N277UP

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 61,520 hrs · 10,884 cycles

R1 DOOR SLIDE TEST LIGHT INOPERATIVE. R & R 2 EA 1.5 VOLT C CELLS BATTERIES AND REPLACED THE LAMP FOR THE PRESS TO TEST INDICATOR IAW WDM 25-61-01. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,433 hrs · 10,852 cycles

EMERGENCY LIGHT, BATTERY 1 LO LEVEL 1 ALERT, R & R EMERGENCY LT BATTERY CHARGER IAW MM 31-51-01. OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 60,980 hrs · 10,702 cycles

LEVEL 1 "AVIONICS FAN OVERD" DURING CRUISE FOUND UPPER MCD SEAL PULLED OUT. REINSTALLED IAW AMM 52-00-00. PERFORMED OPS CHECK OF AVIONICS COOLING FANS IAW KP 3764587, CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE. FIM 21-26-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING EMERGENCY LIGHT TEST, RECEIVED EMERGENCY LIGHT BATTERY 1 LOW MESSAGE. REPLACED BATTERY POWER SUPPLY IAW AMM 33-51-01-400-802. OPS CK NORMAL.

Part: SKIN — DELAMINATED (LT WING) · airframe 58,826 hrs · 10,157 cycles

INSPECTION TYPE:4C, DELAMINATED ON LOWER SURFACE OF LT INBD FLAP VANE NEAR XIFH 258. REPAIRED DELAMINATED IAW SRM 57-50-80, REPAIR 2, WET LAYUP.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 58,826 hrs · 10,157 cycles

INSPECTION TYPE:4C DELAMINATED ON LOWER SURFACE OF LT INBD FLAP VANE NEAR XIFH 200. REPAIRED LT INBD FLAP VANE LOWER SURFACE IAW SRM 57-50-80, REPAIR 2, WET LAYUP.

Part: ANGLE — CRACKED (BS 1278 L47R) · airframe 58,826 hrs · 10,157 cycles

DURING 4C INSPECTION, RT FRAME FITTING ANGLE CRACKED IN LOWER AUX FUEL TANK, BS 1278, L47R. REPLACED RT FRAME FITTING ANGLE IN LOWER AUX FUEL TANK, STA 1278, L47R IAW SRM 51-33-01.

Part: DOOR FRAME — CRACKED (R3 DOOR WAY) · airframe 58,074 hrs · 10,448 cycles

INSPECTION TYPE:4C, R3 DOOR LOWER FWD DOOR JAMB HAS CRACK AT LIGHTNING HOLE. ACCOMPLISHED REPAIR ON R3 DOOR LOWER FWD JAMB BS 1250 - 1256 IAW SRM 53-40-45, REPAIR 3, FIG 201, REV 55.

Part: ANGLE — CRACKED (BS 1278 L47L) · airframe 58,826 hrs · 10,157 cycles

DURING 4C INSPECTION, LT FRAME FITTING ANGLE CRACKED IN LWR AUX FUEL TANK BS 1278, L47L. REPLACED LT FRAME FITTING ANGLE IAW SRM 51-33-01.

Part: STRUCTURE — CORRODED (FUEL CELL) · airframe 58,826 hrs · 10,157 cycles

DURING 4C INSPECTION, DISCOVERED CORROSION ON CENTER WING TANK UPPER FWD AND CENTER SKIN BETWEEN XCW=-81 AND XCW=-100 AT STRINGER 15. ACCOMPLISHED REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN XCW=-81-XCW=-100 AT STRINGER 15 IAW EA 011-5730-01-A5292 AND EO 5730-54227-A

Part: TRACK — GOUGED (L1 DOOR) · airframe 58,826 hrs · 10,157 cycles

INSPECTION TYPE:4C, L-1 DOOR AFT UPPER BOGIE TRACK HAS MULTIPLE GOUGES. ACCOMPLISHED REPAIR ON L1 DOOR AFT UPPR BOGIE TRACK IAW EA 011-2511- 01-A5299 AND EO MD11-5320-54248-A.

Part: STRINGER — CRACKED (RT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, RT WING STRINGER 12 CRACKED AT XORS 623-653. REPAIRED IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (RT WING) · airframe 58,826 hrs · 10,157 cycles

DURING 4C INSPECTION, RT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIRED STRINGER IAW EA 011-5710-01-A5283, REV IR AND EO MD11-5710-54271-A.

