N279UP

Part: NONE — FAILED (LANDING GEAR) · airframe 78,310 hrs · 16,006 cycles

INSPECTION TYPE:NA**EMERG DECLARED** ANTI SKIDE R FAIL DURING FIRST APPROACH WENT AROUND AND ACCOMPLISH QRH PROCEDURE 2ND APPROACH NO INDICATION NON EVENTFUL LANDINGACCOMPLISHED FIMM 32 40 12 00 FIG 110 BLOCKS 1,2, AND 3 FOUND FAULT LAST FLIGHT A/S VALVE SYS 1 3 AND A/S VALVE SYS 1 7 SHOT WIRES REF WDM 32 45 03 FROM R5-1136B PIN 10A TO R5-1336A PIN 3B NO FAULTS AND R5-1136B PIN 8A TO R5-1136 A PIN 3B NO FAULT REPLACED ANTI-SKID CONTROL UNIT REF AMM 32 43 01 401

Part: NONE — NONE (CABIN) · airframe 78,215 hrs · 15,944 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHTING TEST FAILED. "EMER LT BAT 1 LO" MESSAGE.REPLACED EMER LIGHTING BATT PWR SUPPLY. SYS OPS NORMAL. REF AMM 33-51-01.

Part: SLEEVE — DAMAGED (#1 ENG I/B) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:SV#1 ENG. I/B T/R HAS DAMAGED L/E AT 3 OCLOCK POSTIONREMOVED AND REPLACED #1 ENG. I/B T/R SLEEVE IAW MD 11 AMM 78-31-22-00-868 AND AMM 78-31-22-400-868 PN. 221-0503-524 AND SN. 318

Part: LANDING GEAR — NONE (LANDING GEAR) · airframe 78,180 hrs · 15,913 cycles

ATB SDR FILED OPEN*NO EMERG DEC'D* A/C LANDED W/OUT INCIDENT*AFTER T/O ON INTIAL CLIMB OUT, RAISED GEAR THEN GOT" LANDING GEAR" AURAL WARNING. ALL GEAR INDICATORS SHOWED UP GEAR. T/S 31-51-22-00 BLOCK 8 TO EXAMINE CONNECTOR P1-1111. PERFORMED RINGS OUTS FOR CONNECTOR P1-111 IN REF TO MD-11 WDM 27-54-01, 34-55-01, 32-62-01, RING OUTS GOOD. RECONNECTED P1-1111 IN REF TO MD-11 SWPM 20-31-00. PERFORMED LANDING GEAR POSITION WARNING OPERATIONAL TEST WITH AIRCRAFT ON JACKS IAW MD-11 AMM 32-62-00-700-801, OPS CHECK GOOD.

Part: SUPPORT ANGLE — NONE (LT WING) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:1CLT WING O/B FLAP PANEL T/ESUPPORT ANGLE CRACK AT I/B HINGE.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW DWG # ARC2149 AND SRM 51-31-01,51-35-01 (MINOR).

Part: STIFFENER — NONE (AFT CARGO) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:C4AFT CARGO STEP-UP HAS A CRACK STIFFENER AT STA 1841 AND LONGERON 48R.REMOVED,FAB, REPLACED CRACK STIFFENER IAW DWG AGA7170 AND SRM 51-33-01 (MINOR)

Part: STIFFENER — NONE (AFT CARGO) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:C4AFT CARGO STEP-UP HAS A CRACK STIFFENER AT STA 1841 AND LONGERON 49L.REMOVED,FAB, REPLACED CRACK STIFFENER IAW AGA7170 DWG AND SRM 51-33-01

Part: NONE — CORRODED (RT WING O/B FLAP) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:1CRT WING O/B FLAP I/B HINGE BRACKET LOWER LUG HOLE HAS CORROSION AT STA. XW 486.403.REPAIRED CORRODED HINGE BRACKET ASSY. IAW VT-SAA E.A. 011-5740-01-A9481 REV I/R AND UPS EO MD11-5740-82804-A (MINOR).

Part: STIFFENER — NONE (AFT CARGO) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:C4AFT CARGO STEP-UP HAS A CRACK STIFFENER STA 1841 AND LONGERON 47R.REMOVED,FAB,REPLACED CRACK STIFFENER IN THE AFT CAROG AT STA 1841 AND LONGERON 47R IAW SRM 51-31-01 (MINOR)

Part: FLAP — CRACKED (LT WING) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:1CLH O/B FLAP I/B INTERNAL ATTACH FITTING IS CRACK.REMOVED AND REPLACED FLAP ASSY. IAW AMM 27-50-30-000-801 AND AMM 27-50-30-400-802 (MINOR).

Part: SKIN — NONE (L/H WING) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:2CL/H WING L/E SKIN HAS A TEMPORARY REPAIR AT STA XDLE= 330.2745 THAT NEEDS TO BE REPLACED.REMOVED TEMPORARY REPAIR AND REPLACED WITH A PERMANENT REPAIR IAW VT-SAA EA 011-5730-01-A9478 REV. I/R AND UPS EO MD11-5730-82828-A. (MAJOR) REF. FAA FORM 8100-9 BY S. KANG (AR605667) DATED 02/11/2022.

Part: SKIN — CORRODED (CENTER WING BOX) · airframe 78,180 hrs · 15,913 cycles

INSPECTION TYPE:1CMAIN CABIN CENTER WING BOX SKIN HAS CORROSION AT STRINGER 15 BETWEEN XCW=-91 TO XCW=-102.REPAIRED CORRODED CENTER WING BOX SKIN IAW VT-SAA EA011-5730-01-A9475 REV I/R AND UPS EO MD11-5730-82767-A (MINOR)

Part: DOOR — CRACKED (A/C COMP.) · airframe 78,176 hrs · 15,911 cycles

INSPECTION TYPE:2CL/H FWD. A/C COMP. DOOR SKIN HAS CRACKES ON UPPER EDGE OF DOOR.REPAIRED L/H A/C ,COMP. DOOR SKIN IAW SRM 52-40-01 REPAIR 1 FIG. 201. (MINOR)

Part: NONE — NONE (RT WING) · airframe 78,176 hrs · 15,911 cycles

INSPECTION TYPE:1CRT WING T/E LOWER ACCESS DOOR SILL CRACK AT I/B STA. XORS 480.REMOVED AND REPLACED CRACKED SILL IAW SRM 51-33-01 (MINOR).

Part: INTERCOSTAL — DAMAGED (FWD. CARGO) · airframe 78,176 hrs · 15,911 cycles

INSPECTION TYPE:C2LOWER FWD. CARGO CEILING SUPPORT INTERCOSTAL AT STA. X= -108.00 HAS DAMAGED HOLES.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ADA7753 AND SRM 51-35-01. (MINOR)

Part: NONE — NONE (DOORS) · airframe 77,914 hrs · 15,782 cycles

INSPECTION TYPE:NAR1 DOOR SLIDE DISARM LIGHT DOES NOT ILLUMINATE WHEN DOOR IS UNARMEDRELAMPED DOOR DISARM BULBS AS REQUIRED OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME REF AMM 25 61 15

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,741 hrs · 15,675 cycles

EMER LT BAT 1 LO, DURING EMERGENCY LIGHT TEST. DEFERRED PER MEL 33-50-4. DMP C/W. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01-400-802. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 77,665 hrs · 15,627 cycles

INSPECTION TYPE:N/AAIRCRAFT SEEMS OT HAVE DIRTY SOCK. ODOR NOTICED ON CLIMB OUT BUT NOT OFF A PETROLEUM OR ELECTRICAL NATUREREMOVED AND REPLACED ALL 3 COALESCER BAGS IAW MD11 AMM 21-54-05-201 OPS NORMAL

Part: PANEL — BROKEN (L1 DOOR) · airframe 77,636 hrs · 15,611 cycles

INSPECTION TYPE:N/AFUELING REPORTED PANELS FALLING FROM L1 DOORFOUND SLIDING CEILING PANEL & LIGHT BALAST TO BE DAMAGED & TINSTION SPRING BROKEN. R&R SLIDING PANEL AND TINSTION SPRING PER AMM 25-23-3 & R&R SLIDING PANEL LIGHT BALAST PER AMM 33-22-05. BOTH OPS CHECK GOOD PER BOTH AMM'S. A/C GOOD TO RETURN TO SERVICE ESR 25-23-03-27-520/ 33-22-01-05-170J/ 25-23-

Part: UNKNOWN — NOISE (L1 DOOR) · airframe 77,134 hrs · 15,365 cycles

INSPECTION TYPE:NALOUD SQUEAKING/SCRATCHING SOUND ABOVE L1 DOOR ON TAXI ININSPECTED L1 DOOR AREA HIGH & LOW. ALSO ABOVE SLIDING CEILING PANEL. NO ABNORMALIES FOIUND. TRACH CANDOOR IN GALLEY WAS OPEN & FLOPPING . SUSPECT SAME. OK FOR SERVICE. REF MM 52 00 00

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 77,115 hrs · 15,353 cycles

EMERGENCY LITE TEST SHOWS LOW BATTERY. TRANSFERRED TO MEL 33-50-4 PER MMOC DMP C/W CANNON PLUG CAPED & STOWED.REPLACED EMERGENCY LIGHTING BATT WITH REF AMM 33-51-01-000-802 005. TEST GOOD PER AMM 33-51-01-700-802. DMP REVERSED PLACARD REMOVED. THIS CLEARS M738924.

Part: ACTUATOR — MALFUNCTIONED (AILERONS) · airframe 76,986 hrs · 15,294 cycles

INSPECTION TYPE:NA**ATB- NO EMERG DECLARED-NO EMERG EQUIP USED-LANDED UNEVENTFULLY-AC TAKEN OOS**. AFTER T/O CREW CONTACTED FLIGHT CONTROL WITH A LEVEL 2 AILERON DEFLECT DISAGREE MESSAGE. CREW WORKED CHK LIST TO NO AVAIL. LATER CREW CONTACTED FLT CNTRL ABOUT AUTO PILOT FAILURE.REMOVED & REPLACED R/H OUTBOARD AILERON DROOP ACTUATOR IAW AMM 27-16-00-700-801. OPS CHECK GOOD. EFF SOURCE REF: IPC 27-11-30

Part: RELIEF VALVE — RUPTURED (L1 DOOR BOTTLE) · airframe 76,382 hrs · 15,029 cycles

INSPECTION TYPE: NA, ON PREFLIGHT, L1 CREW ENTRY DOOR BELOW GREEN BAND. NEEDS PNEUMATIC SERVICED. PRESSURE RELIEF VALVE RUPTURED DURING SERVICING. R & R FWD LEFT CABIN DOOR EMERGENCY OPEN RESERVOIR AND SERVICED SAW AMM 52-11-35 IPC: 52-11-35-01-001L.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 76,296 hrs · 15,000 cycles

INSPECTION TYPE: N/A. MCD FLOOR PANEL STA 1481-1582 LT SIDE OUTBOARD PANEL. FABRICATED NEW FLOOR PANEL P/N AEA7542-25, IAW EO MD11-5320-27386-C.

Part: ANGLE — CORRODED (NR 2 NACELLE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3LH FWD #2 ENG PICKLE BARREL SUPPORT STRUTURE INSIDE ACCESS PANEL #361EL HAS CORROSION ON AFT ANGLE SUPPORT.REPLACED CORRODED ANGLE SUPPORT AT #2 ENG PICKLE BARREL INSIDE PANEL 361EL IAW SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CORRODED (VERITCAL STAB) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CLOWER VERTICAL STABILIZER INTERCOSTAL IA CORRODED BETWEEN STA. YID= 245 AND YID= 251.REPAIRED CORRODED LOWER VERTICAL STAB INTERCOSTAL BETWQEEN STA. YI=245 TO YID= 251 IAW VT-SAA EA 011-5532-01-A8458 REV. I/R AND UPS EO MD11-5530-77511-A. (MAJOR)

Part: FLOORBEAM — CRACKED (MAIN CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:1C3CMAIN CARGO FLOOR BEAM HAS CRACK AND DENT AT STA Y=979 AND X=-107.REPAIRED FLOOR BEAM AT STA Y=979 AND X=-107 IAW VT-SAA EA # 011-5310-01-A8440-IR AND UPS EO # MD11-5310-77493-A. MAJOR

Part: TEE FITTING — CORRODED (RUDDER) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CLOWER FWD RUDDER R/H T/E BLADE SEAL LANDING TEE HAS CORROSION.REPAIRED LOWER FWD RUDDER R/H BLADE SEAL LANDING TEE CORROSION IAW VT-SAA EA 011-5540-01-A8453 REV. IR AND UPS EO MD11-5540-77501-A. (MAJOR)

Part: TEE FITTING — CORRODED (RUDDER) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CLOWER FWD RUDDER L/H T/E BLADE SEAL TEE HAS CORROSION.REPAIRED LOWER FWD RUDDER L/H T/E BLADE SEAL TEE CORROSION IAW VT-SAA EA 011-5540-01-A8452 REV. IR AND UPS EO MD11-5540-77496-A. (MAJOR)

Part: SKIN — CORRODED (BS 1997-2163) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CRT AFT FUSELAGE SKIN BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERONS 31R - 35R HAS CORROSION.REPAIRED RT AFT FUSLAGE SKIN CORROSION BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERON 31R - 35R IAW VT-SAA EA 011-5330-01-A8459 REV. IR AND UPS EO MD11-5330-77489-A. (MAJOR)

Part: SKIN — CORRODED (BS 2140-2163) · airframe 76,141 hrs · 14,936 cycles

L/H FUSELAGE SKIN HAS CORROSION AROUND HORZ, BODY FAIRING BETWEEN STA. 2140-2163 @ L33L. REPAIRED CORRODED SKIN ON L/H FUSELAGE SKIN BETWEEN STA. 2140-2163 @ L33L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)

Part: SUPPORT BRACKET — BROKEN (RT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, RT WING NR 2 TANK SUPPORT BRACKET AT XORS 97 WAS BROKEN. REPLACED THE SUPPORT BRACKET AT RT WING NR 2 TANK IAW SRM 51-35-01. (MINOR)

Part: SHEAR TIE — CRACKED (BS 1289) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, BLADDER TANK LEFT HAND SIDE SHEAR TIE CRACKED AT LOWER FRAME AT APPROX STA 1289.REMOVED CRACKED SHEARTIE, FABRICATED AND INSTALLED IN LH BLADDER TANK STA 1289 IAW SRM 51-33-01 AND SRM 51-35-01. (MINOR)

Part: SHEAR TIE — CRACKED (BS 1289) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, CENTER WING BLADDER TANK AT RH SIDE HAS SHEAR TIE AT LOWER FRAME WITH A CRACK AT APPROX STA 1289.REMOVED CRACKED SHEARTIE, FABRICATED AND INSTALLED ON RH WING BLADDER TANK AT STA 1289 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)

Part: ANGLE — CRACKED (AFT FUSELAGE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE: C3, ACCESS IN 316 UPPER CEILING RIGHT ABOVE PNEUMATIC DUCT SUPPORT ROD HAS A VERTICAL SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE , FABRICATED AND INSTALLED IN AFT FUSELAGE ACCESS 316 UPPER CEILING IAW SRM 51-33-01 AND DWG AJC7715. ( MINOR)

Part: SKIN — CRACKED (RT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CR/H WING FUEL ACCESS PANEL LANDING HAS 7 FASTENER HOLES WITH CRACKS.REPAIRED R/H WING FUEL ACCESS PANEL (636AB) LANDING IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)

Part: LANDING — CRACKED (LT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3C LEFT WING FUEL ACCESS PANEL (535AB) LANDING HAD 9 FASTENER HOLES WITH CRACKS. REPAIRED THE LT WING FUEL ACCESS PANEL (535AB) LANDING IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LT WING UPPER SKIN HAS CORROSION AROUND A FASTENER HOLE AT XORS 316.9 AND STR 17.ACCOMPLISHED REPAIR ON LH WING SKIN AROUND FASTENER HOLE AT STA XORS 316.9 AND STR 17 IAW EA 011-5730-01-A8448 REV IR AND EO MD11-5730-77434-A. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LEFT WING UPPER SKIN HAS CORROSION AROUND A FASTENER AT APPROX XORS 380 AND REAR SPAR.REPAIRED CORRODED UPPER SKIN AT LH WING AT XORS-380 ABOVE REAR SPAR IAW EA 011-5730-01-A8447 REV IR AND EO MD11-5730-77460-A. (MINOR)

Part: FRAME — BENT (BS 735) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CMAIN CABIN FUSELAGE FRAME AT STA 735 BETWEEN LONGERONS 12R - 13R IS BENT.REPAIRED BENT MAIN CABIN FUSELAGE FRAME AT STA 735 BETWEEN LONGERONS 12R - 13R IAW VT-SAA EA 011-5310-01-A8433 REV. IR AND UPS EO MD11-5310-77478-A. (MAJOR)

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, NR 1 ENG PYLON ABOVE PRECOOLER THE HEAT SHIELD AFT VERTICAL ANGLE IS CRACKED. REPLACED CRACKED VERTICAL ANGLE ON NR 1 PYLON ABOVE PRECOOLER HEAT SHIELD AFT ANGLE IAW SRM 54-05-41 AND SRM 51-31-01. (MINOR)

Part: FORMER — CRACKED (L WING L/E) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LEFT WING FIXED L/E FORMER WAS CRACKED AT XOS 961. REPLACED THE FORMER ASSY AT L/E XOS 961 IAW SRM 51-31-01 (MINOR)

Part: ANGLE — CRACKED (FWD CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, FWD CARGO COMP LT TUNNEL SLOPED PANEL LANDING AT BS 979 IS CRACKED AT BOTTOM. REPLACED CRACKED ANGLE IN FWD CARGO LH TUNNEL AT BS 979 IAW SRM 51-55-01. (MINOR)

