N10060

Part: VIA — MALFUNCTIONED (NR 3) · airframe 67,331 hrs · 28,104 cycles

DURING TAKEOFF ROLL SEVERAL OF THE DU'S STARTED TO FLASH ON AND OFF. ALSO RECEIVED A CONFIGURATION WARNING. ABORTED TAKEOFF AT APPOX 90 KTS. R&R #3 VIA PRECAUTIONARILY - OPS CHK GOOD. REF 31-43-01-4.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 66,910 hrs · 27,811 cycles

RECEIVED LEVEL 1 ALERT "AIR SYS 2 OFF". 2 MINUTES LATER RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL". RAN QRH. LEVEL 3 ALERT EXTINGUISHED WHEN NR 2 THROTTLE PULLED TO IDLE VIA QRH DIRECTION. RESTORED MEL DEACTIVATIONS TO NORMAL CONFIG PERFORMED AIR SYSTEM TEST WITH NO FAILURES NUMEROUS TIMES. REMOVED AND REPLACED RELAY R2-8990 PER FIM 36-23-00-2 AS PRECAUTIONARY. RECHECK AIR SYSTEM TEST WITH NO FAILURES PER FIM 36-23-00-2. DECAY CHECK STILL CHECKS GOOD AT 22 SECS. SYSTEM OK FOR SERVICE.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 66,584 hrs · 27,610 cycles

LT STA.1156 HAS AN OVERSIZE HOLE REF PART # ARB0323-1 REPAIR WILL BE REPAIRED ON E.A. 8-5310-T0344334 REPAIRED PER EA#8-5310-T0344334 FUSELAGE-MAINFRAME-STA.1156 BLKHD TEE CAP- OVERSIZED HOLES REPAIR.

Part: SUPPORT — CORRODED (VERTICAL STAB) · airframe 66,584 hrs · 27,610 cycles

VERTICAL STAB, BOTTOM SUPPORT BRACE FOR PANEL 374FR IS CORRODED. REPLACED BOTTOM SUPPORT WITH NEW SERVICEABLE SUPPORT ANGLE PER MD-10 SRM 51- 31-01 VOL. 2. AND DOUGLAS DRAWING AMC7202.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 66,584 hrs · 27,610 cycles

L/H WING, #3 SPOILER, UPPER SURFACE AT STA. XOSP3 609, HAS AN EXISTING SKIN DOUBLER, APPROX. 4' DIA. REPAIRE PER SRM 57-00-01 FIG.4 SHT.1

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 66,584 hrs · 27,610 cycles

[R/H WING I/B FLAP...TOP FWD SURFACE..APPROX C/L....WEAR MARK/GOUGE ON FLAP SKIN... REFERENCE...SNRM #203, 2018-11-30] REPAIRED THE DAMAGE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & R.S.C. TRACKING EA # 8-5710-T0343639, PART 1

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 66,584 hrs · 27,610 cycles

[R/H WING, I/B FLAP HAS DAMAGE ON TOP OF SKIN BY STA. XIFH 155., 2018-11-30] REPAIRED THE R/H WING, I/B FLAP UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & TRACKING EA # 8-5710-T0343639, PART 3

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 66,584 hrs · 27,610 cycles

[RH INBD FLAP DAMAGED ON TOP SIDE OF FLAP., 2018-11-30] REPAIRED DAMAGE ON THE R/H FLAP, UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL1 & TRACKING EA # 8-5710-T0343639, PART 2

Part: SPAR — OUT OF ALIGNMENT (RT HORIZ STAB) · airframe 66,584 hrs · 27,610 cycles

RT HORIZ SPAR CAP BARREL NUT BOLT HOLE IS MISALIGNED. REPAIRED PER EA 8-5510-T0343409 "HORIZONTAL STABILIZER- RT UPPER REAR SPAR REPAIR"

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 LBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-49 PER DWG AGA7091 REF SRM 51-35-01 VOL 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

LT STA. 1156 FWD HOZ LEG HAS 4 EA. OPEN HOLES BETWEEN LONGERON 38L-39L IN SKIN AND AYB7000-1 FITTING AND 1 EA. OPEN HOLE ON AFT HORZ LEG IN SKIN HAVE CRACK INDICATIONS. REPAIRED PER EA # 8-5310-T0344334 FUSELAGE- MAINFRAME-STA.1156 BLKHD TEE CAP- OVERSIZED HOLES REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 RBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-50 PER DWG AGA7091 REF SRM 51-35-01 VOL 2.

Part: SKIN — CRACKED (RT WING) · airframe 66,584 hrs · 27,610 cycles

RT WING LE INTERNAL STRUCTURE BEADED DOUBLER CRACKED, THREE (3) PLACES, LOCATION APPROX XORS 817, OUTBD OF NR 14 SLAT TRACK, ACCESS THROUGH FUEL VALVE PANEL 626FB. CRACK LENGTHS APPROX 1.00", .500" AND .250". CRACKS CONFIRMED AND ENDS MARKED USING NDT HFEC. REPAIRED SKIN OUTBOARD OF NUMBER 14 SLAT TRACK ON RIGHT WING PER SRM 57-10-00 FIG 71 VOL 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 66,584 hrs · 27,610 cycles

MAIN CABIN, STA 435 - 475 FLOOR IS SPONGY AND DELAMINATED. FABRICATED NEW FLOOR PANEL 225BF, STA 435 TO STA 475 REF DWG SRZ-25-005.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CRACKED AT STA 455 RBL 10. REPLACED FLOOR SUPPORT ABA7423-1 PER SRM 51-31-01 VOL 2, AND DWG ABA7423.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN CARGO COMPT APPROX STA 455 TO 475, X=-47.50 SEAT TRACK CHANNEL CORRODED. INSTALLED SEAT TRACK PER SRM 51-31-01 VOL 2 AND DRAWING NBA6018.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN CARGO COMPT: APPROX STA 435 TO 455, X=8.50 FLOOR SUPPORT SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPROX STATION 435-485, LBL 8.5 REF SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-01 VOL 2 AND DWG SR10-53-002 AND DAC DWG NBA6022.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN CARGO COMPT CENTER FLOOR SUPPORT APPROX STA 392 TO 435, X=0. FLOOR SUPPORT SHOWS CORROSION. INSTALLED NEW SEAT TRACK PER SRM 51-31-01 VOL 2 AND DAC DWG NBA6018.

Part: FITTING — CRACKED (RT WING) · airframe 66,584 hrs · 27,610 cycles

RIGHT WING LEADING EDGE STA 1159 AT APPROX LONG 30 T-CAP ANGLE FITTING IS CRACKED MARKED 23 STATION 1159 RBL. LONG 30 AT LEADING EDGE REMOVED AND REPLACED T-CAP ANGLE FITTING PER SRM 57-20-00 FIG. 6 SHEET 3-503 FRONT SPA TO FRAME REPAIR. ALSO IN CONJUNCTION WITH EA 8-5710-T0344122 A P1. WING-BASIC WING STRUCTURE-RIGHT WING, FORWARD, UPPER SPAR CAP AT STATION 1159 CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN CARGO COMPT: APPROX STA 435 TO 455, X=-8.50 SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPROX STATION 435-485, RBL 8.5 REF SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-01 VOL 2 AND DWG SR10-53-002 AND DAC DWG NBA6022.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK- FOUND EXISTENT FLOOR PANEL REPAIR IS COMING OFF AT STA 775 LBL 100. FABRICATED NEW FLOOR PNL AT STA 775 LBL 100 REF DWG SRZ-25-005.

Part: FLOORBOARD — CORRODED (ZONE 200) · airframe 66,584 hrs · 27,610 cycles

MAIN CABIN FLOORBOARD DELAMINATED, STA 475 TO STA 495 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-005.

Part: SKIN — NONE (A/C DOOR) · airframe 66,584 hrs · 27,610 cycles

#3 AIR COND. COMPT. DOOR, STA. 496-525, HAS AN EXISTING DOUBLER ON TOP EDGE. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 52-10-00 FIG. 2, SHT. 2, VOL. 1.

Part: FLOORBOARD — CORRODED (ZONE 200) · airframe 66,584 hrs · 27,610 cycles

MAIN CABIN FLOORBOARD SHOWS EVIDENCE OF CORROSION, STA 435 TO STA 475 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-005.

Part: SKIN — CRACKED (BS 1156) · airframe 66,584 hrs · 27,610 cycles

R/H FUSELAGE SKIN AT STA. 1156 HAS A .400 IN. CRACK AT THE AFT FASTENER HOLE COMMON TO THE TEE CAP (2 FASTENERS ABOVE LONGERON 39R) PROPAGATING AFT TO THE EDGE OF SKIN PANEL. (MARKED) WORKED I.A.W E.A # 8-5310-T0343606 (FUSELAGE-MAINFRAME-FUSELAGE SKIN AND FRAME AT STATION 1156, L-37 AND JUST ABOVE L-39, R/H/S-REPAIR)

Part: SEAT TRACK — WORN (BS 1260) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK COMPT STA1260 48LBL SEAT TRACK LOBE WORN (MARKED) INSTALLED AND SEAL NEW SEAT TRACK REF. SRM 53-70-00 FIG. 1 VOL. 1 AND SRM 51-31-01 VOL. 2.

Part: SPAR CAP — CRACKED (RT HORIZ STAB) · airframe 66,584 hrs · 27,610 cycles

RT HORIZONTAL STAB, OUTER SECTION UPPER AFT SPAR CAP HAS A CRACK APPROX .400" LONG ORIGINATING AFT OF AFT BARREL NUT HOLE CONTINUING TO AFT EDGE OF SPAR CAP. REPAIRED RT HORIZ STAB SPAR ER EA 8-5510-T0343409 REF SEQ 827 W/O 72895 MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK STA 735 LBL 28-48 FLOOR BOARD SUPPORT HAS CORROSION DAMAGE. REMOVE AN REPLACED NEWLY FABRICATED FLOOR BOARD SUPPORT ACA7417-17 STA 735 LBL 28-48. REF DRAWING ACA7417.

