N375FE

Part: SKIN — GOUGED (BS 1210-1225) · airframe 95,711 hrs · 40,703 cycles

FUSELAGE SKIN GOUGED, COVERED BY THE RR BODY FAIRING, AT THE MID SECTION. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIG 6, VOL 1, 53-00-01, FIG.1A, HFEC IAW NTSPM 06-10-01-001. MAJOR REPAIR.

Part: HINGE — WORN (CENTR CARGO DOOR) · airframe 95,711 hrs · 40,703 cycles

CENTER CARGO DOOR FWD HINGE LOBE DIAMETER, FUSELAGE SIDE, EXCEEDED ITS WEAR LIMITS. REMOVED AND REPLACED CENTER CARGO DOOR FWD HINGE IAW AMM 52-32-04-2, AND SRM 51-31-01. OPS CHECK ACCOMPLISHED ON 52T3906. MAJOR REPAIR

Part: SWITCH — FAILED (R1 DOOR) · airframe 95,418 hrs · 40,520 cycles

DURING PREFLIGHT OF PUSH TO TEST SWITCH FOR THE R1 DOOR, THE SWITCH BROKE INTO PIECES.

Part: COALESCER BAG — DIRTY (ACM) · airframe 95,364 hrs · 40,489 cycles

DURING DESCENT THRU 13000 FT, FUMES FROM PACKS WERE EXCESSIVE. FOLLOWED QRH, NR 1 & 2 PACKS WERE ON. FIRST OFFICER DETECTED A MUSTY ODOR. REMOVED AND REPLACED DIRTY 1, 2, & 3 ACM COALESCER BAGS IAW AMM 21-54-03. INSPECTED PACKS FOR CONTAMINATION, NONE NOTED. COMPLIED WITH CLEANING IAW AMM 21-53-00-7, NO FAULTS NOTED

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 94,723 hrs · 40,135 cycles

NR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-12-01-2. REMOVED AND REPLACED MEC IAW AMM 73-20-01-2. PREFORMED A MAX POWER RUN IAW JRH CHP. 07. ALL POWER SETTINGS NORMAL, NO LEAKS NOTED.

Part: SLIDE — FAILED (L1 DOOR) · airframe 94,394 hrs · 39,964 cycles

WHILE TRYING TO PUT NEW ARD ON ACFT, FOUND L1 DOOR ARMED WENT THRU L2 DOOR AND AFTER TRYING TO RESET L1 DOOR BOTTLE BLEW AND SLIDE FELL OUT OF RETAINER CASE. REMOVED AND REPLACED THE L1 DOOR EVACUATION SLIDE CONTAINER IAW MM 25-61-01-2. OK FOR SERVICE

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 94,098 hrs · 39,783 cycles

R1 DOOR PNEUMATIC ASSIST BOTTLE HAS NO PRESSUE. REMOVED AND REPLACED THE DOOR ASSIST BOTTLE IAW MM 52-11-07-2. OPS CHECKED GOOD IAW AMM 52-10-01-2.

Part: SKIN — CRACKED (LT WING) · airframe 93,021 hrs · 39,200 cycles

LEFT WING, AT THE INBD SLAT AREA, L/E OF WING, THE NR 1 SLAT TRACK CUTOUT IS CRACKED AT THE LOWER INBD CORNER, THE CRACK IS APPROXIMATELY 1" LONG THE CRACK IS NEAR A PREVIOUS REPAIR. REMOVED OLD DOUBLER, FABED A NEW DOUBLER TO INCORPATE THE OLDER DAMAGE IN WITH THE NEW DAMGED AS 1 REPAIR IAW SRM VOL I, 57-10-00, FIG 68.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 93,021 hrs · 39,200 cycles

MAIN DECK FLOORBOARD BETWEEN STA 600-670 AND FROM LBL 75.5-LBL102 HAS PUNCTURE ABOARD, SEVERAL INSERTS DAMAGED. FABRICATED FLOOR PANEL ON T16/1211640. REMOVAL AND INSTALLATION IS COVERED ON RIM, FIT CARDS.

Part: COWLING — ABNORMAL (NR ENGINE) · airframe 918 hrs · 38,492 cycles

AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH COWLING. UNABLE TO GET A DETAILED CLOSER LOOK AT THIS TIME. ADDING PICTURES TO THE DISCREPANCY. REPLACED COWLING & HINGES.

Part: COWL DOOR — MISSING (NR 2 ENGINE) · airframe 918 hrs · 38,492 cycles

AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH COWLING. UNABLE TO GET A DETAILED CLOSER LOOK AT THIS TIME. ADDING PICTURES TO THE DISCREPANCY. DAMAGE FOUND WHERE LE OF FAN COWL REST ON IN TAKE TUBE AROUND 3 O CLOCK POSITION. PICTURES UPLOADED TO DAMAGE FILE, FURTHER DAMAGE EVALUATION REQUIRED. FAN COWL, HINGES & ALL ATTACH HARDWARE ORDERED.

Part: CYLINDER — LEAKING (NLG STEERING) · airframe 916 hrs · 38,352 cycles

AFTER TAKEOFF LEVEL 2 ALERT HYD 1 FAIL FLUID GONE IAW AMM 32-52-01-2-0. UPON ARRIVAL INTO GATE FOUND LT NOSE WHEEL STEERING CYLINDER LEAKING HYD FLUID. R & R LT NOSE WHEEL STEERING CYLINDER IAW AMM 32-52-01-2. LEAK CHECK & OPERATIONS CHECK GOOD IAW WRI 29-114664, 29-11 4665, 29-11 4666 FOR R & R OF NR 1 ENG EDP'S & HYDRO FILTERS. .