Part: ANGLE — CRACKED (FWD CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3FWD CARGO COMP LH TUNNEL SLOPED PANEL LANDING AT STA 919 IS CRACKED AT BOTTOM SIDE.REPLACED CRACKED ANGLE IN FWD CARGO LH TUNNEL AT STA 919 IAW SRM 51-31-01 AND EA 011-5300-01-A8437IR AND EO MD11-5300-77262-A (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3FWD CARGO BILGE INTERCOSTAL CRACKED BETWEEN STA 6-30 AND 6-50 UNDER LH SIDE RAIL.REPLACED CRACKED INTERCOSTAL IN FWD CARGO BILGE BETWEEN STA 6-30 AND 6-50 LH SIDE IAW DWG ACA7049. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3FWD CARGO COMP BILGE AREA INTERCOSTAL BETWEEN STA 6-30 AND 6-50 UNDERNEATH RH SIDE HAS CRACKS AT LIGHTNING HOLES.REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED IN FWD CARGO BILGE BETWEEN STA 6-30 AND 6-50 UNDER RH SIDE RAIL IAW SRM 51-33-01. (MINOR)

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE: C3, FWD CARGO BAY STA 6-70 FLOORBEAM UNDER RT SIDE RAIL HAD A CRACK. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIG 202, REV 67. MAJOR REPAIR.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, NR 1 ENG PYLON ABOVE PRECOOLER THE HEAT SHIELD FWD VERTICAL ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 54-05-41 AND SRM 51-31-01. (MINOR)

Part: SKIN — CRACKED (LT WING LE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LT WING FIXED LE SKIN WAS CRACKED AT THE NR 12 SLAT TRACK CUTOUT. REPAIRED CRACKED SKIN ON LT WING L/E SLAT TRACK CUTOUT XOS 776 IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 67. (MAJOR)

Part: FLOOR SUPPORT — CRACKED (CENTER CARGO) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3C, CENTER CARGO LT SIDE FLOORBOARD LANDING ANGLE WAS CRACKED AT BS 1521. REMOVED, FABRICATED AND REPLACED THE FLOOR SUPPORT ANGLE IA DWG. AEA0341 AND SRM 51-31.01. (MINOR)

Part: FRAME — WORN (TAIL CONE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, TAIL CONE LT CANTED FRAME STA 2165.062 WORN THROUGH. REPAIRED THE FRAME IAW SRM 53-80-07, REPAIR 1, FIG 201.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CL/H WING O/B FLAP I/B T/E IS DELAMINATED BETWEEN STA. XOF= 574 TO 495.REPAIRED DELAMINATED L/H WING O/B FLAP IAW VT-SAA EA 011-5753-01-A8455 REV. I/R AND UPS EO MD11-5750-77481-A. (MINOR)

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LT WING O/B FLAP I/B AFT HINGE FAIRING I/B LOWER T ANGLE IS CRACKED,REPLACED CRACKED T ANGLE AT LT WING O/B FLAP I/B AFT HIMGE IAW SRM 51-31-01. (MINOR)

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, RT INBD FLAP VANE HAD FOUR AREAS OF DELAMINATION AT LOWER SURFACE. REPLACED DELAMINATED FLAP VANE IAW AMM 27-50-22.

Part: SKIN — GOUGED (LT AILERON) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3CLT WING I/B AILERON LOWER SKIN IS GOUGED.REPAIRED GOUGED LT WING I/B AILERON LOWER SKIN IAW VT-SAA EA 011-5751-01-A8475 REV. IR AND UPS EO MD11-5750-77512-A. (MAJOR)

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, LEFT WING OTBD FLAP T/E WEDGE INBD SECTION HAD A LARGE AREA OF DELAMINATION. REPAIRED THE FLAP T/E WEDGE IAW 57-50-80, REPAIR 1, 6" X 5.75" PERMANENT REPAIR. (MINOR)

Part: SKIN — CORRODED (RT WING) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:C3, RT WING UPPER T/E SKIN PANEL LIFTING AT O/B END JUST FWD OF O/B AILERON. ACCOMPLISHED PERMANENT REPAIR ON CORRODED SKIN AT RIGHT WING REAR SPAR UPPER CAP STA XORS 1042 IAW EA 011-5710-01-A8443, REV IR, AND EO MD11-5710-77400-A. (MINOR)

Part: ANGLE — CRACKED (RT WING TE) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3C, RT WING LWR T/E REAR SPAR T ANGLE (SILL) CRACKED JUST FWD OF I/B AILERON.ACCOMPLISHED EA 011-5720-01-A8438 REV IR AND E0 MD11-5720-77383-A ON RH WING T/E LOWER ACCESS DOOR SILL STA XORS=420. (MINOR)

Part: PANEL — CRACKED (LT MLG WW) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3C, LEFT MLG TRUNNION TO WING T/E BLISTER PANEL IS CRACKED.REMOVED AND REPLACED PANEL IAW SRM 51-31-01. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 76,141 hrs · 14,936 cycles

INSPECTION TYPE:3C#1 ENG.O/B T/R AFT FIXED INNER BARREL UPPER SKIN IS CRACKED AT STA. NAC= 194.5.REPAIRED #1 ENG. O/B T/R SKIN IAW VT-SAA EA 011-7830-01-A8446 REV, I/R AND UPS EO MD11-7830-77337-A. (MINOR)

Part: SPRING — BROKEN (L1 DOOR) · airframe 74,772 hrs · 14,378 cycles

INSPECTION TYPE:N/AREF M685305 L-1 PASS DOOR DRIVE CABLEREVERSED DMP. R&R BROKEN TENSION SPRING & INSTALLED NEW CABLE ASSY. REF AMM 52-11-03. OPS CK GOOD. THIS CLEARS M685305

Part: SPRING — BROKEN (L1 DOOR) · airframe 74,760 hrs · 14,370 cycles

CABLE HANGING FROM LEFT SIDE OF L1 DOOR. R/R BROKEN TENSION SPRING & INSTALLED NEW CABLE ASSY. IAWAMM 52-11-03. OPS CK GOOD.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 74,442 hrs · 14,208 cycles

INSPECTION TYPE:N/A ON PREFLIGHT EMERG LT TEST RECEIVED "EMERG LT BAT 1 LO". DEFERRED #1 EMERGENCY LIGHT BATTERY PER MEL 33-50-4 C/W DMP. **SUPPLEMENTAL SDR** REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY UNIT PER MM 33-51-00. OPS CK OK. THIS CLEARS M676092

Part: ACTUATOR — FAULTY (L1 DOOR) · airframe 74,121 hrs · 14,121 cycles

INSPECTION TYPE:NA L1 PASSENGER DOOR DOES NOT CLOSE ON SWITCH COMMAND. L1 PASSENGER DOOR ELECTRICAL ACTUATOR CLOSE LIMIT SWITCH INOP. ITEM DEFERRED PER MEL 52-10-1-2-0-1. DOOR DEACTIVATED ELECTRICAL BY CB PULLED. PLACARD INSTALLED, DMI 67313 OPENED.T/S PER WDM 52-11-01 P1 FOUND R2-177 L FWD DOOR ACTUATOR FAULTY. R/R R2-177 AS PER WDM 52-11-01P1 AND PERFORMED OPS TEST L1 DOOR AS PER AMM 52-11-02/501 FOUND SATIS WITH NO FAULT NOTED. THIS M670313 CLOSED. PLACARD REMOVED. DMP REVERSED.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 73,978 hrs · 14,082 cycles

INSPECTION TYPE:NAR1 DOOR PRE CHARGE BOTTLE LOWSVC R1 DOOR BOTTLE PER MD11 AMM 52-10-01. LEAKS CKS GOOD. A/C OK FOR SVC

Part: ADC — MALFUNCTIONED (NR 1) · airframe 73,926 hrs · 14,059 cycles

AIR TURN BACK - ON TAKEOFF CAPT'S AIRSPEED STAGNATED AT 80 KTS, DECREASED THEN INCREASE WITH ALTITUDE. AIRSPEED UNRELIABLE - CHECKLIST ACCOMPLISHED. CAPC 1 DETERMINED TO BE FAULTY.REMOVED AND REPLACED #1 AIR DATA COMPUTER PER MM 34-16-01-401. OPS CHECK NORMAL PER MM 34-16-01-501 IPC 34-16-01-01 ITEM 055.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 73,926 hrs · 14,059 cycles

AFT BULK CARGO DOOR LWR AFT CORNER DEFLECTED.REPAIRED IAW EO MD11-5230-70321-B.

Part: DOOR — ERRATIC (L1) · airframe 73,926 hrs · 14,059 cycles

L-1 ENTRY DOOR ERRATIC OPERATION INTERMITTENTLY OPERATES IN OPPOSITE OF COMMANDED POSITION AND INTERMITTENLTY SIEZES UP. WILL NOT GO UP OR DOWN . CAN HEAR MOTOR "HUM"Ï¿½AFTER SWITCH COMMANDED OFF.FOUND 115V MISSING FROM RELAY R2-177, LEGS A3 AND C1, REMOVED AND REPLACED R2-177 REF WDM 52-11-01, SWPM 20-20-03 NO HELP. R&R'D L2 DOOR ACTUATOR PER MD11 AMM 52-11-01. OPS NORMAL IPC 52-11-01-20.

