N292UE

Part: STRUCTURE — DAMAGED (TE FLAP)

OVERSIZED BUSHING REQUIRED IN TWO PLACES ON RIGHT FLAP P/N HC579L1400-001, S/N 838H52-86. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1701-692001. (M)

Part: SPRING — BROKEN (NLG BAY)

NLG RIGHT WHEEL BRAKE, SPRING BROKEN. MAINTENANCE REMOVED AND REPLACED BROKENS SPRING GUIDE TUBE, SPRING AND REPAIRED DAMAGE TO THE CEILING OVER NLG BAY. (M)

Part: CIRCUIT BREAKER — INOPERATIVE (OVERHEAD PANEL) · airframe 27,744 hrs · 32,627 cycles

SMELLED ELECTRICAL SMOKE, SAW SPARKS FROM APU/ENGINE START PANEL, APPEARED TO BE START AND CONTINUOUS (A) CENTRAL C/B AND ALL IGNITION (A) AND CONTINUOUS IGNITION (A) 2 AND 3, PULLED C/B`S SPARKS STOPPED. PULLED CONTINUOUS IGNITION (A) 1 AND 4 C/BS. REMOVED AND REPLACED CIRCUIT BREAKERS E27 (L SCREEN HEAT (A)) AND E29 (MANUAL TEMP CONTROL). REMOVED AND REPLACED WIRES 133C AND FE44. GENERATED ADDITIONAL WORK CARDS IN WORK ORDER 52491 FOR OPS CHECKS.

Part: WARNING LIGHT — ILLUMINATED (RUDDER VALVE)

MWS RUDDER VALVE LIGHT IS ILLUMINATED IN FLIGHT AFTER DEPARTURE. AIR RETURN TO ORD. RESET ABD, TESTED IAW.

Part: SLEEVE — OUT OF POSITION (COCKPIT) · airframe 24,871 hrs · 29,096 cycles

EN ROUTE NOTICED FAINT ELECTRICAL SMELL, SWITCHED TO FRESH AIR MODE, ODOR DIMINISHED, BUT STILL PRESENT. ON APPROACH SWITCHED TO APU AIR ODOR GONE. MAINTENANCE RAN ENGINES, TESTED ON ALL AIR SOURCES, INSPECTED BEHIND OVERHEAD ELECTRICAL, REPOSITIONED RUBBER SLEEVE ON OVERHEAD ELECTRICAL PANEL LANYARD.

Part: SLIDE — DEFECTIVE (SERVICE DOOR) · airframe 23,237 hrs · 27,217 cycles

FOUND FWD SERVICE DOOR EVACUATION SLIDE DEPLOYMENT CABLE NOT ATTACHED AND BOTTLE VALVE CABLE MISROUTED. DEPLOYMENT CABLE CONNECTION PIECES MISSING. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY.

Part: WARNING LIGHT — ILLUMINATED (LT MLG) · airframe 22,975 hrs · 26,922 cycles

ON DEPARTURE FROM ORD LT GEAR INTRANSIT LIGHT REMAINS ILLUMINATED. MAINTENANCE SECURED LT MLG DOOR IN INFLIGHT POSITION.

Part: LANDING GEAR — ICED (RIGHT) · airframe 22,816 hrs · 26,729 cycles

RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THAT MLG SWITCHES HAVE EXTREME ICE BUILD-UP. DEICED GEAR, INSPECTED AND FOUND NO DAMAGE TO GEAR.

Part: FCU — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENGINE WHEN AT CRUISE 89-90 PERCENT N1, EXPERIENCED UNCOMMANDED POWER BACK TO 60 PERCENT N1, OTHER INDICATIONS FOLLOWED, 30 SECOND =/1 MINUTE STABILIZED. THIS IS WITH TMS OFF, ALT 25,000 FT, ANTI-ICE OFF. REMOVED AND REPLACED NR 2 ENGINE FUEL CONTROL UNIT. (M)

Part: IGNITOR — CRACKED (NR 1 ENGINE)

NR 1 ENGINE COMBUSTOR OUTBOARD IGNITOR BASE HAS CRACKED IN WELD, NEED DYE PENETRANT TO VERIFY LENGTH FOR SERVICEABILITY. C/W PT INSPECTION PER ENGINE MM AND AWAC NDT SPEC. FOUND TWO CRACKS 180 DEGREES APART IN IGNITOR BOSS, 1 CRACK = .9 INCH, OTHER = .6 INCH. REPLACED NR 1 ENGINE DUE TO OUT OF LIMIT COMBUSTOR CRACKING ON THE IGNITOR BOSS. (M)

Part: LINK — CHAFED (NR 1 PYLON)

NR 1 PYLON TO WING LINK CHAFED, TOP END OUTBOARD SIDE. BLENDED AND POLISHED ABOVE CHAFFED AREA IN PYLON TO WING OUTBOARD LINK, AREA DETAILED VISUAL AND NDT. NO DEFECTS NOTED. BLENDED AREA ON PANEL 454BL THAT WAS RUBBING ON LINK, REF BARA/AVR/1211/99. (M)

Part: RIB — CRACKED (RIGHT WING)

RIGHT WING TIP FALSE RIB HAS A CRACK. REPAIRED ASSY PER ABOVE IAW AW-57-02-9412-06. (M)

Part: CONTROL CABLE — CORRODED (AILERON)

DURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR A6WR95063.

Part: BRACKET — BROKEN (NR 4 PYLON)

DURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OPERATOR CONTROL NR A6WR95059.

