N560FE

Part: CONTROL UNIT — UNKNOWN (FUEL) · airframe 103,347 hrs · 35,208 cycles

ON CLIMBOUT FL280 TANK 3 TIP TRAP FUEL 5.6K TRAPPED. TANK 3 PUMPS OFF. REMOVED AND REPLACED FSC IAW AMM 28-08-01-4. OPS TEST GOOD. A/C OK FOR SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 103,207 hrs · 35,122 cycles

PDIS 560 27-80 4198 06NOV18 MEM FACT U LOGPAGES:2954473 SLAT DISAG WHEN FLAPS 35 SELECTED. WENT AROUND AND DID EXT/ 22 LANDING PER QRH. SHGN 06NOV18 09:01 MEM U T/S IN REF TO MD10 FIM 27-80-00-2. NO SLAT DISAG INDICATION SHOWN. INTERROGATED PSEU, FCC1 AND FCC2. NO FAULTS FOUND. CYCLED FLAPS AND SLATS SEVERAL TIMES WITH NO FAULTS FOUND. PERFORMED PRECAUTIONARY R-T-S OF PSEU IN REF TO MD10 AMM 31-71-01-2. NO FAULTS FOUND. REQUIRES MORE T/S. SHGN 06NOV18 10:50 MEM U PERFORMED RTS REF AMM 22-00-00-5-0. FCC 1 & FCC 2 SLATS RTS PASSED. OK FOR SERVICE. FACT 06NOV18 10:58 MEM U FACT. T/S IN REF TO MD10 FIM 27-80-00-2. NO SLAT DISAG INDICATION SHOWN. INTERROGATED PSEU, FCC1 AND FCC2. NO FAULTS FOUND. CYCLED FLAPS AND SLATS SEVERAL TIMES WITH NO FAULTS FOUND. PERFORMED PRECAUTIONARY R-T-S OF PSEU IN REF TO MD10 AMM 31-71-01-2. NO FAULTS FOUND. REQUIRES MORE T/S. SHGN 06NOV18 10:50 MEM U PERFORMED RTS REF AMM 22-00-00-5-0. FCC 1 & FCC 2 SLATS RTS PASSED. OK FOR SERVICE. FACT 06NOV18 10:58 MEM U FACT.

Part: RIB — GOUGED (LT WING) · airframe 103,191 hrs · 35,117 cycles

LEADING EDGE OF LEFT WING BETWEEN NR 3 AND NR 4 SLATS HAS METAL DAMAGE, ( CAUSED BY MIGRATED ECCENTRIC BOLT, ECCENTRIC BOLT ON SEPARATE NON-ROUTINE.) REPAIRED LEADING EDGE RIB DAMAGE REF EA 8-5710-T0343204 PART 1.

Part: HYDRAULIC LINE — LEAKING (RT AILERON) · airframe 103,129 hrs · 35,072 cycles

HYD 3 FAIL WHEN SLATS EXTENDED, HYD 3 OFF INTO MEM ALTERNATE GEAR EXTENSION USED HYD 3 WENT TO ZERO. FOUND RT AIL PRESS LINE LEAKING STEADY AT BRAZED FITTING JUST OTBD OF INBD AILERON ACTUATOR. REMOVED AND REPLACED NEW LINE USING 2 FITTINGS. REF MM 20-10-01-2. SERVICED AND BLED HYDRAULIC SYS 3 REF AMM 12-13-02-3. PERFORMED LEAK CHECK AT BOTH FITTINGS AND THE B-NUT GOING TO AIL ACTUATOR LINE.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 ENGINE) · airframe 103,120 hrs · 35,068 cycles

AT FL290, DURING DESCENT, RECEIVED A NR 2 ENGINE FIRE ALERT, LOOP A, LOOP B MEL FROM PREVIOUS FLIGHT. RAN QRH, NO OPTION BUT TO SHUTDOWN THE NR 2 ENGINE FOR FIRE ALERT. DISCHARGED THE FIRE BOTTLE. RECIEVED A SECOND FIRE ALERT DURING DESCENT MOMENTARLY, THEN EXTINGUISHED. INSPECTED THE NR 2 ENGINE AND NO SIGNS OF FIRE. REMOVED AND REPLACED THE NR 2 ENGINE PYLON FIRE DETECTOR IAW MM 26-11-02-4. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 102,809 hrs · 34,855 cycles

SLAT DISAG ALERT ON SHORT FINAL WHEN FLAP WAS COMMANDED. ALL STEPS OF TSI 27-80/3882 COMPLIED WITH. REMOVED AND REPLACED D1-118 SLAT PROX SWITCH IAW AMM 27-84-02-4 AND PERFORMED ADJUSTMENT CHECK AND OPS CHECK IAW AMM 27-84-02-4.ALL CHECKS GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 102,233 hrs · 34,508 cycles

SMOKE IN THE COCKPIT, RETURNED TO DEPARTURE. RAN ENGINES AT FLIGHT IDLE FOR 20 MINUTES WITH ALL 3 PACKS RUNNING, NO DISCREPANCY NOTED IAW JRH CHAPTER 6. REMOVED AND REPLACED WATER SEPARATOR COVERS AND COALESCER BAGS IAW AMM 21-53-00-7

