N396FE

Part: SENSOR — FAILED (LE SLAT) · airframe 89,697 hrs · 38,305 cycles

UPON SLAT RETRACT AFTER T/O CHECK LIST, SLAT DISAGREE ILLUMINATED, CYCLED SLAT EXTEND & BACK TO UP WITH NO FAULT. REMOVED AND REPLACED L2B SLAT POSITION SENSOR. OPS CHECKED SATISFACTORY. OK FOR SERVICE.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 89,569 hrs · 38,223 cycles

MAIN ENTRY DOOR 1-L SLIDE RAFT INOP. REMOVED AND REPLACED L1 DOOR SLIDE AND CONTAINER IAW AMM 25-61-01-2. ALL OPS CHECKS AND PRESSURES GOOD. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 89,518 hrs · 38,190 cycles

2" CRACK LT WING BELOW #1 SLAT SHGN 04SEP19 18:09 MEM U CHECKED THE GENERAL AREA FOR CRACKED MATERIAL. USING HFEC REF NDTSPM PART 6. LOCATED A FLAW INDICATING APPROXIMATLY 2 INCHES IN LENGTH. PAINT WILL NEED TO BE REMOVED TO DETERMINE THE ACTUAL LENGTH INSTALLED REPAIR PER SRM 57-10-00 FIG 68 AND EA # : 8-5730-T0349300 PT 1 - WINGS - PLATES AND SKINS - LT WING LEADING EDGE, CRACK ADJACENT TO THE NR 1 SLAT TRACK CUTOUT.

Part: SKIN — CRACKED (TE FLAP) · airframe 89,057 hrs · 37,868 cycles

RT WING OB FLAP UPPER SUFACE SKIN CRACKED (EST 3" FRONT TO BACK) REPAIRED USING SRM 57-10-00 FIG 85 AS A REFERENCE.

Part: TRUSS — CRACKED (NR 3 PYLON) · airframe 88,611 hrs · 37,586 cycles

NR 3 PYLON TRUSS FITTING INBOARD TRUSS HALF OUTBOARD EDGE HAS A CRACK INDICATION. REPAIRED PER E.A. 8-5450-T0342532. MAJOR REPAIR.

Part: LONGERON — CRACKED (NLG WW) · airframe 88,611 hrs · 37,586 cycles

NOSE WHEEL WELL, AFT DOOR ON THE LT SIDE IS BINDING ON THE SKIN WHEN CLOSING, 2018-10-23. REMOVED AND REPLACED THE LONGERON AT STA 548 TO STA 595 LONGERON 48L, NOSE WHEEL WELL PER DWG ACA 3796, EA 8-5310-T0327817 C, PART 3 & SRM 51-31-01 VOL 2.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 88,611 hrs · 37,586 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD STA.1781 LONGERON R42 L-ANGLE BRACKET SHOWING EXFOLIATING CORROSION. REMOVED & REPLACED "T-ANGLE BRACKET" AFB3883-505 AT STA. 1781 LONGERON R42 PER DWG AFA3878.

Part: LONGERON — CRACKED (NLG WW) · airframe 88,611 hrs · 37,586 cycles

NOSE W/W LT DOOR JAMB - LONGERON CRACKED PAST STOP DRILL AT STA.584. PART ACA3796-1 REQUIRES REPLACEMENT. REMOVED & REPLACED LONGERON AT STA. 548-STA.595 L48L NOSE W/W PER DWG ACA3796 & SRM 51-31-01 VOLII

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 88,611 hrs · 37,586 cycles

LT WING NR 5 SPOILER UPPER SKIN HAS 5 3/4 " X 7 1/4" OF DELAMINATION. REPAIRED LT WING NR 5 SPOILER IAW SRM 51-71-00 VOL II PAR 16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 88,611 hrs · 37,586 cycles

FWD CARGO COMPT STA 1099 SHEAR TIE CRACKED AT LEG. REPAIRED CRACKED SHEAR TIE AT STA 1099 PER SRM 53-30-00 VOL 1 PAGE 34.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,611 hrs · 37,586 cycles

R/H WING, TOP SKIN HAS CORROSION OUT OF LIMITS BETWEEN STR. -10 AND 11 XTA. XROS 346 REMOVED CORROSION PER SRM 57-10-00 FIG 61 VOL 1 AND EA# 8-5710-T0342487

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 88,611 hrs · 37,586 cycles

LT WING NR 5 SPOILER UPPER SKIN HAS 5 3/4" X 7 1/4" OF DELAMINATION. REPAIR LT WING NR 5 SPOILER IAW SRM 51-71-00 VOL II PAR 16.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 88,611 hrs · 37,586 cycles

MAIN DECK SEAT TRACK STA 755 LT X=47.5 LBL WORN BEYOND LIMITS. REPLACED DAMAGED SEAT TRACK, FROM STA 745 - 765 REF SRM 53-70-00 FIG 1 V1 & DWG NCA6392.