Part: SEAT TRACK — WORN (BS 1541) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK COMPT STA1541 22RBL SEAT TRACK LOBE WORN (MARKED) REPLACED DAMAGED SECTION OF SEAT TRACK FROM STATION 1541 TO STATION 1581. REFERENCE SRM 53-70-00 FIGURE 1 VOL 1 .

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,584 hrs · 27,610 cycles

MAIN DECK COMPT STA1260 48RBL SEAT TRACK LOBE WORN. REMOVED AND REPLACED SEAT TRACK ON MAIN DECK COMPT AT EXISTING SPLICE FROM APPROX STATION 1246 TO STATION 1330, 48 RBL REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2 AND DWG SR10-53-002.

Part: SKIN — CORRODED (RT WING) · airframe 66,584 hrs · 27,610 cycles

RH WING UPPER SURFACE APPROX XORS 264 STRINGER 12 - CORROSION AROUND FASTENER. REMOVED CORROSION AT APPROX XORS264 STRINGER 12 RH WING UPPER SURFACE AROUND FASTENER REF MD10 SRM 57-10-00 VOL1 FIG 60 SHT 1 MATERIAL REMOVED WAS APPROX .028 MAX ALLOWED IS .017 PER MD 10 SRM 57-10-00 VOL 1 FIG 61 SHT,1. AREA IS OUT OF LIMITS MAX MATERIAL REMOVED IS .028 BOEING FOUND ACCEPTABLE PER NOTED INSTRUCTIONS AS A PERMANENT REPAIR E.A. 8-5710-T0343538. TITLE WINGS BASIC WING STRUCTURE RH WING UPPER SKIN CORROSION REPAIR XORS 264 AT STRINGER 12.

Part: APU — SMOKE · airframe 65,273 hrs · 26,782 cycles

APU SMOKE. APU SHUTDOWN (AUTO). OBSERVED SMOKE FROM APU. DEPLOYED FIRE AGENT TO APU.

Part: TEE FITTING — CRACKED (BS 1156) · airframe 63,892 hrs · 25,988 cycles

BS 1156 BULKHEAD TEE FITTING VERTICAL LEG CRACKED ABOVE LONGERON 39L. REPAIRED IAW EA 8-5310-T0328855

Part: FITTING — CRACKED (NR 3 PYLON) · airframe 63,892 hrs · 25,988 cycles

NR 3 PYLON AFT BULKHEAD FITTING HAS A CRACK INDICATION AT THE FOURTH HOLE FROM OTBD SIDE. REPAIRED IAW EA 8-5400-T0329061.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 63,892 hrs · 25,988 cycles

NR 3 PYLON UPPER WEB OTBD SIDE HAS A CRACK INDICATION. REPAIRED IAW EA 8-5400-T0329061.

Part: BOLT — LOOSE (NR 3 NACELLE) · airframe 63,892 hrs · 25,988 cycles

NR 3 PYLON, UPPER AFT SECTION OF SPAR WEB, HAS 15 LOOSE BOLTS. REAMED HOLES TO FIRST OVERSIZE AND INSTALLED B/P BOLTS IAW SRM 54-20-00 F. 27, VOL I

Part: WEB — CRACKED (NR 3 PYLON) · airframe 63,892 hrs · 25,988 cycles

NR 3 PYLON, UPPERWEB , FOUND CRACK APPROX 1.75 INCH FROM EDGE OF UPPER SPAR WEB THRU 1 FASTENER HOLE TERMINATING AT I/B FASTENER HOLE OF AUB7031-11 DOUBLER. R&R WEB PER EA 8-5400--T0329061 AND SB 54-90.

Part: SKIN — CRACKED (RT WING) · airframe 63,892 hrs · 25,988 cycles

RT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 63,892 hrs · 25,988 cycles

RT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — WORN (RT WING) · airframe 63,892 hrs · 25,988 cycles

RT WING LOWER LEADING EDGE, AREAS COMMON TO PYLON, SKIN IS WORN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 87.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,892 hrs · 25,988 cycles

RIGHT WING INBD FLAP O/B HINGE PANEL 641CR DELAMINATED. REPAIRED THE DAMAGE IAW SRM 51-71-00 VOL II

Part: SKIN — DENTED (RT ELEVATOR) · airframe 63,892 hrs · 25,988 cycles

RIGHT ELEVATOR LOWER SURFACE CREASED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG. 8 VOL. I

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 63,892 hrs · 25,988 cycles

AFT CARGO BAY BS 1841 FLOORBEAM HAS SEVERAL AREAS WITH CORROSION. LBL TO RBL 18. REPAIRED IAW DWG AGA3874

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 63,892 hrs · 25,988 cycles

FWD CARGO ROLLER TRAY AT BS 920 DOOR ENTRY AREA CRACKED. REPLACED THE ROLLER TRAY IAW NDJ6030.

Part: ACOUSTIC PANEL — CRACKED (NOSE COWLING) · airframe 63,892 hrs · 25,988 cycles

NR 1 ENGINE NOSE COWL AT 12 O'CLOCK POSITION BETWEEN NOSE COWL LEADING EDGE AND ACOUSTIC PANEL HAS A CRACK. INSTALLED REPAIR DOUBLER PER SRM 54-11-00 FIG 1A.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 63,892 hrs · 25,988 cycles

RT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39R HAS A .5 IN CRACK AT THE UPPER AND LWR FASTENER. REPAIRED IAW EA 8-5310-T0328704.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 63,892 hrs · 25,988 cycles

LEFT BS 595 BULKHEAD TEE CAP AT LONGERON 39L HAS A .5 IN CRACK AT THE LWR FASTENER. REPAIRED IAW EA 8-5310-T0328709.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 63,892 hrs · 25,988 cycles

RT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .5 IN CRACK AT THE LOWER FASTENER. REPAIRED IAW EA 8-5310-T0328704.

Part: BOLT — SHEARED (NR 3 PYLON) · airframe 63,892 hrs · 25,988 cycles

NR 3 PYLON UPPER WEB SURFACE OTBD SIDE, ALONG THE EDGE HAS A SHEARED BOLT. REPAIRED IAW EA 8-5400-T0329061 AND SRM 54-20-00 FIG. 27, VOL. I.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 63,892 hrs · 25,988 cycles

RT WING FUEL ACCESS PANEL FWD INBOARD CORNER HAS A .200 IN. CRACK. REPAIRED PER SRM 57-10-00 FIG 68.

Part: SEAT TRACK — WORN (BS 1471-1551) · airframe 63,892 hrs · 25,988 cycles

SEAT TRACK BS 1520 RBL 47.50 SHOWS WEAR REPLACED THE SEAT TRACK IAW SRM 53-70- 00 VOL 1 FIG 2.

Part: SEAT TRACK — WORN (BS 1491-1521) · airframe 63,892 hrs · 25,988 cycles

SEAT TRACK BS 1521 LBL 8.50 WORN. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM BS 1491 TO 1531 IAW SRM 53- 70-00 VOL 1 FIG 1.

Part: SLIDE — FAILED (L1 DOOR) · airframe 63,789 hrs · 25,930 cycles

L1 DOOR SLIDE REMOTE PRESSURE TEST LIGHT ON. RELEASED FOR SERVICE IAW MEL: 52-10-03, CATEGORY-C, EXPIRATION: 08SEP16, MEL 52-10-03: L1 MAIN ENTRY SLIDE/RAFT INOPERATIVE, EXTENDED OVERWATER OPS REQUIRES 2 SLIDES AND/OR RAFTS. REPLACED LT DOOR EVACUATION SLIDE REF MM 25-61-02-4 IAW SDR REQUIRED INFORMATION: SLIDE AY, NR 1 LT SLIDE CONTAINER, PN: AWD7274-1L, SN: AA171.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 63,532 hrs · 25,787 cycles

CLIMBING THROUGH 10,000 FT, EXPERIENCED A FUME EVENT. PACKS 1 & 3 ON, PACK 2 OFF. VERY STRONG DIRTY SOCKS ODOR, LASTED 6 TO 8 MINUTES. OCCURRRED 10 MIN, 11,000 FT TO GROUND. R & R PACKS NR 1 AND NR 3 COALESCER BAG IAW AMM 21-54-03-2. CHECKS GOOD. NO LEAKS NOTED AT THIS TIME. RAN APU/PACKS 1 & 3 IAW JRH FOR 15 MINUTES WITH NO ODOR DETECTED. ACFT OK TO CONTINUE.

Part: PDU — SHORTED (CARGO BAY) · airframe 62,957 hrs · 25,488 cycles

LOWER FWD CARGO POS 7R PDU SHORTED, PULLED & COLLARED CB.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 62,849 hrs · 25,419 cycles

NR 1 ENG ANTI-ICE DISAGREE DURING CLIMB WITH ENG ANTI-ICE SELECTED ON. R & R ANTI-ICE VALVE IAW AMM 30-22-02-0-0. OPS CHECKED NORMAL, OK FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (BLEED AIR SYS) · airframe 626 hrs · 25,319 cycles

UPON INITIAL DESCENT WE SELECTED THE WING ANTI-ICE. WE THEN RECEIVED AN AIR MANF 1 FAIL. COMPLIED WITH CHECKLIST & CONTINUED UNEVENTFUL. THE ALERT EXTINGUISHED ON APPROACH AFTER TEMPERATURE DROPPED IN THE DUCT. R & R LT WING MANIFOLD FAIL DETECTOR PRESS SWITCH IAW AMM 36-23-03-4. CHECKED NORMAL. WITH WING ANTI-ICE ON ACCOMPLISHED GVI OF LT WING. CHECKED NORMAL.

Part: PRESSURE SWITCH — FAILED (FIRE AGENT) · airframe 621 hrs · 25,041 cycles

UPON TAXI IN, RECEIVED ENGINE FIRE AGNT LO LEVEL ONE ALERT, ACCOMPANIED BY AN OVERHEAD AGENT 1 LOW LIGHT NR 3 ENGINE. FOUND LOW PRESSURE SWITCH BAD. R & R FIRE EXTINGUISHING CONTAINER IAW & ALL OPERATIONS NORMAL IAW MM 26-21-01,

Part: VALVE — LEAKING (BOTTLE) · airframe 615 hrs · 24,698 cycles

L1 DOOR PNEUMATIC ASSIST BOTTLE NEEDS SERVICE & FOUND LEAKING A SERVICE PORT. REMOVED AND REPLACED RECHARGE VALVE IAW AMM 52-11-07-2. NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 615 hrs · 24,698 cycles

L1 DOOR PNEUMATIC ASSIST BOTTLE NEEDS SERVICE & FOUND LEAKING A SERVICE PORT. R & R RECHARGE VLV. NO LEAKS NOTED, SERVICED. ACFT OK FOR SERVICE.