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 914 hrs · 38,249 cycles

LIGHT INDICATING L1 ENTRY DOOR IS DISARMED & DOES NOT ILLUMINATE WHEN THE DOOR IS DISARMED. RELAMPED L1 ENTRY DOOR, DISARMED LIGHT ASSEMBLY. LIGHT OPERATIONS CHECKED GOOD IAW AMM: 52-11-00.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 91,003 hrs · 37,912 cycles

WING ANTI-ICE DISAGREE AFTER TAKEOFF, FOLLOWED BY AIR SYS 1 OFF. AFTER CONSULTING MOC & GOC RETURNED. TROUBLESHOOTING IAW FIM 30-11 TASK 801. AIR SYS 1 OFF ALERT SUGGESTS USING FIM 36-23 TASK 803. FOUND FAULT BALL ON PNEUMATIC MANIFOLD FAULT INDICATOR PRESS SWITCH LT WING. ORDERED PRESS SWITCH. R & R LT WING MANIFOLD FAIL DETECT PRESS SWITCH IAW AMM 36-23-03-4-0. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (R1 DOOR) · airframe 90,800 hrs · 37,769 cycles

R1 DOOR ESCAPE SLIDE LOW PRESS INDICATOR PRESS TO TEST LIGHT INOPERATIVE. R & R R1 DOOR PRESS TO TEST SWITCH IAW SWPS. OPERATIONS NOW NORMAL. ACFT OK FOR SERVICE.

Part: BULB — FAILED (DOOR SLIDE) · airframe 90,626 hrs · 37,647 cycles

R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT NOT ILLUMINATING WHEN PUSHED. REMOVED AND REPLACED BULBS. CHECKED OK IAW AMM 25-61-03-5.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,424 hrs · 37,519 cycles

ON FINAL GOT NO GEAR DOWN & LOCKED INDICATIONS ON HANDLE OR EAD SYNOPTIC, LIGHTS ALL RED, WENT AROUND, RAN QRH GEAR LIGHTS ALL GREEN AFTER QRH. SUSPECT SWITCH INDICATOR AS MULTIPLE WRITE UPS. FAILED OPERATIONS CHECK & ORIGINAL UNIT REINSTALLED. TROUBLE SHOT PSEU THRU MCDU ALL SENSOR READ OUT & TARGETS READS OK. PERFORMED RTS ON PSEU ALL TEST PASSED, ATTEMPTED TO REPLACE PSE PRECAUTIONARY IAW TO 31-71-01-2 NEW UNIT FAILED OPS TEST WITH INTERNAL FAULT CODE 317046 ORIGINAL UNIT REINSTALLED & OPERATIONS CHECKED IAW MM 31-71-01-2. NO CURRENT FAULTS, TEST PASSED, ACFT OK TO CONTINUE SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,370 hrs · 37,483 cycles

LEFT MAIN GEAR RED LIGHT STAYED ON AFTER RETRACTION. COMPLIED WITH QRH & LIGHT WENT OUT ON SECOND TRY. TROUBLE SHOT IAW FIM 32-30-01. INSPECTED LT MLG HYD COMPONENTS & FOUND NO LEAKS OR OTHER DISCREPANCIES. PERFORMED BITE CHECK OF PSEU & FOUND NO CURRENT FAULTS & NO FAULT HISTORY. PSEU BITE CHECKS GOOD IAW AMM 31-71-01-2. INSPECTED UPLOCK SENSOR & WIRING & FOUND ALL INTACT & SECURE. LT MLG UPLOCK SENSOR OPERATIONS CHECKED GOOD IAW FIM 32-60-06. ACFT OK FOR SERVICE.

Part: BUSHING — MISSING (LT MLG) · airframe 90,370 hrs · 37,483 cycles

LT MLG UNSAFE AFTER TO. FLASHED ON & OFF DURING QRH CHECKLIST. REVIEWED PSEU CURRENT FAULTS, NONE REPORTED IN FAULT REVIEW. REPORTS OF LT GEAR UP & LATCHED, AB SENSOR DISAGREE. VERIFIED CLEARANCE BETWEEN SENSOR & TARGET, FOUND THE ATTACH BOLT FOR THE LINK WAS MISSING A BUSHING & TARGET ON THE DOOR WAS LOOSE. REPLACED BUSHING & TIGHTENED TARGET IAW SMP. OLD SENSOR UNBOLTED BUT WIRING STILL ATTACHED, NEW SENSOR IS BOLTED TO THE MOUNT & NEEDS WIRING RUN THRU CONDUIT & ATTACHED TO TERMINALS. WORK PERFORMED IAW AMM 32-61-15-4. COMPLETED TERMINATION OF PROX SENS D1-81 WIRES IAW SWP. COMPLETED INSTALLATION OF LT MLG UP LATCHED SENSOR IAW AMM 32-61-15-4. PERFORMED RTS PSEU, RTS PASSED, NO FAULTS REPORTED,

Part: AIU — FAILED (NR 2) · airframe 90,089 hrs · 37,293 cycles

RECEIVED A LEVEL ON, AIR SYS 2 OFF ALERT, FOLLOWED BY A LEVEL 3 AIR MANIFOLD 2 FAIL ALERT IN FLIGHT. RED MANIFOLD LIGHT FOR BLEED AIR 2. IAW QRH, THROTTLE IDLE, TEMP IN MANIFOLD 2 DECREASED. R & R NR 2 AIU IAW AMM 31-43-02-4. OPS CHECKED IAW AMM 31-43-02-5. SYSTEM OPS CHECKED NORMAL. NO FAULTS ON AIU 2. ACCOMPLISHED STEP 16 OF MTSI AND TESTED NR 2 SYSTEM LOOPS WITH THE TEST BOX. TEST BOX INDICATES THAT THERE IS A SHORT IN SYSTEM NR 2 LOOP APPROXIMATELY SECTION 536 OR 565. NSPECTED LOOPS IN THE AFT ACCESSORY COMPARTMENT. FOUND SUSPECT LOOP TO BE AFT OF LOWER AFT PRESSURE BULKHEAD JUST INSIDE ACCESS DOOR ON RT SIDE. TEMPORARILY INSTALLED NEW LOOP IAW AMM 36-23-02-4.

Part: UNKNOWN — MALFUNCTIONED (HORIZ STAB) · airframe 89,886 hrs · 37,162 cycles

REJECTED TAKEOFF DUE TO CAWS, STABILIZER MOTION, ALERT AT ABOUT 100KTS NOTICED STAB TRIM WAS 0.2 UNITS, GREATER THAN BEFORE TAKEOFF SETTING. ON SUBSEQUENT TAKEOFF NO CAWS. HOWEVER JUST PRIOR TO ROTATION, FIRST OFFICER NOTED THAT STAB TRIM HAD DECREASED BY 0.2 UNITS & THEN INCREASED BY 0.4 UNITS DURING ROTATION. COMPLIED WITH HIGH ENERGY STOP INSPECTION IAW MM05-56-00-6, CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH HORIZONTAL STAB ELEC CONTROL ADJUSTMENT TEST, CHECKED GOOD NO DEFECTS NOTED IAW MM27-41-00-5.

