N319FE

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 101,889 hrs · 30,798 cycles

RIGHT OUTBOARD FLAP UPPER SIDE INBOARD OF FLAP ATTACH POINT HAS A GOUGE (MWT). C/W EA 8-5750-TO356663 AND N/R N00012, W/O 78394.

Part: MEC — MALFUNCTIONED (ENGINE) · airframe 101,759 hrs · 30,729 cycles

HAD A MAX TAKE OFF POWER SETTING DUE TO AN ANTI SKID MEL. TAKE OFF POWER APPROX 113 N1. APPROACHING 120 KTS, FELT THE AIRCRAFT YAW TO THE RIGHT AND RECEIVED A RED ENGINE FAIL ANNUNCIATION ON THE GLARESHIELD. IMMEDIATLY REJECTED THE TAKEOFF. ONCE CLEAR OF THE RUNWAY ALL ENGINE INDICATIONS APPEARED NORMAL. C/W MTSI. FUEL PUMP R & R C/W. MEC R & R C/W. SEE WRI S 73-12/8150 & 73-20/8151 FOR ALL MX, PARTS & RII DETAILS.

Part: BATTERY — FAILED (MASTER) · airframe 101,729 hrs · 30,711 cycles

HUB REPORTED SMOKE COMING FROM BENEATH AIRCRAFT UPON ARRIVAL DISCOVERED SMOKE COMING FROM BATTERY VENT PORTS. REMOVED AND REPLACED POSITION 1(P/N 31433-001 S/N 10201305) AND POSITION 2 BATTERIES IAW AMM 24-34-01-2. OPS CHECK GOOD OK FOR SERVICE.

Part: BATTERY — SMOKE (MASTER) · airframe 101,729 hrs · 30,711 cycles

HUB REPORTED SMOKE COMING FROM BENEATH AIRCRAFT. UPON ARRIVAL DISCOVERED SMOKE COMING FROM BATTERY VENT PORTS. REMOVED AND REPLACED POSITION 1 AND POSITION 2 BATTERIES IAW AMM 24-34-01-2. OPS CHECK GOOD OK FOR SERVICE.

Part: WEB — CRACKED (NLG WW) · airframe 101,502 hrs · 30,598 cycles

NOSE LANDING GEAR LS WHEEL WELL RS WEB AT STA 485 HAS 4" CRACK. PERM CRACK REPAIRED USING VOL 1 FIG B AS A REFERENCE.

Part: SKIN — DENTED (BS 1581 L49R) · airframe 101,502 hrs · 30,598 cycles

FUSELAGE SKIN AT STA 1581, STRINGER 49R HAS DENT DAMAGE. REPAIRED FUSELAGE SKIN (DOUBLER REPAIR) USING SRM 53-20-00 AS A REFERENCE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 100,604 hrs · 30,106 cycles

INTERMITTANT AIRSYSTEM ODOR INFLIGHT W/PACK 1 MELED INOP & PACKS 2 & 3 ON. PACK OUTLET TEMPS #2=33F,#3=133F. COCKPIT TRIM AIR VALVE=110, ODOR NOT NOTICABLE WHEN PACK #2 TEMP IS BELOW 0F,COCKPIT TRIM AIR VALVE BELOW 70 F. INSPECTED AIR CONDITIONING EXIT DOORS FOR OIL LEAK, NO OIL EVIDENT. CLEANED AIR CONDITIONING PACKS AND DUCTS AND REMOVED AND REPLACED #2 AND #3 PACK WATER SEPERATOR COALESCER BAGS. NO SMELL NOTICED WHILE RUNNING PACKS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 99,979 hrs · 29,757 cycles

#1 AND #3 MANF FAIL OVERHEAD LIGHT ILLUMINATED DECENDING THROUGH FL260. SYSTEM CLOSED BLEEDS 1 AND 3 CAUSING AIR SYS 1 AND 3 OFF. CABIN INFO LO ALERT ALSO DISPLAYED. COMPLIED WITH QRH PERFORMED TROUBLE SHOOTING IN REF. TO FIM 36-23-00-2. NO FAULTS ON MANIFOLD FAULT BALL INDICATOR. PERFORMED DECAY CHECKS SEVRAL TIMES ON SYS 1 AND 3 IN REF. TO AMM 36-00-01-5. ALL CHECKS PASSED. NO FAULTS NOTED. REMOVED AND REPLACED MANIFOLD FAILURE DETECTION CONTROLLER PRECAUTIONARY AND PERFORMED R-T-S IN REF TO AMM 32-23-01-5 AND 36-23-01-4. MPN 35008-2. S/N B695 REMOVED. INSTALLED S/N A195. AIRCRAFT OK FOR SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

AFT T-CORD COMT ACCESS DOOR FRAME STA 475 MILD SURFACE CORROSION FORMING ON T-CORD 10 IN BELOW DOOR. REMOVED MILD SURFACE AND REPAIR AREA REF E.A. T8-5310-T0345485.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO COMPT. RIGHT HAND FLOOR SUPPORT AT STATION 1661, RBL=-72.25 TO RBL=-104.00 SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SP10510130-567 PER DAC DWG WSP0711 AND PER SRM 51-33-01 VOL. 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO COMPT. LEFT HAND SIDE FLOOR SUPPORT AEA0394-503 AT STATION 1219, LBL=72.25 TO LBL=86.25 SHOWS CORROSION. REMOVED CORRODED FLOOR SUPPORT AEA0394-503 AT STATION 1219, LBL=72.25 TO LBL=86.25. MAIN CARGO COMPARTMENT LT AND REPLACED IN ACCORDANCE WITH REF. NEA6018 DAC DWG AND SRM 51-31-01 VOL. 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

NR 1 ACM EXHAUST DOOR CUT OUT LOWER AFT CORNER-CRACK EMANATING FROM FASTENER HOLE TO CUT-OUT. CONFIRMED CONDITION USING NDT HFEC. AREA IS MARKED. REPAIRED NR 1 ACM EXHAUST CUT OUT LOWER AFT CORNER AS REQ. REF. SRM 53-50-00 FIG 3A, SHT 1. PARA. 4A B (3). MAJOR REPAIR

Part: SKIN — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

LT SIDE FUSELAGE STA 1997 -2007 STRINGER 10L CORROSION FOUND APROX 10 INCHES. (ABOVE FIX FAIRING PANEL AJC7837-71) AREA IS MRKD. REPAIRED IAW EA 8-5330-T0345607.

Part: SKIN — CRACKED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

LT FUSELAGE SKIN AT NR 1 PACK DOOR CUT OUT UPPER AFT CORNER HAS A .100 CRACK PROPAGATING OUT OF A FASTENER HOLE. REPAIRED AREA PER SRM 53-50-00 FIG 3A SH1 VOL 1. MAJOR REPAIR.

Part: SPOILER — DELAMINATED (RT WING) · airframe 99,799 hrs · 29,669 cycles

RT WING NR 4 SPOILER TOP SURFACE HAS DELAMINATION APPROX (16" X 21"). REPAIR NR 4 SPOILER IAW SRM 51-71-00 VOL II.

Part: FLOORBEAM — CORRODED (BS 1281.5) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO DECK, STA 1281.5, RBL 47.125 TO LBL 47.125, FLOOR BOARD SUPPORT HAS COROSSION/EXFOLIATION PRIMARILY CLIP NUT HOLES. REPLACED DAMAGED FLOOR SUPPORT (FX AEA0187-9) AT STA 1281.5 RBL 47.125 TO LBL 47.125 REF SRM 51-31-01 VOL 2 & DWG AEA 0187

Part: BOLT — SHEARED (L1 DOOR) · airframe 99,799 hrs · 29,669 cycles

UPON INSPECTION OF L1 DOOR FREEFALL OPERATIONAL/FUNCTIONAL CHECK DOOR FAILED TO FALL. AFTER FURTHER INSPECTION FOUND SHEARED BOLTS IN THE FORWARD SEGMENT OF THE MAIN DRIVE TORQUE TUBE. REPAIRED PER AMM AND PERFORMED NDT ON TORQUE TUBE SEGMENT, INSTALLED NEW BOLTS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO AT APPROX STA 1361 LBL 75 - 105 AFTER REMOVING TAPE AND NUT PLATES FOUND UNDER SIDE OF FLOOR SUPPORT HAS EXFOLIATION CORROSION. FABRICATED AND PROCESSED NEW FLOOR SUPPORT REF DRAWING AEA0394. P/N S2929169T AND SRM REF 51-31-01VOL2. TREATED FLOOR SUPPORT REF SRM 51-21-01V2. INSTALLED NEW FLOOR SUPPORT REF DWG AEA0394 AND SRM 51-31-01VOL2.

