N291UE

Part: SKIN — DENTED (ELEV TRIM TAB)

FOUND DENTS LEFT AND RIGHT ELEVATOR SERVO AND TRIM TABS, LEFT AND RIGHT TRAILING EDGE PANELS RIB 14A TO 15, LEFT WING INBOARD CENTER, OUTBOARD SPOILERS, RT WING INBOARD, CENTER, SPOILERS. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 1698-6910003. (M)

Part: FLAP TRACK — DAMAGED (WING)

INSTALL OF FLAP TRACK NR 1 LANDING PLATE FASTENERS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910005. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

FOUND VERTICAL STAB CLOSING ANGLE RT HAS CRACK. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910004. (M)

Part: PLATE — DAMAGED (NR 1 FLAP)

NR 1 FLAP LANDING PLATE DAMAGED, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910002. (M)

Part: TAB — DAMAGED (TE FLAP)

RIGHT OUTBOARD FLAP TAB TRAILING EDGE DAMAGED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS RED AVMAX FAX 1698-6910001. (M)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

FLAP FAULT LIGHT ILLUMINATED. ZERO FLAP LANDING. 74K LBS, TOUCHDOWN SPEED 170 KNOTS, MODERATE BRAKING, BRAKES APPLIED 80 KNOWTS, BRAKE TEMP MAX 470 DEGREES, BRAKE FANS ON. RESET FLAP SYSTEM, PERFORMED F/C AND SAFETY LANE 2 TEST. COULD NOT DUPLICATE. OK FOR SERVICE PER AMM 27-50-00. NO FURTHER INSPECTIONS REQUIRED PER MOM 14-40-13, TR 108. (M)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

DURING INSPECTION FORWARD CARGO BAY B LOOP ON NR 1 DETECTOR FAILED (POSITION 1FW). MAINTENANCE REMOVED AND REPLACED NR 1 SMOKE DETECTOR, OPERATIONAL TEST GOOD.

Part: LINKAGE — DAMAGED (NR 1 ENGINE)

DURING LANDING ROLL OUT, NR 1 GENERATOR FELL OFF LINE A FEW MOMENTS LATER, NR 1 ENGINE FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE UPPER AND LOWER ENGINE CONTROL LINKAGE ROD ENDS. RE-RIGGED CONTROL LINKAGE AND TMS ACTUATOR, GROUND RAN, OPS CHECK GOOD. (M)

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 24,469 hrs · 28,870 cycles

AIRCRAFT EVACUATED DUE TO FUMES IN CABIN. AIRCRAFT SHUTDOWN, FIRE HANDLES PULLED BUT NOT ROTATED. BLEW 3 OF 4 SLIDES, BOTH FRONT AND LT AFT ENGINES SHUTDOWN BEFORE T-HANDLE PULLED. MAINTENANCE REMOVED AND REPLACED YELLOW SYSTEM TUBE ASSEMBLY AND 3 EVAC SLIDES.

Part: TRANSMITTER — FAILED (HYDRAULIC SYS) · airframe 24,346 hrs · 28,739 cycles

LOSS OF HYDRAULIC QUANTITY YELLOW SYSTEM. MAINTENANCE REMOVED AND REPLACED YELLOW SYSTEM HYDRAULIC PRESSURE TRANSMITTER.

Part: FLOW DIVIDER — LEAKING (NR2 ENGINE) · airframe 23,621 hrs · 27,469 cycles

DURING START OF NR 2 ENGINE, A FLIGHT ATTENDANT AND SEVERAL PASSENGERS VERBALLY REPORTED FIRE. NO INDICATION IN COCKPIT. THE NR 2 ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES WERE RELEASED. ACFT WAS EVACUATED VIA RT SIDE EVACUATION SLIDES. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.

