N314FE

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 55,373 hrs · 17,722 cycles

ON CLIMB OUT, RECEIVED LT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED TO SEA. R & R LT WING ANTI-ICE VALVE IAW MM RE F30-11-02-2. ADJ TEST IAW MM REF 30-11-00-5, NO LEAKS NOTED. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (LEFT) · airframe 55,373 hrs · 17,722 cycles

ON CLIMB OUT, RECEIVED LEFT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED. R & R LEFT WING ANTI-ICE VALVE IAW MM RE F30-11-02-2. ADJ TEST IAW MM REF 30-11-00-5, NO LEAKS NOTED. OPS CKS NML. ACFT OK FOR SERVICE, FINAL CLOSED.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,534 hrs · 17,396 cycles

MAIN CARGO DOOR FRAME, CENTERING GUIDE, LOWER AFT SUPPORT FITTING CRACKED. FABRICATED & INSTALLED SUPPORT FITTING.

Part: STATIC INVERTER — INOPERATIVE · airframe 53,297 hrs · 16,923 cycles

EMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-24-00 FAULT D. FOUND STATIC INVERTER BAD. R & R STATIC INVERTER IAW AMM 24-24-01-2, OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (THERMOCOUPLE) · airframe 51,850 hrs · 16,394 cycles

ON CLIMB OUT OF ANC - NR3 ENGINE EGT GAGE FLUCTUATED WILDLY OUT OF 20,000 FT HIT 1020 GOT "ENG 3 EXCEEDANCE ALL ENG 3 OIL, TEM, PRESSURE SHOWED NORMAL DUMPED FUEL RETURNED TO DEPARTURE. ANC R EGT INDICATION NORMAL AFTER SHUTDOWN, VISUAL INSP OF HARNESS APPEARS NORMAL. R & R ALL (4) THERMOCOUPLE HARNESS SEGMENTS REF MM 77-21-01-2. ALSO REPLACED FWD AND AFT THERMOCOUPLE LEADS REF MM 77-21-02-2. RAN ENGINES IAW JRH ALL INDICATIONS NORMAL.

Part: WARNING LIGHT — ILLUMINATED · airframe 51,440 hrs · 16,247 cycles

AT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-01-4.AS PRECAUTIONARY PERFORMED DECAY CHECK ON ALL 3 MANIFOLDS PER AMM 36-00-01-5.ALL MANIFOLDS PASS

Part: CLAMP — LOOSE (THRUST REVERSER) · airframe 51,382 hrs · 16,227 cycles

BASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOW POWER REQUIRED BY THEN. WE WERE ABOUT 3000FT DOWN THE RWY AND DECIDED TO REJECT THE TAKEOFF. NOTE ENG 3 HAS BEEN RUNNING CONSISTENTLY 100-120 DEG CENTIGRADES HIGHER THAN ENG NR 1 AND NR 2 AT GROUND IDLE. INTERROGATE CFD'S FOUND FAULT CODE " 361033 PRV REGULATOR LOW FAULT " AND " 361031 FAV NOT CLOSING FAULT". FOLLOWED FIM FAULT CODE 36-10-12 OPEN NR 3 ENG COWLINGS AND T/R'S FOUND CLAMP LOOSEN AND OUT OF PLACE WITH BIG GAP ON PNEUMATIC DISCHARGE DUC

Part: THROTTLE — MALFUNCTIONED (NR 3) · airframe 51,082 hrs · 16,122 cycles

AFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OFF, THE THROTTLES WOULD NOT STAY ADVANCED PROBABLY DUE TO THE AIRPLANE TRYING TO PROTECT ITSELF DUE TO THE UPPER FOOT LOWERING BELOW PRESENT AIRSPEED. THE SITUATION IMPROVED AS THE FLAPS WERE LOWERED FOR LANDING. REMOVED AND REPLACED NR 3 THROTTLE THRUST REVERSER SWITCH ASSY S1-529.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 50,821 hrs · 16,028 cycles