Part: FLOORBEAM — CORRODED (BS 1561) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO DECK, STA 1561, BETWEEN RBL = 76 TO RBL = 100, FLOOR BOARD SUPPORT LAND CORROSION AROUND SCREW HOLES REMOVED AND REPLACED FLOORBOARD SUPPORT AT MAIN CARGO DECK STA-1561, BETWEEN RBL=76 TO RBL=100, REF DOUGLAS DRWG NFA6398 AND SRM-51-33-01, VOL-II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO AT APPROX STA 1300 LBL 75 - 105 AFTER REMOVING TAPE AND NUT PLATES FOUND UNDER SIDE OF FLOOR SUPPORT HAS EXFOLIATION CORROSION. FABRICATED AND PROCESSED NEW FLOOR SUPPORT REF DWG AEA0412 (P/N S2929169) AND SRM 51-31-01 VOL II. TREATED FLOOR SUPPORT AND REG SRM 51-21-01 VOL II. INSTALLED NEW FLOOR SUPPORT REF DWG AEA0412 AND SRM 51-33-01 VOL II.

Part: FLOORBEAM — CORRODED (BS 1561) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO DECK, STA 1561, APPROX RBL=60, FLOOR BOARD SUPPORT HAS EXFOLIATING COROSSION. REMOVED AND REPLACED FLOORBOARD SUPPORT AT MAIN CARGO DECK STA-1561, APPROX RBL=60, REF DOUGLAS DRWG NFA6398 AND SRM-51-33-01, VOL-II.

Part: FLOORBEAM — CORRODED (BS 1481) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO AT APPROX STA 1481 LBL75 - 105 AFTER REMOVING MYLAR TAPE AND NUT PLATES FOUND UNDER SIDE OF FLOOR SUPPORT HAS EXFOLIATION CORROSION MARKED #19 REMOVED AND REPLACED FLOOR SUPPORT, MAIN CARGO, STA 1481 LBL 75-105 IAW REF DAC DWG AEA0364, SRM 51-35-01 VOL 2, SRM 51-33-01, SRM 51-21-01 VOL. 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO DECK, STA 14-1, APPROX RBL = 20, CORROSION ON FLOORBOARD SUPPORT PANEL LAND. FABRICATED AND PROCESSED NEW FLOOR SUPPORT REF DWG AEA0397-1 P/N S2929169T AND SRM 51-31-01 VOL II. TREATED FLOOR SUPPORT REF SRM 51-21-01 VOL II. INSTALLED NEW FLOOR SUPPORT REF DWG AEA0397 AND SRM 51-33-01 VOL II.

Part: SPAR WEB — CRACKED (NR 1 PYLON) · airframe 99,799 hrs · 29,669 cycles

NR 1 PYLON UPPER SPAR WEB, NEAR STA YN220, LT SIDE, JUST FWD OF LT REVERSER FWD HINGE ATTACHMENT, WEB IS CRACKED AT FASTENER HOLE. (MKD) REPAIRED CRACKED WEB REF. SRM54-20-00 FIG.5 VOL.I.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO COMPARTMENT - SEAT TRACK AT STA 640, LBL 108, HAS A CRACK APPROXIMATELY 2" LONG. (MARKED) REPLACED DAMAGED SEAT TRACK AT STA-640, LBL-108 REF SRM-53-70-00, FIG-1, VOL-1.

Part: FLOORBEAM — CORRODED (BS 1229) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK APPROX STA 1229 LBL 75 FLOOR SUPPORT HAS EXFOLIATION CORROSION MARKED #9 MAIN DECK STATION 1229 LBL75 REMOVED AND REPLACED FLOOR SUPPORT IAW REF DAC DRWG AEA0410, SRM 53-00-01 VOL 1, SRM 51-31-01 VOL 2 & SRM 51-21-01 VOL. 2

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK AT STA 1481 RBL 76 THRU RBL 106 FLOOR SUPPORT BEAM CORRODED UNDER NUT PLATES (MARKED). REMOVED AND REPLACED FLOOR SUPPORT ON MAIN DECK @ STA 1481, RBL-76 THRU RBL- 106; REF DRWG NEA6018 AND MD-10-SRM-51-22-01, VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK AT STA 1361 RBL76 THRU RBL106 FLOOR SUPPORT "I" BEAM CORRODED UNDER NUT PLATES. REMOVED AND REPLACED CORRODED FLOOR SUPPORT AEA0394 PER SRM 51-35-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK AT STA 1301 RBL76 THRU RBL106 FLOOR SUPPORT "I" BEAM CORRODED UNDER NUT PLATES. FABRICATED AND PROSSED NEW FLOOR SUPPORT REF DWG.AEA0419 P/N 52929169T AND SRM51-31-01 VOL II. TREATED FLOOR SUPPORT REF SRM 51-21-01 VOL II. INSTALLED NEW FLOOR SUPPORT REF DWG AEA0419 AND SRM 51-33-01 VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK: RBL 56 NEAR STA 1900, SEAT TRACK HAS EXFOLIATED CORROSION ON THE BOTTOM SIDE. VIEWED FROM AFT CAGO PIT. MARKED INSTALLED FLOOR SUPPORT REF SRM 51-31-01 VOL 2 AND PER DWG # AFA7544.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK: LBL 47, APPROX STA 635, SEAT TRACK LOBE BROKEN/WORN BEYOND LIMITS. REMOVED & REPLACED EXISTING SEAT TRACK SPLICE PER SRM 53-70-00 VOL I FIG 1A PG7, 51- 31-01 VOL II & DWG SR10-53-002.

Part: SEAT TRACK — CORRODED (BS 1275) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK: RBL 27.50 NEAR STA 1275, SEAT TRACK WORN MARKED RED/DOT 12 REPLACED DAMAGED SEAT TRACK FROM STA 1247 TO STA 1312 RBL 27.50 REF SRM 53-70-00 FIG 1 VOL1 & DWG SR10-53-002 & SRM51-31-01 VOL 2 & SEALED PER SRM 51-41-01 VOL 2

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO COMPT, APPROX STA 1129 X= -47.50, SEAT TRACK SECTION GOUGED. REMOVED AND REPLACED SEAT TRACK AT STA 1129 X=47.50 PER SRM 53-70-00 FIG 1 VOL 1 AND DRAWING SR10-53-002 AND SRM 51-31-01 VOL II AND SRM 51-41-01 VOL II.

Part: SKIN — CRACKED (TE FLAP) · airframe 99,799 hrs · 29,669 cycles

LT WING O/B FLAP UPPER SURFACE I/B END. FLAP ENVELOPE 2ND FROM I/B. VISUAL INDICATION OF 10 INCH SKIN CRACK FORMING ON RIB. REPAIRED CRACKED ON THE UPPER SURFACE OF THE LT OUTB FLAP SKIN REF SRM 57-00-01, FIG. 4, SHEET 2, PAGE 12 VOL. 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK LBL 107.25 NEAR STA 1360, SEAT TRACK WORN. CUTOUT DAMAGED AREA, LOCATED & INSTALLED PLUG CHANNEL PER SRM 53-70-00 FIG 02 PG09.