Part: STRINGER — CRACKED (RT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, RT WING, STRINGER 10 CRACKED BETWEEN XORS 738 AND 773. REPAIRED IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

INSPECTION TYPE:4C, LT WING STRINGER 15 CRACKED AT STA, XORS 433 ACCOMPLISHED PERMANENT REPAIR ON LT WING STRINGER 15, STA XORS 433 IAW EA 011-5710-01-A5285, REV I/R AND EO 5710-54259-A.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, LT WING STRINGER 18 CRACKED NEAR XORS 264. FABRICATED AND INSTALLED REPAIR BETWEEN XORS 211-264 IAW SRM 57-00-03, REPAIR 3, FIG.201.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, LT WING STRINGER 10 CRACKED BETWEEN XORS 738-773. REPAIRED IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, FOUND LT WING STRINGER 12 CRACKED AT XORS 622-653. REPAIRED IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: TEE FITTING — CRACKED (BS 1158) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, FITTING CRACKED IN UPPER AUX FUEL TANK BS 1158. R & R FITTING.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

DURING 4C INSPECTION, LT WING STRINGER 18 CRACKED NEAR XORS 222. FABRICATED AND INSTALLED REPAIR BETWEEN XORS 211-264 IAW SRM 57-00-03, REPAIR 3 FIG 201.

Part: STRINGER — CRACKED (LT WING) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, LT WING LOWER STRINGER 31 AT XORS 1085 IS CRACKED. REPAIRED STRINGER IAW EA 011-5710-01-A5291-IR AND EO 5710-54275-A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 58,826 hrs · 10,157 cycles

INSPECTION TYPE:4C, LT WING INBD FLAP CENTER VANE TRACK CUTOUT GOUGED ON INBD AND OTBD SIDES, FWD AND AFT ACCOMPLISHED REPAIR ON LT WING INBD FLAP CENTER VANE CUTOUT SKIN AND RIB ASSY, INBD AND OTBD SIDES, IAW EA 011-5753-01-A5298, REV I/R AND EO 5750-54246-A.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 58,826 hrs · 10,157 cycles

DURING A 4C INSPECTION, LT WING INBD NR 1 SLAT LOWER SKIN CRACKED. REPAIRED IAW SRM 57-40-01. REPAIR 8, FIG 201, REV 55.

Part: SKIN — DAMAGED (RT WING TE FLAP)

RT WING INBD FLAP COVE PANEL HAS .1250 INCH HOLE, 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52758-A.

Part: SKIN — DAMAGED (RT WING TE FLAP)

RT WING I/B FLAP COVE PANEL HAS .1250" HOLE 120" FROM INBD EDGE. REPAIR IAW EO B747-5750-52755-A.

Part: SKIN — DAMAGED (RT WING TE FLAP)

RT WING INBD MID FLAP COVE PANEL HAS .1250 INCH HOLE 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52756-A.

Part: FAN — FAILED (E/E BAY)

ODOR OF SMOKE IN COCKPIT. FAN IN E & E BELOW CAPTAIN FAILED IN A NOISY STOP. 20 SECONDS LATER A SECOND FAN STARTED, SUSPECT NR 1 AVIONICS RACK FAN FAILED. R & R NR 3 AVIONIC FAN IAW AMM 21-26-02-400. OPS NORMAL. THIS CLEARS DMI M513783 & WAN 2073160. PLACARD REMOVED.

Part: SKIN — NICKED (LT WING TE FLAP) · airframe 56,604 hrs · 9,617 cycles

INSPECTION TYPE:1C, LT INBD FLAP LWR SKIN SURFACE HAS TWO NICKS AT APPX 58.5" FROM INBD EDGE. REPAIRED LT INBD LWR SKIN AT 58.5" FROM INBD EDGE REF SRM 57-50-01, REPAIR 1, FIG 201.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 56,604 hrs · 9,617 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E BEADED DOUBLER CRACKED 18" INBD OF NR 12 SLAT TRACK. REPAIRED RT WING L/E BEADED DOUBLER 18" INBD OF NR 12 SLAT TRACK REF SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,604 hrs · 9,617 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS 646 REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 643-648 IAW UPS EO MD11-5730-48222-A (MAJOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 56,604 hrs · 9,617 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS627. REPAIRED LT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 625-629 IAW EO MD11-5730-48222-A (MAJOR).

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 56,604 hrs · 12,907 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E XOS 613.1502, BEADED DOUBLER FOUND CRACKED. REPAIRED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,604 hrs · 9,617 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS696. REPAIRED LT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 692-698 IAW EO MD11-5730-48222-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,604 hrs · 12,907 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E XOS 640.7174 BEADED DOUBLER FOUND CRACKED. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS 640.7174 REF SRM 57-40-02, REPAIR 15, FIG 203.

