N701BR

Part: NONE — FAILED · airframe 43,856 hrs · 36,606 cycles

WHILE CONFIGURING FOR LANDING AND SELECTING GEAR DOWN RECEIVED €˜GEAR DISAGREE€™ WARNING MESSAGE. RAN QRH FOR GEAR DISAGREEMENT MESSAGE CLEARED AND CONFIRMED GEAR DOWN AND LOCKED. (FLIGHT 5310 - FILED CLOSED) TROUBLESHOT GEAR DISAGREE MESSAGE IN REF TO FIM 32-60-07. NO FAULTS STORED ON PSEU, REMOVED AND REPLACED MAIN LANDING GEAR PRIORITY VALVE WITH SERVICEABLE UNIT IN REF TO AMM 32-32-15. PERFORMED GEAR EXTENSION AND RETRACTION FUNCTIONAL CHECKS WITH NO DEFECTS NOTED IN REF TO AMM 07-11-01. RESTORED AIRCRAFT TO NORMAL CONFIGURATION, OK FOR RETURN TO SERVICE. PLEASE REFERENCE AML 947390 PLEASE REFERENCE AML 947471 PLEASE REFERENCE AML 947390 PLEASE REFERENCE AML 947471

Part: NONE — NONE · airframe 43,255 hrs · 36,081 cycles

ON APPROACH, AFTER SELECTING LANDING GEAR DOWN, GEAR DISAGREE WARNING, WITH NOSE WHEEL INDICATING DOWN AND GREEN, WITH BOTH MAINS RED. SIMULTANEOUSLY, HYD 3 LOPRESS CAUTION POPULATED. INITIATED MISSED APPROACH. DURING INITIAL CLIMB BOTH MAINS CHANGED TO INDICATE DOWN AND LOCKED. HYDRAULIC 3 CAUTION REMAINED, WITH SYNOPTIC PAGE INDICATING APPROXIMATELY 5% VOLUME ON HYD SYSTEM 3.INBOARD BRAKE PRESSURE BLED OFF TO 0 OVER APPROXIMATELY 5 MINUTES. RAN HYD 3LO PRESS QRH. PULLED AND SUBSEQUENTLY STOWED GEAR MANUAL EXTENSION HANDLE ACCORDING TO QRH PROCEDURE. EMERGENCY WAS DECLARED, SUCCESSFUL LANDING AND TOWED TO GATE. (FLIGHT 5100 - FILED CLOSED) PLEASE REFERENCE AML 853891, ALSO REFERENCE AML 852752 FOR CORRECTIVE ACTION , REMOVED AND REPLACED A BURST HYDRAULIC SYSTEM 3A ACMP PRESSURE LINE. CLEANED BOTH SYSTEM 3A AND 3B PUMP AREAS AS REQUIRED, PRESSURIZED SYSTEM AND NO LEAKS WERE NOTED. PERFORMED SEVERAL NORMAL GEAR SWINGS AND AN EMERGENCY EXTENSION. LANDING GEAR SYSTEM OPERATES NORMALLY REFERENCE CRJ-200 AMM 32-30-00. ALSO 32-34-00. NO HYDRAULIC SYSTEM CAUTION MESSAGES POSTED. / OK FOR CONTINUED SERVICE.

Part: SKIN — CRACKED (RT WING LE) · airframe 42,463 hrs · 35,369 cycles

RIGHT WING LEADING EDGE SKIN AT WS 199.0 HAS A 2.25 INCH VERTICAL CRACK. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. REFERENCE CP 23174513 FOR ORIGINAL WRITE UP. (FILED CLOSED) REPLACED R/H WING LEADING EDGE SKIN IN REFERENCE TO CRJ200 SRM 51-77-00 AND RIVETS INSTALLED SRM 51-42-06 ALSO PART NUMBER FOR NEW SKIN IS PCN-601R12057-1-2-121120080427. ALSO FORM M-337 COMPLETED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 41,982 hrs · 34,947 cycles

CAPTAIN WINDOW CRACKED ON CLIMB OUT REMOVED AND REPLACED LH SIDE WINDOW IN REF TO AMM 56-12-01, OPS AND LEAK CHECK GOOD AT THIS TIME. / PLEASE REFERENCE AML 606661 PLEASE REFERENCE AML 606670

Part: SERVO — OVERSERVICED · airframe 41,706 hrs · 34,704 cycles

FIRST OFFICER LEG, ON FINAL APPROACH AFTER DISCONNECTING AUTOPILOT, FLIGHT CONTROLS LOCKED UP AND FO HAD TO APPLY FAIRLY STRONG FORCE TO GET PITCH MOVEMENT OF YOKE TO UNLOCK. THEN TO MAKE ROLL ADJUSTMENTS IN FLIGHT, HAD TO APPLY SIMILAR FORCE TO UNLOCK ROLL MOVEMENT. FLIGHT 5808-FILED CLOSED. PER FLEET COORDINATORS REQUEST WE PERFORMED INSPECTIONS ON BOTH AILERON AND ELEVATOR AUTO PILOT SERVOS. IN REFERENCE TO AMM 22-11-21 FOR THE AILERON AND AMM 22-11-24 FOR THE ELEVATOR SERVO WE REMOVED BOTH SERVOS AND FOUND BOTH TO BE OVER LUBRICATED. CLEANED THE EXCESS GREASE OFF OF BOTH SERVOS AND SERVO MOUNTS IN REFERENCE TO AMM 22-11-21 AND AMM 22-11-24. RE-LUBED BOTH SERVOS IN REFERENCE TO AMM 22-11-14. REINSTALLED AILERON SERVO IN REFERENCE TO AMM 22-11-21 AND REINSTALLED ELEVATOR SERVO IN REFERENCE TO AMM 22-11-24. PERFORMED OPERATIONS CHECK OF THE AUTOPILOT SYSTEM, IN REFERENCE TO AMM 22-11-00. OPERATIONS CHECK GOOD. PERFORMED GVI OF PULLEYS AND CABLES IN THE WHEEL WHEEL, AVIONICS COMPARTMENT AND AFT EQUIPMENT BAY FOUND NO BINDING FOR DEBRIS CAUSING BINDING OR CABLES TO LOCK UP. AIRCRAFT OKAY FOR CONTINUED SERVICE. NO FURTHER DEFECTS OR FAULTS NOTED.

Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

CROSSBEAM CAP STRIP AT FS 589.00, BETWEEN LBL 9.0 AND LBL 27.00 IS CORRODED AROUND NUTPLATES AND THE NUTPLATE ATTACHING RIVETS AND SCORED ACROSS THE CENTER FROM LBL 9.00 TO LBL 27.00. C-CHECK RO 1/16/2021. COMPLIED WITH REMOVAL AND REPLACEMENT OF CROSSBEAM CAP STRIP AT FS 589.00, BETWEEN LBL 9.0 AND LBL 27.00 FOR CORROSION AROUND NUTPLATES AND THE NUTPLATE ATTACHING RIVETS AND SCORED ACROSS THE CENTER FROM LBL 9.00 TO LBL 27.00 REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: STIFFENER — CRACKED (PRESSURE BLKHD) · airframe 41,706 hrs · 34,704 cycles

WHILE WORKING F.S.621 BULKHEAD REPAIR FOUND STIFFENER OUTBOARD OF LBL 36 JUST ABOVE FLOOR LEVEL IN AFT SIDE OF BULKHEAD CRACKED. C-CHECK RO 1/16/2021. INSTALLED STIFFNER P/N 601R36008-51 COMMON TO AFT BULKHEAD AT FS 621 LBL 36, IAW CRJ-200 SRM 51-42-06 REV 38B DATED 25 NOV 2020. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.

Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 41,706 hrs · 34,704 cycles

FOUND INDICATION LT MLG TRUNNION 3RD HOLE FROM FRONT OF STRAP 60% FSH .5 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR OF LT MLG TRUNNION, IAW REO 601R-57-21-3384 REV - DATED 2020-12-30. FORM M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY. COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: TRUNNION — FAILED (LT MLG) · airframe 41,706 hrs · 34,704 cycles

FOUND INDICATION LT MLG TRUNNION AFT HOLE IN STRAP 60% FSH .5 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR IAW REO 601R-57-21-3384 REV - DATED 2020-12-30. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT AFECTED.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 41,706 hrs · 34,704 cycles

RT TRUNNION HAS ONE OVERSIZE HOLE AT AFT HOLE ON STRAP. C-CHECK RO 1/16/2021. PERFORMED REPAIR, IAW REO 601R-57-21-3386 REV - DATED 2020-12-30. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.

Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 41,706 hrs · 34,704 cycles

FOUND INDICATION RT MLG TRUNNION 1ST HOLE AFT OF STRAP 55% FSH .25 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR, IAW REO 601R-57-21-3386 REV- DATED 2020-12-30. M377 AND MAJOR REPAIR TASK CARD ATTACHED NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

FS 280 LBL 9 INBOARD CLIP AND RBL 9 OUTBOARD CLIP ARE CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED TWO EACH CLIPS LBL 9 INBOARD AND RBL OUTBOARD AT FS 280, IAW CRJ 200 SRM 51-24-36, 51-25-21, 51-25-06 AND 51-42-21 MATERIAL TYPE USED PER REO 601R-53-11-171 DATE13-FEB-07 PN S6144-14 PO W71453.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

FS 349 LBL 27 TO LBL 9 IS CORRODED. C-CHECK RO 1/16/2021. UPON EVAL FOUND TO ONLY BE CORROSION ON FASTENERS. REMOVED AND REPLACED CORRODED FASTENERS AND NUTPLATES ON LBL 9 FS 349, IAW CRJ 200 SRM 51-42-13 AND 51-42-15. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NOT REPORTED — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

LBL 9 BETWEEN FS 409+128 AND FS 424 HAS AREAS OF CORROSION. C-CHECK RO 1/16/2021. RBL 9 WAS CORRECT DISCREPANT AREA. REPAIRED RBL 9 FROM FS 409+128-FS 424, IAW MHIRJ REO 601R-53-41-2829 REV- DATED 2020-12-22. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. FORM M337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIGIBLE.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

FS 349 RBL 9 TO RBL 27 IS CORRODED. C-CHECK RO 1/16/2021. FOUND CORROSION ON FS 349 RBL 9 TO RBL 27 TO ONLY BE ON FASTENERS. REMOVED AND REPLACED FASTENERS, IAW CRJ200 SRM 51-42-13. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

FS 349 LT FLOOR SILL TO LBL 27 IS CORRODED. C-CHECK RO 1/16/2021. FASTENERS AND NUTPLATES WERE FOUND TO BE CORRODED. REMOVED AND REPLACED WITH SERVICABLE HARDWARE, IAW CRJ 200 SRM 51-42-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

THERE ARE SEVERAL AREAS OF CORROSION ON RBL 9 BETWEEN FS 409 AND FS 409+64. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR CAP CHANNEL AT RBL 9 FS 409 TO FS 409+112, IAW CRJ200 SRM 51-42-06 AND 51-42-21. C/W MAJOR REPAIR TASK CARD AND 377 FORM. NO WEIGHT CHANGE.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 41,706 hrs · 34,704 cycles

PAX DOOR COVER PLATE AFT MOUNTING BRACKET INBOARD IS CRACKED NEEDS REPLACED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CRACKED MOUNTING BRACKET, IAW CRJ 200 AMM 52-70-04-000-801 AND SRM 51-41-02. OPERATIONS CHECK GOOD AT THIS TIME.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 41,706 hrs · 34,704 cycles

LT CABIN FLOOR BEAM SUPPORT STRAP AT FS 559.00 BETWEEN LBL 36 AND LBL 44 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. REMOVED DAMAGED SUPPORT STRAP AT FS 559 BETWEEN LBL 36 AND LBL 44 AND INSTALLED NEW SERVICEABLE STRAP, IAW CRJ200-SRM-51-42-06, 51-45-00, AND 51-40-11.

Part: ATTACH ANGLE — CRACKED (INTERCOSTAL) · airframe 41,706 hrs · 34,704 cycles

INTERCOSTAL CLIP CRACKED AT FS 484.00 BETWEEN RBL 9 AND RBL 18. REMOVED AND REPLACED UNSERVICEABLE INTERCOSTAL CLIP AT FS 484.00 BETWEEN RBL 9 AND RBL 18 WITH NEW SERVICEABLE INTERCOSTAL CLIP PN: 601R31171-9, IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21.

Part: SPACER — CORRODED (RT ELEVATOR) · airframe 41,706 hrs · 34,704 cycles

RT ELEVATOR OB HINGE ANTI ROTATION DEVICE HARDWARE AND BONDING WIRE HARDWARE CORRODED. C-CHECK RO 1/16/2021. RT ELEVATOR OUTBOARD HINGE ANTI ROTATION HW AND BONDING WIRE HW REPLACED, IAW CRJ 200 AMM 27-34-01-000-801.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

RT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 559.00 +96 TO FS 559.00 +112. C-CHECK RO 1/16/2021. RT FLOOR SILL REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE SILL, IAW CRJ-200 SRM 51-40-11. RECEIVED REO 601R-53-51-539 REV P1 DATED 2020-12-11 IN INSTALLATION OF NEW SILL PLATE. RECEIVED FINAL REO 601R-53-51-539 REV-- DATED 2020-12-13.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR TRACK) · airframe 41,706 hrs · 34,704 cycles

CARGO DOOR FWD LOWER CAM TRACK SUPPORT BRACKET IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CARGO DOOR FWD LOWER CAM TRACK SUPPORT BRACKET, IAW CRJ200 SRM 51-42-06.

Part: BOLT — CORRODED (RT ELEVATOR) · airframe 41,706 hrs · 34,704 cycles

RT ELEVATOR PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR PCU MOUNT HARDWARE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

LT FLOOR SILL FROM FS 409.00 +128 TO FS 559.00 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. COMPLIED WITH BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 FOR CORROSION REPAIR OF LT FLOOR SILL AT FS 409+128-FS 559. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. FORM M-337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

INTERCOSTAL CLIP CRACKED AT FS 484.00 BETWEEN RBL 27 AND RBL 36. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH A SERVICEABLE INTERCOSTAL CLIP AT FS 484.00 BETWEEN RBL 27 AND RBL 36, IAW CRJ 200 SRM 51-42-21.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,706 hrs · 34,704 cycles

DURING INSPECTION OF 36M TASK CARD 53-170-500, FOUND CORROSION BETWEEN RBL 9 AND RBL 27 AT 559+80. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR SUPPORT, IAW CRJ200 SRM 51-42-06 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

RT FLOOR SILL FROM FS 409.00 +128 TO FS 559.00 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. REPAIRED RT FLOOR SILL AT FS 409+128 TO FS 559.00, PER REO 601R-53-41-666 REV C DATED 2012-11-06. C/W FORM M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.

Part: ANGLE — CRACKED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

2 EA INTERCOSTAL CLIPS CRACKED AT FS 484.00 BETWEEN LBL 27 AND LBL 36. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 2 EA INTERCOSTAL CLIPS, IAW CRJ 200 SRM 51-42-21, REFERENCING STEP 14 OF PREVIOUSLY ACCOMPLISHED REO 601R-53-41-059 REV C DATED 2020-03-11 FOR FASTENER CALL OUT ONLY.

Part: BOLT — CORRODED (LT ELEVATOR) · airframe 41,706 hrs · 34,704 cycles

LT ELEVATOR OUTBOARD HINGE MOUNTING HARDWARE AND ANTI ROTATION DEVICE HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT ELEVATOR OUTBOARD HINGE MOUNTING HARDWARE AND ANTI-ROTATION HARDWARE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.

Part: MOUNT — CORRODED (LT ELE HINGE) · airframe 41,706 hrs · 34,704 cycles

LT ELEVATOR CENTER HINGE MOUNTING HARDWARE, PCU MOUNTING HARDWARE AND BONDING WIRE HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED HARDWARE ON FLUTTER DAMPER AND BONDING WIRE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.

Part: FRAME — CORRODED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

FRAME 349.00 FROM STGR 25L TO 25R HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. INSTALLED NEW FRAME AT FS 349 FROM STR 25L TO 25R, IAW SRM 51-42-06, 51-42-21. TASK CARD 51-900-1003-SKY COMPLETED. FORM M-337 ATTACHED, NO WEIGHT AND BALANCE CHANGE.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

2 EA INTERCOSTALS AT FS 349.00 TO FS 364.00 BETWEEN STRINGERS 26L AND 26R HAVE MULTIPLE SPOT OF CORROSION. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 2 EA INTERCOSTALS AT FS 349 TO FS 364 BETWEEN STR 26L AND 26R, IAW SRM 51-42-06, 51-42-21, 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY. FORM M-337 ATTACHED, NO WEIGHT AND BALANCE CHANGE.

Part: SHEAR TIE — CRACKED (PAX DOOR SKIN) · airframe 41,706 hrs · 34,704 cycles

FORWARD UPPER INNER SKIN CORNER ATTACHMENT ANGLES (2 EA) ON PAX DOOR FOUND TO BE CRACKED. C-CHECK RO 1/16/2021. REMOVED, LOCATED AND DRILLED UP NEW SERVICEABLE CORNER ATTACHMENT ANGLES PN 601R38122-1 AND 601R38122-2, IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-40-11. REFERENCE JOB 9744861 OP 11 CAMP 21841018 FOR COMPLETE INSTALL.

Part: BOLT — CORRODED (LT SPOILERON) · airframe 41,706 hrs · 34,704 cycles

LT SPOILERON AND FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REPLACED LT SPOILERON AND FLIGHT SPOILER PCU MOUNTING HARDWARE, IAW CRJ 200 AMM 27-62-01-400-801 SUBTASK 27-62-01-420-001 STEPS (2)-(7). REF CONT CARD FOR WORK PERFORMED.

Part: WASHER — CORRODED (RT SPOILERON) · airframe 41,706 hrs · 34,704 cycles

RT SPOILERON AND FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE, IAW CRJ 200 AMM 27-62-01-000/400-801.

Part: NUT — CORRODED (LT ELEVATOR) · airframe 41,706 hrs · 34,704 cycles

LT FLUTTER DAMPERS HAVE CORRODED NUTS AT ELEVATOR ATTACH POINTS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED HARDWARE ON LT FLUTTER DAMPERS, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.

Part: CONTROL LEVER — CORRODED (ELEVATORS) · airframe 41,706 hrs · 34,704 cycles

LT AND RT ELEVATOR CONTROL LEVER ASSEMBLIES HAS EVIDENCE OF CORROSION AT UPPER AND LOWER LEVERS. C-CHECK RO 1/16/2021. REMOVE AND REPLACED LT AND RT ELEVATOR CONTROL LEVER UPPER AND LOWER LEVERS, IAW CRJ-200 AMM 27-31-35-000-801 AND 27-31-35-400-801. OPERATIONS CHECK GOOD AT THIS TIME.

Part: NUT — CORRODED (RT ELEVATOR) · airframe 41,706 hrs · 34,704 cycles

RT ELEVATOR FLUTTER DAMPERS HAVE CORRODED HARDWARE AT ELEVATOR ATTACH POINTS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR FLUTTER DAMPERS CORRODED HARDWARES WITH SERVICEABLE PARTS, IAW CRJ200 AMM 27-34-05-400-801.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 41,706 hrs · 34,704 cycles

LT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 105 APPROXIMATELY 1 IN LONG X .5 IN WIDE X .015 IN DEEP. C-CHECK RO 1/16/2021. INSTALLED NEW SERVICEABLE LT FLAP VANE LEADING EDGE, IAW CRJ 200 SRM 51-42-13 AND SKYWEST TASK CARD 51-900-1003-SKY. FORM M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.

Part: VANE — DENTED (FLAP VANE LE) · airframe 41,706 hrs · 34,704 cycles

LT INBOARD FLAP VANE LEADING EDGE IS DENTED AT WS 140 APPROXIMATELY .250 IN DIAMETER X .030 IN DEEP. C-CHECK RO 1/16/2021. REMOVED AND REPLACED DAMAGED LT INBOARD FLAP VANE LEADING EDGE WITH NEW SERVICEABLE PN 601R14303-43S, IAW CRJ 200 SRM 51-42-13, FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: VANE — CHAFED (LT WING FLAP LE) · airframe 41,706 hrs · 34,704 cycles

LT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 56 APPROXIMATELY 1 IN LONG X .5 IN WIDE X .015 DEEP. C-CHECK RO 1/16/2021. REPLACED THE LT INBOARD FLAP VANE INBOARD LEADING EDGE SKIN, IAW CRJ 200 SRM 51-42-13 AND 51-40-11 REV B DATED 11/25/2020, TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.

Part: MOUNT BRACKET — CRACKED (ZONE 100) · airframe 41,706 hrs · 34,704 cycles

EXTERNAL SERVICES PANEL LOWER MOUNTING BRACKET IS CRACKED. C-CHECK RO 1/16/2021. REPLACED BRACKET, IAW CRJ SRM 51-42-06. REF CONT CARD FOR WORK PREFORMED.

Part: SKIN — CORRODED (LT AILERON) · airframe 41,706 hrs · 34,704 cycles

LT AILERON UPPER HINGE LINE SKIN IS CHAFED FROM WS 311 TO WS 353 APPROXIMATELY .25 IN WIDE X .020 IN DEEP. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT AILERON UPPER LEADING EDGE, IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. PAINTED TOP COAT, IAW CRJ 200 SRM 51-25-00.

