · airframe 12,327 hrs · 11,659 cycles

FLT 3553 - LGA - LANDING GEAR FAILS TO RETRACT INFLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM. NO DEFECTS NOTED.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 11,361 hrs · 10,714 cycles

FLT 3535- PIT- NR 1 ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE START CONTROL VALVE. OPS CHECKED GOOD.

Part: DAU — FAILED (NR 1) · airframe 11,320 hrs · 10,672 cycles

DATA ACQUISITION UNIT FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 DAU. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (BRAKE TEMP) · airframe 11,185 hrs · 10,551 cycles

FLT 3592 - RIC - BRAKE OVERHEAT MESSAGE ON EICAS JUST BEFORE TAKEOFF. NR 2 BRAKE TEMP INDICATION SPIKES MOMENTARILY. MAINTENANCE DEFERRED LT INBOARD BRAKE TEMP SENSOR.

Part: DUCT — LEAKING (PRECOOLER) · airframe 10,440 hrs · 9,853 cycles

PIT - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOOLER AND PRECOOLER DUCT.

Part: ACTUATOR — OUT OF ADJUST (THRUST REVERSER) · airframe 10,140 hrs · 9,572 cycles

NR 2 ENGINE THRUST REVERSER DISAGREE. DEFERRED NR 2 ENGINE THRUST REVERSER PER MEL 78-34-00. ADJUSTED NR 2 THRUST REVERSER UPPER LEVER STOW ACTUATOR.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 10,133 hrs · 9,566 cycles

3519- PIT- EICAS MESSAGE THRUST REVERSE DISAGREE DURING TAKEOFF. MAINTENANCE PERFORMED, OPS CHECKOF THRUST REVERSE.

Part: TILLER — INOPERATIVE (NLG STEERING) · airframe 9,308 hrs · 8,711 cycles

PIT - AFTER LANDING HAD NO NW STEERING WITH TILLER. MAINTENANCE REMOVED AND REPLACED TILLER ASSY.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CORROSION AT SERVICE DOOR ENTRY AREA DOUBLERS AT FRAME 19 AND 21. MAINTENANCE REMOVED AND REPLACED DOUBLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CORROSION CENTER FLOORBEAM AT RAMP SUPPORT. MAINTENANCE REPLACED CENTER FLOORBEAM.

Part: SEGMENT — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CK FOUND T-SECTION AT PAX DOOR AREA WITH CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED T-SECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - PAX DOORSILL ANGLES HAVE CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED PAX DOOR SILL ANGLES IAW EMB GST-1927/02A.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CORROSION LEFT HAND SILL. MAINTENANCE REMOVED AND REPLACED LEFT HAND SILL.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND FORWARD FLOOR AT FRAME 14 TO FRAME 18 CENTER HAT BEAM CORROSION. MAINTENANCE REMOVED AND REPLACED HAT BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND LEFT HAND FLOORBEAM CORRODED. MAINTENANCE REPAIRED LEFT HAND FLOORBEAM IAW SRM 5321-10.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND AFT STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED AFT STRAP GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CENTER FLOORBEAM GUSSET CORRODED. MAINTENANCE REMOVED AND REPLACED GUSSET.

Part: STRAP — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND FORWARD STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED FORWARD STRAP DIGITAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CORROSION ON LEFT HAND DIGITAL. MAINTENANCE REMOVED AND REPLACED LEFT HAND DIGITAL.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 7,583 hrs · 7,056 cycles

STL - DURING BLOCK CHECK FOUND CORROSION AT SUPPORT ANGLE AT PAX DOOR. MAINTENANCE REMOVED AND REPLACED SUPPORT ANGLE.

Part: STARTER — INOPERATIVE (NR 1 ENGINE) · airframe 7,405 hrs · 6,878 cycles

PIT- NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR TURBINE STARTER.

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 7,338 hrs · 6,810 cycles

PIT- LANDING GEAR DISAGREE MESSAGE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 7,207 hrs · 6,692 cycles

5253-PIT- LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED NUMEROUS LANDING GEAR RETRACTION CYCLES. NO DEFECTS NOTED.

Part: ACM — OVERHEATED (A/C BAY) · airframe 7,140 hrs · 6,629 cycles

5301-RIC- LEFT PACK SMELLS OVERHEATED. MAINTENANCE REMOVED AND REPLACED ACM.

Part: WIRE HARNESS — DAMAGED (BRAKE SYSTEM) · airframe 7,088 hrs · 6,583 cycles

5316-PIT- BRAKE OVER TEMP ADVISORY NR 2 BRAKE. MAINTENANCE DEFERRED PER MEL 32-40-01. SUBSEQUENTLY CLEARING DMI BY REPAIRING WIRE HARNESS.

Part: CONNECTOR — LOOSE (MLG UPLOCK) · airframe 5,816 hrs · 5,282 cycles

RT MAIN GEAR WOULD NOT SHOW UP AND LOCKED AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED NR 2 MLG UPLOCK PROXIMITY SWITCH CONNECTOR. OPS CK OK.

Part: BLEED VALVE — FAILED (COMPRESSOR) · airframe 5,684 hrs · 5,134 cycles

RIC- AUTO TAKEOFF THRUST CONTROL, NO WARNING. MAINTENANCE CHANGED COMPRESSOR BLEED VALVE, OPS CHECK OK.

Part: CONTROLLER — INOPERATIVE · airframe 8,093 hrs · 7,221 cycles

5251-PIT- WINDSHIELD #1 FAIL WARNING. MAINTENANCE REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK.