N594SW

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 42,478 hrs · 37,102 cycles

CARGO DOOR FWD RAIL TOP SUPPORT BRACKET CRACKED. REPLACED CARGO DOOR FWD RAIL TOP SUPPORT BRACKET IN REFERENCE TO CRJ 200 SRM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 40,991 hrs · 35,876 cycles

GEAR DISAGREE WARNING MESSAGE DURING GEAR EXTENSION ON LANDING. COMPLIED WITH QRH. MANUAL GEAR EXTENSION REQUIRED. (FLT#3134) CLOSED PERFORMED FUNCTION CHECK OF MLG EXTENSION AND RETRACTION, AND PERFORMED GEAR DISAGREE OPS CHECK IAW AMM. FUNCTION AND OPS CHECK GOOD. PERFORMED MANUAL RELEASE CHECK, AND NUMEROUS EXTENSION/RETRACTION OPS CHECKS IAW AMM. OPS CHECK GOOD WITH NO DUPLICATION OF DISAGREE FAULT.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

FS 621.00 BULKHEAD DAMAGED. (C-CHECK) RO: 05/16/2019 REPAIRED DAMAGE IAW REO. LEAK CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

CRACK LOCATED AT FS621.00 BETWEEN LBL 36 TO LBL 42. (C-CHECK) RO: 05/16/2019 REMOVED AND INSTALLED NEW ANGLE P/N 601R-53-61-117-1 AT FS621 BETWEEN LBL36 - LBL42 IAW REO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE CORREDED. (C-CHECK) RO: 05/16/2019 REMOVED AND INSTALLED NEW PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE ASSY. P/N: 601R31527-221 IAW SRM.

Part: DRAG ANGLE — DAMAGED (TAILCONE) · airframe 40,121 hrs · 35,161 cycles

TAILCONE DRAG ANGLE HAS 5 ELONGATED FASTENER HOLES. (C-CHECK) RO: 05/16/2019 REPAIRED TAILCONE DRAG ANGLE 5 ELONGATED FASTENER HOLES IAW REO.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

FS621 PRESSURE BULKHEAD HAS DAMAGE. (C-CHECK) RO: 05/16/2019 REPAIRED THE FS621 PRESSURE BULKHEAD IAW REO. LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

LEFT HAND FLOOR SILL IN AFT CARGO COMPARTMENT HAS CORROSION AROUND SCREW HOLE FROM APPROX FS 559+80 TO FS 621. (C-CHECK) RO: 05/16/2019 REPLACED LT FLOOR SILL IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

RIGHT HAND FLOOR SILL IN AFT CARGO COMPARTMENT HAS CORROSION AROUND SCREW HOLE FROM APPROX FS 589 TO FS 621. (C-CHECK) RO: 05/16/2019 REMOVED AND REPLACED THE RT CARGO FLOOR SILL IAW REO. ALL CHECKS GOOD

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,121 hrs · 35,161 cycles

FRAME 349.00 UPPER AND LOWER FLANGES ARE CORRODED BETWEEN STGR25L - 26R. (C-CHECK) RO: 05/16/2019 REMOVED CORROSION ON FRAME 349.00 UPPER AND LOWER FLANGES BETWEEN STGR25L - 26R IAW REO AND SRM.

Part: SKIN — DENTED (PAX DOOR) · airframe 40,121 hrs · 35,161 cycles

2 DENTS LOCATED ON MCD SKIN 4.830" AFT OF FWD LEADING EDGE AND 8.480" FROM TOP EDGE AND 14.5" FWD OF MCD AFT EDGE AND 26.2" FROM MCD TOP EDGE. (C-CHECK) RO: 05/16/2019 COMPLIED WITH REO REPAIR FOR TWO EACH DENTS ON THE PAX DOOR OUTER SKIN. LEAK CHECK GOOD.

Part: MOUNT — CORRODED (ZONE 200) · airframe 36,200 hrs · 30,905 cycles

CLOSET MOUNT CORRODED UNDER 231BLF FLOOR PANEL. REMOVED AND REPLACED THE MOUNT IAW SRM.

Part: MOUNT — CORRODED (ZONE 200) · airframe 36,200 hrs · 30,905 cycles

EVIDENCE OF CORROSION ON FWD CLOSET MOUNT UNDER FLOOR PANEL 231CLF. REMOVED AND REPLACED THE MOUNT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 36,200 hrs · 30,905 cycles

FLOOR SSUPPORT JUST AFT AF BS 559 IS CORRODED. REPAIRED IAW REO AND SRM.