Part: SEAT TRACK — WORN (BS 1731-1741) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK SEAT TRACK: STA. 1731-1741 LBL = 75.25 - WORN. REMOVED & REPLACED SEAT TRACK AT STA 1731 -1741 LBL 75.25 PER SRM 53-70-00 FIG 1 VOL1& FEDEX DRWG SR10-53-002 & SRM51-31-01 VOL2 & SRM 51-41-01 VOL 2

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK SEAT TRACK STA 1581 LBL= 75.25, HAS LIGHT WEAR. REPAIRED AREA AT STA. 1581 LBL 75.25 WITH PLUG AND CHANNEL SPLICE IAW REF SRM 53-70-00 VOL I, FIGURE 2, SHEET 2, PAGE 10, DWG SR 10-53-501, SRM 51-21-01 VOL II.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK: RBL 47.50 NEAR STA 1280, SEAT TRACKS DAMAGED. REPLACED DAMAGED SEAT TRACK ON EXISTING REPAIR REF SRM 53-70-00 VOL I PG 3.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK LBL 75.25 NEAR STA 1265, SEAT TRACK WORN. REPLACED DAMAGED SEAT TRACK FROM STA 1265 TO 1285 REF SRM 53-70-00 FIG 1 VOL 1 & SRM 51-31-01 VOL 2 & SR10053-002 DWG AT LBL 75.25.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN DECK: RBL 47.50 NEAR STA 1397, SEAT TRACK WORN. REPLACED DAMAGED SEAT TRACK FROM STA1397 TO STA1460 RBL47.50 PER SRM 53-70-00 FIG01 VOL I, DWG SR10-53-002.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 99,799 hrs · 29,669 cycles

MAIN CARGO COMPT, APPROX STA 1019 X= -47.50 , SEAT TRACK WORN BEYOND LIMITS. REMOVED REPLACED SEAT TRACK AT STA1019 X=47.50 PER SRM 53-70-00 FIG 1 VOL 1 DWG SR10-53-002 & SRM 51-31-01 VOL II & SRM 51-41-01 VOL II.

Part: DOUBLER — CRACKED (RT WING) · airframe 99,799 hrs · 29,669 cycles

RT WING LE INNER BEADED DOUBLER HAS 1" CRACKED - APPROX XORS 911 - INBD OF NR 16 SLAT TRACK. CRACK CONFIRMED USING NDT HFEC. REPAIRED PER SRM CH 57-10-00, FIG 71, VOL1.

Part: SKIN — CRACKED (LT WING) · airframe 99,799 hrs · 29,669 cycles

LT WING LEADING EDGE SKIN HAS A .500 IN. CRACK AT THE INBOARD AFT CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT. (END MARKED) CUT OUT DAMAGED AREA, INSTALLED FILLER & DOUBLER PER SRM 57-10-00 FIG103 SHT02.

Part: DOUBLER — CRACKED (RT WING) · airframe 99,799 hrs · 29,669 cycles

RT WING LE INNER BEADED DOUBLER HAS 1" CRACKED - APPROX XORS 567 - OUTBD OF NR 10 SLAT TRACK. CRACK CONFIRMED USING NDT HFEC. INSTALLED REPAIR DOUBLER REF SRM CH 57-10-00, VOL 1, FIG 71.

Part: VALVE — FAILED (ZONE 500) · airframe 99,688 hrs · 29,606 cycles

PDIS 319 36-10 6510 22DEC18 MEM FACT U LOGPAGES:3043404 "AIR MANIFOLD 1 FAIL" ALERT LEVEL 3 IN FLIGHT AT FL370. COMPLIED WITH QRH , DECLARED EMERGENCY, LANDED KMEM. AIR MANIFOLD PRESSURE NEVER GOT BELOW 13 PSI RAR #1 MANIFOLD FAIL RELAY R2-5256, #1 AUTO S/O RELAY R2-5016, MANIFOLD FAIL RELAY R2-8962 REF MD10 AMM 24-00-00-2. OPS CHECK GOOD REF MD10 AMM 36-23-00-5. FOUND #1 ENGINE PRV NOT FULLY CLOSED AND DRAGS THRU OPENING AND CLOSING RAR #1 ENIGINE PRV REF MD10 AMM 36-10-00-2 OPS CHECK GOOD. PRESSURIZED #1 PNEUMATIC SYS CHECKED FOR LEAKS AND LOOSE SENSE LINES NO DEFECTS NOTED REF MD10 AMM 36-10-00. RAR #3 AIU IAW MD10 AMM 31-43-02-04 OPS CHECK GOOD. REF WRI 36-22/6512, 6513, 6514, 6515, 6516, AND MTSI 36-22-6511 FOR OTHER WORKED PERFORMED AND PARTS INFO.

Part: CONTROLLER — FAILED · airframe 99,623 hrs · 29,568 cycles

ON DESCENT RECEIVED LBL 1 AIR SYS 1 OFF, FOLLOWED BY LVL 2 AIR MANIFOLD 1 FAIL. REF FIM 36-23-00-810-803 AND 36-23-00-810-801. NOT:; CREW REPORTED THAT WING ANTI ICE WAS NOT IN USE AT TIME OF FAULT OCCURRENCE. FOUND LH WING ANTI-ICE PRESS SW. WAS FAULTED ON MAMIFOLD FAULT BOX IN CAC. RESET FAULT BALL. R&I LH WING DP SWITCH PER MM 36-23-03-4. PERFORMED LEAK CK AND OPS CKS OK. PERFORMED #1 PNEUMATIC PRESSURE DECAY TEST PER MM 36-00-01-5. TEST PASSED. PERFORMED AIR SYSTEM TEST PER MM 36-23-01-5. TEST PASSED. DUE HISTORY REPLACED MANIFOLD FAIL CONTROLLER PER MM 36-23-01-4. PERFORMED CONTROLLER TEST PER MM 36-23-01-5. TEST PASSED. A/C OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 99,358 hrs · 29,412 cycles

EMER LT BAT 1 LO ALERT. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY. OPERATIONAL CHECK NORMAL.

Part: ENGINE — SMOKE (COCKPIT) · airframe 99,114 hrs · 29,291 cycles

AT FL 360 AND WITH NORMAL CRUISE POWER SET WE NOTICED SMOKE FILLING THE COCKPIT. NO INDICATIONS WERE NOTICED. ALL 3 BLEEDS WERE ON AND PACKS NR 1 & NR 3 WERE ON. WE RAN THE QRH AND DECLARED EMERGENCY LANDED RWY KMEM AND AN EMERGENCY GROUND EGRESS WAS PERFORMED. REPLACED THE ENGINE, OPS AND LEAK CHECKED GOOD. ENGINE: GE- CF650C2 SER: 530397 TT: 51256 TC: 18201

Part: SLIDE — DETACHED (L1 DOOR) · airframe 98,812 hrs · 29,122 cycles

L1 DOOR EMERGENY SLIDE FELL ONTO CREW STRAIRS REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMM 25-61-02-4.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 98,747 hrs · 29,084 cycles

CARGO DOOR, FWD RIGHT WARNING ILLUMINATED IN FLIGHT, EXTINGUISHED 16,000 FT. OPS CHECKED THE FWD CARGO DOOR SEVERAL TIMES. DID NOT NOTICE ANY ABNORMALITIES IN THE DOOR WARNING SYSTEM. ALL OPS CHECKED GOOD IAW AMM 52-70-03-2.

Part: INTERLOCK — MALFUNCTIONED (MLG) · airframe 98,251 hrs · 28,824 cycles

GEAR HANDLE WOULD NOT MOVE TO UP POSITION. COMPLIED WITH QRH AND GEAR STILL WOULD NOT RETRACT. CONTINUED TO DESINATION WITH GEAR DOWN. TROUBLESHOT AND FOUND THAT INTERLOCK CRANK IN THE RT MLG WW WAS NOT PULLING CLEAR OF INPUT ROD. BLED RT TRIM CYLINDER AND FUSE IAW MM 32-37-01-2. PERFORMED EXTENSION & RETRACTION SEVERAL TIMES IAW MM 32-30-00-5. OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (STAB TRIM) · airframe 97,765 hrs · 28,568 cycles

STAB OUT OF TRIM LIGHT ILLUMINATED AT 10,000 FT. PERFORMED A LEAK AND OPS CHECK THE STAB MOTOR AND BRAKES. LEAK AND OPS CHECKED GOOD IAW AMM 27-43-01-2. NO DEFECTS NOTED. PERFORMED AN OPS CHECK OF THE STAB DRIVE GEARBOX IAW AMM 27-44-03-2. CHECKED GOOD. OPS CHECKED THE STAB. DRIVE UNIT IAW AMM 27-44-05-2. NO DEFECTS NOTED.

