N309FE

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 51,894 hrs · 16,500 cycles

PDIS: CLIMBING THRU 7000MSL HYD NR 3 PRESSURE CUE LIGHT ILLUMINATED COMPLIED WITH QRH RETURNED TO MEM WHEN THE HYD PUMPS WERE TURNED OFF HYD QTY RETURNED TO 5.7 GALS. WHILE RUNNING QRH CHECKLIST PUMPS WERE TURNED ON HYD QTY DECREASED AND HYD PRESS CUE LIGHT ILLUMINATED. SHUT DOWN HYD SYS 3 QTY SHOWED 6.2 GALS. ALT GEAR HANDLE WAS USED TO EXTEND LANDING GEAR. FOUND HYD FLUID ON TAIL OF A/C FOGGING OUT OF THE DOOR RAN NR 3 HYD SYS AND FOUND SYS 3 HYD S/O VLV MOTOR LEAKING FROM BETWEEN VLV HOUSING AND MOTOR. A GAP CAN BE SEEN BETWEEN VLV MOTOR AND HOUSING. REMOVED AND REPLACED 3-2 NON REVERSIBLE MOTOR PUMP SHUTOFF VALVE. RESET MANUAL EXT HANDLE. CHECKED ENG PUMP AND NR 3 CASE DRAIN FILTER DP INDICATORS. A

Part: SKIN — DAMAGED (ZONE 100) · airframe 51,536 hrs · 16,343 cycles

AIRCRAFT HAS DAMAGE TO SKIN P/N ACA3109-1 AT STA 603 BETWEEN LONGERONS 47 AND 48 AND P/N ACA3039-513 CLIP AND NCA 6313-17 LONGERON 47, AS A RESULT OF A FIRE OF THE EXTERNAL POWER WIRING. EXTERNAL POWER WIRING ALSO HAS DAMAGE. REF N/R 004, CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER SRM 53-20-00. REF N/R 005, CUT OUT DAMAGED STRINGER DRILLED NEW STRINGER PER SRM 51-00-01. REF N/R 006, DRILLED NEW CLIP PER SRM 51-00-01. REF N/R 007. FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-10-00. REF N/R 008, FABRICATED AND INSTALLED NEW BRACKET PER SERVICE BULLETIN 24-11 PG 7. REF. N/R 009, CLEANED POWER FEEDER CABLES PER SMP ISSUED EA NR 8-2440-112390. REF W/O 37161

Part: BUTTERFLY VALVE — CRACKED (BLEED VALVE) · airframe 47,284 hrs · 14,643 cycles

DURING COMPLIANCE WITH WIC 49C1701 SEQ 267, FOUND APU NR 2 SYSTEM LOW PRESSURE BLEED VALVE BUTTERFLY CRACKED AND WITH MISSING MATERIAL THAT RESULTED TO NR 2 ENGINE CHANGE.

Part: THROTTLE CABLE — FROZEN (NR 2 ENGINE) · airframe 47,196 hrs · 14,610 cycles

NR 2 ENGINE THRUST LEVER REMAINED FROZEN AT 80 PERCENT ON DESCENT INTO SJC. DID A PRECAUTIONARY SHUTDOWN AT 10,000 FT. NO OTHER PROBLEMS NOTED. UPON CREW DEBRIEF FOUND NR 2 THROTTLE LEVER STUCK AT 1/3 TRAVEL. MOVED THROTTLE LEVER AND FOUND SLIGHT BIND WHICH ENDED UPON FURTHER CYCLES. QUESTIONED CREW ON SHUTDOWN, AND OIL PRESSURE WAS PRESENT. FOUND NR 2 ENG THROTTLE CABLE TO BE OF THE SEALED TYPE AND THUS CANNOT BE LUBRICATED / BLOWN OUT. REQUIRES CABLE ASSY.

Part: INTERCOSTAL — CORRODED (RT MLG WW) · airframe 47,098 hrs · 14,574 cycles

EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL, AFT BULKHEAD AT LONGERON 36. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 47,098 hrs · 14,574 cycles

CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (LT MLG WW) · corrosion level 2 · airframe 47,098 hrs · 14,574 cycles

CORROSION FOUND ON INTERCOSTAL IN LEFT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 47,098 hrs · 14,574 cycles

EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL, AFT BULKHEAD AT LONGERON 30. REMOVED AND REPLACED INTERCOSTAL.

