N984CA

Part: WATER SEPARATOR — CONTAMINATED · airframe 41,362 hrs · 36,792 cycles

RETURNED TO THE FIELD FOR SMOKE IN THE LAV. CREW REPORTED SMOKE COMING FROM GASPERS. FOUND GLYCOL IN WATER SEPARATOR. REPLACED NR 1AND NR 2 WATER SEPARATORS. OPS CHECKS GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,716 hrs · 36,238 cycles

WHILE PERFORMING BLENDING FOR EXTERIOR SKIN GOUGES FOR ADF ANTENNA ON MX TRANS 11509318, DISCOVERED 4 EACH LIGHTNING STRIKES AT ADF ANTENNA MOUNT HOLES. C-CHECK, UPON FURTHER INVESTIGATION, FOUND TO BE OLD TOOLING MARKS INSTEAD OF LIGHTNING STRIKES. ALSO FOUND 1 ADDITIONAL MARK, 5 TOTAL. BLENDED 5 EA AREAS ON EXTERIOR SKIN UNDER ADF ANTENNA AREA IAW REF SRM. ORIGINAL MATERIAL THICKNESS OF BLEND AREAS IS .058" IAW SRM. NDT LOWEST READING IN 5 EA BLEND AREAS IS .050". ONLY .008" MATERIAL LOSS. RECEIVED STS EA THAT LOWEST REMAINING THICKNESS .050" IS ACCEPTABLE. FOUND THE REWORKED AREAS WITHIN LIMIT.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 40,716 hrs · 36,238 cycles

SEAT TRACK AT LBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO

Part: PRESSURE DECK — CRACKED (BS 458-462) · airframe 40,716 hrs · 36,238 cycles

PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND LBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

LEFT INBD FLAP VANE CHAFED AT INBD L/E. BLENDED THE CHAFE IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 40,716 hrs · 36,238 cycles

CRACK NOTED ON BS 621 BULKHEAD WEB, FWD FACE ALONG BL 0 AT WL 90. C-CHECK. REPAIRED CRACK ON FS 621 BULKHEAD IAW REO. PRESSURE CHECK GOOD. COMPLIED WITH ST 51-900-1003, WEIGHED CUT OUT DAMAGED WEB SECTION AT .002 LBS AND REPAIR PARTS WITH ADDED FASTENERS AT 1.16 LBS WITH SCALE TUC 1755 CAL DUE JUN 2015.

Part: SKIN — DEBONDED (RT WING) · airframe 40,716 hrs · 36,238 cycles

RT WING OTBD L/E 630KL IS DEBONDED. BONDED RT WING OTBD L/E, 630KL IAW REO.

Part: PRESSURE DECK — CRACKED (BS 458-462) · airframe 40,716 hrs · 36,238 cycles

PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND RBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

LEFT INBD FLAP VANE CHAFED AT OTBD L/E. BLENDED THE CHAFE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,716 hrs · 36,238 cycles

PASSENGER DOOR HINGE 5TH LUG BACK IS GOUGED ON THE FUSELAGE SIDE. BLENDED AND FOUND WITHIN LIMITS. IAW REO.

Part: SEAT TRACK — CORRODED (BS 599) · airframe 40,716 hrs · 36,238 cycles

SEAT TRACK AT RBL 9.0 FROM BS 599 - 599+86 CORRODED. R & R THE SEAT TRACK IAW AMM & REO.

Part: SKIN — DEBONDED (RT WING) · airframe 40,716 hrs · 36,238 cycles

RT WING INBD L/E 620JL IS DEBONDED. BONDED RT WING INBD L/E IAW REO.

Part: BULKHEAD WEB — CRACKED · airframe 40,716 hrs · 36,238 cycles

CRACK AT FWD PRESSURE BULKHEAD WEB COMMON TO PARKING BRAKE FITTING, 3 O'CLOCK POSITION WHEN LOOKING FORWARD, REPAIRED IAW REO. PRESSURE CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 409-599) · airframe 40,716 hrs · 36,238 cycles

SEAT TRACK AT RBL 9.0 BS 409+126 - 599 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 40,716 hrs · 36,238 cycles

CRACK NOTED ON FS621 BULKHEAD WEB, FWD FACE, ALONG LBL36.2 AT APPROXIMATELY WL 75 NEAR FLOOR LEVEL. C-CHECK, REPAIRED CRACK IAW REO. PARTS REMOVED WEIGHT 0.01 LBS, REPLACEMENT PARTS WEIGH 0.40 LBS, NET WEIGHT GAINED 0.39 LBS. SCALE TUC 1755, DUE 30 JUN 2015. PRESSURE CHECK C/W CHECKS GOOD IAW AMM,

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 40,716 hrs · 36,238 cycles

SEAT TRACK AT RBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.