Part: TARGET — CONTAMINATED (MLG) · airframe 89,786 hrs · 37,091 cycles

LEFT MAIN GEAR UNSAFE ON RETRACTION. BOTH PRIMARY AND SEC. INDICATIONS UNSAFE WITH GEAR HANDLE UP, CYCLED GEAR IAW QRH. 3 SAFE INDICATIONS BOTH PRI AND SEC. ACCESSED PSEU THROUGH CFDS. FOUND FAULT CODE 317067 "PSEU NO CFDS DATA". TROUBLESHOT IAW MD10 FIM 31-71-07, REF CFDIU IAW FIM 45-45-06, NO FAULTS FOUND. CFDIU OPS CHECKS GOOD. PERFORMED PSEU R-T-S IAW AMM 31-71-01-2, PSEU OPS CHECKS GOOD. GAINED ACCESS AND INSPECTED LMLG UPLOCK PROX SWITCH IAW AMM 32-61-15-4, FOUND SENSOR CLEAN AND SECURE, FOUND TARGET CONTAMINATED WITH GREASE. CLEANED TARGET AND LUBED DOOR LINK. INSPECTED UPLOCK PROX SWITCH CONNECTIONS AT TERMINAL STRIP AND FOUND CLEAN AND SECURE. NO FAULTS FOUND, ALL INDICATIONS CHECK GOOD, ACFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — DIRTY (MLG) · airframe 88,222 hrs · 36,207 cycles

AFTER TAKE OFF, RAISED GEAR. LT MAIN HAD PRIMARY AND SECONDARY UNSAFE INDICATION. COMPLIED WITH QRH PROCEDURE AND CYCLED GEAR. NOW PRIMARY AND SECONDARY INDICATIONS UP AND LOCKED. LT GEAR UP AND LATCHED A/B SENSOR DISAGREE FAULT. CHECKED RTS ON PSEU BOX AND IT CHECKED NORMAL. CHECKED RIG ON ALL GEAR SENSORS AND THEY CHECKED NORMAL, PROXIMITY SENSOR READOUT WAS NORMAL. INSPECTED LT GEAR UPLOCK SENSOR AND WIRING AND CLEANED SENSOR. MM 31-71-01-2. OK TO CONTINUE.

Part: BLADE — DAMAGED (NR 3 ENGINE) · airframe 87,850 hrs · 35,991 cycles

ON POST FLIGHT, FOUND FOD DAMAGE TO NR 3 ENGINE FAN BLADE WITH BIRD REMAINS VISIBLE. PERFORMED FOD BOROSCOPE INSPECTION IAW MD10 AMM 72-00-00-6-1, FIG 609, ITEMS 5 AND 10 WITH NO LIMITING DEFECTS FOUND. PERFORMED FOD CLOSED COWLING INSPECTION IAW AMM 72-00-00-6-1, FIG 607, ITEMS 1 AND 2. THREE 1ST STAGE FAN BLADES FOUND DAMAGED. REMOVED AND REPLACED BLADES IAW AMM 72-21-00.

Part: SHEAR TIE — DAMAGED (BS 1801 L51L) · airframe 87,846 hrs · 35,983 cycles

AFT LOWER FUSELAGE AT STA 1801 L-51L HAS RIVET HEAD SHEARED. REMOVED FASTENERS AND DAMAGED SHEAR TIE IAW SRM 51-31-01. FABRICATED SHEAR TIE. TREATED, PRIMED AND TOPCOATED IAW SRM 53-30-00, SRM 51-21-01 AND SRM 51-21-02. INSTALLED SHEAR TIE IAW SRM 53-30-00 AND SRM 51-33-01. MAJOR REPAIR.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 87,846 hrs · 35,983 cycles

GOUGES IN RT OTBD FLAP LOWER SKIN WS 500 CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01, L=1.0" X W=.50" X D=.085". FABRICATED DOUBLER IAW SRM 57-10-00. INSTALLED DOUBLER IAW SRM 51-31-01.

Part: SEAT TRACK — DAMAGED (BS 1381) · airframe 87,846 hrs · 35,983 cycles

MAIN DECK SEAT TRACK STA 1381, LBL 75 FOUND TO HAVE BROKEN EARS. REMOVED DAMAGED SEAT TRACK SECTION BS 1371 TO 1409. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-70-00, FIG 1 AND SRM 51-31-01.

Part: LAMP — INOPERATIVE (INSTRUMENT PANEL) · airframe 86,446 hrs · 35,258 cycles

BOTH EMERGENCY POWER "OFF" AND "ON" LIGHTS INOPERATIVE REGARDLESS OFF BATTERY SWITCH POSITION. RELAMPED AFFECTED SWITCH LIGHTS IAW AMM 33-11-17-2-0. ALL OPS CHECKS NORMAL.

Part: HANDLE — OUT OF SEQUENCE (R1 DOOR ASSIST) · airframe 86,392 hrs · 35,226 cycles

DURING PREFLIGHT COULD NOT OPERATE DOOR R1, FOUND THE EMERGENCY BOTTLE HANDLE OUT OF SEQUENCE MEL 01APR11, 03:10 IAD R RELEASED FOR SERVICE IAW MEL: 52-10-03 CATEGORY: C EXPIRATION: 11APR11 "MEL 52-10-03: (IDENTIFY L1 OR R1) R1 MAIN ENTRY (IDENTIFY DOOR OR SLIDE/RAFT) RI (IDENTIFY INOP OR REMOVED)." CAT C.

Part: BULKHEAD — CRACKED (BS 1381-1401) · airframe 86,334 hrs · 35,198 cycles

CTR WHEEL WELL, RT SIDE WALL, BETWEEN STA 1381 AND 1401 LIGHTNING HOLE NEAR TOP HAS A CRACK COMING OUT OF IT. VERIFIED BY HFEC REPAIRED CTR WHEEL WELL RT SIDE WALL AT APPROX 1381 AND 1401, REF EA 8-5310-148492 AND EA 8-5310-149330.