Part: DOUBLER — CORRODED (BS 559) · airframe 36,200 hrs · 30,905 cycles

FLOOR SSUPPORT LIPPED DOUBLER PLATE FROM BS 559+96 TO 559+112 HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED A NEW THE FLOOR SUPPORT LIPPED DOUBLER PLATE IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 36,200 hrs · 30,905 cycles

LEFT INBOARD FLAP VANE L/E SKIN CHAFED AT CENTER SECTION. REMOVED AND REPLACED THE LT INBOARD FLAP VANE CENTER VANE CAP IAW SRM AND AMM.

Part: FRAME — CORRODED (BS 559) · airframe 36,200 hrs · 30,905 cycles

AFT FUSELAGE INTERNAL FRAME BS 559+112 BETWEEN STRINGERS 26L AND 26R HAS CORROSION. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM.

Part: PANEL — CORRODED (GALLEY) · airframe 36,200 hrs · 30,905 cycles

GALLEY FLOOR PROTECTOR PANEL UNDER THE SERVICE DOOR HAS CORROSION. INSTALLED NEW GALLEY FLOOR PROTECTOR PLATE IAW SRM.

Part: STRUCTURE — DENTED · airframe 36,200 hrs · 30,905 cycles

SMALL DENT APROXIMATELY 2 INCHES AFT OF BS 589+29, BELOW CARGO DOOR. COMPLIED WITH ALL STEPS OF REPAIR IAW REO.

Part: UNKNOWN — FAILED (RT MLG) · airframe 34,636 hrs · 29,442 cycles

GEAR DISAGREE, ON TAKEOFF. RIGHT GEAR WAS YELLOW, THEN RED, WHEN NOSE AND LT SHOWED UP AND WHITE. REMOVED AND REPLACED THE RT MLG WHEEL BIN IAW AMM. OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 3) · airframe 33,537 hrs · 28,291 cycles

HYD SYS 3 LOW CAUTION MESSAGE ON GEAR RETRACTION, HAD GEAR DISAGREE, THEN STARTING SHOWING 100 PERCENT QUANTITY AND 3200 PSI. RETURNED TO FIELD. BLED NR 3 HYDRAULICS SYSTEM, PERFORMED MULTIPLE EXTENSION/RETRACTION AND MANUAL EXTENSION OPS CHECK OF THE GEAR GOOD IAW AMM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 31,406 hrs · 26,421 cycles

BULKHEAD FOUND CORRODED. C-CHECK, REMOVED CORRODED MATERIAL AND REPAIRED LAV 9G BULKHEAD IAW EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

LT INBD FLAP VANE L/E CHAFED AT CENTER POSITION. C-CHECK BLENDED OUT CHAFING ON LT WING INBD FLAP VANE MID OTBD L/E SKIN IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

LEFT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. C-CHECK, BLENDED OUT CHAFING ON LT WING INBD FLAP VANE OTBD L/E SKIN. ORIGINAL MATERIAL THICKNESS AT REWORKED AREA IS 0.050" IAW SRM AND REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT CTR POSITION. C-CHECK, BLENDED OUT CHAFING ON RT WING INBD FLAP VANE MID OTBD L/E SKIN IAW REO.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 31,406 hrs · 26,421 cycles

FUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTED, INBD & OTBD ENDS. C-CHECK, FUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTING REPAIRED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. C-CHECK BLENDED OUT CHAFING ON RT WING INBD FLAP VANE OTBD L/E SKIN IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

LT INBD FLAP VANE L/E CHAFED AT INBD POSITION. C-CHECK, BLENDED OUT CHAFING ON LT WING INBD FLAP VANE INBD L/E SKIN IAW SRM AND REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,406 hrs · 26,421 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT INBD POSITION. C-CHECK, BLENDED OUT CHAFING ON RT INBD FLAP VANE INBD L/E SKIN IAW REO.

Part: PANEL — OUT OF TOLERANCE (HORIZONTAL STAB) · airframe 31,406 hrs · 26,421 cycles

THE LOWER LT HORIZONTAL STABILIZER VISOR PANEL 326BL FAILED ITS GAP CHECK. C-CHECK, RECONTOURED VISOR PANEL 326BL IAW REO.

Part: PANEL — OUT OF TOLERANCE (HORIZONTAL STAB) · airframe 31,406 hrs · 26,421 cycles

THE UPPER RT HORIZONTAL STABILIZER VISOR PANEL 326AR FAILED ITS GAP CHECK. C-CHECK, R & R NEW VISOR PANEL 326AR IAW REO C.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 31,406 hrs · 26,421 cycles

THE LOWER RT HORIZONTAL STABILIZER VISOR PANEL 326BR FAILED ITS GAP CHECK. C-CHECK, R & R NEW VISOR PANEL 326BR IAW REO.