Part: BAR — DETACHED (R1 DOOR) · airframe 97,339 hrs · 28,354 cycles

BAR ON R1 DOOR DETACHED. ATTACHED MANUAL LIFT BAR ON R1 DOOR IAW MM 25-61-02-5. OK FOR SERVICE.

Part: SCHRADER VALVE — LOOSE (L1 DOOR) · airframe 97,215 hrs · 28,294 cycles

CABIN DOOR L1 PRESSURE GAUGE READS O PSI. FOUND SCHRADER VALVE LOOSE, SERVICED L1 DOOR AIR RESERVOIR AS REQUIRED, REF AMM 52-11-07-2, NO LEAK'S NOTED, A/C OK FOR CONTINUE SERVICE.

Part: SCHRADER VALVE — LOOSE (L1 DOOR) · airframe 97,215 hrs · 28,294 cycles

CABIN DOOR L1 PRESSURE GAUGE READS O PSI. FOUND SCHRADER VALVE LOOSE, SERVICED L1 DOOR AIR RESERVOIR AS REQUIRED, REF AMM 52-11-07-2, NO LEAK'S NOTED, A/C OK FOR CONTINUE SERVICE.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 97,160 hrs · 28,266 cycles

NOSE GEAR WHEEL WELL, LT VERTICAL BULKHEAD AT FWD UPPER END ADJACENT AN UNDERNEATH MAIN CARGO DOOR RESERVOIR HYDRAULIC LINES. APPROX TWO INCH CRACK ON BULKHEAD. REPAIRED THE LT VERTICAL BULKHEAD IN REF TO SRM 53-30-00 FIG 6 SHEET 3 VOL 1.

Part: FLOOR SUPPORT — CORRODED (BS 1321) · airframe 97,160 hrs · 28,266 cycles

MAIN DECK BS 1321, RBL 21, FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-31-01.

Part: SUPPORT BRACKET — CRACKED (LT W FUEL DOOR) · airframe 97,160 hrs · 28,266 cycles

LT WING FIXED L/E FUELING STATION DOOR AFT OTBD CORNER OF DOOR SUPPORT BRACKET CRACKED. REPAIRED IAW SRM 57-00-01 FIG. 10 SHT. 1 PAGES 29-32. VOL. 1

Part: SKIN — CORRODED (RT AILERON) · airframe 97,160 hrs · 28,266 cycles

RIGHT WING OTBD AILERON LOWER SKIN, XOA 991. SKIN IS BULGING WITH AREAS OF CORROSION. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 51-211-01, PAGE 12, REMOVED AND REPLACED THE AILERON IAW MM 27-10-02-4.

Part: FLOOR SUPPORT — CORRODED (BS 1501) · airframe 97,160 hrs · 28,266 cycles

MAIN CABIN BS 1501, LBL 20 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AEA0397, AND SRM 51-31-01, V2.

Part: DOUBLER — CRACKED (NR 3 PYLON) · airframe 97,160 hrs · 28,266 cycles

NR 3 PYLON UPPER WEB AT YN338, FEED THROUGH HOLE FOR GENERATOR LEAD INSULATOR BOOT, ATTACH FLANGE IS CRACKED AT OTBD SCREW HOLE. REMOVED AND REPLACED DOUBLER IAW SRM 51-31-01,V2. AND DWG AUB 7031.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 97,160 hrs · 28,266 cycles

LEFT INBD FLAP UPPER SKIN HAS THREE CRACKS AT RIVET ROW XIFH 231. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1..

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 97,160 hrs · 28,266 cycles

LEFT INBD FLAP UPPER SKIN HAS TWO CRACKS AT RIVET ROW XIFH 225. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1.

Part: SKIN — CRACKED (TE FLAP) · airframe 97,160 hrs · 28,266 cycles

LEFT INBD FLAP UPPER SKIN HAS TWO CRACKS AT RIVET ROW XIFH 165. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1.

Part: FRAME — CRACKED (LT WING) · airframe 97,160 hrs · 28,266 cycles

LEFT WING FIX LE, XORS 893 FORMER/FRAME IS CRACKED. REPAIRED THE FRAME IAW SRM 57-00-01, FIG 1, SHT 1, VOL 1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 97,160 hrs · 28,266 cycles

LEFT INBD FLAP UPPER SKIN HAD ONE CRACK AT RIVET ROW XIFH 159. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL.1.

Part: RUB STRIP — DEBONDED (TE FLAP VANE) · airframe 97,160 hrs · 28,266 cycles

RIGHT OUTBOARD FLAP VANE, FOUND FROM OUTBOARD SECOND RUB STRIP IS DISBONDED AND DELAMINATED. REPAIRED IAW SRM 51-71-00.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 97,160 hrs · 28,266 cycles

[MAIN CABIN, BS 655, SEAT TRACK IS WORN. REMOVED AND REPLACED THE SEAT TRACK, IAW SRM 53-70- 00 FIG 1A VOL 1, AND SRM 53-70-00 00 FIG 1A VOL 1.

Part: SEAT TRACK — WORN (BS 1099) · airframe 97,160 hrs · 28,266 cycles

MAIN DECK, NEAR BS 1099, LBL 8.5 SEAT TRACK WORN. FOUND TO BE WITHIN LIMITS AFTER BLEND OUT.

Part: SEAT TRACK — DAMAGED (BS 1650) · airframe 97,160 hrs · 28,266 cycles

MAIN CABIN BS 1650, LBL 12 SEAT TRACK LOBE OBLONGED. SEAT TRACK FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00, FIG 5.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 97,160 hrs · 28,266 cycles

MAIN CABIN BS 1290, RBL 24 SEAT TRACK LOBES ARE OBLONGED AND WORN. SEAT TRACK FOUND TO BE WITHIN LIMITS AFTER BLEND OUT IAW SRM 53-70-00, FIG 5.

Part: SEAT TRACK — DAMAGED (BS 1240-1260) · airframe 97,160 hrs · 28,266 cycles

BS 1240 - 1260, RBL 72, SEAT TRACK LOBES DAMAGED. REMOVED AND REPLACED SMALL SECTION OF SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 96,652 hrs · 28,027 cycles

DURING "EMER LT" TEST RECEIVED LEVEL 1 ALERT EMER LT BAT 1 LO. R&R EMERG EXIT LIGHTS BAT POWER SUPPLY IN REF TO AMM 35-51-01-4. OPS CHECK GOOD. A/C GOOD FOR SERVICE.

Part: CONTROL CABLE — OBSTRUCTED (COCKPIT) · airframe 96,180 hrs · 27,811 cycles

FLAPS WOULD NOT EXTEND, DIAL-O-FLAP WHEEL VERY DIFFICULT TO MOVE. OPENED RT SIDE PEDESTAL ACCESS PANEL FOR FLAP, FOUND FOD, FLIGHT DECK TRASH BAG JAMMING CABLES AND CONTROLS. REMOVED DEBRIS, REINSTALLED RT ACCESS PANEL, ACCOMPLISHED FLAP AND SLAT, AND DIAL A FLAP OPS CHECKS, REF AMM 27-50-00-5. WILL PERFORM DETAILED INSPECTION OF AVIONICS BAY AND UNDER PEDESTAL AREA NEXT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,038 hrs · 27,336 cycles

FI CARGO DISCHARGE FLASHING. MX IMMEDIATELY CHECKED CARGO, NO INDICATION FIRE. DISCHARGE SWITCH NOT PUSHED DUE IMMEDIATE INSPECTION MX. PULLED & RESET MISC CB IAW MM 31-42-01-5. OPERATIONS CHECKED OK. ALSO INSPECTED FWD CARGO LOWER BAY. NO EVIDENCE OF SMOKE. OK FOR SERVICE.

