N560UA

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,732 hrs · 21,147 cycles

CABIN FLOORBEAM STA 377 HAS CORROSION AT LBL-61. INSTALLED PARTIAL UPPER FLOORBEAM CHORD REPLACEMENT REPAIR TO STA 377 BETWEEN LBL 12 AND LBL 70 REF ECRA 5310-05536.

Part: SKIN PANEL — UNKNOWN (FUSELAGE) · airframe 71,732 hrs · 21,147 cycles

CATEGORY 'B' REPAIR INSTALLED FROM STA 590 - 630 BETWEEN S-14L AND S-19L.

Part: RECEPTACLE — DAMAGED (EXTERNAL POWER) · airframe 71,718 hrs · 21,144 cycles

GROUND POWER RECEPTICLE DAMAGED. CASING IS CRACKED, 4 PINS DAMAGED. REPLACED RECEPTACLE PER MM.

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE) · airframe 71,637 hrs · 21,129 cycles

IN REF TO RIGHT ENGINE SHUTDOWN, EPCS PAGE SHOWN DIS-EEC, S SVA OR FCU-EEC, P SVA OR FCU-EEC. LOWER RIGHT BOTTOM DISPLAYED OIL P RED. REPLACED FUEL PUMP AND FUEL CONTROL UNIT PER AMM.

Part: LIGHT — UNSECURE (CABIN) · airframe 71,237 hrs · 21,053 cycles

SEAT SIDE LIGHTS FALLING OUT AT ROW 5 AND 10. SECURED ROW 5 AND REPLACED FWD LIGHT ASSEMBLY AT 5B. EMERGENCY LIGHTS CHECK OKAY.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 70,171 hrs · 20,846 cycles

RIGHT ENGINE HI STAGE EICAS MSG ON TAKEOFF ROLL. ABORTED TAKEOFF AT 80 KTS. CREW STATES DURING TAKEOFF ROLL LIGHT CAME ON APPX 40-50 KTS LIGHT DID NOT EXTINGUISH AND FINAL SPEED REACHED WAS APPROX 80-90 KTS WHEN TAKEOFF ABORTED. COMPLIED WITH MEL 3611D. REPLACED HIGH STG VLV AND CONTROLLER NEEDS ENGINE RUN-UP TO CONFIRM OPS CHECK.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 69,745 hrs · 20,764 cycles

ON APPROACH, INPUT FLAPS 25, FLAPS ONLY WENT TO 22. SAME ON SECOND APPROACH. AFTER TOUCHDOWN FLAPS MOVED TO 25 DEGREES. DECLARED EMERGENCY PRIOR TO SECOND ATTEMPT. TRAILING EDGE EICAS ILLUMINATED. ACCOMPLISHED FLAP SYS. RESET & OPS TESTED PER AMM. ALL FLAPS AND INDICATIONS NORMAL, NO FSEU FAULTS NOTED.

Part: WIRE — FAULTY (FSEU) · airframe 69,362 hrs · 20,691 cycles

FSEU 2 TRIPPED DURING CRUISE. MEGGER WIRES FROM CB FSEU 2 SENSOR TO BENCH PLUG D3258A PIN F3, & TO T153 PWR TFMR, CHECKED GOOD. CHECKED ALL FLAP POSITION SENSOR OHMS, RESISTANCE TO FSEU M10332, CHECKED OKAY.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 68,985 hrs · 20,619 cycles

UPON START LEFT ENGINE PACK WOULD NOT SHUT DOWN WITH PACK SWITCH AND NO EICAS PACK OFF LIGHT. REPLACED LT PACK FLOW CONTROL VALVE, OP'S CHECKED OKAY.

Part: TRANSMITTER — FAULTY (NR 1) · airframe 68,990 hrs · 20,620 cycles

STATUS MESSAGE FLAP-SLAT ELECTRIC APPEARS CHRONIC. ALL CBS IN. REPLACED L/E SLAT PDU POSITION TRANSMITTER PER MM. FSEU CHECKS GOOD PER MM. PART BORROWED FROM CONTINENTAL. P/N 18-1969-14 AND S-N 0245A. NEXT SEGMENT RCV'D FLAP-SLAT ELEC ON STATUS PAGE---REPEAT WRITE UP. REPLACED NR 2 FSEU.

