N383FE

Part: SWITCH — OUT OF ADJUST (L1 DOOR) · airframe 97,520 hrs · 41,280 cycles

PDIS 383 52-10 7066 08FEB19 MEM FACT U LOGPAGES:3071704 DOOR L1 WILL NOT CLOSE ALL THE WAY LIGHT SHOWING AT THE TOP MEL 08FEB19 15:43 MEM U RELEASED FOR SERVICE PER MEL : 52-10-01 CATEGORY : C EXPIRATION : 18FEB19 "MEL 52-10-01: L1 ELECTRIC DOOR ACTUATOR - INOP. FOR EMERGENCY EGRESS, USE PNEUMATIC SYSTEMTO OPERATE DOOR." FACT 10FEB19 16:48 MEM U AMM: 52-11-00-5-0 MD10 REACTIVATED L1 DOOR FROM M.E.L. CONFIG. FOUND CLOSE LIMIT SW OUT OF ADJ. ADJ CLOSE LIMIT SW. L1 DOOR UNDERFAIR NOW IN LIMITS.

Part: SKIN — CRACKED (LT AILERON) · airframe 97,074 hrs · 41,011 cycles

DURING LT WING O/B AILERON INSTALL L/E FORWARD I/B SKIN IS CRACKED. ACCOMPLISHED EA 8-5750-T0342670, WINGS - FLIGHT SURFACES - LT WING, O/B AILERON, L/E I/B SKIN CRACK - PARTIAL SKIN REPLACEMENT REPAIR - COVER EA MAJOR REPAIR.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 97,074 hrs · 41,011 cycles

RT INBD ELEVATOR LWR SURFACE HAS (1 EACH ) DENTS. EVALUATED DENT RT I/B ELEVATOR LWR SURFACE, FOUND TO BE OUT OF LIMITS IAW SRM 55-00-01 FIG 1A. REPAIRED DENT IAW SRM 55-00-01 FIG NR 3. REF EA 8-5520-T0342588. STABILIZERS - ELEVATORS - RT I/B ELEVATOR, LWR SURFACE DENT - SRM REPAIR RSC TRACKING. MAJOR REPAIR.

Part: SUPPORT — DAMAGED (ZONE 200) · airframe 97,074 hrs · 41,011 cycles

MAIN CARGO COMPARTMENT FLOOR STRUCTURAL SUPPORT IS BROKEN LOCATED AT BODY STATION 1259 AT RH SIDE X82 AT AREA LOCATED UNDERNEATH MAIN CARGO COMPT. FLOOR PANELS 252LF AND 262BF. REMOVED CRACKED ANGLE FLOOR SUPPORT IAW MD-10 SRM 51-31-01. RECEIVED FABBED FLOOR SUPPORT ON TRAVELER # T18/1366685 LOCATED, DRILLED AND DEBURRED HOLES IN FLOOR SUPPORT IAW MD-10 SRM 51-31-01. TREATED AND PRIMED FLOOR SUPPORT IAW MD- 10 SRM 51-21-01. INSTALLED FABBED FLOOR SUPPORT IAW MD-10 SRM 51-31-01.MAJOR REPAIR

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 97,074 hrs · 41,011 cycles

AFT CARGO AT STA 1787 RBL 10 BELOW FLOOR PNL, FRAME LOWER AREA HAS CORROSION. REMOVED AND REPLACED LOWER J-ANGLE AT AFT CARGO PIT STA 1781 RBL 10 BELOW FLOOR PNL FRAME IAW SRM 51-33-01. MAJOR REPAIR.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 97,074 hrs · 41,011 cycles

LOWER FWD CARGO DOOR CUT OUT AFT LOWER SECTION PREVIOUS REPAIR SKIN EDGE HAS GOUGED. REMOVED EXISTING REPAIR DOUBLER LWR FWD CARGO DOOR CUT OUT IAW SRM 51-31-00. INSTALLED REPAIR DOUBLER LWR FWD CUTOUT IAW SRM 53-20-00. THIS IS A CLASS 2 REPAIR. MAJOR REPAIR.

Part: NONE — NONE · airframe 96,968 hrs · 40,935 cycles

TANK 3 TIP TRAPPED & TNK 3 FUEL QTY LO ALERT AT CRUISE FUEL QTY- 21.0K, QRH COMPLIED WITH. ELECTED TO PUT FUEL SYSTEM MANUAL AND TRANSFER FUEL FROM TANK NR 2. ALERT WENT AWAY. FUEL SYSTEM BACK TO AUTO. ALERTS RETURN DURING ARRIVAL AND APPROACH. FUEL QTY 16K. EMERGENCY DECLARED WITH ATC. LEAK CHECKED IRW MM 28-00-00-2-1. LEAK CHECK GOOD. REMOVED, REPLACED, AND INSPECTED TRANSFER FLOAT VALVE AND TRANSFER VALVE, INSPECTED IRW MM 28-21-10-2. OPS CK GOOD. REMOVED REPLACED AND INSPECTED TRANSFER FLOAT VALVE MOTIVE SHUTOFF VALVE, TRANSFER SHUTOFF VALVE, AND JET PUMP IRW MM 28-21-10-2/ 28-21-11-2 OPS CHECK GOOD. REMOVED AND REPLACED FLOAT SWITCHES (S1-122), S1-124), (S1-178) IRW 28-43-01-2. OPS CHECK GOOD. INSPECTED WIRING IRW WDM 28-41-08. NO DEFECTS NOTED

Part: HEAT EXCHANGER — FAILED (NR 2 ENGINE) · airframe 96,794 hrs · 40,815 cycles

DURING CLIMBOUT, THE NR 2 ENGINE OIL TEMP PEAKED AT 184 DEGREES IN THE RED BAND AND ALSO RECEIVED A LEVEL 2 ALERT FOR NR 2 ENG OIL TEMP HIGH. SHUTDOWN THE NR 2 ENGINE ALL OTHER ENGINE PARAMETERS NORMAL. NO VIBRATIONS. COMPLETED INSTALLATION OF THE NR 2 ENGINE FUEL/OIL HEAT EXCHANGER IAW AMM 79-20-03-2. DRY MOTORED THE NR 2 ENGINE IAW JRH. LEAK CHECKED GOOD. ACCOMPLISHED MPA RUN IAW JRH. ALL PARAMETERS WITHIN LIMITS.

Part: FLOAT — INOPERATIVE (NR 3 TIP TANK) · airframe 96,476 hrs · 40,616 cycles

NR 3 TANK PUMPS OFF, NR 3 TANK TIP TRAPPED FUEL, 5800 LBS IN TIP TANK IS UNUSABLE. NR 3 TANK FUEL QTY LOW. 7600 - 7200 - 7800 TIP TANK AMBER. COMPLIED WITH PRELIMINARY INSPECTION AS REQUIRED. NO DISCREPANCIES NOTED. REMOVED AND REPLACED THE RT OTBD FUEL FLOAT SWITCH IAW AMM 28-43-01-2, REV 19. OPS & LEAK CHECKED GOOD.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 95,418 hrs · 39,974 cycles

AT FLT LEVEL 370, HEARD A LOUD BANG AND NOTICED THE NR 2 ENGINE STALLED & N1 DECREASED TO 30%. DESCENDED TO FL 310 & RAN QRH FOR ENGINE COMPRESSOR STALL & WAS ABLE TO REGAIN NORMAL ENGINE OPERATION FOR APPROXIMATELY 5 MINUTES, WHEN THE NR 2 ROLLED BACK AGAIN TO 30% N1. SECURED THE ENGINE IAW QRH. DECLARED AN EMERGENCY & DIVERTED. R & R THE NR 2 ENGINE.

Part: CHANNEL — CRACKED (NR 2 PLYON) · airframe 95,060 hrs · 39,786 cycles

NR 2 ENGINE PYLON HAS A CRACKED HAT CHANNEL ON THE RT SIDE, PS 270. REMOVED THE DAMAGED HAT CHANNEL. LOCATED, DRILLED, AND TRIMMED A NEW HAT CHANNEL. PAINTED IAW SRM 51-21-01. INSTALLED IAW EA 8-5430-T0330704 REV A, AND IAW SRM 51-31-01VOLUME II. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (ACM DOOR) · airframe 94,457 hrs · 39,480 cycles

NR 3 ACM DOOR 114AR UPPER CENTER STR CRACK. R & R DAMAGE INTERCOSTAL WITH NEW ONE, IAW DWG ACA3820.

Part: VANE — PUNCTURED (RT WING TE FLAP) · airframe 94,457 hrs · 39,480 cycles

.250 INCH PUNCTURE FOUND ON LOWER SIDE OF RT OTBD FLAP VANE. REPAIRED THE FLAP VANE IAW SRM 51-71-00 VOL 2.

Part: LONGERON — DAMAGED (BS 595) · airframe 94,457 hrs · 39,480 cycles

BULKHEAD BS 595 LT SIDE LONGERON 38L IS DAMAGED. LONGERON REPAIRED IAW SRM 53-10-00 VOL 1 FIG 2 SHT 1

Part: SLEEVE — CRACKED (HORIZ STAB) · airframe 94,457 hrs · 39,480 cycles

HORIZONTAL STABILIZER CONSTANT SECTION BEARING, SLEEVE UNDER LT PIVOT BEARING SHAFT CRACKED IN 2 PLACES. NOTE: IPC REF 55-51-01-01, ITEM 270 MM, REF: 55-51-01-2. REMOVED SLEEVE AND BOLT , INSPECTED AREA, NO NOTED DEFECTS, INSTALLED NEW BOLT AND SLEEVE PER AMM 55-51-01-21

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

MAIN CARGO DECK STA 675, LBL 88 FOUND CORROSION ON FLOOR SUPPORT 5121819. REMOVED DAMAGED FLOOR SUPPORT, VERIFY MATERIAL 7075-T6, REF DWG WSP07111. TRANSFER HOLES TO NEW FLOOR SUPPORT REF DWG WSP0711. OK TO ALODINE AND FRAME PRIME. ALODINE & FRAME PRIMED IAW SRM 51-21-01, VOL II. OK TO INSTALL. FLOOR SUPPORT INSTALLED IAW DWG WSP0711.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

CENTER CARGO COMPARTMENT BILGE STA 1661, ABOVE L52, FRAME J-CHANNEL CORRODED. REPAIRED IAW EA 8-5310-T0327297 P-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

CENTER CARGO COMP BILGE BS 1621 ABOVE L52 FRAME CHANNEL CORRODED. REPAIRED IAW EA 8-5310-T0327270.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

CENTER CARGO COMP BS 1641 ABOVE L52 FRAME CHANNEL CORRODED. REPAIR IAW EA 8-5310-T327294B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK STA 1997, 5 LBL SEAT TRACK HAS CORROSION THROUGH FASTENER HOLE MARKED. R & R SEAT TRACK SRM 51-31-01, VOL II.