Part: BOTTLE — EMPTY (CREW ENTRY) · airframe 73,520 hrs · 13,935 cycles

LOAD PLANNING REPORTS LH CREW DOOR WILL NOT OPEN. FOUND LH CREW DOOR PARTIALLY OPEN AND EMERGENCY LEVER DEPLOYEDMANUALLY OPENED LH DOOR AND RESERVICED PASSENGER DOOR PNEUMATIC STORAGE SYSTEM REF MD11 AMM 52-11-02-010-806 AND 12-25-04-600-801 LH PASS DOOR OPS NORMAL

Part: ACTUATOR — UNSERVICEABLE (RT ELEVATOR) · airframe 73,500 hrs · 13,926 cycles

PITCH CONTROL DURING CLIMBOUT WAS DIFFICULT TO PREDICT. HEAVY DOWNWARD FORCE WOULD COME AND GO. CONTROLL COLUMN WOULD OSCILLATE.REPLACED RH ELEVATOR INBOARD ACTUATOR PER MM 27-30-00-710-801/802.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 73,500 hrs · 13,926 cycles

R1 SLIDE NITROGEN BOTTLE OUT OF GREEN ARC. SERVICED R1 SLIDE NITROGEN BOTTLE PER AMM TASK 12-25-04-600-801.

Part: PAN — CRACKED (CARGO DOOR) · airframe 72,966 hrs · 13,753 cycles

BULK CARGO DOOR LOWER AFT CORNER WAS DEFLECTED AND THE PAN HAD A 1 INCH CRACK THAT ENDS IN A RIVET HOLE. REPAIRED IAW EO MD11-5230-70321-A.

Part: PANEL — INOPERATIVE (L1 DOOR SLIDE) · airframe 72,637 hrs · 13,665 cycles

L1 DOOR SLIDE INOPERATIVE, OVERHEAD SLIDING PANEL WAS STUCK. REPAIRED THE SLIDING PANEL IAW SRM 51-62-01, REPLACED THE SPRING AND CABLE ASSY IAW MM 25-23-23, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 72,329 hrs · 13,596 cycles

ON PREFLIGHT; ''EMER LT BAT 1 LO''. R&R EMERGENCY POWER SUPPLY IAW MM 33-51-01. OPS CK GOOD.

Part: BARRIER — CRACKED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL AT STA 500.17 AND X=-47.5 IS CRACKED. REPAIRED CRACKED RIGID CARGO BARRIER WALL AT STA 500.17 AND X=-47.5 IAW EA 011-5320-01-A7311 REV I/R AND EO MD11-5320-69066-A. (MAJOR)

Part: BARRIER — CORRODED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER CLOSE-OUT HAS CORROSION AT STA 488.812 BETWEEN X=70 THRU X=78. REPAIRED CORRODED RCB WALL LOWER CLOSE-OUT AT STA 488.812 AND BETWEEN X=70 THRU X=78 IAW EA 011-5310-01-A7319 REV I/R AND EO MD11-5320-69053-A. (MINOR)

Part: BARRIER — CRACKED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER CLOSE-OUT IS CRACKED AT STA 488.81 AND X=-49.9. REPAIRED CRACKED RIGID CARGO BARRIER WALL LOWER CLOSE-OUT AT STA 488.81 AND X=-49.5 IAW SRM 53-20-53 REPAIR 1 FIG. 201. (MAJOR)

Part: BARRIER — CRACKED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER CLOSE-OUT IS CRACKED AT STA 488.81 AND X=-47.5. REPAIRED CRACKED RIGID CARGO BARRIER WALL LOWER CLOSE-OUT AT STA 488.81 AND X=47.5 IAW SRM 53-20-53 REPAIR 1 FIG 201. (MAJOR)

Part: BARRIER — CRACKED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER FWD CLOSE-OUT IS CRACKED AT STA 488.81 AND X=-27.5. REPAIRED CRACKED RIGID CARGO BARRIER WALL LOWER FWD CLOSE-OUT AT STA 488.81 AND X=-27.5 IAW SRM 53-20-53 REPAIR 1 FIG 201. (MAJOR)

Part: FITTING — CORRODED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

RIGID CARGO BARRIER FLOOR FITTING NR 1 HAD CORROSION. REMOVED AND REPLACED THE RIGID CARGO BARRIER FLOOR FITTING IAW EO MD11-2520-58701-D.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

RIGID CARGO BARRIER FLOOR FITTING NR 7 HAD CORROSION. REMOVED AND REPLACED THE RIGID CARGO BARRIER FLOOR FITTING IAW EO MD11-2520-58701-D.

Part: FLAP — CRACKED (RT WING) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RT IB FLAP T/E SPLIT AT STA XIFH183. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND SRM 51-62-01. (MINOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

MAIN CABIN BS 460 - 475, FLOOR PANEL WAS CORRODED AT RIGID CARGO BARRIER FLOOR FITTING NR 7. REMOVED AND REPLACED THE FLOOR PANEL IAW EO MD11-2520-58701-D.

Part: BARRIER — CORRODED (MAIN CABIN) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER FWD. FACE HAS CORROSION AT STA 488.812 AND BETWEEN X=-54 THRU X=-78 AND Z=-19. REPAIRED CORRODED RIGID CARGO BARRIER WALL LOWER FWD FACE AT STA 488.812 AND BETWEEN X=-54 THRU X=-78 AND Z=-19 IAW EA 011-5310-01-A7318 REV I/R AND EO MD11-5320-69060-A. (MINOR)

Part: STIFFENER — CRACKED (FWD CARGO BAY) · airframe 72,324 hrs · 13,592 cycles

FWD CARGO BAY SUB FLOOR BEAM, VERTICAL STIFFNER ANGLE WAS CRACKED AT BS 6-70, ABOVE LONGERON 43L. REMOVED, FABRICATED, AND REPLACED THE STIFFNER IAW DWG A6A7092, AND SRM 51-33-01.

Part: BEAM — CRACKED (FWD CARGO) · airframe 72,324 hrs · 13,592 cycles

FWD CARGO BAY SUB FLOOR, LT HORIZONTAL BEAM WAS CRACKED AT STA 6-73, ABOVE LONGERON 43L. REMOVED AND REPLACED THE HORIZONTAL BEAM IAW SRM 51-31-01, 51-33-01, AND 51-35-01.

Part: FLAP — CRACKED (LT WING) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, LT IB FLAP T/E SPLIT AT STA XIFH 233. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND 51-62-01. (MINOR)

Part: STIFFENER — CHAFED (TAIL CONE) · airframe 72,324 hrs · 13,592 cycles

TAIL CONE UPPER PATIO DOOR LT SIDE STIFFNER ANGLE, BEHIND SPRING SEAL HAD DEEP WEAR. REMOVED, FABRICATED, AND REPLACED THE STIFFNER ANGLE IAW DWG AKC7868, AND SRM 51-31-01.

Part: LONGERON — CORRODED (BS 1531-1561) · airframe 72,324 hrs · 13,592 cycles

CENTER CARGO, BS 1551 CENTERLINE LONGERON 52 HAD CORROSION, INBD OF THE DRAIN. REMOVED AND REPLACED THE DAMAGED SECTION OF LONGERON BETWEEN BS 1531 - 1561 IAW SRM 51-31-01, 51-33-01, AND 53-50-05.

Part: TEE FITTING — CRACKED (BS 1340) · airframe 72,324 hrs · 13,592 cycles

MAIN CABIN LONGERON 15L TEE FITTING WAS CRACKED AT BS 1340. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA7568, AND SRM 51-33-01.

Part: LONGERON — CRACKED (BS 1159-1179) · airframe 72,324 hrs · 13,592 cycles

MAIN CABIN LONGERON 18L WAS CRACKED BETWEEN BS 1159 - 1179. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA0220, AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1321) · airframe 72,324 hrs · 13,592 cycles

MAIN CABIN LONGERON SPLICE 14R WAS CRACKED AT BS 1321. REMOVED, FABRICATED, AND REPLACED THE LONGERON SPLICE IAW DWG AEA7600, AND SRM 51-33-01.

Part: TEE FITTING — CRACKED (BS 1340) · airframe 72,324 hrs · 13,592 cycles

MAIN CABIN LONGERON 15R, TEE FITTING WAS CRACKED AT BS 1340. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.

Part: ANGLE — CRACKED (RT WING SLAT) · airframe 72,324 hrs · 13,592 cycles

RT WING NR 2 SLAT OTBD EDGE ANGLE WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG ARB1647, AND SRM 5135-01.

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 72,324 hrs · 13,592 cycles

TAIL CONE RT CENTER GUIDE PIN ATTACH INTERCOSTAL AND PLATE WERE CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL AND DOUBLER IAW DWG AKC7520, AND SRM 53-80-07, REPAIR 7.