Part: LATCH — OUT OF ADJUST (CABIN) · airframe 68,963 hrs · 20,615 cycles

OXYGEN MASK DOOR AT DOOR 2R HANGING OPEN. RT MID GALLEY HAS O2 MASKS FROM PREVIOUS 2 CLASS CONFIG, O2 MASK BOX IN GALLEY IS CONSIDERED INOPERATIVE, HOWEVER NO SEATS ARE TO BE BLOCKED. CONFERRED WITH TOMC. MID GALLEY O2 BOX TAPED OVER. ADJUSTED LATCH MECHANISM DOOR LATCH, OPS CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 68,470 hrs · 20,520 cycles

EEL LIGHT BROKEN AT SEAT 9B. REPLACED LIGHT ASSY, OPS CK GOOD.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 68,427 hrs · 20,512 cycles

LEFT CENTER FUEL PUMP LOW PRESS DOES NOT ILLUMINATE, BULB CHECKS GOOD. MEL PROCEDURE COMPIED WITH, EICAS MESSAGE CHK'D OKAY. RESET SYS RAN PUMPS WITH FUEL DOOR OPENED, OPS OK. CLOSED DOOR PUMPS OFF.

Part: ENGINE — MAKING METAL (LEFT) · airframe 68,196 hrs · 20,468 cycles

AFTER NR 1 ENGINE START, LT ENGINE OIL FILTER EICAS AND STATUS MESSAGES, FOLLOWED FM PROCEDURES. MX REPORTED METAL IN MAIN OIL FILTER, ANGLE GEARBOX CD, MAIN GEARBOX CD AND ON NR 1, 2, & 3 BEARING CD, REPLACED LEFT ENGINE PER AMM.

Part: SCREW — MISSING (TE FLAP) · airframe 68,128 hrs · 20,455 cycles

SCREW MISSING ON OTBD FLAP ASSY OTBD SIDE AFT PART ON LEFT WING. REPLACED MISSING SCREW ON RIGHT O/B TE FLAP FAIRING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,476 hrs · 20,332 cycles

EMERGENCY LIGHT AT SEAT 18C AND 21C INOPERATIVE. REPLACED EMERGENCY LIGHT. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (ROW 25) · airframe 66,705 hrs · 20,179 cycles

ROW 25 EMERGENCY PATH LIGHT IS INOPERATIVE. REPLACED PATH LIGHT, CHECKED OKAY.

Part: CONTROL UNIT — FAULTY · airframe 66,618 hrs · 20,162 cycles

RIGHT RECIRCULATION INOPERATIVE WITH EQUIPMENT OVERHEAT EICAS & LIGHT WITH OEV OPEN EQUIPMENT CLOG FLOW STATUS MESSAGES. REPLACED BPCU PER MM AND RELAY K10079 POWER TRANSFER RELAY REF WDM, RAN ENGINE PER JRH. ALL SYSTEMS OP OK. RESET ALL SYSTEMS, NO MESSAGES OR FAULTS.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 66,098 hrs · 20,058 cycles

EXIT SIGN AT 8B FALLING OFF. SUPPLEMENTAL DATA UPDATE SECURED LENS.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 65,717 hrs · 19,982 cycles

HIGH PITCH SQUEAL WINDOW 1L STARTED ABOUT 20 MINUTES AFTER LEVEL AT CRUISE. WINDOW FOUND DEFECTIVE. REPLACED WINDOW.

Part: SUPPORT ANGLE — CORRODED (BS 1020-1040) · airframe 65,202 hrs · 19,884 cycles

UPPER CABIN RIGHT SIDE, BL 70.5 FROM FUSELAGE STATION 1020-1040 HAS CORROSION ON OTBD SUPPORT ANGLE ON BOTTOM SIDE AROUND RIVETS. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED CREASE BEAM PER INSTRUCTIONS ON EA PD57-53-087. THIS REPAIR CONSIDERED A PERMANENT REPAIR PER 8100-9.

Part: PRESSURE DECK — CORRODED (BS 1681) · airframe 65,202 hrs · 19,884 cycles

CORROSION ON AFT PRESSURE DECK AT BS 1681 FROM RBL 0 TO RBL 50. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL PER SRM FOUND AREAS OUT OF LIMITS. A PERMANENT REPAIR ACCOMPLISHED PER SRM REPAIR 2 USING EA 57-53-090 AND 8100-9 DATED FEB 25, 2011.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 65,202 hrs · 19,884 cycles

CORROSION ON FLOORBEAM BS 1640, RBL 30, RBL 19, RBL 13, AND RBL 10. MAJOR REPAIR ACCOMPLISHED: FOUND TO BE OUT OF LIMITS, R & R DAMAGED SECTION IAW SRM.