Part: SUPPORT CHANNEL — CRACKED (LT WING) · airframe 61,189 hrs · 24,477 cycles

FLIGHT CONTROL PULLEY SUPPORT CHANNEL IS CRACKED AT LT WING REAR SPAR ABOVE NR 1 PYLON AFT FAIRING. R & R PULLEY SUPPORT CHANNEL IAW SRM 51-31-01 & COMPLIED WITH EA 8-5720-T0312122 REV A TITLE WING SECONDARY WING STRCT ARB0107-501 SUPPORT ASSEMBLY. MAJOR REPAIR.

Part: HINGE — CRACKED (PANLE) · airframe 61,189 hrs · 24,477 cycles

PANEL 362CR UPPER AFT HINGE LOBE IS BROKEN ON ACFT SIDE. REPAIR OF THE NACELLES, PYLON FILLETS FAIRINGS PANEL 362CR UPPER HINGE BROKEN LOBE. SPLICE REPAIR HAS BEEN ACCOMPLISHED IAW EA 8-5480-T0312263P1, WRI 54809675 STEPS 1 - 14, MAJOR REPAIR.

Part: RUB STRIP — CRACKED (APU DOOR) · airframe 61,189 hrs · 24,477 cycles

APU DOOR AFT RUB STRIP HAS WEAR MARKED & CRACKED. ACCOMPLISHED APU DOOR FORMER REPAIR IAW WRI 52409664 REV A OF EA 8-5240- T0311763 A.

Part: SKIN — GOUGED (RT WING) · airframe 61,189 hrs · 24,477 cycles

DEEP WEAR MARK ON RT WING LOWER SURFACE INBD END ALONG BUTT STRAP FWD END AREA. COVERED BY PANEL 154AB. BLENDED DAMAGE IAW SRM 57-00-01 FIG 14 SHEET 3. MECHANICALLY MEASURED MATERIAL LOSS .070 USING TOOL ID T83340 DUE 2/27/15. FOUND BLENDED AREA OUT OF LIMITS IAW SRM 57-00-01 FIG 1A SHEET 3. ACCOMPLISHED REPAIR IAW EA 8-5730-T0311636. COMPLIED WITH EA 8-5730-T0311636 REV NO POS P1.

Part: DOUBLER — CHAFED (NACELLE) · airframe 61,189 hrs · 24,477 cycles

PANEL 488DL THE INNER SURFACE DOUBLER IS CHAFED NEAR FASTENER HOLES PANEL ON PANEL RACK. AFTER REMOVAL OF DOUBLER FOUND ANGLE STIFFENER DAMAGED. REPAIRED DOUBLER & ANGLE STIFFENER IAW EA 8-5480-T0311956 REV NO PS P1. MINOR REPAIR.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 61,189 hrs · 24,477 cycles

AFT CARGO DOOR FWD LOWER CORNER SKIN EDGE DEFORMED & CRACKED. REMOVED FASTENERS & CUT OUT CRACKED AREA 1.3 INCH WIDTH X 1.750 IAW SRM 52-10-00 FIG 17 SHEET 1. NDT WAS PERFORMED ON CUT OUT IAW NTSPM 06-10-01. FILLER WAS FABRICATED 2024-T3 .071 BATCH 0001941519, FABRICATED EXTERNAL DOUBLER 2024-T3 .080 BATCH 0002670881 IAW SRM 52-10-00 FIG 17 SHEET 1. TREATED & PRIMED PARTS & AREA IAW SRM 51-21-01. INSTALLED REPAIR IAW SRM 52-10-00 FIG 17 SHEET 1. TOP COATED AREA IAW SRM 51-21-02. EA 8-5240-T0312000 DOORS SERVICE AFT CARGO DOOR SKIN REPAIR ISSUED FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

Part: ANGLE — GOUGED (LT WING) · airframe 61,189 hrs · 24,477 cycles

LEFT WING INBD TE PANEL ANGLE GOUGED AT OTBD END. REPAIRED IAW SRM VOL I 57-00-01 FIG.9

Part: STRUCTURE — GOUGED (NR 2 ENGINE) · airframe 61,189 hrs · 24,477 cycles

NUMBER 2 ENG LT CORE COWL UPPER EXTRUSION HAS DEEP GOUGE FWD OF AFT HINGE. REPAIR ACCOMPLISHED IAW EA 8-7113-T0311830 REV NO PS P1. MINOR REPAIR.

Part: FRAME — CHAFED (NR 2 ENGINE) · airframe 61,189 hrs · 24,477 cycles

NUMBER 2 ENG LT CORE COWL 2ND FRAME FROM AFT HAS CHAFE MARK. REPAIR ACCOMPLISHED IAW EA 8-7113-T0312063 REV NO PS P1. TITLE POWER PLANT COWL NR 2 END LT PYLON CORE COWL CHAFE. WELD ACCOMPLISHED ON T14 1096831. MINOR REPAIR.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 61,189 hrs · 24,477 cycles

CENTER CARGO DOOR FWD LOWER CORNER SKIN EDGE HAS CHAFED. REMOVED EXISTING REPAIR IAW SRM 51-31-01. INCREASED EXISTING CUT OUT TO INCLUDE NEW DAMAGE IAW SRM 52-10-01 FIG 17 L 3.20 INCHES W 1.06 INCHES. HFEC INSP CUT OUT IAW NTSPM 06-10-01, NO DEFECTS NOTED. FABRICATED NEW REPAIR PARTS & INSTALLED IAW SRM 52-10-01 FIG 17. EA 8-5240-T0312003 DOORS SERVICE CTR CARGO DOOR SKIN REPAIR ISSUED FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,189 hrs · 24,477 cycles

FUSELAGE STATION 1156 BETWEEN LONGERON 51L & 51R THRU CAC DOOR CUTOUT HAS CORRODED FRAME. R & R DAMAGED SHEAR TIE TEE-ANGLE IAW SRM 51-31-01. FABRICATED SHEAR TIE TEE-ANGLE ON TR 14 1093156 BATCH 0002362407. T ANGLE HAD 95% MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-00-01 FIG 1B MAJOR REPAIR.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

FORWARD CARGO DOOR CUT OUT AFT LOWER CORNER DOUBLER REPAIR HAS GOUGE. REMOVED DAMAGED REPAIR DOUBLER IAW SRM 51-31-01, FABRICATED NEW REPAIR DOUBLER FROM 2024 T3 .080 IAW SRM 53-50-00. INSTALLED NEW REPAIR DOUBLER IAW SRM 51-31-01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 979-1301) · corrosion level 2 · airframe 61,189 hrs · 24,477 cycles

SEAT TRACK LBL 108 BS 979 - 1301 HAS CORROSION. BLENDED SEAT TRACK IAW SRM 53-00-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-10- 00 FIG 5 SHEET 2 ITEM 3. R & R DAMAGED SEAT TRACK IAW SRM 53-70-00 & SRM 51-31-01.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL UPPER SKIN IS PUNCTURED AT BS 1661 - 1761 LBL 8 TO RBL 8. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094695. R & R FLOOR PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN CARGO DECK STATION 747, APPROX BL 0, FLOOR PANEL IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094694. R & R PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL ASSEMBLY STATION 1887 - 1902, LBL 59 - 90 HAS DELAMINATED SECTION. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094559. R & R FLOOR PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,189 hrs · 24,477 cycles

MAIN CARGO DECK STATION 731 APPROX BL0 FLOOR PANEL IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094693. R & R FLOOR PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MDCC FLOOR PANEL 273FF AFT CORNER FILLER VOID AT STATION 1401 TO 1501 RBL 8.50 TO RBL 27.50. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094554. MAJOR REPAIR.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 61,189 hrs · 24,477 cycles

MAIN CABIN DECK FLOORBOARD BETWEEN STATION 890 & 770, RBL 8 & RBL 24 BOARD IS SPONGY, DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1099577. R & R FLOOR PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (BS 890-979) · airframe 61,189 hrs · 24,477 cycles

MAIN CABIN DECK FLOORBOARD BETWEEN BS 890 - 979, LBL 8 - RBL 8 HAS 14 PUNCTURES ON LOWER SURFACE. FABRICATED NEW FLOORBOARD IAW SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL STATION 1361 - 1481 RBL 78 - 108 HAVE DAMAGE AT INSERT AREA. FABRICATED NEW PANEL IAW SRZ 25-005 ON T14 1094573. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL BS 1381 - 1481, RBL 8 - 24 HAVE DAMAGE AT INSERT AREA. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094574. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

CABIN FLOOR PANEL STATION 1281 - 1321 LBL 8 - RBL 8 IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094556. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,189 hrs · 24,477 cycles

MAIN CARGO COMPARTMENT FLOORBOARD BETWEEN STATION 1159 & 1239 & FROM SEAT TRACK RBL 75.25 & RBL 47.50 EDGE CORNER DAMAGE & DISBONDED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094557. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL STATION 1481 - 1501 RBL 8 - 24 HAVE DAMAGED AT INSERT AREA. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094571. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL STATION 1481 - 1561 RBL 48 - 78 HAVE DAMAGED INSERT AREA. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094572. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 1319-1321) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL AT BS 1319 - 1321 LBL 48 - 78 DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094578.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL STATION 1321 - 1361 LBL 48 - 78 HAVE DAMAGE AT INSERT AREA. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094575. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

FLOOR PANEL STATION 1321 - 1381 RBL 8 - LBL 8 DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094555. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (BS 1100-1160) · airframe 61,189 hrs · 24,477 cycles

MAIN DECK FLOOR PANEL BS 1100 - 1160 RBL 0 - 17 HAVE DELAMINATED SECTION. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 ON T14 1094560. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,189 hrs · 24,477 cycles