Part: HOUSING — GOUGED (E/E DOOR HANDLE) · airframe 41,706 hrs · 34,704 cycles

MAIN AVIONICS BAY DOOR OUTER HANDLE HOUSING IS GOUGED AT (3) LOCATIONS. C-CHECK RO 1/16/2021. MAIN AVIONICS BAY DOOR OUTER HANDLE HOUSING IS GOUGED AT (3) LOCATIONS FOUND TO BE OUT OF LIMITS, IAW REO 601R-52-42-052 REV- DATED 2014-04-25. LOCATED AND DRILLED NEW SERVICEABLE DOOR OUTER HANDLE, IAW CRJ-200 SRM 51-40-11. INSTALLED MAIN AVI DOOR HANDLE, IAW CRJ-200 AMM 52-42-03-400-801. INSTALLED DOOR IAW CRJ-200 AMM 52-42-00-400-801. OPERATIONS CHECK GOOD.

Part: SKIN — DENTED (PAX DOOR) · airframe 41,706 hrs · 34,704 cycles

PAX DOOR FORWARD AND AFT, UPPER INNER SKIN CORNERS ARE DENTED WITH DAMAGED FASTENERS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED PAX DOOR FWD AND AFT UPPER INNER SKIN CORNERS WITH NEW SERVICEABLE PARTS, IAW SRM 51-42-06, 51-42-13,51-40-11. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.

Part: HOUSING — CHAFED (CARGO DOOR HANDL) · airframe 41,706 hrs · 34,704 cycles

CARGO DOOR HANDLE HOUSING IS CHAFED AT THE FORWARD UPPER EDGE. C-CHECK RO 1/16/2021. CARGO DOOR HANDLE HOUSING IS OUT OF ALLOWABLE LIMITS, IAW REO 601R-52-31-086 REV- DATED 05-NOV-07. REPLACED CARGO DOOR HANDLE HOUSING, IAW CRJ-700 SRM 51-42-21 INSTALLED NEW SERVICABLE CARGO DOOR HANDLE, IAW CRJ 200 AMM 52-31-03-400-801 AND SRM 51-42-06. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.

Part: HOUSING — CHAFED (PAX DOOR HANDLE) · airframe 41,706 hrs · 34,704 cycles

PAX DOOR OUTER HANDE HOUSING IS CHAFED. C-CHECK RO 1/16/2021. REMOVED CHAFE DAMAGE FROM PAX DOOR OUTER SKIN AND HANDLE HOUSING ASSEMBLY, IAW CRJ-200 SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR, IAW REO 601R-52-11-2844 REV-- DATED 2020-12-11.

Part: BUSHING — DAMAGED (LT AILERON) · airframe 41,706 hrs · 34,704 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LT AILERON WING AFT SPAR, REF CRJ 200 AMM 20-26-00-910-804. C-CHECK RO 1/16/2021. REPLACED LT AILERON BUSHINGS AND HARDWARE ON THE LT AILERON WING AFT SPAR, IAW CRJ 200 AMM 20-26-00-910-803. FABRICATED BUSHINGS, IAW BOMBARDIER REO 601R-57-51-015 DATED AUG 09 1995. M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY ATTACHED. NO WEIGHT CHANGE, REF CONT CARD FOR WORK PERFORMED.

Part: BUSHING — DAMAGED (RT AILERON) · airframe 41,706 hrs · 34,704 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RT AILERON WING AFT SPAR, REF CRJ 200 AMM 20-26-00-910-804. C-CHECK RO 1/16/2021. RECEIVED NEW SERVICEABLE BUSHING REQUIRES FABRICATION, IAW BOMBARDIER REO 601R-57-51-015 REV NC LPI AND CAD PLATE C/W INSTALLED BUSHING AND HARDWARE ON RT AILERON WING SIDE, IAW AMM 20-26-00-910-803 REV 62 DATED 10-2020. C/W MAJOR REPAIR TASK CARD AND 377 FORM NO WEIGHT CHANGE.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 41,706 hrs · 34,704 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: -, SERIAL NUMBER: 7448, POSITION: C-CHECK RO 1/16/2021. COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7448. COMPLETED SKYWEST TASK CARD AND ATTACHED COMPLETED FORM M-337. WEIGHT CHANGE OF INCREASE OF 28.48, WITH ARM OF 733.0 AND MOMENTS RESULT OF 20875.84.

Part: STRUT — LOW (NLG) · airframe 39,002 hrs · 32,352 cycles

GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. WOW INPUT AND STEERING INOP CAUTION MESSAGES. WOW OUTPUT FAIL STATUS MESSAGE. MAIN GEARS WERE UP AND LOCKED WHILE NOSE GEAR REMAINED DOWN. RAN QRH AND ALL MESSAGES CLEARED EXCEPT WOW INPUT AND WOW OUTPUT FAIL. LANDED WITHOUT INCIDENT AND NOSE WHEEL STEERING WAS OPERATIVE ON THE GROUND. (FLT#5713) CLOSED PERFORMED FULL SERVICE OF NLG SHOCK STRUT ON JACKS IAW AMM. PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM. AFTER STRUT SERVICE, ENSURED THAT STRUT FULLY EXTENDED. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: STRUT — LOW (NLG) · airframe 38,855 hrs · 32,217 cycles

NOSE GEAR DISAGREE ON TAKEOFF. THE NOSE GEAR WAS IN THE DOWN POSITION. COMPLIED WITH QRH PROCEDURE. RETURNED TO FIELD. (FLT 5109) FO: 02/28/2019 CLOSED PERFORMED A FULL STRUT SERVICE ON THE NLG IAW AMM. SWUNG THE NLG SEVERAL TIMES IAW AMM. OPS CHECKS GOOD.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 35,977 hrs · 29,663 cycles

CRACK FOUND FWD ON PASSENGER DOOR EDGE MEMBER TOP STAIR. REMOVED AND REPLACED EDGE MEMBER IAW SRM.

Part: SKIN — CHAFED (LT WING) · airframe 35,977 hrs · 29,663 cycles

LEFT LOWER WING PLANK IS CHAFED UNDER FWD TIP OF FLAP HINGE FAIRING 586AB. REPAIRED THE FLAP HINGE FAIRING IAW SRM AND REO.

Part: SKIN — GOUGED (BS 409) · airframe 35,977 hrs · 29,663 cycles

BELLY SKIN CHAFED AND GOUGED BS 409+55 LT DME ANTENNA CUT-OUT AND RT DME ANTENNA CUT-OUT. REPAIRED THE DAMAGE IAW REO.

Part: SKIN — CHAFED (FUSELAGE) · airframe 35,977 hrs · 29,663 cycles

FUSELAGE SKIN HAS CHAFE DAMAGE AFT SIDE OF APU EXHAUST CUT-OUT. REPAIRED THE SKIN IAW REO.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 35,977 hrs · 29,663 cycles

VERTICAL SURFACE OF SILL PLATE AT SERVICE DOOR IS CORRODED. REMOVED AND INSTALLED A NEW SERVICE DOOR SILL PLATE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,977 hrs · 29,663 cycles

RIGHT WING INBD L/E FLAP VANE CHAFING SKIN MID LEADING EDGE. REMOVED AND REPLACED THE RT WING INBD FLAP CENTER VANE CAP IAW SRM.

