N302FE

Part: CONTROL UNIT — FAILED · airframe 91,174 hrs · 27,570 cycles

DURING COCKPIT PREFLIGHT, CYCLED EMERGENCY POWER SWITCH TO ON-SELF TEST LATER FAILED. R & R EPCU REF AMM 24-08-01-4, RTS TEST PASS. OK FOR SERVICE, EMERGENCY PWR TEST PASS. ACFT ALREADY CAT 2. FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: BATTERY — DISCHARGED · airframe 90,350 hrs · 27,224 cycles

DURING SERVICE CHECK, FOUND EMERGENCY POWER FAIL ALERT ON EAD. FOUND BOTH BATTERY VOLTAGES BELOW LIMITS. R & R BOTH BATTERIES IAW AMM 24-34-01-4. ACCOMPLISHED EMERGENCY POWER TEST, TEST PASSED. ACFT OK FOR SERVICE.

Part: VALVE — FAILED · airframe 90,164 hrs · 27,154 cycles

AFTER TAKE OFF, PASSING 1500 FT. RECEIVED AURAL TRI-TONE FOR NR 2 MANIFOLD FAIL, CHECKED AIR SYS SYNOPTIC VERIFIED, REDUCED POWER TO IDLE NO HELP, STILL RED MANIFOLD INDICATIONS. RED TABS ACCOMPLISHED, RETURNED TO DEPARTURE. R & R VALVE IAW AMM 21-41-15-4, LEAK AND OPS CHECKED GOOD. PERFORMED DECAY CHECK AND NOW PASSES AT 21 SECONDS. REF FOR SECOND TEST. REMOVED MEL AND RESET MANIFOLD FAIL SYS TO NORMAL OPERATION AND COMPLETED AN AIR SYS TEST WITH NO FAULTS. FINAL CLOSED.

Part: CONTACTOR — DAMAGED (INDICATOR LIGHT) · airframe 89,295 hrs · 26,805 cycles

EMERGENCY PWR OFF, LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 24-08-03-01 CATEGORY: C EXPIRATION: 01AUG12 "MEL 24-08-03-01: EMER PWR OFF LIGHT - INOP." FOUND THAT THE CENTER CONTACT BEHIND THE EMER PWR OFF LIGHT ASSY HAS NO SPRING PRESSURE. NEED TO REPLACE THE ELEC SYS CONTROL PANEL. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL REF AMM 24-08-02-4.

Part: DIMMER — FAILED (COCKPIT LIGHTS) · airframe 88,154 hrs · 26,360 cycles

DURING CRUISE, EXPERIENCED VERY LOUD ELECTRICAL ARCING SOUND IN OVERHEAD PANEL FOLLOWED BY THICK SMOKE FROM SAME AREA. DECLARED EMERGENCY AND DIVERTED. COMPLIED WITH QRH REMOVED SEVERAL OVERHEAD PANEL`S IN FLIGHT DECK TO LOOK FOR SOURCE OF SMOKE. INSPECTED ELECTRICAL AND ELECTRONIC`S IN OVERHEAD INST PANEL`S AREA, FOUND OVERHEAD INST LIGHTING DIMMER SMELLING SMOKED, R & R OVERHEAD INST LIGHT DIMMER IAW MM 33-11-03-2-0. OPS TESTED GOOD IAW SAME MM REINSTALLED REMOVED OVERHEAD CONTROL PANEL`S IAW MM`S 24-08-02-4-0, 29-08-02-2-0, 21-08-02-4-0 OK FOR SERVICE. REMOVED SEVERAL OVERHEAD PANEL`S IN FLIGHT DECK TO LOOK FOR SOURCE OF SMOKE. INSPECTED ELECTRICAL AND ELECTRONIC`S IN OVERHEAD INST PANEL`S AREA, FOUND OVERHEAD INST LIGHTING DIMMER SMELLING SMOKED, R & R OVERHEAD INST LIGHT DIMMER IAW MM 33-11-03-2-0. OPS TESTED GOOD IAW SAME MM. REINSTALLED, REMOVED OVERHEAD CONTROL PANEL`S IAW MM`S 24-08-02-4-0, 29-08-02-2-0, 21-08-02-4-0. OK FOR SERVICE.

Part: CHARGER — MALFUNCTIONED (APU) · airframe 86,957 hrs · 25,901 cycles

DURING POWER TRANSFER FROM EXT TO APU, ELECT LOAD HELD FOR 15 SEC APU THEN DID AUTO SHUTDOWN. AFTER 3 MIN S/D CYCLE, APU RESTARTED. EMERGENCY POWER LT ANNUNCIATED BATTERY CHARGING REMAINED ANNUNCIATED AS WELL AS EMERGENCY POWER TEST FAIL. RESET BATTERY CHARGER, AND PERFORMED EMERGENCY POWER TEST. OPS CHECKED NORMAL.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 86,859 hrs · 25,864 cycles

DOOR L1 SLIDE GIRT BAR COMES OUT EVERYTIME DOOR IS DISARMED AND OPENED. ACTUACTED ARM/DISARM AND OPENED SEVERAL TIMES IAW MM 52-11-00-6, OP'S CHECK GOOD. ACFT OK FOR SERVICE.

Part: ADIRU — MALFUNCTIONED · airframe 84,456 hrs · 25,040 cycles

ENROUTE, RECEIVED AMBER ALT. LIGHT IN PFD. F/O RECEIVED AMBER ALT; IAS LIGHTS ON PFD. RECEIVED A PITOT HEAT & WINDSHEAR DET FAIL ALERT LIGHT. AUTO THROTTLES & AUTOPILOT DISCONNECTED. RECEIVED SEL ELEV FEEL MAN, SEL FLAP LIM OVRD IND, SUSPECT OR ERRATIC CHECKLISTS, CAPTAINS A/S DATASHWED 270 KTS. WHILE F/O'S AIRPEED & STANDBY AIRSPEED WITHIN 5 KTS OF EACH OTHER. DESCENDED TO FL 240. F/O'S & STANDBY AIRSPEED UNRELIABLE. DETERMINED CADC 1 RELIABLE. FOLLOWED GRH & CADC 1 INDICATIONS TO RETURN, APPROACH, LANDING & TAXI BACK TO RAMP UNEVENTFUL. R & R NR 1 & 2 AIR DATA INERTIAL REF UNIT'S. PURGED PITOT & STATIC, CAPT, F/O AND AUX & LEAK CHECKED, NONE FOUND. R & R NR 2 FCC, ALL C/W IAW AMM.

Part: WIRE HARNESS — DAMAGED (ENGINE) · airframe 83,413 hrs · 24,671 cycles

CLIMB 320 TO 340 AUTO THROTTLES ENGAGED NR3 ENG EXCEEDANCE HIGH EGT 1021, REQUIRED THROTTLE REDUCTION TO MAINTAIN EGT LIMITS. COMPLIED WITH EO 8-7720-7-5001. EGT PROBES ON NR 3 CHECKED GOOD. OPENED BORESCOPE PLUGS B3-1 AND B3-2 FOR QA ON NR 3 ENG. COMPLIED WITH BORESCOPE INSP ON NR 3 ENGINE IAW AMM PAGE 72-00-00-1 5 ON 1ST AND 2ND STAGE HPT BLADES NO DEFECTS NOTED. THE DFDR READOUT SUGGESTS THE EGT INDICATION SYS WAS FAULTY AND NEEDS TO BE FURTHER TROUBLESHOT. REMOVED AND REPLACED ALL 4 HARNESSES AND BOTH FWD AND AFT LEADS REF AMM 77-21-01-2 AND 77-21-02-2. LWR LT HARNESS NEEDS TO BE CHANGED AGAIN DUE TO FAULTY THREADS ON CONNECTOR. NEEDS ENGINE RUN OPS CHECK. FINISHED INSTALLING NR 3 ENG AFT EGT PROBE IAW AMM ATA 77-21-00-6. EGT PROBES CHECKED GOOD ON NR 3 ENG IAW AMM ATA 77-21-01-2. DID MPA TEST ON NR 3 ENG IAW JRH. EGT WITHIN PARAMETERS ON NR 3 ENG. CLOSED

Part: THROTTLE CABLE — BINDING (NR 2) · airframe 82,917 hrs · 24,512 cycles

PDX - MEM ON INITIAL DESCENT CLEARANCE, THE NR 2 THROTTLE WOULD NOT RETARD, N1 WAS APPROX 80 PERCENT ON N2. THROTTLE REMAINED FROZEN DURING ARRIVAL AND ENGINE WAS SHUTDOWN PER QRH ON DOWNWIND AT 4000 FT NR 2 THROTTLE DID FREE UP ON SHORT FINAL AND NO FURTHER BINDING WAS NOTED. WX IN PDX WAS LIGHT RAIN. FOUND SEVERAL INCHES OF WATER IN ACCESS BAY BEHIND PANEL 364FR. CLEARED DRAIN HOLES OF FOD AND DRAINED WATER. REMOVED AND REPLACED NR 2 ENG THROTTLE PUSH PULL CABLE PER MD10 76-11-01-2. PATIO DOORS AND ACCESS PANELS ARE STILL OPEN. OPS/RIG CHECK GOOD.

Part: SUPPORT BRACKET — CORRODED (CARGO DOOR) · airframe 82,756 hrs · 24,449 cycles

CENTER LOWER CARGO DOOR SPOOL BRACKET NR 2 FROM FRONT HAS DIFFERENT COLOR POWDER COMING OUT BEHIND SEALANT AND SUPPORT BRACKET, RUST COLOR. CORROSION REMOVAL PER SRM 53-50-00. HFEC BOTH HOLES TOP 2 LAYER NO CRACK INDICATION PER NDT SPM. INSTALLED FITTING REF DWG AFA-7132 AND SRM 51-00-01. INSTALLED 2 EA. REPAIR BUSHINGS IN LOWER POSITION PER SRM 53-50-00. C/W EA 8-5310-121723. INSTALLED NEW DOOR SPOOL BRAKCET PER MM 52-32-00-5 AND OPS CHECK GOOD.