Part: STRUCTURE — DAMAGED (LT WING TIP) · airframe 31,406 hrs · 26,421 cycles

LEFT WING TIP EXTENSION HAS COMPOSITE DAMAGE ON UPPER T/E. C-CHECK, REPAIRED LT WING TIP EXTENSION AT UPPER T/E IAW REO AND SRM.

Part: PANEL — DAMAGED (RT WING) · airframe 31,406 hrs · 26,421 cycles

RIGHT WING LOWER SURFACE HAS FRETTING ON MATING SURFACE FOR PANEL 650KB. C-CHECK, BLENDED OUT DAMAGED AREAS TO A SMOOTH CONTOUR ON LANDINGS OF PANEL 650KB, RT SIDE IAW REO.

Part: SKIN — DAMAGED (RT WING) · airframe 31,406 hrs · 26,421 cycles

RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640BT HAS FRETTING. C-CHECK FRETTING TO RT UPPER WING SKIN AT PANEL 640BT REPAIRED IAW EA.

Part: PANEL — DAMAGED (RT WING) · airframe 31,406 hrs · 26,421 cycles

RT WING PANEL 640CT HAS FRETTING ON MATING SURFACE. C-CHECK, REPLACED PANEL 640CT WITH FABRICATED PANEL, PN 600-10003-37 IAW STS EA.

Part: PANEL — CHAFED (LT WING) · airframe 31,406 hrs · 26,421 cycles

LEFT WING PANEL 599BB IS CHAFED. C-CHECK LT WING PANEL 599BB CHAFES REPAIRED IAW REO.

Part: PANEL — CHAFED (LT WING) · airframe 31,406 hrs · 26,421 cycles

LEFT WING PANEL 599CB IS CHAFED. C-CHECK LT WING PANEL 599CB CHAFES REPAIRED IAW REO.

Part: DRAIN MAST — CRACKED · airframe 31,406 hrs · 26,421 cycles

CORE COWL 445AB DRAIN MAST CRACKED. C-CHECK, REPAIRED CRACK IN DRAIN MAST ON PANEL 445AB IAW EA.

Part: SKIN — DAMAGED (RT WING) · airframe 31,406 hrs · 26,421 cycles

RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640CT HAS FRETTING. C-CHECK, FRETTING TO RT UPPER WING SKIN AT PANEL 640CT REPAIRED IAW EA.

Part: SKIN — DAMAGED (RT WING) · airframe 31,406 hrs · 26,421 cycles

RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640AT HAS FRETTING. C-CHECK, FRETTING TO RT UPPER WING SKIN AT PANEL 640AT REPAIRED IAW EA.

Part: PANEL — CHAFED (LT WING) · airframe 31,406 hrs · 26,421 cycles

LT WING PANEL 699AB CHAFED. C-CHECK, LT WING PANEL 699AB CHAFED, REPAIRED IAW REO.

Part: PANEL — CHAFED (LT WING) · airframe 31,406 hrs · 26,421 cycles

LT WING PANEL 699BB CHAFED. C-CHECK, LT WING PANEL 699BB CHAFED, REPAIRED IAW REO.

Part: PANEL — CHAFED (LT WING) · airframe 31,406 hrs · 26,421 cycles

LT WING PANEL 699CB IS CHAFED. C-CHECK, LT WING PANEL 699CB CHAFED REPAIRED IAW REO.

Part: TUBE — DAMAGED (SERVICE DOOR) · airframe 31,406 hrs · 26,421 cycles

SERVICE DOOR HARNESS CONVOLEX TUBING DAMAGED. C-CHECK, REPLACED THE SERVICE DOOR HARNESS CONVOLEX TUBING IAW REO.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,294 hrs · 25,524 cycles

FLOOR EMERGENCY LIGHTS AFT OF ROW 8 DO NOT ILLUMINATE. REPLACED BATTERY CHARGER ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,361 hrs · 24,793 cycles

MAIN CABIN DOOR LOWER EMERGENCY LIGHT SINGLE BULB IS BURNED OUT. FLT 6481 RELAMPED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,224 hrs · 24,714 cycles

SMOKE COMING FROM SIDE WALL LIGHTS AT 7A. FLT 3475 REPLACED LIGHT FIXTURE AT SEAT 7A, IAW AMM. PN BC1-0065-003

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 29,156 hrs · 24,676 cycles

BURNING SMELL FROM EMERGENCY LIGHT EXIT SIGN ROW 7AB. FLT 6191 REPLACED AFFECTED LIGHT FIXTURE AT ROW 7AB IAW AMM PN ON/OFF BCI-0065-003.