Part: TRUNNION — CRACKED (NLG) · airframe 56,604 hrs · 12,907 cycles

INSPECTION TYPE:1C NLG LT TRUNNION CRACKED ON LOWER END. REPAIRED TRUNNION IAW SRM 53-10-14, REPAIR 2, FIG 202.

Part: SWITCH — FAILED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS TEST BUTTON INTERNALLY FAILED. R & R EMERGENCY EXIT LIGHT TEST SWITCH S1-402, OPS CHECKED GOOD IAW MM 33-50-00.

Part: BLEED VALVE — INOPERATIVE (APU)

WITH LEVEL II, AIR SYS 2 PRESSURE LOW ON DESCENT LEVEL II, AIR SYSTEM 1, PRESSURE LOW ILLUMINATED. EMERGENCY DECLARED. SHORTLY AFTER LEVEL II, AIR SYS 3, PRESSURE LOW (NO CABIN PRESSURE). ACCOMPLISHED EMERGENCY DESCENT. R & R APU LOAD BLEED VALVE IAW AMM 36-16-02.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS)

EXIT SIGN OVER R1 DOOR CAME OFF DURING FLIGHT. RESINTALLED R1 EXIT SIGN REF MM 33-52-05.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,037 hrs · 8,956 cycles

INSPECTION TYPE: 2C, RIGHT WING FIXED L/E COMPT BEADED DOUBLER CRACKED ABOVE INBD REFUEL PORT. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS610-616 IAW EO 5730-42916-C AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 54,037 hrs · 8,956 cycles

INSPECTION TYPE: 2C, LEFT INBD FLAP VANE LOWER SURFACE DELAMINATED, APPROX 21" INBD OF CENTER TRACK (XIFH192). REPAIRED LT INBD FLAP VANE LOWER SURFACE IAW SRM 57-50-80. REPAIR 2 WET, LAY-UP BONDED REPAIR.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,037 hrs · 8,956 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER ABOVE REFUEL PORT CRACKED. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS625-629 IAW EO MD11-5730-42916-C AND SRM 57-40-02 REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RWS 667-673) · airframe 54,037 hrs · 8,956 cycles

INSPECTION TYPE: 2C, RIGHT WING FIXED L/E BEADED DOUBLER CRACKED 2 PLACES THROUGH ACCESS PANEL 619DB (XOS667-673). REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS667-673 IAW EO MD11-5730-42916-C.

Part: WIRE — DAMAGED (FUSELAGE)

EMERGENCY DECLARED - RECEIVED LEVEL 3 CABIN SMOKE, LEVEL 2 SEL FADEC OFF AND SEVERAL LEVEL 1 ALERTS. SMOKE IN THE COCKPIT. ACFT OUT OF SERVICE. INSPECTION FOUND THE WIRES DAMAGED ABOVE R1 DOOR DROP CEILING PANEL. REPAIR OF THOSE WIRES C/O. COMPLIED WITH EO MD11-2000-43813-A. THOSE RELATED SYSTEMS CHECKED OK IAW EO MD11-2000-43813-A.

Part: VANE — DAMAGED (LT WING TE FLAP)

LT WING, OTBD FLAP VANE HAS DAMAGED LOWER SKIN 25.5" FROM OTBD EDGE. REMOVED DAMAGE AND REPAIRED IAW EO MD11-5750-43408-A.

Part: CHECK VALVE — FAULTY (NR 3 FUEL TANK)

EMERGENCY DECLARED - LVL 2 TANK WING OVERFILL TO FUEL INBALANCE, FUEL IMBALANCE. FUEL OFF SCHEDULE. NR 3 TANK GAUGE INDICATED 41.700. SUSPECT FLOAT SWITCH OR FILL VALVE AFTER CONFERMING WITH AMC SDF. COULD NOT FILL NR 3 TANK. FUEL WAS MOVING FROM UPR AUX TO NR3 W/AUX TRANSFER PUMPS ON AND NO FILL VLV OR FLOW INDICATION ON SYNOPTIC. T/S C/O AND PERFORMED FSC R-T-S-TEST IAW AMM 28-08-00-5, REV69, DATE11-0 1-10. FOUND SATIS. C/O FUEL QTY BITE TEST IAW AMM 28-41-00-5 REV69, 11 -01-10. FOUND SATIS. FOUND NR 3 TANK TRANSFER PUMP CHECK VLV AT FAULT. DEFERRED ITEM IAW MEL 28-22-4. DMP C/W. FOUND OK. DMI OPENED.