SEAT TRACK STATION 1159 - 1219 LBL 78 HAVE CORRODED AREAS. REMOVED CORROSION FROM SEAT TRACK IAW SRM 53-70-00. CHECKED LIMITS IAW SRM 53-70-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 NOTE 8. REMOVED SEAT TRACK FROM STATION 1129 - 1249 IAW SRM 51-31-01. FABRICATED SEAT TRACK & REPAIR SPLICE IAW SRM 53-70-00. INSTALLED SEAT TRACK & SPLICE IAW SRM 51-31- 01. PART MARKED IAW GMM 7-0-1001. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,189 hrs · 24,477 cycles

MAIN CARGO COMPARTMENT SEAT TRACK RBL 8.50 BETWEEN STATION 1129 & 1139 HAS GOUGED & CORROSION. FOUND AREA OUT OF LIMITS IAW SRM 53-70-00 FIG 5. REMOVED DAMAGED SECTION & FABRICATED NEW SEAT TRACK, 1 EA REPAIR SPLICE & 1 EA SPLICE PLATE, MATERIAL USE 7075-T6 .050C, 607158 7075 T6511, 60-4508 7075-T6511 IAW SRM 53-70-00 FIG 1A SHEET 1. INSTALLED SEAT TRACK IAW SRM 53-70-00 FIG 1A SHEET 1. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,189 hrs · 24,477 cycles

FOUND DAMAGED & CRACKED INTERCOSTAL AT FS 590 LONGERON 44L INSIDE ACFT BAY NR 1, CRACK RUNS THROUGH & OUT OF THE TOP OF THE LARGE FASTENER. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-31-01. LOCATED AND DRILLED NEW INTERCOSTAL. FABRICATED ON T14/1094058 IAW SRM 51-31-01. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW INTERCOSTAL IAW SRM 51-31-01.

Part: SWITCH — INTERMITTENT (R1 DOOR) · airframe 59,898 hrs · 23,824 cycles

ON PRE-FLIGHT, FOUND R1 DOOR ENTRY SLIDE PUSH TO TEST INOPERATIVE, OPS CHECKED PTT SWITCH ON R1 DOOR. OPS CHECKED GOOD IAW AMM 25-61-03-5.

Part: BATTERY PACK — INOPERATIVE (TEST LIGHT) · airframe 59,886 hrs · 23,818 cycles

R-1 ENTRY DOOR SLIDE INOPERATIVE IAW CREW DEBRIEF, R1 SLIDE INOPERATIVE FOR PRESSURE TEST, LIGHT NO WORKING. R & R TEST LIGHT BATTERIES IAW AMM 26-61-02-2. OPS CHECKED GOOD.

Part: LAMP — WRONG PART (ESCAPE SLIDE) · airframe 59,416 hrs · 23,583 cycles

EVACUATION SLIDE PRESS TO TEST LIGHT INOPERATIVE ON LT DOOR DURING PREFRIGHT. FOUND WRONG LAMPS INSTALLED. INSTALLED CORRECT LAMPS IAW SMP DR SIDE LIGHT WORKS NORMAL . ACFT OK FOR SERVICE.

Part: SLAT TRACK — DAMAGED (LE SLATS) · airframe 59,390 hrs · 23,559 cycles

LEVEL 2, SLAT DISAGREE ON TAKEOFF QRH COMPLIED WITH LEVEL 2 SLAT DISAGREE WITH FLAPS 15 DURING LANDING APPROACH. LEVEL 2 SLAT DISAGREE AFTER TAKEOFF, QRH COMPLIED WITH. TROUBLESHOT & FOUND NR 10 SLAT IDLE TRACK ON NR 4 SLAT RT WING WITH EXCESSIVE SIDE TO SIDE PLAY. WAS ABLE TO DUPLICATE PROBLEM BY HOLDING TRACK TO ONE SIDE OR THE OTHER. PSEU WOULD GO FROM OK TO ADJUSTMENT NEEDED. INSTALLED NR 10 SLAT IDLER TRACK AND R & R NR 8 SLAT IDLER TRACK REF AMM 27-80-04-4. ADJUSTED NR 4 SLAP POSITION SENSOR R4B. RETURNED ACFT TO SERVICE.

Part: PSEU — FAILED (FLAP/SLATS) · airframe 59,383 hrs · 23,554 cycles

WHEN FLAPS/SLATS EXTENDED TO FLAP 15, RECEIVED A SLAT DISAGREE ALERT. RAN QRH AND AND LANDED FLAPS 22/RET. CHECKED SYS IAW AMM 27-84-00-5 AND ALL TESTS OK, CFDS SHOWS NO PSEU SENSOR RIGGING FAULTS FOR THE LAST 10 LEGS, BUT DID INDICATE NUMEROUS LANDING GEAR FAULTS, BUT NO FLAP/SLAT FAULTS. PSEU FAULTS DURING RTS AFTER FLAPS/SLATS WERE CYCLED, R & R PSEU AND SYS OPS AND RST OK IAW AMM 31-71-01-2.

Part: PROXIMITY SWITCH — MALFUNCTIONED (SLAT/FLAPS) · airframe 59,381 hrs · 23,553 cycles

WHEN FLAPS/SLATS EXTENDED TO FLAP 15, RECEIVED A SLAT DISAGREE ALERT. RAN QRH AND LANDED. CHECKED SYS IAW AMM 27-84-00-5 AND ALL TESTS OK, CFDS SHOWS NO PSEU SENSOR RIGGING FAULTS FOR THE LAST 10 LEGS, BUT DID INDICATE NUMEROUS LANDING GEAR FAULTS, BUT NO FLAP/SLAT FAULTS. PSEU FAULTS DURING RTS AFTER FLAPS/SLATS WERE CYCLED, R & R PSEU AND SYS OPS AND RST OK IAW AMM 31-71-01-2.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 58,427 hrs · 23,019 cycles

LEFT WING NR 7 SLAT UPPER SURFACE INBD UPPER EDGE MISREPAIRED. REPAIRED AS PER EA 8-5750-162580 . REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,427 hrs · 23,019 cycles

MAIN DECK FLOOR SUPPORT BS 1900 X =60 CORRODED. REMOVED AND REPLACED AS PER DRAWING AGA 7551 REVISION 5 AND AMM 20-50-02 REVISION 14.3. E.O. 8-5100-7-5001B2 PART 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: STRUT — MISREPAIRED (BS 1964) · airframe 58,427 hrs · 23,019 cycles

AFT CARGO BAY STRUT, BS 1964 X = -56 MISREPAIRED. REPAIRED AS PER EA 8-5310-159893 . REPAIR CLASSIFED MAJOR AS PER GMM 6-2- 100 REV. 115

Part: FLOORBEAM — MISREPAIRED (ZONE 100) · airframe 58,427 hrs · 23,019 cycles

CENTER CARGO BAY FLOORBEAM AT BS 1701, LBL 34 MISREPAIRED. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01, VOL.2, REV.99. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 1801-1821) · airframe 58,427 hrs · 23,019 cycles

SKIN AFT OF CENTER CARGO DOOR CUTOUT AT BS 1801 TO 1821, BETWEEN LONGERON 41 RIGHT AND LONGERON 42 RT MISREPAIRED. CARRIED OUT REPAIR AS PER E.A.#8-5330-159882.

Part: SKIN — MISREPAIRED (BS 1851) · airframe 58,427 hrs · 23,019 cycles

FUSELAGE INTERIOR SKIN AT BS 1851, BETWEEN LONGERON 37 AND 38 RT. REPAIRED EA 8-5330-159882. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

LT WING OTBD FLAP LOWER SKIN MISREPAIRED. REPAIRED AS PER SRM 57-10- 00 FIG.85 VOL.I REV.99. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.

Part: SKIN — MISREPAIRED (RT WING AILERON) · airframe 58,427 hrs · 23,019 cycles

RT WING INBD AILERON UPPER SKIN MISREPAIRED. REPAIRED AS PER SRM 57-10-00 FIG.85 VOL.I REV.99 SHEET 2. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 58,427 hrs · 23,019 cycles

LT WING L/E NR 3 SLAT UPPER SURFACE APPROX AT STATION XOS 515 FOUND WITH SCRATCHES. REPAIRED AS PER SRM 57-10-00 SHEET 1 TO SHEET 2 FIGURE 43 VOLUME 1 REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 58,427 hrs · 23,019 cycles

LEFT WING NR 4 SLAT STATION XOS 645 MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159885. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION115.

Part: FRAME — MISREPAIRED (BS 535 L23L) · airframe 58,427 hrs · 23,019 cycles

FRAME BS 535, L23L MISREPAIRED. REPAIRED IAW SRM 53-30-00 FIGURE 13 VOLUME I REVISION 99 AND E.A. 8-5310-159883. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: FRAME — MISREPAIRED (BS 535 L19L) · airframe 58,427 hrs · 23,019 cycles

FRAME AT BS 535, LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-30-00 FIGURE 14 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SPAR CAP — CRACKED (LT WING) · airframe 58,427 hrs · 23,019 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON LT WING REAR SPAR LOWER CAP AT XORS 345 FOUND TWO CRACK INDICATIONS ON INBD CENTER HOLE AT 7 O'CLOCK AND 10 O'CLOCK POSITION FROM FORWARD LOOKING UP. APPROX 0.025 AND 0.187 INCH LENGTH RESPECTIVELY STARTING FROM UPPER EDGE OF SECOND LAYER DOWNWARD. REPAIRED AS PER EA 8-5710-159886, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SPAR CAP — CRACKED (LT WING) · airframe 58,427 hrs · 23,019 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON LT WING REAR SPAR LOWER CAP AT XORS 345 FOUND 01 EA CRACK INDICATION ON INBD FORWARD HOLE AT 7 O'CLOCK POSITION FROM FORWARD LOOKING UP. APPROX 0.035 IN LENGTH STARTING FROM UPPER EDGE OF SECOND LAYER DOWNWARD. CARRIED OUT REPAIR AS PER EA 8-5710-159886, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: FRAME — MISREPAIRED (BS 535 L19R) · airframe 58,427 hrs · 23,019 cycles

FRAME AT CABIN BS 535, L19R MISREPAIRED. REPAIRED AS PER SRM 53- 30-00 FIGURE 14 VOLUME 1 REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: FRAME — MISREPAIRED (BS 535 L23R) · airframe 58,427 hrs · 23,019 cycles