Part: WEB — CRACKED (BS 1381-1401) · airframe 86,334 hrs · 35,198 cycles

CTR WHEEL RT SIDE WALL, BETWEEN THE SECOND AND THIRD STATIONS AFT OF THE FWD BULKHEAD APPROX STA 1381 TO 1401. THERE ARE 9 CRACKS IN A DOUBLER. REMOVED AND REPLACED BARREL KEEL SPLICE DOUBLER. REF SRM 51-33-01 VOL 2 AND E.A. 8-5310-149330 AND E.A. 8-5310-148492

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 2007 TO STA 2014 LONGERON 50R. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. SKIN REPLACEMENT CARRIED OUT IAW DWG AJC7207 REV FK AND SRM 51-31-01 VOLUME II, REV 96. EO 8-5100-7-5001, A7, PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: BULKHEAD — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LONGERON 42R AND LONGERON 43R. EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LONGERON 42R AND LONGERON 43R EVALUATED AND FOUND NOT IAW SRM REPAIR. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW EA 8-5310-132441. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 BETWEEN LONGERON 48R AND LONGERON 47L. EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 BETWEEN LONGERON 48R AND LONGERON 47L EVALUATED AND FOUND NOT CONFORM TO SRM. EXISTING REPAIR R & R WITH NEW REPAIR IAW E.A. 8-5330-138587. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (BS 495) · airframe 85,460 hrs · 34,744 cycles

FUSELAGE STA 495, BETWEEN LONGERON 25R TO LONGERON 27R, SKIN FOUND WITH DENT AND AN ELONGATED HOLE AFTER EXISTING TEMPORARY REPAIR DOUBLERS REMOVED. FUSELAGE STA 495, BETWEEN LONGERON 25R TO LONGERON 27R, SKIN REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 (SHEET 5) VOLUME I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110. REF TO WRI 53-30/8911 FOR WORK DETAILS.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L-31R. EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L31R EVALUATED AND FOUND NOT IAW SRM REPAIR. EXISTING REPAIR R & R WITH NEW REPAIR IAW EA 8-5330-138581 TITLE: MAINFRAMES - PLATES AND SKINS - PREVIOUS REPAIR AT STA 859 BETWEEN LONGERON 30 AND 31H. EO 8-5100-7-5001, A7 PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT WASTE TANK COMPARTMENT FRAME STATION 1986 L-50L TO L-50R. PRVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND REPLACED WITH NEW REPAIR AS PER SRM 53-30-00 FIG. 5 VOL. 1 REV. 96. EO 8-5100-7-5001 A7 PT2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: FLOORBEAM — MISREPAIRED (BS 979) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979. EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT INACCORDANCE WITH SRM REPAIR SCHEME. EXISTINGREPAIR REMOVED AND REPLACED WITH NEW REPAIR AS PER E.A. 8-5310-140395 & E.O. 8-5100-7-5001 A7 PT2 . REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 85,460 hrs · 34,744 cycles

EXISTING FLUSH REPAIR AT RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN XFS 289. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT AS PER E.A. 8-5510-132438. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE SKIN LOWER STA 795 BETWEEN LONGERON 49L AND LONGERON 50L. EXISTING REPAIR REMOVED AND REPLACED AS PER SRM 53-20-00 FIG 6 VOL 1 REV 96 EO 8-5100-7-5001 A7 PT1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (BS 919) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE SKIN BELLY STA 919, 6 O'CLOCK POSITION. EVALUATED PREVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND REPLACED AS PER SRM 53-20-00 FIG. 6 VOL. I REV. 96. E.O. 8-5100-7-5001 A7 PT1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (BS 859) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE ABOVE FWD LOWER CARGO DOOR CONTROL PANEL STA 859. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND CARRIED OUT REPAIR AS PER E.A. 8-5330-138581. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — UNKNOWN (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE UPPER SKIN STA 1771 BETWEEN LONGERON 4R TO LONGERON 5R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW SRM 53-20-00, FIG 6, VOL I, REV 96. EO8-5100-7-5001, A7 P1 TITLE: "STRUCTURES-REPAIR CATALOG - REPAIR IDENTIFICATION, CLASSIFICATION & TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14 CFR 121.368, 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: FRAME — MISREPAIRED (BS 899 L49-50L) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE FWD CARGO FLOOR LANDING STA 899 L-49L TO L-50L. EVALUATED AND FOUND NOT CONFORM TO SRM. REMOVED AND REPLACED WITH NEW REPAIR AS PER SRM 53-00-01 FIG 8 VOL 1 REV 96 EO 8-5100-7-5001 A7 P1 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: FRAME — MISREPAIRED (BS 919 L51L/R) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FWD CARGO FRAME STA 919, L-51L TO L-51R. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM. REMOVED AND AND NEW REPAIR ACCOMPLISHED PER SRM 53-00-01 FIG 8 VOL I REV 96 EO 8-5100-7-5001 A7 PT2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: LONGERON — DAMAGED (BS 879-899) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FWD CARGO STA 879 TO STA 899, LONGERON 51R. REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-10-00 FIG 2 VOL I REV 96 EO EO 8-5100-7-5001 A7 PT 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110. TO PERFORM INITAIL INSPECTION AT 15,000 FLIGHT CYCLE AND REPETITIVE INSPECTION AT 10,000 FLIGHT CYCLE.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE SKIN LOWER STATION 836 L-50R TO L-51R. EVALUATED AND FOUND NOT CONFORM TO SRM. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-20-00 FIG. 6 VOL. I REV. 96. E.O. 8-5100-7-5001 A7 PT1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REV 110.

Part: LONGERON — UNKNOWN (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FORWARD CARGO STATION 879 TO STATION 899 LONGERON 50R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-00-00 FIG 2 VOL I REV 96 EO EO 8-5100-7-5001 A7 PT 2.

Part: LONGERON — DAMAGED (BS 899-919) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FWD CARGO, STA 899 TO STA 919, LONGERON 52R. REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-10-00 FIG 2 VOL I REV 96 EO 8-5100-7-5001 A7 PT 2. EVALUATED AND FOUND NOT CONFORM TO SRM. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER MD10 SRM 53-10-00 FIG 2 VOL I REV 96. EO 8-5100-7-5001 A7 PT 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110. TO PERFORM INITIAL INSPECTION AT 15,000 FLIGHT CYCLE AND REPETITIVE INSPECTION AT 10,000 FLIGHT CYCLE.