Part: SKIN — DAMAGED (BS 1621-1721) · airframe 94,457 hrs · 39,480 cycles

UPPER FUSELAGE, EXTERIOR SKIN, 6 EACH RIVET HEADS BURNED/MELTED. LOCATED BETWEEN BS 1621-1721 AT LONGERON 1L. POSSIBLE LIGHTNING EXIT POINTS. REMOVED RIVETS BURNISHED MINOR DAMAGE PER SRM 51--00-01 VOL1. REAMED RIVET HOLES TO .245 AND COMPLIED WITH NDT. INSTALLED LOCK FASTENER IAW SRM 53-20-00 FIG13 SHEET 1 VOL 1.

Part: SKIN — CORRODED (BS 1542) · airframe 94,457 hrs · 39,480 cycles

LOWER FUSELAGE LEFT SIDE, LONGERON 48, BS 1542, SKIN AREA JUST ABOVE BEAUTY STRIP IS CORRODED. REMOVED THE CORROSION AND TREATED SKIN IAW SRM 51-21-01

Part: SKIN — CORRODED (BS 1733) · airframe 94,457 hrs · 39,480 cycles

LONGERON 48, BS 1733 SKIN AREA JUST ABOVE BEAUTY STRIP IS CORRODED. CLEANED THE CORROSION AND TREATED IAW SRM 51-21-01.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK HAS BROKEN LUGS AT LOCK POSITION, STA 1140 AT LBL 48 R & R SECTION OF ELECTRICAL SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1. VOL 1.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

LEFT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A TWO INCH CRACK TERMINATING AT THE RADIUS AND .9 ' CRACK AT THE UPPER ADJECENT FASTENER HOLE. REPAIRED IAW EA 8-5310-T0326744.

Part: SEAT TRACK — DAMAGED (BS 620-630) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK DAMAGED FROM BS 620 - 630 LBL 48. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 VOL1.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 94,457 hrs · 39,480 cycles

L-1 DOOR SLIDE WAS INCORRECTLY INSTALLED FROM STATION "IND" AND RE-SECURED AT STATION "BDL". MAINTENANCE FOUND THE SLIDE PINS AND CHORDS DISASSEMBLED UPON REMOVING AND ARE REPLACING THE SLIDE DURING C-CHECK FOR THE EVACUATION SLIDE WORK CARD 52C1501. R & R SLIDE WITH A NEW SLIDE PACK.

Part: SEAT TRACK — DAMAGED (BS 745-765) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK DAMAGED AT BS 755 LB L48. REMOVED AND REPLACED DAMAGED SECTION OF THE SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK STA 1950, 22LBL SEAT TRACK HAS CORROSION NEAR FASTENER HOLE, MARKED. R & R SEAT TRACK IAW SRM 51-31-01, VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK STA 1997, 5 LBL SEAT TRACK HAS CORROSION THROUGH FASTENER HOLE, MARKED. R & R IAW SRM 51-31-01, VOL II.

Part: SEAT TRACK — WORN (BS 760) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK IS WORN BEYOND LIMITS AT BS 760 LBL 75.25 AT LOCK POSITION. REPAIRED THE SEAT TRACK IAW SRM 51-70-00 FIG 1 VOL II.

Part: SEAT TRACK — BROKEN (BS 760) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK HAS A BROKEN LUG AT BS 760 LBL 47.50 AT LOCK POSITION. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — WORN (BS 1510-1670) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK HAS CORROSION AT LBL 6 APPROX BS 1531. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — WORN (BS 1510-1670) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK HAS CORROSION AT LBL 6 APPROX BS 1581 - 1600. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-01 VOL 1.

Part: SEAT TRACK — WORN (BS 1470-1510) · airframe 94,457 hrs · 39,480 cycles

MAIN DECK SEAT TRACK HAS CORROSION AT LBL 24 BS 1610. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: TRANSMITTER — INOPERATIVE (FLAP HANDLE) · airframe 94,353 hrs · 39,414 cycles

DURING FLAP RETRACTION AFTER TAKEOFF, GOT A FLAP DISAGREE ALERT, FLAPS WERE UNRESPONSIVE TO FLAP HANDLE MOVEMENT. R & R FLAP HANDLE POSITION HANDLE TRANSMITTER IAW MM 27-54-03-4. PERFORMED ADJUSTMENT & TEST IAW MM 27-50-00-5. ALL TEST PASSED.

Part: MEC — INOPERATIVE (NR 1 ENGINE) · airframe 94,040 hrs · 39,263 cycles

ON APPROACH, NR 1 THROTTLE WOULD NOT GO BELOW 65% N, AT THE IDLE STOP F FLOW 2350 RAN THE ENG. SHUTDOWN IN FLIGHT CHECK LIST. R&R THE ENGINE NR 1 MEC PER AMM 73-20-01-2 AND ADJUSTMENT AND TEST PER EO 8-7320-7-5000 C. RAN ENGINE PER JRH CHPT 7.7. ENGINE LEAK CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 930 hrs · 38,701 cycles

DURING EMER LIGHT TEST, RECEIVED LEVEL 1 FAULT, EMER BATT 1 LO, ALERT. R & R EMER LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-4-1. OPERATIONAL CHECK NORMAL OF EMER LIGHTING SYS.

Part: TRANSMITTER — INTERMITTENT (TE FLAP SYSTEM) · airframe 928 hrs · 38,601 cycles

AFTER TAKEOFF WHEN FLAPS WERE RETRACTED, RECEIVED A MOMENTARY LVL 2 FLAP DISAGREE. WENT AWAY ALMOST IMMEDIATELY. DURING SLAT RETRACT SLATS RETRACTED & OTBD FLAPS EXTEND TO 6 DEG. USED QRH & EXTENDED SLATS, NO ROLLING MOVEMENT. QRH PROCEDURE TO EXTEND FLAPS TO 50 DEG. SET LANDING FLAPS, USED A MOMENTARY FLAP OVER SPEED OF 5 KTS AT FLAPS 35 DEG WAS EXPERIENCED. A FLAPS 35 DEG LANDING WAS MADE. DURING TAXI IN FLAPS FLUCTUATED BETWEEN 35 DEG & 40 DEG. RETURNED & LANDED WITHOUT INCIDENT. TROUBLESHOT IAW FIM 27-50-00-2 TASK 806. ALL FLAP POSITION INDICATIONS ON FCC1 AND FCC2 READOUTS WERE WITHIN LIMITS. DUE TO BEING INTERMITTENT, REMOVED AND REPLACED THE LT FLAP POSITION TRANSMITTER IAW AMM 27-54-02-4.

Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 923 hrs · 38,325 cycles

AIRCRAFT FUME EVENT DURING CLIMB OUT. DIRTY SOCK OR MOLDY CHEESE SMELL CONSTANTLY FROM 4000' THROUGH 10,000' ON CLIMB OUT. THIS SMELL IS CAUSED BY ENG OIL OR HYD FLUID LEAKING INTO THE PNEUMATIC SYS & THEN BEING THERMALLY DECOMPOSED. THESE FUMES CAN BE HARMFUL TO HEALTH.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

RIGHT MLG AFT TRUNNION LUGS HAVE CORROSION, AFT TRUNNION FWD LUG HAS CORROSION IN ITS BORE & AFT FACE, AFT TRUNNION AFT LUG HAS CORROSION IN ITS BORE. REMOVED CORROSION AFT TRUNNION FWD LUG BORE IAW SRM 57-20-00. BORE FOUND TO BE OUT OF LIMITS MEASURING 4.176 IAW FIG 23 OF SRM 57-20-00. REMOVED CORROSION FROM AFT FACE AFT TRUNNION & LUG BORE. AFT FACE & BORE FOUND TO BE WITHIN LIMITS IAW SRM 57-20-00. COMPLIED WITH EA 8-5740-T0310906 REV NO PS P1 FOR AFT TRUNION FWD LUG. MAJOR REPAIR.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 91,800 hrs · 37,990 cycles

LEFT WING FLAP TRACK FAIRING 536ER REPAIR WASHER DISBONDED. FAIRING 536ER WAS FOUND TO BE DELAMINATED BEYOND SRM 57-00-01 REPAIRABLE LIMITS. REMOVED ALL DAMAGE, FABRICATED FILLER & DOUBLERS & REPAIRED IAW EA 8-5710-T0310303 REV NR PS P1. MINOR REPAIR.

Part: LATCH — DAMAGED (RT ELEVATOR) · airframe 91,800 hrs · 37,990 cycles

RIGHT DETACHABLE ELEVATOR HAS BROKEN FWD LATCH PIN HANDLE. R & R LATCH ASSEMBLY IAW SRM 51-31-01. REPAIRED DAMAGED LATCH SUPPORT CHANNEL FOUND DURING INITIAL INVESTIGATION IAW SRM 51-31-01. TWO EACH INTERCOSTALS & ONE CHANNEL FABRICATED ON T14 1085322, T14 1085321 & T141 1085588. LATCH CHECKED GOOD IAW AMM 27-30-03. EA 8-5520-T0310748 REV NO PS P1 GENERATED FOR TRACKING RSC. MAJOR REPAIR.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

CENTER CARGO COMPARTMENT ROLLER TRAY HAS CORROSION AT X 48 INCHES BETWEEN STATION 1761 - 1781. REMOVED CORROSION FROM ROLLER TRAY, MATERIAL ORIGINAL .080 INCHES, MATERIAL LOSS .030 INCHES, MATERIAL REMAINING .050 INCHES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 01 FIG 1A. REMOVED ROLLER TRAY FROM STATION 1701 - 1781 IAW SRM 51-31-01. REMOVED ROLLER GUIDE STOP IAW SRM 51-31-01. REMOVED CORROSION FROM GUIDE STOP ORIGINAL MATERIAL .100 INCHES, MATERIAL LOSS .040 INCHES, REMAINING MATERIAL 060 INCHES. FOUND TO BE OUT OF LIMITS. FABRICATED NEW ROLLER TRAY NEW PART MATERIAL PN S4929250-12000. DRILLED, LOCATED & INSTALLED NEW ROLLER TRAY & STOP GUIDE IAW SRM 51-31- 01. ROLLER TRAY & STOP GUIDE TREATED & PRIMED IAW SRM 51-21-01. TOP COATED IAW SRM 51-21-02. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