Part: PANEL — CRACKED (UNKNOWN) · airframe 40,716 hrs · 36,238 cycles

PANEL 221CLC HAS CRACKS AROUND SCREW HOLE. REPAIRED CRACKS AROUND SCREW HOLE ON PANEL IAW EA.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

LEFT INBD FLAP HAS DENT ON LOWER SKIN OUTBD OF PANEL 584AB. REPAIRED IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

RT WING INBD FLAP VANE L/E CHAFED 70.5" FROM OTBD END. BLENDED AND REPAIRED IAW REO.

Part: BELLCRANK — CHAFED (RT MLG DOOR) · airframe 40,716 hrs · 36,238 cycles

RT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. C-CHECK, OUT OF LIMITS IAW DWG. R & R RT MLG DOOR BELLCRANK ASSY, REF AMM, CW REO.

Part: ROD END — CHAFED (RT MLG DOOR) · airframe 40,716 hrs · 36,238 cycles

RIGHT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE RT MLG DOOR STRUT.

Part: SKIN — CHAFED (LT AILERON) · airframe 40,716 hrs · 36,238 cycles

LEFT AILERON UPPER L/E CHAFED. LT AILERON UPPER L/E SHROUD FOUND TO BE OUT OF LIMITS IAW REO REPLACED.

Part: PANEL — CRACKED · airframe 40,716 hrs · 36,238 cycles

PANEL 222CLC, HAS CRACKS AROUND SCREW HOLE. REPAIRED PANEL IAW EA.

Part: ATTACH FITTING — CHAFED (LT MLG DOOR) · airframe 40,716 hrs · 36,238 cycles

LEFT MLT DOOR ROD ATTACH LUG ON DOOR IS CHAFED. C-CHECK, R & R THE LT MLG DOOR ATTACHMENT LUG REF SRM & REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

LEFT INBD FLAP VANE CHAFED AT CENTER L/E. BLENDED IAW REO.

Part: ROD END — CHAFED (LT MLG DOOR) · airframe 40,716 hrs · 36,238 cycles

LEFT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE LT MLG DOOR STRUT IAW AMM, DWG AND REO.

Part: BELLCRANK — CHAFED (LT MLG DOOR) · airframe 40,716 hrs · 36,238 cycles

LT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. R & R THE LT MLG DOOR BELLCRANK ASSY REF AMM, COMPLIED WITH REO AND DWG.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED 7.5" FROM OTBD END. BLENDED IAW REO. FOUND WITHIN LIMITS IAW REO.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

RT WING INBD FLAP VANE L/E HAS SMALL GOUGE 27.5" FROM OTBD END. BLENDED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED 43 INCHES FROM OTBD END. BLENDED CHAFE IAW REO AND SRM. FOUND WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,716 hrs · 36,238 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED 91.5 INCHES FROM OTBD END. BLENDED CHAFE IAW REO.

Part: PANEL — DAMAGED (COCKPIT) · airframe 40,716 hrs · 36,238 cycles

PANEL 326AL ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL 326AL. FOUND WITHIN LIMITS IAW REO.

Part: PANEL — FAILED · airframe 40,716 hrs · 36,238 cycles

PANEL 326BR, ZONE 300 FAILED GAP CHECK, CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.

Part: PANEL — DAMAGED · airframe 40,716 hrs · 36,238 cycles

PANEL 326AR, ZONE 300 FAILED GAP CHECK. CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.

Part: PANEL — FAILED · airframe 40,716 hrs · 36,238 cycles

PANEL 326BL, ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL IAW REO AND AMM.

Part: SKIN — FAILED (FWD FUSELAGE) · airframe 40,716 hrs · 36,238 cycles

DENTED LT FUSELAGE SKIN PANEL ON NOSE, BELOW CAPTAIN'S WINDOW. REPAIRED IAW REO.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 39,721 hrs · 35,422 cycles

LT ENGINE FORWARD MOUNT YOKE BUSHING HAS GALLING. INSTALLED NEW LT ENGINE FWD YOKE MOUNT IAW AMM.

Part: TORQUE LINK — GALLED (ENGINE MOUNT) · airframe 39,721 hrs · 35,422 cycles

LT ENGINE FORWARD MOUNT TORQUE LINK ASSEMBLY HAS GALLING IN BUSHING. INSTALLED NEW LINK ON THE LT ENGINE FWD YOKE MOUNT IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 39,497 hrs · 35,246 cycles

LEFT OVERWING EMERGENCY LIGHT IS BURNED OUT. R & R LT OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW AMM.

Part: AUTOPILOT SYS — DISCONNECTED · airframe 39,504 hrs · 35,252 cycles

AUTOPILOT INITIATED UNCOMMANDED PITCH CHANGE A/P WAS MANUALLY DISCONNECTED, FLIGHT PATH CORRECTED AND REENGAGED WITHOUT FURTHER INCIDENT. PERFORMED SERVO SPIN TEST IAW AMM. NO DEFECTS NOTED AND NO RELEVENT MDC MESSAGES WERE FOUND.