Part: SKIN — DENTED (GROUND SPOILER) · airframe 35,977 hrs · 29,663 cycles

RIGHT INBD GROUND SPOILER HAS A SMALL DENT FOUR INCHES FROM TRAILING EDGE. REPAIRED THE SPOILER SKIN IAW REO.

Part: SKIN — DENTED (BS 589-605) · airframe 35,977 hrs · 29,663 cycles

DENT BETWEEN BS 589 - 605, STRINGERS 19-20R IS OUT OF LIMITS. REWORKED THE DENTED AREA AND ENSURED NO DAMAGE TO UNDERLYING STRUCTURE IAW REO AND SRM. PRESSURE CHECKED GOOD.

Part: TIRE — VIBRATION (NLG) · airframe 34,683 hrs · 28,425 cycles

NOSE WHEEL HIGH VIBRATION ON TAKEOFF ROLL. RETURN TO FIELD. REMOVED AND REPLACED BOTH NOSE TIRES IAW AMM. ALSO LUBED TORQUE LINKS IAW AMM. AIRCRAFT OK FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 32,426 hrs · 26,316 cycles

GEAR DISAGREE NLG DOWN WITH MANUAL EXTENSION. R & R NLG SELECTOR VALVE IAW AMM. PERFORMED LANDING GEAR EXTENSION/RETRACTION WITH NO FAULTS, OPS CHECKED GOOD.

Part: SKIN — DENTED (RT WING) · airframe 31,578 hrs · 25,528 cycles

DENT ON RT WING WS 137.04, INBD L/E ON OTBD SIDE. REPAIRED IAW REO.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 31,578 hrs · 25,528 cycles

FOUND AFT CUP BRACKET AND CLEAT COMMON ON PAX DOOR SILL CORRODED. R & R AFT CUP BRACKET AND CLEAT WITH NEW BRACKET AND CLEAT ON PAX DOOR SILL IAW SRM.

Part: SKIN — DENTED (CARGO DOOR) · airframe 31,578 hrs · 25,528 cycles

DENT APPROX 6" AFT BY 2" BELOW AFT LOWER CORNER OF CARGO DOOR. REPAIRED IAW EA.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,615 hrs · 23,007 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,174 hrs · 22,673 cycles

RIGHT NR 2 EXTERIOR FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R THE BULB IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,749 hrs · 22,332 cycles

FWD EMERGENCY LIGHT ON THE LT SIDE IS BURNED OUT. REPLACED THE LAMP IAW AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

DENT ON EXTERNAL FUSELAGE SKIN FWD OF FS 235 BELOW STRINGER 13R IAW REO. C-CHECK REPAIRED DENT ON EXTERNAL FUSELAGE SKIN FWD OF FS 235 BELOW STRINGER 13R IAW REO.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

RT SIDE OF NOSE AREA DAMAGED AT LOCATION NR 17. C-CHECK PERFORMED PERMANENT REPAIR TO RT SIDE FUSELAGE DAMAGE LOCATION NR 17 IAW REO.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

RT SIDE OF NOSE AREA DAMAGED AT LOCATION 10 & 16. C-CHECK REPAIRED RT SIDE OF NOSE AREA DAMAGE LOCATIONS 10 & 16 IAW REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

NEW DAMAGE FOUND LOCATION NR 1C, FS 265.70 2.0 INCHES BELOW STRINGER 23R. C-CHECK REPAIRED DENT WITH SCRATCH AT LOCATION NR 1C, FS 265.7 2.0 INCHES INCHES BELOW STRINGER 23R IAW REO.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

RT SIDE OF NOSE AREA DAMAGED AT LOCATION 4 & 5. C-CHECK REPAIRED DAMAGE AT LOCATION 4 & 5 IAW REO.

Part: STRUCTURE — SCRATCHED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

NEW DAMAGE FOUND LOCATION NR 1A, FS 187.9 1.75 INCHES ABOVE ADG OPENING. C-CHECK REPAIRED SCRATCH DAMAGE AT LOCATION NR 1A, FS 187.9 1.75 INCHES ABOVE ADG OPENING IAW REO.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

RT SIDE OF NOSE AREA DAMAGED AT LOCATION 1, 3, 6, 7, 9, 13, 14 & 15. C-CHECK REPAIRED DAMAGE AT LOCATION 3, 6, 7, 9, 13, 14 & 15 IAW REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

NEW DAMAGE FOUND LOCATION NR 1B, FS 229.00 1.20INCHES ABOVE STRINGER 15R. C-CHECK REPAIRED DENT WITH SCRATCH AT LOCATION NR 1B, FS 229.0 1.2" ABOVE STRINGER 15R IAW REO.

Part: SKIN — DENTED (LT WING) · airframe 27,240 hrs · 21,929 cycles

REPLACE LT WING CTR LE SKIN. C-CHECK REPLACED LT CTR LE SKIN WITH NEW SKIN IAW SRM & REO.

Part: STRUCTURE — CRACKED (RT WING) · airframe 27,240 hrs · 21,929 cycles

CRACKED AT RT WING DRAIN FWD & AFT ATTACHMENT HOLES LOCATED BETWEEN WS 0.00 & WS22.50 & BETWEEN STRINGER 5 & STRINGER 7. C-CHECK REPAIRED IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

LT INBD FLAP VANE LE IS CHAFED AT INBD BUMP STOP POSITION. C-CHECK BLENDED & RESTORED FINISHES OF LT INBD FLAP VANE INBD IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

RT INBD FLAP VANE LE IS CHAFED AT INBD BUMP STOP POSITION. C-CHECK BLENDED CHAFE & RESTORED FINISHES TO RT INBD FLAP VANE INBD LOCATION IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

RT INBD FLAP VANE LE IS CHAFED AT CENTER BUMP STOP POSITION. C-CHECK BLENDED CHAFE & RESTORED FINISHES IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

RT INBD FLAP VANE LE IS CHAFED AT OTBD BUMP STOP POSITION. C-CHECK BLENDED CHAFE & RESTORED FINISHES TO RT INBD FLAP VANE OTBD IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

LBL 9 LOWER FLOOR SUPPORT HAS CRACK FS 280. C-CHECK REPLACED REPAIR ANGLE FILLER & REPAIR ANGLE ON FS280, LBL9 LOWER FLOOR SUPPORT IAW REO.

Part: STRUCTURE — CHAFED (PAX DOOR) · airframe 27,240 hrs · 21,929 cycles

PAX DOOR OUTER HANDLE CUT OUT CHAFED FWD TOP EDGE. C-CHECK CHAMFERED DAMAGE TO A 45 DEGREE & TO A SMOOTH CONTOUR IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

FS 280 CROSS BEAM INBD & OTBD CLIPS CRACKED AT LBL 9. C-CHECK REPLACED INBD & OTBD CLIPS AT LBL 9 FS 280 IAW SRM & REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,240 hrs · 21,929 cycles

FS 280 CROSS BEAM INBD & OTBD CLIPS CRACKED AT RBL 9. C-CHECK REPLACED FS280 CROSS BEAM INBD & OTBD CLIPS AT RBL 9 IAW SRM & REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,240 hrs · 21,929 cycles

SUSPECTED CRACK ON PAX DOOR AFT DRAG ANGLE BY PULL IN CABLE PULLEY BRACKET. C-CHECK REPAIRED CRACK ON PAX DOOR AFT DRAG ANGLE IAW REO.