Part: SKIN — DAMAGED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT FUSELAGE NR 3 PACK DOOR TOP AFT CORNER RIGHT HAND SIDE STATION 525 TO 545, L33R TO L34R. FUSELAGE NR 3 PACK DOOR TOP AFT CORNER RIGHT HAND SIDE STATION 525 TO 545, L33R TO L34R REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 3 VOL 1 REV 96 EO 8-5100-7-5001 A7 P1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — UNKNOWN (ZONE 600) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT RT WING TIP LWR SKIN XW931, 38" FROM AFT T/E. REMOVED AND REPLACED WITH NEW REPAIR AS PER EA 8-5710-140406 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOORBEAM — MISREPAIRED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR FOUND AT FORWARD CARGO COMPARTMENT FLOORBEAM FLANGE STATION 1059 RBL 24. EXISTING REPAIR FOUND AT FORWARD CARGO COMPARTMENT FLOORBEAM FLANGE STATION 1059 RBL 24. EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. REPAIR ON FLOORBEAM FLANGE STA 1059 RBL24 CARRIED OUT IN ACCORDANCE WITH E.A. 8-5310-140396. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (RWS 906) · airframe 85,460 hrs · 34,744 cycles

RT L/E LOWER ACCESS FWD CUTOUT AREA FOUND 01 EA EXISTING REPAIR INBD OF ACCESS PANEL 626FB. EXISTING REPAIR AT RT L/E LOWER ACCESS FWD CUTOUT AREA INBD OF ACCESS PANEL 626FB FOUND NOT CONFORM TO SRM. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW SRM 57-10-00, FIG 49, REV 96. EO 8-5100-7-5001 A7 PT2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: LONGERON — MISREPAIRED (BS 655-670) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR FOUND AT FORWARD CARGO STA 665 TO STA 670, LONGERON 45R. EXISTING REPAIR AT FWD CARGO STA 665 TO STA 670, LONGERON 45R EVALUATED AND FOUND NOT IAW SRM REPAIR. LONGERON REPAIR CARRIED OUT IAW EA 8-5310-138568 REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: RIB — MISREPAIRED (ZONE 600) · airframe 85,460 hrs · 34,744 cycles

RT NR 1 SLAT INBD FACE AREA FOUND 01 EACH EXISTING REPAIR. EXISTING REPAIR AT RT NR 1 SLAT INBD FACE AREA EVALUATED AND FOUND NOT CONFORMING TO SRM. EXISTING REPAIR R & R WITH NEW REPAIR IAW SRM 57-00-01, FIG 4, VOL I, REV 96 AND EA 8-5750-140394 EO 8-5100-7-5001 A7 PT2 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — UNKNOWN (NR 2 SLAT) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT RT WING NR 2 SLAT INNER SKIN XIS 260. EXISTING REPAIR AT RT WING NR2 SLAT INNER SKIN XIS 260 R & R WITH NEW REPAIR IAW SRM 57-00-01, FIG 4, VOL I, REV 96, EO 8-5100-7-5001, A7 PT 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — UNKNOWN (ZONE 600) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT RT WING NR5 SLAT L/E LOWER SKIN XORS 738. EXISTING REPAIR AT RT WING NR5 SLAT L/E LOWER SKIN XORS 738. R & R WITH NEW REPAIR IAW SRM 57-10-00, FIG 31, VOL I, REV 96, EO 8-5100-7-5001, A7 PT2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STA 1015 X=-8.5 SEAT TRACK FOUND DAMAGED. CARRIED OUT REPAIR AND SECTION SEAT TRACK REPLACED AT STA 989 TO STA 1029 IAW SRM 53-70-00 FIG 1, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (BS 2150 L8-9L) · airframe 85,460 hrs · 34,744 cycles

EXISTING REPAIR AT UPPER FUSELAGE SKIN STATION 2150 LONGERON 8L TO LONGERON 9L EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT ON UPPER FUSELAGE SKIN STATION 2150 LONGERON 8L TO LONGERON 9L AS PER MD10 SRM 53-00-01 FIG 4 VOL I REV 96. EO 8-5100-7-5001 A7 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.

Part: SKIN — DAMAGED (ZONE 500) · airframe 85,460 hrs · 34,744 cycles

LEFT INBOARD TRAILING EDGE FLAP LOWER SURFACE 01 EACH EXISTING REPAIR FOUND AT INBOARD LOWER SEGMENT AREA XIFH 150.300. EXISTING REPAIR AT LEFT HAND INBOARD TRAILING EDGE FLAP LOWER SURFACE INBOARD LOWER SEGMENT AREA XIFH 150.300 REMOVED AS PER MD10 SRM 51-35-02 VOL II REV 96. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER MD10 SRM 57-00-01 FIG 4 VOL I REV 96 EO 8-5100-7-5001 A7 PT2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 85,460 hrs · 34,744 cycles

RT OTBD T/E FLAP UPPER SURFACE 01 EACH FOUND CRACKED. ON SKIN LOCATION 12 INCH FROM INBD EDGE, 6 INCH FROM T/E. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 7, VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (ZONE 500) · airframe 85,460 hrs · 34,744 cycles

LT WING TIP UPPER SURFACE AT FWD SIDE FOUND DENTED. REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 4, VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 85,460 hrs · 34,744 cycles