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING OTBD FLAP UPPER SURFACE AT XOF 587 IS CRACKED 26 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-10-00 V1, FIG 85, SH 3 & 4.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING OTBD FLAP UPPER SURFACE AT XOF 581 IS CRACKED, 22 INCHES FWD OF TRAILING EDGE. PERFORMED A REPAIR IAW SRM 57-10-00 V1, FIG 85, SH 3 & 4.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING OTBD FLAP UPPER SURFACE AT XOF 581 IS CRACKED, 13 INCHES FWD OF TRAILING EDGE. PERFORMED A REPAIR IAW SRM 57-50-00 V1, FIG 85, SH 3 & 4.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING OTBD FLAP UPPER SURFACE AT XOF 587 IS CRACKED 10 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-10-00 V1, FIG 85, SH 3 & 4.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING OTBD FLAP UPPER SURFACE AT XOF 587 IS CRACKED 8 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-10-00 V1, FIG 85, SH 3 & 4.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 102,232 hrs · 34,507 cycles

MAIN CABIN, STA 1790 RBL 60 SEAT TRACK HAS WEAR INDICATION. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 AND DWG.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 102,232 hrs · 34,507 cycles

MAIN CABIN, STA 1778 RBL 60 SEAT TRACK HAS WEAR INDICATION. OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 DWG.

Part: SKIN — CANNING (RT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

RIGHT WING INBD FLAP, LWR SURFACE XIFH 310 SKIN IS OIL CANNED. REMOVED AND REPLACED THE SKIN PANEL IAW DWG ARC2443 AND ARC 2458.

Part: SEAT TRACK — WORN (BS 1697) · airframe 102,232 hrs · 34,507 cycles

MAIN CABIN, BS 1697, RBL 12, SEAT TRACK LOBE WORN, OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM 53-70-00, FIG 1.

Part: CHANNEL — CORRODED (BS 2007) · airframe 102,232 hrs · 34,507 cycles

AFT WASTE TANK AREA, BS 2007 BULKHEAD, LT SIDE UPPER SUPPORT FITTING HAS CORROSION. REMOVED AND REPLACED THE CHANNEL IAW DWG NJC6040. MAJOR REPAIR

Part: LUG — CORRODED (LT WING TE FLAP) · airframe 102,232 hrs · 34,507 cycles

LEFT OTBD FLAP INBD AFT HINGE INBD PIVOT BORE LUG CORRODED. REMOVED CORROSION IAWCMM 57-52-02 AND E.A. 8-5710-T0337658

Part: DOUBLER — CRACKED (LT WING) · airframe 102,232 hrs · 34,507 cycles

LEFT WING LOWER FIXED L/E. JUST INBD OF FUEL PANEL 519CB. FWD L/E STRUCTURE IS CRACKED. REMOVED AND REPLACED THE DOUBLER IAW DWG ARB1180, SRM 51-35-01, VOL II, AND SRM 51-33-01, VOL II.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 102,232 hrs · 34,507 cycles

RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39R HAS A .250 INCH CRACK. REPAIRED IAW DWG SR10530064, & EA 8-5310-T0337596.

Part: TEE FITTING — CRACKED (BS 595) · airframe 102,232 hrs · 34,507 cycles

LEFT BS 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A .500 IN. CRACK AT THE LOWER FASTENER HOLE. REPAIRED IAW EA 8-5310-T0337595.

Part: SKIN — DENTED (BS 675) · airframe 102,232 hrs · 34,507 cycles

BS 675 STRINGER 38, SKIN DENTED AND CREASED. REPAIRED IAW SRM 53-20-00 FIG.5, SHT. 1 VOL. 1.

Part: SKIN — CORRODED (BS 1139) · corrosion level 2 · airframe 102,009 hrs · 34,412 cycles

SKIN ON THE RT FUSELAGE, AT BS 1139, STRINGER 44R IS BULGING AND RIVETS DISHING. INSTALLED A REPAIR IAW SRM 53-20-00, FIG 6.

Part: BATTERY PACK — INOPERATIVE (SLIDE PRESSURE) · airframe 101,938 hrs · 34,370 cycles

FOUND THE EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATOR FOR THE L1 DOOR INOPERATIVE. REMOVED AND REPLACED THE L1 SLIDE PACK PRESSURE REMOTE INDICATOR BATTERIES IAW AMM 25-61-03-2. OPS CHECKED GOOD IAW 25-61-03-5.

Part: THERMOCOUPLE — FALSE INDICATION (NR 3 ENGINE) · airframe 101,660 hrs · 34,205 cycles

RECEIVED A NR 3 ENGINE EXCEEDANCE LEVEL ONE MOMENTARILY ON THE TAKEOFF ROLL (AFTER 80 KTS) ELECTED TO CONTINUE DUE TO A REPEAT WRITE UP. DURING CLIMB EGT WAS FLUCTUATING INTO RED, 1072 . RETURNED TO DEPARTURE. REMOVED AND REPLACED THE UPPER LEFT, LOWER LEFT, UPPER RIGHT AND LOWER RIGHT THERMOCOUPLE HARNESSES IAW MM 77-21-01-2. REMOVED AND REPLACED FWD AND AFT THERMOCOUPLE LEADS IAW MM 77-21-02-2, STEP 1 AND 2 OF TSI. COMPLETED TSI 77-20/2868. PERFORMED POWER ASSURANCE CHECK IAW JRH. EGT PARAMETERS ARE WITHIN LIMITS WITH NO FLUXUATIONS OR DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: SENSOR — FAILED (NR 2 ENGINE) · airframe 100,136 hrs · 33,379 cycles

8 MINUTES AFTER T/O, CLIMBING THROUGH FL 190, WE GOT A LEVEL 2, ENG 2 OIL TEMP HI, 2 OIL TEMP WAS AMBER AT 170. TEMP CONTINUED TO CLIMB TO 181 AND TURNED RED. THE QRH WE SHUT THE ENGINE DOWN AND RETURNED TO DEPARTURE. R & R NR 2 ENGINE OIL TEMP SENSOR.