Part: CHECK VALVE — FAULTY (NR 3 FUEL TANK)

EMERGENCY DECLARED - LVL 2 TNK WING OVERFILL TO FUEL IMBALANCE, FUEL IMBALANCE. FUEL OFF SCHEDULE. NR 3 TANK GAUGE INDICATED 41.700. SUSPECT FLOAT SWITCH OR FILL VALVE AFTER CONFIRMING. COULD NOT FILL NR 3 TANK. FUEL WAS MOVING FROM UPR AUX TO NR 3 W/AUX TRANSFER PUMPS ON AND NO FILL VLV OR FLOW INDICATION ON SYNOPTIC. PERFORMED ADJUSTMENT TEST OF THE CROSSFEED MANIFOLD REF AMM 28 22 00 5. CHECKS GOOD, THIS CLEARS M448304.

Part: ADC — INOPERATIVE (COCKPIT)

AFTER T/O AIRSPEED DIFF OF 15KNTS CAPTAIN'S LOWER THAN F/O. DURING CLIMB AIRSPEED CLOSED TO WITHIN 5 KNOTS, CAPTAIN ALWAYS LOWER. AMBER IAS ALERT. PERFORMED PITOT STATIC LEAK CHECK IAW AMM 34-11-00-2, LEAK CHECK WAS GOOD, FOUND A SPLIT BETWEEN CAPT'S AND F/O'S AIRSPEED INDICATION. R & R NR 1 ADC IAW AMM 34-16-01-4 AND 34-16-01-5, ALL CHECKS ARE GOOD.

Part: SUPPORT — CRACKED (NACELLE) · airframe 51,796 hrs · 8,427 cycles

INSPECTION TYPE:1C, NR2 ENGINE INLET HAS METAL STRIP CRACKED AT TWELVE 12 O`CLOCK POS. TRIMMED OUT DAMAGE ON CRACKED FLANGE OF NR2 INLET SUPPORT ANGLE AT STA 2166 AT 12:00 POS. FABRICATED ANGLE, FILLER AND EXTERNAL REPAIR D DOUBLER AND INSTALLED REF EO MD11-5410-41229-A AND STA, SA EA 011-5400-01-A2846.

Part: DOUBLER — CRACKED (RT WING LE SLAT) · airframe 51,796 hrs · 8,427 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E COMPARTMENT, BEADED DOUBLER INBD OF SLAT TRACK NR 17, FOUND WITH SUSPECTED CRACK AT 2 LOCATIONS XOS 698.5-703. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 51,796 hrs · 8,427 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E COMPARTMENT, THRU ACCESS PANEL 619EB, BEADED DOUBLER FOUND CRACKED AT 2 LOCATIONS AS MARKED XOS 643.5-647. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: COMPUTER — FAULTY (FLT CONTROL)

ATB - BOTH AUTO PILOT FAIL TO ENGAGE. RECYCLE CBS NO HELP. FOUND FCC 1 CURRENT FAULT IRU-1, IRU-2, IRU-3, AND FCC-1. ALSO FCC-2 CURRENT FAULT IRU-1, IRU-2, IRU-3, AND FCC-2. PERFORMED FCC-1 AND FCC-2 AFS RTS TEST AND AUTOLAND TEST. ALL TEST PASSED IAW AMM 22-01- 01-5.

Part: SWITCH — INOPERATIVE (R1 DOOR SLIDE)

R1 DOOR SLIDE REWORK INDICATION SWITCH LIGHT REMOVED WITH UPPER DOOR LINING UNDER DEFERRED IAW MEL 25-61-2 DMP C/W. CONTROL NR M424413 ASSIGNED. R&R BATTERIES AND TESTED IAW MM 25-61-04-4. THIS CLEARS M424413. OPS CHECK GOOD.

Part: DISPLAY — INOPERATIVE (COCKPIT)

DIVERSION - F/O'S MCDU SCREEN WENT BLANK, UNABLE TO RESTORE. DEFERRED D422762 ASSIGNED. SWAPPED NR 2 & NR3 IAW MM 31-65-01-4. NR 2 MCDU OPS CHECK NORMAL. TRANSFER NR 3 MCDU TO MEL 31-65-1-5 AND RTS PASSED.

