N614AW

Part: DOOR FRAME — CRACKED (PAX DOOR)

AFT PAX DOOR, AFT SIDE FRAME, HAS TWO CRACKS APPROXIMATELY .75 INCH LONG NEAR DOOR SNUBBER ATTACHMENT AREA. MAINTENANCE COMPLIED WITH PERMANENT REPAIR. INSTALLED REPAIR PLATE HC521H9032-200 IAW BAE FAX BARA/AVR/6571/03-MK. (M)

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENGINE WENT SUB-IDLE ON APPROACH, HUNG AT 39-40 PERCENT NR 2 AND WOULD NOT ACCELERATE. CREW SHUT DOWN ENGINE. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL.

Part: J-BOX — SMOKE (GENERATOR)

PILOTS REPORT THE FORWARD CARGO SMOKE WARNING LIGHT ILLUMINATED, FIRE BOTTLE WAS FIRED. MAINTENANCE INSPECTED AND FOUND THE SOFT START RESISTOR BOX SMOLDERING. REMOVED AND REPLACED THE RESISTOR BOX ASSEMBLY.

Part: ELEVATOR — CONTAMINATED (TAIL) · airframe 25,130 hrs · 33,643 cycles

PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINTED WATER FROM ELEVATORS.

Part: COUPLING — CRACKED (NR 3 ENGINE) · airframe 24,620 hrs · 33,066 cycles

PIPE ASSEMBLY COUPLING, BOTTLE RT, TO COUPLING FLOW VALVE WAS CRACKED ON NR 3 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE PIPE ASSEMBLY FROM FIRE EXTINGUISHER BOTTLE RT TO FLOW VALVE.

Part: COVER — MISSING (DOOR SLIDE)

UPON REMOVAL OF LEFT FORWARD EVACUATION SLIDE, FOUND D-SHACKLE ASSY MISSING. INSTALLED LT FORWARD EVAC SLIDE. C/W COVER LATCH PULL CHECK AND BATTERY EFFICIENCY CHECK. BOTH CHECKS FOUND WITHIN REQUIRED PARAMETERS. ALL WORK ACOMPLISHED IAW BAE MM AND AIR CRUISERS CMM. CLEVIS AND PIN INSTALLED. SN OFF 0340. PART TC: 10,434. (X)

Part: FASTENER — FAILED (RT MLG WW)

RIGHT MLG BAY, ON EACH FASTENER BROKEN IN MAIN BEAM TO SIDESTAY AT FRAME 29, FASTENER JUST INBOARD APPEARS TO BE LOOSE. REPLACED ONE EACH BROKEN HI-LOC. REMOVED HI-LOC FASTENER JUST INBOARD OF BROKEN FASTENER. CLEANED AND INSPECTED HOLE, HOLE FOUND OK, REPLACED HI-LOC FASTENER. (X)

Part: WEB — CRACKED (NLG WW)

NOSE LANDING GEAR SIDEWALL DIAPHRAGM CRACKED AT UPPER PIN BOSS. REPLACED LT NOSE GEAR DIAPHRAGM IAW BARA/AVRO/3677/99. (X)

Part: BOLT — FAILED (NR 3 PYLON)

NR 2 ENGINE PYLON TO WING, OUTBOARD LOWER BOLT HAD IS SHEARED OFF. REPLACED LOWER OUTBOARD WING TO PYLON BOLT IAW MM 54-52-00. (X)

Part: SKIN — CRACKED (FRAMES 35-36)

THERE IS A 2.75 INCH CRACK IN LT FUSELAGE BETWEEN FRAMES 35 AND 36 AT STR 19, 6 INCHES FORWARD OF FRAME 38. CRACK RUNS STRAIGHT ALONG EDGE OF INNER LAP JOINT. REPAIRED SAID CRACK BY CUTTING OUT DAMAGE AND RIVETING PATCH IAW BAE FAX REF BARA/AVRO/3667/99 DATED JULY 6, 1999. (X)

Part: SLIDE — DAMAGED (PASSENGER DOOR)

MKE - FLT 621 - LEFT FORWARD PASSENGER DOOR EMERGENCY SLIDE HAS DROPPED DOWN IN ITS OWN CONTAINER. REMOVED AND REPLACED LEFT FORWARD PASSENGER SLIDE IAW MM BATTERY EFF CHECK DUE 3-5-99. COVER LATCH PULL OFF TEST C/W. S/N OFF 0310. S/N ON 0340.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP)

CLIMBING OUT OF 20,000 FT, FLAP FAULT ILLUMINATED WITH FLAP GAUGE SHOWING 24 DEGREES AFTER LANDING. FLAPS RETRACTED NORMALLY, GAUGE INDICATED 0 DEGREES.