FRAME AT CABIN BS 535, LONGERON 23 RT MISREPAIRED. REPAIRED AS PER SRM 53-30-00 FIGURE 13 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 959 L40-41R) · airframe 58,427 hrs · 23,019 cycles

FORWARD CARGO DOOR CUTOUT EXTERIOR SKIN BS 959, BETWEEN LONGERON 40 - 41 RT MISREPAIRED. CARRIED OUT REPAIR AS PER 53-50-00 FIG.26 VOL.I REV.99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV.115

Part: SEAT TRACK — CORRODED (BS 1962) · corrosion level 2 · airframe 58,427 hrs · 23,019 cycles

MAIN DECK RT CURVE SEAT TRACK AT BS 1962, X = -107.25 FOUND CORRODED. REPAIRED AS PER SRM 53-70-00, FIGURE 1 VOLIME I, REVISION 99 AND EA 8-5310-159881. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 1790-1801) · airframe 58,427 hrs · 23,019 cycles

FUSELAGE EXTERIOR SKIN BS 1790 - 1801, BETWEEN L44 - 45 L MISREPAIRED. CARRIED OUT REPAIR AS PER EA 8-5330-159889 PART 1. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV 115.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

RIGHT INBD ELEVATOR LOWER SURFACE INBD T/E WEDGE FOUND DENTED. REPAIRED IAW SRM 55-33-00, FIG 2, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (BS 1775-1786) · airframe 58,427 hrs · 23,019 cycles

FUSELAGE EXTERIOR SKIN BS 1775 TO 1786, BETWEEN L45 - 46 L MISREPAIRED. CARRIED OUT REPAIR AS PER EA 8-5330-159889 PART 1. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

RT WING INBD FLAP T/E UPPER SKIN XIFH 237 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL 1, REV 99 AND EA 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

RT WING INBD FLAP UPPER SKIN STATION XIFH 217 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL.1, REV 99 AND EA NR 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

LEFT INBD ELEVATOR LOWER SURFACE T/E WEDGE MISREPAIRED. REPAIRED AS PER SRM 55-30-00 FIG.2 VOL.I REV.99. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.

Part: SKIN — MISREPAIRED (RT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

RIGHT OTBD ELEVATOR LOWER SURFACE MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL 1, REV 99 & EO 8-5100-7-5001B2, PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — DENTED (BS 1995 L39L) · airframe 58,427 hrs · 23,019 cycles

LOWER FUSELAGE EXTERIOR SKIN FOUND DENT AT STATION 1995, LONGERON 39 LT. DENT EXCEEDED LIMITS IAW SRM 53-20-00, FIGURE 13, VOL 1, REV 99 CARRIED OUT REPAIR IAW SRM 53-20-00, FIG 6, SHEET 16, VOL 1, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

LEFT WING INBD FLAP LOWER SURFACE APPROX STATION XIFH 201 MISREPAIRED. REPAIRED IAW EA 8-5750-159899, STEP 1 AND STEP 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

RT WING INBD FLAP T/E UPPER SKIN XIFH 207 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL 1, REV 99 AND EA 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (FWD CARGO DOOR) · airframe 58,427 hrs · 23,019 cycles

FORWARD CARGO DOOR LOWER AFT CORNER EXTERIOR SKIN MISREPAIRED. REPAIRED IAW EA NR 8-5230-159887. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

LEFT ELEVATOR UPPER SKIN STATION XE 233 MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL I, REV 99. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100 REV 115.

Part: FRAME — MISREPAIRED (BS 1381 L52) · airframe 58,427 hrs · 23,019 cycles

FRAME MISREPAIRED AT CENTER WHEEL WELL BS 1381, LONGERON 52. REPAIRED IAW SRM 53-30-00, FIG 4 VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (RT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

RIGHT INBD ELEVATOR UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL 1, REV 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

LEFT ELEVATOR UPPER SKIN STATION XE 142 MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL I, REV 99. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100 REV 115.

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 58,427 hrs · 23,019 cycles

LEFT ELEVATOR UPPER SKIN STATION XE 206 MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8 VOL I, REV 99. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100, REV 115.

Part: WEB — CRACKED (NR 3 NACELLE) · airframe 58,427 hrs · 23,019 cycles

NR 3 PYLON ON UPPER WEB STATION YN = 224 MISREPAIRED. REPAIRED IAW EA 8-5450-159884. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (NR 5 SLAT) · airframe 58,427 hrs · 23,019 cycles

LEFT WING NR 5 SLAT LOWER SKIN XORS 640 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 31, VOL 1, REV 99 AND EA 8-5750-159896. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115,

Part: SKIN — CRACKED (ZONE 500) · airframe 58,427 hrs · 23,019 cycles

LT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00, FIG 68, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 58,427 hrs · 23,019 cycles

RT WING NR 2 SLAT L/E UPPER SKIN APPROX STATION XIS 247 MISREPAIRED. REPAIRED IAW AMM 27-80-01-4, REV 14.3. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 58,427 hrs · 23,019 cycles

RT WING NR 1 SLAT UPPER SKIN STATION XIS 168.66 MISREPAIRED. REPAIRED IAW EA NR 8-5750-159897. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

RT WING OTBD FLAP LOWER SKIN MISREPAIRED. REPAIR ACCOMPLISHED IAW SRM 57-10-00, FIG 85, VOL I, REV 99, EO 8-5100-7-5001B2 PART 2. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 58,427 hrs · 23,019 cycles

LT WING L/E NR 7 SLAT LOWER SURFACE STATION XOS 900 MISREPAIRED. REPAIR AS PER EA 8-5750-162583. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115

Part: STRUCTURE — DEFORMED (CARGO DOOR) · airframe 58,427 hrs · 23,019 cycles

CENTER CARGO DOOR FORWARD LOWER CORNER FOUND DEFORMED. DEFORMED AREA TRIMMED OUT AND REPAIR CARRIED OUT EA 8-5230-159880. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 58,427 hrs · 23,019 cycles

CENTER LANDING GEAR WHEEL WELL LT VERTICAL BULKHEAD FOUND CRACKED AT BS 1492. REPAIRED IAW EA 8-5310-159894. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

LT WING INBD FLAP UPPER SKIN STATION XIFH 133 MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159899, STEP 1 & 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

LEFT WING INBD FLAP, UPPER SKIN STA XIFH 261.690 MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159899, STEP 3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,427 hrs · 23,019 cycles

LT WING INBD FLAP UPPER SKIN MIDREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159899 STEP 1 & 6. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE) · airframe 58,068 hrs · 22,830 cycles

ENGINE FAIL LIGHT ON. REJECTED T/O BY 96 KIAS. ACFT SET FOR AUTO THROTTLE TAKE OFF, NR 1 THROTTLE LAGGED 2 & 3. CLEARED DUST AND DEBRIS FROM AUTO CLUTCHES AND ACCOMPLISHED RTS TEST OF NR 1FCC (THRUST CONTROL MODULE) AND NR 2 FCC - RESULTS WERE FCC-1 ALL RTO TESTS PASSED WITH NORMAL THROTTLE MOVEMENT (FWD / AFT) NR 2 FCC ALL RTO TESTS PASSED WITH NORMAL THROTTLE MOVEMENT (FWD / AFT) SEVERAL TIMES ACCOMPLISHED MPA RUN PER MD-10-10 JRH ON NR 1, 2, & 3 ENGINES ALL READINGS WITHIN LIMITS. POWERPLANT ALIGNMENT TEST AT 85% AND 90% N1 TEST GOOD WITH NR 1 AND 3 ALIGNED & 2 1/4 KNOB AHEAD (ALL WITHIN LIMITS).

Part: AILERON SYS — MALFUNCTIONED · airframe 57,781 hrs · 22,668 cycles

AILERON FLIGHT CONTROL FEEL ABNORMALLY HEAVY FLIGHT CONTROL FEEL WHILE HAND FLYING. IT WAS SOME WHAT DIFFICULT TO FLY A PRECISE HEADING OR COURSE WHILE HAND FLYING. REMOVED AND REPLACED AILERON CONTROL CABLE UB, REPLACED PULLEY BRACKET. ADJUSTED AND RIGGED AILERONS CONTROL CABLES UB AND WB REF MD10-10 MM 27-10-00-5, 27-11-02-2, 27-00-00-2. OPS CHECKED OK FOR TEST FLIGHT.

Part: THRUST REVERSER — DAMAGED (ZONE 400) · airframe 57,394 hrs · 22,463 cycles

DURING TAXI, FOUND RT HALF OF NR 2 THRUST REVERSER TRANSCOWL BROKEN LOOSE AND BARELY HANGING ON TO ACFT. R & R NR 2 THRUST REVERSER.

Part: ENGINE — OVERTEMP (NR 3) · airframe 57,084 hrs · 22,301 cycles

ENG 3 EXCEEDENCE ON TAKEOFF. REJECTED TAKEOFF AT 93 KTS NR 3 N2 SHOWED 101.0 AMM 72-00-00-6-0, NR 3 ENGINE N2 OVERSPEED, 101.0, REQUIRES BORESCOPE OF CORE COMPRESSOR & HPT WITHIN 10 CYCLES. AMM 72-00-00-6-0. DEBRIEFED CREW NO HIGH BRAKE TEMP DURING REJECT OR TAXI BACK NOTED. COMPLIED WITH INSP OF INLET AND EXHAUST AREA OF NR 3 ENGINE. ITEM TRANSFERRED TO OIL. PERFORMED BORESCOPE NR 3 ENGINE ON HPC & HPT SECTION ON ENGINE NO LIMITING DEFECTS NOTED MM 72-00-6-0. TERMINATING ACTION ACCOMPLISHED FOR AMM 72-00-00-6-0. INSTALLED BOROSCOPE PLUGS B1-0, B1-1, B1-10, B1-15, B3-1 AND B3-2 AFTER INSPECTION.