RT INBD ELEVATOR TOP SURFACE INBD SIDE FOUND DENT. DENT MEASURED D = 0.055" 20 X D = 1.10 (MIN L) EXISTING L = 0.75" FOUND OUT OF LIMIT AS PER SRM 55-00-01 FIG 4A VOL I REV 96. NEW FILLER SKIN AND REPAIR SPLICE FABRICATED AND INSTALLED AS PER SRM 55-10-00 FIG 7 VOL I REV 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STATION 1219 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II REV 96. ORIGINAL THICKNESS = 0.147", REMAINING THICKNESS = 0.113", MATERIAL REMOVED = 0.034" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA NR 8-5710-132436, REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STATION 1212 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS:0.149", MATERIAL REMOVED: 0.040", REMAINING THICKNESS: 0.109" FOUND EXCEED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA NR 8-5710-132436. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1205 XCW=108 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.132", REMAINING THICKNESS = 0.106", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (CENTER WING) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STATION 1195 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV. 96. FOUND EXCEED LIMIT IAW SRM 57-20-00 FIG 8A, VOL I, REV 96.ORIGINAL THICKNESS: 0.143", REMAINING THICKNESS: 0.106", MATERIAL REMOVED 0.037". REPAIR CARRIED OUT IAW EA 8-5710-132436. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1229 XCW=105 - XCW=117 CTR WING UPPER AFT PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS = 0.150", REMAINING THICKNESS = 0.131", MATERIAL REMOVED = 0.019" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOLUME I REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1181 XCW=109 - XCW=111 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.133", REMAINING THICKNESS = 0.098", MATERIAL REMOVED = 0.035" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (BS 1229) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STA 1229 XCW=-97 - XCW=-105 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.147", REMAINING THICKNESS = 0.125", MATERIAL REMOVED = 0.022" FOUND EXCEEDED LI REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STA 1189 XCW=108 - XCW=111 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.132", REMAINING THICKNESS = 0.105", MATERIAL REMOVED = 0.027" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1219 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS = 0.148", REMAINING THICKNESS = 0.121", MATERIAL REMOVED = 0.027" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOLUME I, REV 96. REPAIR CARRIED OUT IAW EA NR8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1229 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.151", REMAINING THICKNESS = 0.120", MATERIAL REMOVED = 0.031" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STATION 1205 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV I 96. ORIGINAL THICKNESS = 0.142", REMAINING THICKNESS = 0.110", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STA 1195 XCW=108 - XCW=114 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II REV 96. ORIGINAL THICKNESS = 0.133", REMAINING THICKNESS = 0.112", MATERIAL REMOVED = 0.021" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: PANEL — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STA 1171 XCW=110 - XCW=114 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.130", REMAINING THICKNESS = 0.104", MATERIAL REMOVED = 0.026" FOUND EXCEEDED LIMIT IAW SRM 57-20-00. FIG 8A, VOL I, REV 96. REPAIR CARRIED OUT IAW EA NR 8-5710-132436, REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1236 XCW=104 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.155", REMAINING THICKNESS = 0.121", MATERIAL REMOVED = 0.034" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436. THIS REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1212 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.143", REMAINING THICKNESS = 0.102", MATERIAL REMOVED = 0.041" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOL I, REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CORRODED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN RT STA 1189 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.139", REMAINING THICKNESS = 0.107", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOLUME I REVISION 96. REPAIR CARRIED OUT IAW EA.NR 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 REV 110.

Part: WEB — CORRODED (ZONE 100) · airframe 85,460 hrs · 34,744 cycles

FWD CARGO DOOR LOWER SILL APPROX STA 899 WEB PLATE EDGE FOUND CORRODED. AREA TRIMMED OUT IAW SRM 53-00-01, VOL 1, REV. 96. REPAIR DOUBLER AND FILLER FABRICATED, FASTENERS HOLES TRANSFERRED, TREATED AND PAINTED IAW SRM 53-00-01, VOL. 1, REV. 96. REPAIR DOUBLER AND FILLER INSTALLED IAW SRM 51-35-01 VOL.II, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN - LEFT STATION 1275 X=117 UNDER FLOOR STRUCTURE SHEAR TIE FOUND CRACKED. SHEAR TIE REMOVED AND REPLACED PER SRM 51-31-01 VOL II REV 96. NEW SHEAR TIE FABRICATED PER DRAWING AEA 0343 REV T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: FRAME — CRACKED (BS 1721 S13R) · airframe 85,460 hrs · 34,744 cycles

CABIN - RT STA 1721, STR 13R FRAME FOUND CRACKED. REPAIRED IAW SRM 53-30-00, FIG 5, VOL I REVISION 96. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110. INITIAL INSP TO BE CARRIED OUT AT 12,000 CYCLES AND SUBSEQUENT REPITITIVE INSP TO BE CARRIED OUT AT 8,000 FLIGHT CYCLES.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON FIRST LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLE NR-A & NR-B. REPAIR CARRIED OUT IAW EA : 8-5310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON SECOND LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 5 LOWER JAMB FITTING AT HOLE NR-A. REPAIR CARRIED OUT IAW EA : 8-5310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON SECOND LAYER CHORD FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB FITTING AT HOLE NR-A AND NR-C. CRACKED BOLT HOLES NR A AND NR C (DIA =0.520") ON SECOND LAYER CHORD AT MAIN CARGO DOOR NR 1 LOWER JAMB FITTING AREA, BUSHING REPAIR CARRIED OUT IAW EA: 8-5310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON FIRST LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE NR-D. CRACKED BOLT HOLES NR D (DIA =0.520") ON FIRST LAYER BEAM AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AREA, BUSHING REPAIR CARRIED OUT IAW EA: 8-5310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON SECOND LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLE NR-D. REPAIR CARRIED OUT AS IAW EA : 8-5310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON FIRST LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLE NR-A, NR-B AND NR-C. REPAIR CARRIED OUT IAW EA 8-5310-132426, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV110.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 85,460 hrs · 34,744 cycles

CRACK INDICATION FOUND ON SECOND LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NO.6 LOWER JAMB FITTING AT HOLE NR-A. COMPLIED WITH EA 8-0310-132426. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 85,460 hrs · 34,744 cycles

CABIN LT STATION 1119 X=47.5 SEAT TRACK FOUND DAMAGED. DAMAGED SEAT TRACK AT CABIN STATION 1119 X=47.5 LT AREA CARRIED OUT REPAIR AND SECTION SEAT TRACK REPLACED AT STATION 1109 TO STATION 1129 X=47.5 IAW SRM 53-70-00, FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (LT NR 3 SLAT) · airframe 85,460 hrs · 34,744 cycles

LT WING FIXED L/E NR 3 SLAT TELESCOPIC UPPER DOOR CUTOUT OTBD AREA FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR 8-5710-132424, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (ZONE 600) · airframe 85,460 hrs · 34,744 cycles

RT FIXED L/E NR 3 SLAT TELESCOPIC DUCT UPPER DOOR CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5710-132425. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-110, REV 110.