Part: FLOW VALVE — DETACHED (NR 2 ENGINE)

ATW - NR 2 DIRECTIONAL FLOW VALVE FLAPPER FOUND DETACHED DURING SCHEDULED MAINTENANCE. REPLACED VALVE. VALVE IS PART OF NOSE COWL P/N HC716H001-028B, S/N SB/BAE/0385.

Part: RIVETS — MISSING (FUSELAGE)

INSTALL 2 RIVETS AT RIGHT FUSELAGE FRAME 19 AND STRINGER 21 (REF W/C 2132). INSTALLED 2 RIVETS.

Part: STOP — WORN (LT SPOILER)

LT INBOARD LIFT SPOILER OUTBOARD HINGE BOLT ANTI-ROTATION STOP WORN FROM WORKING BOLT HEAD. REMOVED AND REPLACED ANTI-ROTATION STOP. (M)

Part: SPRING — CORRODED (RT AILERON)

RIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.

Part: STOP — WORN (LT SPOILER)

LEFT MIDDLE LIFT SPOILER INBOARD HINGE BOLT ANTI-ROTATION STEP WORN FROM WORKING BOLT HEAD. REMOVED AND REPLACED ANTI ROTATION STOP. (M)

Part: SKIN — CRACKED (LT SPOILER)

LEFT INBOARD LIFT SPOILER HAS SMALL CRACK IN TOP SKIN AT CENTER HINGE AREA. REPAIRED LEFT INBOARD LIFT SPOILER CENTER, HINGE AREA IAW BAE FAX DJR/RJ0498-97.

Part: BOLT — FAILED (NR 4 TE FLAP)

LEFT NR 4 FLAP UPPER CARRIAGE TO MAIN FLAP FAIL/SAFE BOLT FAILS NDT. INSTALLED SERVICEABLE FAIL/SAFE BOLT AT LEFT NR 4 UPPER CARRIAGE TO FLAP POSITION.

Part: STRUCTURE — CRACKED (FUSELAGE)

UPPER FRAME IN STRUCTURE AFT OF FRAME NR 50 HAS ITS LOWER RIGHT CORNER CRACKED AND THE CLEAT THAT ATTACHES IT TO THE UPPER RIGHT HINGE MEMBER IS LOOSE WITH ONE RIVET MISSING (REF SRM 53-40-31 PG 3 ITEM 14). REPAIRED UPPER FRAME STRUCTURE AFT OF FRAME 50 AT RIGHT CORNER IAW BAE FAX DJR/RJ049697 AND DJH/RJ0749-96.

Part: LINK — CHAFED (NR 1 ENGINE)

NR 1 ENGINE REAR LINK UPPER HALF CHAFED BEYOND MAX ALLOWABLE DEPTH. REPLACED NR 1 ENGINE REAR LINK UPPER HALF, REF ENG CHANGE CHECKLIST FOR DETAILS.

Part: BOLT — CRACKED (FUSELAGE)

FUSELAGE MAIN FRAME LEFT OUTBOARD LOWER FRAME 4 BOLT CRACK INDICATION UNDER HEAD. REPLACED LEFT OUTBOARD LOWER FRAME 4 ATTACH BOLT TO FLT DECK FL00R IAW BAE 146MM. (M)

Part: BOLT — CRACKED (FUSELAGE)

FUSELAGE MAIN FRAME, RIGHT INBOARD LOWER FRAME 4 DAMAGED BOLT NO CRACK INDICATIONS. REPLACED RT INBOARD LOWER FRAME 4 BOLT FOR FLT DECK FLOOR IAW BAE 146 MM. (M)

Part: ACTUATOR BOLTS — FAILED TEST (LT SPOILER)

LEFT OUTBOARD LIFT SPOILER ACTUATORS AFT ATTACH BOLT FAILS NDT. INSTALLED SERVICEABLE BOLT AT LEFT OUTBOARD SPOILER AFT ACTUATOR ATTACH POINT IAW BAE MM. (M)

Part: RIB — CHAFED (VERT STAB)

VERT STABILIZER LEADING EDGE NOSE RIB NR 1 HAS CHAFING DAMAGE ON BOTH SIDES OF LIGHTNING HOLE AT ITS LIP. RT SIDE IS CRACKED DOWN TO THE LIPS RADIUS AND LEFT SIDE IS WORN A LITTLE AWAY AND WAS CAUSED BY ANTI-ICE DUCTING THAT PASSES THROUGH THE HOLE. REPAIR VERT STABILIZER RIB NR 1 CHAFING DAMAGE IAW BAE FAX NR DS/W/TS/28376/0 AND DJR/RJ0930-96. (M)