Part: ENGINE — DAMAGED (NR 3) · airframe 56,777 hrs · 22,139 cycles

AFTER T/O AT 1500 AGL, EXPERIENCED HEAD WINDSHEAR ALERT AND DURING ESCAPE MANUEVER NR 3 N2 EXCEEDED LIMITS AT MAX OF 101.2 FLAPS WERE 14.2 DEG GEAR WAS UP. COMPLIED WITH INSPECTION OF NR 3 ENGINE INLET AND EXHAUST AREAS REF AMM 72-00-00-6-1. INTERRIGATED VIA FOR EXCEEDENCE, CONFIRMED N2 101.2%. PER CREW, NO EXCESSIVE MANUVERS PERFORMED. NR 3 ENGINE N2 EXCEEDANCE 101.2 FOR 3 SECONDS REQUIRES BORESCOPE INSPECTION OF CORE COMPRESSOR & HPT REF: M/M 72-00-00-6-1 PAGE 3 , N2 OVERSPEED INSPECTION. REMOVED THE FOLLOWING BORESCOPE PLUGS CALLED OUT ON PAGES 21 AND 22. FOR HPT. B3-1 AND B3-2. FOR COMPRESSOR INSPECTION:B1-0,B1-1,B1-10 COMPRESSOR BLADES/VANES AND HPT FOR BLADE DAMAGE IAW AMM 72-00-00-6-1 2C NO DEFECTS NOTED.

Part: LENS — MISSING (L1 DOOR SLIDE) · airframe 56,430 hrs · 21,935 cycles

L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATOR LENS COVER MISSING, PRESS TO TEST WORKS NORMAL. R & R L1 DOOR PRESS TO TEST CAP ASSY. PERFORMED OPS CHECK IAW AMM 25-61-02-5-0. PRESSED TO TEST SYS FOR BATTERY AND LIGHT FUNCTION. REMOTE INDICATOR LIGHT/SWITCH, LIGHT CAME ON. RELEASE SWITCH, LIGHT WENT OFF. OK FOR SERVICE.

Part: ANGLE — GOUGED (TAILCONE) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

LT TAILCONE APPROX AT STA 2230 PATIO DOOR HAS GOUGE ON MAIN FRAME. ACCOMPLISHED TAILCONE LT PATIO DOOR MAIN FRAME REPAIR IAW EA 8-5210-141189, MAJOR REPAIR.

Part: HINGE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

FWD PIT DOOR HINGE INTERIOR SURFACE HAS CORROSION. REMOVED AND REPLACED HINGE SECTIONS IAW SRM 51-31-01. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (DOOR FRAME LATCH) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 1 HAS DEFECT INDICATIONS IN BOLT HOLES: A, B, AND C. REWORKED MCD LOWER DOOR JAMG FITTING NR 1 BOLT HOLES A, B, AND C PER E.A. 8-5310-142239. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 6 HAS DEFECT INDICATIONS IN BOLT HOLES: A,B,C,& D. REWORKED PER E.A. 8-5310-42239. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 7 HAS DEFECT INDICATIONS IN BOLT HOLES: A,B,C,& D. REWORKED PER E.A. 8-5310-142239. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 5 HAS DEFECT INDICATIONS IN BOLT HOLES: A, B, C,& D. REWORKED PER E.A. 8-5310-142239. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 2 HAS DEFECT INDICATIONS IN BOLT HOLES: A, B, & C. REWORKED MCD LOWER DOOR JAMG FITTING NR 2 BOLT HOLES A, B, & C PER E.A. 8-5310-142239. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 55,724 hrs · 21,590 cycles

MCD LOWER DOOR JAMB FITTING NR 3 HAS DEFECT INDICATIONS IN BOLT HOLES: A, B, C, D. REWORKED MCD LOWER DOOR JAMG FITTING NR 3 BOLT HOLES A, B, C, AND D PER E.A. 8-5310-142239. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1490-1530) · airframe 55,724 hrs · 21,590 cycles

SEAT TRACK AT LBL 48 BETWEEN STA. 1490 AND STA. 1530 HAS SEVERAL WORN TRACK SCALLOPS. BLENDED AREA , AFTER REWORK FOUND OUT OF LIMITS PER SRM 53-70-00 PAGE 21. REMOVED SEAT TRACK PER SRM 53-70-00. FABRICATED NEW SEAT TRACK ON TRAVELER T10/848815 FROM 7075-T6511 BATCH 0001367821. LOCATED AND DRILLED NEW SEAT TRACK PER SRM 53-70-00 AND INSTALLED PER SRM 51-31-01.

Part: SEAT TRACK — WORN (BS 1381-1400) · airframe 55,724 hrs · 21,590 cycles

SEAT TRACK AT LBL 48 BETWEEN STA. 1381 AND STA. 1400 HAS SEVERAL WORN TRACK SCALLOPS. REMOVED AND REPLACED MCD SEAT TRACK SEGMENT AT LBL 48 BETWEEN STA. 1381 TO STA. 1400 IAW SRM 53-70-00, MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1630-1661) · airframe 55,724 hrs · 21,590 cycles

SEAT TRACK AT LBL 48 BETWEEN STA 1630 AND STA 1661 HAS SEVERAL WORN TRACK SCALLOPS. ABRICATED NEW SECTION OF SEAT TRACK ON STAM TRAVELER T10/848877 AND REPAIR PARTS ON TRAVELER T10/848872. REPLACED SEAT TRACK IAW SRM 53-70-00. CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 55,724 hrs · 21,590 cycles

FWD PIT DOOR FRAME BELOW DOOR MOTOR HAS STRESS CRACK ON LOWER SURFACE. REMOVED DAMAGE IAW SRM 53-50-00, PERFORMED HFEC OF REMOVAL AREA IAW NTSPM 06-10-01 WITH NO CRACK INDICATIONS NOTED. REPLACED TEE ANGLE AT STA 919 FROM EXTRUSION 60-10846 BATCH 0001894810 IAW SRM 51-31-01. FABRICATED REPAIR DOUBLER FROM 7075-T6 0.125 BATCH 1788276 IAW SRM 53-50-00. INSTALLED REPAIR DOUBLER IAW SRM 53-50-00 FIG. 10. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 55,724 hrs · 21,590 cycles

SEAT TRACK AT LBL 48 BETWEEN STA 1761 AND STA 1825 HAS SEVERAL WORN TRACK SCALLOPS. REPAIRED SEAT TRACK IAW SRM 53-70-00. FABRICATED PARTS ON STAM TRAVELER T10/848878 AND T10/848873. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 55,724 hrs · 21,590 cycles

SEAT TRACK AT LBL 48 BETWEEN STA. 1239 AND STA. 1360 HAS SEVERAL WORN TRACK SCALLOPS. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-70-00. FABRICATED AND INSTALLED NEW SEAT TRACK ON TRAVELER T10/849149 AND IAW SRM 53-70-00.

Part: SKIN — CRACKED (ZONE 500) · airframe 53,210 hrs · 20,342 cycles

LT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E.

Part: SKIN — CRACKED (LT WING) · airframe 53,210 hrs · 20,342 cycles

LT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: ACCESS PANEL — CRACKED (NR 3 NACELLE) · airframe 53,210 hrs · 20,342 cycles

AFTER REMOVAL ACCESS PANELS OF PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND CRACK ON HORIZ WEB UPPER. REPAIRED CRACK IAW SRM 54-00-01 FIG 2B SHT 2 VOL I.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

AIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP. REPAIRED AREA IAW SRM 53-00-01 FIG 8 SHT 1, 3, 4 VOL I.

Part: ANGLE — CORRODED (APU BAY) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

AIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP.

Part: SKIN — WORN (ZONE 600) · airframe 53,210 hrs · 20,342 cycles

RT WING L/E DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 39.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

DURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

DURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 SHT 1-4 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

FWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION.

Part: SKIN — CORRODED (NR 2 SPOILER) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

RT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

FWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.

Part: SKIN — CORRODED (NR 2 SPOILER) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

RT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2. NO ACTION TAKEN SPOILER WILL BE REPLACED WITH NRC N01190.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 53,210 hrs · 20,342 cycles

LT MLG WW FOUND CRACK ON VERTICAL BULKHEAD.

Part: BULKHEAD — CRACKED (BS 1501) · airframe 53,210 hrs · 20,342 cycles

LT MLG WW FOUND CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 4 VOL I.

Part: SKIN — CORRODED (RUDDER) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

UPPER AFT RUDDER FOUND CORROSION MODERATE ABOVE SKIN AND SUSPECT INNER SKIN. REPAIRED AREA IAW SRM 55-10-00 VOL I FIG 2.

Part: RIB — CRACKED (ZONE 500) · airframe 53,210 hrs · 20,342 cycles

RT WING L/E DROOPED FOUND NR 3 BROKEN ANGLES INT DROOPED. REPAIRED AREA IAW SRM 57-00-01 FIG 1,3,4 VOL I.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

AFT CARGO COMPT TUNNEL AREA FOUND MODERATE CORROSION ON STRUT. REPAIRED AREA IAW SRM 53-00-01 FIG 7 SHT 4 TO 7 VOL I.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

AFT CARGO COMPT TUNNEL AREA FOUND MODERATE CORROSION ON STRUT.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

AFT CARGO COMPT TUNNEL AREA FOUND MODERATE CORROSION ON STRUT.

Part: SILL — CORRODED (ZONE 800) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

CTR CARGO COMPT DOOR SILL AREA FOUND CORROSION WITH EXFOLIATION ON TEE CAP OF JAMB. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 3-10 AND 11 VOL I AND FIG 4 SHT 2 VOL I.

Part: SILL — CORRODED (BS 1701) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

CTR CARGO COMPT DOOR SILL AREA FOUND CORROSION WITH EXFOLIATION ON TEE CAP OF JAMB.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

FWD CARGO COMPT BILGE AREA FOUND ELONGATED HOLE.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

FWD CARGO COMPT BILGE AREA FOUND ELONGATED HOLE. REPAIRED AREA IAW SRM 53-10-00 FIG 1/2 VOL I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN DAMAGED HOLES ON SEAT TRACK.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN DAMAGED HOLES ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN EXFOLIATION CORROSION ON SEAT TRACK. REPAIR AREA IAW SRM 53-70-00 FIG 1 VOL 1.