Part: SWITCH — DIRTY (CALL BELL) · airframe 948 hrs · 27,226 cycles

AFTER TAKEOFF MECH CALL BELL SOUNDED, RANDOMLY NUMEROUS TIMES, NO LESS THAN 100 TIMES, PLUS AUDIO PANEL MECH LIGHT ILLUMINATED. SWITCH S1-240 FOUND STICKY, CLEANED SWITCH. OPS CHECKED GOOD.

Part: CONTROL MODULE — DIRTY (TE FLAP) · airframe 942 hrs · 26,985 cycles

FLAPS WOULD NOT EXTEND FOR LANDING. EXTENDED TO THE FLAP 0 & SLATS EXTEND POSITION THEN FROZE. CLEANED & INSPECTED FLAP CONTROL MODULE. TESTED FLAP HYD ACTUATION IAW AMM 27-50-00-5. OPERATIONS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (RT WING) · airframe 941 hrs · 26,911 cycles

CRUISING AT FL370 RECEIVED AIR SYS OFF LEVEL 1, FOLLOWED BY AIR MAN NR 3 FAIL LEVEL 3. COMPLIED WITH CHECKLIST & LAND AT NEAREST SUITABLE. RELEASED FOR SERVICE IAW MEL 36-10-02-A. PERFORMED NR 3 PNEU SYS DECAY CHECK IAW AMM 36-00-04-5. 13 SECONDS FROM 30-20 PSI DECAY TIME. OK TO CONTINUE. REMOVED PANEL IMMEDIATELY OTBD OF NR 3 ANTI-ICE VLV PANEL. REMOVED NR 3 MANIFOLD DETECTION SWITCH IAW AMM 36-23-03-4 STEPS 1 THRU 2 A 6. AFTER REMOVING SWITCH NOTED SWITCH MOUNTING BRACKET IS CRACKED. INSTALLED NEW RT WING MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW MM.

Part: CONTROL UNIT — FAILED (EMERGENCY POWER) · airframe 937 hrs · 26,745 cycles

DURING PUSHBACK RECEIVED AN EMERGENCY POWER ON ALERT, RESET WITH MX DIRECTION. DURING CLIMB OUT GOT ANOTHER EMERGENCY POWER ON ALERT WITH FUMES. COMPLIED WITH QRH, RESET PROCEDURE. EMERGENCY POWER ON ALERT RETURNED. R & R EPCU IAW AMM 24-08-01-4-0. OPERATIONS CHECKED EPCU IAW AMM 24-08-01-5- 0, CHECKED GOOD, ACFT TO REMAIN CAT 3 IAW AMM 22-00-00-2-0 & THE PREVIOUSLY REFERENCED OPERATIONS CHECKED AMM.

Part: BOTTLE — EMPTY (PAX DOOR) · airframe 936 hrs · 26,737 cycles

R1 DOOR WON'T CLOSE. EMERGENCY HANDLE IS IN THE INCORRECT POSITION, AIR PRESSURE IN BOTTLE IS ZERO. RESET CONTROL VALVE AT RESERVOIR, CHARGED TO 1500 PSI, LEAK CHECKED NORMALLY.

Part: KEYPAD — INOPERATIVE (COCKPIT DOOR) · airframe 935 hrs · 26,684 cycles

COCKPIT DOOR KEYPAD INOPERATIVE. REMOVED AND REPLACED COCKPIT DOOR KEY PAD IAW AMM 52-54-01-2-2. OPS CHECKED GOOD IAW AMM 52-54-01-5-0.

Part: WINDOW FRAME — CORRODED (COCKPIT) · airframe 935 hrs · 26,684 cycles

CAPTAIN`S WINDSHIELD FOUND DELAMINATED. CAPTAIN`S WINDSHIELD FRAME SURFACE CORROSION ON SEVERAL AREAS OF EXTERNAL SURFACE OF LOWER FRAME SEGMENT. REPAIRED IAW EA 8-5310-T0315060.

Part: SHEAR TIE — CRACKED (BS 1305) · airframe 93,562 hrs · 26,684 cycles

MAIN DECK SIDEWALL BS 1305 SHEAR TIE CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM VOL II AND SRM 51-31- 01 VOL II.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE 1G81D20 DAMAGED. REMOVED AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE E111-39-20 DAMAGED. REMOVED AND REPLACED THE WIRE IAW SWPM 20-10-01.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE SPR414A20 DAMAGED AT PRESSURE FEED THRU P3-ZWA LT SIDE. LEFT SIDE REMOVE AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE SPR434A20 DAMAGED OVER AUX TANK. REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE Q928C20 DAMAGED OVER AUX TANK. REMOVED AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE 2H1503B24 DAMAGED OVER AUX TANK.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE 2H1805D20 DAMAGED NEAR D1-27 SENSING ELEMENT LT SIDE. R & R THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE E103-163-24 DAMAGED. REMOVED AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE E111-92-20 DAMAGED. REMOVED AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE 1G78D20 DAMAGED. REMOVED AND REPLACED THE WIRE.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE K257E16 DAMAGED OVER AUX TANK.

Part: WIRE — DAMAGED (N/A) · airframe 93,562 hrs · 26,684 cycles

WIRE NR E105-11-20 DAMAGED OVER AUX TANK. ROUTED WIRE AT MAIN DECK & WHEEL WELL IAW SWPM 20-10-01. REPLACED WIRE E105-11-20 AND TERMINATED AT CONNECTOR P1-239 IAW WDM 27-54-01. TERMINATED WIRE AT CONNECTOR P1-802 AND PERFORMED SATISFACTORY COUNTINUITY CHECK IAW WDG 27-54- 01 AND SWPM 20-10-01. PERFORMED FLAP POSITION INDICATION IAW MM 27-50-00-5 OPS CHECKED GOOD.

Part: WIRE — DAMAGED · airframe 93,562 hrs · 26,684 cycles

WIRE NR G201-226-22 DAMAGED OVER AUX TANK. R & R WIRE G201-226-22.

Part: PANEL — DELAMINATED (LT WING) · airframe 93,562 hrs · 26,684 cycles

LEFT WING INBD TE TRAP PANEL ARC0269-503 HAS DELAMINATION, REQUIRED RE-SKIN. REPAIR TRAP PANEL ARC0269-503 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: PANEL — GOUGED (RT WING) · airframe 93,562 hrs · 26,684 cycles

PANEL 635DL HAS A DEEP GOUGE IN IT. REPAIRED AREA IAW SRM 51-71-00 VOL 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 93,562 hrs · 26,684 cycles

LOWER FWD FUSELAGE RT HAS A DENT APPROX STATION 348. FOUND DENT OUT OF LIMITS. REPAIRED IAW SRM 53-20-00 FIG 13.

Part: SKIN — CORRODED (BS 1701-1781) · airframe 93,562 hrs · 26,684 cycles

LEFT LOWER CTR FUSELAGE SKIN HAS SURFACE CORROSION UNDER RUB STRIP FROM BS 1701 - 1781. REPAIRED SKIN IAW SRM 53-20-00 FIG 6. CLASS 1 REPAIR.

Part: SKIN — CRACKED (BS 1701) · airframe 93,562 hrs · 26,684 cycles

LEFT LOWER FUSELAGE BS 1701 SKIN CORRODED & CRACKED UNDER RUB STRIP. REPAIRED SKIN IAW SRM 53-20-00 FIG 6. CLASS 1 REPAIR.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 93,562 hrs · 26,684 cycles

LEFT WING OTBD FLAP, OTBD HINGE FITTING AFT LOWER HINGE PANEL 536JL HAS CRACKED SUPPORT ANGLE ON INBD SIDE. DOT 6 INSTALLED SUPPORT ANGLE IAW SRM 51-35-01 VOL II PN ARC 2481-17.