Part: RESERVOIR — LEAKING (NR 3 HYD SYSTEM) · airframe 46,925 hrs · 14,512 cycles

HYD SYS 3 ELEV OFF LT ILLUMINATED IN CRUISE AT FL 270 PERFORMED RED TAB PROCEDURES, DUMPED FUEL & RETURNED TO MEM. NR 3 HYD QUANT DROPPED TO 0. FOUND NR 3 HYD RESERVOIR LEAKING AT TOP ON INBOARD OF SIGHT EYE. SIGHT GLASS CRACKED. REMOVED AND REPLACED RELIEF AND SAMPLING VALVE, SIGHT GLASS ON RESERVOIR. SERVICED NR 3 SYSTEM HYDRAULICS. PERFORMED LEAK CK ON SYSTEM, NO LEAKS NOTED. RED TAB PROCEDURE MANUAL GEAR EXTEND HANDLE USED. RESTORED MANUAL GEAR HANDLE TO NORMAL CONFIGURATION. REMOVED AND REPLACED BOTH LT & RT NR 3 EDP'S CHECKED NR 3 HYDRAULIC MANIFOLD FILTERS, OK ALL OPS AND LEAK CHECK GOOD.

Part: RELAY — FAILED (ANNUNCIATOR) · airframe 44,916 hrs · 13,901 cycles

IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1MIN THEN WENT OUT. RED TABS REQUIRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5-5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD.

Part: RELAY — FAILED (ANNUNCIATOR) · airframe 44,916 hrs · 13,901 cycles

IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1 MIN THEN WENT OUT. RED TABS REQUIRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5-5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD.

Part: ENGINE — FAILED (OIL SYSTEM) · airframe 44,008 hrs · 13,630 cycles

APPROX 1710Z FL330 CRUISE, RECEIVED A NR 1 ENG OIL LOW LIGHT, WITH L/O PSI & 0 OIL QUANTITY. ENG WAS SHUT DOWN IAW RED TABS. WINDMILL RPM REMAINED THROUGH OUT FLT. PER FLIGHT CREW EMP 447288 THE NR 1 ENG WAS RUN AT IDLE FOR A MINIMUM OF 2 MIN PER MM REF 72-00-00-6-1. THE ENG WAS OPERATED WITHOUT OIL PRESSURE IN IDEL FLIGHT OR GROUND FOR 2 MINS. THE ENG MUST BE REMOVED. REMOVED AND REPLACED NR 1 ENG PER W/C 71T0101-1 & 71T0.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 42,175 hrs · 13,104 cycles

ENGINE NR 3 TEMP LIMITING POWER ALL REGIMES. SHORTLY AFTER TAKEOFF RECEIVED LOOP B FIRE LIGHT. ENGINE 3 FIRE LOOPS, A AND B BOTH TEST PROPERLY, REDUCED PWR, LOOP LIGHT EXTINGUISHED, PARAMETERS STABLE. DIVERTED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 41,902 hrs · 12,997 cycles

AFTER T/O ON FLAP & SLAT RETRACTION HAD SLAT DISAGREE LIGHT ILLUMINATE. FOLLOWED RED TAB TO SLAT EXTEND LIGHT EXT. RETURN TO AIRPORT. DUMPED FUEL. INSPECTED ALL 6 SENSORS & TARGETS. PERFORMED BITE TEST ON SENSOR AT PROX BOX. ALL TESTS GOOD. DID SHAKE TEST ON ALL SLATS AT SENSORS, NO DISAGREE LIGHT SHOWING. CYCLED SLATS MANY TIMES & COULD NOT REPRODUCE MALFUNCTION. R&R PROX SWITCH CONTROL BOX FOR PRECAUTION & REPEATED ALL ABOVE TESTS. ALL CHECK NORMAL. NO HISTORY SHOWN. ALL MX DONE IAW MM 27-80-01-6 2 AND 27-84-01-2.