Part: WINDOW — CRACKED (COCKPIT) · airframe 27,894 hrs · 23,652 cycles

FLT 4440, CAPTAIN`S SIDE WINDOW SUSTAINED MULTIPLE CRACKS. REPLACED CAPTAINS SIDE WINDOW IAW AMM.

Part: UPLOCK SENSOR — OUT OF RIG (RT MLG) · airframe 27,725 hrs · 23,496 cycles

GEAR DISAGREE WARNING. (FLT 4680) RIGGED RT MLG UPLOCK SENSOR IAW AMM. SWUNG GEAR. OPS CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CORROSION ON INTERCOSTAL AT FS 349.0 O/B LEFT NEAR MAIN CABIN DOOR OPENING. (C-CHECK) COMPLIED WITH FS 349 FLOOR CROSS BEAM REPAIR AT LBL 40 IAW STS ENGINEERING AUTHORIZATION.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CORROSION FOUND UNDER SERVICE DOOR SILL AT REAR ANGLE AT FS 349.00. (C-CHECK) COMPLIED WITH FS 349 FLOOR CROSS BEAM AT LBL 40.00 REPAIR IAW STS EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

FS 280.0 BULKHEAD WEB, BETWEEN LBL 20.75 AND RBL 20.75 UPPER AND LOWER RADIUS CRACKED AT RBL 3.0 BULKHEAD WEB CORRODED BEYOND LIMITS, AT LBL 9.0 OUTBD-INBD CLIPS CRACKED, AT RBL 9.0 INBD CLIP CRACKED. (C-CHECK) REPAIRED FS 280.0 BULKEAD WEB, BEAM AND ALL ATTACHING CLIPS IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

FS 202 BULKHEAD IS CRACKED APPROXIMATELY 1 INCH, AT PARKING BRAKE CONTROL ROD. (C-CHECK) FS 202 BULKHEAD CRACK AT PARKING BRAKE CONTROL ROD REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CRACK INDICATION ON RIGHT FS 559 PRESSURE BULKHEAD. (C-CHECK) REPAIRED CRACK ON RIGHT FS 559 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

RIGHT UPPER PRESSURE FLOOR SILL HAS AREAS OF CORROSION AT APPROXIMATELY FS 461.00, FS 484.00 AND FS 499.00. (C-CHECK) REPAIRED 11 EACH, AREAS OF LIGHT CORROSION ON RIGHT FLOOR SILL ANGLE FROM APPROXIMATELY FS 461.00 TO FS 559.00 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

LEFT UPPER FLOOR PRESSURE SILL HAS AREAS OF CORROSION AT APPROXIMATELY FS 461.00, FS 484.00 AND FS 544.00. (C-CHECK) REPAIRED 11 EACH, AREAS OF LIGHT CORROSION ON LEFT FLOOR SILL ANGLE FROM APPROXIMATELY FS 461.00 TO FS 559 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CRACK ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 46.99 WL 108.64 AT LINTEL FITTING. (C-CHECK) COMPLIED WITH FS 621 BULKHEAD REPAIR FOR LINTEL FITTING IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

LEFT CARGO SILL HAS CORROSION AROUND NUT PLATES. (C-CHECK) REPLACED CARGO DOOR SILL IAW REO.

Part: ACCESS PANEL — CHAFED (RT AILERON) · airframe 27,710 hrs · 23,483 cycles

RIGHT AILERON ACCESS PANEL 699BB CHAFED. (C-CHECK) REPAIRED RIGHT AILERON ACCESS PANEL 699BB IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CRACK ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 27.50 WL 131.00 ABOVE AFT CARGO DOOR AFT TRACK. (C-CHECK) COMPLIED WITH FS 621 BULKHEAD, CARGO DOOR TRACK REPAIR IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CRACK IN RIGHT FS 409 +128 VERT POST AT RBL 18, O/B C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED RIGHT FS 409 +128 VERT POST AT RBL 18 O/B C-CHANNEL OF AFT RADIUS IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CRACK NOTED AND MARKED IN CTR FS 409 +128 VERT POST AT BL 0.0, LEFT C-CHANNEL IN AFT RADIUS. (C-CHECK) REMOVED AND REPLACED CENTER POST AT FS 409 +128 BL 0.0 IAW REO.