Part: SUPPORT — GOUGED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

RT WING INBD FLAP VANE OTBD ACTUATOR SUPPORT STRUCTURE IS GOUGED. C-CHECK BLENDED RT WING INBD FLAP VANE OTBD ACTUATOR SUPPORT STRUCTURE IAW REO.

Part: SUPPORT — GOUGED (TE FLAP) · airframe 27,240 hrs · 21,929 cycles

RT WING INBD FLAP VANE INBD ACTUATOR SUPPORT STRUCTURE IS GOUGED. C-CHECK REPAIRED RT WING INBD FLAP VANE ACTUATOR SUPPORT STRUCTURE GOUGE IAW REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 27,048 hrs · 21,798 cycles

IAW CP 10284197, ITEM NR 18 FOUND CRACKED AT RHS NOSE FS 185 BETWEEN STRINGERS 23 - 24R. C-CHECK COMPLIED WITH TEMPORARY REPAIR OF ITEM NR 18 NOSE RHS FS 185 STRINGERS 23 - 24R IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,694 hrs · 21,524 cycles

OVERHEAD EMERGENCY LIGHT BURNED OUT. FLT 6223 REPLACED OVERHEAD EMERGENCY LIGHT POD BULB.

Part: PRIORITY VALVE — FAILED (LANDING GEAR) · airframe 26,651 hrs · 21,490 cycles

DURING LANDING RECEIVED A GEAR DISAGREE WARNING MESSAGE ALONG WITH A NOSE DOOR WARNING MESSAGE THE WARNING MESSAGE WAS PERSISTENT FOR ABOUT 10 SECONDS BEFORE RETURNING TO NORMAL. FLT#5298 REPLACED THE PRIORITY VALVE IAW AMM. OPERATIONS & LEAK CHECKED GOOD. THE GEAR WAS SWUNG WITH HYDRAULICS & EMERGENCY EXTENSION. PN 4622, SN ON: 539A, SN OFF: 1253A

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,600 hrs · 21,446 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5548 RELAMPED.

Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 26,585 hrs · 21,434 cycles

9 FOOT SECTION OF EMERGENCY FLOOR LIGHTING FROM ROW 2-5 DOES NOT ILLUMINATE. SERVICE CLEANED MOISTURE FROM EMERGENCY FLOOR STRIPS CONNECTORS WITH CONTACT CLEANER. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 26,107 hrs · 21,042 cycles

MLG FAILED TO EXTEND WHEN GEAR LEVER CYCLED TO DOWN POSITION. RAN QRH. GEAR MANUAL EXTENSION SUCCESSFUL. FLT#6345 REPLACED MLG SELECTOR VALVE IAW AMM. PN 750005000, SN ON 0022T & SN OFF 0639.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 25,657 hrs · 20,716 cycles

DURING CLIMBOUT, RUDDER TRIM WENT FULL NOSE LEFT, UNCOMMANDED, TRIM KNOB SEEMED TO BE SLIGHTLY STICKING TO THE LEFT. REPLACED THE AIRLERON/RUDDER TRIM CONTROL PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,331 hrs · 20,506 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 6465) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,090 hrs · 19,577 cycles

NR 3 CEILING OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,636 hrs · 19,231 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5534) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — CRACKED · airframe 23,544 hrs · 19,161 cycles

RIGHT WINDOW CRACKED. (FLT 5511) REPLACED RIGHT SIDE WINDOW IAW AMM. PART OFF: NP-139322-6 S/N: 00195H3056

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,391 hrs · 19,041 cycles

ONE SECTION OF FLOOR LEVEL EMERGENCY LIGHTS AT ROW 11 IS OUT. (FLT 6459) RELAMPED IN REFERENCE TO AMM.

Part: POWER CABLE — FAILED (CABIN) · airframe 23,268 hrs · 18,943 cycles

EMERGENCY FLOOR LIGHTING IS OUT. (FLT 5415) REPLACED MID CABIN POWER CABLE IN REFERENCE TO ESPM.

Part: INVERTER — FAILED (CABIN) · airframe 23,268 hrs · 18,943 cycles

EMERGENCY SIDEWALL AND FLOOR LIGHTING IS OUT. (FLT 5542) REPLACED NR 2 INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,431 hrs · 18,268 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6485) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 22,401 hrs · 18,246 cycles

RIGHT SIDE EXIT ROW LOWER EMERGENCY LIGHT IS INOPERATIVE. (FLT 5605) REPLACED NR 3 EMERGENCY LIGHT INVERTER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,319 hrs · 18,179 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5234) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,319 hrs · 18,179 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5234) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,212 hrs · 18,091 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4530) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,121 hrs · 18,019 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5611) RELAMPED EMERGENCY LIGHT.

Part: CONTROL UNIT — MALFUNCTIONED (ADG) · airframe 22,073 hrs · 17,977 cycles

FLT 6299, ADG DEPLOYED AFTER TAKEOFF. RESTOWED ADG AND REPLACED ADG AUTO CONTROL UNIT. PN: , SN OFF:

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,969 hrs · 17,902 cycles

NR 2 FORWARD OF RIGHT WING ON FUSELAGE EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,918 hrs · 17,860 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6340) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,918 hrs · 17,860 cycles

NR 2 RIGHT WING AFT EMERGENCY LIGHT IS OUT. (FLT 5652) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,751 hrs · 17,732 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6250) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,511 hrs · 17,551 cycles

FORWARD CEILING EMERGENCY LIGHT IS OUT. (FLT 5484) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,332 hrs · 17,407 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,170 hrs · 17,266 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,109 hrs · 17,210 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6477) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,087 hrs · 17,192 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6288) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,943 hrs · 17,067 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6386) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,732 hrs · 16,901 cycles

LEFT WING FORWARD EMERGENCY EXIT LIGHT IS OUT. (FLT 6387) RELAMPED EMERGENCY LIGHT.

Part: CHARGER — FAILED (CABIN) · airframe 20,732 hrs · 16,901 cycles

RIGHT SIDE FLOOR EMERGENCY LIGHTS AT ROWS 6-8 ARE OUT. (FLT 6503) REPLACED BATTERY PACK CHARGER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,683 hrs · 16,861 cycles

RIGHT OVERWING MIDDLE EMERGENCY LIGHT IS OUT. (FLT 6442) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,635 hrs · 16,827 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,614 hrs · 16,815 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 5407) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,410 hrs · 16,643 cycles

RIGHT AFT EXTERIOR FUSELAGE EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,204 hrs · 16,493 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6229) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,036 hrs · 16,366 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6829) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,000 hrs · 16,334 cycles

LT WING EXTERIOR AFT EMERGENCY LIGHT IS OUT. (FLT 6818) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,718 hrs · 16,106 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6581) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,092 hrs · 15,580 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6856) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,961 hrs · 15,454 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6708) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,520 hrs · 15,062 cycles

FS 621.0 PRESSURE BULKHEAD FORWARD SIDE CRACKED AT AFT, UPPER CARGO TRACK. (C-CHECK) REPAIR PER REO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,659 hrs · 15,181 cycles

FS 280 FLOORBEAM CRACKED. (C-CHECK) REPAIRED PER REO.