Part: TAIL CONE — WORN (FUSELAGE) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, TAIL CONE STA 2165.6 HAS DEEP WEAR AT BX=-36.5 AND BETWEEN Z=-35 TO Z=-61.5. REPAIRED TAIL CONE AT SAID LOCATION IAW EA 011-5320-01-A7307 REV I/R AND EO MD11-5350-68943-A. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 72,324 hrs · 13,592 cycles

LEFT UNDERWING ACCESS PANEL LANDING WAS CRACKED AT XORS 542. REMOVED, FABRICATED, AND REPLACED THE ACCESS PANEL LANDING DOUBLER IAW DWG ARB2933, SRM 51-33-01, AND 51-35-01.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 72,324 hrs · 13,592 cycles

RT WING FIXED L/E BEADED DOUBLER WAS CRACKED AT XOS 494 - 500. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 72,324 hrs · 13,592 cycles

INSPECTION TYPE:2C, NR 3 I/B T/R AFT UPPER OUTER SKIN HAS A CRACK APPROX 4" FROM AFT EDGE OF UPPER SIDE. REPAIRED NR 3 I/B T/R AFT UPPER OUTER SKIN IAW EA 011-7830-01-A-7305 REV IR AND EO MD11-7830-68876-A. (MINOR)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,709 hrs · 13,414 cycles

FOUND THE CABIN RT EMERGENCY LIGHT LENS MISSING ABOVE GALLEY, REPLACED THE LENS & CHECK NORMAL IAW AMM 33-52-04 .

Part: CHANNEL — DAMAGED (X=30.78 STA 999) · airframe 71,023 hrs · 13,244 cycles

FWD CARGO COMPT HAT CHANNEL STABILIZER STRAP DAMAGED AT CEILING 4TH FRAME IN FROM THE DOOR OPENING POS NR 4 STA 1049FAB AND INSTALLED NEW CHANNEL IAW EO 3510-66480-A.

Part: DOOR — DEFECTIVE (COCKPIT) · airframe 70,950 hrs · 13,223 cycles

CPT SEAT LIFE VEST DOOR WILL NOT STOW. REPAIR PER MM 25-11-00-201 OPS CHKS GOOD.

Part: RELAY — INOPERATIVE (R1 DOOR) · airframe 70,576 hrs · 13,134 cycles

R1 DOOR WILL NOT OPERATE. REPLACED THE R1 DOOR ACTUATOR CONTROL RELAY IAW FIM 52-11-03. TESTED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,935 hrs · 13,001 cycles

EMERGENCY LIGHT INOPERATIVE AT COCKPIT DOOR. REPLACED THE LAMPS IAW MM 33-32-04. TESTED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,909 hrs · 12,988 cycles

EMERGNECY LIGHTS SYSTEM INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-5- 01-400-802. OPS CHECKED NORMAL IAW 33-51-01-700-802.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 69,886 hrs · 12,981 cycles

EMERGENCY 1 BATTERY LOW ILLUMINATED. R & R THE BATTERY IAW MM 33-51-01-400-802. OPS CHECKED NORMAL.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 69,664 hrs · 12,919 cycles

RIGHT INBD FLAP TOP SIDE PUNCTURED. REPAIRED IAW EO MD11-5750-68086-A.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 69,664 hrs · 12,919 cycles

PUNCTURE IN THE RT INBD FLAP BOTTOM SIDE MEASURES 1.5 X 3. REPAIRED IAW EO MD-11 57-50-63782-B.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,515 hrs · 12,866 cycles

EMERGENCY LIGHT SYS TEST FAILED. R & R THE BATTERY PACK IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: PIN — DAMAGED (L1 DOOR) · airframe 69,369 hrs · 12,836 cycles

L1 DOOR STUCK HALF WAY UP. DOOR WILL NOT OPERATE ELECTRICALLY, L1 DOOR CLOSED MANUALLY. REPLACED THE L2 DOOR LOCK PIN IAW AMM 52-10-06.

Part: BRACKET — FAILED (PBE) · airframe 69,317 hrs · 12,824 cycles

PBE IN SUPERNUMERARY AREA CAME OFF WALL DURING TAKEOFF. R & R THE PBE BRACKET ASSY IAW AMM 35-31-01.

Part: SMOKE BARRIER — DAMAGED (CABIN) · airframe 69,240 hrs · 12,809 cycles

SMOKE CURTAIN AT 12:00 POSITION HAS HOLE & NOT SECURED. COMPLIED WITH INTERIM REPAIR OF THE SMOKE CURTAIN IAW EO MD11 2550-39020B. OK FOR SERVICE.

Part: SMOKE BARRIER — DAMAGED (CABIN) · airframe 69,240 hrs · 12,809 cycles

SMOKE CURTAIN AT RT LOWER HAS NUMEROUS HOLES. COMPLIED WITH INTERIM REPAIR IAW EO MD11-2550-39020B.

Part: LANYARD — DETACHED (ESCAPE ROPE) · airframe 68,929 hrs · 12,741 cycles

CAPTAINS ESCAPE ROPE RESTRAINT LANYARD UNATTACHED. SECURED CAPT'S ESCAPE ROPE RESTRAINT.

Part: STRUCTURE — BENT (L1 DOOR) · airframe 68,414 hrs · 12,603 cycles

L1 ENTRY DOOR UPPER CORNER BENT. REPAIR IAW EO MD11-5210-62155-C.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 68,359 hrs · 12,591 cycles

UPPER FWD CORNER OF L1 DOOR CATCHING CAUSING DOOR SKIN DAMAGED. REPAIR MADE PER EO MD11-5210-62155-C. MAJOR REPAIR.

Part: SKIN — CHAFED (LT WING LE) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, LT WING FIXED L/E SKIN CHAFED AT XDLE 330.2745. REPAIRED IAW EA O11-5710-01-A6398-IR AND EO MD11-5740-61670-A.

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE:1C, LT WHEEL WELL INTERCOSTAL IS CRACKED ON KEELBEAM STA 1381. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AT SAID LOCATION IAW DWG AEA7094 AND SRM 51-33-01, MINOR.

Part: TRUNNION — CORRODED (MLG) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, CENTER LANDING GEAR TRUNNION FITTING AFT MOUNT HOLE HAS CORROSION. REPAIRED THE TRUNNION FITTING IAW SRM 53-40-14 REPAIR 1 FIG201.

Part: LANDING — CRACKED (RT WING) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE:1C, RT WING LOWER PANEL, 636AB LANDING AT STA XORS 683.4 TO 713.65 IS CRACKED. REPAIRED CRACKED RT WING LOWER PANEL 636AB, LANDING AT STA XORS 683.4 TO 713.65 IAW SRM 57-20-02, REPAIR 5, FIG 201.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING HAS CORROSION. REPAIRED THE FITTING IAW SRM 53-40-14 REPAIR 1 FIG. 201.

Part: STRUCTURE — CORRODED (RT WING) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE:1C, RT OTBD WING T/E REAR SPAR PANEL LANDING HAS CORROSION BETWEEN XOSP.548.881 TO 568.881. REPAIRED THE RT WING T/E REAR SPAR PANEL LANDING IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)

Part: STRUCTURE — CORRODED (RT WING) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, RT WING UPPER T/E PANEL LANDING HAS CORROSION BETWEEN XOSP. 624.052 - 657.203. REPAIRED THE RT WING PANEL LANDING IAW SRM 57-50-02 REPAIR 10 FIG. 201.

Part: HINGE FITTING — CHAFED (NR 1 NACELLE) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, NR 1 ENGINE OTBD FAN COWL FWD HINGE FITTING HAS CHAFE DAMAGE. REPAIRED IAW EA 011-7110-01-A6405 REV. I/R AND EO MD11-7110-61645-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, RT OTBD WING REAR SPAR UPPER CAP HAS CORROSION AT XORS 690. REPAIRED THE RT WING REAR SPAR UPPER CAP IAW EA 011-5710-01-A6409 REV. I/R.

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, RT MLG WW INTERCOSTAL IS CRACKED AT BS 1441 - 1461 X-31.5 & Z 56. REPAIRED THE INTERCOSTAL IAW SRM 53-40-12 REPAIR 3 FIG. 201. (MAJOR)

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, LT MLG WW INTERCOSTAL IS CRACKED AT BS 1441 - 1461 X 31.5, Z 56. .REPAIRED THE INTERCOSTAL IAW SRM 53-40-12 REPAIR 3 FIG. 201. (MAJOR)

Part: RIB — CRACKED (LT WING) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, LT WING L/E RIB IS CRACKED AT XOS 545. REMOVED, FABRICATED AND REPALCED THE LEFT WING L/E RIB IAW DWG. ARB2918 AND SRM 51-35-01.

Part: BEAM — CORRODED (RT WING MLG WW) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, RT WING MAIN LANDING GEAR WHEEL WELL T/E BEAM HAS INCOMING BLENDOUT DAMAGE. REPAIRED IAW EA 011-5720-01-A6406 REV. I/R AND EO MD11-5720-61647-A.