Part: ACCESS PANEL — CHAFED (RT AILERON) · airframe 27,710 hrs · 23,483 cycles

RIGHT AILERON ACCESS PANEL 699AB CHAFED. (C-CHECK) REPAIRED RIGHT AILERON ACCESS PANEL 699AB IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,710 hrs · 23,483 cycles

CARGO FLOORBEAM HAS CORRODED NUT PLATE TABS AT LBL 27.5 JUST FORWARD OF TENSION FITTING FS 621. (C-CHECK) REMOVED AND REPLACED CARGO FLOORBEAM CAP IAW REO.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 27,710 hrs · 23,483 cycles

AUTOPILOT RWD CAUTION MESSAGE APPEARED AND AIRCRAFT TURNS TO LEFT UNCOMMANDED. (FLT 4859) OPERATED AUTOPILOT AND AILERON SERVO OPS CHECKS IAW AMM. OPS CHECKS GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,829 hrs · 20,177 cycles

ENGINE BEAM LOWER SKIN IS CRACKED ON RT SIDE AT ACCESS PANEL CUTOUT FWD I/B SIDE RADIUS. REPAIRED ENG BEAM LOWER SKIN PER CRJ REO 601-53-61-358 REV B.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 23,015 hrs · 19,498 cycles

FLIGHT 5285 - AFTER TAKEOFF FROM CVG LOST ALL NR 3 SYSTEM HYDRAULIC FLUID, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED RUPTURED HYDRAULIC LINE ON ACMP 3B. (A)

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 21,455 hrs · 18,236 cycles

FLIGHT 5467 - DURING CLIMBOUT UPON GEAR RETRACTION TEMPORARILY RECEIVED A LANDING GEAR DISAGREE MESSAGE. REPLACED THE MLG PRIORITY VALVE.

Part: HANDLE — WARNING MESSAGE (PAX DOOR) · airframe 20,670 hrs · 17,604 cycles

FLIGHT 5153 - PAX DOOR OUTER HANDLE MESSAGE IN FLIGHT. RAN QRH PROCEDURE AND DIVERTED TO ACY AND LANDED SAFELY. TRANSFERRED TO DMI LIST PER 52-70-01-1.

Part: UPLOCK — FAULTY (NLG) · airframe 19,914 hrs · 16,989 cycles

FLIGHT 5013 - NOSE GEAR DISAGREE ON APPROACH, NOSE GEAR SHOWED WHITE BOX, RAN QRH NOSE GEAR DOWN AND LOCKED. PERFORMED EMERGENCY LANDING IN JFK. AIRCRAFT LANDED SAFELY. UPLOCK FAULTY.

Part: BPSU — FAULTY (RT TE FLAP) · airframe 19,378 hrs · 16,565 cycles

FLIGHT 5227 - FLAP FAIL CAUTION MESSAGE GOING FROM 8 TO 20 DEGREES ON APPROACH, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT BPSU.

Part: FLAP — MALFUNCTIONED (WING) · airframe 19,369 hrs · 16,558 cycles

FLIGHT 5508 - FLAP FAIL CAUTION MESSAGE FLAPS SELECTED AT 8 DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C).

Part: DETECTOR — MALFUNCTIONED (SKEW) · airframe 17,381 hrs · 14,990 cycles

AT THE GATE IN SFO, RECEIVED A FLAPS DEGRADED STATUS MESSAGE. REPLACED SKEW DETECTION UNIT. OPERATIONAL CHECK GOOD, PN 601R59014-1, SN OFF A560.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 15,581 hrs · 13,611 cycles

RIGHT SIDE GALLEY EXIT LIGHT INOPERATIVE. REPLACED NR 1 ELBP IAW MM 33-51-04. OPERATIONAL CHECK GOOD.

Part: RIB — CRACKED (LT WING) · airframe 16,666 hrs · 14,452 cycles

LEFT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601-57-51-046.

Part: RIB — CRACKED (RT WING) · airframe 16,666 hrs · 14,452 cycles

RIGHT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046.

Part: PCU — INOPERATIVE (FLIGHT SPOILERS) · airframe 13,719 hrs · 12,127 cycles

SPOILERONS FAULT NR 1 SYSTEM PCU INOPERATIVE. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: APU — FIRE (APU BAY) · airframe 13,249 hrs · 11,753 cycles

APU SHUT DOWN WITHOUT WARNING. ATTEMPTED RESTART. GROUND PERSONNEL ADVISED FLAMES PRESENT. DISCHARGED APU BOTTLE. INSPECTED APU COMPARTMENT AND AIRFRAME, NO FIRE DAMAGE NOTED. APU FIRE BOTTLE DISCHARGED. REPLACED APU WITH A SERVICEABLE UNIT IAW 49-10-00. OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 12,915 hrs · 11,495 cycles

STAB TRIM DISENGAGES AFTER TAKEOFF. REMOVED AND REPLACED THE CAPTAINS STAB TRIM DISCONNECT SWITCH IAW AMM 27-41-30.