Part: HANDLE — WORN (CABIN DOOR) · airframe 17,175 hrs · 13,918 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6484) REPLACED DOOR HANDLE ASSEMBLY.

Part: OIL SYSTEM — LOW (APU) · airframe 16,416 hrs · 13,272 cycles

FLIGHT 5607, CMH TO IAH - AT FL310 THE CREW RECEIVED AN APU OIL PRESSURE MESSAGE ON EICAS. THE CREW FOLLOWED THE QRH AND DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL LEVEL LOW. THE APU WAS SERVICED WITH 1QT OF BP2380 OIL IAW 12-13-49. OPERATIONAL CHECKS GOOD, NO DEFECTS OR LEAKS NOTED.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 16,417 hrs · 13,273 cycles

FLIGHT 5607, SDF TO IAH - AT FL280 THE CREW RECEIVED AN APU OIL PRESS MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO AEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL LEVEL LOW. THE APU WAS SERVICED WITH 1QT OF BP2380 IAW 12-13-49, OPERATIONAL CHECKS GOOD, NO LEAKS NOTED. LATER ON 4/28/2009, THE LOW OIL PRESSURE SWITCH WAS REPLACED AND THE CONNECTOR INSPECTED. NO DEFECTS WERE NOTED, OPS AND LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,097 hrs · 13,028 cycles

DURING INSPECTION THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOP. THE LIGHT WAS RE-LAMPED AND OPERATED NORMALLY.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 15,827 hrs · 12,813 cycles

FLIGHT 5650 ELP TO IAH - THE CREW REPORTED THAT ON GEAR RETRACTION THERE WAS A NOSE LANDING GEAR DISAGREE MESSAGE AND THE NOSE LANDING GEAR DOORS INDICATED RED AND THE NOSE LANDING GEAR INDICATED "IN TRANSIT". THE AIRCRAFT CONTINUED ON TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GEAR SWINGS AND THE GEAR RETRACTS NORMALLY BUT THERE WERE NO GREEN LIGHTS FOR THE NOSE GEAR. A PSEU WAS SLAVED IN WITH NO FIX. THE RIGHT NOSE LANDING GEAR DOOR PROX SWITCH HAD DAMAGED PINS ON THE HARNESS SIDE. THE PINS WERE REPLACED BUT DID NOT FIX THE FAULT. THE NOSE LANDING GEAR UPLOCK PROX SWITCH HARNESS WAS THEN REPLACED AND THE GEAR OPERATED NORMALLY.

Part: SEQUENCE VALVE — LEAKING (MLG) · airframe 15,799 hrs · 12,794 cycles

FLIGHT 5503, SDF TO IAH - UPON GEAR RETRACTION DURING INITIAL CLIMB, THE GEAR WOULD INDICATE FULL UP FOR A FEW SECONDS FOLLOWED BY AMBER HASHED INDICATIONS. THIS REPEATED SEVERAL TIMES ACCOMPANIED BY A LOUD THUMPING. THERE WERE NO CAUTION, WARNING, OR AURAL WARNINGS RECEIVED. THE GEAR WAS EXTENDED NORMALLY WITH CORRECT INDICATIONS AND THE AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE FAULT WITH THE AIRCRAFT ON JACKS AND TRACED THE FAULT TO THE MAIN LANDING GEAR SEQUENCING VALVE. THE VALVE WAS REPLACED AND THE GEAR OPERATED NORMALLY.

Part: PROXIMITY SENSOR — LOOSE (LT MLG) · airframe 15,770 hrs · 12,771 cycles

FLIGHT 5541, LIT TO IAH - UPON GEAR RETRACTION, THE FLIGHT CREW REPORTED A RYTHMIC VIBRATION ACCOMPANIED BY A BRIEF GEAR DISAGREE MESSAGE ON EICAS. THE MESSAGE WENT AWAY BUT THE VIBRATION DID NOT. THE GEAR INDICATION LIGHTS WERE FLASHING AND THE CREW WAS UNABLE TO DETERMINE THE CAUSE OF THE FAULT. THE CREW RAN THROUGH THE APPROPRIATE CHECKLISTS AND PREPARED TO RETURN TO LIT. THE GEAR WAS LOWERED MANUALLY AND THERE WAS A 3 DOWN AND LOCKED INDICATION, AND THE VIBRATION WENT AWAY. THE FLIGHT LANDED WITHOUT INCIDENT IN LIT. THE RETRACTION SYSTEM WAS PLACED ON MEL AND THE AIRCRAFT WAS FLOWN TO IAH FOR FURTHER TROUBLESHOOTING. IN IAH MAINTENANCE FOUND THE PROX SWITCH ON THE LEFT UPLOCK BOX WAS LOOSE. THE SWITCH AND CONNECTOR WERE RE-SECURED AND THE RETRACTION SYSTEM OPS CHECKED GOOD.

Part: CLAMP — LOOSE (ANTI ICE SYSTEM) · airframe 15,727 hrs · 12,738 cycles

FLIGHT 5652, ATL TO CLE. DURING DESCENT INTO CLE THE AIRCRAFT ENCOUNTERED ICING CONDITIONS AT APPROXIMATELY 11,000 FT. BETWEEN 8,000 AND 6,000 FT THE FLIGHT CREW RECEIVED AN ICE INDICATION ON EICAS AND TURNED ON THE WING ANTI-ICE AND RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE. THE QRH WAS FOLLOWED AND APPROACH INSTRUCTED TO CLIMB OUT OF THE ICING. AFTER CLEARING THE AIRCRAFT WAS CLEANED FOLLOWING THE WRITTEN PROCEDURE. DUE TO THE WEATHER CONDITIONS AT CLE IT WAS DECIDED TO DIVERT TO CMH WHERE THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO A LOOSE V-BAND CLAMP ON THE RIGHT WING INBOARD PICCOLO TUBE CAUSING A LEAK. THE CLAMP WAS RE-INSTALLED AND THE ANTI-ICE SYSTEM OPERATED NORMALLY.

Part: CONTROL PANEL — FAULTED (COCKPIT)

FLIGHT 5601 IAH TO JAX. DURING FLIGHT THE CREW RECEIVED AN E2 REV ICON INTERMITTENTLY. THE REVERSER DID NOT DEPLOY. THE FLIGHT LANDED WITHOUT INCIDENT. THE REVERSER WAS PLACED ON MEL AND THE ACFT WAS RELEASED BACK TO SERVICE. THE MEL WAS CLEARED ON THE 22ND WHEN THE THRUST REVERSER CONTROL PANEL WAS REPLACED.