AFT CARGO COMPARTMENT RT FLOOR SUPPORT HAS CORROSION AT STATION X=-60 BETWEEN STATION Y 1801 - 1841. REMOVED CORROSION IAW SRM 51-16-01, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1C PG 13. DIM L=3 INCHES, W=2 INCHES, D=.025 INCHES. FABRICATED NEW FLOOR SUPPORT ON T14 1084369. R & R FLOOR SUPPORT IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

CORROSION AT FASTENER HOLES, FWD PIT FLOOR FRAME STATION 879, LT TO RT. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1A SH 1. R & R FLOOR SUPPORT IAW SRM 51-31-01. FLOOR SUPPORT FABRICATED FROM S2929841-12000, BATCH 0002672891. MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

CENTER WING LOWER BOX LT SIDE AT STATION 1216 SPLICE LOWER SKIN HAS BULGING & UNDERNEATH THE SKIN HAS CORROSION, AS MARKED. SPLICE REPAIR AT STA 1216 ACCOMPLISHED IAW EA 8-5710-T0310385 REV NR WINGS-BASIC WING STRUCTURE-CENTER TANK STRINGER EXFOLIATION. MAJOR REPAIR

Part: WEB — CRACKED (LT MLG WW) · airframe 91,800 hrs · 37,990 cycles

LEFT MLG WW CUT OUT OTBD WEB AFT OF DOOR TANG IS CRACKED. REMOVED RIB WEB & ZEE ANGLE BOTH CRACKED IAW SRM 51-31-01. RECEIVED RIB WEB ON T14 1082623 & ZEE ANGLE T14 1082624. DRILLED, LOCATED, COUNTERSUNK & DEBURED IAW SRM 51-31-01. TREATED & PRIMED, RIB & ZEE ANGLE IAW SRM 51-21-01. TOP COATED IAW SRM 51-21-02. PART MARKED ZEE ANGLE & RIB WEB IAW GMM 7-0-1001. INSTALLED IAW SRM 51-31-01. TOP COATED FASTENERS IAW SRM 51-21-02. MAJOR REPAIR.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 91,800 hrs · 37,990 cycles

NUMBER 3 PYLON WEB AT PYLON STATION YN 240 THE OTBD SIDE IS CRACKED. REMOVED WEB IAW SRM 51-31-01. FABRICATED WEB ON T14 1085372 MATERIAL 7075.063 BATCH 0002072617. LOCATED & DRILLED WEB IAW SRM 51-31-01. TREATED & PRIMED IAW SRM 51-21-01. INSTALLED NEW WEB IAW SRM 51-31-01. REMOVED & REINSTALLED SEVEN EACH BRACKETS IAW SRM 51-31-01. MAJOR REPAIR

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

FORWARD CARGO COMPARTMENT CEILING, FLOORBEAM TO CGO DOOR UPPER BOX ATTACH FITTING HAS CRACK STATION 874. REMOVED TWO EACH BRACKETS FOR ACCESS IAW SRM 51-31-01. REMOVED CRACKED TEE FITTING IAW SRM 51-31-01. FOUND SMALL BRACKET REMOVED FOR ACCESS TO HAVE ELONGATED HOLES. FABRICATED NEW BRACKET ON TRAVELER T14 1083750. FABRICATED NEW TEE FITTING ON TRAVELER T14 1084262. LOCATED & DRILLED NEW BRACKET & TEE FITTING IAW SRM 51-31-01. TREATED & PRIMED NEW BRACKET & TEE FITTING IAW SRM 51-21-01. INSTALLED TEE FITTING & TWO EACH BRACKETS IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

AFT CARGO COMPARTMENT RT FLOOR SUPPORT HAS SEVERAL SPOTS OF CORROSION AT STATION X=-60" BETWEEN STATION Y1841 - 1902. FOUND FLOOR SUPPORT CRACKED TO BE OUT OF LIMITS. REMOVED IAW SRM 51-31-01. FABRICATED ONE EACH NEW FLOOR SUPPORT T14 1084929. LOCATED, DRILLED & INSTALLED NEW FLOOR SUPPORT AT STATION 1841 - 1902 IAW SRM 51-31-01. MAJOR REPAIR.

Part: STANCHION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

AFT CARGO COMPARTMENT STANCHION HAS CORROSION AT STATION X=-20, STATION Y1967. REMOVED STANCHION, WEB, ANGLE TO GAIN ACCESS. REMOVED CORROSION FROM STANCHION, ORIG MAT .063, REMAINING MAT .045, OUT OF LIMITS. WEB WAS CRACKED OUT OF LIMITS. FABRICATED NEW STANCHION USING S252585 EXT BATCH 1905847. FABRICATED WEB ON T14 1084839. TREATED, PRIMED & INSTALLED NEW STANCHION, NEW WEB & ANGLE IAW SRM 51-312-01 53-00-01 FIG 1C & 51-21-01 MAJOR REPAIR.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

AFT PIT LT LOWER TRANSITION PANEL HAS CRACK AT STATION 1851. R & R TRANSITION PANEL IAW SRM 51-31-01. FABRICATED NEW TRANSITION SUPPORT PN FX- AGA3857-1 TRAVELER T14 1083344, BATCH 0002623803. LOCATED & DRILLED IAW SRM 51-31-01. TREATED & PRIMED IAW SRM 51-21-01. INSTALLED NEW TRANSITION SUPPORT PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

MAIN CABIN SEAT TRACK X=76.25 AT STATION 1259 GOUGED. CHECKED LIMITS ORIGINAL MATERIAL .145 MAT.035 INCHES LOSS REMAINING MATERIAL .110 INCHES OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG 5 SHEET 1 - 2. REMOVED DAMAGED SEAT TRACK 1249 - 1286 LBL 76.25 IAW SRM 53-70-00 SHEET 3. FABRICATED NEW SEAT TRACK MAT 60-10964 BATCH 2064395 & TWO EACH SPLICE HAT SECTION TRAV T14 1083343. LOCATED & DRILLED PARTS IAW SRM 51-31-01. TREATED & PRIMED IAW SRM 51-21-01 & INSTALLED ALL MATERIAL REPAIR PARTS IAW SRM 51-31-01 & SRM 53-70-00 FIG 1A. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

AFT CARGO COMPARTMENT LT FLOOR SUPPORT HAS SEVERAL SPOTS OF CORROSION AT STATION X= 50 BETWEEN STATION Y1902 - Y1964. REMOVED CORROSION & CHECKED LIMITS, ORIGINAL MATERIAL IS .050 INCHES IAW SRM VOLUME III 53-16-01, FIG 6, MATERIAL MEASURED .034 INCHES TOTAL MATERIAL REMOVED IS .016 INCHES. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW VOL I SRM 53-10-01. REMOVED FLOOR SUPPORT, RECEIVED NEW PART FROM FAB SHOP TRAVELER T14 1084370. LOCATED & DRILLED IAW SRM VOL II 51-31-01. TREATED & PRIMED IAW SRM VOL II 51-21-01. THEN INSTALLED NEW FLOOR SUPPORT IAW SRM 51-35-01. MAJOR REPAIR.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

FWD PIT LT ROLLER TRAY LBL 58 STATION 1079 - 1099 CORROSION AT FASTENER HOLES. REMOVED CORROSION FROM ROLLER TRAY IAW SRM 51-21-01. CHECKED LIMITS MAT ORIG .080 INCHES, MAT LOSS .040 INCHES & MAT REMAINING .040 INCHES. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. CUT OUT DAMAGE AREA IAW SRM 53-00-01. FABRICATED NEW REPAIR FILLER & STRAP IAW SRM 53-00-01, MATERIAL 2024 T3 .080C BATCH 2627022. TREATED & PRIMED REPAIR IAW SRM 51-21-01. LOCATED & DRILLED IAW 51-31-01. INSTALLED NEW REPAIR IAW SRM 53-00-01. TOP COAT IAW SRM 51-21-01. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

MAIN CABIN SEAT TRACK X= -47.5 AT STATION 695 GOUGED. AFTER FURTHER INVESTIGATION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 SHEET 1. REMOVED 2 EA FLOOR PANELS FOR ACCESS IAW AMM 53-21-29. CUT DAMAGED SEAT TRACK FROM STATION 685 TO 705, RBL 47.5 IAW SRM 53-20-00. FABRICATED SPLICE HAT & SPLICE PLATE FROM T14 1083310 & T14 1083401. LOCATED & DRILLED IAW SRM 51-31-01. INSTALLED NEW SEAT TRACK & SPLICES IAW SRM 51-31 01. REINSTALLED 2 EA FLOOR PANELS IAW SRM 51-31-01. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

MAIN CABIN SEAT TRACK X= -8.5 AT STATION 775 GOUGED. BLENDED GOUGE IAW SRM 51-21-01. CHECKED LIMITS ORIGINAL MATERIAL 0.145 INCHES, MATERIAL LOSS 0.030. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG 5. CUT OUT DAMAGED SEAT TRACK FROM STATION 725 - 775 IAW SRM 53-70-00. FABRICATED SEAT TRACK FROM MATERIAL PN 60-10964 18, BATCH 0001367821, SPLICE HAT UNDER TRAVELER T14 1083403 & SPLICE PLATE UNDER TRAVELER T14 1083405 IAW SRM 53-70-00. INSTALLED SEAT TRACK, SPLICE HAT & PLATE IAW SRM 53-70-00 VOL I FIG I. MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 3 ENGINE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

NR 3 ENG AFT MOUNT PYLON SIDE HAS SEVERAL RUSTY SPOTS. R & R NR 3 AFT ENG MOUNT SUPPORT IAW CMM 71-20-02 & MM 20-20-01-2. MINOR REPAIR.