Part: ACTUATOR — FAULTED (LT AILERONS) · airframe 76,492 hrs · 22,358 cycles

NR 1 A/P DISENGAGE AFTER T/O. RE-ENGAGED 1 TIME WITH IMMEDIATE DISENGAGED AGAIN. PERFORMED NR 1 AND 2 FCC TEST PER MD 10-30 MM 22-00-00-5. FOUND LIB AILERON ACTUATOR AT FAULT. ALSO, NR 1 AND 2FCC AND AFSCP. REMOVED AND REPLACED 2 FCC, AFSCP AND LIB AILERON ACTUATOR PER MD10-30 MM 27-113-01-4. PERFORMED OPS CKS AND CKS GOOD. PERFORMED BOTH FCC TEST AND R-T-S PER ABOVE MM. GND OPS CKS GOOD. SERVICED HYD SYSTEMS AS REQUIRED. SECURED ALL PANELS.

Part: COMPUTER — MALFUNCTIONED (NR 1 FCC) · airframe 76,492 hrs · 22,358 cycles

NR 1 A/P DISENGAGED ON CLIMBOUT. RE-ENGAGED 3 TIMES & EACH TIME IMMEDIATELY DISENGAGED AGAIN. REMOVED AND REPLACED RD FCC1. PASSED R-T-S PER MM 22-00-00-5.

Part: STRUCTURE — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E FOUND 1 CRACK 1" LONG ON CHORD FIXED PANEL AT STA XORS 798. REPAIRED STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F160724-3 IAW SRM 57-10-00 FIG 49 VOL 1.

Part: SPRING — UNKNOWN · airframe 75,861 hrs · 22,155 cycles

FOUND CARTRIDGE SPRING ASSY ITEM 820 P/N ARH 1694-1 WITHOUT EO# 8-2780-7-4308 APPLICABLE. ACCOMPLISHED EO# 8-2780-7-4308 P1 ATTACHED, IN CONJUNCTION WITH NRC FEDEX, N00263/F160263.

Part: REPAIR — UNKNOWN (BS 357) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1 FOUND DOUBLER DIMENSION 4" BY 3" RT EXTERNAL FUSELAGE STA 357 LONG 31. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA NR 8-5330-93226 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1 E3, TREATED AREAS IAW SRM 51-21-01 VOL 2.

Part: SKIN — CRACKED (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

RT WING OUTBOARD FLAP FOUND 6 CRACKS ON UPPER SKIN FROM STA XOF 543 TO STA XOF 575. BURNICHED AND BLENDED INTERESTED AREAS IAW SRM 57-00-01 FIG 1A SHT 3 VOL 1, CONFIRMED 4 CRACKS STA 549 1 CRACK LONG .300" AT STA 564 FOUND 3EA CRACKS FOR TOTAL LONGEST 1" WORKED IAW NDI SPM08. CUT OUT CRACKED AREAS, FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160343-3 FILLER, F160343-5 REPAIR DOUBLER, F160343- 7 FILLER, F160343-9 REPAIR DOUBLER IAW SRM 57-10-00 FIG 85 SHT 3-4 VOL 1. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85 SHT 3-4 VOL 1.

Part: REPAIR — UNKNOWN (NR 2 SLAT) · airframe 75,861 hrs · 22,155 cycles

FOUND LT WING SLAT NR 2 INT SKIN FOUND A FLUSH REPAIR DIM 5" BY 4.75" BY 5" XORS 264. REMOVED SLAT NR 2 LT, AND EXISTING REPAIRS, TRIMMED OUT PORTION OF INNER SKIN. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161061-3/N01061-3, F161061-5/N01061-5, F161061-7/N01061-7. INSTALLED PARTS AND SLAT NR 2 LT. REMOVED, REPAIRED AND REINSTALLED SLAT NR 2 LT IAW M/M 27-80-01-6, SRM 51-35-01 PAG 1- 13, SRM 51-35-02 PAGE 3-9, SRM 57-10-00 FIG 29 VOL 1, SRM 51-35-01 VOL 2. RIG AND FUNCTIONAL CHECK IAW M/M 27-80-01-6, FOUND OK.

Part: FLOORBEAM — MISREPAIRED (BS 1902) · airframe 75,861 hrs · 22,155 cycles

AFT CARGO COMPT AT STA 1902 FOUND 1 FLOORBEAM REPAIRED FROM X 55 LT TO X -55 RT AT Z-83 WITH 1 SPLICE AND 1 WEB. STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. PERFORMED INSPECTION AND REPORTED VALUE ON ATTACHED SHEET. PERFORMED CONDUCTIVITY INSPECTION REPORTED VALUES ON ATTACHED SHEET. REMOVED AND REPLACED PARTS IAW FEDEX EA# 8-5310-93235. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160289-3 SPLICE CHANNEL, F160289-5 SPLICE CHANNEL, AND F160289-7 SPLICE PLATE IAW FEDEX EA# 8-5310-93235.

Part: SKIN — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E FOUND 1 CRACK 3.50" LONG ON SKIN AT STA XORS 505 AND 1 CRACK ON INT STRUCTURE LOWER CHORD FIXED PANEL. CLEANED AREA IAW M/M 12-22-01. REMOVED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. REMOVED FASTENERS, WEB AND SKIN AS REQUIRED, REMOVED AND REPLACED TEE IAW DWG ARB1137. REMOVED AND REPLACED DOUBLER IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01. REINSTALLED FASTENERS ON WEB AND SKIN IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01 PAGE 34/47 VOL 2 AND DWG ARB1137. REPAIRED CRACK ON L/E SKIN IAW SRM 57-10-00 FIG 68 SHT 2/3 VOL 1. REINSTALLED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER #F160730/N00730.

Part: REPAIR — NONE (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

FOUND MAIN CARGO COMPT STA 1921 Z 31 BY 92 FOUND 1 NEW SECTION OF FRAME 33" LONG WITH 2 SPLICE. PERFORMED INSPECTION ON FRAME IAW SRM 53-30-00 FIG 5 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33/24 VOL 2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

FOUND DOUBLER LENGTH 9" WIDTH 8" ON RT EXT FUSELAGE AT STA 879 LONG 36. REMOVED AND REPLACED REPAIR IAW 1-109812697-7 AND SRM 53-20-00 FIG 6 SHT 5- 6 VOL 1 AND FEDEX EA# 8-5310-93218. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160401-2 INNER EXTERNAL DOUBLER AND F160401-4 OUTER EXTERNAL DOUBLER IAW SRM 52-20-00 FIG 6 SHT 5-6 VOL 1.

Part: REPAIR — NONE (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.75 INCHES BY 2.75 INCHES AT STA XORS 521. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.

Part: REPAIR — UNKNOWN (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING SLAT NR 2 FOUND DOUBLER REPAIR ON UPPER SKIN T/E OB SIDE DIM 3 INCHES BY 3 INCHES. REMOVED REPAIR IAW SRM 51-35-01 PAGE 13 AND SRM 51-33-01 PAGE 34/47. CLEANED AREAS AND REMOVED PART IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDI SPM08. FOUND CRACK 2 INCHES LONG SIGNED STOP CRACK, REPAIRED SKIN IAW SRM 57-10-00 FIG 30 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161048-2 SKIN F161048-4 FILLER AND F161048-6 STRAP IAW SRM 57-10-00 FIG 30 VOL 1.

Part: DOUBLER — DAMAGED (BS 595) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO 8-5100-7-5001-P1 FOUND DOUBLER DIM 15 INCHES BY 14 INCHES LT EXT FUS STA 595 LONG 46 TO LONG 48. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1D E3.

Part: ANGLE — CRACKED (NR 4 SLAT) · airframe 75,861 hrs · 22,155 cycles

LT WING SLAT NR 4 FOUND 1 CRACK 1" LONG ON ANGLE AT STA XORS 506. REPLACED CLIP IAW MD-10-30 M/M 27-80-01-7 FIG 401 SHT 1 AND PERFORMED ADJUSTMENT IAW MD-10-30 M/M 27-80-01-7 FIG 408 SHT 1.

Part: NONE — NONE (NONE) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.25 INCHES BY 1.75 INCHES AT STA XORS 532. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO# 8-5100-7-5001-1D FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.

Part: REPAIR — UNKNOWN (CARGO DOOR) · airframe 75,861 hrs · 22,155 cycles

FWD LOWER CARGO DOOR FOUND EXTERNAL DOUBLER FROM STA 885 TO STA 959 DIM 11 X 12 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 6 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F161770-3, DOUBLER IAW SRM 52-10-00 FIG 6 VOL 1.

Part: REPAIR — MISINSTALLED (BS 655-675) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND 1 DOUBLER DIMENS 13" BY 10" RT EXT FUSELAGE STA 665 LONG 41. REMOVED DOUBLER IAW SRM 51-30-00 AND SRM 51-35-02 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. REMOVED FINGER DOUBLER EXTERNAL IAW SRM 51-35-01 VOL 1. REMOVED CHANNEL AND BUMPER FOR ACCESS IAW DC10-30 MM 20-50-02. ACCOMPLISHED REPAIR IAW BOEING ROD SKETCH 05-10-18-004R1 AND FEDEX EA NR 8-5330-93228. INSTALLED CHANNEL AND BUMPER IAW DC10-30 MM 20-50-02. REPROTECTED AREA AND SEAL REPAIR IAW SRM 51-21-01 VOL 2.

Part: INTERCOSTAL — CRACKED (BS 879) · airframe 75,861 hrs · 22,155 cycles

FWD CARGO COMPT AT STA 879 RT AT LONG 39 AFTER REMOVAL INTERCOSTAL WITH N/R C40124 FOUND ON STRUT 1 CRACK 2.50" LONG. REMOVED PLATE IAW SRM 51-33-01 PAGE 34/47 VOL 2. TRIMMED OUT CRACKED FLANGE. FABRICATED PART IAW DETAIL PART TRAVELER F161706/3 IAW SRM 53-00-01 FIG 9. INSTALLED REPAIR ANGLE P/N F161706/3 IAW SRM 53-00-01 FIG 9 VOL 1.

Part: REPAIR — UNKNOWN (LT ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

INBOARD LT ELEVATOR UPPER SIDE FOUND 1 EXTERNAL DOUBLER REPAIR DIA 3" AT XE 160. PERFORMED INSPECTION OF REPAIR DOUBLER IAW SRM 55-00-01 VOL 1 FIG 3. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24.

Part: REPAIR — PROPER (FUSLEAGE) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P1 FOUND DOUBLER DIMENS 14" BY 4" RT, EXTERNAL FUSELAGE STA 959 LONG 40 TO LONG 42. PERFORMED A GVI OF REPAIR IAW SRM 53-50-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1P E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (LT ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

FOUND UPPER INBOARD LT ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR BETWEEN XE 240 AND XE 191 DIMENS. 45" BY 8". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2.