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 84,360 hrs · 34,171 cycles

NR 1 ENG HIGH TEMP AT 1075 NO FUEL DUMP- NO EMERGENCY BUT IT DIDNT SEEM TO BE AN INDICATOR. CHECKED RESISTANCE OF NR 1 ENGINE EGT HARNESSES AND THERMOCOUPLE LEADS. ALL 4 SEGMENTS HAVE RESISTANCES THAT ARE OUT OF LIMITS PER MD10 MM 77-21-02-2. NR 1 ENGINE EGT HARNESS REPLACED AND INSTALLED PER MM 77-21-01-2. ALL INDICATIONS ARE NORMAL.

Part: CONTROL UNIT — INOPERATIVE (ANTI-SKID SYS) · airframe 83,475 hrs · 33,721 cycles

ANTI-SKID FAIL ALERT ON SHORT FINAL WENT AROUND RAN RED TABS WHICH HAD US DO ANTI-SKID TEST, ALERT WENT OUT. ALERT REAPPEARED ON NEXT GEAR EXTENSION. A/C C/W GO AROUND AND LANDED WITHOUT INCIDENT. T/S ANTI SKID FAULT CODES PER FIM 32-45-20. REMOVED AND REPLACED ANTISKID CONTROL UNIT PER MM 32-45-01-5. ALL TESTS PASSED. ACFT OK FOR SERVICE.

Part: ROD END — LOOSE (MLG HANDLE) · airframe 82,550 hrs · 33,263 cycles

AFTER ROTATION GEAR HANDLE DID NOT MOVE TO UP POSITION COMPLIED WITH QRH. GEAR HANDLE DID MOVE UP WITH HANDLE RELEASE BUTTON PUSHED. LANDED AT KLCK, FOUND ROD END AS DESCRIBED IN AMM 32-24-01-2 FIGURE 201 SHEET 1 AS ITEM "G" TO HAVE LOWER END DISCONNECTED FROM THE LINKAGE IT IS NORMALLY ATTACHED. ALL ATTACH HARDWARE WAS MISSING. FOLLOWING AMM 32-24-01-2 INSPECTED AND REATTACHED ROD END WITH NEW HARDWARE DESCRIBED IN THE ORIGINAL WRITE UP. INSPECTED THE GROUND SENSE MECHANISM AND SURROUNDING AREA PER THE DESCRIPTIONS IN AMM 32-24-01-2. ALL CHECKS NORMAL.

Part: SLIDE — FAILED (R1 DOOR) · airframe 82,009 hrs · 32,981 cycles

AFTER LANDING AND BLOCK-IN, COULD NOT GET R1 DOOR ELECTRICAL SWITCH TO ENGAGE. R-1 DOOR OPENED PNEUMATICALLY, SLIDE DEPLOYED BUT DID NOT INFLATE. INSTALLED SLIDE/CONTAINER ASSY REF AMM CH 25-61-01-2 RII:445700.

Part: BOLT — UNDERTORQUED (TE FLAP) · airframe 77,194 hrs · 30,802 cycles

MX FOUND BOLT INSTALLED IN INBOARD FLAP VANE INSTALLED, UNDER TORQUED. MX INSTALLED BOLT IN LEFT I/B FLAP VANE ATTACH POINTS.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 75,667 hrs · 30,097 cycles

COMPLY WITH E.A.8-5350-70377.FUSELAGE- LOWER CARGO DOOR- LOWER JAMB SKIN GOUGE REWORK. CLOSING ACTION ON 05/21/03. COMPLIED WITH E.A.8-5350-70377.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 75,667 hrs · 30,097 cycles

LT INBD FLAP TRACK UPPER ROLLER SURFACE WORN ALONG WITH SIDE ROLLER SURFACE. FOUND LT I/B FLAP TRACK UPPER ROLLER SURFACE ALONG WITH SIDE ROLLER SURFACE TO BE OUT OF LIMITS IAW DC-10 CMM 57-52-01 REMOVED AND REPLACED TRACK IAW M/M 51-32-01.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 75,667 hrs · 30,097 cycles

RT O/B FLAP UPPER O/B UPPER SURFACE HAS TWO DEEP GOUGES. CLOSING ACTION OM 05/20/03. REMOVED AND REPLACED RT O/B FLAP VANE IAW M/M 27-50-03-2.OP'S CHECK TO BE ACCOMPLISHED ON W/C E-8-5750-7-5000 PT2.

Part: HINGE — DAMAGED (LT WING TE FLAP) · corrosion level 2 · airframe 75,667 hrs · 30,097 cycles

S 26 COMPLY WITH E.A.8-5740-70391. WINGS LT I/B FLAP HINGE ASSY ATTACH LUG REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70391

Part: HINGE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 75,667 hrs · 30,097 cycles

S 20 COMPLY WITH E.A.8-5750-70378. WINGS-OUTBD FLAP RT-INBD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/NARC0502. CLOSING ACTION ON 05/13/03 COMPLIED WITH .8-5750-70378. WINGS-OUTBD FLAP R/H-INBD HINGE BRACKET-ACTUATOR ATTACH HOLE REPAIR P/N ARC0502.

Part: SKIN — CRACKED (ZONE 700) · airframe 75,667 hrs · 30,097 cycles

N 1059 SMALL WINGLET FAIRING AT TOP OF LT MLG STRUT DOOR IS CRACKED AND MISSING A PIECE. CHAFFED IN SEVERAL AREAS. CLOSING ACTION ON 05/13/03. REMOVED SKIN AND BACK PLATE IAW SRM 51-31-01. FAB NEW SKIN FROM 7075-T6.065, BATCH 0000509285 BACK PLATE FROM 2024-T3 .063 BATCH 0000545293. INSTALLED NEW SKIN AND BACK PLATE IAW SRM 51-31-01.

Part: HINGE — INOPERATIVE (RT WING TE FLAP) · airframe 75,667 hrs · 30,097 cycles

COMPLY WITH E.A. 8-5740-70384 WINGS- RT OUTBD FLAP, INBD HINGE ASSY P/N ARC1984. FACT 13MAY03 22:27 BFM R COMPLIED WITH E.A.# 8-5740-70384.