Part: A/C PACK — LEAKING (NR 3) · airframe 100,102 hrs · 33,359 cycles

AFTER TAKEOFF AT ABOUT FL 200, INCREASED TEMP ON ALL THREE TEMP SELECTORS AND COCKPIT FILLED WITH SMOKE. TURNED THE TEMP SELECTORS TO FULL COLD AND RAN THE SMOKE, FIRE, AND FUMES CHECKLIST IN THE QRH. THE SMOKE DISIPATED. RAN ALL THREE ENGINES, UNABLE TO DUPLICATE FAULT. ISOLATING ENGINES AND PACKS. INSPECTED PACK COLESER BAGS, FOUND OIL LEAKING IN NR 3 PACK.

Part: SEAT TRACK — DAMAGED (BS 1381-1341) · airframe 100,000 hrs · 33,298 cycles

LOCK S1388 BETWEEN POSITION 7L AND 8L FOUND LOOSE, UPON FURTHER INSPECTION FOUND SEAT TRACK IS DAMAGED. REPLACED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00.

Part: SLIDE — CONTAMINATED (CONTROL HANDLE) · airframe 99,981 hrs · 33,285 cycles

WHEN GEAR HANDLE WAS PLACED TO THE DOWN POSITION THE GEAR DID NOT EXTEND, IN ADDITION THE GO AROUND BUTTON WAS PUSHED AND AC DID NOT CYCLE TO G/A. FOUND THE GEAR HANDLE SLIDE WAS STICKING, GEAR WAS DOWN AND LOCKED BUT INDICATED RED UNSAFE. CLEANED STICKY SUBSTANCE FROM SLIDING HANDLE. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD PER AMMS 12-22-01-7 AND 32-30-00-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

FORWARD CARGO, BILGE AREA , CORRODED AT STATION 824, LONGERON 51R & 52. NR 532 APPLIES TO THIS REPAIR. REPAIRED FWD CARGO BILGE IAW EA 8-5330-T0322604 PART 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

FORWARD CARGO AREA STATION 765 - 824, LONGERON L51 IS CRACKED AT AFT END. R & R LONGERON IAW SRM 51-33-01.

Part: SKIN — WORN (RT WING) · airframe 99,239 hrs · 32,922 cycles

RIGHT WING, FIXED LE SURFACE ISLAND, ABOVE 3 PYLON, LOWER SKIN SURFACE SHOWS WEAR FROM CONTACT WITH DROOP LE. REPAIRED IAW EA 8-5730-T0322697.

Part: FRAME — CRACKED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

LEFT SIDE FUSELAGE STATION 1159, HAIR PIN FITTING FOUND CRACKED FROM FWD EDGE AT TOP HOLE, PROPAGATING AFT TO CTR WEB. CRACK CONTINUED THRU RADIUS & STOPS. NR 560 INCLUDED ON THIS REPAIR. REPAIRED IAW EA 8-5310-T0322543 PART 1.

Part: NOSE COWL — CRACKED (NR 3 ENGINE) · airframe 99,239 hrs · 32,922 cycles

NUMBER 3 ENG INLET NOSE COWL APPROX 6:00 POSITION HAS HORIZONTAL CRACK UNDER BOLTS. R & R NR 3 ENG NOSE COWL IAW MM 71-11-00-2.

Part: RIB — CRACKED (NR 1 NACELLE) · airframe 99,239 hrs · 32,922 cycles

NUMBER 1 ENG PYLON HORSE SHOE RIB, JUST FWD OTBD OF PRECOOLER AT BRACKET ATTACH POINT, HAS A 2 INCH CRACK. R & R WEB IAW DWG AUB7027.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK, SEAT-TRACK DAMAGED, STATION 1641, LBL 9. REMOVED DAMAGED SEAT TRACK SECTION & INSTALLED NEW ONE IAW SRM 57-70-00 FIG 1.

Part: BOLT — LOOSE (THRUST REVERSER) · airframe 99,239 hrs · 32,922 cycles

NUMBER 3 ENG LT THRUST REVERSER, MOUNTING RING LATCH ASSEMBLY HAS 16 LOOSE BOLTS. QUALITY CONTROL REQUESTS, TORQUE CHECK, ON ALL MOUNTING RING ATTACHMENT FASTENERS. TIGHTENED AND TORQUE CHECKED ALL BOLTS ON MOUNTING RING LATCH ASSY IAW AMM 78-32-11-2.