Part: TRUNNION — CRACKED (NLG) · airframe 67,958 hrs · 12,502 cycles

INSPECTION TYPE: 1C, LEFT NOSE LANDING GEAR TRUNNION FITTING IS CRACKED. REPAIRED THE TRUNNION FITTING IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, RIGHT WING FIXED L/E BEADED DOUBLER AT XOS 542-547 IS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT WS 698-703. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG.203. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER AT XOS. 667-673 IS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: FITTING — CRACKED (MAIN CABIN) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-02-910-801.

Part: DOUBLER — CRACKED (LT WING) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT WS 768-772. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 67,954 hrs · 12,499 cycles

INSPECTION TYPE: 1C, LEFT WING ACCESS PANEL 536AB LANGING BETWEEN XORS. 683.4 - 713.65 HAS SEVERAL CRACKS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MAJOR)

Part: SKIN — DAMAGED (L1 DOOR) · airframe 67,739 hrs · 12,437 cycles

L-1 DOOR OUTER SKIN DAMAGED, REF EO MD11-5210-61106-B FOR REPAIR.

Part: BOTTLE — LEAKING (R1 DOOR) · airframe 67,052 hrs · 12,267 cycles

RT DOOR EMERGENCY DEPLOY BOTTLE PRESSURE LOW, LEAKING. R & R R1 DOOR BOTTLE IAW MM 52-11-04. OPS AND LEAKS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,043 hrs · 12,265 cycles

INSPECTION TYPE: LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW ALERT WHEN TESTING EMERGENCY LIGHTS. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-01, OPS TEST PASS.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE: 1C, LT INBD FLAP SKIN CORRODED BETWEEN XIFH 133-141. REPAIRED CORRODED SKIN IAW EA011-5753-01-A5826, REV I/R AND EO MD11-5750-57621-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, RT WING L/E INNER BEADED DOUBLER CRACKED, XOS756, ADJACENT TO EXISTING REPAIR XOS 759-763. REMOVED EXISTING REPAIR, INSTALLED NEW BEADED DOUBLER REPAIR XOS 753-763 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: FORMER — CRACKED (RT WING) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, RT WING L/E INTERNAL FORMER CRACKED IN RADIUS AT XOS 1035. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 2920 AND SRM 51-35-01.

Part: SHEAR TIE — CRACKED (BS 2047) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, SHEAR TIE CRACKED IN 311 COMPARTMENT CEILING BS 2047. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE IAW DWG AJC7021 AND SRM 51-33-01.

Part: SHEAR TIE — CRACKED (BS 2103) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, SHEAR TIE CRACKED IN 311 COMPARTMENT CEILING AT BS 2103. R & R SHEAR TIE IAW SRM 51-35-01, 51-31-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, LT WING L/E INNER BEADED DOUBLER CRACKED XOS 640. REPAIRED LT WING BEADED DOUBLER XOS636-643 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, LT WING L/E INNER BEADED DOUBLER CRACKED XOS 628. REPAIRED LT WING BEADED DOUBLER XOS 625-629 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: SHEAR TIE — CRACKED (BS 2140) · airframe 65,041 hrs · 11,763 cycles

INSPECTION TYPE:3C, SHEAR TIE CRACKED BS 2140. R & R SHEAR TIE IAW SRM 51-33-01, 51-35-01.

Part: LIFE VEST — TORN (COURIER)

COURIER SEATS ONE LIFE VEST PACKAGE TORN. R & R COURIER SEAT LIFE VEST REF EO NR M2560-30108-E.

Part: FLOOR PANEL — CORRODED (BS 475) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, RIGID CARGO BARRIER FLOOR PANEL HAS CORROSION AT BS 475 X-47.50 REPAIRED FLOOR PANEL IAW EA 011-5310-01-A5383 AND EO 5310-54594-A.

Part: TEE FITTING — CHAFED (NR 2 NACELLE) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, NR 2 ENGINE PYLON ACCESS PANEL 458AR AFT FAIRING TEE FITTING FOUND CHAFED. FABRICATED AND REPLACED TEE FITTING IAW EA 011-5450-01-A5397, REV I/R AND EO 5450-54528-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER PANEL HAS CORROSION AT STRINGER 15, STA 1225-1231, X=75.25 TO X=107.25. ACCOMPLISHED REPAIR TO CENTER AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231, X=75.25 TO X=107.25 IAW EA 011-5730-01-A5396 REV I/R AND EO 5730-54565-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231 X=27.50 TO X=8.50. ACCOMPLISHED REPAIR ON CENTER AUX UPPER SKIN PANEL AT STRINGER 15 STA 1225-1231, X=27.50 TO X=8.50 IAW EA 011-5730-01-A5396, REV I/R AND EO 5730-54565-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231, X=-47.50 TO X=-75.25. ACCOMPLISHED REPAIR ON CENTER WING UPPER SKIN PANEL AT STRINGER 15 STA 1225-1231, X=-47.50 TO X=-75.25 IAW EA 011-5730-A5396, REV I/R AND 5730-54565-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL AT STRINGER 15 HAS CORROSION STA 1225-1231, X=-75.25 TO X=-107.25. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN AT STRINGER 15 STA 1225-1231, X=-75.25 TO X=-107.25 IAW EA 011-5730-01-A5396 REV I/R AND EO 5730-54565-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231 X=-8.50 TO X=-27.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15 STA 1225-1231 X=-8.50 TO X=-27.50 IAW EA 01-5730-01-A5396, REV I/R EO 5730-54565-A.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, R3 DOOR FRAME LOWER FWD LIGHTNING HOLE IS CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION ON STR 15 AT STA 1225-1231, X=27.50 TO X=47.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231 X=27.50 TO X=47.50 IAW EA 011-5730-01-A5396, REV I/R AND EO 5730-54565-A.

Part: DOOR FRAME — CRACKED (R3 DOORWAY) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, R3 DOOR FRAME LOWER AFT LIGHTNING HOLE CRACKED. REPAIRED IAW SRM 53-40-15, REPAIR 3, REV 55.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, L3 DOOR FRAME LOWER FWD LIGHTNING HOLE IS CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER PANEL SKIN HAS CORROSION AT STRINGER 15 STA 1225-1231 X=-27.50 TO X=-47.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN AT STRINGE 15 STA 1225-1231 X=-27.50 TO X=-47.50 IAW EA 011-5730-01-A5396, REV I/R AND EO 5730-54565-A.

Part: PANEL — CORRODED (FUEL CELL) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15, STA 1225-1231 X=8.50 TO X=-8.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231 X=8.50 TO X=-8.50 IAW EA 011-5730-01-A5396 AND EO 5730-54565-A (MINOR)

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, RIGHT INBD FLAP VANE HAS DELAMINATION AT LWR SURFACE JUST OTBD OF CENTER TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201, REV 55.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, LEFT INBD FLAP VANE LWR SURFACE HAS DELAMINATION BETWEEN CENTER AND OTBD TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201, REV 55.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, RIGHT INBD FLAP VANE HAS DELAMINATION AT LOWER SURFACE JUST INBD OF CENTER TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201 REV 55.

Part: INTERCOSTAL — CRACKED · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CRACK FOUND ON NR 2 ENGINE UPPER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL Y 2164. ACCOMPLISHED DOUBLER REPAIR ON NR 2 ENG UPPER CENTER SPAR TO REAR SPAR INTERCOSTAL AFT EDGE AT STA Y 2164 IAW SRM 55-30-02, FIG 204, REPAIR 7.

Part: STRINGER — CRACKED (RT WING) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, RT WING UPPER STRINGER, NR 5 CRACKED BETWEEN STA XORS 1070 AND 1093. ACCOMPLISHED REPAIR ON RT WING UPPER STRINGER NR 5 BETWEEN STA XORS 1070 AND 1093 IAW EA 011-5710-01-A5381, REV I/R AND EO 5710-54584-A.

Part: TRIPLER — CHAFED (BS 1159) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, TRIPLER IS CHAFED ON RT LOWER FUSELAGE BS 1159, L44R. ACCOMPLISHED REPAIR TO TRIPLER IAW EA011-5330-01-A5403, REV I/R AND EO MD11-5330-54575-A.

Part: BEAM — CRACKED (LT WING) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, LT WING T/E BEAM ASSY LOWER CAP CRACKED BETWEEN XW 332.76 AND XW 312. ACCOMPLISHED SPLICE REPAIR ON LT WING T/E BEAM ASSY LOWER CAP STA XW 332 TO XW 312 IAW EA 011-5720-01-A5361, REV I/R AND EO 5720-54420-A.

Part: STRINGER — CRACKED (RT WING) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, RT WING STRINGER 15 IS CRACKED AT STA XORS 433-455. REPAIRED STRINGER IAW EA 011-5710-01-A5382, REV I/R AND EO MD11-5710-54618-A.

Part: STRINGER — CRACKED (LT WING) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, LT WING UPPER STRINGER 9 HAS CRACK AT STA XORS 799.4 TO 826.5. REPAIRED IAW SRM 57-00-03 REPAIR 5, FIG 202.

Part: FORMER — CRACKED (RT WING) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, CRACKED FORMER IN RT WING FIXED L/E NEAR XORS 917. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 2920, SRM 51-35-01, 51-31-01, 51-33-01.