Part: BRACKET — CRACKED (PYLON COWL MT)

DURING SCHEDULED INSPECTION, FOUND NR 1 PYLON SHOULDER COWL LORD MOUNT ATTACHMENT BRACKET CRACKED. REPLACED BRACKET. (X)

Part: PYLON — RIVETS SHEARED (NR 4)

DURING SCHEDULED INSPECTION, FOUND 3 RIVETS SHEARED OFF IN NR 4 PYLON BOX AT POSITIONS B, C, D. REPLACED FASTENERS IAW AVRO RL HC546H9009. (X)

Part: PLATE — CORRODED (FR 15-18)

DURING STRUCTURAL INSPECTION, FOUND TWO SUPPORT PLATES AT 3RD INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR BETWEEN FUSELAGE FRAMES 15 AND 18 CORRODED. REPLACED BOTH PLATES. REFERENCE: OPERATOR CONTROL NR A6WR95065. (X)

Part: PLATE — CORRODED (FR 15-18)

DURING STRUCTURAL INSPECTION, FOUND TWO SUPPORT PLATES AT 3RD INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR BETWEEN FUSELAGE FRAMES 15 AND 18 CORRODED. REPLACED BOTH PLATES. REFERENCE: OPERATOR CONTROL NR 96ZZZX824. (X)

Part: INTERCOSTAL — CORRODED (LT FWD FR 15-18)

DURING STRUCTURAL INSPECTION, FOUND 2ND INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR, BETWEEN FRAMES 15 AND 18, CORRODED. REPLACED INTERCOSTAL. (X)

Part: ROD END — WORN (ELEV G-WEIGHT)

FOUND WORN ROD-END ON ELEVATOR G-WEIGHT CONNECTING ROD. REPLACED ROD-END AND RIGGED SYSTEM IAW AMM. (X)

Part: COMBUSTION CASE — FLANGE CRACKED (NR 1 ENGINE)

DURING SCHEDULED INSPECTION, FOUND BLEED AIR FLANGE AT 3 O'CLOCK POSITION ON COMBUSTION CASE CRACKED. REPAIRED IAW TEXTRON (ALLIED SIGNAL) ENGINE MM. (X)

Part: BOLT — CRACKED (LT WING SPOILER)

DURING SCHEDULED NDT INSPECTION, FOUND CRACK INDICATION ON LEFT WING INBOARD AFT SPOILER JACK ATTACH BOLT. REPLACED BOLT. (X)

Part: BOLT — CORRODED (LT ELEV HINGE)

DURING STRUCTURAL INSPECTION, FOUND CORROSION ON LT ELEVATOR NR 2 HINGE UPPER A-FRAME BOLT. REPLACED BOLT. (X)

Part: BRACKET — CRACKED (NR 2 PYLON MOUNT)

DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LORD MOUNT EYE BOLT BRACKET CRACKED. REPLACED BRACKET. (X)

Part: CONTROL CABLE — CORRODED (AILERON)

DURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR 96ZZZX761. (X)

Part: RIVETS — SHEARED (NR 3 PYLON)

DURING SCHEDULED INSPECTION, FOUND 4 RIVETS SHEARED OFF IN NR 3 PYLON BOX AT POSITIONS A, B, C, AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)

Part: BRACKET — BROKEN (NR 4 PYLON)

DURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OPERATOR CONTROL NR 96ZZZX760. (X)

Part: BOLT — CORRODED (RT ELEV HINGE)

DURING STRUCTURAL INSPECTION, FOUND RT ELEVATOR NR 1 HINGE A-FRAME LOWER BOLT CORRODED. REPLACED BOLT. (X)

Part: HOSE — DEFECTIVE (APU FUEL)

DURING SCHEDULED INSPECTION, FOUND EXTERIOR COVERING OF APU FUEL SUPPLY HOSE BROKEN OPEN. REPLACED FUEL HOSE. (X)

Part: BOLT — DAMAGED (LT ELEV HINGE)

DURING STRUCTURAL INSPECTION, FOUND LT ELEVATOR NR 2 HINGE LOWER A-FRAME BOLT TO HAVE DAMAGED THREADS AND CORROSION. REPLACED BOLTS. (X)

Part: BOLT — CORRODED (RT AIL RIB)

DURING STRUCTURAL INSPECTION, FOUND RIGHT AILERON RIB 18 UPPER A-FRAME BOLT CORRODED. REPLACED BOLT. (X)

Part: PIVOT PIN — CRACKED (RT FLAP NR 3)

DURING SCHEDULED NDT INSPECTION, FOUND NR 3 RIGHT FLAP TRACK TAB OPERATING ROD-TO-CROSSHEAD, PIVOT PIN WITH CRACK INDICATION. REPLACED PIN. (X)

Part: JO-BOLT — FAILED (FR 29, STR 12 RT)

DURING SCHEDULED INSPECTION, FOUND BROKEN HEAD ON JO-BOLT AT FRAME 29, STR 12 RIGHT. REPLACED JO-BOLT. (X)

Part: FREIGHT ANGLE — CRUSHED (FS FR 21)

FORWARD CARGO BAY FREIGHT ANGLE AT FRAME 21 CRUSHED. REPLACED FREIGHT ANGLE. (X)

Part: RIVETS — SHEARED (NR 2 PYLON BOX)

DURING SCHEDULED INSPECTION FOUND 2 RIVETS SHEARED OFF IN NR 2 PYLON BOX AT POSITIONS C AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)