Part: OVERHEAT LOOP — FAULTY (LT MLG) · airframe 12,817 hrs · 11,421 cycles

INFLIGHT RECEIVED (MLG OVHT FAIL) MESSAGE. REPLACED LT GEAR FIRE LOOP AND WIRE HARNESS, MLG OVHT OPS CHECKS GOOD. P/N: 244-03615.

Part: CONNECTOR — DIRTY (OVERHEAT LOOP) · airframe 12,662 hrs · 11,298 cycles

RIGHT JETPIPE LOOP B-INOP. REMOVED OVERHEAT AND FIRE DETECTOR CONTROL BOX CONNECTORS. CLEANED CONTACTS AND REINSTALLED CONNECTORS. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,577 hrs · 10,477 cycles

PULLEY INTERCOSTAL ANGLE CRACK AT STA 484 LBL 27 O/B. REPAIRED INTERCOSTAL ANGLE IAW CRJ REO 601R-53-41-059 & RII 53-401 ON LBL 27.0. P/N: 601R31171-17.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 11,602 hrs · 10,496 cycles

CARGO PIT CRACKS FOUND ON FLOOR LANDING PLATE AT FS 589.00 LBL 42 WL 73.50 AND FS 605.00, LBL 42 WL 73.5. REPAIRED DAMAGED AREAS IAW CRJ REO 601R-53-61-433 REV A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,577 hrs · 10,477 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401. P/N: 601R31113-57.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,577 hrs · 10,477 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401. P/N: 601R31113-58.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,577 hrs · 10,477 cycles

PULLEY INTERCOSTAL ANGLE CRACK AT STA 484 RBL 27 O/B. REPAIRED INTERCOSTAL ANGLE IAW CRJ REO 601R-53-41-059 REV A & RII 53-401 ON RBL 27.0. P/N: 601R31171-9.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 10,664 hrs · 9,772 cycles

STAB TRIM CH2/ MACH TRIM MESSAGE ON TAXI OUT. REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT IAW MM 27-41-01. REMOVED AND REPLACED COPILOTS STAB TRIM SWITCH WITH A SERVICEABLE UNIT IAW MM 27-41-05. NR 2 PN 309-4334

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 10,641 hrs · 9,752 cycles

STAB CHANNEL 2 HSTCU WOULD NOT ENGAGE DURING PREFLIGHT. CLEANED PINS & RE-RACKED CONTROL UNIT. PERFORMED OPS CHECK. REMOVED AND REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT WITH A SERVICEABLE UNIT IAW MM 27-42-05. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,641 hrs · 9,752 cycles

STAB CHANNEL 1 HSTCU DISENGAGED DURING FLIGHT, UNABLE TO RE-ENGAGE. MACH TRIM FAILURE INFLIGHT DESCENDING FROM 11000 MSL AND SLOWING FROM 280 KIAS, ABLE TO RE-ENGAGE VIA QRH. REMOVED & REPLACED HSTA IAW MM 27-42-01. REMOVED & REPLACED MCU IAW 27-42-05. OPS CHECKS GOOD IAW 27-41-00. P/N OFF/ON 7062-3, S/N OFF 606, S/N ON 734.

Part: AMPLIFIER — FAULTY (NR 1 ENGINE) · airframe 10,102 hrs · 9,351 cycles

APPROXIMATELY 2 MINUTES AFTER TAKEOFF THE RIGHT ENGINE ROLLED BACK AND WOULD NOT PRODUCE POWER. TRIED TO RESTART, BUT RELIGHT FAILED. RETURNED TO IAH.TROUBLESHOOTING SYSTEM DETERMINED THE RIGHT ENGINE N1 AMPLIFIER TO BE FAULTY. SUPPLEMENTAL REPORT FORTHCOMING. UPDATE: 5/20/03 SLC: REMOVED AND REPLACED NR 2 RT AMPLIFIER IAW MM 73-21-03. RUN RT ENGINE IAW MM 71-00-00. OPS CHECK GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 9,191 hrs · 8,652 cycles

FUEL AND EXHAUST ODOR THROUGH THE PACKS AFTER APU START AND BLEED SWAP. RAN AIR CONDITIONER SYSTEM IAW CRJ MM 21-51-00. INSPECTED APU COMPARTMENT, NO LEAKS FOUND. SYSTEM OPERATED NORMALLY WITH NO ODOR OF FUEL OR EXHAUST IN COCKPIT AND CABIN AREA.