Part: DUCT — CHAFED (LEFT) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, REPAIR DOUBLER IS CHAFED AND EDGE IS BENT AROUND LT TELESCOPIC DUCT CUTOUT. REPAIRED IAW SR M57-40-01 REPAIR 10, FIG 201, REV 55.

Part: SKIN — DAMAGED (BS 1531) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BS 1531, L49-50R FABRICATED AND INSTALLED REPAIR DOUBLER AT NOTED LOCATION IAW EA 011-5330-01-A5401, REV IR AND EO MD11-5330-54623-A.

Part: SKIN — GOUGED (BS 655-675 S32R) · airframe 68,173 hrs · 11,249 cycles

4C INSPECTION, FIVE GOUGES ON FUSELAGE SKIN BETWEEN BS 655-675, STRINGER 32R REPAIRED IAW EA 011-5330-01-A5408 REV I/R AND 5330-54569-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL DAMAGED, BS 1059, BL 0. FABRICATED NEW FLOOR PANEL IAW EO MD11-5320-27386-C.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE)

L1 DOOR SLIDE TEST FAILED. REPLACED LAMP IAW AMM 52-00-00. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

DURING EMERGENCY LIGHT TEST, EMERGENCY LIGHT BATTERY ON LOW DISPLAYED. DEFERRED EMERGENCY LIGHT SYS IAW MEL 33-50-4. C/W DMP 33-50-4. PLACARD INSTALLED. ASSIGNED M505057. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-1-01, IPC REF 33-51-10-01-008. SYS TESTS OK. THIS CLEARS M505057.

Part: PRESSURE GAUGE — CONTAMINATED (R1 DOOR SLIDE)

R1 DOOR SLIDE PRESSURE GAUGE CONTAMINATED WITH MOISTURE. ILLEGIBLE. DEFERRED IAW MEL 52-10-3-2. PLACARD INSTALLED. LOG UPDATED. R & R R1 DOOR PNEUMATIC STORAGE RESERVOIR PRESSURE GAUGE AND RELIEF VALVE REF AMM 52-11-04 AND IPC 52-11-35-01. THIS CLEARS M505028. PLACARD REMOVED.

Part: WARNING LIGHT — FALSE INDICATION (EMERGENCY LIGHTS)

DURING EMERGENCY LIGHT TEST, LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW DISPLAYED. ACCOMPLISHED SYS OPS TEST IAW AMM 33-51-700-802. ALL SYSTEMS OPS NORMAL.

Part: DOUBLER — CRACKED (RT WING) · airframe 60,474 hrs · 10,592 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS545 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS542-547 IAW EO MD11-5730-48222-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 60,474 hrs · 10,592 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS669. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS667-673 IAW EO MD11-5730-48222-A (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 60,474 hrs · 10,592 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 701 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS698-703 IAW EO MD11-5730-48222-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 60,474 hrs · 10,592 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS770. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 768-772 IAW EO MD11-5730-48222-A (MAJOR).

Part: RIB — DAMAGED (LT WING)

LEFT WING L/E RIB CAP DAMAGED AT STA X0S 470.2. REPAIRED IAW EO MD11-5720-48563-B.

Part: WARNING MESSAGE — ILLUMINATED (CABIN)

AIR TURN BACK DUE TO SMOKE INDICATION FROM MAIN CABIN. EMERGENCY DECLARED. OPEN.

Part: CONTROLLER — FALSE ACTIVATION (SMOKE DETECTION)

SMOKE INDICATION FROM MAIN CABIN. EMERGENCY DECLARED. R & R MISCELLANEOUS SYS CONTROLLER REF MM 31-42-01. PERFORMED RTS TEST OF MISCELLANEOUS SYS CONTROLLER SYS CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

ONE EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-12-15.

Part: COVER — LOOSE (EMERGENCY LIGHT)

L1 FWD DOOR HANDLE EMERGENCY LIGHT COVER LOOSE. R & R LIGHT ASSY IAW MM 33-52-02. OPS CHECKED GOOD.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT)

F/O'S FORWARD SLIDING WINDOW LOCK MECHANISM DOESN'T LOCK WINDOW. HANDLE DOES NOT MOVE FORWARD. ADJUSTED WINDOW IAW AMM 56-12-01-5 OPS AND TEST IAW AMM 56-12-01.

Part: PANEL — DAMAGED (LT WING) · airframe 58,582 hrs · 10,083 cycles

INSPECTION TYPE: 2C, LT WING FIXED L/E DOOR 518AB HAS ONE ELONGATED FASTENER HOLE. DURING DISASSEMBLY ALSO FOUND ELONGATED HOLE IN ADJACENT WEB ARB2883- 3. REPAIRED DOOR AND WEB IAW STA SA EA 011-5730-01-A3761 REV IR & EO MD11-5730-46514-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 58,582 hrs · 10,083 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E COMPT THRU ACCESS 618GB BEADED DOUBLER CRACKED ABOVE OTBD OF FUEL RECEPTACLE. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS643-648 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-C.

Part: DOUBLER — CRACKED (RT WING) · airframe 58,582 hrs · 10,083 cycles

INSPECTION TYPE:3C, RIGHT WING FIXED L/E BAY BEADED DOUBLER BETWEEN XOS 759-763 CRACKED INBD OF NR 12 SLAT TRACK. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-C.

Part: SKIN — CRACKED (LT WING) · airframe 58,582 hrs · 10,083 cycles

INSPECTION TYPE:2C, LT WING L/E IS CRACKED AT NR 14 SLAT TRACK CUT-OUT STA XOS894. REPAIRED LT WING L/E EXTERNAL SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SPAR — CORRODED (LT WING) · airframe 54,037 hrs · 8,956 cycles

INSPECTION TYPE: 2C, LEFT WING UPPER REAR SPAR SURFACE HAS CORROSION AND PANEL LIFTING, LWS 608.25 TO 638.25. ACCOMPLISHED STA-SA EA 011-5720-01-A3705 I/R AND EO MD11-5720-46237-A.

Part: WEB — DAMAGED (BS 1521)

WEB DAMAGED AT STA 1521. REPAIRED IAW EO MD11-5310-45418B.

Part: CYLINDER — INOPERATIVE (MLG)

AIR TURN BACK. LANDING GEAR WOULD NOT RETRACT. R & R TRIM CYLINDER FUSE IAW AMM 32-37-06-4, WITNESSED GEAR SWING.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR)

L1 DOOR WILL NOT OPEN. RESEATED DOOR SLIDE AND REPOSITIONED GIRT BAR. STOWED SAFETY PIN IN SLIDE POUCH. OPS CHECKS GOOD AMM 52-10-01-860 FOR L1 DOOR ASSY,

Part: STRINGER — BROKEN (LWS 661-674) · airframe 564,629 hrs · 536 cycles

INSPECTION TYPE:1C, LT WING L/E COMPARTMENT HORIZONTAL STRINGER HAS PIECE BROKEN OFF NEAR STA XOS668 FWD SIDE OF L/E. FABRICATED AND INSTALLED REPAIR IAW EO MD11-5710-41945-A AND STASA EA 011-5720-01-A2965 REV IR.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 56,462 hrs · 9,536 cycles

INSPECTION TYPE:1C, RT WING L/E COMPARTMENT CEILING DOUBLER IS CRACKED AT 2 EA FASTENERS, XOS 654, ABOVE PULLY AND BRACKET. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 56,462 hrs · 9,536 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACK AT XOS STA 703 APPX JUST INBD OF SLAT TRACK REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW MD-11 SRM 57-40-02 REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 56,462 hrs · 9,536 cycles

INSPECTION TYPE:1C, RT WING L/E COPARTMENT CEILING DOUBLER IS CRACKED AT FASTNERS XOS 612. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 56,462 hrs · 9,536 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACK AT STA XOS 671 APPX. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 56,462 hrs · 9,536 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E COMPRT. BEADED DOUBLER CRACKED AT AFT END STA XOS 525 ABOVE SLAT LATCH MECHNISM AND DIVE CABLES. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW MD-11 SRM 57-40-02, REPAIR 9 FIG. 203

Part: CONTROL UNIT — INOPERATIVE (ELECTRICAL BUSS)

ON DESCENT, ENCOUNTERED BUSS AC 1 OFF AND LEVEL 2 SELECT FADEC ALTERNATE. RAN FADEC CHECKLIST AND SELECTED ALTERNATE ON ALL 3 ENGINES. OTHER ALERT ON ELC SYNOPTIC WERE (AC T/E OFF, EMER PWR ON, AND GEN 1 OFF). EMERGENCY DECLARED. ON ELECT CONTROL PANEL MANUAL LIGHT STAYS ON WITH SW IN AUTO & EPCU DISPLAYED CURRENT FAULTS, APU FAULTS APU DPCT RELAY/INTFC, BTR 1 TRIP/INTFC, GR1-INTFC, REPLACED EPCU IAW AMM 24-08-1-4 AND PERFORMED RTS ON EPCU. NO DESCREPANCIES NOTED.