Part: SLIDE — FAULTY (R1 DOOR)

INSPECTION TYPE:N/A ON PDC FOUND R1 DOOR EVAC SLIDE REMOTE PRESS INDICATING SYSTEM ALWAYS ILLUMINATED. REPLACED R1 SLIDE ASSY PER AMM 25-61-01-4. M411057 CLEARED

Part: SWITCH — INOPERATIVE (DOOR SLIDE)

ON PRE-FLIGHT FOUND RT FWD ENTRY DOOR SLIDE PUSH-TO-TEST INOP M410106. DEFERRED RT FWD ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PUSH-TO- TEST INDICATION SYSTEM PER MEL 25-61-2. COMPLIED WITH DMP 25-61-2. BOTTLE PRESSURE CHECKS OK.

Part: SKIN — DELAMINATED (AILERON) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C RT OUTBOARD AILERON P/N NRC6741-504, S/N 0043 T/E "T" SECTION IS DELAMINATED FROM WEDGE LOWER SURFACE. REMOVED AND REPLACED DELAMINATED SECTION OF COMPOSITE SKIN ON RT OUTBOARD T/E WEDGE, 82.5 INCHES FROM THE OUTBOARD END AND 36.5 INCHES AFT OF THE FWD HINGE LINE PER DAC DWG SG11570003, UPS EO MD11-5750-35098-A, AND SAA EA 011-5751-01-A2046.

Part: SKIN — DENTED (TE FLAP) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C SMALL DENT ON UPPER SKIN I/B FLAP LT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-00-01 FIG 201 REPAIR 1 SHEET 1 OF 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 277-F1-05 CENTER FUSELAGE SKIN APPROX BETWEEN STA 1139 AND 1159 AND BETWEEN L-41R AND L-43R IS NOT CORRELATED TO SRM MD11 5300-01 FIG 201. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW IPXA EO MD11-5330-35044-A AND SAA 011-5330-01- A2033.

Part: SKIN — CRACKED (RT WING) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C RT WING TELESCOPIC DUCT CUTOUT I/B UPPER CORNER CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-40-01 REPAIR 10, FIGURE 201.

Part: SKIN — CRACKED (LT WING) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C LEFT WING FIXED L/E 2 EA CRACK AT TELESCOPIC DUCT CUTOUT UPPER LT AND RT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW MD-11 SRM 57-40-01 REPAIR 10 FIG 201.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 48,920 hrs · 7,737 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 277-F1-03 EXISTING REPAIR AT LT LOWER AFT CARGO DOOR APPROX BETWEEN STA 1926 AND 1953 AND BETWEEN INTERCOSTAL NR 4 AND LOWER PAN DOES NOT CORRELATE TO SRM MD-11 52-10-00 FIG 5 REV 40. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5231-01-A2030 AND UPS EO MD11-5230-35096-A.

Part: SKIN — GOUGED (FUSELAGE)

INSPECTION TYPE:N/A DENT IN FUSELAGE FWD OF FWD CARGO DOOR CONTROL. FOUND DENT TO ALSO HAVE A GOUGE. BLENDED GOUGE PER SRM 53-00-01. DENT/GOUGE IS 2 X 3 X .092 INCH DEEP. HFEC AREA PER PART 6-51-0001. NO CRACK NOTED. THICKNESS REMAINING IS .056. PERFORMED INTERNAL HFEC PER MD11 DTSPM 06-10-01.001. NO CRACKS NOTED.

Part: POWER SUPPLY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTING INOP REF M394199. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY. THIS CLEARS M394199.

Part: COVER — DEFECTIVE (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR EXTERNAL CONTROL SW COVER W/N LATCH. RE-SECURED L-1 LATCH COVER AS REQUIRED SRM 51 31 01 VOL II.

Part: INDICATOR — NO TEST (LT DOOR SLIDE)

LEFT ENTRY DOOR SLIDE PUSH TO TEST LIGHT WILL NOT ILLUMINATE. R&R L1 SLIDE PRESSURE INDICATOR ASSY IAW AMM 25-61-15-4. OPS CHECK SATISFACTORY.

Part: STRUCTURE — CRACKED (RT WINGLET) · airframe 46,209 hrs · 7,065 cycles

INSPECTION TYPE-C, RT WING LWR WINGLET FOUND CRACKED AT AFT FITTING. DURING BOROSCOPE INSPECTION. RT WING LOWER WINGLET CRACKED AFT FITTING REPLACED IAW EO MD11-5720-276 80-A APPENDIX E.