Part: REPAIR — UNKNOWN (LT ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

LEFT OUTBOARD ELEVATOR REPAIR ASSESSEMENT FOUND 1EA EXT DOUBLER ON LOWER SIDE AT XE 345 DIMENIONS 7 X 4.5 INCH. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2.

Part: REPAIR — DAMAGED (ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE 80 FOUND 1EA REPAIR DOUBLER 3.5 INCH DIA. PERFORMED A GVI OF REPAIR IAW SRM 55-00-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2.

Part: REPAIR — PROPER (LT ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

LT LOWER INBOARD ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 243 DIMENS 17" BY 6". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24.

Part: REPAIR — PROPER (ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 70 DIMENSION 4" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2.

Part: REPAIR — UNKNOWN (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH 236 DIMENIONS 3.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2.

Part: REPAIR — PROPER (ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 60 DIMENSION 7" BY 6.5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 VOL 1 FIG 8 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EONR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24.

Part: REPAIR — UNKNOWN (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 155 DIMENIONS 3.25 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2.

Part: REPAIR — UNKNOWN (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENIONS 8.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2.

Part: REPAIR — PROPER (LT WING FLAP) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 7.75" BY 4.75" ON LOWER SKIN AT STA XIFH 133. PERFORMED A GVI OF REPAIR IAW EA NR 8-5710-90133 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 AND TREATED STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2.

Part: REPAIR — PROPER (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING INBOARD FLAP FOUND A DOUBLER 8" BY 1" ON UPPER SKIN AT STA XIFH 147.300. PERFORMED A GVI OF REPAIR IAW SRM 57-20-00 FIG 11 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — PROPER (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY IN THE AFT FUSELAGE SECTION ZONE 316 AT STA Y 2140 FOUND 1 REPAIR ANGLE ON THE FRAME'S CAP AT X10 SIZE 10" X 2.5". PERFORMED A GVI OF REPAIR IAW SRM 53-30-00 VOL 1 FIG 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — PROPER (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P2 FOUND DOUBLER DIMENS 12" BY 7.5" EXTERNAL FUSELAGE AT STA 1370 LONG 51 RT TO 51 LT. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1P RESTORED PAINT ON STRIPPED AREA IAW SRM 52-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (BULKHEAD) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND ANGLE LENGTH 30" ON AFT CARGO BULKHEAD PRESSURE STA 2007 X =0 Z-19. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 16 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

FOUND RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH294 DIMENSION 4.5" BY 8". PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (FUSLEAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P FOUND DOUBLER LENGTH 14" WIDTH 10" RT EXT FUSELAGE AT STA 565 TO STA 575 FROM LONG 14 TO LONG 11. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 6 SHT 3,4 REV 93 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

DISCREPANCY IN THE AFT WASTE TANK AREA BULKHEAD STA 2007 FOUND NEW SECTION OF FLOOR T-CAP ANGLE Z-19 LENGTH 35" FROM X75 TO X 40 AND JUNCTION SPLICE. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 16 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3, PERFORMED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

FOUND CENTER CARGO COMPT FOUND A NEW SECTION OF BEAM AT STA 1701 X-60 TO X-22 Z-100, DIMENSION 40" LENGTH WITH A SPLICE 8" LONG AND 5" HEIGHT. PERFORMED A GVI OF REPAIR IAW SRM 53-60-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

RT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 210 DIMENSION 5 INCH BY 3 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 2P RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (LT WING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING UPPER SURFACE FOUND A DOUBLER 30.50" BY 12.50" ON SKIN AT STA XORS 130. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 44 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-500, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

FOUND DOUBLER DIAMETER 3.5 INCH RT INT FUSELAGE AT STA 809 LONG 50. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1, FOUND DOUBLER DIAMETER 3.5" LT SIDE INT FUSELAGE AFT CARGO COMPT STA 1876 LONG 31 AND LONG 32. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. THIS IS -NOT- AN SDR.

Part: REPAIR — UNKNOWN (BS 839) · airframe 75,861 hrs · 22,155 cycles

FOUND INTERNAL DOUBLER LENGTH 4.5" WIDTH 8" AT STA 839 LONG 35 RT FUSELAGE. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P1. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24.

Part: REPAIR — UNKNOWN (BS 809) · airframe 75,861 hrs · 22,155 cycles

FOUND DOUBLER DIAMETER 3.5 INCH LT SIDE INT FUSELAGE AT STA 809 LONG 50. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND DOUBLER DIA 3.5 INCH INT FUSELAGE RT SIDE AT STA 1879 LONG 41. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1.

Part: SKIN — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING TIP WING CRACKED 1 INCH LONG ON LOWER SKIN. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER IAW SRM 57-00-01 FIG 4 AND SRM 51-35-01 PG 1/13. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160709/N00709 IAW SRM 57-00-01 FIG 4.

Part: REPAIR — PROPER (LT WING FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBOARD FLAP UPPER SKIN FOUND A DOUBLER 35 X 4.25 INCHES AT STA XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.

Part: REPAIR — PROPER (BS 304-357) · airframe 75,861 hrs · 22,155 cycles

TWO EXTERNAL DOUBLERS ON LT NOSE SKIN FROM STA 304 TO STA 357 Z-15. PERFORMED AN INSPECTION ON REPAIR IAW SRM 53-00-02 VOL 1 FIG 5 SHT 12 AND 14 WAVINESS CONDITION IS WITHIN LIMITS IAW SRM 53-00-02 VOL 1 PG 4A PAR 5 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P1 E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — PROPER (LT WING FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBOARD FLAP LOWER SKIN FOUND DOUBLER 35.50 X 4.50 INCHES XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.

Part: REPAIR — IMPROPER (LT WING SLAT) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E SLAT FOUND A DOUBLER 20 X 7 INCHES ON LOWER SKIN BETWEEN STA XW 340 AND STA XW 309. REMOVED PART. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 55 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001E3.

Part: REPAIR — PROPER (ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE82 FOUND 1EA FLUSH REPAIR DOUBLER 6 X 4 INCHES. PERFORMED A GVI OF REPAIR IAW EA 8-5510-90123 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.

Part: REPAIR — PROPER (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING LOWER SURFACE FOUND DOUBLER REPAIR ON PANEL 8 X 5 INCHES. PERFORMED INSPECTION TAP TESTING, NO DELAMINATION FOUND IAW SRM 51-61-01 VOL 2 AND PERFORMED INSPECTION ON REPAIR IAW SRM 57-71-00 VOL 2 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBOARD FLAP UPPER SKIN FOUND A FLUSH DOUBLER 39.25 X 36.50 INCHES WITH INSIDE SPLICES BETWEEN XOF 593 AND XOF 557. REMOVED T/E SECTION OF O/B FLAP IN ORDER TO ACCOMPLISH REPAIR IAW DRAW ARC 453. INSTALLED REPAIR IAW FED EX EA 8-5750-88900 AND SRM 57-10-00 FIG 7 VOL 1. REINSTALLED T/E SECTION OF O/B FLAP IAW DRAW ARC 1653.

Part: DOUBLER — UNKNOWN (WS 1070) · airframe 75,861 hrs · 22,155 cycles

LT WING LOWER SURFACE FOUND A DOUBLER 24.5 X 8 INCHES ON SKIN AT STA XORS 1070. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 FIG 85 VOL 1.

Part: REPAIR — UNKNOWN (BS 695-675) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW (IAW 8-500-7-5001-1P) FOUND DOUBLER LENGTH 12 INCHES WITH 6 INCHES LT INT FUSE AT STA 695 TO STA 675 LONG 51 TO LONG 52. STRIPPED PAINT IAW SRM 51-21-01 VOL 2 PAR 33. REMOVED RIVET AND INSTALLED FASTENERS PER SRM 52-20-00 FIG 13 VOL 1, TREATED AND PROTECTED AREA IAW SRM 51-21-01 VOL 2.

Part: REPAIR — UNKNOWN (BS 675) · airframe 75,861 hrs · 22,155 cycles

MAIN CARGO COMPT AT STA 675 L12 RT FOUND FRAME WITH REPAIR DOUBLER 11 X 3 INCHES AND FLUSH REPAIR Z 60 X 92. STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 1. REMOVED AND REPLACED FASTENERS AS REQ ON SRM 53-30-00 FIG 4 VOL 1. TREATED AND PROTECTED AREA IAW SRM 51-21-01 VOL 2.

Part: REPAIR — PROPER (WS 458) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XOF 458 DIMENS 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.

Part: REPAIR — PROPER (TE FLAPS) · airframe 75,861 hrs · 22,155 cycles

FOUND LT WING OUTBOARD FLAP LWR SKIN FOUND A DOUBLER 6" BY 4" AT XOF 467. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3.

Part: REPAIR — PROPER (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENS.8.5 X 5 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — UNKNOWN (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING INBOARD FLAP FOUND DOUBLER 5" BY 5" ON UPPER SKIN AT STA XIFH 177. PERFORMED AGVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3.

Part: REPAIR — PROPER (L3 DOOR FRAME) · airframe 75,861 hrs · 22,155 cycles

MAIN CARGO COMPT L3 JAMB DOOR AT STA 1256 BY 92 AND Z-14 FOUND 1 REPAIR DOUBLER 7" BY 8". PERFORMED A INSPECTION ON REPAIR IAW SRM 53-50-00 FIG 19 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 AND RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — PROPER (LT WING AILERON) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBOARD AILERON UPPER SURFACE FOUND A REPAIR 5" BY 2.75" ON SKIN AT STA XOA 997. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3.

Part: REPAIR — PROPER (BS 304-357) · airframe 75,861 hrs · 22,155 cycles

TWO EXT DOUBLER ON LEFT NOSE SKIN FROM STA 304 TO STA 357 Z-15. PERFORMED INSPECTION ON REPAIR IAW EA 8-5310-46689 STEP 12 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-1P E3 AND RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33.

Part: REPAIR — PROPER (BS 885) · airframe 75,861 hrs · 22,155 cycles

FOUND DOUBLER LENGTH 7 INCHES WIDTH 21 INCHES ON RIGHT EXT FUSELAGE AT STA 885 FROM LONG 39 TO LONG 41. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA8-5320-40401 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1 E3.

Part: REPAIR — PROPER (RT AILERON) · airframe 75,861 hrs · 22,155 cycles

RT WING OUTBOARD AILERON FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN FROM STA XOA 1003 TO STA 1041 DIMENSION 38" BY 26". PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 E3.