LT HORIZ STABILIZER L/E, FOUND 1EA CRACK 1,5" LONG ON UPPER FRONT SPAR CAP AT XE 115 REPAIRED IAW SRM 55-20-00 VOL 1, FIG9.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,821 hrs · 16,028 cycles

DURING INSP EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN OF CTR CARGO DOOR 4"X2" DEEP .120". REPAIRED DENT IAW SRM 52-10-00, FIG 6, VOL I.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 50,821 hrs · 16,028 cycles

RT WING INBD FLAP UPPER SKIN FOUND DEEP DENT AND OIL CANING 2.50 INCH X 1.50 INCH DEEP .055 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1-4 VOL I.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 50,821 hrs · 16,028 cycles

INSPECTED UPPER CARGO DOOR JAMB STRUCTURE CORROSION ON UPPER DOOR JAMB. ACCOMPLISHED EA NR 8-5310-129649.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,821 hrs · 16,028 cycles

CTR CARGO COMPT REF EO 8-2550-7-2354 P2 STEP "E1" AFTER REMOVAL PARTS FOUND DEEP CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 50,821 hrs · 16,028 cycles

LT WING EXT STRUCTURE FOUND CRACKED ON LWR EXT SKIN L/E SLAT NR 4. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 & SRM 57-10-00 FIG 43 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 50,821 hrs · 16,028 cycles

LT WING L/E FOUND CRACKED ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: HINGE — NICKED (LT WING TE FLAP) · airframe 50,821 hrs · 16,028 cycles

LT WING INBD FLAP FOUND ON OUTBD HINGE "ON WING" INBD SIDE DEEP NICKS. REPAIRED AREA IAW SRM 57-20-00 FIG 17 SHT 1 VOL I.

Part: BEAM — CRACKED (ZONE 100) · airframe 50,821 hrs · 16,028 cycles

CTR CARGO BILGE INSP FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I.

Part: ANGLE — CRACKED (ZONE 200) · airframe 50,821 hrs · 16,028 cycles

UPPER INT. FUSELAGE COMPT "ZONE 312" DURING REPAIR ASSESSMENT WITH EO 8-5100-7- 5001-P2. FOUND CRACK ON ANGLE UPPER SIDE AFT VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 2B VOL I.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 50,821 hrs · 16,028 cycles

RT WING EXT SURFACE FOUND CRACK ON UPPER EXT SKIN OTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 50,821 hrs · 16,028 cycles

LT WING EXT FOUND 1 EA DENT .75 INCH X 1 INCH MAX DEEP .060 INCH ON INBD FLAP LWR EXT. SKIN LWR PANEL. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 50,821 hrs · 16,028 cycles

LT WING EXT FOUND 2 EA DENTS ON INBD FLAP LOWER EXT. SKIN LWR PNL. 1): 0.75 INCH X 0.50 INCH MAX DEEP 0.070 INCH. 2): 0.50 INCH X 0.50 INCH MAX DEEP 0.060 INCH. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.

Part: SKIN — LOOSE (ZONE 600) · airframe 50,821 hrs · 16,028 cycles

RT WING EXT SURFACE FOUND NR 180 EA LOOSE FASTENERS ON UPPER EXT SKIN OUTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 & SRM 57-20-00 FIG 2 VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 50,821 hrs · 16,028 cycles

DURING INSPECTION LT AIR COND FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 50,821 hrs · 16,028 cycles

RT WING LWR EXT SURFACE FOUND CRACKS AND NR 100 EA LOOSE FASTENERS ON LWR EXT SKIN OTBD FLAP. REPAIRED AREA IAW SRM 57-10-00 FIG 7, SHT 3, VOL I.

Part: FRAME — WORN (ZONE 100) · airframe 50,821 hrs · 16,028 cycles

DURING INSP LT AIR COND FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & 4A VOL I.

Part: FRAME — WORN (ZONE 100) · airframe 50,821 hrs · 16,028 cycles

DURING INSP AVIONIC COMPT BILGE AREA FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4, VOL I.