Part: STANCHION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

AFT CARGO COMPARTMENT STANCHION HAS CORROSION AT STATION X=20, STATION Y=1967. REMOVED STANCHION AT 1967 AT X 20 IAW SRM 51-31-01. REMOVED CORROSION OFF STANCHION, ORIGINAL THICKNESS .071, .050 REMAINING. FOUND STANCHION OUT OF LIMITS IAW SRM 53-00-01, FIG 1C PG 13. FABRICATED REPLACEMENT STANCHION USING S2525885 BATCH 0001905847 IAW DWG AGA 3224 REV 6 SH 2. ALODINE & PRIMED IAW SRM 51-21-01. INSTALLED STANCHION IAW SRM 51-31-01. MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,800 hrs · 37,990 cycles

FORWARD PIT FLOOR FRAME STATION 879 UPPER CHORD CORRODED BL0 RT END. SUPPORT ANGLE CORRODED THROUGH PART. REMOVED SUPPORT IAW SRM 51-31-01. FABRICATED NEW SUPPORT IAW SRM 51-10-01 FIG 1 FROM BAC 1518 - 653, BATCH 2405327. LOCATED & DRILLED SUPPORT IAW SRM 51-31-01. TREATED & PRIMED IAW SRM 51-21-01. INSTALLED SUPPORT IAW SRM 51-31-01. MAJOR REPAIR.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

MAIN CABIN SEAT TRACK X=47.5 AT STATION 755 GOUGED. UPON FURTHER INVESTIGATION TWO EACH SCALLOPS BROKEN & OUT OF LIMITS IAW SRM 53-70-00 FIG 5 SHEET 1. REMOVED SECTION OF SEAT TRACK FROM STATION 745 TO 765 LBL 47.5 IAW SRM 53-70-00 VOL I FIG 1 SHEET 1 - 2. FABRICATED REPAIR SECTION IAW SRM 51-10-01 FIG 24. INSTALLED REPAIR SECTION IAW SRM 51-31-00. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 775) · airframe 91,800 hrs · 37,990 cycles

MAIN CABIN SEAT TRACK X 8.5 AT BS 775 GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00, VOL. I, FIG. 5. CUT OUT DAMAGED SEAT TRACK IAW SRM 53-70-00. FABRICATED SEAT TRACK, SPLICE & SPLICE PLATE IAW SRM 53-70-00. INSTALLED SEAT TRACK, SPLICE HAT & SPLICE PLATE IAW SRM 53-70-00, VOL. I, FIG. I. MAJOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,800 hrs · 37,990 cycles

APPROX 4.5 INCHES LONG CRACK AT NLG WW LT WALL FWD END. CUT OUT CRACK & PERFORMED REPAIR IAW SRM 53-00-01 FIG 10 SHEET 5 & 51-31-01. MATERIAL 7075-T6 063C BATCH 2629113 & 7075-T6 071 BATCH 1874677. MAJOR REPAIR.

Part: ACTUATOR — FAILED (RT MLG) · airframe 91,778 hrs · 37,980 cycles

AFTER TAKEOFF RT MAIN GEAR PRIMARY & SECONDARY INDICATORS SHOWED GEAR NOT UP. COMPLIED WITH QRH & WAS UNABLE TO RESOLVE INDICATION PROBLEM. TROUBLE SHOT & FOUND RT MAIN GEAR DOWNLOCK ACTUATOR FAILED. R & R RT MAIN GEAR DOWNLOCK ACTUATOR. ALL OPERATIONS CHECKED NORMAL.

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 91,401 hrs · 37,762 cycles

DURING DEPARTURE, NR 1 ENGINE EXCEEDED EGT 932 DEGREES WITH MOMENTARY SPIKE IN N1, RETARDED NR 1 THROTTLE, N1 STEADY AT 93 & EGT 700 - 750 AT FL310. FOUND ENG 1 EXCEEDANCE MESSAGE DISPLAYED & NR 1 EGT INDICATOR WAS FLAGGED AT 999. OPENED NR 1 CORE COWL & SHOOK DOWN EGT HARNESS, FOUND EGT FLUCTUATED WHILE SHAKING FLEX HARNESS AT J BOX. R & R NR 1 ENG EGT FWD LEAD IAW MM 77-21-02-2.

Part: FAN — FAILED (E/E BAY) · airframe 90,991 hrs · 37,545 cycles

FLIGHT 360, A VERY LOUD ELECTRICAL ARCING SOUND BEGAN IN FWD E & E BAY WITH VERY STRONG ODOR OF BURNING ELECTRICAL EQUIPMENT. EMERGENCY DECLARED & LANDED. R&R AVIONICS RACK COOLING FAN CIRCUIT BREAKER IAW SRM 21-26-0 AND INSTALLED AVIONICS RACK COOLING FAN NR 3, IAW AMM 21-26-02-4. SYSTEM OPS CHECKED NORMAL.

Part: BULKHEAD — CRACKED (BS 1521) · airframe 90,005 hrs · 37,032 cycles

INBOARD BULKHEAD CRACKED 30 INCHES FWD OF BS 1521 AND 3 INCHES DOWN FROM UPPER BULKHEAD. R & R CRACKED SKIN APPROX BS 1521 IAW SRM 53-00-01, FIG 10.

Part: BULKHEAD — CRACKED (BS 1381) · airframe 90,005 hrs · 37,032 cycles

LEFT BULKHEAD CRACKED 17 INCHES AFT OF BS 1381 AND 1.5 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED AREA USING EA 8-5310-157384 AS REF.

Part: PROBE — MALFUNCTIONED (FUEL QTY) · airframe 89,667 hrs · 36,834 cycles

TANK 2 PUMPS OFF ILLUMINATED ON DURING CRUISE FLIGHT. MONITORED FUEL DISPLAY. FUEL BEING FED TO NR 2 ENGINE VIA CROSSFEED FROM EITHER NR 3 OR NR 1 TANKS, ALTERNATING AS NECESSARY TO MAINTAIN BALANCE. FUEL TANK 2 QTY DROPPED TO 6200 LBS THEN CAME UP TO 7200 LBS WITH NO FUEL BEING TRANSFERRED INTO TANK 2. FLUXUATION CONTINUED AND INCREASED UNTIL ALERT LEVEL 2 "FUEL QTY FAULT" ON. ON FLT CREW DEBRIEF, WAS TOLD FUEL QTY WENT UP AND DOWN THOUSANDS OF LBS UNTIL IT FINALLY WENT TO X ON SYNOPTIC. TRIED PERFORMING RTS ON FSC SEVERAL TIMES, EACH TIME FAILED TANK NR 1, NR 3 TANK OTBD FILL VALVES. ORDERING FSC AND AUX CONTROLLER. R & R FSC AND ANCILLARY FUEL CONTROLLER IAW MM 28-08-01-4 AND 28-08-03-4. PERFORMED RTS IAW MM 28-00-00-5, SAME CONDITION EXIST , FAILS BOTH NR 1AND NR 3 OTBD FUEL VALVE. REPLACED THE NR 2 TANK LT COMPENSATOR PROBE REF A/C M/M 28-41-01-2 WILL NEED LEAK CHECK.

Part: SKIN — DAMAGED (BS 1701-1910) · airframe 89,209 hrs · 36,563 cycles

FUSELAGE SKIN HOLES THAT GO UNDER BEAUTY STRAP WERE COUNTERSUNK AT STA 1701 - 1910, STR 36R & 48R. INSTALLED BUSHINGS AND C/W EA 8-5310-157930, STEPS 14,15 & 16 ON NR N00548. MAJOR REPAIR.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 89,209 hrs · 36,563 cycles

LEFT OTBD FLAP, INBD HINGE FITTING CORRODED AT FACE OF LWR ATTACH POINT. COMPLIED WITH EA 8-5744-157932. BLENDED SURFACE CORROSION FROM LWR MOUNT FACE AND BONDED SHIM IAW EA 8-5744-157932. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1741-1911.5) · airframe 89,209 hrs · 36,563 cycles

RT FUSELAGE SKIN DAMAGED. SPLICED NEW SKIN SECTION IAW EA 8-5310-157930 AT BS 1741 - 1911.5 L36 - 48R. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1781-1887) · airframe 89,209 hrs · 36,563 cycles

RT FUSELAGE SKIN DOUBLER DAMAGEDAMAGED BS 1781-1887 L36-48R. SPLICED NEW SKIN SECTION IAW EA 8-5310-157930 . MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 89,209 hrs · 36,563 cycles

SEAT TRACK AT X=75.25 , AT STA: 1381 CROWN AREA BETWEEN SCALLOPS MISSING. REMOVED SEAT TRACK SPLICE IAW SRM 51-31-01. FABRICATED NEW SPLICE . INSTALLED SEAT TRACK SPLICE IAW SRM 51-31-01.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 89,209 hrs · 36,563 cycles

FWD CARGO DOOR HINGE FWD SEGMENT INNER SURFACE CRACKED. PERFORMED HEFC INSPECTION OF AREA IAW NTSMPM 06-10-01. FOUND POSITIVE ID OF CRACK. REMOVED FWD CARGO DOOR IAW AMM 51-32-04-2. REMOVED THE CRACKED HINGE SECTION IAW SRM 51-31-01. FABRICATED SHIM IAW 51-31-01 INSTALLED SHIM IAW 51-31-01, LOCATED NEW HINGE IAW SRM 51-31-01.

Part: LEVER — DAMAGED (MLG) · airframe 88,914 hrs · 36,404 cycles

RT MAIN GEAR LIGHT RED AFTER GEAR RETRACTION, BOTH ON PRIMARY AND SECONDARY INDICATION SYS. GEAR RECYCLED IAW QRH, LIGHTS THEN NORMAL. WHILE TROUBLESHOOTING FOUND RT MLG CRANK ASSY BROKEN AND PROX SENSOR HANGING BY THE WIRES. REMOVED AND REPLACED LEVER ASSY IAW AMM 32-34-03-2-1. OPS CHECKED NORMAL.

Part: SLIDE — LEAKING (L1 DOOR) · airframe 88,540 hrs · 36,209 cycles

PRE-DISPATCH CHECK, FOUND L1 DOOR SLIDE REMOTE PRESSURE CHECK LIGHT INOPERATIVE. REPLACED BATTERIES IAW AMM 25-61-03-2-0. INDICATOR LIGHT NOW REMAINS ON AT ALL TIMES. RESEARCHING SLIDE BOTTLE PRESSURE VERIFICATION PRESSURE PROCEDURE. CONFIRMED SLIDE BOTTLE IS DISCHARGED, REF MEL 25-60-01. R & R LT L1 DOOR SLIDE ASSY REF TO AMM 25-61-02-2. NEW BATTERIES INSTALLED IN DOOR LIGHT LOW PRESSURE INDICATION MODULE. PUSH TO TEST LOW PRESSURE DOOR SLIDE INDICATOR IS NOT ILLUMINATED AND LIGHTS WHEN TESTED AS NORMAL. L1 DOOR OPS CHECKS GOOD. ACFT OK FOR SERVICE.