Part: REPAIR — PROPER (NR 1 SLAT) · airframe 75,861 hrs · 22,155 cycles

RT WING, SLAT 1 FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN, DIMENS 11.5 X 8.5 INCHES. PERFORMED A GVI OF REPAIR IAW EA 8.5710-90122 AND FOUND IN COMPLIANCE WITH REQUEST BY EO 83500.7.5001.

Part: REPAIR — PROPER (WS 256) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD VANE FLAP, FOUND DOUBLER ON UPPER SKIN AT STA XIFH 256 DIMENS 4 INCH DIAM. PERFORMED INSPECTION FOUND NO DELAMINATION IAW SRM 51-61-01 VOL 2 TAP TEST. PERFORMED INSPECTION ON REPAIR IAW SRM 51-71-00 VOL 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3.

Part: REPAIR — PROPER (WS 458 RT) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XOF 456 DIMENSION 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3.

Part: REPAIR — PROPER (LT WING) · airframe 75,861 hrs · 22,155 cycles

FOUND LT WING L/E EXT SKIN FOUND A FLUSH DOUBLER DIMENSIONS 3" BY 2" AT STA XORS 512. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P.

Part: REPAIR — PROPER (LT WING FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING INBOARD FLAP FOUND A DOUBLER 6" BY 5" ON UPPER SKIN AT STA XIFH 288. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3.

Part: REPAIR — UNKNOWN (BULKHEAD) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 13.5 INCHES WIDTH 11 INCHES FWD NLG BULKHEAD LT STA 490 Z-40. STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. REPLACED FASTENERS AS REQUIRE IAE SRM 53-30-00 FIG 6 VOL 1 AND TREATED AREA IAW SRM 51-21-01 VOL 2.

Part: REPAIR — PROPER (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBOARD FLAP LOWER SKIN FOUND A FLUSH DOUBLER 40" BY 34" WITH A EXTERNAL SPLICE BTWN STA XOF 605 AND XOF 639. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 57-10-00 FIG 7 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3.

Part: REPAIR — UNKNOWN (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 3" BY 5.25" ON LWR SKIN AT STA XIFH 177. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3.

Part: REPAIR — PROPER (WS 997 LT) · airframe 75,861 hrs · 22,155 cycles

LEFT WING OUTBOARD AILERON LOWER SURFACE FOUND A FLUSH DOUBLER 27 X 16.5 INCHES ON SKIN AT STA XOA 997. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 2 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3.

Part: REPAIR — UNKNOWN (RT WING SPOILER) · airframe 75,861 hrs · 22,155 cycles

RT WING SPOILER NR 3 FOUND DOUBLER REPAIR ON LOWER SKIN DIMENSION 10 X 6 INCHES. INSPECTED, REMOVED AND INSTALLED SPOILER NR 3 RT WITH NEW HARDWARE IAW MM 27-60-01-4. PERFORMED FUNCTIONAL TEST IAW MM 27-60-01-4.

Part: REPAIR — PROPER (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING INBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN L/E AT STA XIFH 155 DIMENS. 2.5 X 2 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3.

Part: RIB — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING DROP CRACK ON RIB AND OLD REPAIR. REMOVED AND SCRAP EXISTING REPAIR IAW SRM 51-33-01 PG 34/47 VOL 2. INSTALLED NEW PART P/N F161121-3B IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1 AND SRM 51-33-01 PG 34/47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161121/N01121 IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1.

Part: REPAIR — PROPER (RT WING) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING TIP WING FOUND DOUBLER REPAIR ON LOWER SKIN DIMENS 10 X 10 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3.

Part: REPAIR — UNKNOWN (BULKHEAD) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 11 INCHES WIDTH 13.5 INCHES FWD NLG BULKHEAD RT AT STA 490 Z-40. STRIPPED PAINT AREA IAW SRM 51-21-01 PAR 33 VOL 2. REPLACED FASTENERS AS REQUIRED IAW SRM 53-30-00 FIG 6 VOL 1. TREATED AREA IAW SRM 51-21-01 VOL 2.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 75,861 hrs · 22,155 cycles

IN THE RIGHT DETACHABLE ELEVATOR UPPER SURFACE AT STA XE 75 FOUND 1 EA CRACK 4 INCHES LONG. REMOVED EXISTING DOUBLER NEAR CRACK, CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. TOUCH UP WHITE TOP COAT ON REPAIR DOUBLER IAW TF110, FABRICATED PART IAW DETAIL PART TRAVELER F160767 IAW SRM 55-10-00.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

RIGHT WING OUTBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN FROM STA XOF 560 TO STA XOF 599 DIMENSIONS 36.5 X 39 INCHES. REPAIR ACCOMPLISHED WITH EA FEDEX.

Part: REPAIR — UNKNOWN (BS 645-755) · airframe 75,861 hrs · 22,155 cycles

LEFT EXT FUSELAGE FOUND DOUBLER LENGTH 100 INCHES WIDTH 10 INCHES AT STA 755 TO STA 645 LONG 42. NO ACTION TAKEN EO8-5100-7-5001.

Part: REPAIR — UNKNOWN (BS 1019-1099) · airframe 75,861 hrs · 22,155 cycles

RIGHT EXTERNAL FUSELAGE FOUND DOUBLER LENGTH 80 INCH WIDTH 12 INCH AT STA 1019 TO STA 1099 LONG 42. NO ACTION TAKEN EO 8-5100-7-5001-1.

Part: REPAIR — UNKNOWN (BS 999-1099) · airframe 75,861 hrs · 22,155 cycles

LEFT EXT FUSELAGE FOUND DOUBLER LENGHT 100 INCHES WIDTH 12 INCHES AT STA 999 TO STA 1099 LONG 43. NO ACTION TAKEN EO 8-5100-7-5001-1.

Part: LONGERON — CORRODED (BS 1523) · airframe 75,861 hrs · 22,155 cycles

THE CENTER CARGO COMPT BILGE UNDERFLOOR SPACE AT STA 1523 L45 LT SIDE FOUND CORROSION WITH EXFOLIATION ON INTERNAL OF LONGERON AROUND FASTENERS. REMOVED FASTENERS IAW SRM 51-33-01 PG 6/10 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 ORIGINAL MATERIAL THK IS .250 INCH REMAIN MATERIAL THK .170 MATERIAL. REMOVED IS OUT OF LIMITS IAW SRM 53-00-00 FIG 1B. FABRICATED PART IAW DETAIL PART TRAVELER F160212-5 IAW SRM 53-10-00 VOL 2 FIG 2A SHT 1. TREATED REWORKED AREA IAW SRM 51-21-01 PAR 31-24 VOL 2. INSTALLED A REINFORCE/REPAIR ANGLE IAW SRM 53-10-00 VOL 2 FIG 2A SHT 1. INSTALLED FASTENERS IAW SRM 51-33-01 PG 34/47.

Part: REPAIR — UNKNOWN (BS 755-645) · airframe 75,861 hrs · 22,155 cycles

RIGHT EXT FUSELAGE FOUND DOUBLER LENGTH 100 INCHES WIDTH 10 INCHES AT STA 755 TO STA 645 LONG 42. EO8-5100-7-5001.

Part: REPAIR — UNKNOWN (BS 731-791) · airframe 75,861 hrs · 22,155 cycles

RIGHT EXT FUSELAGE FOUND DOUBLER LENGTH 60 INCHES WIDTH 12 INCHES AT STA 731 TO STA 791 LONG 42 AND 43. NO ACTION TAKEN EO8-5100-7-5001-1.

Part: ANGLE — CRACKED (BS 1156) · airframe 75,861 hrs · 22,155 cycles

FOUND CENTER ACCESSORY COMPARTMENT FOUND 1 CRACK 3'' LONG ON T ANGLE, FRAME TO BULKHEAD ATTACH AT STA 1156 Z-29 X-107 RT SIDE. REMOVED FASTENERS FROM AEA0159 FRAME IAW SRM 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160433-3 SPLICE PLATE, F160433-5 FILLER, F160433-11 FILLER, F160433-14 SPLICE ANGLE AND F160433-16 SPLICE ANGLE IAW SRM 53-30-00 FIG 7 VOL 1. REPAIRED FRAME IAW SRM 53-30-00 FIG 7. INSTALLED FASTENERS ON AEA0159 FRAME IAW SRM 51-33-01 PAGE 34-47.

Part: REPAIR — PROPER (BS 1341) · airframe 75,861 hrs · 22,155 cycles

IN MAIN CARGO COMPT AT STA 1341 X-47 Z-19 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: SKIN — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E FOUND 1 CRACK 1'' LONG ON SKIN AT STA XORS 670. REPAIRED CRACK ON SKIN IAW SRM 57-10-00 FIG 68 SHT 1 AND IAW SRM 51-33-01 PAGE 34-47.

Part: REPAIR — PROPER (BS 1771) · airframe 75,861 hrs · 22,155 cycles

MAIN CARGO COMPT AT STA 1771 X-27 Z-15 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 VOL 1 FIG 2A. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: REPAIR — PROPER (HORIZONTAL STAB) · airframe 75,861 hrs · 22,155 cycles

LT HORIZONTAL STABILIZER T/E FOUND NR 1 OLD REPAIR ON UPPER SURFACE AT XE 99.195. THE MEASURE 24'' LONG 5.5'' LARGE. PERFORMED INSPECTION ON SKIN REPAIR DOUBLER IAW EA NR 8-5510-63525, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: REPAIR — PROPER (BS 775) · airframe 75,861 hrs · 22,155 cycles

FOUND UPPER FUSELAGE LT SIDE FOUND DOUBLER REPAIR ON EXTERNAL SKIN AT STA 775 FROM LONG 23 TO LONG 24 Z 5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 53-50-00 FIG 9 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P1.

Part: REPAIR — PROPER (BS 1651) · airframe 75,861 hrs · 22,155 cycles

IN MAIN CARGO COMPT AT STA 1651 X-47 Z-19 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: REPAIR — UNDAMAGED (FUSELAGE) · airframe 75,861 hrs · 22,155 cycles

PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 1D P1 FOUND 3EA DOUBLER REPAIR DIMENSION 9'' BY 8'' ON INTERNAL FUSELAGE SKIN AT STA 275 TO 300 LONG 36 LT. PERFORMED INSPECTION ON REPAIR FRAME AND SKIN IAW EA NR 8-5310-46689 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P1.