Part: SKIN — CRACKED (RT WING) · airframe 92,285 hrs · 26,163 cycles

FOUND CRACK ON RT WING FWD OF SLAT DRIVE DOOR. TRIMMED OUT CRACK AREA, FABRICATED FILLER & LOCATED FASTENER HOLES IAW SRM 57-10-00.

Part: PRESSURE SWITCH — FAILED (BLEED AIR) · airframe 90,321 hrs · 25,310 cycles

AIR SYS 3 OFF ALERT RAN QRH THEN MANIFOLD FAIL ALERT DIVERT KMCI. PERFORMED SATISFACTORY PNEUMATIC SYSTEM PRESSURE DECAY TEST WITH APU REF AMM 36-00-01-5. ON MCDU AIU 1 SHOWS CURRENT FAULT 314212 "NO LOOP 3 INPUT RCVD DURING MANF PREFLT TST-P". ON FRONT OF MANIFOLD FAILURE DETECTION CONTROLLER, RT WING PRESSURE SWITCH FAULT BALL IS DISPLAYED. REF FIM. BEFORE CHANGING SWITCH RAN PNEUMATIC SYSTEM 3 AND PERFORMED A PRESSURE DECAY CHECK PER AMM 36-00-01-5. ALL CHECKS PASSED. CHECKED FOR LEAKS ON LEADING EDGE AND FOUND NO LEAKS INDICATED. CHECKED MANIFOLD FAILURE CONTROLLER AND FOUND RT WING PRESSURE SWITCH FAULT BALL ILLUMINATED. CLEARED FAULT. REMOVED AND REPLACED MANIFOLD FAILURE DETECTION PRESSURE SWITCH S1-650 PER AMM 36-23-03-4. PERFORMED MANIFOLD FAILURE ADJUSTMENT TESTED PER AMM 36-23-01-5-1 AND NO FAULTS. SUPPLIED PRESSURE TO NR 3 PNEU SYSTEM AND TURNED ON WING ANTI-ICE. NO PRESSURE SWITCH FAULT ON CONTROLLER.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 89,183 hrs · 24,845 cycles

BRIEFLY DETECTED, WHITE SMOKE AND AN OILY ODOR FROM COCKPIT ECS, AS TEMP CONTROLLER WAS INCREASED DURING CRUISE. R & R CLOGGED COALESCER BAG ON PACK. NR 1 IAW AMM 21-54-03-2.

Part: LAMP — INOPERATIVE (SLIDE LIGHT) · airframe 87,924 hrs · 24,324 cycles

LT CREW ENTRANCE DOOR SLIDE LIGHT INOPERATIVE. RELAMPED PER SMP, NO DEFECTS NOTED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 87,300 hrs · 24,079 cycles

RT FUSELAGE AT APPROX STA 1887, L47R HAS BULGING SKIN. REMOVED FASTENERS AND SPOT FACED 5 EA, 1 IN CIRCLE AREAS TO ACCESS CORROSION AREAS REF SRM 53-20-00 FIG 6, SH 5 CUT OUT CORROSION REF SRM 53-20-00, VOL 1. FABRICATED REPAIR FILLER REF SRM 53-20-00, VOL 1, FABRICATED DOUBLER AND TRIPLER REF SRM 53-20-00, VOL 1, FABRICATE FINGER DOUBLERS REF SRM 53-20-00, VOL 1. INSTALLED PARTS IAW SRM 53-20-00, FIG 6, SH 5.

Part: STRAP — MALFUNCTIONED (COCKPIT) · airframe 87,066 hrs · 23,988 cycles

UNABLE TO DEPLOY CAPTS LEFT SHOULDER STRAP. NO DEFECTS NOTED IAW MM 25-11-01-8-0. OK TO CONTINUE.

Part: BLEED VALVE — OVERHEATED (NR 1 ENGINE) · airframe 86,729 hrs · 23,870 cycles

BLEED AIR 1, HI TEMP LEVEL 3, ALERT. REPLACED NR 1 ENG FAN VALVE IAW MM36-13-04-4 AND RAN ENG NO FAULTS FOUND.

Part: WARNING LIGHT — ILLUMINATED (CARGO FIRE) · airframe 86,305 hrs · 23,712 cycles

DURING PREFLIGHT ACTVITIES STARTED APU. AFTER APU START AND WAITING FOR ELECTRICAL SWITCH OVER, GOT A LEVEL 3 CARGO FIRE LWR1 ALERT. FOLLOWED QRH AND DISCHARGED FIRE BOTTLE (FLASHING DISCHARGE SWITCH). REMOVED AND INSTALLED LOWER CARGO COMPTMENT FIRE EXTINGUISHER IAW MM 26-22-01-4 AND INSTALLED LOWER CARGO COMPARTMENT FIRE DISCHARGE CARTRIDGE IAW 26-22-04-4 AND TEST LOWER CARGO FIREX DISCHARGE CURCUIT IAW MM 26-22-01-5. OPS CHECK NORMAL. OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.

Part: WARNING SYSTEM — MALFUNCTIONED (CARGO FIRE) · airframe 83,358 hrs · 22,698 cycles

CARGO FIRE WARNING LWR AFT COMPARTMENT WARNING WAS INTERMITTENT, SMOKE INDICATOR LWR AFT COMPARTMENT (AFT INDICATOR) IN VIEW. FIRED LWR AFT FIRE BOTTLE, LWR FWD BOTTLE FIRED BY ITSELF. AFTER ACFT WAS PARKED ALSO SAW FAILED SMOKE INDICATOR IN LWR CTR COMPARTMENT.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 83,357 hrs · 22,697 cycles

REC'D A LEVEL 3 "AFT CARGO FIRE" WARNING. PERFORMED QRH IMMEDIATE ACTIONS. DISCHARGED BOTTLE, LANDED WITHOUT WARNING ILLUMINATED. AFT ABK INDICATION OF FIRE. COMPLIED WITH MTSI 26-10/6387, INSP OF CONNECTOR PLUGS AND REMOVED AND REPLACED AFT AND CENTER CARGO SMOKE DETECTORS, REF TSI FOR PARTS INSPECTED ABK CARGO, NO EVIDENCE OF FIRE. REMOVED AND REPLACED LWR CARGO FIRE EXTINGUISHER BOTTLE, REF MTSI 26-10-6387 FOR SMOKE DETECTORS REPLACEMENT. ACFT OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 100) · corrosion level 2 · airframe 82,838 hrs · 22,523 cycles

DEFECT TRANSFERED FROM NRC N00340, DURING REMOVAL RAIL CHANNEL ON CENTER CARGO COMPT FOUND CRACK AND CORROSION OUT OF LIMIT ON CTR DOOR JAMB. REPAIRED AREA IAW EA 8-5310-128537.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 82,838 hrs · 22,523 cycles

RT INBOARD FLAP UPPER SURFACE FOUND DEEP SCRATCH 4 INCHES LONG AND DEEP MAX .078 INCHES ON UPPER SKIN, DAMAGE IS "NON/FLIGHT AIRCRAFT STRIKE DAMAGE". REPAIRED SKIN IAW SRM 57-10-00 FIG 85 1-4 VOL I.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 82,838 hrs · 22,523 cycles

CTR CARGO COMPT PERFORMED INSPECTION AFTER LINING REMOVAL WITH OAN J/C DC10- 2552CI80-3JR FOUND SEVERE CORROSION WITH EXFOLIATION ON TEE. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I AND SRM 53-70-00 FIG 7 SHT 5 VOL I.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 82,838 hrs · 22,523 cycles

DURING REPAIR ACCOMPLISHMENT PER NRC NR N00497 FOUND ON LT WING NR 2 SLAT CRACK ON INNER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 43 SHT 1, VOL I.