Part: WEB — CRACKED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

UPPER AFT FUSELAGE COMPT INTERNAL ZONE FOUND CRACK ON HORIZONTAL WEB. REPAIRED AREA IAW SRM 53-40-00 FIG 41 VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN EXFOLIATION CORROSION ON SEAT TRACK. REPAIR AREA IAW SRM 53-70-00 FIG.1 SHT 3 AND 4 VOL I.

Part: BEAM — CRACKED (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

CTR CARGO COMPT SUMP AREA FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 53,210 hrs · 20,342 cycles

LT WING L/E FOUND CRACK ON INT RIB L/E . REPAIRED RIB IAW SRM 57-00-01 VOL I FIG 10 SHEET 1.

Part: SKIN — CRACKED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN, 2 CRACKS 2 INCHES AND 1.5 INCHES LONG ON WEB ON FWD R3 JAMB AT STA 1254 BTWN L26 AND L27 RT SIDE. REPAIR JAMB IAW SRM 53-50-00 FIG 19 SHEET 1, 3, AND 6 VOL 1.

Part: SKIN — CRACKED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN, CRACK 1.5 INCH LONG ON WEB ON AFT L3 JAMB AT STA 1306 BETWEEN L23 AND L27 LT SIDE. REPAIR JAMB IAW SRM 53-50-00 FIG 19 SHEET 2, 3 AND 6 VOL 1.

Part: SKIN — CRACKED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN, 2 CRACK 1.5 INCH LONG ON WEB ON AFT R3 JAMB AT STA 1306 BTWN L26 AND L27 RT SIDE. REPAIR JAMB IAW SRM 53-50-00 FIG 19 SHEET 2, 3 AND 6 VOL 1.

Part: ANGLE — CRACKED (LT WING TIP) · airframe 53,210 hrs · 20,342 cycles

LT WING L/E, FOUND 1 CRACK 1" LONG ON ANGLE INT WING TIP. REPAIR ANGLE IAW SRM 57-00-01 VOL.1 FIG.10 SHT 1.

Part: SKIN — CRACKED (ZONE 200) · airframe 53,210 hrs · 20,342 cycles

MAIN CABIN, 2 CRACKS 2 INCH AND 1.5 INCH LONG ON WEB ON FWD L3 JAMB AT STA 1254 BTWN L26 AND L27 LT SIDE. REPAIR JAMB IAW SRM 53-50-00 FIG 19 SHEET 1, 3 AND 6 VOL 1.

Part: SKIN — DENTED (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

EXT FUSELAGE LWR SURFACE FOUND DENT 1 INCH BY 1 INCH DEEP .080 INCH ON SKIN NEAR EDGE OF DOUBLER. REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHEET 2 A & SHEET 5 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

EXT FUSELAGE LWR SURFACE FOUND DENT 1 INCH BY 0.85 INCH DEEP .080 INCH ON SKIN DOUBLER (SEE NRC N00072). REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHEET 2 A & SHT 5 VOL I.

Part: SKIN — WORN (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

DURING INSPECTION EXT LWR FUSELAGE FOUND DEEP WEAR ON SKIN AND ON EXISTING DOUBLER OF AFT JAMB FWD CARGO DOOR.

Part: SKIN — WORN (ZONE 100) · airframe 53,210 hrs · 20,342 cycles

DURING INSPECTION, EXT LWR FUSELAGE FOUND DEEP WEAR ON SKIN AND ON EXISTING DOUBLER OF AFT JAMB FWD CARGO DOOR. REPAIRED AREA IAW SRM 53-50-00 FIG 9 SHT 1 AND 2 VOL I AND FIG 15A SHT 9 VOL I.

Part: SKIN — GOUGED (FUSELAGE) · airframe 51,087 hrs · 19,229 cycles

MAIN CARGO DOOR BOTTOM JAMB AREA EXTERNAL FUSELAGE SKIN IS GOUGED AT 19 PLACES, LONGERON 27L TO LONGERON 28L STA 615 TO STA 765 BLENDED AREA, FROM STA 702 TO STA 773, FOUND TO BE WITHIN LIMITS IAW DC10-10 SRM 53-00-01 FIG 1, VOL I, AREAS FROM STA 615 - STA 676 AT L27L TO L28L FOUND TO BE BEYOND LIMITS IAW DC10-10 SRM 53-00-01 FIG 4 VOL1. FABRICATED REPAIR IAW DC10-10 SRM 53-50-00 FIG 6 VOL II ALODINED AND PRIMED REPAIR IAW DC10-10 SRM 51-21-01 VOL II PG 20 AND 21. INSTALLED REPAIR IAW DC10 SRM 53-50-00 VOL II FIG. REMOVED AND REINSTALLED DUCTS IAW DC10 AMM 36-14-02. ACCOMPLISHED LEAK CHECK IAW DC10 AMM 36-14-02-04 LEAK CHECK GOOD MAJOR REPAIR.

Part: SKIN — CRACKED (L/E SLAT) · airframe 51,087 hrs · 19,229 cycles

RIGHT WING NR 2SLAT OUTBOARD TRAILING EDGE UPPER AND LOWER SKIN IS CRACKED ACCOMPLISHED REPAIR IAW DC10 SRM 57-10-00 FIG 32 PG 3 VOL I, 57-10-00 FIG 43 PG 145 VOL I, 57-00-01 FIG 10 PG 29 VOL I, 51-35-01 VOL II AND DAC DWG ARB1647 REV C. THIS WAS A MAJOR REPAIR. COULD NOT ADJUST SLAT TO CLEARANCES AFTER REPAIRS, SLAT WAS REMOVED AND REPLACED WITH SERVICABLE SLAT, SEE SNRM N00604 AND N01262 ON FEDEX WORK ORDER 00033777, S/N OFF46989, S/N ON MAC33.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 51,087 hrs · 19,229 cycles

LEFT MLG FWD TRUNNION, GREASE FITTINGS ARE NOT TAKING GREASE, 2 W/O 33777-N/R N01306. REMOVED GREASE FITTINGS REF DC10MM 12-21-01-3. REMOVED FWD AND AFT LUG BUSHINGS REF DC10 MM 32-11-01-4. CORROSION REMOVAL FWD AND AFT LUGS FOUND TO BE WITHIN LIMITS REF MD/DC10 SRM 57-20-00 VOL I. FABRICATED, ALODINED, PRIMED AND INSTALLED NEW BUSHINGS REF DAC DWG APB 3846-513 REV F, MD/DC10 SRM 51-21-00 VOLII, DC10 MM 32-11-01-4 AND MD/DC10 SRM 57-20-00 VOL I. GREASE FITTINGS INSTALLED AND LUBED PER DC10 MM 12-21-01-3 AND FEDEX CARD 32B1101. LT MLG INSTALLED ON CARD 32T1701-L, MAJOR REPAIR.

Part: ATTACH ANGLE — CORRODED (ZONE 500) · corrosion level 2 · airframe 51,087 hrs · 19,229 cycles

LEFT WING TIP LOWER CENTER ACCESS OPENING, DOUBLER AND NUT PLATES CORRODED. REMOVED WING TIP IAW DC 10-10 MM 57-23-01-2. REMOVED CORRODED ATTACH ANGLES. FABRICATED UPPER ANGLE -5 IAW DAC DRW ARC0777-5, REV C. FABRICATED LOWER ANGLE -3 IAW DAC DRW ARCO605-3 REV F. CORROSION TREATED IAW MD/DC 10-10 SRM 51-21-01 VOL II. INSTALLED INNER WEB AND ANGLES IAW DAC DWG ARC 077-5 REV C. INSTALLED CONTROL ROD AND FITTING REFERENCE DC 10-10 MM 27-10-02-4. RECONNECTED WING TIP LIGHTS AND OPS CHECKED IAW DC 10-10 MMM 33-44-01 AND 33-47-00-5. MEG OHM CHECK STATIC WICKS IAW DC 10-10 MM 23-60-00-2. CHECK GOOD. THIS IS A MAJOR REPAIR. SEE SNRM N00516 OF FEDEX WORK ORDER 00033777.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,087 hrs · 19,229 cycles

MAIN CABIN SEAT TRACK WORN BETWEEN STA1159 AND 1190 BBL 47. NON-ROUTINE-N00378 REMOVED AND REPLACED CORRODED SEAT TRACK, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK IAW MD/DC 10 SRM 53-70-00 VOL I PAGE 21 AND 52-21-01 VOL II PAGE19. MECH 110207, QC 388.

Part: LONGERON — CRACKED (ZONE 100) · airframe 51,087 hrs · 19,229 cycles

IN AFT FUSELAGE ACCESS 311AB, IS CRACKED JUST FORWARD OF AFT BULKHEAD. NON-ROUTINE-N00883 REPAIR IAW EA 8-5310-96497-FUSELAGE, AFT BODY KEEL CAP SPLICE AT STA 2040, REPAIR. MECH 7965 QC 423 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1169-1249) · airframe 51,087 hrs · 19,229 cycles

FOUND CABIN STA 1169-1249 RBL76 SEAT TRACK CORRODED. REMOVED, DRILLED AND INSTALLED SEAT TRACK AND SPLICE IAW 53-70-00, FIG,1 VOL I, MAJOR REPAIR MECH 4644 QC388.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,087 hrs · 19,229 cycles

FOUND MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 842 AND STA 890 RBL 8. REMOVED CORROSION, FABBED AND INSTALLED SPLICE, LOCATED, DRILLED AND INSTALLED SEAT TRACK IAW MD/DC 10 SRM 53-70-00 FIGURE 1A PAGE 7, VOL I, AND 51-31-01 VOL II MAJOR REPAIR MECH 7593 QC311.

Part: FITTING — CORRODED (ZONE 700) · airframe 51,087 hrs · 19,229 cycles

LEFT MAIN LANDING GEAR FWD TRUNNION GREASE FITTINGS ARE NOT TAKING GREASE, W/O 33777-N/R N1306.

Part: LONGERON — CORRODED (ZONE 100) · airframe 51,087 hrs · 19,229 cycles

CENTER CARGO BAY L52 STA.1521-1526, UPPER SURFACE IS CORRODED. REMOVED AND REPLACED CORRODED LONGERON, LOCATED, DRILLED AND INSTALLED LONGERON IAW DRAWING NEA 6076, REV AK, MD SRM 51-33-01 FIG 1, PAGE 1, VOL II. MAJOR REPAIR, MECH 7198 QC340.