Part: FASTENER — SHEARED (LT ELEVATOR) · airframe 9,191 hrs · 8,652 cycles

DURING ELEVATOR FIRST FLIGHT OF THE DAY CHECKS FOUND THAT SYSTEM NR 3 WOULD NOT OPERATE THE LT ELEVATOR. SYSTEM NR 1 AND 2 OPERATE NORMALLY. FOUND LEFT ELEVATOR NR 3 PCU HI-LOC SHEARED AT ATTACH POINT ON AFT LINKAGE. REMOVED HI-LOC AND REPLACED IT WITH A SERVICEABLE ONE IAW SRM 51-42-20. OPS CHECK GOOD.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 8,759 hrs · 8,325 cycles

ON ROTATION AT TAKE OFF THE CARGO DOOR LIGHT CAME ON. WE RETURNED TO SLC. COMPLIED WITH THE HARD/OVERWEIGHT LANDING INSPECTION IAW ST 12-407. INSPECTED CARGO DOOR HANDLE, NO DEFECTS NOTED. CARGO DOOR HANDLE WAS FOUND POPPED WHEN AIRCRAFT ARRIVED. CARGO HANDLE OPS CHECK GOOD.

Part: SUPPORT BRACKET — DAMAGED (PAX DOOR) · airframe 8,416 hrs · 8,052 cycles

PASSENGER DOOR HARD TO OPEN. REMOVED AND REPLACED INBOARD SUPPORT BRACKET WITH NEW BRACKET. CLEANED, INSPECTED AND LUBED BEARINGS IAW MM 52-11-02. OPS CHECKS GOOD.

Part: WIRE — BROKEN (RUDDER TRIM) · airframe 8,198 hrs · 7,880 cycles

RUDDER TRIM INOP, WILL NOT MOVE LEFT OR RIGHT. FOUND WIRE BROKEN OFF OF RUDDER TRIM SWITCH. SOLDERED WIRE BACK ONTO SWITCH. OPERATED RUDDER TRIM & CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,091 hrs · 7,799 cycles

EMERGENCY EXIT ROW LIGHT ROW 2-5 INOP. EMERGENCY DOOR LIGHT INOP ROW 8 LEFT SIDE. REPLACED EMERGENCY LIGHT FLOOR STRIP FROM ROW 1 TO 7. ALL LIGHTS CHECK GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 7,992 hrs · 7,723 cycles

ELECTRICAL SMOKE SMELL IN COCKPIT JUST AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED THE SAME SMELL IN THE CABIN WITH A VERY LIGHT SMOKE IN THE REAR OF THE CABIN. VISUALLY INSPECTED CABIN LIGHTING AND BALLAST FOR EVIDENCE OF OVERHEAT. NO FAULTS FOUND. RAN LEFT AND RIGHT ECS, DID DETECT SLIGHT ODOR. RAN PACKS IN HOT, NO SMOKE OCCURRED AND AFTER SEVERAL MINUTES ODOR WAS NOT DETECTABLE. SELECTED PACKS BACK TO COLD, NO ODOR PRESENT AND PACK OPERATION NORMAL. UNABLE TO DUPLICATE ANY SMOKE.

Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP) · airframe 7,929 hrs · 7,672 cycles

ON TAXI IN WITH FLAPS TO 20 DEGREES, FLAPS FAIL CAUTION. REMOVED & REPLACED FCU WITH SERVICEABLE UNIT. ALSO COMPLIED WITH AD 98-20-01.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 7,012 hrs · 6,989 cycles

AT AIRSPEEDS ABOVE 290 KIAS THERE IS A VIBRATION IN THE RUDDER PEDALS. ALSO NOTICED A VIBRATION 2 MINUTES AFTER SHUTDOWN ON THE GROUND. REPLACED NR 1 YAW DAMPER ACTUATOR IAW MM 22-22-01. OPS CHECKS GOOD.

Part: WIRE — BROKEN (COCKPIT) · airframe 6,886 hrs · 6,881 cycles

WIRES BROKEN OFF OF THE ROLL DISCONNECT SWITCH. REMOVED AND REPLACED ROLL DISCONNECT SWITCH IAW CRJ MM 27-12-10. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 6,647 hrs · 6,687 cycles

RT WINDSHIELD IS CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,647 hrs · 6,687 cycles

ABORTED TAKEOFF DUE TO WING OVERHEAT MSG. ACCOMPLISHED HIGH POWER ENG RUN WITH CREW ASSISTANCE. COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD.