Part: SENSOR — FAULTY (RT WING TE FLAPS)

FLIGHT 5994, RDU TO SDF. DURING CLIMB AT 3,000 FT THE FLAPS WERE SELECTED FROM 3 DEGREES TO ZERO AND THE CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW REPORTED THAT THE LEFT FLAP STOPPED AT 3 DEGREES AND THE RIGHT FLAP STOPPED AT ZERO. MAINTENANCE RIGGED THE FLAPS AND BPSU`S AND REPLACED THE INBOARD SKEW SENSOR ON THE RT OUTBOARD FLAP. (A)

Part: CONTROL UNIT — FAULTY (TE FLAPS)

FLIGHT 5994, RDU TO IAH. UPON FLAP RETRACTION FROM FLAPS 8 TO ZERO AFTER TAKEOFF FROM RDU, THE FLIGHT CREW RECEIVED A FLAPS FAIL MESSAGE ON EICAS. THE MESSAGE WAS CONFIRMED AND THE FLAPS WERE FAILED AT 3 DEGREES ON THE LEFT FLAP AND ZERO DEGREES ON THE RIGHT FLAP. THE QRH WAS FOLLOWED AND THE FLIGHT LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND FOUND THE FAULT CODES FROM THAT FLIGHT POINTED TO THE FECU ITSELF AS BEING THE CAUSE OF THE FAULT. THE FECU WAS REPLACED ALONG WITH THE SKEW DETECTION UNIT AND THE NR 4 SKEW DETECTOR. (A)

Part: BRACKET — UNSECURE (RT WING TE FLAPS)

FLIGHT 5586, RDU TO CLE. UPON FLAP RETRACTION FROM FLAPS 20 TO FLAPS 8 THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESSAGE WAS CONFIRMED AND THE LT FLAP WAS AT 11 DEGREES WHILE THE RT FLAP WAS AT 10 DEGREES. THE QRH CHECKLIST WAS FOLLOWED AND THE AIRCRAFT LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND THE RT OUTBOARD FLAP FAIRING SPACER BRACKET UNSECURED AND BINDING AGAINST THE ACTUATOR ARM. THE BRACKET WAS RE-SECURED, FLAPS RESET AND THE SYSTEM OPS CHECKED GOOD. THERE WAS NO DAMAGE TO EITHER PART AND THE AIRCRAFT WAS RELEASED. (A)

Part: FLAP SYSTEM — OUT OF RIG (TE FLAPS)

FLIGHT 5716 - IAH TO JAX. DURING CLIMB WHEN THE FLAPS WERE SELECTED FROM 8 TO 0 THE RT FLAP RETRACTED TO 0 AND LT FLAP FROZE AT 3 DEGREES AND A FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROPRIATE CHECK LISTS WERE FOLLOWED AND THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A FLAP RE-RIG AND THE FLAP SYSTEM OPERATED NORMALLY. (A)

Part: SENSOR — INOPERATIVE (RT WING TE FLAPS)

FLIGHT 5716, IAH TO JAX. DURING CLIMB WHEN THE FLAPS WERE SELECTED FROM 8 TO 0 THE RT FLAP RETRACTED TO 0 AND LT FLAP FROZE AT 3 DEGREES AND A FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROPRIATE CHECK LISTS WERE FOLLOWED AND THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A FLAP RE-RIG AND THE FLAP SYSTEM OPERATED NORMALLY. (A)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

MAINTENANCE FOUND THE EXTERNAL EMERGENCY LIGHT AFT OF THE SERVICE DOOR TO BE INOPERATIVE DURING TESTING. THE LIGHT WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. (A)

Part: ENGINE — DAMAGED (NR 2)

FLIGHT 5531, SDF TO IAH. ON CLIMBOUT OF KSDF, AT APPROXIMATELY 4,000 FT, THE FLIGHT CREW HEARD A LOUD BAND AND THE E2 ITT CLIMBED INTO THE RED AREA ALONG WITH A TRIPLE CHIME. WHILE PREPARING TO RETURN TO KSDF, THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED AND E2 WAS SHUT DOWN. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DURING INITIAL INSPECTION THAT MULTIPLE FAN BLADES ALONG WITH THE CORE COWL WERE DAMAGED ON E2. DURING A BORE SCOPE INSPECTION OF THE CORE DAMAGED 1ST STAGE VG VANES WERE FOUND. THE AIRCRAFT IS CURRENTLY OUT OF SERVICE FOR E2 ENGINE CHANGE. (A)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,098 hrs · 10,818 cycles

ON APPROACH, THE FLAPS FAILED AT 30 DEGREES. THE AIRCRAFT PERFORMED A GO-AROUND, THE QRH WAS FOLLOWED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE AIRCRAFT AND THE FAIL MESSAGE CLEARED, AFTER OPERATING THE FLAP SYSTEM SEVERAL TIMES THE FAIL MESSAGE DID NOT RETURN AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,800 hrs · 10,593 cycles

IAH TO MAF - ON APPROACH TO MAF, CREW RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS WERE SELECTED TO 30 DEGREES. THE FLAPS FAILED AT 30 DEGREES AND THE QRH WAS FOLLOWED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FLAP SYSTEM, AND RESET IT AFTER FINDING NO MESSAGES. THE FLAP SYSTEM OPERATED NORMALLY AFTER RESET.

Part: PUMP — LEAKING (NR 2) · airframe 12,702 hrs · 10,526 cycles

CMH TO IAH - DURING CRUISE FLIGHT, LOST HYDRAULIC SYSTEM 2 FLUID AND PRESSURE. CREW RAN APPROPRIATE CHECKLISTS AND LANDED AT THE NEAREST SUITABLE AIRPORT (LITTLE ROCK). AFTER LANDING, THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAINTENANCE SERVICED THE NR 2 HYDRAULIC SYSTEM AND INSPECTED FOR LEAKS. THE NR 2 ENGINE DRIVEN PUMP WAS FOUND TO BE LEAKING. THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED AND THE HYDRAULIC SYSTEM WAS LEAK TESTED. AFTER THE SUCCESSFUL LEAK CHECK, THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

STALL FAIL MSG POSTED AFTER T/O. FOUND NO FAULTS LOGGED ON STALL SYSTEM. RESET STALL COMPUTER AND NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: THERMAL SWITCH — FAILED (BLEED AIR SYS)

EVENT SUMMARY STATED 14TH STAGE BLEED AIR FAIL. REMOVED AND REPLACED STANDBY THERMAL SWITCH & HEAT SENSOR.

Part: CLAMP — LOOSE (LT ENGINE)

L-14TH DUCT WARNING MESSAGE ON CLIMBOUT WITH SINGLE ENGINE (LEFT ENGINE IDLE) APPROACH AND LANDING. EMERGENCY WAS DECLARED. MX FOUND DUCT CLAMP LOOSE IN LT PYLON AT COWL ANTI ICE DUCT. TIGHTENED AND REPOSITIONED CLAMPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,607 hrs · 5,462 cycles

DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNED OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,023 hrs · 5,000 cycles

DURING INSPECTION THE AISLE CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: BATTERY — DISCHARGED (FUSELAGE)

DURING MAINTENANCE INSPECTION, THE LT AND RT OVERWING EMERGENCY LAMPS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINTENANCE INSPECTION, A SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FOUR EMERGENCY FLOOR TRACK LIGHT STRIPS AND AN INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (RT OVRWING LIGHT)

DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT OVERWING EMERGECNY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL CHANGED THE BULB AND PERFORMED A SATISFOACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT INSPECTION FOR THE FLIGHT FROM LGA TO SAV, THE CREW REPORTED THAT THE CENTER, OVERHEAD, EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE CENTER, OVERHEAD EMERGENCY FLOOD LIGHT. AN OPERATIONAL CHECK OF THE LIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.