Part: RELAY — MALFUNCTIONED (CABIN DOOR)

RT CABIN DOOR WILL NOT OPEN. M426670, T/S IAW FRIM 52-11-00-1. R & R RELAY R2-176 R FWD DOOR ACTUATOR. OPS TESTED - NORMAL. DMI CLOSED.

Part: SKIN — MISREPAIRED (LT WING) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, REPAIR SURVEY SEQ NR 279-W3-06 PREVIOUS REPAIR DOUBLER NOT IN SRM LT WING NR 4 SLAT APPROX BTWN STA XOS 559-570. REMOVED DOUBLER AND FILLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW STASA EA 011-5754-01-A2164 I/R AND EO MD11-5750-36728-A.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, RT FUSELAGE UNDER HORIZONTAL STAB HAS CORROSION AROUND FASTNER HOLES AND SKIN FROM STA 2033 TO 2160 CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-70-01, REPAIR 3, FIG. 201.

Part: SKIN — CRACKED (LT WING) · airframe 53,598 hrs · 8,930 cycles

INSP TYPE:4C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED ON UPPER INBD AND OTBD CORNERS. CUT OUT DAMAGE AREA AND FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.

Part: SKIN — MISREPAIRED (RT WING SLAT) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQ NR 279-W4-06 RT DROOP L/E BETWEEN STA XDLE 298-309 EXISTING REPAIR DOUBLER NOT IN SRM. REMOVED EXISTING REPAIR FROM RT DROOP L/E BETWEEN STA XDLE 301-309. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11-5750-36630-A AND EA 011-5754-01-A2149.

Part: SKIN — CRACKED (RT WING) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:C4 RT WING FIXED L/E SLAT TRACK NR 14 SKIN CUT-OUT CRACKED AT AFT END. CUT OUT DAMAGE AT XOS891, FABRICATED AND INSTALLED FILLER AND DOUBLER REF MD11 SRM 57-40-02 FIG 201 REPAIR 7.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 53,598 hrs · 8,930 cycles

INSP TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-W4-04 RT INBD FLAP LOWER EXISTING REPAIR BTWN STA XIFH 177-183 NOT CORRELATED TO SRM 57-00-01 FIG 7 IS NOT APPLICABLE FOR PRIMARY STRUCTURE ELEMENT. REMOVE DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW STA SA EA 011-5753-01-A2155 I/R AND EO MD11-5750-36623-A.

Part: SKIN — CRACKED (RT WING) · airframe 53,598 hrs · 8,930 cycles

INSP TYPE:C4, RT WING FIXED L/E TELESCOPING DUCT INBD AFT CUTOUT CRACKED AT CORNER. CUT OUT DAMAGED AREA FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED AT BOTTOM SKIN OTBD END CUT OUT DELAM SKIN 2 IN. DIAM APPLIED WET LAYUP REPAIR REF SRM 57-50-80 REPAIR 2 FIG 201.

Part: SKIN — MISREPAIRED (NR 3 SLAT) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-W3-01, NR 3 SLAT L/E SKIN HAS (I EA) FLUSH REPAIR BTWN STA XOS 419 AND XOS 429. REPAIR DOES NOT CORRELATE TO SRM 57-10-00 VOL I, FIG 35. RADIUS IS .500" TYP. SHOULD BE 1.0" REMOVED DOUBLER, INCREASED TRIM OUT, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLERS IAW STA SA EA 011-5750-01-A2150 I/R AND EO MD11-5750-36704-A

Part: SKIN — GOUGED (BS 1152 L44R) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, EXTERNAL FUSELAGE SKIN IS GOUGED FROM RUBBING ON FAIRING NR 154AB APPROX STA 1152. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLERS IAW STA SA EA 011-5330-01-A2167 I/R AND EO MD11-5330-36696-A.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 53,598 hrs · 8,930 cycles

INSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-52-01 AT RT INBD DETACHABLE ELEVATOR ON LOWER INBD END BETWEEN STA XE 61.56 AND XE 73.56 REPAIR IS DELAMINATED WITH FABRIC EXPOSED. REMOVED PREVIOUS REPAIR AND DAMAGED AREA. BONDED REPAIR PLIES IAW SRM 55-20-80 REPAIR 2 PARA 4.D.B AND 51-62-01 PARA 8.0. (2) (A).

Part: SEAT TRACK — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A POS 3 R/L LOCK INOP TRACK DAMAGED. C/W PERM REPAIR PER SRM 53-00-52 STANDARD SEAT TRACK REPAIR DAMAGE REMOVED AND PLUGGED, REPAIR 3.

Part: APU — MALFUNCTIONED (APU BAY)

INSPECTION TYPE:N/A APU PRODUCED LOUD BANG AND THEN SMOKE WITH FLAMES. REMOVED AND REPLACED APU PER TC 9112, LEAKS CHECKS GOOD, THIS CLEARS M402696. PLACARD REMOVED.

Part: FLOORBOARD — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A BULK PIT FLOOR DAMAGED. FABRICATED NEW FLOOR IAW EO MD11-5320-27386.

Part: FLOORBOARD — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A BULK PIT FLOORBOARD DAMAGED. FABRICATED NEW PANEL PER EO MD11-5320-27386.

Part: ENGINE — OVERTEMP (NR 2)

AT 2600FT NR 2 ENGINE EGT CLIMBED TO 668 DEGREES FOR 30 SECONDS. VIBRATION FELT IN THE AIRFRAME. PERFORMED ENG OPERATIONAL OVERLIMITS INSPECTION AFTER EGT OVERTEMP IAW AMM 70-00-04-6-2. NO PHYSICAL DAMAGE NOTED. RAN ENGINE AT FLIGHT IDLE, ALL PATAMETERS CHECKED NORMAL ON THE GROUND IAW AMM 71-00-00.

Part: FITTING — CRACKED (RT WINGLET) · airframe 51,111 hrs · 8,270 cycles

INSPECTION TYPE:C RT WING LOWER WINGLET AFT FITTING FOUND CRACKED. RT WING LOWER WINGLET AFT FITTING REPLACED AS PER EO MD11-5720-27 680-A, APPENDIX E.

Part: SKIN — DENTED (CARGO DOOR) · airframe 51,111 hrs · 8,270 cycles

INSPECTION TYPE:C REF D-374482: AFT BULK CARGO DOOR, DOOR SKIN DENT (DEFERRAL TRANSFER ITEM). EXISTING REPAIR DOUBLER REMOVED PER SRM 51-31-01VIIR40. DISCREPANT LWR SKIN TRIM-OUT PER EN1386-08 & REPROTECTED PER SRM 51-21-01VII R40. HFEC INSP C/O PER DAC NDTSPM REV13 06-10-01.001 ON TRIM-OUT AREA, NO CRACK EVIDENT. NEW SKIN, REPAIR DOUBLER & INTERNAL DOUBLER FAB. FAB SKIN & DOUBLERS INSTALLED PER EN1386-08.

Part: CONTACT — DIRTY (EVAC SLIDE)

RT SLIDE REMOTE PRESS CK LIGHT INOP. DEFERRED PER MEL 25-61-2 DMP C/W. CLEANED CONTACTS. OPS CHECK GOOD.

Part: SLIDE — DAMAGED (R1 DOOR)

R1 SLIDE DAMAGED, R1 SLIDE DEACTIVATION PIN INSTALLED. REF TO WAN 1300451 REMOVED AND REPLACED SLIDE ON R1 DOOR IAW AM CH 25-61-15 & TC 8033. REMOVED DEACTIVATION PIN.

Part: GIRT BAR — DETACHED (ENTRY DOOR)

RIGHT SIDE ENTRY DOOR GIRT BAR NEED TO BE REATTACHED FORWARD END. REATTACHED RIGHT SIDE DOOR GIRT BAR AS REQUIRED PER MM 25-61-01-42-00. OPS CHECK NORMAL.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS)

INSPECTION EMERGENCY LIGHTS BAT (1) LOW LIGHT ILLUMINATES DURING EMERGENCY LIGHTS TEST. RE-TEST EMERGENCY LIGHTS AFTER 30 MINUTES. SATIS PER AMM 33-50-00-5.

Part: SLIDE — NO TEST (R1 DOOR)

INSPECTION TYPE:N/A R1 SLIDE WILL NOT PRESS TO TEST. DEFERRED IAW MEL 25-61-2 PLACARD INSTALLED. DEF 362353.

Part: RIB — CRACKED (RT WING) · airframe 48,115 hrs · 7,711 cycles

INSPECTION TYPE:2C RIGHT NR 16 SLAT TRACK INBOARD L/E RIB FITTING IS CRACKED. REMOVED AND REPLACED RIGHT NR 16 SLAT TRACK INBOARD L/E RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE)

INSPECTION TYPE:N/A L1 DOOR SLIDE ARMING LIGHT INOP. REPLACED BATTERY & REPLACED LIGHT BULBS. OPS TESTED, WORKING FINE. DEFERRAL CLOSED AND PLACARD REMOVED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

R1 DOOR EMERGENCY EXIT SIGN, HALF OF THE BULBS ARE BURNED OUT. RELAMPED, OPS CKS NORMAL IAW MM CH 33-50-00.