Part: ATTACH BOLT — LOOSE (THRUST REVERSER) · airframe 99,239 hrs · 32,922 cycles

NUMBER 3 ENG LT THRUST REVERSER, UPPER LATCH ATTACH BOLTS LOOSE, 5 EACH. TORQUED UPPER LATCH ATTACH BOLTS IAW AMM 78-32-11-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK AT BALL MAT AREA, SEAT TRACK LUG IS DAMAGED AT APPROX BS 615, RBL 28. REMOVED DAMAGED TRACK & REINSTALLED NEW SECTION.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK SEAT-TRACK LUG IS DAMAGED AT APPROX BS 637, RBL 8. REMOVED DAMAGED SEAT TRACK. INSTALLED NEW TRACK SRM 53-70-00.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 99,239 hrs · 32,922 cycles

RIGHT VERTICAL STAB AFT FAIRING SKIN HAS A .100 INCH CRACK INDICATION, PROPAGATING FWD OF A REPAIR WASHER AT STATION 2159. REPAIRED IAW EA 8-5530-T0322471. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1635, RBL48. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1641, 48 RBL. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK AT BALL MAT AREA, SEAT TRACK LUG IS DAMAGED AT APPROX STATION 754, LBL 47. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1765, 28 RBL. REPLACED DAMAGED SEAT TRACK IAW 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,239 hrs · 32,922 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1444, 28 LBL. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00.

Part: SOCKET — LOOSE (L1 DOOR) · airframe 982 hrs · 32,301 cycles

L1 DOOR LIGHT WILL NOT CHECK. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C EXPIRATION 07 APR 15. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01. VERIFY & RECORD IN THE AML. EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. VERIFIED SLIDE SYS CHARGED. FOUND INDICATOR SOCKET ASSEMBLY LOOSE. SECURED RETAINER. OPERATIONS CHECKED GOOD IAW MM 25-61-03.

Part: CABLE — LOOSE (L1 DOOR) · airframe 979 hrs · 32,170 cycles

FOUND RT DOOR 1L CABLE OFF OF PULLEY. REMOVED AND INSTALLED L1 DOOR DRIVE CABLES IAW AMM 52-10-02-2-0. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FUSE — CRACKED (HYDRAULIC SYS) · airframe 97,045 hrs · 31,662 cycles

DURING NORMAL GEAR RETRACTION AT 170KTS HYD SYS NR 3 FAILED. FLUID QTY RAPIDLY DECREASED TO ZERO, OCCURRED WHILE USING RMP'S TO PRESSURIZE HYD SYS NR 3. ENG NR 3 PUMPS WERE SELECTED OFF. GEAR HAD BEEN CYCLED 5 TIMES PRIOR TO THIS FAILURE WITH NO PROBLEM. R & R HYD TRIM FUSE BLED NR 3 SYS & TRIM CYLINDER. PERFORMED GEAR SWING INCLUDING ALTERNATE EXTENSION & RETRACTION. ALL SYS CHECKED NORMAL, NO LEAKS NOTED. SUBSEQUENT TEST FLIGHT TESTED GOOD.

Part: CONTROL VALVE — CRACKED (PRIMARY TRIM) · airframe 96,483 hrs · 31,383 cycles

HYD 3 FAIL ON CLIMB OUT OF BQN. 4 FLUID IN NR 3 ADDED MPN PE5-5GL CPN 0022024 QTY 2 FLUID MSN 1342557. PRIMARY TRIM CONTROL VLV INSTALLED IAW MD10 AMM 27-43-03-4. SERVICING NR 3 HYD SYS. WILL PERFORM LEAK & OPERATION CHECK IAW MD10 AMM 27-43-03.

Part: UNION — LEAKING (HYD SYSTEM) · airframe 95,939 hrs · 31,080 cycles

DURING CLIMB TO FL 330, RECEIVED LEVEL 1 HYD 3 ELEV OFF. HYD QTY INDICATED 4.7 GAL. QTY DECREASED TO 2.7 AND RECEIVED HYD 3 OFF. USED ALTERNATE GEAR EXTENSION. NR 3 ENGINE RAN FOR APPROX 25 MINUTES WITH HYD 3 OFF. R & R HYDRAULIC LINE UNION AND CHECK VALVE. GEAR SWING REF AMM 32-31-03-2

Part: BATTERY — INOPERATIVE (R1 DOOR SLIDE) · airframe 95,525 hrs · 30,870 cycles

R1 DOOR SLIDE INDICATOR LIGHT IS DIM WHEN TESTED. REPLACED R1 DOOR SLIDE BATTERIES, OPS CHECKED NORMAL.

Part: SKIN — CORRODED (BS 1721-1761) · corrosion level 2 · airframe 94,354 hrs · 30,226 cycles

CENTER CARGO CORROSION FOUND ON SKIN STA 1721-1761, LONGERON 51R-52. REPAIRED CORRODED AREA AS PER EA 8-5310-153338.

Part: SKIN — CORRODED (BS 1129-1145) · airframe 94,354 hrs · 30,226 cycles

LOWER FUSELAGE, LT SIDE AT APPROX STA 1129-1145, LONGERON 43L-48L, HAS AN EXISTING REPAIR DOUBLER APPROX 16 X 37", DOT 18 EXFOLIATION CORROSION FOUND ON SPLICE AT STA 1131 LONGERON 45L. REMOVED CORROSION AT BODY STA 1130 THRU 1141, LONGERON 48L. PERFORMED UT THICKNESS MEASUREMENT ON AREA. FABRICATED FILLER, INNER DOUBLER AND OUTER DOUBLER. INSTALLED FAB'D PARTS IAW EA 8-5330-160916.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,354 hrs · 30,226 cycles

AFT CARGO ON TOP OF FLOORBEAM HAS LIGHT CORROSION AT STA 1841 FROM BL 0 - LBL 30. R & R FLOORBEAM AND ANGLE IAW SRM 51-31-01 AND DWG AGA 3874.