Part: POWER UNIT — MALFUNCTIONED (T/E FLAP) · airframe 6,363 hrs · 6,473 cycles

AFTER SETTING FLAPS 45 DEGREES, FLAPS FAIL CAUTION MESSAGE CAME ON. FLAPS FAILED AGAIN IN SLC. REMOVED AND REPLACED ELECTRONIC FLAP COMPUTER, OPS CHECK GOOD. REMOVED AND REPLACED PDU IAW CRJ MM 27-52-01, RIGGED BPSU IAW CRJ MM 27-51-10, REMOVED AND REPLACED FLEX SHAFT NR 4 IAW CRJ MM 27-53-10, FUNCTION CHECK OF FLAP SYSTEM GOOD. P/N OFF 601R93100-103, S/N OFF 837.

Part: CONTROL UNIT — FAILED (T/E FLAP) · airframe 6,313 hrs · 6,432 cycles

AFTER LEVELING OFF AT FL330, FLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED FECU PER MM 27-51-05. OPS CHECK OF SYSTEM GOOD.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 6,307 hrs · 6,427 cycles

FLAPS FAILED AT 11 DEGREES DURING FLAP RETRACTION. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. ADJUSTED POTENTIOMETERS 6 AND 7 (6 FROM -0.019 TO 0.011; 7 FROM -0.013 TO 0.011). OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 6,141 hrs · 6,292 cycles

IN CRUISE FLIGHT AND DURING DESCENT INTO RNO RUDDER SYSTEM INDICATED UNCOMMANDED RUDDER MOVEMENT LEFT AND RIGHT. REMOVED AND REPLACED LEFT AND RIGHT YAW DAMPER ACTUATORS AND NR 1 AND NR 2 AHRS COMPUTERS. ALL OPS CHECK GOOD.

Part: CIRCUIT BOARD — FAULTY (AUTOPILOT SYS) · airframe 6,124 hrs · 6,279 cycles

ON DESCENT, NOTICED RUDDER FLUTTER. BOTH RUDDER INDICATION & AERODYNAMIC FLUTTER OBSERVED AT VARIOUS SPEEDS. ON THE GROUND, STILL OBSERVED RUDDER FLUCTUATIONS (ABOUT 3 DEGREES BOTH SIDES). AT FL330 AND MACH .77 EXPERIENCED AN UNCOMMANDED RUDDER MOVEMENT. VERIFIED BY FEELING A/C MOVE ABOUT VERT AXIS AND FLIGHT CONTROL PAGE. INSPECTED PRIMARY & SECONDARY BREAKOUT FORCE ON RUDDER FEEL MECHANISMS. WITHIN TOLERANCES PER 27-21-00. REPLACED NR 1 AND NR 2 FCC CIRCUIT CARD ASSEMBLIES. AUTOPILOT SYSTEM OPS CHECK GOOD IAW MM22-11-07.

Part: PCU — FAULTY (SPOILERON) · airframe 6,119 hrs · 6,273 cycles

SPOILERONS FAULT STATUS MESSAGE (RIGHT SPOILERON). REMOVED AND REPLACED RIGHT INBOARD PCU FOR SPOILERON IAW 27-62-01. OPS AND LEAK CHECK GOOD ON RIGHT INBOARD SPOILERON.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 6,065 hrs · 6,236 cycles

FLAP FAIL CAUTION ON AT DEPLOYMENT TO 8 DEGREES. C/W AD 98-20-01. FLAP FAIL MESSAGE RESET. CHECKS OK.

Part: PROXIMITY SWITCH — OUT OF ADJ (PAX DOOR) · airframe 6,119 hrs · 6,273 cycles

PAX DOOR OUTER HANDLE CAUTION - WOULD NOT GO OUT PER QRH PROCEDURE, DID EXTINGUISH ON DESCENT. RETURNED TO RNO. INSPECTED PASSENGER DOOR PER 52-70-04, CHECKS NORMAL. INSPECTED AND FOUND DOOR TO BE SECURE. PROBLEM IS INDICATION ONLY. ADJUSTED PASSENGER DOOR OUTER HANDLE PROXIMITY SWITCH IAW RJ MM 52-70-04. SYSTEM OPS CHECK GOOD.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 5,931 hrs · 6,121 cycles

STAB TRIM AND MACH TRIM MESSAGE AFTER TAKEOFF. RE-ENGAGED BOTH SYSTEMS. BOTH SYSTEMS FAILED AGAIN. RETURNED TO SLC. REMOVED AND REPLACED HSTA WITH A SERVICEABLE UNIT IAW AMM 27-42-01. ALSO REMOVED AND REPLACED MCU WITH A SERVICEABLE UNIT IAW AMM 27-42-05. PERFORMED OPS CHECKS OF HSTCA & MCU PER MM 27-40-00. OPS CHECK GOOD. CAT II UPGRADE. HSTA S/N OFF: 951, MCU P/N: 7062-3, S/N ON: 606, S/N OFF: 468.