Part: STRUCTURE — CRACKED (LT WINGLET) · airframe 46,209 hrs · 7,065 cycles

INSPECTION TYPE-C, LT WING LOWER WINGLET FOUND CRACKED AT AFT FITTING DURING BOROSCOPE INSPECTION. LT WING LOWER WINGLET CRACKED AFT FITTING REPLACED IAW EO MD11-5720- 27680-A APPENDIX D.

Part: FUEL TANK — LEAKING

ATB - PASSING 15000, RECEIVED A FUEL QUANTITY/USED CHECK LEVEL 2 ALERT. POSSIBLE FUEL LEAK. RAN CHECKLIST AND DETERMINED THERE WAS A LOSS OF FUEL. A/C BLOCKED IN WITH 89,600 LBS REMAINING FUEL. FUEL USED WAS 22,440 LBS TOTAL FUEL = 112,040 LBS. A/C INITIALLY FUELED TO 122,988 LBS. COMPLIED WITH FIM 28-14-00 FIG 102 SHEETS 9810. NO FAULTS FOUND. NO ALERTS PRESENT AT BLOCK IN.

Part: HANDLE — INOPERATIVE (LANDING GEAR)

LANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. PERFORMED CHECKLIST, GEAR WOULD NOT RETRACT. FOUND RT TRUCK BEAM ACT PRESS RELIEF VALVE AND ONE WAY RESTRICTOR FAILED. BOTH REPLACED IAW AMM 32-37-01 AND 04. ALSO REPLACED TWO-WAY RESTRICTOR AND TRIM ACTUATOR. SYSTEM BLEEDING AND LEAK CHECK PERFORMED. LANDING GEARS SWING TEST PERFORMED. ALL ARE OK.

Part: BATTERY — DISCHARGED (EMERGENCY EXIT)

ALERT MSG "EMER LT BAT 1 LO" DISPLAYED DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED EMERG LIGHT BATTERY PER 33-51-01, OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 1 PYLON)

INSPECTION TYPE:N/A NR 1 ENGINE OUTBOARD PYLON HAS 1.5 INCH CRACK THRU A RIVET. REPAIRED PER SRM 54-00-01.

Part: SMOKE BARRIER — TORN (COURIER COMPT)

INSPECTION TYPE:N/A SMOKE SCREEN ON CARGO ACCESS DOOR TORN IN THE COURIER COMPT. SECURED SLIDING RIGID CARGO BARRIER BY MD11 MM 59-16 PG 401.