Part: BUSHING — DAMAGED (ENGINE MOUNT) · airframe 39,417 hrs · 35,170 cycles

LEFT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING HAS CORRODED. REPLACED LT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 39,198 hrs · 35,004 cycles

FORWARD EMERGENCY LIGHT OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.

Part: SIGN — BURNED OUT (EMERGENCY LIGHTS) · airframe 39,046 hrs · 34,894 cycles

LOWER RIGHT OVERWING EXIT EMERGENCY SIGN IS BURNED OUT. REPLACED SIGN AND INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,918 hrs · 34,037 cycles

CEILING EMERGENCY LIGHT IN AFT POSITION BURNED OUT. FLT#5374 RELAMPED, PN 1317.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,604 hrs · 33,797 cycles

CEILING POD LIGHT ABEAM BURNED OUT. FLT#6224 RELAMPED.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 36,751 hrs · 33,170 cycles

RECEIVED GEAR DISAGREE WARNING MSG. BY THE TIME WE RAN CHECKLIST, ISSUE SELF-CORRECTED. NO PROBLEMS WITH LANDING GEAR EXTENSION ON LANDING. REPLACED 3A ELECTRIC HYD PUMP IAW AMM, PN: 848847, SN ON: MX572122, SN OFF: MX520285.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,638 hrs · 33,077 cycles

TRU WEB IS CRACKED AT FS 193 RIGHT. (C-CHECK) REPAIRED TRU WEB AT FS 193.00 RIGHT IAW REO.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,638 hrs · 33,077 cycles

TRU WEB IS CRACKED AT FS 193 LEFT. (C-CHECK) INSTALLED REPAIR ON TRU WEB FS 193 LEFT IAW REO.

Part: CAP — WORN (TE FLAP VANE) · airframe 36,638 hrs · 33,077 cycles

LEFT INBD FLAP, INBD FLAP VANE CAP IS WORN BEYOND LIMITS. (C-CHECK) REPLACED WORN LEFT INBD FLAP, INBD FLAP VANE CAP IAW SRM.

Part: CAP — WORN (TE FLAP VANE) · airframe 36,638 hrs · 33,077 cycles

RIGHT INBD FLAP, MIDDLE FLAP VANE CAP IS WORN BEYOND LIMITS. (C-CHECK) REPLACED RIGHT INBD MIDDLE FLAP VANE ON RIGHT INBD FLAP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,267 hrs · 32,769 cycles

LOWER EMERGENCY LIGHT BY MAIN CABIN DOOR BURNED OUT. (FLT 6304) RELAMPED EMERGENCY LIGHT.

Part: CONTROL CABLE — FAILED (LT THROTTLE) · airframe 35,329 hrs · 32,007 cycles

DURING CLIMB THRUST SETTING, LEFT THRUST LEVER HAD MOVEMENT BUT NO N1 THRUST REDUCTION. AFTER CYCLING THRUST, N1 STOPPED AT 93% AND WOULD NOT FURTHER TO THROTTLE MOVEMENT. INITIALLY STARTED QRH SINGLE ENGINE PROCEDURE, BUT THRUST LEVER WOULD NOT SHUT OFF. USED THE ENGINE FIRE PUSH TO SECURE THE ENGINE. (FLT 6433) REPLACED LEFT ENGINE THROTTLE CONTROL CABLE IAW CRJ 200 MM. P/N: 1603730-007

Part: SKIN — DENTED (FUSELAGE) · airframe 35,328 hrs · 32,006 cycles

LEFT LOWER FORWARD FUSELAGE SKIN HAS A DENT. (SERVICE) REPAIRED LOWER FORWARD FUSELAGE SKIN IN REFERENCE TO REO.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 35,034 hrs · 31,745 cycles

LEFT PACK OVERTEMP CAUTION MESSAGE ON GROUND, WITH SMOKE COMING OUT OF THE AIR VENT. (FLT 6255) REPLACED LEFT AIR CYCLE MACHINE. P/N: 782790-15 S/N OFF: 9906073

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,446 hrs · 31,291 cycles

EMERGENCY LIGHTS NEAR MAIN CABIN DOOR ARE OUT. (FLT 6283) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,305 hrs · 31,195 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6348) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,008 hrs · 30,968 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5480) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,383 hrs · 29,661 cycles

PAX DOOR EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: POST — CRACKED (FUSELAGE) · airframe 32,352 hrs · 29,635 cycles

FS 409.00+128 RBL 18.0 OUTBOARD LOWER RADIUS OF VERTICAL POST IS CRACKED. (C-CHECK) REPLACE VERTICAL POST PER SRM AND REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 32,352 hrs · 29,635 cycles

PAX DOOR INTERCOSTAL BETWEEN FS 311 TO FS 320 IS CRACKED. (C-CHECK) REPLACED INTERCOSTAL PER SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 32,352 hrs · 29,635 cycles

(C-CHECK) FS 409 + 128 RBL 18.00 INBOARD AFT RADIUS OF VERTICAL POST IS CRACKED. REPLACED POST PER SRM.