Part: SHEAR PIN — RUSTED (NR 1 PYLON)

NR 1 PYLON INBOARD SHEAR LINK PIN IS RUSTY, BOLT HAS BEEN REMOVED. REPLACED NR 1 PYLON INBOARD SHEAR LINK PIN IAW BAE DRAWING HC574H0030. (M)

Part: ANGLE — CRACKED (PAX DOOR)

FORWARD PASS DOOR ANGLE CRACKED UNDER MOUNTING BOX TO DOOR OPERATING MECHANISM. REF SRM 52-11-11 FIG 1 (SHEET 1 INCH, DETAIL 'E') ITEM NR 27. REPLACED BOTH ANGLES PER SRM AND FAN DJR/RJ0318-97. (M)

Part: GUSSET — CORRODED (CABIN)

GUSSET PLATE AT FRAME 15, 2ND INTERCOSTAL INBOARD FROM LEFT SIDE AT FORWARD END IS CORRODED IN THE FORWARD VESTIBULE FLOOR SUPPORT STRUCTURE. REPLACED GUSSET PLATE AND REAPPLIED PROTECTIVE FINISHES. (M)

Part: CONTROL CABLE — CORRODED (AILERON)

CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER MAIN AILERON INTERCONNECT CABLES, TENSIONED TO PROPER SETTING AND SAFETIED, (GEN NEW W/C FOR FUNCTIONAL TEST).

Part: BOLTS — DAMAGED (LT AILERON)

LEFT AILERON RIB 20 'A FRAME' BOLTS SHOW EVIDENCE OF DISPLACED 'FAIL/SAFE' PIN. INSTALLED SERVICEABLE FAIL/SAFE BOLTS LEFT RIB 20 AILERON 'A FRAMES'.

Part: BOLT — DAMAGED (RUDDER ACT)

TOP RUDDER ACTUATOR AFT BOLT WAS SCRAPPED BY INSPECTED DEPT DUE TO THREAD DAMAGE. INSTALLED A NEW BOLT IN TOP RUDDER ACTUATOR AFT POSITION.

Part: INTERCOSTAL — CRACKED (CABIN)

FRAME 29 UNDER CABIN FLOOR INTERCOSTAL CRACKED 19 AND 3, 9 FRAME 32 UNDER CABIN FLOOR INTERCOSTAL CRACKED NR 19. REPAIRED INTERCOSTALS AT FRAME 29 AT NR 3, 9 AND 19 POSITIONS AND AT FRAME 32 NR 19 POSITION IAW BAE REPAIR DRAWING HC536H9211 AND FAX DJR/RJ0450-97. REF NDT C/W 5/16/97.

Part: BOLTS — FAILED (RT ELEVATOR)

RIGHT ELEVATOR NR 4 'A' FRAME BOTH BOLTS FAILED NDT. INSTALLED NEW BOLTS IN RIGHT NR 4 ELEVATOR 'A' FRAME. SECURED AND SAFETIED.

Part: BOLTS — CORRODED (LT ELEVATOR)

LEFT ELEVATOR A FRAME HINGE ATTACH BOLTS (BOTTOM) AT HORIZ STAB REAR SPAR AT HINGE POSITIONS 1, 2 AND 4 HAVE PITTING CORROSION AND LESS OF CADNIUM PLATING. REPLACE 3 BOLTS. INSTALLED NEW BOLTS AT LEFT ELEVATOR 'A' FRAME LOWER POSITIONS AT 1, 2 AND 4 HINGES, SECURED AND SAFETIED.

Part: BRACKET — CRACKED (LT WING)

LEFT WING UPPER TRAILING EDGES SHROUD STIFFENER IN AREA BETWEEN WING RIB 3 AND 4 HAS THE BRACKET AT ITS AFT END CRACKED AND A CRACK AT A RIVET HOLE WHERE SAME BRACKET ATTACHES TO LOWER LIP. REPAIRED IAW SRM AND FAX'S DS/W/TS/28612/97 AND DS/W/TS/28596/97 ON LEFT UPPER TRAILING EDGES OF WING SHROUD STIFFENER BETWEEN WING RIB 3.

Part: THRESHOLD — CORRODED (PAX DOOR)

AFT PASSENGER DOOR THRESHOLD HAS HOLE CORRODED THROUGH THRESHOLD. REPLACED AFT PASSENGER DOOR SILL PLATE.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED BETWEEN FRAME 14/15 JUST BELOW REPAIR PATCH RT. ALSO, OIL CANNING OF SKIN HAS BEEN FOUND JUST AFT OF PATCH. COMPLIED WITH RT FUSELAGE PART SKIN REPLACEMENT LAP JNT E FRAME 14-19 RT SKIN CUT LINE APPROX 83.75 INCHES BELOW LAP JNT E. REPAIR ACCOMP IAW INFO CONTAINED IN SRM, BAE FAXS DS/W/TS/28352/97, DH/RJ0495-97. WC GEN TO INSTALL 2 FASTENERS FRAME 19.