Part: BULB — INOPERATIVE (PRESSURE SWITCH) · airframe 87,832 hrs · 35,815 cycles

FOUND R1 DOOR EVACUATION SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. DURING BLOCK IN. REPLACED BATTERIES. NO HELP. CHECKED WIRE CONNECTIONS AND JACK CONNECTOR. NO OBVIOUS DISCREPANCIES. RELEASED FOR SERVICE PER MEL: 25-61-01 REPLACED BULBS IN DOOR TEST LIGHT P/B SWITCH IAW SMP AND IPC 25-61-20. TEST GOOD.

Part: OXYGEN MASK — BROKEN · airframe 87,501 hrs · 35,639 cycles

COURIER OXYGEN MASK BROKEN. RELEASED FOR SERVICE PER MEL: 25-11-03 CATEGORY: D EXPIRATION: 27JUN11 "MEL 25-11-03: LT OUTBOARD COURIER SEAT INOP. DO NOT OCCUPY FOR TAXI, TAKEOFF AND LANDING." REMOVED AND REPLACED LT MOST OUTBOARD COURIER SEAT O2 MASK ASSY REF MD10-10 AMM 35-13-03-2 - OP'S AND LEAK CHECK GOOD.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 86,629 hrs · 35,220 cycles

LT WING TIP AFT CAP AT STA XW 930 FOUND EXISTING REPAIR.REPAIR EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5730-140434, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR FOUND AT LONGERON 46L AT STA 1541 TO STA 1561. EXISTING REPAIR AT LONGERON 46LT AT STA 1541 TO STA 1561 EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-33-01 VOL. II REV. 96, AND REPAIR ACCOMPLISHED AS PER E.A. 8-5310-132460. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.

Part: FLOORBEAM — MISREPAIRED (BS 1099) · airframe 86,629 hrs · 35,220 cycles

FORWARD CARGO - EXISTING REPAIR AT FLOORBEAM STA 1099, X = 4 TO X = 14. EXISTING REPAIR AT FORWARD CARGO FLOORBEAM EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND NEW REPAIR CARRIED OUT PER E.A. 8-5310-140428, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE - EXISTING REPAIR DOUBLER FOUND AT FUSELAGE SKIN AT LT STA 1541 TO STA 1561, LONGERON 45L. SKIN EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-33-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5310-132460, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE - EXISTING REPAIR DOUBLER FOUND AT FUSELAGE SKIN AT RT STA 1541 TO STA 1561, LONGERON 45R. SKIN EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME AND DRAWING. EXISTING REPAIR REMOVED PER SRM 51-33-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5310-132460, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: LONGERON — DAMAGED (BS 1671 L46R) · airframe 86,629 hrs · 35,220 cycles

CTR CARGO - UPON REMOVAL OF EXISTING REPAIR IAW SNRM N01182, EXISTING LONGERON 46R, SPLICE AT STA 1671 FOUND WITH 6 EACH FASTENER HOLES ELONGATED. DAMAGED LONGERON 46R AT CENTER CARGO STA 1671 TRIMMED OUT PER SRM 53-10-00 FIGURE 1 AND 2 VOLUME I REVISION 96 AND REMOVED PER SRM 51-31-01 VOLUME II REVISION 96. NEW REPAIR CARRIED OUT PER SRM 53-10-00 FIGURE 1 AND 2 VOLUME I REVISION 96. E.O.8-5100-7-5001 A7 PART 2, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110. TO CARRY OUT INITIAL INSPECTION AT 15,000 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTION AT EVERY 10,000 FLT CYCLES.

Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 86,629 hrs · 35,220 cycles

RT WING NR3 SPOILER PANEL UPPER SURFACE FOUND WITH DELAMINATION. REPAIR CARRIED OUT IAW EA NR8-5770-132457, TITLE: "WINGS - RT WING NR 3 SPOILER DELAMINATION - REPAIR." THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT LONGERON 52 FROM STA 979 TO STA 1039. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-35-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER FEDEX E.A. 8-5310-140425, EO 8-5100-7-5001 A7 PART 2, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110. TO PERFORM INITIAL INSPECTION AT 15,000 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 10,000 FLIGHT CYCLES.

Part: SKIN — GOUGED (BS 1921-1941) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE SKIN AT LT STA 1921 TO STA 1941 LONGERON 48L FOUND WITH 1 EACH GOUGE MARK. REPAIR CARRIED OUT PER E.A. 8-5310-132455, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.

Part: BULKHEAD — MISREPAIRED (BS 2163) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR FOUND ON AFT CANTED BULKHEAD LOWER AREA STA Y = 2163. EXISTING REPAIR ON AFT CANTED BULKHEAD EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-35-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5330-140420 REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: RIB — DAMAGED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

RIGHT WING NR 1 SLAT AFTER REMOVAL OF EXISTING REPAIR DOUBLER IN REFERENCE TO SNRM N00954, RIB FOUND WITH AN EXISTING DRILL HOLE. RIB FOUND WITH AN EXISTING DRILL HOLE AT RIGHT WING NO. 1 SLAT, REPAIR ACCOMPLISHED PER SRM 57-00-01 FIG. 10 VOL. I REV. 96. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.

Part: SPAR CAP — DAMAGED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

RIGHT HAND WING, DURING REMOVAL OF FASTENERS AT WING REAR SPAR LOWER CAP, FOUND 01 EACH HLT339-12 FASTENER NOT STATED INSIDE E.O. 8-5710-7-5007 PART 2. COMPIED WITH E.A. 8-5710-140422, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 86,629 hrs · 35,220 cycles

L4 DOOR UPPER EXTERIOR SKIN FOUND WITH 2 EACH EXISTING REPAIR DOUBLER. EXISTING REPAIR AT L4 DOOR UPPER EXTERIOR SKIN EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 52-10-00 FIGURE 12B VOLUME I REVISION 96. EO 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED MAJOR PER GMM 6-2 -100 REVISION 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT FUSELAGE SKIN, STA 1741, LONGERON 52. EXISTING REPAIR AT FUSELAGE SKIN STA 1741, LONGERON 52 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOL II, REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 (SHEET 5) VOL I, REV 96. EO NR8-5100-7-5001, A7, PART 1, TITLE: "STRUCTURES - REPAIR CATALOG -REPAIR ID AND TRACKING SMR'S ON ACFT BEING INDUCTED INTO MX SYS 14CFR 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR FOUND AT LT WING (TELESCOPIC DUCT) L/E UPPER SKIN. EXISTING REPAIR FOUND AT LT WING (TELESCOPIC DUCT) L/E UPPER SKIN EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND NEW REPAIR CARRIED OUT IAW EA8-5710-138589. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (NR 1 SLAT) · airframe 86,629 hrs · 35,220 cycles

RT WING NR1 SLAT INNER SKIN AT STA XIS 151 FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING NR1 SLAT INNER SKIN STA XIS 151 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-33-01, VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 29 VOL I REV 96. EO8-5100-7-5001, A7, PART 2, TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR ID, CLASSIFICATION AND TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT CENTER CARGO STA 1721 LOWER FRAME FORWARD LOWER CHORD BETWEEN LONGERON 50R AND LONGERON 51R EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR ANGLE REMOVED PER SRM 51-33-01 VOLUME II REVISION 96 AND REPAIR CARRIED OUT PER SRM 53-00-01 FIGURE 8 VOLUME I REVISION 96. EO 8-5100-7-5001, A7 PART 2, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 86,629 hrs · 35,220 cycles

LT WING NR4 SLAT INNER SKIN AT STA XOS 549 FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING NR4 SLAT INNER SKIN AT STA XOS 549 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01 VOL II, REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 31, VOL I REV 96. EO NR8-5100-7-5001, A7, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE - EXISTING REPAIR DOUBLER FOUND ON FUSELAGE SKIN AT LT STA 1761 TO STA 1781 BETWEEN LONGERON 11L TO LONGERON 12L. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AS PER SRM 51-31-01 VOL. II REV. 96 AND NEW REPAIR CARRIED OUT AS PER SRM 53-20-00 FIG. 6 VOL. I REV. 96. E.O. 8-5100-7-5001 A7 PT1. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.

Part: BULKHEAD — MISREPAIRED (ZONE 700) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR DOUBLER FOUND AT RT MLG WHEEL WELL AFT BULKHEAD LOWER OTBD SIDE AT STA 1501. EXISTING REPAIR DOUBLER AT RT MLG WHEEL WELL AFT BULKHEAD LOWER OTBD SIDE AT STA 1501 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01, VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 10, VOL I, REV 96. EO NR8-5100-7-5001, A7, PART 2, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SHEAR TIE — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT STA 859 LOWER FRAME FWD SHEAR CLIP FROM LONGERON 51L TO LONGERON 52. EXISTING REPAIR AT STA 859 LOWER FRAME FWD SHEAR CLIP FROM LONGERON 51L TO LONGERON 52 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-385-01 VO II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-30-00, FIG 10 VOL, I REV 96. EO 8-5100-7-5001, A7 PT2, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR ID, CLASSIFICATION & TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR 121.368, 121.707 ACCOMPLISHED. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 110.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT STA 879 LOWER FRAME FWD SURFACE FROM LONGERON 50L TO LONGERON 50R. EXISTING REPAIR AT FWD CARGO STA 879 LOWER FRAME FWD SURFACE L-50L TO L-50R EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR ANGLE REMOVED IAW SRM 51-33-01, VO II, REV 96 AND REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 8 VOL I, REV 96. EO 8-5100-7-5001, A7 PT2, TITLE: STRUCTURES - REPAIR CATALOG. REPAIR ID, CLASSIFICATION & TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR 121.368, 121.707 ACCOMPLISHED. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE EXISTING REPAIR DOUBLER FOUND ON FUSELAGE SKIN AT RT STA 339 TO STA 348 BETWEEN LONGERON 34R TO LONGERON 36R. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AS PER SRM 51-33-01 VOL II REV. 96 AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-20-00 FIG. 6 SHEET 3 REV. 96. E.O. 8-5100-7-5001 A7 PT2. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6- 2-100 REV. 110.