Part: SKIN — GOUGED (R1 DOOR) · airframe 65,202 hrs · 19,884 cycles

MED R1 HAS INTERNAL SKIN GOUGE UNDER COCKING ROD END-TORQUE TUBE BOLT. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 365 RBL 15) · airframe 65,202 hrs · 19,884 cycles

CORROSION ON FLOORBEAM AT LOCATION BS 365 AT RBL 15. MAJOR REPAIR ACCOMPLISHED: CORROSION REMOVAL IS BEYOND LIMITS REQUIRING REPLACEMENT. REPLACED FLOORBEAM IAW SRM. TREATED AND PRIMED AREA.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 64,152 hrs · 19,684 cycles

FIRST OFFICER'S O2 MASK NOT TESTING (NO YELLOW X DURING TEST) REPLACED F/O OXYGEN MASK AND STOWAGE BOX.

Part: ACM — FAULTY · airframe 63,865 hrs · 19,628 cycles

F/A REPORTS UNUSUAL AIR NOISE COMING FROM OVERHEAD EXIT SIGN BY COCKPIT DOOR. OPEN THE AREA INSIDE AND DO A CLOSE INSP OF THE AREA. ACCOMPLISHED INSP AS REQ REF EG4766 & EG4764. ALSO REPLACED LT ACM REF SEQ 8652011. REF SEQ 8652005 FOR AIR NOISE BELOW FLOOR 2C. AND ACP EG4771 FOR FASTENER INSTALLATION.

Part: SEAL — LEAKING (CABIN WINDOW) · airframe 63,559 hrs · 19,568 cycles

WINDOW AT 9A LEAKING FROM BOTTOM OF WNDOW PANE DURING RAINSTORM INTO CABIN AND ONTO FLOOR. WINDOW AT 9A LEAKING FROM BOTTOM OF WNDOW PANE DURING RAIN STORM INTO CABIN AND ON TO FLR. FOUND LT AFT EMERGENCY DOOR EXIT SEAL OUT OF RETAINER APPROX 3 INCHES AT BOTTOM FWD, SECURED SEAL. WINDOW PANE OK.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 62,651 hrs · 19,388 cycles

F/O MASK MICROPHONE INOPERATIVE. REPLACED MASK ASSY, GROUND CK NORMAL.

Part: LIGHT — BROKEN (SEAT 8 AB) · airframe 62,437 hrs · 19,347 cycles

SEAT 8AB 1 EACH SEAT MOUNTED EMERGENCY LIGHT BROKEN OFF. REPLACED LIGHT ASSY, CHECKS GOOD.

Part: LIGHT — BROKEN (SEAT 8 AB) · airframe 62,437 hrs · 19,347 cycles

SEAT 8AB 1 EACH SEAT MOUNTED EMERGENCY LIGHT BROKEN OFF. REPLACED LIGHT ASSY. CHECKS GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 62,313 hrs · 19,324 cycles

CREW REPORTED NOSE GEAR DID NOT EXTEND WITH ALTERNATE EXTEND SWITCH ON (3) ATTEMPTS. PERFORMED LANDING ALT EXTENSION CHECK WITH ACFT ON JACK, TESTED ALT GEAR EXTENSION 3 TIMES, OPS CHECK IS GOOD, ACFT WILL BE ON TEST FLT AND WILL BE VERIFIED BY EG CREW. WORK IS ACP ON NR 2009N00226 AND INSP BY QC 828. CHECK OF ALT GEAR EXT GOOD. WILL CHECK ON DESCENT. ON DESCENT, CHECKED ALT GEAR EXT-OPS WAS NORMAL. NFF

Part: LANYARD — OUT OF POSITION (L4 GIRT BAR) · airframe 60,004 hrs · 18,880 cycles

DOOR 4L IS DIFFICULT TO ARM AND DISARM. CLEANED OUT EXCESS STRING FROM THE BOTTOM OF TRACK. GIRT BAR STRING WAS OUT OF POSITION AND REINSTALLED.

Part: LAMP — NO TEST (EMERGENCY LIGHTS) · airframe 59,511 hrs · 18,782 cycles

EMERGENCY LIGHT AT 20DEF, ON OVERHEAD STOW BIN, WILL NOT ILLUMINATE DURING TEST. RELAMPED, CHECKS GOOD.