Part: PIPE — LEAKING (HYDRAULIC SYS)

HYDRAULIC SMOKE/MIST NOTED IN CABIN AND HYDRAULIC BAY. REMOVED AND REPLACED YELLOW HYDRAULIC SYSTEM PIPE FROM T-CAP TO ANTI-SKID CONTROL VALVE, BLED LEFT SIDE, LEAK CHECKED GOOD. (M)

Part: INTERCOSTAL — CRACKED (BS 9)

INTERCOSTAL IS CRACKED JUST FORWARD OF MAIN LANDING GEAR ROOF LONGERONS AT STATION 9 FRAME 29 FLOOR LOCKDOWN PLATE. REPAIRED IAW FAX REF BARA/AVR/4205/99. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING UPPER WING STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPLACED RT WING UPPER WING STIFFENER AT THIS TIME OUTBOARD OF RIB 8 IAW BAE FAX NR REF DJR/RJ0630-98. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING UPPER WING STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPLACED UPPER WING STIFFENER INBOARD OF RIB 9 AT THIS TIME IAW FAX REF DJR/RJ0630-98. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END AND BETWEEN RIBS 9/10. REPLACED RT WING STIFFENER BETWEEN RIBS 9/10 AT THIS TIME IAW BAE FAX REF DJR/RJ0630-98. (M)

Part: STIFFENER — CRACKED (LT WING)

UPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK IS CRACKED AT FORWARD END, LEFT WING. REPLACED LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK. WORK ACCOMPLISHED IAW BAE SRM STD PRACTICES. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK. WORK ACCOMPLISHED IAW BAE FAX REF JM/RJO317/97 AND FAX REF DJR/RJ0630-98. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IAW BAE FAX DJR/RJ0630-98. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF RIB 9 IAW BAE FAX DJR/RJ0630-98. (M)

Part: LONGERON — CHAFED (FUSELAGE)

THE RIGHT AIRBRAKE UPPER HINGE OPENING UPPER AND LOWER FRAMES HAVE BEEN BADLY CHAFED BY CONTACT WITH THE AIRBRAKE ACTUATOR. REPLACED UPPER LONGERON PER SRM AND FAX BARA/AVR/4144/99. NEW WORKCARD GENERATED TO REPAIR LOWER LONGERON. (M)

Part: INTERCOSTAL — CRACKED (BS 9)

INTERCOSTAL IS CRACKED JUST FORWARD OF MAIN LANDING GEAR ROOF LONGERONS AT STATION 9 FRAME 29 LOWER FLANGE. REPAIRED IAW BAE REPAIR DRAWINGS HC536H9211 AND FAX REF NR DJR/RJ0207/97. (M)

Part: LONGERON — CRACKED (BS 3/7/15/19/20)

MAIN LANDING GEAR ROOF LONGERONS ARE CRACKED AT STATION 3, 7, 15, 19 AND 20 AT FRAME 29. REPAIRED IAW BAE REPAIR DRAWING HC536H9211 AND FAX REF NR DJR/RJ0207-97. (M)

Part: BRACKET — CRACKED (PAX DOOR)

LEFT FORWARD PAX DOOR INTERNAL STRUCTURE HAS 2 ANGLE BRACKETS WITH 1 CRACK IN EACH. MFG AND REPLACED ABOVE 2 ANGLE BRACKETS USING SRM AND DRAWINGS HC521H0507-000 AND HC521H0508-000. REAR 2 EACH TOP AND BOTTOM FASTENERS REPLACED WITH NAS BOLTS PER FAX DJR/RJ0318-97. (M)

Part: WIRE — BROKEN (NR 2 ENGINE)

DEN - FLT 661 - NR 2 EXTINGUISHER USED LT 'ON' ON NR 2 ENGINE. REPAIRED BROKEN WIRE AT TERMINAL STRIP AT FIRE BOTTLE. (X)

Part: WIRE — BROKEN (NR 2 ENGINE)

NR 2 EXTINGUISHER USED. LIGHT 'ON' ON NR 2 ENGINE. REPAIRED BROKEN WIRE AT TERMINAL STRIP AT FIRE BOTTLE.

Part: CLAMP — LOOSE (NR 1 PACK)

DEN - FLT 567 - NR 1 PACK ALREADY ON MEL. DURING CLIMB-OUT THE NR 2 PACK FELL OFF-LINE AND WOULD NOT COME BACK ON FOR 5 MINUTES. TIGHTENED BLOWN CLAMP ON NR 2 PACK. RESET CIRCUIT BREAKER FOR NR 1 PACK, OPS CHECKED OK.