Part: SHEAR TIE — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT STA 840 LOWER FRAME AFT SHEAR CLIP FROM LONGERON 51L TO LONGERON 52. EXISTING REPAIR AT FWD CARGO STA 840 LOWER FRAME AFT SHEAR CLIP FROM LONGERON 51L TO LONGERON 52 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-35-01, VOLUME II, REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-30-00, FIG 10 VOLUME I, REV 96. EO8-5100-7-5001, A7, PART 2, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT STA 840 LOWER FRAME FWD FROM LONGERON 51L TO LONGERON 51R. EXISTING REPAIR AT FWD CARGO STA 840 LOWER FRAME FWD FROM LONGERON 51L TO LONGERON 51R EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-35-01, VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 8, VOL I, REV 96. EO 8-5100-7-5001, A7, PART 2, TITLE:"STRUCTURES -REPAIR CATALOG - REPAIR ID, CLASSIFICATION AND TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: BULKHEAD — MISREPAIRED (MLG WW) · airframe 86,629 hrs · 35,220 cycles

LT MLG WHEEL WELL - EXISTING REPAIR DOUBLER FOUND AT MLG WHEEL WELL AFT BULKHEAD LOWER OTBD SIDE AT STA 1501. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOLUME II, REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 10 VOL I REV 96. EO 8-5100-7-5001, A7, PART 2. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT FUSELAGE SKIN STA 1746 TO STA 1758 LONGERON 48L. EXISTING REPAIR AT FUSELAGE SKIN STA 1746 TO STA 1758 LONGERON 48L EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 VOL I, REV 96. EO8-5100-7-5001, A7, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: TEE FITTING — CRACKED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - LT TUNNEL STA 709, LONGERON 31 TEE CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 96. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — DENTED (BS 1781-1801) · airframe 86,629 hrs · 35,220 cycles

FUSELAGE SKIN AT RT STA 1781 TO STA 1801 LONGERON 5R TO LONGERON 7R FOUND (1 EA) DENT. MEASURED AND FOUND WITHIN LIMIT IAW SRM 53-00-01, FIG 13 VOL I, REV 96. D = 1.3", Y = 0.045", D/Y = 28.8. D/Y IS GREATER THAN 25.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

FWD CARGO - EXISTING REPAIR AT SUMP PANEL AREA AT STA 899 BETWEEN LONGERON 51L AND LONGERON 51R LW AFT FRAME. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER SRM 53-00-01 FIGURE 8 VOLUME I REVISION 96. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: SKIN — MISREPAIRED (ZONE 800) · airframe 86,629 hrs · 35,220 cycles

L4 DOOR UPPER EXTERIOR SKIN FOUND WITH (2 EA) EXISTING REPAIR DOUBLER. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. 2 EACH EXISTING REPAIRS REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 52-10-00 FIGURE 12B VOLUME I REVISION 96. E.O.8-5100-7-5001 A7 PART 2, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.

Part: SUPPORT — CORRODED (BS 420-430) · corrosion level 2 · airframe 86,629 hrs · 35,220 cycles

MAIN DECK CARGO - STA 420 TO STA 430 RBL 25, GALLEY SUPPORT FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 96. REPAIR CLASSIFIED MAJOR PER GMM 6-2- 100 REVISION 110.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 86,629 hrs · 35,220 cycles

AFT CARGO - WHILE REMOVING FLOORBEAM IN AFT UPPER CHORD ABOVE LONGERON 45R AT STA 1841, FLOORBEAM FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5310-132456, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

RT WING NR1 SLAT INNER SKIN AT STA XIS 237 FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING NR1 SLAT INNER SKIN STA XIS 237 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01 VOLUME II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 29, VOL I, REV 96. EO NR 8-5100-7-5001, A7, PART 2, . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SUPPORT — MISREPAIRED (ZONE 500) · airframe 86,629 hrs · 35,220 cycles

LT WING FIXED L/E LOWER PANEL SUPPORT STRIP AT STA XOS 906 FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING FIXED L/E LOWER PANEL SUPPORT STRIP AT STA XOS 906 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER AT LT WING FIXED L/E LOWER PANEL SUPPORT STRIP AT STA XOS 906. REMOVED IAW SRM 51-31-01 VOL II REV 96 AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 49, VOL I REV 96. EO 8-5100-7-5001, A7, PART 2, TITLE: SRM, REPAIR ID, CLASSIFICATION AND TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR, 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

CTR CARGO - EXISTING REPAIR AT LONGERON 46R, STA 1661 TO STA 1701. EXISTING REPAIR AT CTR CARGO LONGERON 46R STA 1661 TO STA 1701 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOL II, REV 96 AND NEW REPAIR CARRIED OUT IAW EA 8-5310-140438, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

CTR CARGO - EXISTING REPAIR AT LONGERON 45R STA 1661 TO STA 1701. EXISTING REPAIR AT CTR CARGO LONGERON 45R, STA 1661 TO STA 1701 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOL II, REV 96 AND NEW REPAIR CARRIED OUT IAW EA 8-5310-140437, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SPAR CAP — DAMAGED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

HFEC INSP CARRIED OUT AND FOUND 1 EACH HOLE DAMAGED ON RT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140422, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 86,629 hrs · 35,220 cycles

HFEC INSP CARRIED OUT AND FOUND 1 EACH HOLE WITH CRACK INDICATION ON LT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140423, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SPAR CAP — DAMAGED (LT WING) · airframe 86,629 hrs · 35,220 cycles

HFEC INSP CARRIED OUT AND FOUND 3 EACH HOLES DAMAGED ON LT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140423, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CHAFED (BS 1386) · airframe 86,629 hrs · 35,220 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK FOUND EDGE CHAFED AT STA 1386, RBL 72. REPAIRED BY SECTIONAL SEAT TRACK. REPLACEMENT FROM STA 1331 TO STA 1411, RBL 75.5 IAW SRM 53-70-00 FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT FUSELAGE SKIN, STA 1069 TO STA 1099, LONGERON 38R. EXISTING REPAIR AT FUSELAGE SKIN STA 1069 TO STA 1099 LONGERON 38R EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6, VOL I. EO 8-5100-7-5001 A7 PART 1. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT FUSELAGE SKIN STA 1134 TO STA 1146 LONGERON 43L. EXISTING REPAIR AT FUSELAGE SKIN STA 1134 TO STA 1146 LONGERON 43L EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-35-01, VOL II REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 VOL I, REV 96. EO NR 8-5100-7-5001, A7, PART 1, TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING SMR'S ON ACFT BEING INDUCTED INTO MX SYS 14CFR 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR FOUND AT FUSELAGE SKIN RT STA 1199 TO STA 1219 BETWEEN LONGERON 51R AND LONGERON 52. EXISTING REPAIR EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 VO. II, REV. 96 AND REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6 SHEET 3, VOL I, REV 96. EO 8-5100-7-5001, A7, PT1. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,629 hrs · 35,220 cycles

EXISTING REPAIR AT FUSELAGE SKIN STA 979 TO STA 996, LONGERON 37R. EXISTING REPAIR AT FUSELAGE SKIN STA 979 TO STA 996, LONGERON 37R EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-35-01, VOL II, REV 96 AND NEW REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6, VOL I REV 96. EO 8-5100-7-5001, A7 PART 1, TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING OF SMR'S ON ACFT BEING INDUCTED INTO MX SYS 14CFR 121.368, 121.707" HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SUPPORT FITTING — CRACKED (LT WING TE FLAP) · airframe 86,629 hrs · 35,220 cycles

LT WING INBD FLAP ENCLOSURE AREA, INBD FLAP ROLLER SUPPORT FITTING FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5340-140419, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 86,629 hrs · 35,220 cycles

RT WING OTBD FLAP ASSY UPPER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 85, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (LT WING) · airframe 86,629 hrs · 35,220 cycles

LT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 68, VOLUME I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (RT WING) · airframe 86,629 hrs · 35,220 cycles

RT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-10-00, FIG 68, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SKIN — DENTED (LT NR 3 SLAT) · airframe 86,629 hrs · 35,220 cycles

LT WING - NR 3 SLAT, APPROX STA XOS 390 TO XOS 440 EXTERIOR FWD SKIN FOUND WITH DENTS. R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (RT NR 7 SLAT) · airframe 86,629 hrs · 35,220 cycles

RT WING - NR 7 SLAT ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

RT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5710-140426, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 86,629 hrs · 35,220 cycles

LT WING INBD FLAP ASSY LOWER SURFACE, OTBD LOWER SEGMENT FOUND WITH DENTS. REPAIRED IAW SRM 57-10-00, FIG 3, VOLUME I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (LT NR 6 SLAT) · airframe 86,629 hrs · 35,220 cycles

LT WING - NR 6 SLAT, APPROX STA XOS 789 EXTERIOR FWD SKIN FOUND WITH DENT. REPAIRED IAW SRM 57-10-00, FIG 11, VOL I REV 96. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 86,629 hrs · 35,220 cycles

RT WING - NR 6 SLAT, ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. NR 6 SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.

Part: ACCESS DOOR — CRACKED (ZONE 600) · airframe 86,629 hrs · 35,220 cycles

RT WING - WING TIP LOWER SURFACE AFT OF STROBE LIGHT ACCESS DOOR FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5720-138577, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 86,629 hrs · 35,220 cycles

LT WING INBD FLAP ASSY LOWER SURFACE, INBD LOWER SEGMENT FOUND WITH DENTS. TRIMMED OFF AND REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (LT WING) · airframe 83,840 hrs · 33,836 cycles

LEFT WING TIP T/E AREA EXTERNAL SKIN IS CRACKED. REMOVED DAMAGED AREA PER DC/MD-10 SRM 57-00-01;VOL I. FABRICATED A DOUBLER REPAIR PER DC/MD-10 SRM 57-00-01; VOL I. ALODINED AND PRIMED DOUBLER REPAIR PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER REPAIR PER DC/MD-10 SRM 51-35-01; VOL II AND DC/MD-10 SRM 57-00-01; VOL I; SHEET 2; FIG 4.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 83,840 hrs · 33,836 cycles

LEFT WING TIP INSIDE PANEL NR 528 DB INTERCOSTAL UPPER ANGLE IS CRACKED IN NUMEROUS PLACES. REMOVED LEFT WING TIP IAW MD-10 AMM 57-23-01-2. REPAIRED THE WING TIP IAW DC/MD-10 SRM 57-00-01, FIG 4, VOL I AND SRM 57-20-00, VOL I. COMPLIED WITH FEDEX EA 8-5720-118527 TITLE " WINGS - LT WING TIP FORMER AT YIO 833.430". REINSTALL LT WING TIP IAW MD-10 AMM 57-23-01-2. OPS CHECK OF THE HIGH INTENSITY AND NAV LIGHTS IS GOOD IAW MD-10 AMM 33-47-00-4; PG 9 AND AMM 33-44-00-4, PG 6.