Part: COOLING FAN — FAILED (E&E BAY) · airframe 58,505 hrs · 18,593 cycles

ODOR IN COCKPIT AND CABIN FL370 OBH FOLLOWED BY EQUIP OVRHT EICAS AND OVHT ON EQUIP COOLING SW. FOUND PRIMARY E&E COOLING FAN FAILED, SMELLED BAD AND BEARING FAILED. NO DEBRIS IN DUCTING. REMOVED & REPLACED PRIMARY E&E COOLING FAN. OPS CHECK NORMAL. NO SMELL IN COCKPIT OR CABIN WITH PACKS ON & OFF. TEST ACCOMPLISHED.

Part: GUIDE VANE — LEAKING (NR 1 ENGINE) · airframe 58,188 hrs · 18,533 cycles

OIL ODOR IN CABIN. FOUND THE EXIT GUIDE VANES OIL SPLASHED ALL AROUND THE AREA AND A SMALL PUDDLE RT UNDER THE 6:00 O'CLOCK POS UNDER THE EXIT GUIDE VANES. REPLACED NR 1 ENGINE.

Part: ENGINE — ODOR (LEFT) · airframe 58,161 hrs · 18,528 cycles

ACRID ODOR IN COCKPIT ON TAKEOFF ROLL AND TAKEOFF CLIMB. NEARLY CAUSE FOR ABORT. ODOR SLOWLY DISSIPATED ON CLIMB. ODOR MUCH LIKE A HOT PAC. SUSPECT LT ENGINE. REPLACED NR 1 ENGINE. RAN ENGINE AT IDLE FOR 5 MINUTES, CHECKED EPCS PAGE OF EICAS FOR FAULTS. CHECKED FOR LEAKS AT MAIN OIL FILTER, LAST CHANCE OIL FILTER, NR 4 BEARING SCAVENGE MANIFOLD, OIL FILTER DIFFERENTIAL PRESSURE SWITCH, CHIP DETECTORS, AIR-OIL HEAT EXCHANGER, SCAVENGE PUMP, OIL TANK AND ACCESSORIES, OIL PRESSURE TRANSMITTER, AND LOW OIL PRESSURE SWITCH. ACP LEAK CHECK DURING IDLE RUN. NO LEAKS OR DEFECTS NOTED.

Part: FASTENER — IMPROPER PART (LIGHT FIXTURE) · airframe 57,812 hrs · 18,462 cycles

RAT FAILED TO DEPLOY. FOUND HOLE IN PITOT STATIC LINE. HOLE CAUSED BY TOO LONG FASTENER IN LIGHT FIXTURE IN CEILING AREA. INSTALL NEW STATIC LINE SECTION AND LEAK CHECKS GOOD. OPS CHECK OF RAT DEPLOYMENT CHECKS NORMAL.

Part: STATIC LINE — DAMAGED (PITOT/STATIC SYS) · airframe 57,812 hrs · 18,462 cycles

RAT FAILED TO DEPLOY. FOUND HOLE IN PITOT STATIC LINE. HOLE CAUSED BY TOO LONG FASTENER IN LIGHT FIXTURE IN CEILING AREA. INSTALL NEW STATIC LINE SECTION AND LEAK CHECKS GOOD. OPS CHECK OF RAT DEPLOYMENT CHECKS NORMAL.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW PRESSURE PULLEY STEM LEAKING. REMOVED & REPLACED SHAFT O-RING AND BACK-UP RING.

Part: CONTACT — DIRTY (R2 DOOR SLIDE) · airframe 56,036 hrs · 18,123 cycles

THE R2 DOOR SLIDE IND LIGHT INOP, STAYS DIM. CONTACT AT INDICATOR LIGHT 2R DOOR IS DIRTY. CLEANED CONTACT AT DOOR 2R INDICATOR LIGHT, ALL OPS CHECKS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,266 hrs · 17,783 cycles

EMERGENCY LIGHT INOP AT DOOR 1R. FOUND BULB INOP. RELAMPED BULB.

Part: REGULATOR — LEAKING (OXYGEN MASK) · airframe 53,840 hrs · 17,703 cycles

FIRST OFFICER OXYGEN MASK HARNESS LEAKING AIR AND WILL NOT INFLATE. FOUND LEAKING REGULATOR. REPLACED FO O2 MASK. OPS CHECKED OK.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 52,473 hrs · 17,446 cycles

SEAT 19ABC EEL LIGHT CONNECTOR IS BROKEN OFF AT EEL LIGHT CONNECTOR.

Part: HANDLE — STICKS (R4 DOOR) · airframe 51,340 hrs · 17,228 cycles

FLT ATTENDANT STATED DOOR 4R DISARM HANDLE STICKS. FOUND DIRT AND GARBAGE IN GIRT BAR RETAINER. CLEANED AND LUBRICATE.