Part: FEEDER CABLE — BURNED (NR 3 ENGINE) · airframe 94,354 hrs · 30,226 cycles

NR 3 ENG POWER FEEDER BUNDLE, PHASE "B" CABLE ARCED INSEDE OF THE PYLON AT STA YN-362. REPLACED POWER FEEDER CABLE ASSY IAW EO 8-2450-7-5009 P2, OPS CHECK COMPLIED WITH. STAND-OFF BRACKET, CLAMPS AND HARDWARE REPLACED.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 94,354 hrs · 30,226 cycles

LEFT WING OTBD FLAP HINGE FWD RT ATTACH FITTING HAS A CRACK. REMOVED CRACKED ATTACH FITTING. LOCATED HOLES IN NEW FITTING AND SPOTFACED AS REQUIRED PER PRINT NRB6013. INSTALLED NEW FITTING PER SRM 51-41- 01, PRINT NRB6013, SRM 51-33-01, AND AMM 20-20-01-2.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 94,354 hrs · 30,226 cycles

LEFT WING OTBD FLAP INBD HINGE FWD LT ATTACH FITTING APPEARS TO HAVE A CRACK BETWEEN THE 2ND AND 3RD LOCK FASTENER. REMOVED CRACKED FITTING. LOCATED NEW FITTING AND SPOTFACED PER PRINT B6013. INSTALLED NEW FITTING PER SRM 51-41-01, PRINT B6013,SRM 51-33-01,AND AMM 20-20-01-2.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,354 hrs · 30,226 cycles

TEE AT THE LEFT SLANT PANEL CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED TEE ANGLE IAW SRM 53-40-00 FIG.11 SHEET 2.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,354 hrs · 30,226 cycles

SUPPORT ANGLE CORRODED IN MULTIPLE PLACES. REMOVED CORRODED ANGLE IAW DWG APB7080. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW DWG APB7080.

Part: BLADES — DAMAGED (NR 3 COMPRESSOR) · airframe 93,990 hrs · 30,031 cycles

ON TAKEOFF, WITH INITIAL ADVANCE OF THROTTLES, GOT NUMEROUS COMPRESSOR STALLS. RETARDED THROTTLES AND NOTICED ENGINE NR 3 EGT HIGH. SHUTDOWN ENG NR 3 AND RETURNED TO GATE. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST OF NR 3 ENGINE NO OBVIOUS DEFECTS NOTED. NR 3 VIA SHOWS NO EXCEEDENCES. PER STALL INSPECTION IAW 72-00-06-1. FOUND VSV FEEDBACK CABLE BENT BY BELLCRANK. PERFORMED BORESCOPE ON NR 3 ENGINE FOUND SEVERAL BLADES WITH TIP CLANGE ON THE 4TH STAGE OF COMPRESSOR. REMOVED AND REPLACED NR 3 ENGINE AS PER WORK CARD 71T0701-3. A/C OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,277 hrs · 29,654 cycles

EMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK IAW MM 33-51-01-4-0. CKS NORMAL.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 93,255 hrs · 29,643 cycles

RT FLAP T/E (BACKSIDE) HAS NUMEROUS POPPED RIVETS AND CRACKED SKIN BETWEEN THE RIVETS (SEVERAL INCHES LONG) APPROX 15 FT IN FROM OTBD END OF FLAP. TEMPORARY REPAIR ACCOMPLISH IAW SRM 57-10-00 FIG 9, VOLUME 1 AND EA 8-5750-153011.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 92,392 hrs · 29,191 cycles

PRIOR TO DESCENT FROM CRUISE, 3 LEVEL 1 ALERTS APPEARED. TANK 3 TIP TRAPPED, TANK 3 PUMP OFF, TANK 3 TRANSFER PUMP OFF. SEVERAL MINUTES AFTER INITIAL DESCENT BEGAN THE ALERTS WENT AWAY AND PUMPS BEGAN OPERATING . EMERGENCY WAS DECLARED. R & R 3 & 4K FLOAT SWITCH IAW AMM28-43-01. OPS AND LEAK CHECKED GOOD.

Part: SWITCH — FAILED (TANK FLOAT) · airframe 92,134 hrs · 29,062 cycles

TANK 3 TIP TRAPPED ALERT IN ADDITION TANK 3 FUEL QUANTITY LOW ALERT.BOTH ALERTS WENT AWAY ON SHORT FINAL. REMOVED & REPACED 4K, 6K FLOAT SWITCH. PER AMM 28-43-01. CLOSED PANEL 633 AT IAW 28-00-00. OPS CHECK, LEAK CHECK GOOD.

Part: ATTACH BRACKET — CORRODED (RT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

RT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR 3 FROM FWD, FOUND LOWER FWD HOLE "BORE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

RIGHT WING - INBOARD FLAP ASSEMBLY INBOARD FLAP TRACK MOUNTED FITTING NR 3 FROM FORWARD, FOUND LOWER FORWARD HOLE "SPOT FACE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6- 2-100 REVISION 110.

Part: ATTACH FITTING — CORRODED (LT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

LT WING INBD FLAP ASSY INBD ACTUATOR LOWER ATTACHMENT FITTING FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140360, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: BRACKET — CORRODED (ZONE 600) · airframe 91,835 hrs · 28,910 cycles

RIGHT WING - INBOARD FLAP ASSY INBOARD FLAP TRACK MOUNTED FITTING NR 3 FROM FWD, FOUND UPPER FORWARD HOLE "SPOT FACE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6- 2-100 REVISION 110.

Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

RT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR3 FROM FWD, FOUND UPPER FWD HOLE, BORE CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: FITTING — CHAFED (ZONE 600) · airframe 91,835 hrs · 28,910 cycles

CHAFED - RT WING LOAD FITTING. REMOVED AND REPLACED AS PER AMM 20-50-02 REVISION 10.

Part: FITTING — CHAFED (ZONE 500) · airframe 91,835 hrs · 28,910 cycles

CHAFED - LT WING LOAD FITTING. REPAIR CARRIED OUT PER E.A. 8-5750-132416, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.

Part: LONGERON SPLICE — CRACKED (BS 1863 L45L) · airframe 91,835 hrs · 28,910 cycles

AFT CARGO COMPARTMENT - LONGERON 45 LT SPLICE FITTING AT STA 1863 FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II REVISION 96. NEW SPLICE FITTING FABRICATED PER DRAWING AFA3082 REVISION NC. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — DENTED (RT WING AILERON) · airframe 91,835 hrs · 28,910 cycles

DENTED LOWER SURFACE INBOARD EDGE OF RT INBOARD AILERON ASSY. DENT AREA MEASURED 0.008" TO 0.060" DEEP, FOUND ACCEPTABLE AS PER SRM 51-80-01 VOLUME II REVISION 96. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 06-10-01.001 ON DENT AREA AND FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: BULKHEAD — CRACKED (BS 1159) · airframe 91,835 hrs · 28,910 cycles

CTR ACCESORY COMPARTMENT AFT PRESSURE BULKHEAD AT STA 1159 "X" = 5 FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5730-140357, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 91,835 hrs · 28,910 cycles

RT WING - FUEL TANK ACCESS PANEL NR 634AT CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 8-5710-132418, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — SCRATCHED (NR 5 SLAT RT) · airframe 91,835 hrs · 28,910 cycles

RT WING - NR 5 SLAT ASSY LOWER SURFACE MID AREA FOUND SCRATCHED MARK. REPAIRED IAW EA 8-5740-132420, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

RT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) ACTUATOR ATTACHMENT LUG INBD SURFACE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140351, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: PANEL — DAMAGED (FUEL TANK) · airframe 91,835 hrs · 28,910 cycles

RT WING - FUEL TANK PANEL NR 631AT CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 8-5710-132418, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CHAFED (NR 8 SLAT RT) · airframe 91,835 hrs · 28,910 cycles

RT WING - NR8 SLAT ASSY OTBD LOWER EDGE FOUND TRIM OFF. REPAIRED AS PER SRM 57-00-01 VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 91,835 hrs · 28,910 cycles

RT WING - FUEL TANK ACCESS PANEL NR 638AB CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIRED IAW EA 8-5710-132419, REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 110.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 91,835 hrs · 28,910 cycles

CTR WING TANK FWD UPPER PANEL 01 EACH STIFFENER CRACKED AT STR 21, "X" =30. R & R IAW SRM 51-31-01, VOLUME II, REV 96. NEW STIFFINER FABRICATED IAW DWG NPB6072, REV AL. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100, REV 110.

Part: SKIN — CHAFED (NR 7 SLAT RT) · airframe 91,835 hrs · 28,910 cycles

RT WING - NR 7 SLAT ASSY LOWER MID SURFACE FOUND TRIM OFF. REPAIRED PER SRM 57-00-01 VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 91,835 hrs · 28,910 cycles

DURING HFEC OPEN HOLE INSP AT LT WING REAR SPAR LOWER CAP STA XORS = 345.75 INBD FWD FASTENER HOLE FOUND CRACKED INDICATION ON UPPER LAYER. R & R IAW SRM 51-33-01 VOL II, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

LT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) LOWER LUG INBD SIDE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140350, REPAIR CLASSIFIED MINOR PER GMM 6 -2-100 REVISION 110.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 91,835 hrs · 28,910 cycles

LT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) PIVOT POINT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT PER MD10 CMM 57-52-01 REVISION 50. NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-01 REVISION 50. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.

Part: WEB — CRACKED (CARGO DOOR) · airframe 91,835 hrs · 28,910 cycles

DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLE AT MAIN DECK CARGO DOOR FITTING NR 1, HOLE "C" FOUND CRACKED INDICATION ON FIRST LAYER OF WEB FROM TOP. REPAIR CARRIED OUT IAW EA NR8-5310-140345, REPAIR CLASSIFIED MAJOR GMM 6-2-100 REV 110.

Part: STIFFENER — CRACKED (CENTERWING) · airframe 91,835 hrs · 28,910 cycles

CTR WING TANK - FWD UPPER PANEL 01 EACH STIFFENER CRACKED AT STR 21 'X' = -30. R & R IAW SRM 51-31-01 VOL II REV 96. NEW STIFFINER FABRICATED IAW DWG NPB6072 REVISION AL. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 91,835 hrs · 28,910 cycles

MAIN DECK CARGO -STA 824, X =75 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 765 TO STA 835 LBL 75 IAW SRM 53-70-00 FIGURE 1, VOLUME I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SUPPORT FITTING — CHAFED (TE FLAP) · airframe 91,835 hrs · 28,910 cycles

LT WING - INBD FLAP INBD TRACK MOST FWD SUPPORT FITTING FOUND CHAFED. REPAIRED AS PER E.A. 1-5740-140356, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 110.