Part: SEAT TRACK — GOUGED (BS 1154) · airframe 51,087 hrs · 19,229 cycles

FOUND CABIN STA 1154 LBL 27 SEAT TRACK SCALLOP GOUGED, W/O 33777, N00393. REMOVED GOUGE IAW SRM 51-21-01 VOL. 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 SHEET 2. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: FRAME — CORRODED (ZONE 100) · airframe 51,087 hrs · 19,229 cycles

CENTER LANDING GEAR, FWD SIDE OF FRAME AT STA 1381, L52 CORRODED. REMOVED CORROSION, FABBED FILLER AND DOUBLER. INSTALLED REPAIR IAW MD/DC 10 SRM 53-30-00 VOL I,51-31-01 VOL I.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,087 hrs · 19,229 cycles

MAIN CABIN AT APPROX STA 631, SEAT TRACK AT LBL 27 IS GOUGED. REMOVED, FABBED AND INSTALLED NEW SEAT TRACK IAW DC10-SRM 51-21-01 VOL II PAGE1, 51- 21-01 VOL II, PAGE II.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,087 hrs · 19,229 cycles

MAIN CABIN SEAT TRACK WORN BETWEEN STA 1055 TO 1062 RBL 27 REMOVED CORROSION, FABBED SEAT TRACK. INSTALLED SEAT TRACK IAW MD/DC-10 SRM 51-31-01, 51-21-01, 53- 70-00.

Part: LONGERON — CORRODED (BS1681-1701 S39L) · airframe 51,087 hrs · 19,229 cycles

CORROSION IN SEVERAL PLACES AT L-39L LT TUNNEL OF CARGO PIT BETWEEN FS 1681 AND 1701. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW MD/DC 10-10 SRM 53-10-00 VOL I, 53-20--00 VOL I FIG 6.

Part: SEAT TRACK — GOUGED (BS 999-1011) · airframe 51,087 hrs · 19,229 cycles

FOUND MAIN CABIN SEAT TRACK BETWEEN STA 999 TO 1011, AT LBL 8 IS GOUGED. REMOVED DAMAGED SEAT TRACK (OUT OF LIMIT AREA) IAW DC10 SRM 53-70-00 VOL 1. INSTALLED REPAIR (PLUG IN SEAT TRACK) IAW DC10 SRM 53-70-00 PG 11 VOL 1. REINSTALLED FLOOR PANELS STA 999-1099 LBL 8 -28 IAW DC10 AMM 53-21-08-02.

Part: FRAME — GOUGED (BS 590) · airframe 51,087 hrs · 19,229 cycles

NR 1 A/C COMPT FRAME AT STA 590 HAS DEEP GOUGES DOT K2963 REPAIRED FRAME AT STA 590 OF NR 1 A/C COMPARTMENT IAW DC10 SRM 53-30-00 VOL 1 FIG 4 PG 13.

Part: SKIN — DENTED (TE FLAP) · airframe 51,087 hrs · 19,229 cycles

LT OB FLAP, MID LOWER SKIN NUMEROUS DENTS DOT M5582 DENTS FOUND TO BE OUT OF LIMITS IAW DC/ MD -10 SRM 57-10-00 FIG 48 VOL 1. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER AND FILLER IAW DC/ MD 10 SRM 57-10-00 FIG 85 VOL 1. ALODINED AND PRIMED IAW DC/ MD SRM 51-21-01 PAGE 21 THRU 24 VOL 2. INSTALLED DOUBLER AND FILLER IAW DC/ MD 10 SRM 51-35-02 PG 1 VOL 2.

Part: DOUBLER — CHAFED (RT WING) · airframe 51,087 hrs · 19,229 cycles

RT WING O/B OF NR 3 ENGINE L/E DOUBLER IS CHAFED. REMOVED CHAFED DOUBLER IAW DC/MD10 SRM 51-35-01 VOL II MAT. ID FOR NEW DOUBLER 7075-T6 - .050 PO 543347.6 AND FABRICATED IAW DC/MD10 SRM 57-10-00 FIG 40 VOL 1. ALODINED AND PRIMED IAW DC/MD10 SRM 51-21-01 PG 21-24 VOL II. INSTALLED DOUBLER IAW DC/MD10 SRM 51-35-01 VOL II.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 48,738 hrs · 18,007 cycles

CLIMBING THROUGH 5000 FT, WINGS LVL, THERE WAS A STICK SHAKER ANNUNCIATION WITH ASSOCIATED SLAT RESET LIGHT DUE TO AUTO-SLAT EXTEND. COMPLETED UNSCHEDULED AUTO SLAT EXTENSION &/OR UNSCHEDULED STICK SHAKER RED TAB PROCEDURE. ELECTED TO RETURN TO IND, & LANDED UNEVENTFULLY. PERFORMED ADJ/TEST OF BOTH AT/SC COMPUTERS NR 1 CKS NORMAL. NR 2 COMP TEST WAS INTERMITTENT. R/R,D NR 2 AT/SC AND TESTED PER DC10-10 AMM 22-31-01-2. SYS OPS CHK NORMAL. PERFORMED ADJ/TEST OF BOTH NR 1 & NR 2 LAU,S PER DC10-10 AMM 22-11-01-2. BOTH OPS CHK NORMAL. AUTO SLAT TEST PER DC10-10 AMM 22-30-00-5. SYS OPS CHK OK. STALL WARNING TEST OF NR 1 AND NR 2 SYSTEMS FROM COCKPIT PER DC10-10 AMM 22-33-00-0. BOTH SYSTEMS OPS CHK OK.

Part: HINGE — CORRODED (ZONE 500) · airframe 48,733 hrs · 17,999 cycles

LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC19-10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED AND FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1,0005 INCHES IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS-LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP-REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 48,733 hrs · 17,999 cycles

LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1.0005 IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP REPAIR. REFERENCE NON-ROUTINE N00468.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,733 hrs · 17,999 cycles

CABIN SEAT TRACK F CORRODED FUSELAGE STATION 959 - 1130. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION OF SEAT TRACK IAW DC10 SRM 53-70-00 VOL 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,733 hrs · 17,999 cycles

CABIN SEAT TRACK -B- CORRODED BETWEEN FUSELAGE STATION 1850 - 1879. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC10 SRM 53-70-00 VOL I AND 51-31-01 VOL 2.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 48,272 hrs · 17,767 cycles

LT, INBD SIDE, NR 1 SLAT HAS APPROX. 56 INCH LONG CRACK ON INNER SURFACE, BOTTOM EDGE BELOW CLOSEOUT WEB. FASTENERS MISSING/PULLED. INSTALLED NEW NR 1 SLAT LT S/N MAC86 PER AMM 27-80-01-4 PARA 3(B) 1-13. RIGGED AND ADJUSTED LT NR 1 SLAT PER MM 27-80-01-4 3(B) 14-23.

Part: SLAT TRACK — WORN (LT WING) · airframe 48,272 hrs · 17,767 cycles

LT WING FIXED L/E WORN FROM NR 1 SLAT TRACK INBD TO FUSELAGE IN SEVERAL PLACES, CAUSED FROM NR 1 SLAT LWR LIP. CUT OUT DAMAGED AREA FAB REPAIR DOUBLER PER SRM 57-10-00 FIG 40. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 PAGE 129 FIG 40. N/R 64 GENERATED TO SUPPLEMENT ORIGINAL N/R 47. DISCREPANCY REPAIR ACCOMPLISHED ON LT FIXED L/E EXCEEDS SRM 57-10-00 FIG 40 LIMITS IN AREA ADJACENT TO NR 1 SLAT TRACK CUT OUT ON INBD SIDE. FABRICATED (1) REPAIR SKIN FROM .040 CLAD 7075-T6; AND FABRICATED(1) REPAIR DOUBLER FROM .025 301 1/2 HD S.S. INSTALLED REPAIR IN REF TO SRM 57-10-00 VOL1 FIG 39 REPAIR 4 AND REF SRM 57-10-00 VOL 1 FIG 40.

Part: BOLT — LOOSE (NR 3 PYLON) · airframe 45,976 hrs · 16,770 cycles

NR 3 ENG UPPER PYLON HAS NUMEROUS 1/4 BOLT LOOSE ON LT, RT, FWD AND AFT SIDE OF FWD AND AFT THRUST LINK FITTING (MARKED WITH RED). REPLACED (24) LOOSE BOLTS AND TORQUED REMAINING FASTENERS REF SRM 51-31-01 AND M/M 20-50-02-2. HFEC INSPECTED AROUND NEW BOLTS, NO INDICATIONS.

Part: BOLT — LOOSE (NR 1 PYLON) · airframe 45,976 hrs · 16,770 cycles

NR 1 PYLON, TOP PYLON COVER PLATE (AFT OF FWD PYLON MT TO AFT PYLON TO WING MT), BOLTS ARE LOOSE.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 45,633 hrs · 16,615 cycles

HYD SYS 3 ELEV OFF LIGHT & NR 3 HYD SYS QTY LOSS, EN ROUTE. ACCOMPLISHED RED TABS AND LANDED ATL. MANUFACTURED HYDRAULIC LINE AND ACCOMPLISHED REPAIR PER M/M 20-10-01-02, PRESSURIZED NUMBER THREE HYDRAULIC SYSTEM AND LEAK CHECKED GOOD. COMPLIED WITH EA NR 8-2912-71222 PART 1. NOTE ITEM GENERATED DUE TO FAILED HYD LINE IN NR 3 SYSTEM REPAIRED AS NOTED ABOVE.

Part: SWITCH ACTUATOR — DAMAGED (LANDING GEAR)

AFTER TAKEOFF WITH GEAR HANDLE UP, GOT THREE RED GEAR INDICATORS WITH GEAR HORN. CYCLED GEAR 2 TIMES, NO CHANGE. COMPLIED WITH EMERGENCY PROCEDURES. FOUND LANDING GEAR SWITCH 5341 ACTUATOR DAMAGED. REMOVED AND REPLACED SWITCH ACTUATOR 5341 PER M/M 76-11-04. OPS CHECKED NORMAL.