N290UE

Part: BOTTLE — DISCHARGED (NR 1 INTAKE)

NR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M)

Part: SMOKE — DETECTED (COCKPIT)

ON TAXI, CABIN AND COCKPIT FILLED WITH SMOKE. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURES PER SUP 96-31. CABIN TEMP CONTROL OPS NORMAL, OK FOR SERVICE. (M)

Part: SKIN — DENTED (AIR BRAKE)

DENTS OUT OF LIMITS ON THE RT AIR BRAKE. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584-6900003.

Part: STRUCTURE — DENTED (ELEVATOR TAB)

DENTS OUT OF LIMITS ON THE RT ELEVATOR AND TABS. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584.

Part: PANEL — DENTED (FUSELAGE)

DENTS OUT OF LIMITS ON THE LT WING PANEL BETWEEN RIB 14A AND 15. REPAIR REQUESTED FOR BAE SYSTEM REF.

Part: LONGERON — CORRODED (FUSELAGE)

FORWARD CARGO DOOR CUTOUT LOWER LONGEORN CORROSION DAMAGE COMPLETELY THROUGH THE FACE LONGERON. REPAIR REQUESTED FOR BEE SYSTEM REF AVMAX-FAX 1584-60000. (M)

Part: FRAME — CRACKED (FUSELAGE)

FRAME 32 MLG WHEEL WELL RIGHT AFT BULKHEAD CRACKED IN TWO PLACES IN LOWER FALSE DIAPHRAGM FOR FAIRING ATTACHMENT. PATCH TWO ABOVE AREAS PER SRM 51-71-11. DOUBLE ROW RIVETS 2024 T3 .050 ALUM. (M)

Part: FCU — MALFUNCTIONED (NR 3 ENGINE) · airframe 24,974 hrs · 29,352 cycles

DURING CLIMB NR 3 ENGINE DID NOT RESPOND TO THRUST LEVER POWER CHANGES THEN NR 3 ENGINE TGT STARTED CLIMBING TO 870 DEGRESS PERFORMED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT.

Part: CABLE — DETACHED (SLIDE) · airframe 23,907 hrs · 28,087 cycles

FWD PAX SLIDE DEPLOY CABLE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,592 hrs · 27,720 cycles

FLIGHT ATTENDANT REPORTED LIGHT SMOKE ODOR COMING FROM SEAT 18 D&F AREA INFLIGHT. MAINTENANCE INSPECTED SEAT AREA, NO ODOR NOTED. NO ODOR NOTED FROM AIR CONDITIONING PACKS AS WELL.

Part: BATTERY — DISCHARGED (ESCAPE SLIDE)

NR 2 EVAC SLIDE LIGHTING BATTERY FAILS VOLTAGE CHECK. REMOVED AND REPLACED NR 2 SLIDE ASSY. (M)

Part: VALVE — OUT OF ADJ (NR 2 ENGINE)

NR 2 ENGINE PRODUCED 89.0 PERCENT N1 ON FULL POWER APPLICATION AT ASE N1 REF CALLED FOR 93.4 PERCENT ENGINE ANTI-ICE ON 904 TGT. REMOVED AND REPLACED NR 2 ENGINE FCU POPPET VALVE C/W BLEED BAND ADJUSTMENT AND TAKEOFF POWER CHECK. (M)

Part: RIB — CRACKED (CARGO DOOR)

AFT CARGO DOOR UPPER MOST RIB IS CRACKING LOCATED UNDER UPPER AFT HINGE 'L' BRACKET ON UPPER MOST RIB IAW BAE REPAIR DRAWING REF HC523H9001 AND FOUND SERVICEABLE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: BRACKET — CRACKED (LT WING)

LEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STIFFENER — BROKEN (LT WING)

LEFT WING TE TOP SHROUD SKIN STIFFENER TO FALSE SPAR (AFT END) BROKEN BETWEEN RIBS 7 AND 8. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: BRACKET — CRACKED (LT WING)

LEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: ANGLE — CORRODED (FRAME 50)

RIGHT WEB CLOSING ANGLE AFT OF FRAME 50 HAS ONE INCH CRACK. REPAIRED IAW BAE SRM 51-71-11 FIG 2. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STRUCTURE — CRACKED (FRAME 50)

FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: GUSSET — CRACKED (FRAME 50)

FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE HAS A FILLER PANEL CRACKED AT THE LIGHTNING HOLE. REPLACED GUSSET PLATE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: RIVET — SHEARED (FRAME 50)

FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STRUCTURE — CRACKED (FRAME 50)

FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RIGHT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER FAX JM/RJ049-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: RIVET — SHEARED (FRAME 50)

FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RT UPPER AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: ANGLE — CRACKED (PASSENGER DOOR)

FORWARD PASSENGER DOOR HAS 2 EACH CRACKED ANGLES IN THE HANDLE BOX AREA. MFG AND REPLACED PER BAE DRAWINGS HC521H0507 AND HC521H0508. INSTALLED ANGLES PER SRM AND BAE FAX DJR/RJ0049-97. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: SEAT — CRACKED (CABIN)

FORWARD F/A SEAT PAN CRACKED. REPLACED PAN. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: GUSSET — CORRODED (CABIN)

SEVERAL GUSSET PLATES ON FLOOR ARE CORRODED (SURFACE CORROSION) AFT VESTIBULE. REPLACED CORRODED GUSSET PLATES, 2 EACH. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: LONGERON — CRACKED (FRAME 29)

FRAME 29 MLG BAY ROOF LONGERONS CRACKED, NR 3 AND NR 15, NEAR FORWARD ENG. REPAIRED PER BAE REPAIR DRAWING HC536H9211. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: BOLT — BROKEN (WING)

FRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INSPECTED HOLE, PREP, ALODINE, PRIMED AND INSTALLED NEW BOLT AND NUT IAW FAX DJR/RJ0022/96 AND DJR/RJ0721-96. WITCO BOND WILL BE APPLIED ON WORKCARD 2166. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)

Part: STRUCTURE — CRACKED (NLG)

DURING SCHEDULED NDT INSPECTION OF NGL RETRACTION JACK MOUNT STRUCTURE, FOUND CRAKS IN JACK PIN STRUCTURE BORE. (M)

Part: SWITCH — CONTAMINATED (MLG)

MYR - FLT 690 - UPON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. CLEANED SQUAT SWITCHES.

Part: ROD — BROKEN (PASSENGER DOOR)

ATW - FORWARD PASSENGER DOOR DROPS BELOW DOOR FRAME WHEN OPENED AND DOES NOT DROP AND LATCH PROPERLY WHEN CLOSED. REPLACED BROKEN LOWER ROD END ON THE CONTROL SHAFT ASSY TO TORQUE SHAFT CONTROL ROD. REPLACED LOWER HINGE COVER. NOTE: REMOVED AND REPLACED EVACUATION SLIDE TO FACILITATE MAINTEANCE. DOOR OPERATION CHECKED NORMAL.