Part: BOLT — CRACKED (LT/RT WING)

FRAME 27 LEFT AND RIGHT WING TO FUSELAGE LUG ATTACHMENT BOLT, LOWER, APPEARS TO BE BROKEN. REMOVED BOLTS, NDT SHOWED CRACKS IN BOLTS. CLEAN, INSPECTED HOLE, DIM CHECKS OK, ALODINE, INSTALLED REPLACEMENT BOLT IAW SRM AND FAX DJR/RJ0022-96, FRAME 29 LT/RT WITH COBOND C/W TESTED OK.

Part: CAM BOX SPRING — CORRODED (RT WING)

RIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.

Part: CONTROL CABLE — CORRODED (LT/RT ELEVATOR)

LEFT AND RIGHT ELEVATOR CONTROL CABLES HAVE SIGNS OF CORROSION AT TOP VERTICAL STAB PULLEYS. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR CONTROL CABLES FROM CABLE COMPENSATORS TO REAR PRESSURE BULKHEAD. ADJUSTED IAW MM 27-31-00. GEN W/C FOR FUNCTIONAL CHECK (REF W/C 3055).

Part: FAIRING — CRACKED (LT TE FLAP)

LEFT INBOARD FLAP TRACK AFT FAIRING HAS DAMAGE ON THE INBOARD SIDE. REMOVED AND REPLACED LEFT INBOARD FLAP TRACK AFT FAIRING. (M)

Part: HARNESS — FAILED (RT MLG)

LANDING GEAR HANDLE REQ OVERRIDE ON GEAR RETRACTION AFTER TAKEOFF FROM ORD. REMOVED AND REPLACED RIGHT MLG WEIGHT OFF HARNESS ASSY.

Part: ANTENNA — FAILED (NR 1 VHF)

DEN - FLT 354 - NR 1 COMM RADIO BECOMES TOTALLY UNUSEABLE AS DISTANCE INCREASES TO STATION. COMPLETELY DEAD ON 1ST CENTER FREQUENCY. REMOVED AND REPLACED NR 1 VHF COMM ANTENNA PER MM. OPS CHECK GOOD.

Part: HYD SELECTOR VLV — FAILED (LANDING GEAR)

GEAR FAILED TO EXTEND WHEN SELECTED. WENT TO EMERGENCY AND GEAR EXTENDED. LANDED WITHOUT INCIDENT. SENT REPLACEMENT VALVE AND ACTUATOR TO DEN. REPLACED VALVE AND ACTUATOR.

Part: STIFFENER — CRACKED (BS 25.94)

LEFT AND RIGHT FRAME 29 STIFFENERS CRACKED AT STA 25.94 E.O. E95/005/653. ORIGINAL ISSUE NEEDS TO BE C/W. REPAIRED CRACKED STIFFENERS IAW E.O. E95/005/653, ORIGINAL ISSUE. REPAIR DRAWINGS AW-53-20-9506-06.

Part: SILL — CORRODED (PAX DOOR)

FORWARD PASSENGER DOOR LOWER SILL TO FLOOR FLANGE SILL CORRODED, FRAME 15-18. DRILLED OUT CORROSION, CONFIRMED AREA FREE FROM CRACKS AND CORROSION VIA NDT (DOC ON ANOTHER W/C) REPROTECTED AREA, PRIMED AND REPAINTED. (M)

Part: FIREWALL — CRACKED (APU BAY)

CRACKING HAS BEEN NOTED AT FWD FACE OF THE APU BAY FWD. FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W)

Part: SMOKE HOOD — MALFUNCTION (FWD FLT ATTEND)

FORWARD FLIGHT ATTENDANT SMOKE HOOD APPEARS TO BE ACTIVATED. REPLACED THE SMOKE HOOD.

Part: UPLOCK JACK — REQ BLEED (RT MLG)

AFTER TAKEOFF FROM ATW RT MAIN GEAR WOULD NOT COME UP. RECYCLE ONE TIME GEAR CAME UP. JACKED A/C AND BLEED RT UPLOCK JACK. OPS CK OK. GEAR SWING OK.

Part: BREAKER — TRIPPED (Q-HEATER)

AFTER TAKEOFF FROM ATW, Q-HEATER FAIL WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ATW. MAINTENANCE RESET HEATER ELEMENTS C/B, OPS TESTED OK SEVERAL TIMES.