Part: REPAIR — PROPER (BS 910) · airframe 75,861 hrs · 22,155 cycles

IN MAIN CARGO COMPT AT STA 910 X-47 Z-19 FOUND FLUSH REPAIR ON TRACK 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: REPAIR — PROPER (NR 1 SLAT) · airframe 75,861 hrs · 22,155 cycles

LT WING SLAT NR 1 ON INT SKIN FOUND 1EA FLUSH DOUBLER 22'' BY 22'' AT STA XORS 80. PERFORMED INSPECTION ON SLAT NR 1 REPAIR DOUBLER IAW EA NR 8-5710-90122. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: REPAIR — PROPER (BS 808) · airframe 75,861 hrs · 22,155 cycles

FOUND UPPER FUSELAGE NR 2 LT DOOR FOUND EXTERNAL DOUBLER AT STA 808. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 52-10-00 FIG 12A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 75,861 hrs · 22,155 cycles

RT MLG WHEEL WELL 2EA CRACKS ON VERTICAL WEB AT STA 1485 X-95 OUTBOARD SIDE. REPAIRED IAW SRM 53-50-00 FIG 2A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161133-29 REPAIR WEB, F161133-3 FILLER (QTY 2), F161133-31 STRAP, F161133-31A STRAP AND F161133-31B STRAP IAW SRM 53-50-00 FIG 2A.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING L/E INTERNAL STRUCTURE FOUND 1EA CRACK 0.25'' LONG ON RIB AT STA XORS 873. REPAIRED L/E FORMER PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-35-01 PAG1-13 AND SRM 51-33-01 PAGE 34-47.

Part: FRAME — CORRODED (BS 919) · airframe 75,861 hrs · 22,155 cycles

IN THE FWD CARGO COMPT SUMP AREA AT STA 919 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L 51 LH TO L 50 RH. TRIMMED OUT FRAME CAP CORRODED REMOVED REMAINING CORROSION IAW SRM 51-21-01 PAR 34 VOL2 ORIGINAL MATERIAL THK IS .071 INCHES MATERIAL REMOVED .019 INCHES. REMAIN MATERIAL THK .052 INCHES MATERIAL REMOVED 26.25 PERCENT REMAIN 73.25 PERCENT IAW SRM53-30-00 FIG8 (NOTE2)FAB PARTS IAW DETAIL PARTS TRAVELER F160441-3 FILLER, F160441-5 CHANNEL, F160441-9 SHEAR CLIP AND F160441-7 SPLICE IAW SRM 53-30-00 FIG 10 AND FIG 8, SRM 53-13- 01 FIG 17 VOL 3 INSTALLED PARTS IAW SRM 53-30-00 FIG 8-10 INSTALLED 3EA HILOCKS .250 INCHES DIA IAW SRM 51-33-01 PAR 6-10 VOL 2.

Part: DOUBLER — CRACKED (BS 885) · airframe 75,861 hrs · 22,155 cycles

FOUND DOUBLER LENGTH 8.5 INCH WIDTH 6 INCHES ON RT EXTERNAL FUSELAGE AT STA 885 FROM L 31 TO L32. REMOVED AND REPLACED REPAIR IAW SRM 53-50-00 FIG 8 AND FEDEX EA NR 8-5350-88889 FAB PARTS IAW DETAIL PARTS TRAVELER F160357-1 AND F160357-2 IAW SRM 53-50-00 FIG 8 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING L/E INT STRUCTURE FOUND 1CRACK 0.50'' ON RIB AT STA XORS 974. REPAIRED L/E FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 75,861 hrs · 22,155 cycles

MAIN CARGO COMPARTMENT JAMB DOOR R3 STA 1256 X92 AND Z61 FOUND PLATE IN THE UPPER SECTION OF JAMB CRACK FOR 0.5 INCH LONG. REPAIRED CRACK IAW SRM 53-50-00 FIG 19 VOL1 FAB PART IAW DETAIL PART TRAVELER N01159.

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 75,861 hrs · 22,155 cycles

RT MAIN LANDING GEAR WHEEL WELL INT CRACK LONG 1.5 INCH ON HORIZONTAL INTERCOSTAL AT STA 1475 Z-103 OB SIDE. FAB PART IAW DETAIL PART TRAVELER F 161131-3 IAW SRM 53-50-00 FIG 2. INSTALLED STRAP DOUBLER F161131-3 IAW SRM 53-50-00 FIG 2 VOL 1.

Part: STRUCTURE — CORRODED (BS 1561-1581) · airframe 75,861 hrs · 22,155 cycles

IN THE CENTRAL CARGO COMPT BILGE UNDERFLOOR SPACE BETWEEN STA 1561 TO 1581 L 45 RT SIDE FOUND LIGHT CORROSION ON INTERNAL OF LONGERON AROUND FASTENERS. REMOVED FASTENERS IAW SRM 51-33-01 PAR 6-10 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2; AT THE END OF LONGERON ORIGINAL THK IS .060'' AFTER REMOVED, CORROSION MATERIAL AT 2.50 INCHES OF THE END FOUND THK .040'' MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1 B VOL 1. FAB PART IAW DETAIL PART TRAVELER F160211- 3 REPAIR CHANNEL IAW SRM 53-10-00 FIG2A. TREATED REWORKED AREA IAW SRM 51-21-01, PAR 31-24. INSTALLED REPAIR CHANNEL IAW SRM 53-10-00 FIG2A.

Part: SKIN — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING L/E CRACK ON CHORD FIXED PANEL AT STA XORS 498. FAB AND INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-35-01 PAG 1-13. FAB PART IAW DETAIL PART TRAVELER F160742/N00742 PER SRM 57-10-00 FIG 49.

Part: SKIN — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E WING TIP FOUND 1 EA CRACK .50 INCH LONG ON EXISTING REPAIR ON LOWER SKIN AT STA XW99. TRIMED OUT CRACKED PORTION SKIN REPAIR IAW SRM 57-00-01 FIG 4 VOL 2 FAB PART IAW DETAIL PART TRAVELER N00550/F160550.

Part: SEAT TRACK — CRACKED (BS 1029) · airframe 75,861 hrs · 22,155 cycles

MAIN CABIN AT STA 1029 LT SIDE AT X27.500 ON SEAT TRACK FOUND 1EA CRACK 10 INCHES LONG. CUT OUT CRACKED SECTION OF SEAT TRACK, REPLACED NEW SECTION IAW SRM 53-70-00, FIG 1 SHT1-2, VOL1. FAB PARTS IAW DETAIL PARTS TRAVELER F161689/N01689.

Part: FRAME — CORRODED (BS 1505) · airframe 75,861 hrs · 22,155 cycles

LT MLG WHEEL WELL FOUND SEVERE CORROSION ON FRAME AND ANGLE AT STA Y1505 X62. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 ORIGINAL THK OF FRAME IS .090''. MATERIAL REMOVED IS .045',' REMAIN MATERIAL THK .045''. MATERIAL REMOVED 50 PERCENT IS OUT LIMIT IAW SRM 51-21-01 FIG 1B; TRIMMED OUT DAMAGED FRAME, FAB PARTS IAW DETAIL PARTS TRAVELER F161114-3 FILLER AND F161114-5. REPAIR ANGLE IAW SRM53-00-01 FIG 8. INSTALLED PARTS IAW SRM 53-00-01 FIG 8 SHT 1.

Part: WEB — CORRODED (COCKPIT) · airframe 75,861 hrs · 22,155 cycles

INTERNAL LOWER COCKPIT AREA FOUND CORROSION INTERGRANULAR ON MEMBRANE BETWEEN STA 330 TO STA 313 X42 LT SIDE. REPAIRED MEMBRANE IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01 PAG 1-13 FAB PARTS IAW DETAIL PARTS TRAVELER F160481/N00481 PER SRM 53-00-01 FIG 10 SHT 4

Part: SKIN — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E NR 517 CT FOUND 1 CRACK 3'' LONG ON SKIN. REPAIRED PANEL IAW SRM 57-10-00 FIG 10-A VOL 1 AND SRM 51-35-01 PAGE 1-13 VOL 2.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 75,861 hrs · 22,155 cycles

IN CARGO COMPT JAMB L3 DOOR AT STA 1256 X 92 AND Z 61 FOUND PLATE IN THE UPPER SECTION OF JAMB WITH 1 CRACK 0.5"LONG. REPAIRED CRACK IAW SRM 53-50-00 FIG 19 VOL 1. FAB PART IAW DETAIL PART TRAVELER N01158.

Part: SKIN — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING OUTBD FLAP CRACK LONG 1 INCH ON UPPER SKIN AT STA XOF787. CUTE DAMAGED AREA AND REPAIRED PER SRM 57-10-00 VOL 1 FIG 85 FAB PART IAW DETAIL PART TRAVELER F160347/N00347 PER SRM57-10-00 VOL 1 SHT 4.

Part: FRAME — DAMAGED (BS 485) · airframe 75,861 hrs · 22,155 cycles

IN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 AND Z=-84 THERE IS DEEP WORN ON THE FRAME. TRIMMED OUT DAMAGE TO FRAME AND INSTALLED REPAIR CHANNEL IAW SRM 53-30-00 FIG 4 AND SRM 51-33-01 PAGE 34-4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160563/N00563 IAW SRM 53-30-00 FIG 4.

Part: FRAME — CORRODED (BS 959) · airframe 75,861 hrs · 22,155 cycles

FWD CARGO COMPT UNDERFLOOR SUMP AREA AT STA 959 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L51 RT TO L51 LT. CUT AND REMOVED SECTION OF FRAME CAP IAW SRM 51-35-01 PAGE 1-13. FAB PART IAW DETAIL PART TRAVELER F160315-3 REPAIR SPLICE AND F160315-5 FRAME CAP IAW SRM 53-30- 00 FIG 5-8 AND SRM 53-13-01 FIG 17 VOL 3, INSTALLED REPAIR CAP AND SPLICE IAW SRM 53-30-00 FIG 5-8.

Part: SKIN — NICKED (TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LT WING OUTBD FLAP UPPER SURFACE FOUND DEEP DENT AND NICK ON SKIN AT STA XOF 467. TRIMMED OUT DAMAGE SKIN INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 85 SHT 1 AND SRM 51-35-02 PAGE 3/9 VOL 2. COLD BOND PER SRM 51-71-00 PAR 16C VOL 2 FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160232/N00232 PER SRM 57-10-00 FIG 85.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

FOUND LT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0.50" LONG ON RIB AT STA XORS 523. REPAIRED RIB PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-33-01 PAGE 34-47.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 516. REPAIRED L/E FORMER PER SRM 51-20-00 FIG 1 SHT 6 VOL 3 AND SRM 51-33-01 PAGE 34-47.