Part: COVER — OUT OF ADJUST (SERVICE DOOR) · airframe 33,827 hrs · 30,823 cycles

SERVICE DOOR HANDLE COVER CATCHES ON HINGE ARM WHEN OPENING. (C-CHECK) ADJUSTED SERVICE DOOR HANDLE COVER PER SRM.

Part: STRUCTURE — CORRODED (BS 320-329) · airframe 33,966 hrs · 30,938 cycles

C-CHECK, CORROSION AT DATUM NR 1 BETWEEN FS 320.10 AND FS 329.75 OF PASSENGER DOOR. REPAIRED CORROSION AT DATUM NR 1 BETWEEN FS 320.10 AND FS 329.75 PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,827 hrs · 30,823 cycles

FLOOR SUPPORT ANGLE AT FS 621 LBL 41 IS CRACKED. (C-CHECK) REPAIRED FLOOR SUPPORT ANGLE AT FS 621 LBL 41 PER CRJ200 SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,827 hrs · 30,823 cycles

CRACK ON INTERCOSTAL AT FS 319 DATUM 6 AT LOWER PORTION PAX DOOR. (C-CHECK) REPLACED INTERCOSTAL AT FS 319 DATUM 6.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,827 hrs · 30,823 cycles

CORROSION ON INNER FORMER OUTER INTERCOSTAL LOWER PAX DOOR FS 320.10 TO FS 338.00. (C-CHECK) REPLACED INTERCOSTAL IN PAX DOOR PER SRM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 33,827 hrs · 30,823 cycles

CRACK ON INTERCOSTAL BETWEEN FS 338.75 AND FS 347.25 AFT LOWER INNER SECTION PASSENGER DOOR. (C-CHECK) REPLACED INTERCOSTAL BETWEEN FS 338.75 AND FS 347.25 IN REF CRJ200 SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,827 hrs · 30,823 cycles

PASSENGER DOOR FRAME AT FS 320.0 CRACKED UNDER THE HINGE AREA FOR THE BOTTOM FOLDING STEP. (C-CHECK) REPLACED PASSENGER DOOR FRAME AT FS 320.0 PER REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 33,827 hrs · 30,823 cycles

PAX DOOR INTERCOSTAL AT FS 342.0 AND DATUM 1 UPPER AFT CORNER CRACKED. (C-CHECK) REPLACED PAX DOOR INTERCOSTAL AT FS 342.0.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 33,827 hrs · 30,823 cycles

CRACKED INTERCOSTAL BETWEEN FS 311.75 AND FS 320.25 AFT LOWER INNER SECTION OF PAX DOOR. (C-CHECK) REPLACED INTERCOSTAL AT FS 311.75 AND 320.25 IN REF CRJ200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,352 hrs · 29,635 cycles

GALLEY SERVICE DOOR EMERGENCY LIGHT IS OUT. (FLT 5383) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,166 hrs · 29,504 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5342) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,581 hrs · 28,994 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6248) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,715 hrs · 28,301 cycles

AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6247) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,457 hrs · 28,080 cycles

EMERGENCY LIGHTS OVER ROW 4 INOPERATIVE. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,397 hrs · 28,036 cycles

LAST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6375) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,397 hrs · 28,036 cycles

RIGHT WING EXTERIOR EMERGENCY LIGHT OUT. (FLT 6850) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,028 hrs · 27,727 cycles

MIDDLE RIGHT EMERGENCY LIGHT OVERWING AND AFT LEFT SIDE EMERGENCY LIGHT OVER WING INOPERATIVE. (FLT 6631) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,973 hrs · 27,672 cycles

AFT CABIN EMERGENCY CEILING FLOODLIGHT INOPERATIVE. (FLT 6918) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,690 hrs · 27,441 cycles

NR 1 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6744) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,151 hrs · 26,994 cycles

NR 3 CEILING LEVEL FLOODLIGHT INOP. (FLT 6867) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,767 hrs · 26,632 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 5868) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,489 hrs · 26,411 cycles

EMERGENCY LIGHTS NR 3 AND NR 4 INOP. (FLT 6833) RELAMPED EMERGENCY LIGHTS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 27,989 hrs · 25,991 cycles

FLT 6341 - MOST AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 28,270 hrs · 26,223 cycles

FS 280 BULKHEAD GOUGED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,270 hrs · 26,223 cycles

FS 280 LEFT OUTBOARD CLIP CRACKED. (C CHECK) REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,270 hrs · 26,223 cycles

FS 621 BULKHEAD WEB CRACKED AT AFT CARGO DOOR ROLLER GUIDE RAIL. (C CHECK) REPAIRED PER REO.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 28,270 hrs · 26,223 cycles

FS 559 DAMAGED AT LBL 18 AND LBL 9 FRAME CAPS. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,816 hrs · 25,839 cycles

OVERHEAD EMERGENCY LIGHT BY LAV INOP. (FLT 6484) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,538 hrs · 25,625 cycles