Part: BATTERY — INOPERATIVE · airframe 50,854 hrs · 17,136 cycles

FLIGHT DIVERTED DUE TO BATTERY MESSAGE. TEMPORARILY LOST ALL F-O FLT INSTRUMENTS. CAME BACK ON AFTER A FEW MINUTES. [08-07-07] FO INSTRUMENTS CAME BACK ON AFTER A FEW MINUTES. REPLACED MAIN BATTERY AND BATTERY CHARGER.

Part: HYDRAULIC SYSTEM — UNKNOWN (RIGHT) · airframe 48,718 hrs · 16,728 cycles

LOST RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY. DAMAGED RT SYSTEM HYD RETURN LINE WAS REPLACED.

Part: ODOR — DETECTED (CABIN) · airframe 45,073 hrs · 16,030 cycles

MADE DESCENT TO 11,000 FEET DUE TO CABIN PRESSURE PROBLEM AND ODOR IN THE CABIN. REPLACED AUTO PRESSURE CONTROLLER PER MM21-31-02. OPS CHECK OK.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

AFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. FRAME HAS BEEN REPAIRED PER TIMCO REO G-09850, REV A, WITH A J-ANGLE PER EVA 40168.

Part: SLIDE — LEAKING (CABIN)

POROSITY THROUGHOUT DOGLEGS AROUND ASPIRATOR FLANGES AND SEAMS. POROSITY LEAKAGE FOUND AT DOGLEGS, ASPIRATOR FLANGES AND SEAMS. REPLACED INFLATABLES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FRAME DENTED ON INBD FLANGE STA 1480, STR 25L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 39,821 hrs · 14,700 cycles

RT WING, INBOARD FLAP, UPPER SKIN CHAFED ON OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH .032 INCH BONDED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FLOORBEAM CAP AT BS 324, LBL 50 - LBL 72 CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH T-CAP SPLICE.

Part: ACTUATOR — FAILED (RAT) · airframe 39,821 hrs · 14,700 cycles

RAT FAILED MANUAL DEPLOY OPS CHECK. RAT ACTUATOR FAILED AND WAS POPPING THE CIRCUIT BREAKER. REPLACED ACTUATOR. DURING ACTUATOR REPLACEMENT, FOUND BENT BLADE. REPLACED HUB ASSY.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

AFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FRAME DENTED STA 1580 ABOVE STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH A NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FRAME DENTED ON INBD FLANGE, BS 1400 STR 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED A NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FRAME AT STA 1540 ABOVE STR 25L IS DENTED, INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

FRAME IS DENTED STA 1500, STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH NESTED J-ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,821 hrs · 14,700 cycles

BS 365, RBL 10-RBL 72, FLOORBEAM CAP CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH ANGLES AND SHIMS.

Part: CREASE BEAM — CORRODED (STA TO) · airframe 39,821 hrs · 14,700 cycles

CABIN FLOOR CREASE BEAM WEB CORRODED ON UPPER SURFACE FROM STA 968.5 TO 969.5, RBL 70 - RBL 71. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLER.

Part: LIGHT — BURNED OUT (ESCAPE SLIDE) · airframe 36,558 hrs · 13,523 cycles

EXTERIOR EMERGENCY SLIDE LIGHT IS INOP AT DOOR 1R. RELAMPED

Part: EEC — FAILED (RT ENGINE) · airframe 31,358 hrs · 11,608 cycles

RIGHT ENGINE ROLLBACK ON TAKEOFF. PRIMARY ENGINE CONTROL MESSAGE P-EEC, P275-16. REPLACED EEC. CHECKED SENSE LINES, FOUND SECURE. ANOTHER WRITE UP OCCURRED AFTER THE EEC WAS REPLACED FOR ENGINE ROLL BACK AT START. THE LOWER PB WATER TRAP VENT HOLE WAS FOUND CLOGGED. ENGINE OPERATION HAS BEEN NORMAL SINCE THEN. THE PROBLEM LIKELY OCCURRED DUE TO A COMBINATION OF THE EEC PB TRANSDUCER AND THE CLOGGED LINE.

Part: SENSE LINE — LOOSE · airframe 31,144 hrs · 11,542 cycles

ABORTED TAKEOFF DUE TO LOSS OF POWER ON RIGHT ENGINE. BURNER SENSE LINE LOOSE.SECURED SENSE LINE.