Part: LONGERON — CORRODED (BS 485) · airframe 75,861 hrs · 22,155 cycles

FOUND IN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 ON THE SKIN SPLICE LONGERON 36 MODERATE CORROSION AND N35 SELF ALIGNMENT NUTS RUST. REPLACED NUTS IAW SRM 51-31-01 PAR 6 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAGE 28 ORIGINAL MATERIAL IS .094 FOR TEE AND FOR DOUBLER .071 THK REMAINING IS .083 FOR TEE AND .063 FOR DOUBLER MTL. REMOVED IS WITHIN LIMITS IAW SRM 53-00-01 FIG 1B TREATED AREA IAW SRM 51-21-01 PAR 31-34 VOL 2.

Part: STRUCTURE — CORRODED (BILGE) · airframe 75,861 hrs · 22,155 cycles

IN THE CENTER CARGO COMPT BILGE SUMP AREA AT STA 1781 BETWEEN L 51 RT TO L 51 LT. FOUND MODERATE CORROSION ON THE FRAME'S CAP. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2. ORIGINAL THK MATERIAL IS .071'', AFTER REMOVED MATERIAL FOUND THK .042''. MATERIAL REMOVED IS OUT LIMITS IAW SRM 53-30-00 FIG 8 SHT 1 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER F160215-1 IAW SRM 53-30-00 FIG 8 SHT 1 VOL 1. INSTALLED REPAIR CHANNEL IAW SRM 53-30-00 FIG 8 VOL 1.

Part: FRAME — CORRODED (BS 440) · corrosion level 2 · airframe 75,861 hrs · 22,155 cycles

AVIONICS COMPT FOUND CORROSION WITH EXFOLIATION ON FRAME STA 440 X-49 RT SIDE. TRIMMED OUT DAMAGE FLANGE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-30-00 FIG 4 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161176/N01176 IAW SRM 53-30-00 FIG 4.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING INT L/E, 3EA CRACKS ON DOUBLER AT STA XORS 685.REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160836/N00836 PER SRM 57-10-00 FIG 71 VOL 1.

Part: PANEL — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING INT L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 803. REPAIRED STRINGER DOUBLER PER SRM 57-10-00-00 FIG 49 VOL 1 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F161054/N01054 PER SRM 57-10-00 FIG 49 VOL 1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 3" LONG ON SKIN AT STA XOF 557. TRIMMED OUT DAMAGE SKIN INSTALLED FILLER DOUBLER PER SRM 57-10-00 FIG 85 AND SRM 51-35-01 PAGE 1-13 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F160229/N00229 SRM 57-10-00 FIG 85.

Part: RIB — CRACKED (LTWING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING L/E ON INTERNAL STRUCTURE FOUND 1 CRACK 0.50'' LONG ON RIB AT STA XORS 427. PERFORMED INSPECTION IAW NDT SRM 06, NO CRACK FOUND ON RIB AT STA XORS427 LT WING L/E ONLY PENCIL MARK.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0.50" LONG ON RIB AT STA XORS 490. REPAIRED RIB IAW SRM 57-20-00 FIG1 SHT 6 VOL 2 AND SRM 51-33-01 PAGE 34-37.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 75,861 hrs · 22,155 cycles

INTERNAL LWR COCKPIT AREA FOUND 2 CRACKS ON SAME MEMBRANE 1ST .50" LONG; 2ND IS 2" LONG; BETWEEN STA 304 TO STA 318; AND BETWEEN X12 TO X13 LT SIDE. REPAIRED MEMBRANE IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160482/N00482 AND IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LEFT WING OUTBD FLAP UPPER SURFACE FOUND 2 EA CRACKS 0.25" LONG ON SKIN AT STA XOF 787. TRIMMED OUT DAMAGE SKIN INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 85 COLD BOND IAW SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3/9. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160228/N00228 PER SRM 57-10-00 FIG 85.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0,5" ON UPPER DOUBLER AT STA XORS 683. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160726/N00726 PER SRM 57-10-00 FIG 71 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING EXT L/E, CRACK LONG 0,5'' ON EXT SKIN AT STA XORS 804. REPAIRED CRACK PER SRM 57-00-01 FIG 4 SHT 2 VOL 1 AND SRM 51-33-01 PAGE 34-47 FABRICATED PART IAW DETAIL PART TRAVELER F161055/N01055 PER SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 75,861 hrs · 22,155 cycles

INTERNAL COCKPIT FLOOR AREA FOUND 1 EA CRACK 2 INCHES LONG ON TEE ANGLE AT STA 275 X -45, RT. PERFORMED INSPECTION IAW NDT SPM 06, NO CRACK FOUND ON FLOOR AREA TEE ANGLE STA 275 X-45 ONLY PENCILE MARK.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING INT L/E CRACK LONG 1,5" ON INTERCOSTAL AT STA XORS 980. REPAIRED CRACK INSTALLED 2 ANGLE PER SRM 57-00-01 FIG 3 SHT 2 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160838-N00838 PER SRM 57-00-01 FIG 3 SHT 2 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WIND INT L/E, CRACK LONG 1, 5" ON RIB AT STA XOS 450. REPAIRED CRACK PER SRM 57-20-00 FIG 1 SHT 3 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160840/N00840 PER SRM 57- 20-00 FIG 1 SHT VOL 1.

Part: FRAME — DAMAGED (BS 959) · airframe 75,861 hrs · 22,155 cycles

MAIN CABIN AT STA 959 LT AT L6 DURING REM/INST STAND OFF PER J/C SP10240303-7003-17F FOUND ON FRAME EXISTING HOLE OVALIZED (1/4 INCHES DIA). CUT OUT DAMAGED AREA OF FRAME FABRICATED PARTS IAW DETAIL PART TRAVELER F161528-1 REPAIR ANGLE IAW SRM 53-30-00 FIG 13 AND DWG ADA 0049 INSTALLED REPAIR ANGLE PER SRM 53-30-00 FIG 4 VOL 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E INT STRUCTURE FOUND 1 CRACK 5" LONG ON UPPER DOUBLER AT STA XORS 660. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160729/N00729 PER SRM 57-10-00 FIG 71 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 770. REPAIRED FORMER PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-35-01 PAGE 1 3 AND SRM 51-33-01 PAGE 34-47.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 0.50" LONG ON SKIN AT STA XOF 563. TRIMMED OUT DAMAGE SKIN FABRICATED FILLER DOUBLER AND INSTALLED PER SRM 57-10-00 FIG 85 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F160230/N00230 PER SRM 57-10-00 FIG 85.

Part: PANEL — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

FOUND RT WING L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 442. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160798/N00798 PER SRM 57-10-00 FIG 49.

Part: ATTACH FITTING — CORRODED (BS 595) · airframe 75,861 hrs · 22,155 cycles

FWD CARGO FOUND STA 595 LT SIDE X-95 CORROSION ON POTABLE WATER SYSTEM ATTACHMENT. ACCURATELY POLISHED AREA ON SUPPORT AND BULKHEAD IAW MM 12-22-01-7 PERFORMED VISUAL INSPECTION ON AREA FOUND LIGHT CORROSION ON SUPPORT CLAMP REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2. ORIGINAL THK MATERIAL IS .100'' REMAIN MATERIAL THK IS .081''. MATERIAL REMOVED IS WITHIN LIMITS IAW SRM 53-00-01 FIG 1B VOL 1. PROTECTED REWORKED AREA IAW SRM 51-21-01 PAR 31-24 VOL 2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 75,861 hrs · 22,155 cycles

LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 CRACK 1" LONG ON SKIN AT STA XOF 575. TRIMMED OUT DAMAGED SKIN INSTALLED FILLER AND DOUBLER IAW SRM 57-10-00 FIG 85 AND COLD BOND SRM 51-71-00 PAR 16C VOL2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160231/N00231 IAW SRM 57-10-00 FIG 85.

Part: RIB — CRACKED (LT WING) · airframe 75,861 hrs · 22,155 cycles

LEFT WING L/E INT STRUCTURE FOUND 1 EA CRACK 1" LONG ON RIB AT STA XORS 676. REPAIRED L/E FORMER PER SRM 57-20-00 FIG 1 SHT 3 VOL 1. INSTALLED REPAIR ANGLE-31 PER SRM 51-35-01 PAGE 1-13 AND SRM-51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160727/N00727 PER SRM 57-20-00 FIG 1 SHT 3 VOL 1.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,861 hrs · 22,155 cycles

RT WING INT L/E, CRACK LONG 0,5" ON INTERNAL DOUBLER AT STA XORS 540. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160799/N00799 PER SRM 57-10-00 FIG 71 VOL 1.

Part: SKIN — CRACKED (LT WING AILERON) · airframe 75,861 hrs · 22,155 cycles

FOUND LT WING OUTBD AILERON WITH ONE CRACK 2" LONG WITH A STOP HOLE ON SKIN LOWER SURFACE AT STA XOA 824. TRIMMED BLEND OUT DAMAGE SKIN INSTALLED DOUBLER IAW SRM 57-10-00 FIG 85 AND SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PART IAW DETAIL PART TRAVELER F160226/N00226 IAW SRM 57-10-00 FIG 85.

Part: SHUTOFF VALVE — LEAKING (HYD SYSTEM) · airframe 75,459 hrs · 21,998 cycles

APPROXIMATELY 5 MINUTES AFTER TAKEOFF, MASTER CAUTION LIGHT ILLUMINATED AND OBSERVED BOTH LT & RT NR 2 EDP LIGHT ON, PRESSURE AND QUANTITY RAPIDLY WENT TO ZERO. FOUND 1-2 NONREVERSIBLE MOTOR PUMP SHUTOFF VALVE LEAKING FROM BACKUP RING.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 75,241 hrs · 21,936 cycles

AMJ PUNCTURED SKIN LT SIDE APPROX 10 FT FWD OF LWR FWD CARGO DOOR. FABRICATED REPAIR FILLER DOUBLERS REF SRM VOL 1 53-20-00 FIG 6 SHEET 11. INSTALLED CLASS 111 REPAIR REF SRM 53-20-00 FIG 6 SHEET 11, TO STAY IN OIL OFF TO 5000 CYCLES.