Part: FITTING — CRACKED (ZONE 500) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, LEFT WING LEADING EDGE NR 16 TRACK ROLLER FITTING FOUND CRACKED. LEFT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. LEFT WING LEADING EDGE NR 16 SLAT TRACK FITTING REMOVED PER SRM 51-33-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. LEFT WING L/E NR 16 SLAT TRACK ROLLER SUPPORT FITTING REPLACED PER SRM 51-35-01 V.2 R.35. LEFT WING NR 16 SLAT TRACK INSTALLED PER AMM 27-80-32-R.50.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 29 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 29 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 29 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 29 LEFT PER EO MD11-5510-19409-H & EN 1308-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 32 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 32 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 32 LEFT & INSTALLED SLEEVE BUSHING PER EOMD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 LT PER EO MD11-5510-19409-H & EN 1309-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C HORZ STAB NR 34 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 34 RT REMOVED, BLENDED AND REAMED TO 1.162 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 34 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 34 RT IAW EO MD 11-5510-19409-H AND EN:1307-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C HORZ STAB NR 31 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLEND AND REAMED TO 1.178 INCH AT B/N HOLE NR 31 RT FOUND OUT OF LIMITS. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 31 RT IAW EO MD11-5510-19409-H. REPAIR C/OUT AT B/N HOLE NR 31 RT IAW EO MD1 1-5510-19409-H AND EN:1302-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 4 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED BLEND & REAMED TO 0.974 INCH AT BARREL NUT HOLE NR 4 RIGHT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 4 RIGHT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 4 RIGHT FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:1303-04 FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 19 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 19 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 19 RIGHT INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 19 RIGHT PER EO MD11-5510-19409-H & EN 1295-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORZ STAB NR 13 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AMD BEARING SURFACE CORROSION AT B/N HOLE NR 13 RT REMOVED, BLENDED AND REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 13 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 13 RT IAW EO MD 11-5510-19409-H AND EN:1297-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 35 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 35 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 35 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 35 LEFT PER EO MD11-5510-19409-H & EN 1298-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORZ STAB NR 4 LT BARREL NUT HOLE FOUND CORRODED AT BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 4 LT REMOVED, BLENDED AND REAMED TO 0.944 INCH, FOUND OUT OF LIMIT FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 4 LT IAW EO MD11-5510-19409-H. REPAIR CUT OUT AT B/N HOLE NR 4 LT IAW EO MD 11-5510-19409-H AND EN:1296-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 16 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL BEARING SURFACE. CORROSION AT NR 16 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 16 RIGHT & INSTALLEDD SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 16 RIGHT PER EO MD11-5510-19409-H & EN 1299-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 23 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 23 LT, REMOVED, BLENDED & REAMED TO 1.067 INCH. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H AT BARREL NUT HOLE NR 23 LEFT. REPAIR CUTOUT AT BARREL NUT HOLE NR 23 LEFT, FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:1289-04 & FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 26 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 26 LT AT BEARING S/W BLENDED & REAMED TO 1.067 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING AS PER EO MD11-5510-19409-H. PR1 422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 26 LT AS PER EO MD11-551 0-19409-H & EN:1291-04, FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 26 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 26 RIGHT REMOVED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING FAB PER EO MD11-5510-19409-H. APPLIED SEALANT PR142 2B1/2 & INSTALLED PER SLEEVE BUSHING AT BARREL NUT NR 26 RIGHT PER EO MD11-5510- 19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 26 RIGHT FOUND WITHIN LIMIT PER EO MD11 -5510-19409-H & EN:1287-04 & SATISFACTORY.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 32 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 1.178 INCH FOUND OUT OF LIMIT AT BARREL NUT HOLE NR 32 RT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 32 RT PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 RT PER EO MD11-5510-19409-H & EN: 1294-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 17 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT NR 17 LT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 17 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 17 LT PER EO MD11-5510-19409-H & EN 1288-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 14 LEFT BARREL NUT FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSION REMOVED & REAMED TO 0974 INCH AT BARREL NUT HOLE NR 14 LEFT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED PR1422B1/2 AT BLEND OUT AREA AT BARREL NUT HOLE NR 14 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 LEFT PER EO MD11-5510-19409-H & EN 1290-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 31 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 31 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 31 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 31 LEFT PER EO MD11-5510-19409-H & EN 1292-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 20 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 20 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 20 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 20 RIGHT PER EO MD11-5510-19409-H & EN 1284-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 36 BARREL NUT RIGHT FOUND CORRODED AT BOTTOM S/W & BEARING SURFACE. CORROSION AT NR 36 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 0.100 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING AT BARREL NUT HOLE NR 36 RIGHT CLEANED, SMOOTHED & PROTECTED PER SRM 51-21-01 V2R35. EXISTING SLEEVE BUSHING INSPECTED & REUSED. APPLIED 1422B1/2 & BARREL NUT INSTALLED PER MD11-5510-19409-H & FOUND WITHIN LIMIT AS PER EN:1286-04.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 14 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.988 INCH AT BARREL NUT HOLE NR 14 RT, FOUND OUT OF LIMIT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H & EN:1283-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 25 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 25 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 25 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BULKHEAD NUT HOLE NR 25 RIGHT PER EO MD11-5510-19409-H & EN 1270-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 34 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 34 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 34 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 34 LEFT PER EO MD11-5510-19409-H & EN 1282-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: WINDOW FRAME — CORRODED (ZONE 210) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, COCKPIT CORROSION ON BEARING SURFACE OF SUPPORT FRAME FOR LEFT NR 1 WINDSHIELD. COCKPIT BEARING SURFACE OF SUPPORT FRAME CORROSION REMOVED PER SRM 51-21-01 V.2R.35.V. INSPECTION CUT OUT ON TAE REWORK AREA FOUND CORROSION FREE. NEW FILLER FAB & INSTALLED PER EN1313-04. TASK ACCOMPLISHED OF REMOVING CORROSION AT COCKPIT BEARING SURFACE OF SUPPORT FRAME FOR LT NR 1 WINDSHIELD FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORZ STAB NR 22 LT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT B/N HOLE NR 22 LT REMOVED, BLENDED AND REAMED TO 1.067 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 22 LT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 22 LT IAW EO MD11-5510-19409-H AND EN:1271-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE-C, HORZ STAB NR 21 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 21 RT BARREL NUT HOLE REMOVED, BLENDED AND REAMED TO 1.067 INCH. FOUND OUT OF LIMIT FAB SLEEVE BUSHING IAW EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 21 RT AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 21 RT IAW EO MD11-5510-19409-H AND EN 1248-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 30 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 30 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 30 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 30 LEFT PER EO MD11-5510-19409-H & EN 1252-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORZ STAB NR 33 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE CORROSION REMOVED, BLEND AND REAMED TO 1.162 INCH AT B/N HOLE NR 33 RT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 33 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 33 RT IAW EO MD11 -5510-19409-H, EN:1253-04, FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 15 RIGHT BARREL NUT HOLE FOUND CORRODED ON SIDEWALL, BOTTOM AND BEARING SURFACE. CORROSION AT NR 15 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 15 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 15 RIGHT PER EO MD11-5510-19409-H & EN 1249-04 FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORZ STAB NR 15 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLENDED AND REAMED TO 1.067 INCHES AT B/N HOLE NR 15 LT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 15 LT IAW EO MD11-5510-19409-H. REPAIR C/OUT AT B/N HOLE NR 15 LT IAW EO MD11-5510-19409-H AND EN:1272-04 FOUND WITHIN LIMIT AND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 18 RIGHT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT NR 18 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 18 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 18 RIGHT PER EO MD11-5510-19409-H & EN 1247-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 1 RIGHT BARREL NUT HOLE FOUND CORROSION ON BOTTOM S/W & BEARING SURFACE. CORROSION AT NR 1 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 1.549 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT AFFECTED BARREL NUT HOLE NR 1 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT NR 1 BARREL NUT HOLE RIGHT PER EO MD11-5 510-19409-H & EN1256-04, FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 2 BARREL NUT HOLE RIGHT FOUND CORRODED ON BOTTOM & BEARING SURFACE. CORROSION AT NR 2 BARREL NUT HOLE RIGHT, BLEND, REMOVED & REAMED TO 1.035 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11-55 10-194O9-H & EN:1255-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 9 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2, AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510- 19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510-19409-H & EN:1 250-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 6 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. PR1422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 6 LEFT PER EO MD11-5510-1 9409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 6 LEFT FOUND WITHIN LIMIT PER EO MD11- 5510-19409-H & EN:1254-04 FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C, HORIZONTAL STAB NR 27 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 27 LT REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 27 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 27 LT PER EO MD11-5510-19409-H & EN 1251-04, FOUND WITHIN LIMIT & SATISFACTORY.