Part: DRIVE SHAFT — SHEARED (CARGO DOOR) · airframe 40,274 hrs · 12,441 cycles

CENTER CARGO DOOR LIFT ACT OUTPUT DRIVE SHAFT SHEARED, CAUSING DOOR TO FREE FALL AND IMPACT MAINTENANCE STAND.

Part: DRIVE SHAFT — SHEARED (CARGO DOOR) · airframe 40,274 hrs · 12,441 cycles

CTR CARGO DOOR LIFT ACTUATOR OUTPUT DRIVE SHAFT SHEARED, CAUSING DOOR TO FREE FALL AND IMPACT MAINTENANCE STAND. REMOVED AND REPLACED ACTUATOR CTR CARGO COMPARTMENT PER MM 52-32-01 & 52-32-07.

Part: PROXIMITY SENSOR — FAULTY (L/E SLAT) · airframe 39,163 hrs · 12,059 cycles

SLAT DISAGREE LIGHT ILLUMINATED. FOLLOW RED TABS. REMOVED AND REPLACED PROX BOX PER IAW MM 32-61-01-2. OPS CHECK GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 37,867 hrs · 11,636 cycles

AFT FUSELAGE COMPARTMENT ZONE 312 BS Y2122.881 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PER DRAWING AJC 7372.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 37,867 hrs · 11,636 cycles

FUSELAGE COMPARTMENT ZONE 312 BS Y2092.880 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PER DRAWING AJC 7028.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 37,867 hrs · 11,636 cycles

AFT FUSELAGE COMPARTMENT ZONE 312 BS Y2046.000 CANT UPPER ANGLE BRACKET FOUND CRACKED. *S/D* ANGLE FAB AND REPLACED PER DRAWING AJC 7021.

Part: WARNING — ACTIVATED (AC DOOR)

AIR COND DOOR LIGHT ON S/O PNL ILLUM IN FLT DURING CLIMB. VERIFIED AND RECORDED IN AML. AC DOORS ARE CLOSED BY VISUAL INSP PRIOR TO EACH DEPARTURE.

Part: VANE — FAILED (RT TE FLAP)

BUFFET ENCOUNTERED AS FLAPS SEL TO 35 DEG EXT BUFFET INCREASED WHEN FLAPS 50 DEG EXT SEL. REMOVED AND REPLACED RT I/B AND O/B FLAP VANE ASSY AND OPS CK NORM PER MM 27-50-03-2.

Part: SKIN — DAMAGED (AC COMPT DOOR)

FOUND DAMAGED SKIN OF NR 3 AIR CONDITION COMPARTMENT ACCESS DOOR AT ARRIVAL. INSPECTED INSIDE OF NR 3 PACK COMPARTMENT, FOUND OK. OPS TESTED NR 3 PACK, FOUND NO VIBRATION. INSPECTED INSTALLATION AND CONDITION OF THE RT LANDING LIGHT, FOUND GOOD. DAMAGED SKIN OF NR 3 PACK COMP DOOR SHEET METAL WAS REPAIRED PER SRM 52-10-00 VOL 1 AND REWORK CONDITION WAS GOOD.

Part: DOOR — DAMAGED (NR 3 A/C COMPT)

97-0215 NRT STBD SIDE AIR CONDITIONING DOOR FOUND DAMAGE ON PRE FLIGHT. CANNIBALIZED THE NR 3 AIR COND COMP DOOR ASSY BETWEEN A/C N313FE'S AIR COND COMP DOOR. DOOR OPERATION CHECKS OK. THIS IS A DUPLICATE TO CORRECT THE OPERATOR CONTROL NR IT WAS SENT AS 97FDEA00215 IT SHOULD HAVE BEEN 97FDEA00792.

Part: DOOR — DAMAGED (NR 3 A/C COMPT)

97-0215 NRT STBD SIDE AIR CONDITIONING DOOR FOUND DAMAGE ON PREF LIGHT. CANNIBALIZED THE NR 3 AIR COND COMP DOOR ASSY BETWEEN A/C N313FE'S AIR COND COMP DOOR. DOOR OPERATION CHECKS OK.