Part: FIRE LOOP — DAMAGED (NR 2 PYLON) · airframe 73,650 hrs · 21,390 cycles

NR 2 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB, CHECKLIST COMPLETE, LIGHT WENT OUT. DUMPED FUEL AND RETURNED TO MEM. LANDED UNEVENTFULLY. *S/D* PERFORMED DECAY CHECK OF NR 2 SYSTEM REF DC10-30 JRH. DECAY TEST FAILED FOUND THE CENTER CARGO JET PUMP SHUTOFF VALVE STUCK IN THE OPEN. REMOVED AND REPLACED THE CARGO JET PUMP SHUTOFF VALVE REF DC-10MM 21-41-03-2. FOUND LOOPS IN NR 2 PYLON BAD. REMOVED AND REPLACED LOOPS D1-29, D1-28B, D1-28CREF: DC-10-30 MM 36-23-02-4. PERFORMED MANIFOLD FAILURE SYSTEM TEST PER DC10-30 MM 36-23-00-2, WITH NO DEFECTS NOTED. OPS AND LEAK CHECK OF CARGO JET PUMP SHUTOFF VALVE PER DC-10-30 MM 21-41-03-2, CHECKS GOOD. PRESS DECAY CHECK PER THE JRH CHECKS GOOD. RETURNED TO SE

Part: SEAL — OUT OF POSITION (CARGO DOOR) · airframe 73,135 hrs · 21,216 cycles

APPROX 7,000 FT, ACFT FAILED PRESSURIZATION & CENTER ACCESS COMPT FLOW OFF LIGHT ILLUMINATED. RAN RED TABS ON AND AT APPROX 3K ACFT REGAINED PRESSURIZATION AND LIGHT WENT OUT. RETURNED TO BASE. PERFORMED ALL DOORS SEALS INSPECTION. AFTER PRESSURIZING A/C FOUND 2 FEET OF SEAL OUT OF TRACK ON FWD LOWER CARGO DOOR AFT CORNER, ALSO AROUND 10 INCHES OFF TRA CK FROM MAIN CARGO DOOR LWR AFT CORNER. RE-INSTALLED SEALS AND PERFORMED A/C PRESS PER JRH CHP 7-1. GROUND OPS CKS GOOD.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

MAIN CABIN AT FS 835 - 870 AT LBL 8.5 SEAT TRACK HAS CORROSION AFT INBOARD FLANGE. REMOVED CORRECTED SECTION OF SEAT TRACK. FABRICATED NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC10 SRM 53-42-01 VOL 1, DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-21-01 VOL 2.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2.

Part: HINGE — DAMAGED (TE FLAPS) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

REWORK BARREL NUT HOLE NR 10 IS LARGER THAN CMM LIMIT ON RT WING O/B-I/B FLAP HINGE FITTING. CLARIFICATION OF N01776. N01776 & N02167 REMOVED BUSHING & OPEN BORE TO .748 IAW DC10 MM 57-44-08, HEAT TREATED BUSHING MAT'L IAW DPS 5.00-2 & DPS 1.05.5, ETCHED BORE IAW DC10 CMM 20-11-02. HFEC BORE IAW DC 10 NDT MANUAL PT6 51-00-01 NO CRACKS, ROTO PEENED BORE IAW DC10 CMM 20-11-01, FABRICATED BUSHING IAW DC 10 CMM 57-44-08. INSTALLED BUSHING IAW DC10 CMM 57-44-08 AND EO 8-5710-75068.

Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

PITTING INSIDE SEAL GROOVE/MATING SURFACE ON FUEL TANK ACCESS PANEL 638BB. PITTING OUT OF LIMITS. REPLACED PANEL 638BB IAW DC10 MM 28-00-00-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

AFT LWR CARGO COMPARTMENT FS 1971 AFT SIDE OF FRAME BETWEEN L-51L AND L-51R SHEAR TIE IS CORRODED. REMOVED SHEAR TIE, INTERCOSTAL, CLIPS AND SPLICE FRAME. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW SHEAR TIE, INTERCOSTAL CLIP AND SPLICE FRAME IAW DC10 SRM 51-35-01 VOL 2 AND 51-33-01 VOL 2.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

CORROSION ON FUEL TANK ACCESS 534CB, AT MATING SURFACE. RECEIVED NEW PANEL P/N ARB0872-507, TO BE INSTALLED ON WORK CARD 575I5503-01.

Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

REWORK RT OUTBD FLAP OUTBD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION WRITTEN FOR CLARIFICATION JPF. REMOVED BUSHING & CORROSION IAW DC10 CMM 57-44-09, FINAL HOLE SIZE 1.192, FOUND OUT OF LIMITS. FABRICATED BUSHING IAW DC10 CMM 57-44-09 AND EO 8-5710-75066. HEAT TREATED BUSHING IAW DPS 5.00.2 & DPS 1.05.5. MPI BUSHING IAW DPS 4.204, NO CRACKS NOTED. CAD PLATED BUSHING PER QQ P 416 TYPE Z CLASS 2 BY VENDOR PO433296. HFEC BORE IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. ETCH BORE IAW CMM 20-11-02, NO CORROSION NOTED. PEENED BORE IAW DC10 CMM 57044-09 & 20-11-01. PRIMED BORE IAW DC10 CMM57-44-09. INSTALLED REPAIR BUSHING IAW DC10 CMM 57-44-09 & EA 8-5710-75066.

Part: MOUNT — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

DURING C-CHECK INSPECTION, CORROSION WAS FOUND IN THE CENTER BORE OF THE ANB7016-6 RT INBOARD FLAP DRIVE BEARING MOUNT BORE. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.0210 INCH DIA. REMOVED FITTING IAW DC10 SRM 51-31-00 VOL II. REMOVED CORROSION IAW DC10 SRM 57-20-00 VOL 1. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-75080 AND DC10 SRM 57-20-00 VOL 1. CORROSION LEVEL 1. FITTING INSTALLATION COMPLETED ON FEDEX CARD N02040.

Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING AND FOUND BORE TO BE 2.322, OUT OF LIMITS IAW DC10 CMM 57-44-08. HEAT TREATED MATERIAL FOR BUSHING IAW DPS 5.00.2 & DPS 1.05.5. PERFORMED HFEC IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. FABRICATED OVERSIZED BUSHING IAW DC10 CMM 57-44-08. PERFORMED MPI IAW DPS 4.704 NO CRACKS, ETCHED BORE, NO CORROSION FOUND, PEENED HOLES IAW DC10 CMM 20-11-01 AND 20-11-02. CAD PLATED BUSHING IAW 57-44-08 PER QQP-416, TYPE 2 CLASS 2. PRIMED BORE AND INSTALLED BUSHING IAW CMM 57-44-08. FINAL BORE ID 2.2505. LEVEL 2 CORRODED BORE NR 4.

Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING C-CHECK INSPECTION CORROSION WAS FOUND IN THE INNER BORE OF ARC0538-501 OUTBOARD FLAP FORWARD CLEVIS FITTING. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.220 INCH IN THE RIGHT FITTING AND 1.200 IN THE LT FITTING. REAMED FITTING MOUNT HOLES IAW DAC CMM 57-44-07 TO 1.220, ALL CORROSION REMOVED. FABRICATED REPAIR BUSHING IAW DWG 54928911N16-022 AND EO 8-5710-75084.

Part: HINGE — CORRODED (ZONE 600) · airframe 73,027 hrs · 21,172 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING EO 5750-7-5000, CORROSION WAS FOUND IN THE 2 RIGHT OUTBOARD FLAP HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1.192 INCH AND 1.908 INCH. REMOVED CORROSION, FABRICATED BUSHINGS AND INSTALLED BUSHINGS IAW DC10 CMM 57-44-09 AND EA 8- 5710-75066.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING AUCT MOUNT POINT HOLE HAS CORROSION AT BORE 5 A&B. DURING EO 8-5750-7-5000, CORROSION WAS FOUND IN THE 2 RT FLAP OUTBOARD HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1.192 AND 1.1908. REAMED BORES TO REMOVE CORROSION, FABRICATED AND INSTALLED OVERSIZED BUSHINGS IAW DC 10 CMM 57-44-09 AND EO 8-5710-75066.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REWORK LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REMOVED BUSHING AND CORROSION IAW CMM 57-44-8. FABRICATED AND INSTALLED OVERSIZED BUSHING IAW DC10 CMM 57-44-08 AND EA8-5710-75068.

Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,027 hrs · 21,172 cycles

REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING, REPAIRED HINGE PER FEDEX EA 8-5710-75067 DATED 01-23-04.

Part: PRESSURE SWITCH — FAILED (PNEUMATIC SYS) · airframe 70,584 hrs · 20,361 cycles

ON TAKEOFF, WITH WING ANTI-ICE ON NR 1, PNEUMATIC FAIL LIGHT ILLUMINATED, RAN RED TABS IAW TAFI, FOUND PRESSURE SWITCH FAULT, LEFT WING. REPLACED MANIFOLD FAILURE DET PRESSURE SWITCH. OPERATIONS AND LEAK CHECK, GOOD IAW MM.

Part: SUPPORT — CRACKED (LT WING) · airframe 69,827 hrs · 20,108 cycles

FOUND CRACK INDICATION ON MLG RETRACT CYLINDER SUPPORT FRAME AFT HANGER SUPPORT. R&R SUPPORT FRAME ON LT MLG PER EO 8-5740-7-4312 P3 SEQ NR 00009.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 31,811 hrs · 6,964 cycles

INTERMITTENT PILOT MASTER CAUTION LIGHT WITH NO OTHER IND. REMOVED AND REPLACED MASTER WARN CONTROLLER. GROUND CHECK NORM.

Part: CONTROLLER — INOPERATIVE (ANTI-ICE SYS)

ON ROTATION ENG 2 A/I DISAGREE LIGHT ILLUM (SW OFF) COMPL W/RED TABS. FLT RECORDER CAUTION LIGHT ILLUM ON S/O PNL AND AOA HT C/B POPPED. REMOVED AND REPLACED HEATER CONTROLLER/MONITOR PER MM 30-35-01-2. PER OPS TEST PER 30-30-00-2, SYS OPS NORM. WRI ASSIGNED TO NR 2 A/I (30-20-7682) WRI ASSIGNED TO FLT REC LT (31-30-7681).