OVERWING LEFT EMERGENCY DOOR FLOODLIGHT INOP. (FLT 6583) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,428 hrs · 25,538 cycles

SECOND TO LAST CEILING EMERGENCY LIGHT INOP. (FLT 6359) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 27,428 hrs · 25,538 cycles

EMERGENCY EXIT SIGN AT 8A INOP. (FLT 6408) REPLACED EXIT SIGN.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 27,214 hrs · 25,369 cycles

EMERGENCY EXIT LIGHT INOP. (FLT 6541) RESEATED CONNECTOR.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,214 hrs · 25,369 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. (FLT 6228) DOWN POWERED AIRCRAFT, OPERATION NORMAL ON POWER UP.

Part: CONNECTOR — DIRTY (CABIN) · airframe 27,180 hrs · 25,341 cycles

FLOOR LEVEL EMERGENCY LIGHT INOP. (FLT 6416) CLEANED CONNECTOR.

Part: CIRCUIT CARD — CORRODED · airframe 26,459 hrs · 24,759 cycles

C-CHECK, CORROSION ON NR 1 HIRF CARD. REPLACED CARD.

Part: RELAY — OVERHEATED · airframe 26,459 hrs · 24,759 cycles

C-CHECK, RELAY K1LL SHOWS SIGNS OF OVERHEATING. REPLACED RELAY.

Part: PLUNGER — INOPERATIVE (PAX DOOR HANDLE) · airframe 26,077 hrs · 24,353 cycles

UNABLE TO OPEN MAIN CABIN DOOR. (FLIGHT NR 2791) INSPECTED AND CLEANED INNER HANDLE PLUNGER. REPLACED PAX DOOR WHEEL SPRING IAW MM 52-11-13. OPS CHECK GOOD.

Part: CHARGER — FAULTY (CABIN) · airframe 25,282 hrs · 23,564 cycles

FLT 2871 - EMERGENCY LIGHTS CYCLE ON AND OFF DURING FLIGHT. REPLACED NR 4 BATTERY PACK AND CHARGER IAW AMM 33-51-04. OPS CHECK GOOD, PN AD-2013-1A SN/OFF 66453.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 25,120 hrs · 23,425 cycles

FLT 1001 - SMOKE TOILET CAUTION MESSAGE ON APPROACH WITH NO SMOKE OBSERVED. INSPECTED AND CLEANED SMOKE DETECTOR. OPS CHECK GOOD PER 26-16-00.

Part: FRAME — CRACKED (BS 682) · airframe 25,520 hrs · 23,762 cycles

STN 682.00 AT LBL 4.0 AND WL47.5 FRAME IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW FRAME ANGLE PER CRJ200 SRM 51-42-06 P 11 AND 51-42-21 P 17.

Part: FRAME — CRACKED (BS 280) · airframe 25,520 hrs · 23,762 cycles

STN 280 AT RBL 9.0 ON LOWER FRAME IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER REO601R 53-11-171 REV D.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 25,520 hrs · 23,762 cycles

FORWARD KEEL BEAM FITTING ATTACHMENT HARDWARE IS CORRODED, FOUND AT C-CHECK. REPLACED KEEL BEAM ATTACHING HARDWARE PER CRJ200 REO 601R-53-31-034 AND DRAWING 601R31060 FLAG NOTE 27.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,190 hrs · 21,910 cycles

FLIGHT 5196 - ONE SEGMENT OF FLOOR EMERGENCY LIGHTS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHT, OPS CHECK GOOD. NO FURTHER DEFECTS.

Part: SERVICE DOOR — OPEN (OXYGEN SYSTEM) · airframe 22,972 hrs · 21,726 cycles

FLIGHT 5519 - AFTER DEPARTURE FROM JFK THE OXYGEN SERVICE DOOR OPENED. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. SECURED OXYGEN SERVICE DOOR CLOSED.

Part: LANDING GEAR — LACK OF LUBE · airframe 21,524 hrs · 20,249 cycles

FLIGHT 5857 - INBOUND TO CVG RECEIVED A LANDING GEAR DISAGREE MESSAGE, CREW DECLARED AN EMERGENCY, ABORTED APPROACH THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. CHECKED UPLOCK AND PROXIMITY SENSORS FOR CORRECT ADJUSTMENT, LUBRICATED LANDING GEAR AND PERFORMED GEAR SWINGS. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 20,437 hrs · 19,631 cycles

FLIGHT 5196 - PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,276 hrs · 19,489 cycles

FLIGHT 5795- LEFT ENGINE REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON T/R PER MEL.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,118 hrs · 19,355 cycles

FLIGHT 5805 - EN ROUTE LGA-GSP RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE. CREW DIVERTED TO JFK, FLIGHT LANDED WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,056 hrs · 19,295 cycles

FLIGHT 5606 - LT REVERSER UNLOCKED CAUTION. FOUND NO DEFECTS. T/R WAS ON DEFERRED MAINTENANCE LIST.