Part: SKIN — DAMAGED (ZONE 800) · airframe 82,838 hrs · 22,523 cycles

FWD LOWER CARGO DOOR, DEFORMED FWD LOWER SKIN CORNER. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

MAIN CABIN FOUND A CRACK ON WEB JAMB DOOR.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

MAIN CABIN FOUND A CRACK ON WEB JAMB DOOR. REPAIRED AREA IAW SRM 53-50-00 FIG 19 SHT 2 VOL I.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 82,838 hrs · 22,523 cycles

RT WING FOUND CRACK ON INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 82,838 hrs · 22,523 cycles

RT WING L/E FOUND CRACK ON INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 82,838 hrs · 22,523 cycles

RT WING L/E FOUND CRACK ON INTERCOSTAL. REPAIRED AREA IAW SRM 57-00-01 FIG 3 SHT 2 VOL I.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 82,838 hrs · 22,523 cycles

RT WING FOUND CRACK ON INTERCOSTAL. REPAIRED AREA IAW SRM 57-00-01 FIG 3 SHT 2 VOL I.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON STIFFENER ABOVE.

Part: ANGLE — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON ANGLE. REPAIRED ANGLE IAW SRM 53-30-00 FIG 2 A VOL I.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON STIFFENER ABOVE. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 2 SHT 2 VOL I.

Part: ANGLE — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON ANGLE.

Part: SKIN — CRACKED (NR 4 SPOILER) · airframe 82,838 hrs · 22,523 cycles

LT WING NR 4 SPOILER FOUND CRACK ON UPPER SURFACE SPOILER. SDR WRITTEN IN ERROR, SPOILER WAS REMOVED AND REPLACED WITH OVERHAULED UNIT.

Part: SKIN — CRACKED (NR 4 SPOILER) · airframe 82,838 hrs · 22,523 cycles

LT WING NR 4 SPOILER FOUND CRACK ON UPPER SURFACE SPOILER.

Part: FLOORBEAM — NONE (ZONE 100) · airframe 82,838 hrs · 22,523 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON FLOORBEAM. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 82,838 hrs · 22,523 cycles

LT WING L/E FOUND CRACK ON SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 39. VOL I.

Part: ANGLE — CRACKED (ZONE 500) · airframe 82,838 hrs · 22,523 cycles

LH WING SLATS FOUND CRACK ON ANGLE OUTBOARD SIDE NR 2 SLAT.

Part: ANGLE — CRACKED (LT WING SLAT) · airframe 82,838 hrs · 22,523 cycles

LT WING SLATS FOUND CRACK ON ANGLE OTBD SIDE NR 2 SLAT. REPAIRED ANGLE IAW SRM 57-00-01 FIG 3 SHT 2 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 82,838 hrs · 22,523 cycles

LH WING L/E FOUND CRACK ON SKIN L/E.

Part: WEB — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10- 0600C210-1JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: WEB — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: WEB — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 82,838 hrs · 22,523 cycles

FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 82,838 hrs · 22,523 cycles

DURING U/S INSP OF HORIZ STB, FOUND UPPER INTERIOR SKIN PANELS PN 7229-1, PN 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS, INSP FINDING FORM FOR DETAIL. ACCOMPLISHED EA NR 8-5510-125425.

Part: SKIN — CRACKED (ZONE 300) · airframe 82,838 hrs · 22,523 cycles

DURING U/S INSP OF HORIZONTAL STAB, FOUND UPPER INTERIOR SKIN PANELS P/N 7229-1, P/N 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS,

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 82,838 hrs · 22,523 cycles

DURING INSPECTION NLG W/W FOUND CRACK ON VERTICAL WEB.

Part: BULKHEAD WEB — CRACKED (NLG WW) · airframe 82,838 hrs · 22,523 cycles

DURING INSP NLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 2-3 VOL I.

Part: SKIN — CRACKED (LT WING) · airframe 82,838 hrs · 22,523 cycles

LT WING L/E CRACK ON EXT LOWER SKIN.

Part: SKIN — DENTED (ZONE 100) · airframe 82,838 hrs · 22,523 cycles

LOWER FUSELAGE DENT ON EXT SKIN DIM: 2" X 2" DEPTH 0.09". REPAIRED DENT IAW SRM 53-20-01 FIG 13 SHT 2A VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 82,838 hrs · 22,523 cycles

LT WING L/E CRACK ON EXT LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 82,838 hrs · 22,523 cycles

LOWER FUSELAGE DENT ON EXT SKIN DIM, 2 INCH BY 2 INCH DEPTH 0.09 INCH.

Part: SEAT TRACK — WORN (BS 1099-1321) · airframe 80,346 hrs · 21,351 cycles

MCD SEAT TRACK FROM STA 1099 TO STA 1321 RBL 47 HAS 6 AREAS WITH WORN LUGS. FOUND DURING C CHECK AT MAE, REMOVED AND REPLACED DAMAGED SEAT TRACK

Part: HANDLE — PULLED (SERVICE DOOR) · airframe 79,160 hrs · 20,844 cycles

DESCENDING THRU 4000 FT GOT BOTH LEFT AND RIGHT CABIN DOOR ANNUNCIATOR LIGHTS ILLUM. PRESSURIZATION WENT TO ZERO DIFF PRESS AND CABIN ALT= ACFT ALT. LANDED EWR WITHOUT INCIDENT. FOUND BOTH AFT DOORS OPEN ON WALKAROUND, TRIED TO ELECTRICALLY CLOSE DOORS NO HELP. FOUND ALL C/B'S IN OVERHEAD PANEL OF MCD PULLED AND COLLARED. RESET C/B'S NO HELP. BOTH RED T-HANDLES WERE TAPED DOWN. BOTH DOORS ARE IN THE ARMED POSITION. RECOLLARD C/B'S, PANEL IS STILL OPEN AND WILL NEED TAPED. PERFORMED ADJUSTMENT AND TEST PER DC10 MM 52-10-01-2. FOUND RED EMERGENCY HANDLE HAD BEEN PULLED ON BOTH DOORS. SUSPECT HANDLE INADVERTENTLY BEEN PULLED DURING "B" CHECK. RESET HANDLES/DOORS PER SAME MM. NO OTHER DEFECTS NOTE

Part: DOOR — OPEN (NR 4 PAX DOOR) · airframe 78,740 hrs · 20,655 cycles

LEFT AFT NR 4 ENTRY PASS/CREW DOOR CAME OPEN IN FLIGHT. FOUND THAT THE LEFT AFT NR 4 PASS/CREW SERVICE DOOR -RED- EMERGENCY HANDLE WAS PULLED PRIOR TO DEPARTURE. SUSPECT HUB PERSONNEL LIFTED HANDLE TO RAISE DOOR WITH NO RESULTS, THEN RELEASED HANDLE WITH NO COCKPIT DOOR WARNING INDICATION. DUPLICATED THIS SCENERIO WHEN THE AIRCRAFT RETURNED TO GATE AFTER TRANSLOAD. CLOSED, LOCKED, AND SECURED DOOR PER DC-10-30 M/M CHPT 52-12-00-0. A/C OK FOR SERVICE.

Part: MANIFOLD — FAILED (NR 2 PNEU SYS) · airframe 77,876 hrs · 20,310 cycles

CLIMBING TO 1800 NR 2 MANIFOLD FAILURE. COMPLIED WITH QRH UNABLE TO REDUCE NR 2 PNEUMATIC PRESSURE .LANDED AT NEAREST SUITABLE AIRPORT. "MEL 36-01-A: NR 2 PNEUMATIC SUPPLY SYSTEM - INOP." INSTALLED NEW FLANGE, RETAINER & SEAL AT NR 2 ENG OVER PRESSURE VALVE.