Part: COOLING FAN — FAILED (CABIN) · airframe 30,252 hrs · 11,228 cycles

SMOKE IN CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST CONFIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HONEYWELL IS WORKING ON FIXING THESE COOLING FAN FAILURES RESULTING IN APU REMOVALS.

Part: COOLING FAN — FAILED (COCKPIT) · airframe 30,225 hrs · 11,216 cycles

SMOKE IN CABIN AND COCKPIT. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST CONFIGURATION (-6) WHICH WAS INSTALLED ON THIS APU ON JUNE 11, 1999. THIS HAS BEEN A LONG TIME PROBLEM, AND HONEYWELL IS WORKING IN FIXING THESE COOLING FAN FAILURES RESULTING IN APU REMOVALS.

Part: COOLING FAN — FAILED (COCKPIT) · airframe 30,222 hrs · 11,213 cycles

SMOKE IN THE COCKPIT AND CABIN. SUPPLEMENTAL DATA UPDATE FOUND COOLING FAN SHAFT SHEARED AND FAN HOUSING BROKEN. THIS IS THE LATEST -6 FAN WHICH WAS INSTALLED ON THIS APU. HONEYWELL IS WORKING ON THIS LONG TIME PROBLEM WHICH HAD CAUSED MANY DELAYS AND DISCREPANCIES, RENDERING THE APU INOPERATIVE RESULTING IN APU REMOVALS.

Part: FUEL CONTROL — OUT OF ADJ (NR 1 ENGINE) · airframe 25,668 hrs · 9,473 cycles

DIVERTED TO MCI DUE TO NR 1 ENGINE SURGE. *S/D* THE FUEL CONTROL UNIT WAS FOUND TO BE OUT OF ADJUSTMENT. THE FCU WAS REPLACED.

Part: SHAFT COUPLING — SHEARED (NR 5 SCAVENGE)

DIVERTED TO DEN UNDER AMBER ALERT DUE TO LOSS OF OIL PRESSURE ON THE NR 2 ENGINE. *S/D* FOUND OIL LUBE SCAVENGE UNIT WITH A SHEARED SHAFT. ENGINE WAS REPLACED. UPON DISASSEMBLY OF OIL LUBE SCAVENGE FOUND 8/40 BOLT INSIDE THE NR 5 SCAVENGE PUMP. UPON ENGINE DISASSEMBLY ALL BEARINGS WERE REPLACED AND EXPOSED AREAS WERE INSPECTED. NO METAL WAS FOUND.

Part: GIRT BAR — OUT OF ADJUST (DOOR 3R)

DOOR 3R WOULD NOT ARM. *S/D* SLIDE ARMED LIGHT DID NOT COME ON WHEN SLIDE ARMED. FOUND GIRT BAR OUT OF SEQUENCE. READJUSTED GIRT BAR. OPS CHECKS NORMAL.

Part: RESERVOIR — LOW PRESS (NR 2 RT DOOR)

NUMBER TWO RIGHT DOOR HAD EMERGENCY POWER RESERVOIR HAD LOW PRESSURE. REPLACED THE EMERGENCY POWER RESERVOIR PER MM 52-11-30.

Part: FUEL STORAGE — LEAKING (RT AFT SPAR)

EVIDENCE OF FUEL LEAKING FROM REAR SPAR INBOARD OF NR 2 ENGINE PYLON. AIRCRAFT INSPECTED AND DETERMINED SAFE TO FERRY TO SFO FOR REPAIR. *S/D* SEALED LEAK AT WB 16 RIGHT AFT SPAR, OPERATION CHECKS NORMAL.

Part: EEC — DEFECTIVE (SOLDER JOINTS)

EEC EXHIBITS FRACTURED SOLDER JOINTS: CHAN 'A' PROCESSOR BD. LOCATION U427, PIN NR 15 (UVPROM) BD ASSY 781336-9-068, SN 89011490. CHAN 'B' PROCESSOR BD. LOCATION U427, PIN NR 14 (UVPROM) BD ASSY 781338-9-068, SN 89012339. CAUSE OF FRACTURING IS UNKNOWN AT THIS TIME. SUSPECT OXIDIZED CHIP LEADS.

Part: ENGINE — MALFUNCTION (RT ENG)

RIGHT ENGINE MADE UNCOMMANDED INCREASE TO MAX POWER. SHUTDOWN ENGINE. DISASSEMBLY SHOWED SIGNS OF METAL SLIVERS ON THE LOW SIDE OF THE PRESSURE RELIEF VALVE WHICH CAUSED THE VALVE TO MALFUNCTION.