Part: HOUSING — GOUGED (LT WING STROBE) · airframe 83,840 hrs · 33,836 cycles

LEFT WING TIP T/E LIGHT ASSY HOUSING IS CHAFED AND THE LENS ATTACH HOLES ARE ELONGATED. REMOVED LEFT T/E HIGH INTENSITY LIGHT IAW MD 10 AMM 33-47-00-4. REMOVED AND REPLACED THE STROBE BRACKET AND STROBE IAW DC/MD 10 SRM 51-35-01, VOL II. REINSTALLED LEFT T/E HIGH INTENSITY LIGHTS IAW MD-10 AMM 33-47-00-4.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

CENTER WING LOWER BARREL INTERNAL FRAME AFT FACE LOWER FLANGE HAS CORROSION JUST BELOW THE BLEED AIR DUCT; FS 1381; STRINGER 51R TO STRINGER 51L. REMOVED CORROSION. ORIGINAL THICKNESS, 0.080. MATERIAL LOSS IS 0.029. REMAINING THICKNESS 0.051 IAW SRM 53-00-01, VOL I. REMOVED THE FRAME AND INTERCOSTAL IAW DAC DWG AEA 0273, REV G. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. APPLIED TOP COAT IAW SRM 51-21-01, VOL II. PART MARKED IAW GMM 7-0-1001.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

LEFT MLG WW AFT BULKHEAD OUTBD SIDE OF THE WELL INTERCOSTAL AT FS 1521 JUST BELOW THE FLAP BUSS PULLEY IS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-35-01, VOL II. FABRICATED A NEW INTERCOSTAL IAW DWG AEA 0026, REV M. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. PART MARKED INTERCOSTAL P/N FX AEA0026-5 IAW GMM 7-0-1001.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

AFT CARGO BILGE SEAT TRACK IS CORRODED AT STA 1831 TO 1840 AND LBL 20. REMOVED CORROSION IAW SRM 51-21-01, VOL II. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00, VOL I. REMOVED SEAT TRACK FROM STA 1781 TO 1960 IAW SRM 51-31-01, VOL II. MATERIAL ID FOR THE NEW SEAT TRACK S4929311. MACHINED SCALLOPS AND FORMED TRACK IAW DWG AGA 3855, REV H. DRILLED AND COUNTERSUNK IAW SRM 51-31-01, VOL II. PART MARKED SEAT TRACK IAW GMM 7-0-1000. ALODINED AND PRIMED IAW SRM 51-21-01, PGS 21 AND 25, VOL II. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01, VOL II.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

RIGHT MLG WW AT FS 1521; INTERCOSTAL NEXT NEXT TO THE FLAPS BUSS PULLEYS IS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED A NEW INTERCOSTAL IAW DAC DWG AEA0026, REV M. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED INTERCOSTAL P/N FX - AEA0026-6 IAW FEDEX GMM 7-0-1001.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

RIGHT MLG WW AFT BULKHEAD AT L 36R WEB IS CORRODED AT THE STANSION. REMOVED AND REPLACED THE INTERCOSTAL IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED A NEW INTERCOSTAL IAW DAC DWG NR AEA 0027, REV S. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED INTERCOSTAL P/N FX - AEA0024-6 IAW FEDEX GMM 7-0-1001.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 83,840 hrs · 33,836 cycles

MAIN CABIN SEAT TRACK LOBE IS BROKEN OUT AT FS 755; LBL 48. REPLACED THE MAIN CABIN SEAT TRACK FROM STATIONS 675 TO 760; LBL 48 IAW SRM 53-70-00; VOL I; PG 3. INSTALLED 4 FLOORBOARDS AT STATIONS 675-765; LBL 27-48; STATIONS 675-835; LBL 48-76 IAW SRM 51-31-01; VOL II; PG 1.

Part: SKIN — CORRODED (BS 1195-1216) · airframe 83,840 hrs · 33,836 cycles

INTERIOR FUSELAGE SKIN HAS CORROSION IN AREAS AROUND THE DRAIN HOLES FROM FS 1195 - 1216; STRINGERS 51R - 51L.

Part: NONE — NONE (NOT AN SDR) · airframe 83,840 hrs · 33,836 cycles

FOUND A REPAIR LOCATED AT STA 1517-1527; STRINGER 46R THAT REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS INSTALLED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NO APPROVED FAA DATA. REPAIRED IAW FEDEX EA 8-5310-118524 "FUSELAGE - STA 1521 BULKHEAD TEE CAP AT L-46R - REPAIR".

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

CENTER WING LOWER (BARREL), INTERIOR FUSELAGE SKIN HAS CORROSION; FS 1257 - 1278; STRINGER 52L - STRINGER 51L. REMOVED/BLENDED CORROSION ON THE INTERNAL SURFACE OF THE SKIN AND FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 53-00-01; VOL I. ORIGINAL THICKNESS, 0.080. REMAINING THICKNESS AFTER CORROSION REMOVAL, 0.034. MATERIAL REMOVED, 0.046. UT GAUGE USED T8225R. CUTOUT DAMAGE; FABRICATED REPAIR DOUBLERS AND FINGER DOUBLERS IAW DC/MD-10 SRM 53-20-00; FIG 6; VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED THE REPAIR IAW DC/MD-10 SRM 53-20-00; FIG 6; VOL I; SHEET 2.

Part: LONGERON — CRACKED (ZONE 100) · airframe 83,840 hrs · 33,836 cycles

FOUND L52 AT STA 1575 CRACKED. REMOVED DAMAGED L52 AND INSTALLED A NEW LONGERON P/N AEA 0541-1 IAW DAC DWG NEA 6076; REV AK.

Part: LONGERON — CRACKED (ZONE 100) · airframe 83,840 hrs · 33,836 cycles

FOUND L 52 AT STA 1575 CRACKED. REMOVED DAMAGED L 52 AND INSTALLED A NEW LONGERON P/N AEA 0451-1 IAW DAC DWG NEA 6076; REV AK.

Part: FLOORBEAM — MISREPAIRED (BS 1701) · airframe 83,840 hrs · 33,836 cycles

FOUND THE REPAIR LOCATED IN THE CENTER PIT FLOORBEAM LOWER CARGO FLANGE AT STA 1701; RBL 28 TO RBL 39 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO COMPLY WITH FAA APPROVED DATA. REPAIRED CENTER PIT FLOORBEAM IAW DC/MD-10 SRM 53-60-01; VOL I; FIG 3.

Part: SKIN — CRACKED (BS 913-933) · airframe 83,840 hrs · 33,836 cycles

FWD PIT, IN THE DOOR SILL AREA BETWEEN STRINGER L43R AND STRINGER L44R 36 INCH AFT OF THE FWD EDGE OF THE DOOR CUTOUT, THE WEB SKIN IS CRACKED. ACCOMPLISHED EA 3 8-5310-118513, FUSEALGE FWD CARGO COMPT JAMB INNER TORQUE BOX SKIN AND DOUBLER REPAIR. REPAIR WAS ACCOMPLISHED BETWEEN L43-44R FROM BS 913-933.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

AFT BAGGAGE COMPARTMENT FRAME AT BS 1853 RBL 12 TO LBL 12 HAS CORROSION. REMOVED CORROSION IN REF TO SRM 51-21-01; VOL II. ORIGINAL THICKNESS 0.071 IN REF TO SRM 51-10-01; VOL III. REMOVED 0.017. REMAINING THICKNESS IS 0.054. AREA IS OUT OF LIMITS IN REF TO SRM 53-00-01; FIG 1-B; VOL I. REPAIRED AREA IN REF TO SRM 53-30-00; VOL I; FIG 8.

Part: LONGERON — CRACKED (BS 1500) · airframe 83,840 hrs · 33,836 cycles

LEFT MLG WHEEL WELL UNDER UPPERWING TO BODY FAIRING AT FS 1500 LONGERON IS CRACKED. REMOVED & RE-ISTALLED THE LT GILL LINER PANEL FROM BS 1521-1561 FOR ACCESS IAW SRM 51-31-01; VOL II. REMOVED LONGERON. FABRICATED & INSTALLED IAW DWG AEA 0472, REV NC SRM 51-33-14, VOL II; & 51-35-01, VOL II. ALODINED & PRIMED IAW SRM 51-21-01, VOL II.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 83,840 hrs · 33,836 cycles

MAIN CARGO DOOR LOWER JAMB NR 5 SPOOL FITTING LOWER JAMB SUPPORT FITTING IS CORRODED AND CRACKED. PERFORMED HFEC INSPECTION PER STSPM 6-10-01-00 ON THE LOWER JAMB FITTING FOR THE MCD AT SPOOL FITTING AT THE NR 5 LOCATION AND VERIFIED THAT NO CRACK WAS NOTED AT THIS TIME.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 83,840 hrs · 33,836 cycles

MAIN CARGO DOOR LOWER JAMB NR 7 SPOOL FITTING LOWER JAMB FITTING IS CORRODED AND CRACKED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,840 hrs · 33,836 cycles

THE FUSELAGE SKIN IS BULGING AT FS 1943 STRINGER 46 L. REMOVED DOUBLER IN REF TO SRM 51-33-01; VOL II. REMOVED CORROSION IN REF TO SRM 51-21-01; VOL II. ORIGINAL THICKNESS 0.068 IN REF TO SRM 53-36-01; VOL III. REMOVED 0.015, MATERIAL REMAINING IS 0.053. AREA IS OUT OF LIMITS IN REF TO SRM53-00-01; FIG 1A; VOL I. REPAIRED AREA IN REF TO SRM 53-20-00; VOL I. MATERIAL ID FOR THE REPAIR PARTS DOUBLER AND TRIPLER IS 0.050 2024-T3, PO 610199.1 AND FINGER DOUBLERS ARE 0.040 2024-T3, PO 614599.2.