Part: WARNING LIGHT — INTERMITTENT (A/C DOOR) · airframe 77,283 hrs · 20,041 cycles

DURING CRUISE FLIGHT, WE GOT THE AIR CONDITIONER DOOR OPEN LIGHT THAT CAME ON SEVERAL TIMES. GRADUALLY COMING ON FOR LONGER PERIODS RAN QRH & LANDED AT NEAREST FIELD,KIND. INSPECTED ALL THREE AC BAY DOOR SWITCHES IAW 52-42-01-2 FOUND ALL 3 DOOR SWITCHES TO OPERATE NORMAL. INSPECTED F/E ANNUNCIATOR LIGHT PANEL, FOUND NUMEROUS ANNUCIATOR CONTACT PINS TO BE DAMAGED & COULD CAUSE AC DOOR LIGHT TO FLICKERON & OFF W/ VIBRATION. R&R'D F/E'S ANNUNCIATOR LIGHT PANEL IAW 33-15-02-2 OPS NORMAL. RETURNED A/C TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (PNEU MANIFOLD) · airframe 73,623 hrs · 19,053 cycles

NR 3 MANIFOLD FAILURE LIGHT ILLUMINATED IN CRUISE AT FL 370. RED TABS FOLLOWED. T/S PER TAFI 36-23-00 FAULT CODE BC/YZ. PROBLEM DUPLICATED WITH OR WITHOUT PNEU SYS NR 3 PRESSURIZED. ACCOMPLISHED NR 3 PNEUMATIC SYSTEM DECAY CHECK PER DC-10 JRH TEST PASSED. WHEN DUPLICATING PROBLEM PNEU PRESSURE SWITCH FAULT BALL WOULD ILLUMINATE ON FAULT INDICATOR WITH FAIL LIGHT. REMOVED AND REPLACED NR 3 PNEUMATIC MANIFOLD FAILURE PRESSURE SWITCH PER MM 36-23-03-4. OPS CHECKED NORMAL. ITEM CLEARED, A/C OK TO CONTINUE.

Part: PROXIMITY SENSOR — INOPERATIVE (ZONE 700) · airframe 71,529 hrs · 18,379 cycles

UPON GEAR RETRACTION AFTER DEPARTURE, FRONT DISPLAY (F/O) LT MAIN GEAR LIGHT REMAINED RED, ALL OTHERS EXTINGUISHED. RECYCLED GEAR IAW RED TAB PROCEDURE- GEAR RETRACTED NORMALLY; ALL LIGHTS EXTINGUISHED. R/R PROX BOX.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 70,486 hrs · 18,023 cycles

CENTER CARGO DOOR COUNTER BALANCE BEAM CRACKED AT FORWARD BRACKET. REMOVED AND REPLACED COUNTER BALANCE BEAM ASSEMBLY IAW MM.

Part: MEC — OUT OF RIG (NR 3 ENGINE) · airframe 68,855 hrs · 17,505 cycles

ON TAKEOFF NR 3 ENG W/N ATTAIN MAX PWR. ADJUSTED NR 3 ENG MEC 1/2 TURN UPTRIM, RAN ALL ENG PER JRH CHAPTER 5 AND ACCOMPLISHED MAX. ALL ENGINES OPERATING OKAY.

Part: DOOR — DAMAGED (MAIN CARGO) · airframe 65,472 hrs · 16,616 cycles

SNRM N-1 A/C STRIKE MAIN CARGO DOOR AQS/LAX NOTE: A/C MAIN CARGO DOOR DAMAGED IN OAKLAND AND FERRIED TO LAX FOR REPAIRS. ** S/D ** R&R DOOR PER EA 8-5230-49684 AND SRM 51-31-01 VOL II.

Part: TRANSFORMER — FAULTY (COCKPIT) · airframe 65,970 hrs · 16,615 cycles

DURING SAFETY CHECK FOUND OVERHEAD SWITCH PANEL LIGHTS (CB) POPPED. RESET NORM. BEGAN TO SMELL FUMES AND SMOKE FROM OVERHEAD PANEL. INSTALL TRANSFORMER T1-94, OPS NORM PER MM 33-11-07-2.

Part: DOOR — CORRODED (E/E BAY) · airframe 64,587 hrs · 16,154 cycles

AVIONICS COMP DOOR NR 115AZ FOUND CORRODED INTERIOR. *S/D* REMOVED AND REPLACED PER DRAWING NR ACA 3777, MM 52-41-01-2.

Part: CONTROL CABLE — BROKEN (LT WING SLAT) · airframe 64,587 hrs · 16,154 cycles

LT WING LEAD EDGE SLAT NR 6 EXTEND CABLE NR 63 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-11-4.

Part: CONTROL CABLE — BROKEN (LT WING SLAT) · airframe 64,587 hrs · 16,154 cycles

LT WING LEAD EDGE SLAT NR 7 EXTEND CABLE NR 65 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-13-4.

Part: CLIP — CRACKED (BS 1225-1375)

SNRM 308,309,310 LT WING TO FUSELAGE UPPER FAIRING SUPPORT RIBS ATTACH CLIP CRACKED AT BS 1225, BS 1289, BS 1300, BS 1310, BS 1341 AND BS 1375. L/H WING TO SELAGE FARIR BOTTOM SUPT RIBS CRACKED. CARRIED OUT REPAIRS PER AEA 0553, ANB 7140, ANB 7139, AEA 0552, ANB 7101, PER SRM 51-35-01.

Part: CONNECTOR — DIRTY (NLG)

97-0197 - WITH GEAR RETRACTED RED NOSE GEAR UNSAFE LIGHT ON F/E PANEL INTERMITTENT ON (NO LIGHT ON FWD PANEL) RECYCLED GEAR NO CHANGE. INSPECTED NOSE GEAR PROX SWITCHES FOR DAMAGE ALL OK PROX BOX. REMOVED AND CLEANED ELECTRICAL PINS GOOD BITE TEST NOW OK FOR SERVICE.

Part: GEAR LIGHT — FAILED (CENTER GEAR)

ON EXTENSION OF THE LANDING GEAR THERE WAS NO GREEN GEAR LIGHT FOR THE CENTER GEAR. RECYCLED GEAR TO NO AVAIL. RELAMPED BOTH F/E AND PILOT CENTER GEAR POSITION LIGHT, OPS CK'D GOOD.

Part: HYD PUMP — LEAKING (NR 3 ENG)

TOTAL LOSS OF HYDRO SYSTEM NR 3 ON CLIMBOUT, PERFORMED RED TAB PROCEDURE AND LANDED 35/EXT 16L SEA WITHOUT INCIDENT. MAINTENANCE FOUND 2/3 REVIISABLE MOTOR PUMP LEAKING. REMOVED AND REPLACED 2/3 REVIISABLE MOTOR PUMP PER M/M 29-22-01, LEAK AND OPS CHECK GOOD. REMOVED AND REPLACED NR 3 ENG PRESSURE AND CASE DRAIN FILTERS, NO CONTAMINATION NOTED.

Part: GEAR LIGHT — MALFUNCTIONED (LT MLG)

ON TAKEOFF, RAISED GEAR AND ALL LIGHTS OUT, BUT AFTER A FEW SECONDS THE LEFT MAIN LIGHT ON FWD PANEL CAME ON. NO LIGHTS ON S/O PANEL. CYCLED THE GEAR AND ALL LIGHTS WENT OUT AND REMAINED OUT. LIGHTS CAME BACK ON BRIEFLY DURING DESCENT AND BACK OUT, SEVERAL TIMES. PERFORMED PROXIMITY BOX BITE CHECK AND ALL OK. CHECKED PROXIMITY SWITCH FOR SECURITY AND OPS WITH HAND HELD TARGET. CHECKED WIRING FOR SECURITY AND BREAKS, CHECKED PER TAFI 32-30-00 AND ALL CHECKS NORMAL.

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG)

AFTER TAKEOFF, A FEW MINUTES AFTER GEAR WAS RAISED THE LEFT MAIN REG LIGHT ON THE FWD PANEL ILLUMINATED. NO LIGHTS ON S/O'S PANEL. CYCLED THE GEAR AND ALL LIGHTS EXTINGUISHED. LIGHTS ILLUMINATED AGAIN DURING APPROACH PHASE. REPEAT WRITE-UP. REPLACED D1-81 LT MAIN GEAR DOOR UP AND LATCHED SENSOR IAW MM 32-61-03, OPS CKS GOOD.