Part: SKIN — DAMAGED (TE FLAP) · airframe 91,835 hrs · 28,910 cycles

RT WING - INBD FLAP ASSY LOWER SURFACE FOUND MULTIPLE DENT AND SCRATCHES. REPAIRED SRM 57-10-00, FIG 3 VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAWGMM 6-2-100, REV 110.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 91,835 hrs · 28,910 cycles

MAIN DECK CARGO - FLOORBEAM FOUND CRACKED AT STA 1305, X = 107. REPAIRED IAW SRM 53-00-01 FIG 9, VOL I, REV 96 AND EA 8-5310-140346, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — SCRATCHED (NR 5 SLAT LT) · airframe 91,835 hrs · 28,910 cycles

LT WING - SLAT NR 5 LOWER SURFACE FOUND SCRATCHED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 31 VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: LONGERON — CORRODED (ZONE 100) · airframe 91,835 hrs · 28,910 cycles

AFT CARGO COMPARTMENT: STA 1853 TO STA 1871 LONGERON 45 LT, INBD SIDE FOUND CORROSION. REPAIRED IAW SRM 53-10-00, FIG 1, VOL I, REV 96. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: FITTING — CRACKED (ZONE 500) · airframe 91,835 hrs · 28,910 cycles

LT WING - INBD FLAP WELL, FLAP SIDE LOAD FITTING FOUND CRACKED. LT WING INBD FLAP WELL AREA FLAP ROLLER FITTING R & R IAW SRM 51-31-01 VOL II REV 96. NEW FLAP ROLLER FITTING FABRICATED IAW DWG ANB7394 REVISION AA. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: BEAM — CRACKED (L3 DOOR) · airframe 91,835 hrs · 28,910 cycles

MAIN DECK CARGO COMPARTMENT - LT 3 DOOR ASSY, BEAM NR 2 FROM LOWER FOUND CRACKED. CRACKED NR 2 BEAM AT MAIN DECK CARGO COMPARTMENT LT NR3 DOOR ASSY. REPAIRED IAW SRM 51-31-01, VOLUME II AND EA NR 8-5210-139247, REPAIR CLASSIFIED MAJOR GMM 6-2-100 REV 110.

Part: BEAM — CRACKED (R3 DOOR) · airframe 91,835 hrs · 28,910 cycles

MAIN DECK CARGO COMPARTMENT - RT 3 DOOR ASSY, BEAM NR 1 FROM UPPER FOUND CRACKED. CRACKED BEAM AT MAIN DECK CARGO COMPARTMENT RT NR3 DOOR ASSY, NR1 FROM UPPER R & R IAW SRM 51-31-01 VOL II, REV 110.

Part: SKIN — CRACKED (LT WING) · airframe 91,835 hrs · 28,910 cycles

LT WING - INBD ASSY UPPER SURFACE OTBD AREA FOUND CRACKED. REPAIRED IAW SRM 57-10-00 VOL I, REVISION 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: RIB — CRACKED (NR 2 SLAT LT) · airframe 91,835 hrs · 28,910 cycles

LT WING - NR 2 SLAT OTBD RIB FOUND CRACKED. R & R IAW SRM 51-31-01 VOLUME II. NEW RIB FABRICATED IAW DWG ARB1647, REV C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,835 hrs · 28,910 cycles

FUSELAGE - CTR ACCESSORY COMPARTMENT FWD PRESSURE BULKHEAD ANGLE FOUND CRACKED AT "X" = 0, "X" = -6, "X" = 6 AND "X" = 12. REPAIR CARRIED OUT IAW SRM 53-40-00 FIG 17 VOLUME I, REV 96 AND NR 8-5310-140362, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (LT WING) · airframe 91,835 hrs · 28,910 cycles

LT WING FIXED L/E TELESCOPIC DUCT CUT OUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR 8-5740-139241, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (A/C BAY DOOR) · airframe 91,835 hrs · 28,910 cycles

FUSELAGE - NR 2 AIR CONDITION BAY, DOOR FOUND CRACKED AT APPROX STA 515. REPAIRED IAW SRM 52-00-01. VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (RT WING) · airframe 91,835 hrs · 28,910 cycles

RT WING FIXED L/E TELESCOPIC DUCT CUT OUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5740-139241, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: WARNING LIGHT — FALSE ACTIVATION (LANDING GEAR) · airframe 89,757 hrs · 27,869 cycles

ON TAKEOFF KIND OBSERVED LEFT MAIN GEAR RED UNSAFE WITH GEAR HANDLE UP ON BOTH PRIMARY AND SECONDARY INDICATORS RAN QRH, CYCLED GEAR PER CHECKLIST AND GOT GEAR UP AND LOCKED BOTH INDICATORS. PSEU FAULT REVIEW SENSOR FAULT LEG 01 317075 INTERMITTENT LEFT GEAR UP AND LATCHED A/B SENSOR DISAGREE PROBABLE CAUSE SENSOR/TARGET RIGGING. RTS OF PSEU PASSES PER MM 31-71-01-2. PER ADJ/TST MM 32-61-15-5, FAR INDUCTANCE READINGS ARE WITHIN LIMITS FOR LGUPLCHA (4.718) AND LGUPLCHB (4.757). MORE T/S REQUIRED.