Part: MEMBRANE — CRACKED (ZONE 200) · airframe 50,821 hrs · 16,028 cycles

AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: MEMBRANE — CRACKED (ZONE 200) · airframe 50,821 hrs · 16,028 cycles

AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,821 hrs · 16,028 cycles

DURING INSP OF COSTANT SECTION STB, FOUND UP PANEL, INSP POSITION 3, WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-129688.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 50,202 hrs · 15,697 cycles

CENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTENSION HANDLE WAS PULLED. ON LANDING ROLLOUT HYD QUE ILLUMINATED, HYD SYS 3 ELEV ILLUMINATED. FOUND HYD LINE TO CENTER GEAR UNLOCK CYLINDER LEAKING, AND UPPER LOCK LINK LUGS FOR UNLOCK CYLINDER ROD DAMAGED. REPLACED LEAKING UNLOCK CYLINDER HYD LINE, UPPER LOCK LINK, AND UNLOCK CYLINDER AND TESTED CENTER GEAR PER M/M 32-38-02-2, 32-16-01-4, AND 32-10-01-5. CENTER GEAR OPERATION TESTED NORMAL. NR 3 HYD RESERVOIR SERVICED TO 7.5 GAL. CENTER GEAR STRUT SERVICED PER STRUT SERVICE PLACARD.

Part: ENGINE — FAILED (NR 1) · airframe 49,964 hrs · 15,565 cycles

DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUST AREA. NO OIL QTY ON NR 1 ENGINE. CREW BLEW NR 1 ENGINE FIRE BOTTLE. REMOVED AND REPLACED ENGINE PER WORK CARDS 71T0101-1 AND 71T0701-1 RUN AND OPS CHECKS GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 49,964 hrs · 15,565 cycles

DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM - INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUST AREA. NO OIL QTY ON NR 1 ENGINE. CREW BLEW NR 1 ENGINE FIRE BOTTLE. REMOVED AND REPLACED ENGINE PER WORK CARDS 71T0101-1 AND 71T0701-1 RUN AND OPS CHECKS GOOD.

Part: ANTI-ICE SYSTEM — INOPERATIVE (RT WINDSHIELD) · airframe 38,953 hrs · 11,414 cycles

RIGHT WINDSHIELD ANTI/ICE INOPERATIVE LIGHT ILLUMINATED SHORTLY AFTER TAKE OFF. REMOVED AND REPLACED RIGHT WINDSHIELD IAW M.M. 56-11-00-2. REMOVED AND REPLACED WINDSHIELD ANTI/ICE CONTROLLER IAW MM 30-41-01-2. GROUND OPS CHECK NORMAL.

Part: TRANSMITTER — LEAKING (HYD SYSTEM) · airframe 37,084 hrs · 10,857 cycles

AFTER 2+15 OF FLT HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PERFORMED RED TABS, WITH FLUID DOWN TO 4.5 GALS. WHEN ENG 3 HYD PUMPS TURNED BACK ON, STARTED TO SLOWLY DECREASE TO 3.5 GALS. ENG HYD PUMPS TURNED OFF WITH QTY HOLDING AT 3.5 GALS. ON LANDING APPROX, NR 3 HYD WENT TO 0.5 GALS/NEARLY ZERO. REMOVED AND REPLACED NR 3 HYD PRESSURE TRANSMITTER, FOUND LEAKING FROM SEAL. OPS CHECK GOOD AS PER MM CHAPTER 29-31-03-2. SERVICED HYD SYSTEM TO NORMAL READING AS PER MM CHAPTER 12-13-01-3. RAN ENGINES AS PER JRH CHAPTER 5 A AND PERFORMED HYD PUMP OPERATIONAL TEST AS PER JRH CHAPTER 9-1. ALL INDICATIONS NORMAL, A/C OK FOR SERVICE.