Part: LANDING GEAR — MALFUNCTIONED · airframe 81,767 hrs · 32,890 cycles

WHEN GEAR INITIALLY LOWERED FOR LANDING, ALL INDICATIONS REMAINED RED. RECYCLED GEAR AND AFTER A DELAY ALL INDICTIONS READ GREEN. DURING CREW DEBRIEF, CREW STATED WHEN GEAR INITIALLY LOWERED THERE WAS NO PHYSICAL IND VIBRATION OR FEELING THAT THE GEAR WAS EVEN LOWERING UNTIL RECYCLED AND THEN AFTER SOME DELAY COULD FEEL THE GEAR ACTUALLY LOWERING AND AFTER MORE DELAY GOT THREE GREENS. TROUBLE SHOT PER FIM 32-30 UP TO STEP 5. VERIFIED RIGGING FROM GEAR HANDLE TO SELECTOR VALVE. ALL CHECKS NORMAL REF MD10-10MM 32-31-01-5. REMOVED AND REPLACED EMERGENCY LANDING GEAR CONTROL MICROSWITCH S1-392 PER MD10 MM 32-32-01-2. OPS CHECK NORMAL PER MM 32-30-00-5.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,090 hrs · 32,611 cycles

CENTER LANDING GEAR COMPARTMENT, LONGERON 48R CORRODED ON FWD ND AFT SIDES OF FRAME 1501. REPAIRED BY REPLACING 26" SECTION OF LONGERON 48R IAW DC10/MD10 SRM 53-00-01 FIG9 SHEET3 VOL I. ALL PARTS ALODINED AND PRIMERED PER DC10/MD10 SRM 5121-01 VOL II. SEE FEDEX NONROUTINE N01062, OF WORK ORDER 00034441.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 970 TO 1099, 48"RIGHT OF B/L SEAT TRACK HAS WORN AND GOUGED AREAS. REMOVED, FABBED, ALODINED AND PRIMED AND INSTALLED SEAT TRACK IAW 51-21-01 VOL II PG1-24,53-70-00 VOL I PG1. MAJOR REPAIR MECH 110847 QC311.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 970 TO 1099,48" RIGHT OF B/L SEAT TRACK HAS WORN AND GOUGED AREAS. REMOVED, FABBED, ALODINED, PRIMED AND INSTALLED SEAT TRACK IAW 51-21-01 VOL II PG1-24,53-70-00 VOL I PG1. MAJOR REPAIR MECH 110847 QC311

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

SEAT TRACK AT STA 514 RBL 7.5 HAS DAMAGE TO FLOORBOARD ATTACH FLANGE. REMOVED AND REPAIRED SEAT TRACK S4929405 REF DC/MD 10 SRM 53-42-01 FIG 5 VOL 1, 53-42-01 FIG3 VOL III. DRILLED, COUNTERSUNK, ALODINED AND PRIMED AND INSTALLED SEAT TRACK AND SPLICES REF DC/MD-10 SRM 51-31-01 PAGE 1 VOL II, 51-21-01 VOLI PAGE 1 AND 53-70-00 VOL1. MAJOR REPAIR MECH 110217 QC227.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CABIN SEAT TRACK "D" LBL 28 CHAFED AT STA 783. REMOVED, FABBED, ALODINED AND PRIMED AND INSTALLED SEAT TRACK REF DC/MD 10 SRM 53-70-00 VOL 1, 51-21-01 VOL II PAGE 1-24.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CABIN SEAT TRACK "D" LBL28 CHAFFED AT STA 783. REMOVED, FABBED, ALODINED AND PRIMED AND INSTALLED SEAT TRACK REF DC/MD 10 SRM 53-70-00 VOL 1, 51-21-01 VOL II PAGE 1-24.

Part: SEAT TRACK — CRACKED (ZONE 700) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 915, 28" RIGHT OF BUTT-LINE, SEAT TRACK CRACKED. REMOVED, FABRICATED, ALODINED AND PRIMED AND INSTALLED SEAT TRACKED REF DC/MD, 10 SRM 53-70-00 VOL I, 51-31-01 VOL II, 51-33-01 VOL II, 51-21-01 VOL II AND MECH 3545, QC231.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CABIN SEAT TRACK C LBL 48 HAS AN ELONGATED HOLE AT FS 1381. REPAIRED SEAT TRACK, FABRICATED, ALODINED AND PRIME, INSTALLED REF DC/MD 10 SRM 53- 70-00 PAGE 5 VOL 1. FABBED AND INSTALLED SPLICE PLATE AND SPLICE HAT REF 53-70-00 VOL I PAGE4.

Part: ANGLE — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

CENTER CARGO DOOR AT AFT UPPER CORNER, AT THE DOOR EDGE HAS GOUGE. REMOVED EXISTING DAMAGED ANGLE IAW DC/10 SRM 51-31-01 VOL II. FABBED NEW REPAIR ANGLE IAW DC/MD 10 SRM 52-10-00 VOL I FIG 17. ALODINED AND PRIMED, AND INSTALLED IAW DC10/MD10 SRM 51-21-01 VOL II AND 51-31-01 VOL II, MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 1761 TO 1884, 9 INCHES RIGHT OF B/L SEAT TRACK HAS WORN AND GOUGED AREAS. REMOVED AND REPLACED SEAT TRACK IAW DC/MD10 53-70-00 FIGURE 1 VOL I. REMOVED AND REINSTALLED FLOOR PANELS IAW MD 10-10 AMM 53-70-00 FIGURE 1.

Part: LONGERON — CRACKED (ZONE 100) · airframe 81,090 hrs · 32,611 cycles

CENTER PIT STA 1750 TO 1761 L44L IS CRACKED. REPAIRED LONGERON L44L AT STA 1750 TO 1761 IAW DAC DRAWING AFA 3276 REV D, AND AGA3082 REV A, AND MD/DC 10 SRM 53-10-00 FIG 1 AND 2 VOLI.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 1761 TO 1884, 9 INCHES RIGHT OF B/L SEAT TRACK HAS WORN AND GOUGED AREAS. REMOVED AND REPLACED SEAT TRACK IAW DC/MD10 53-70-00 FIGURE 1 VOLI. REMOVED AND REINSTALLED FLOOR PANELS IAW MD 10-10 AMM 53-70-00 FIGURE 1.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,090 hrs · 32,611 cycles

MAIN CARGO COMPARTMENT STA 1761 TO 1884, 9 INCHES RIGHT OF B/L SEAT TRACK HAS WORN AND GOUGED AREAS. REMOVED AND REPLACED SEAT TRACK IAW DC/MD10 53-70-00 FIGURE 1 VOL I. REMOVED AND REINSTALLED FLOOR PANELS IAW MD 10-10 AMM 53-70-00 FIGURE 1.

Part: PITOT TUBE — CLOGGED (NR 1) · airframe 77,866 hrs · 31,211 cycles

ON TAKEOFF ROTATION CADC NR 1 FAILURE, LOST CAPT A/S, ALT, F/D, AP, ATS. COMPLIED WITH QRH. REPEAT WRITE UP. CONFIRMED NR 1 PITOT TUBE WAS CLOGGED FOUND WATER PITOT TUBES AND DRAIN HOLES CLOGGED. ALSO PURGED PITOT SYSTEM IAW MD-10 MM 34-11-00. SYSTEM OP'S CHECKS GOOD IAW MD-10 MM 34-11-00, NO FAULTS NOTED.

Part: ENGINE — FAILED (NR 3) · airframe 75,409 hrs · 30,109 cycles

AT CRUISE THRUST, NR 3 ENGINE STARTED COMPRESSOR STALLING FL 310. ALL PARAMETERS SHOWING MAJOR FLUCUATIONS, ALONG WITH AIRCRAFT YAW. NR 3 THROTTLE PULLED TO IDLE AND ALL INDICATIONS STABILIZED. AFTER A FEW MINUTES N1 STARTED FLUCUATIONS OF 10-12 PERCENT AND EGT 60 DEG CELSIUS. ENGINE SHUTDOWN AND DIVERTED TO MEM. THERE IS TIP CLANG ON SEVERAL STAGES OF THE HIGH PRESSURE COMPRESSOR. REMOVED AND REPLACED NR 3 ENGINE AS PER FED EX WORK CARDS 71T0701-3, LEAK AND OPS CHECK GOOD. A/C RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 76,070 hrs · 30,433 cycles

HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-72224 (REF FEDEX NRC N0410) REPLACED PANELS: ALC7205-1, ALC7206-1, ALC7207-1, ALC7208-1.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 73,992 hrs · 29,450 cycles

DURING CLIMBOUT AFTER T/O PASS 16,000 NR 3 GEN FAIL LIGHT ILLUMINATED. ACCOMPLISHED RED TABS THAT REQUIRE NR 3 GEN CSD TO BE DISCONNECTED. STARTED APU & IT RAN NORMAL FOR 10 MINS THEN APU LOW OIL PRESSURE LIGHT ILLUMINATED & APU SHUT DOWN. DUMPED FUEL & RTN DUE TO WX EN ROUTE TO MEMPHIS.

Part: CAP — CRACKED (L/E SLAT) · airframe 72,143 hrs · 28,505 cycles

LEFT WING SLAT INBOARD END CAP CRACKED IN NUMEROUS PLACES. UPON REMOVAL OF END CAP FOUND 1 OTHER INTERNAL RIB CRACKED.

Part: BRAKE — FIRE (NR 7)

NR 7 BRAKE ON FIRE AT BLOCK-IN. REMOVED AND REPLACED NR 7 BRAKE ASSY AND NR 7 MAIN TIRE REF MM 32-43-01, 32-41-01.

Part: TARGET — BROKEN (RH MG DOOR) · airframe 71,948 hrs · 28,403 cycles

01-203 ON T/O AT GEAR RETRACTION RMLG IND (BOTH PILOT & S/O POS) REMAIN RED WITH L/MAIN & NOSE GEAR IND UP, RECYCLED GEAR PER RED TABS PROC & RMG IND REMAIN RED. R&R RH GEAR DOOR UPLOCK TARGET PER DC10 MM 32-34-2-1.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 70,844 hrs · 27,876 cycles

DURING AC P-F CONVERSION AT AERONAVALI A, 6 INCH CRACK FOUND AT Y=1386 ON P/N AEA0501-2 KEEL WEB UPPER SPLICE ONLY. REPAIR REQUIRES A STOP DRILL ON BOTH ENDS OF THE CRACK AND THE INSTALL OF A REPAIR DOUBLER AS PER FEDEX 8-5314-48005.

Part: FRAME — GOUGED (FUSELAGE) · airframe 70,844 hrs · 27,876 cycles

DUR AC P-F CONVERSION AT AERONAVALI, A DEEP GOUGE WAS FOUND ON LH Y=595 FUSELAGE FRAME, I/B FLANGE, I/B SIDE AT Z=-18. REPAIR REQUIRES A CUT OUT OF DAMAGE AND INSTALL OF FILLER AND REPAIR STRAP PER FEDEX EA 8-5312-47975.