Part: PUSHROD — BENT (SPOILER) · airframe 66,941 hrs · 19,126 cycles

SPOILERS WOULD NOT DEPLOY INFLT. HANDLE WOULD NOT MOVE MORE THAN 1/3 DOWN. REMOVED AND REPLACED THROTTLE INTERLOCK PUSHROD ASSY PER MM 27-62-01-2-1. SYS CK NORM. OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE)

ON PUSHBACK AT GATE 3 EWR, HEARD LOUD NOISE ON LEFT SIDE OF ACFT, DETERMINED THAT ACFT HAD BEEN PUSH INTO LOAD DOCK. PULL CVR D/B. ACFT TOWED TO GATE, INTERIM REPAIR WAS COMPLETED PER EA 8-5320-49721. *S/D* REPAIR PER EA 8-5310-46689.

Part: GEAR HANDLE — LACK OF LUBE (COCKPIT)

LANDING GEAR HANDLE WAS PLACED IN DOWN POS. ALL 8 LANDING GEAR POSITION INDICATORS STAYED RED. RECYCLED LANDING GEAR HANDLE, NO HELP. RED TAB PROCEDURE FOLLOWED. ATL LANDING GEAR EXTENSION HANDLE WAS PULLED. ALL 8 GEAR POSITION INDICATORS WENT GREEN. CLEANED AND LUBED HANDLE ASSY PER M/M 32-31-02-7. FOUND PUSH PULL CABLES OUT OF ADJ. RIGGED CABLES PER MM 32-31-02-2, OPS CKS GOOD.

Part: SWITCH — FAILED (LANDING GEAR)

LANDING GEAR HANDLE WAS PLACED DOWN, ALL INDICATORS REMAINED RED. LANDING GEAR HANDLE WAS CYCLED TWICE, NO JOY. ALTERNATE EXTENSION HANDLES WERE ACTUATED IN ACCORDANCE WITH ED TAB PROCEDURES. ALL INDICATORS WENT GREEN. REPEAT. INSTALLED GEAR PINS, REPLACED LANDING GEAR CONTROL SWITCH PER M/M 32-61-04-2 PG 201-203.98743. OPERATED GEAR HANDLE SEVERAL TIMES. GEAR LIGHT WERE RED WITH HANDLE UP AND GREEN WITH HANDLE DOWN. OK FOR SERVICE. REMOVED GEAR PINS.

Part: CONTROL UNIT — FAILED (LANDING GEAR)

ON FINAL LANDING GEAR CAME DOWN BUT NO GREEN GEAR LIGHT DOWN LIGHT. RECYCLED LANDING GEAR UP AND THAN DOWN AND THAN RECEIVED 4 GREEN LIGHTS. REMOVED AND REPLACED CONTROL UNIT PER M/M 32-61-01, BITE TEST GOOD.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR)

AFTER TAKEOFF, GEAR HANDLE UP GAVE RED LEFT MAIN INDICATION ON F/O PANEL AND UP FRONT. RAN RED TAB, NO HELP. CHECKED WIRING INTEGRITY FROM S3-682 TERMINAL 4 AND 5 (PROX ELETR UNIT) AS PER WDM 32-61-04 PG 2, FOUND OK. REMOVED AND REPLACED PROXIMITY ELECTRONIC UNIT PER M/M 32-61-01-2.

Part: PROX SENSOR — DAMAGED (LT MLG)

BOTH FRONT AND BACK LEFT MAIN GEAR INDICATOR UNSAFE LIGHTS ILLUMINATED AFTER TAKEOFF. FOLLOWED RED TAB. FRONT LIGHT EXTINGUISED, BACK LIGHT REMAINED ILLUM UNTIL LEVEL OFF. PRIOR TO LANDING BOTH FRONT AND BACK LIGHT MAIN GEAR UNSAFE LIGHTS ILLUM, UNTIL LANDING GEAR WAS LOWERED. ALL GEAR LTS IN GREEN UPON LANDING. FOUND LEFT MAIN GEAR DOOR PROX SWITCH (SENSOR) BADLY SCRATCHED. REMOVED AND REPLACED AND ADJUSTED SWITCH PER M/M 32-61-03. PERFORMED PROX BOX TEST, FOUND OK.

Part: THROTTLE ROD — FAILED (NR 1 ENGINE)

97-0200 - NR 1 ENGINE ROLLED BACK. NR 1 ENGINE WAS SHUTDOWN IN ACCORDANCE WITH RED TABS. ALT FL310. N1 50.0 PERCENT EGT 380 N2 75 PERCENT FF 2160. NOTE: WENT TO IDLE NO THROTTLE RESPONSE.OPEN FAN COWL ON NR 1 ENG AND FOUND THE THROTTLE ROD DISCONNECTED FROM FUEL CONTROL WITH BOLT AND NUT IN COWLING. REPLACED BOLT ASSY FOR THROTTLE ROD AND C PINNED AND TORQUE STRIPPED. VISUALLY INSPECTED NR 1 ENG FOR OTHER DEFECTS. NONE NOTED. CHECKED RIGGING AND RAN THROTTLE THROUGH SEVERAL TIMES. CKS GOOD FOR SERVICE.

Part: LANDING GEAR — DAMAGED (NLG)

HARD LANDING, A HARD LANDING INSP WAS PERFORMED. THE INSP FOUND NOSE LAND GEAR COVERED IN 5605. MX DISASSEMBLED AND REPACKED SAME. LEFT MAIN TIRES NR 5 AND NR 6 BLOWN AND WHEELS BENT. THE NR 1, 2, 5 AND 6 WHEELS TIRES AND BRAKES WERE REPLACED. LEFT STRUT SCRAPER RING FOUND HANGING OUT OF STRUT. THE LEFT STRUT WAS DISASSEMBLED, INSP AND REPACKED. THE STRUT LOWER CYLINDER METERING ROD HAD NUMEROUS DENTS AND WAS REPLACED. THE NR 2 WHEEL AXLE SLEEVE HAD SPUN ON THE AXLE AND WAS REPLACED.

Part: CONTROL CABLE — CUT (LT LE SLAT)

ON POSTFLT CHECK, FOUND LT WING OUTBOARD SLAT NR 3 DRIVE EXTEND CABLE HAD BEEN CUT OFF. REMOVED AND REPLACED LEFT SLAT NR 3 DRIVE EXTEND CABLE PER MM 27-89-03-4 AND ADJUSTED SLAT SYSTEM PER MM 27-80-00-5. REMOVED AND REPLACED DAMAGED METAL SEALS FOR LT SLAT BETWEEN NR 3 TO NR 4, NR 4 TO NR 5. INSPECTED ALL WING SLAT SYSTEM AND FOUND NO DAMAGE. ALL SYSTEM TEST OK PER MM 27-80-00.

Part: ACTUATOR — MALFUNCTIONED (NLG)

ON TAKEOFF, THE NOSE LIGHT ON BOTH PANELS REMAINS RED. HYD SYS 3 WAS NORMAL, RAN THE RED TAB PROCEDURES AND LANDING GEAR SHOWED 4 GEAR LIGHT WITH GEAR HANDLE DOWN. TRIED TO RAISE THE GEAR AGAIN WITH NO SUCCESS, RED LIGHT STILL ON WITH HANDLE UP. LOWERED GEAR AND LANDED. REPLACED NOSE GEAR RETRACT CYLINDER AND PROXIMITY CONTROL BOX FOR PRECAUTIONALLY.

Part: LOCK SENSOR — MALFUNCTIONED (NLG)

ON T/O, NOSE GEAR WOULD NOT INDICATE UP AND LOCKED ON BOTH FRONT AND S/OS PANEL. CYCLED GEAR SEVERAL TIMES WITH NO UP AND LOCKED INDICATION. DOWN AND LOCKED OK, COMPLIED WITH RED TABS, DUMPED LANDED. VISUALLY INSPECTED NOSE GEAR AND DOOR, NO DAMAGED NOSE LANDING GEAR AREA. JACKED NOSE GEAR, CYCLED NOSE RETRACTION CHECKS OPS NORMAL WITH BOTH PRIM AND ALT IND PER MM32-20-00, MM32-60-00. REPLACED NOSE GEAR LOCKED SENSOR LT AND RT PER MM32-60-00 AND 32-61-00 GEAR RETRACTION BOTHS PRIM AND ALT SYS NORMAL CPN 0023070.

Part: PROX BOX — MALFUNCTIONED (NLG)

ON T/O, NOSE GEAR INDICATED NO RETRACT, BOTH INDICATIONS. ON LANDING NR 2 T/R WOULD NOT DEPLOY. RAN APPROPRIATE CHECKLIST, DUMPED FUEL AND RETURNED TO ANC. INSPECTED NOSE GEAR, PROX ELECTRONIC UNIT FROM A/C 315, INSTALLED IN A/C 302. JACKED NOSE GEAR, CYCLED NOSE GEAR SEVERAL TIMES. ALL INDICATION NORMAL, OK FOR SERVICE SEE AML 603806 FOR T/R NR 2.

Part: DOOR — OUT OF ADJUST (CABIN)

VCP: BOTH CABIN DOORS DID NOT SEAL AND A/C WOULD NOT PRESSURIZE. ADJUSTED DOORS PER MM 52-11-00, PG 520. PRESSURED A/C USING APU, LEAK CHECKED OK.

Part: INDICATION — MALFUNCTIONED (NLG)

AFTER GO-AROUND, NOSE GEAR RED LIGHT ON AT BOTH PANELS WITH HANDLE UP, HYD SYS-3 NORMAL. PUT HANDLE DOWN AND BOTH LIGHTS GREEN ON NOSE GEAR. PERFORMED BITE CHECK ON PROXIMITY BOX, FOUND NO DEFECTS. PERFORMED GEAR RETRACTION TEST PER MM 32-60-00, UNABLE TO DUPLICATE PROBLEM. SWUNG GEAR 6 TIMES, OPS CK GOOD.

Part: CYLINDER — FAILED (NLG STEERING)

LOST SYS 3 HYD AFTER LANDING, MADE TURN ON TO TAXIWAY LOST ALL FLUID CONFIRMED EXTERNAL LEAK FROM A/C ON GROUND. REMOVED AND REPLACED NOSEWHEEL STEERING CYLINDER PER MM 32-52-01. RESERVICED NR 3 HYDRO SYS TO FULL, ALL SYSTEMS CHECK GOOD.

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

LANDING GEAR TOOK EXCESSIVE AMOUNT OF TIME TO EXTEND. JACKED A/C AS PER MM 7-10-00, LUBED LANDING GEAR, CLEANED LANDING GEAR SELECTOR LEVER IN COCKPIT AND CYCLED LANDING GEAR AS PER MM 32-30-00. CHECKED OK AND NO DEFECTS FOUND.