Part: THROTTLE CABLE — FAILED (NR 2 ENGINE) · airframe 88,223 hrs · 27,160 cycles

NR 2 THROTTLE STUCK AT HIGH POWER SETTING AT CRUISE ALTITUDE. ALL ATTEMPTS TO THAW LINKAGES WERE UNSUCCESSFUL. NR 2 ENGINE WAS SHUT DOWN ON APPROACH TO KMEM. AFTER LANDING THROTTLE OPERATED NORMALLY. REMOVED AND REPLACE NR 2 ENGINE THROTTLE CABLE AND THROTTLE DRUM BEARING PER MM 76-11-01-2. PERFORMED RIGGING OF NR 2 THROTTLE CABLE, REF. MM 76-11-01-2. OPS CHECK GOOD. OK FOR SERVICE

Part: COMPUTER — MALFUNCTIONED (FLT CONTROL) · airframe 87,229 hrs · 26,712 cycles

ON APPROACH TO PDX, RECEIVED LVL 2 SLAT DISAG WHEN SELECTING 35 FLAPS. EXECUTED GO-AROUND AND RAN SLAT DISAG CHECKLIST IN QRH. LANDED WITH FLAPS 22/EXTEND. ON CHECK OPERATION OF SLATS PER MAINTENANCE MANUAL 27-84-00-5. SLAT OPERATES NORMAL. FOUND FCC'S FAULTED AND AOA FAULTED. REMOVED AND REPLACED RT AOA SENSOR AND OPS CHECK PER MAINTENANCE MANUAL 22-00-05-5. REMOVED AND REPLACED NR 1 FCC AND PERFORMED RTS AND AFS TEST PER MAINTENANCE MANUAL 22-00-00-5. TEST PASS.

Part: BULB — INOPERATIVE (NLG INDICATOR) · airframe 83,432 hrs · 25,025 cycles

PER FLIGHT CREW DEBRIEF (EMP 66912). ON INITIAL GEAR EXTENSION, DID NOT GET GREEN LIGHT FOR NLG ON THE PRIMARY LANGING GEAR INDICATION. CHANGED THE BULBS FOR THE NLG GREEN IND. THEN GOT THE NLG GREEN INDICATION, AND HAD A NORMAL LANDING. PERFORMED FUNCTIONAL TEST IAW MM 31-12-04-2 PAR 5. OPS CHECK NORMAL AT THIS TIME. DUE TO FLIGHT CREW REMOVED AND REPLACED BULBS OF THE PRIMARY NOSE LANDING GEAR IND.

Part: CONTROL VALVE — MALFUNCTIONED (TE FLAPS) · airframe 83,039 hrs · 24,851 cycles

AFTER TAKEOFF, DURING FLAP RETRACTION LEVEL 2 FLAP DISAGREE ALERT. O/B FLAPS SHOWED 5 AND 6 INBOARD FLAPS WERE AT 0. PER QRH ATTEMPTED TO RETURN FLAPS TO LAST POS THAT ALERT WAS NOT DISPLAYED. AT 12 O/B FLAPS STAYED AT 5 AND 6. DURING RETURN TO KMEM O/B FLAPS STAYED AT 5 AND 6 WHEN 22 FLAPS SELECTED. AT SOME POINT DURING SLOW DOWN O/B FLAPS EXT TO 22. NORMAL LANDING WAS MADE WITH FLAPS 50. REMOVED AND REPLACED THE RIGHT O/B AND THE LEFT O/B FLAP CONTROL VALVES PER MM 27-52-02-2. REMOVED AND REPLACED ALL RESTRICTORS AND CHECK VALVES. CONNECTED AND SAFTIED CONTROL RODS. LEAK CHECKED VALVES AND OPS CHECKED THE FLAP SYSTEM AS WELL AS FLAP IND SYSTEM. OPS CHECKS AND LEAK CHECKS GOOD.

Part: ENGINE — STALLED (NR 3) · airframe 81,533 hrs · 24,161 cycles

AT FL330, SELECTED ENGINE AND WING ANTI-ICE ON, ENGINE 3 ANTI-ICE DISAGREE AND COMPRESSOR STALL AT SAME TIME. N1 ROLLED BACK TO 67 PERCENT. RAN COMPRESSOR STALL CHECKLIST. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN APPROXIMATELY 1+05 FLIGHT TIME REMAINING (WINDMILLING).

Part: CONTROL VALVE — MALFUNCTIONED (TE FLAPS) · airframe 80,691 hrs · 23,778 cycles

DURING FLAP RETRACTION AFTER TAKEOFF GOT FLAP DISAGREE ALERT. INBOARD FLAPS DID NOT RETRACT, STAYED AT 11; OUTBOARD LEFT INDICATED 5 AND OUTBOARD RIGHT INDICATED 6. QRH PROCEDURE ACCOMPLISHED. NOTE: TAKEOFF FLAP SETTING WAS 10.9. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE AS PER MM 27-52-02-2. CYCLED FLAPS SEVERAL TIMES AND OPERATIONAL CHECK IS NORMAL. LEAK CHECK IS SATISFACTORY. SERVICED HYDRAULIC FLUID AS PER MM 12-13-02-3.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 81,335 hrs · 24,068 cycles

HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-70174 (REF FEDEX NRC N1048) PANELS REPLACED: ALC7204-1, ALC7205-1, ALC7207-1, ALC7208-1.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 81,294 hrs · 24,050 cycles

HORIZONTAL STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF FEDEX NRC N1102) *S/D COMING*

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 81,294 hrs · 24,050 cycles

HORIZ STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF NRC N1102)