Part: COVER — CRACKED (COCKPIT WINDOW) · airframe 75,667 hrs · 30,097 cycles

CAPT'S SLIDING WINDOW LWR TRACK, FWD ATTACH COVER CRACKED. REMOVED PANEL IAW SRM 51-31-01. FAB NEW PANEL IAW DWG ABN7039. FROM 6061- 0.0.032. INSTALLED NEW PANEL IAW SRM 51-31-01.

Part: PLATE — CRACKED (NACELLE) · airframe 75,667 hrs · 30,097 cycles

NR 3 ENGINE O/B T/R TRANSILATING COWL UPPER SLEVE WALL PANEL CRACKED. REMOVED SIDEWALL PANEL PLATE IAW SRM 51-35-01. RECEIVED NEW PART ON TRAVELER T2/331654, LOCATED AND DRILLED HOLES IAW SRM 51-35-01, PRIMED IAW SRM 51-21-01, INSTALLED PLATE IAW SRM 51-35-01.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 75,667 hrs · 30,097 cycles

NR 1 PYLON AFT FAIRING O/B AFT SECTION CRACKED. NEW PART FAB ON TRAVELER T2/231892. INSTALLED IAW SRM 51-43-01.

Part: DOUBLER — CORRODED (BULKHEAD) · airframe 75,667 hrs · 30,097 cycles

IN CENTER ACCESSORY COMPT STA 1156, BULKHEAD BETWEEN LONGERONS L50-49, LT LOWER CORNER OF BATTERY HAS CORROSION AT DOUBLER. REMOVED DOUBLER IAW SRM 51-31-01. FAB NEW DOUBLER ON TRAVELER 2/330509. INSTALLED NEW DOUBLER IAW SRM 51-33-01. PAINTED AREA IAW SRM 51-21-01.

Part: ENGINE — FAILED (NR 1) · airframe 75,083 hrs · 29,803 cycles

IN CRUISE, FL 330, NR 1 ENGINE FAILED. OIL PRESSURE 0, OIL QUANTITY AND TEMPERATURE NORMAL. FUEL PRESSURE NORMAL. HYDRAULIC QUANTITY, PRESSURE AND TEMPERATURE NORMAL. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE. CLOSED COWLING IAW SMP. RAN NR 1 ENGINE IAW JRH, OPS CHECK AND LEAK CHECK NORMAL.

Part: PDU — FAULTY (THRUST REVERSER) · airframe 73,295 hrs · 28,958 cycles

UPON TAKEOFF PWR THE GREEN REVERSER LIGHT FLICKERED THEN ILLUMINATED STEADY, IT W/N EXTINGUISHED UNTIL PWR REDUCED TO IDLE. SYS TO BAD DRIVE UNIT. REMOVED AND REPLACED PDU PER DC10-10 MM 78-31-01-2, OPS CHECK GOOD.

Part: CONTROL BOX — FAULTY (COCKPIT) · airframe 73,295 hrs · 28,958 cycles

GREEN REVERSER THRUST LIGHT ILLUM AFTER APPLYING T/O POWER. REMOVED AND REPLACED MASTER WARNING CONTROL BOX PER DCN MM 33-15-01-2. OPS CHECK NORMAL.

Part: SPLICE — CRACKED (FUSELAGE)

CLG W/W COMPT LT SIDEWALL SPLICE DOUBLER IS CRACKED LOC AFT OF AIL/SPOILER DETRIM ACT.

Part: ENGINE — FIRE (NR 2 ENGINE) · airframe 72,372 hrs

NR 2 ENGINE FIRE ON T/O. FIRED FIRE BOTTLES.

Part: ENGINE — FIRE (NR 2 ENGINE)

NR 2 ENGINE FIRE AFTER LANDING.

Part: LONGERON — CORRODED (CARGO BAY)

SNRM N 215 CORROSION ON STR AT NR 49L BETWEEN BS 1811 TO 1841, JUST INSIDE AFT LWR CARGO COMP DOORWAY. *S/D* REMOVED AND REPLACED STR, SHEAR CLIPS, INTERCOSTAL PER SRM 51-00-01.

Part: ENGINE — MALFUNCTIONED (NR 1)

ON ROTATION AIRCREW HEARD LOUD NOISE, SEEMING TO ORIGINATE FROM LEFT SIDE OF A/C. NR 1 EGT AMBER O/H LIGHT ILLUM ON LANDING (AFT LAND). MEM TOWER SAW 2-3 ORANGE FLAMES COMING OUT OF NR 1 ENGINE. REPLACED ENGINE.

Part: BELLFRAME — CRACKED (BS 1781)

UPPER INTERNAL FUSELAGE AREAE BS 1781, LONGERON 13L, FUSELAGE BELL FRAME CRACKED. REMOVED AND REPLACED DAMAGED AREA PER SRM 53-30-00 FIG 5.

Part: FRAME — CRACKED (BS 1741)

REPAIR OF INTERNAL FUSELAGE AREA BS 1741 LONGERON 13L, FUSELAGE BELL FRAME CRACKED. REPAIRED PER SRM 53-30-00 FIG 5.

Part: STRUCTURE — CORRODED (L3 DOORWAY)

MAIN CABIN INTERIOR FUSELAGE BOX STRUCTURE ABOVE ENTRY DOOR L3, CORROSION ON TOP OF BOX STRUCTURE AND HARDWARE. *S/D* REMOVED CORROSION AREA BLENDED WITHIN LIMITS PER SRM 53-00-01 FIG 1A PG 6A. ALODINED AND PRIMED.

Part: BELLFRAME — CRACKED (BS 1761)

UPPER INTERNAL FUSELAGE BS 1761, LONGERON 13L BELL FRAME CRACKED.

Part: VANE — CRACKED (RT TE FLAP VANE)

RT O/B FLAP VANE UPPER EXTERNAL SURFACE BY NR 4 TRACK IS CRACKED APPROX 4 INCHES LONG AT THE EDGE OF RUB STRIP DOT NR 2. *S/D* REPAIRED PER SERVICE BULLETIN A57-110 PG 40. REPAIR IS IN COMPLIANCE WITH EO 8-5750-7-4319 PART 3 EOCN E4.