Part: WARNING LIGHT — ILLUMINATED (STALL FAIL) · airframe 18,931 hrs · 18,311 cycles

FLIGHT 5687 STALL FAIL MESSAGE AFTER T/O. FOUND 02 SERVICE DOOR OPEN. CLOSED DOOR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,239 hrs · 16,835 cycles

SKIN RADIUS AT FS 235, BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT CORNER CRACKED APPROXIMATELY .25 INCH. REPAIRED IAW REO 601R-53-11-048.

Part: FRAME — CRACKED (FUSELAGE) · airframe 16,662 hrs · 16,356 cycles

CRACK ON LEFT HAND FS 718 BETWEEN STRINGER 11 AND 12. REPAIRED FRAME BETWEEN STRINGER 11 AND 12 ON CT FS 718.00 IAW REO 601R-53-61-193.

Part: ANTI-ICE VALVE — FAULTY (LEFT) · airframe 16,564 hrs · 16,262 cycles

FLIGHT 5351 WING OVERHEAT MESSAGE. REPLACED THE LEFT WING MODULATING VALVE.

Part: HYDRAULIC LINE — LEAKING (LT MLG WW) · airframe 16,192 hrs · 15,952 cycles

FLIGHT 5588 HYDRAULIC SYSTEM 2 LOW PRESSURE CAUTION. REPLACED DEFECTIVE HYDRAULIC LINE IN LEFT WHEEL WELL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 14,225 hrs · 14,299 cycles

FLIGHT 5118 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY PACKS.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 14,066 hrs · 14,158 cycles

FLIGHT 5879 RIGHT ENGINE OVER TEMPERATURE, INDICATED 901 DEGREES CELSIUS. REPLACED ENGINE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,496 hrs · 13,645 cycles

FLIGHT 5132 EMERGENCY FLOOR PATH LIGHTING ROWS 1 THRU 5 IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY.

Part: FAN · airframe 13,434 hrs · 13,584 cycles

FLIGHT 5490 VIB WARNING WHEN T/O THRUST APPLIED.COULD NOT DUPLICATE - INSPECTED ENGINE AND FOUND NO DISCREPANCIES, C/W A FAN TRIM BALANCE AND REDUCED VIB FROM .9 TO .4

Part: ENGINE · airframe 13,266 hrs · 13,440 cycles

FLIGHT 5658 N2 VIB INDICATION DURING T/O.COULD NOT DUPLICATE. VIB INDICATIONS WERE WITHIN LIMITS DURING MAINTENANCE RUNS.

Part: ENGINE · airframe 13,248 hrs · 13,425 cycles

FLIGHT 5048 LEFT ENGINE N2 VIB INDICATION.COULD NOT DUPLICATE. NO VIB INDICATIONS DURING ENGINE RUNS.

Part: ENGINE · airframe 13,143 hrs · 13,322 cycles

FLIGHT 5115 LEFT ENGINE N2 VIBE MESSAGE DURING T/O.COULD NOT DUPLICATE, INSPECTED ENGINE, FOUND NO DEFECTS.

Part: ENGINE · airframe 12,801 hrs · 13,020 cycles

FLIGHT 5511 LEFT ENGINE VIB MESSAGE.COULD NOT DUPLICATE. NO VIB LOGGED IN MDC.

Part: COMPUTER — MALFUNCTIONED (LEFT ENGINE) · airframe 12,801 hrs · 13,021 cycles

FLIGHT 5585 LEFT ENGINE VIB MESSAGE.COULD NOT DUPLICATE REPLACED THE VIB SIGNAL CONDITIONER.

Part: WING · airframe 12,717 hrs · 12,938 cycles

FLIGHT 5229 ANTI-ICE DUCT WARNING.COULD NOT DUPLICATE. INSPECTED BLEED LEAK SENSORS AND WIRING.

Part: ACCELEROMETER — MALFUNCTIONED (LT ENG) · airframe 12,388 hrs · 12,628 cycles

FLIGHT 5058 N2 VIB INDICATION, LEFT ENGINE DURING T/O.REPLACED THE LT ENGINE EVM TRANSDUCER.

Part: PUMP — FAILED (RT ENGINE) · airframe 7,584 hrs · 7,765 cycles

FLIGHT 5310. DURING CRUISE FLIGHT RECEIVED A #2 HYDRAULIC SYSTEM LOW RESSURE CAUTION MESSAGE, UNSCHEDULED LANDING AT CLE, AIRCRAFT LANDED SAFELY.REPLACED THE #2 ENGINE DRIVEN HYDRAULIC PUMP.

Part: INSULATION — CONTAMINATED (CARGO) · airframe 11,546 hrs · 11,816 cycles

FLIGHT 5861 STRONG ROW FUEL ODOR IN CABIN AND COCKPIT.REMOVED FUEL CONTAMINATED INSULATION UNDER CARGO FLOOR - CLEANED BELLY OF A/C AND REPLACED INSULATION.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 11,022 hrs · 11,277 cycles

EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 1-5. REPLACED FLOOR LIGHTS CABLE ASSEMBLY.