Part: SUPPORT FITTING — CRACKED (SLAT TRACK) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, RIGHT WING LEADING EDGE SLAT TRACK NR 16 ROLLER SUPPORT FITTING CRACKED. RIGHT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. RIGHT WING LEADING EDGE NR 16 TRACK FITTING REMOVED PER SRM 51-33-01, 51-35-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. RIGHT WING L/E NR 16 SLAT TRACK ROLLER SUPPORT FITTING REPLACED PER SRM 51-35-01 V.2.R35. RIGHT WING NR 16 SLAT TRACK INSTALLED PER AMM27-80-32-R.50.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, STA Y 695 TO 755 SEAT TRACK FOUND CORRODED AT STA X=-27.50. CORROSION AT SEAT TRACK STA Y695-755 AT X=-27.50. CORROSION REMOVED FOUND EXCEEDED LIMIT. ORI,THK=0.100 INCH & REMAIN THK=0.050 INCH. NEW SEAT TRACK & SPLICE FAB AS PER SRM 53-70-00, F1, V1, R35. NEW SEAT TRACK & SPLICE INSTALLED AT STA Y695-755 AS PER SRM 53-70-00 F1, V1, R35, FOUND SATISFACTORY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE:C STA Y 755 TO 859 X=-27.50 SEAT TRACK FOUND CORRODED. CORROSION AT SEAT TRACK STA Y755-859 AT X=-27.50 REMOVED FOUND EXCEED LIMIT. ORI THK=0.08 INCH & THK REMAIN=0.041 INCH. NEW SEAT TRACK & SPLICE FAB & INSTALLED PER SRM 53-70-00 F1, V1, REV 35, FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 34,333 hrs · 5,038 cycles

INSPECTION TYPE: C, HORIZONTAL STAB NR 1 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT NR 1 BARREL NUT HOLE BEARING S/W SURFACE REMOVED & REAMED TO 1.549 INCH, FOUND OUT LIMITS. FAB SLEEVE BUSHING PER EO MD11-5510-19409- H. PR1422B1/2 SEALANT APPLIED AT BLEND OUT AREA & INSTALLED SLEEVE BUSHING AS PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 1 LT IS WITHIN LIMITS AS PER EN1273-04.