Part: SEAL — SPLIT (HYD TRANSMITTER) · airframe 36,929 hrs · 10,815 cycles

HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PRESSURE WAS NORMAL, QTY ABOUT 4.5 GALS. RAN RED TABS. LANDED AT TJSJ. HYD LEAK CONFIRMED BY COMPANY MX AFTER LANDING. UPON EXAMINATION, FOUND LEAK TO BE COMING FROM NR 3 HYD PRESSURE XMITTER. REMOVED XMITTER AND FOUND SEAL WAS SPLIT. REPLACED SEAL, P/N NAS 1611-210 AS PER SMP. SERVICED NR 3 HYDRAULICS PER MM 12-13-01. HYD SYS 3 ELEV OFF LIGHT EXTINGUISHED.

Part: PERISEAL — FAILED (PNEUMATIC SYS) · airframe 36,507 hrs · 10,695 cycles

AFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP.

Part: SENSOR — DAMAGED (NLG WW) · airframe 33,248 hrs · 9,773 cycles

AFT T/O AND LAND GEAR UP S/O PNL IND RED UNSAFE NOSE GEAR. RECYCLED LG AND NOSE RED UNSAFE LIGHT ON EXT AND RETRACTION. *S/D* REPLACED DAMAGED NOSE GEAR LOCKED SENSOR PER A/W/D 32-61-04 PG 1 D1-79 AND S/M/P CHAP 20 MM 32-61-03-2. OPS CK NORMAL.

Part: TIRE — DISINTEGRATED (MLG)

00-317 NR 3 & 4 TIRE REQUIRES REPLACEMENT DUE TO DISINTEGRATION ON T/O OUT OF CDG. R&R NR 3, 4, 7, 8 TIRES, & DAMAGED PANELS 152PT, 152MT, 152NT, PER MM 20-21-01-2.

Part: CONTROLLER — MALFUNCTIONED (SLATS)

DURING CLIMB HAD UNCOMMANDED AUTO SLAT EXTENSION.

Part: VALVE — FAILED (ACM BAY)

LOUD BANG FROM REAR OF A/C PRESS BUMP FELT. REMOVED AND REPLACED AIR CONDITIONING SYS AIR CK VALVE IN REF TO AMM 21-22-03-2. OPS CK NORM.

Part: CONNECTOR — FAILED (HYD PUMP)

NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. REPLACED WIRE HARNESS, PLUG CONNECTOR PER WD/M 29-21-01, 29-21-02. REPLACED HYD PUMP AND ELECT MOTOR PER MM 29-21-01-2. OPS AND LEAK CK GOOD.

Part: CONNECTOR — FAILED (HYD PUMP)

NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE.

Part: TRANSMITTER — FAILED (TE FLAP)

99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SIDE. FOUND LT OTBD FLAP POS TRANSMITTER BAD. REMOVED AND REPLACED SAME PER MM 27-54-03-2. OPS CK GOOD. FOUND DUPLEX ACTUATOR INOP MM 27-56-01-2.

Part: TEMP GAUGE — INOP (NR 3 HYD SYST)

NR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AND REPLACED HYDRAULIC GAUGE AFTER TROUBLESHOOTING, RAN SYS, OK FOR SERVICE MM 29-33-01.

Part: CONTROL UNIT — FAILED (LANDING GEAR)

97-0260 - ON T/O CTR AND RT GEAR RED LIGHTS WERE SLOW TO EXTINGUISH, LEFT GEAR LIGHT WENT FROM EXTINQUISHED TO RED RECYCLE GEAR AND ALL LIGHTS EXTINGUISHED. ON LANDING, ALL GEAR LIGHTS AND WARNING HORNS INDICATED UNSAFE, RECYCLED GEAR AND INITIALLY LEFT AND RIGHT MAIN LDG SHOWED DOWN AND LOCKED LANDING WAS UNEVENTFUL. A/C ON JACK FOR INTERNAL LEAKAGE CHECKED ON BOTH UP AND DOWN NIL LEAKAGE FOUND, FREE FALL OK. REPLACED PROX SWITCH CONTROL UNIT LANDING GEAR OPERATION CHECKED PER M/M 32-30-00-5 ALL, SATISFIED.