Part: FLAP · airframe 10,971 hrs · 11,220 cycles

FLIGHT 5801 FLAPS FAILED WHEN SELECTED UP AFTER LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: FLAP · airframe 10,747 hrs · 11,011 cycles

FLIGHT 5360 FLAPS FAILED AT 20 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: O-RING — DAMAGED (APU) · airframe 10,632 hrs · 10,906 cycles

FLIGHT 5310 JET FUEL SMELL IN COCKPIT WITH LEFT A/C PACK OPERATING. REPLACED LEAKING O-RING ON APU FUEL CONTROL.

Part: FLAP · airframe 10,500 hrs · 10,767 cycles

FLIGHT 5712 FLAPS FAILED DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: FLAP · airframe 10,451 hrs · 10,714 cycles

FLIGHT 9872 FLAPS FAIL CAUTION MESSAGE.COULD NOT DUPLICATE, INTEROGATED FLAP COMPUTER, NO DEFECTS NOTED.

Part: BPSU — MALFUNCTIONED (L/H) · airframe 10,270 hrs · 10,539 cycles

FLIGHT 5450 FLAPS FAILED AT 28 DEGREES DURING LANDING ROLL.REPLACED THE L/H BPSU.

Part: FLAP · airframe 10,160 hrs · 10,420 cycles

FLIGHT 5598 - FLAPS FAILED AT 28 DEGREES AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: VALVE — MALFUNCTIONED (R/H) · airframe 10,102 hrs · 10,360 cycles

FLIGHT 5791 R/H ENGINE COWL ANTI ICE CAUTION MESSAGE.REPLACED THE COWL ANTI ICE VALVE

Part: BPSU — MALFUNCTIONED (R/H) · airframe 9,816 hrs · 10,067 cycles

FLIGHT #6054 FLAPS FAILED AT 8 DEGREES.REPLACED THE R/H BPSU.

Part: ANGLE — CORRODED (F.S.280) · corrosion level 2 · airframe 9,666 hrs · 9,922 cycles

FWD/J - ANGLE AT F.S. 280 HAS CORROSION.REPAIRED FWD J-ANGLE I/A/W WVAC EO 601R-53-2775.

Part: WEB — CRACKED (BEAM) · airframe 9,666 hrs · 9,922 cycles

L/H AND R/H LOWER WEBS ARE CRACKED ON ENGINE SUPPORT BEAM AT F.S. 625.30.REPAIRED L/H AND R/H LOWER WEBS I/A/W CANADAIR R.E.O. 601R-53-61-366 REV. C.

Part: ACTUATOR — BINDING · airframe 9,203 hrs · 9,405 cycles

FLAPS FAILED AT 8 DEGREES.REPLACED THE LEFT HAND #3 FLAP ACTUATOR.

Part: FLAP — MALFUNCTIONED · airframe 9,203 hrs · 9,404 cycles

FLAPS FAILED AT 45 DEGREES.REPLACED THE FECU.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 8,301 hrs · 8,515 cycles

GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 8,228 hrs · 8,444 cycles

STAB TRIM AND MACH TRIM DISENGAGED. WOULD NOT RESET. REPLACED THE HSTCU.

Part: SENSOR — MALFUNCTIONED (RT WING) · airframe 7,964 hrs · 8,179 cycles

RIGHT HAND WING OVERHEATER WARNING. REPLACED WING TEMP SENSOR.

Part: IDG — LACK OF LUBE (NR 1 GENERATOR) · airframe 7,704 hrs · 7,916 cycles

GENERATOR NR 1 OFF CAUTION MESSAGE. SERVICED THE IDG TO PROPER OIL LEVEL, SYSTEM CHECKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,650 hrs · 7,857 cycles

DAMAGE TO FUSELAGE SKIN FROM APU DOOR SCREWS SHEARING AND SLAMMING THE DOOR AFT. REPAIRED FUSELAGE SKIN AROUND APU INLET DOOR IAW WVAC EO 601R-53-1501B. SHEARED SCREWS WERE REPLACED ON LOG BOOK ENTRY 198257.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,650 hrs · 7,857 cycles

DAMAGED TO FUSELAGE SKIN FROM APU DOOR SCREWS SHEARING AND SLAMMING THE DOOR AFT. REPAIRED FUSELAGE SKIN AROUND APU INLET DOOR IAW WVAC EO 601R-53-1501B. SHEARED SCREWS WERE REPLACED ON LOG BOOK ENTRY 198257.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,617 hrs · 7,825 cycles

FUSELAGE SKIN FWD OF PAX DOOR AT FS 310 HAS DAMAGE FROM DOOR PIN. REPAIRED FUSELAGE SKIN IAW CANADAIR REO 601R-53-21-180.

Part: ACTUATOR — BINDING (TE FLAP)

FLAPS FAIL MESSAGE DURING APPROACH. REPLACED LEFT I/B FLAP ACTUATORS.

Part: FLAPS — FAILED (LT & RT WING)

FLAPS FAILED. RESET FLAP SYSTEM PER AD 98-20-01.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: DOUBLER — CRACKED (BS 718)

DOUBLER CRACKED AT FS 718 AT STRINGER 11 ON RIGHT SIDE. REPLACED WITH NEW DOUBLER.

Part: ANGLE — CRACKED (BS 621)

CARGO FLOOR SUPPORT ANGLE AT FS 621 WL 73, LEFT SIDE IS CRACKED. REPAIRED PER CANADAIR REO 601R-53-61-117 REV A.

Part: LIGHT — CRACKED (CABIN)

EMERGENCY LIGHT FLOOR TRACK LIGHT (P/N 5873-1) IS CRACKED AND THE END CAPS ARE MISSING. REPLACED TRACK LIGHT.

Part: LIGHT — BROKEN (CABIN)

FORWARD FUSELAGE EMERGENCY LIGHTING STRIP IS BROKEN. REPLACED LIGHTING STRIP.

Part: DOUBLER — CRACKED (BS 718)

DOUBLER CRACKED AT FS 718 AT STRINGER 11 ON LEFT HAND SIDE. REPLACED WITH NEW DOUBLER.

Part: FRAME — CRACKED (BS 718)

FRAME FLANGE AT FS 718 STRINGER 11 ON RIGHT SIDE CRACKED. REPAIRED IN ACCORDANCE WITH WVAC E 601R-53-0075, SRM 51-42-21.

Part: STRIKER — DAMAED (PAX DOOR)

PAX DOOR SEAL STRIKER DAMAGED AT FS 310, LOWER PART OF OPENING. REPAIRED PAX DOOR SEAL STRIKER IN ACCORDANCE WITH REO 601-52-11-008 REPAIR A.

Part: LIGHT — CRACKED (CABIN)

EMERGENCY FLOOR TRACK LIGHT (P/N 5872-8) HAS SEVERAL BREAKS AND IS MISSING END CAPS. REPLACED TRACK LIGHT.

Part: FRAME — CRACKED (BS 71800)

FRAME 71800, STR 11 CRACKED AT FLANGE AND AFT SIDE DOUBLER ON RHS FUSELAGE AND AT AFT SIDE DOUBLER ON LHS FUSELAGE STR 11, FS 17800. REPLACED FRAME 71800 RHS IAW WVAC EO 601R530075. REPAIRED DOUBLER AT FS 71800 + STR 11 RHS IAW WVAC EO 601R530073. REPAIRED DOUBLER AT FS 71800 + STR 11 LHS IAW WVAC EO 601R530072.

Part: ANGLE — CRACKED (BS 62100)

CARGO FLOOR SUPPORT ANGLE AT FS 62100, WL 73 LEFTHAND SIDE IS CRACKED. REMOVED CRACKED PART AND REPLACED WITH NEW ANGLE AND DOUBLER IAW CANADAIR REO 601R5361117, REV A.

Part: GENERATOR — FAILED (NR 2)

NR 2 GENERATOR FAULT MESSAGE DURING TAKEOFF. ABORTED AND RETURNED TO THE GATE. DEFERRED NR 2 GENERATOR.

Part: WINDSHIELD — SHATTERED (LT COCKPIT)

PILOTS WINDSHIELD SHATTERED.\NREPLACED WINDSHIELD.

Part: SENSOR — DEFECTIVE (RT WING)

WING ANTI ICE DUCT MESSAGE. REPLACED 7 DEFECTIVE OVERHEAT SENSORS IN RIGHT HAND WING.

Part: DAMPENER — LEAKING (RT AILERON)

RIGHT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER.

Part: FLEXSHAFT — CORRODED (RT TE FLAP)

RIGHT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT.

Part: FLEXSHAFT — CORRODED (LT TE FLAP)

LEFT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT.

Part: DAMPENER — LEAKING (LT AILERON)

LEFT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER.

Part: LAMP — FAILED (LT EXTERIOR)

LEFT HAND EXTERIOR EMERGENCY LIGHT INOPERABLE. REPLACED LAMP.

Part: PITOT — CONTAMINATED (FWD FUSELAGE)

AIRSPEED COMPARATOR WARNING DURING TAKEOFF. PURGED WATER FROM THE PITOT SYSTEM.

Part: WARNING — ACTIVATED (RT BLEED AIR)

LEFT HAND AND RIGHT HAND BLEED AIR DUCT LEAK WARNING MESSAGE. COULD NOT DUPLICATE DISCREPANCY. SYSTEM TEST WAS NORMAL.

Part: HSTCU — MALFUNCTIONED (E/E COMPT)

STAB CHANNEL 1 DISENGAGED DURING APPROACH. REPLACED THE HSTCU.