Part: SKIN — UNKNOWN (ZONE 300) · airframe 88,611 hrs · 37,586 cycles

REPAIR ASSESSMENT: R/H DETACHABLE ELEVATOR, UPPER SURFACE, STA. XE 91, 28" FROM TRAILING EDGE, HAS AN EXISTING DOUBLER. APPROX 4" DIA. DOT 105 REPAIR WAS PREVIOUSLY INSTALLED PER SRM 55-00-01 FIG. 3 SH.2 VOL.1. REF. E.A. 8-5100- T034059 "STRUCTURES-REPAIR CATALOG-MD10" ATTACHMENT A-1 # 105. REF. E.A. 8-5520- T0342428A "STABILIZER/ELEV-RH INBD DET ELEV-RSC TRACKING" "MAJOR REPAIR"

Part: SKIN — CRACKED (RT WING) · airframe 88,611 hrs · 37,586 cycles

RT LWR WING ACCESS DOOR CUTOUT FASTENER ATTACH HOLE 1 EA HAS A CRACK INDICATION AT FWD EDGE HOLE. REPAIRED AREA PER EA. 8-5730-T0342637.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,611 hrs · 37,586 cycles

RT WING UPPER SKIN AT FASTENERS SURFACE CORROSION STA XORS 360. REMOVED CORROSION PER SRM 57-10-00.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,611 hrs · 37,586 cycles

RT WING UPPER SKIN SURFACE CORROSION AT ROW OF FASTENERS AFT O/B OF PYLON CENTERLINE STA XORS 346. REMOVED CORROSION PER SRM 57-10-00.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,611 hrs · 37,586 cycles

RT WING UPPER SKIN CORROSION AT FASTENER STA XORS 400 20 INCH FWD OF AFT SPAR. REMOVED CORROSION PER SRM 57-10-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 88,611 hrs · 37,586 cycles

MAIN DECK SEAT TRACK STA 635 RT X = -8.50 LBL WORN BEYOND LIMITS. REPAIRED SEAT-TRACK SPLICE PER SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 88,611 hrs · 37,586 cycles

MAIN DECK SEAT TRACK STA 755 LT X = 8.50 LBL WORN BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 VOL I FROM STA 725-780.

Part: SOLENOID — CORRODED (L1 DOOR) · airframe 87,707 hrs · 37,028 cycles

L1 DOOR WILL ONLY OPEN 12 INCHES. DOOR CLOSED AND LOCKED. CND PROBLEM OPS CHECKED NORMAL SEVERAL TIMES, BUT DID NOTICE THE OPEN CLOSE SOLENOID WAS RUSTY, POSSIBLY INTERMITTENTLY CAUSING THE PROBLEM. REMOVED AND REPLACED OPEN - CLOSE LOCK SOLENOID.

Part: SWITCH — FAILED (PAX DOOR) · airframe 87,656 hrs · 36,999 cycles

PDIS 396 52-10 5671 09DEC17 MEM OPEN U LOGPAGES:2767437 POST FLIGHT, UNABLE TO OPEN L1 DOOR. INDICATES DISARMED. REMOVED AND REPLACED L1 INTERIOR DOOR SWITCH S1-1205 PER MD10 WDM 52-10-01 AND SWPM CHAP 20. L1 PASSENGER DOOR OPS CK'S OK PER MD10-10 M/M REF 52-10-01-5. PER GMM 12-7-600 SDR EVENT......TRACKING LEVEL 0 PART.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 86,910 hrs · 36,525 cycles

SMOKE IN COCKPIT ON ARRIVAL AT FL 300. WHITE ACRID SMOKE DISSAPATED WITHIN 3-5 MINUTES. AIR TEMP KNOBS WERE TURNED DOWN AND NR 2 PACK TURNED OFF. NO ALERTS, BELLS, LIGHTS, OR WARNINGS OF ANY KIND. REMOVED AND REPLACED THE WATER SEPARATOR CONICAL COALESCER ON ALL 3 PACKS IAW AMM 21-54-03-2. OP CHECKED GOOD. ACFT OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 86,350 hrs · 36,218 cycles

ON PREFLIGHT- SELECTING EMERGENCY POWER TO "ARM"- NO "ON" LIGHT. PERFORMED EPCU RTS IAW AMM 24-08-01-5, NO DEFECTS NOTED. PERFORMED ELECTRICAL EMERGENCY POWER SYSTEMS TEST IAW AMM 24-00-00-5, NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 979) · corrosion level 2 · airframe 85,800 hrs · 35,947 cycles

FWD CARGO BS 979, BS 979 LBL 18 FLOORBEAM CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-01 FIG.3 SHEET 1.

Part: FLOORBEAM — CORRODED (BS 979) · corrosion level 2 · airframe 85,800 hrs · 35,947 cycles

FWD CARGO BS 979, RBL 16 FLOORBEAM HAS CORROSION 1.5 BY 3 INCHES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-60-01 FIG.3 SHEET 1.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

ACM BAY 1, BS 594 APPROX LONGERON 33L IS CRACKED ON THE OUTER SKIN DOUBLER. REPAIRED THE DOUBLER IAW EA 8-5330-T0328088.

Part: COWLING — CRACKED (RT ENGINE) · airframe 85,800 hrs · 35,947 cycles

NR 2 ENGINE RT FAN COWL FORWARD LANDING, A/C SIDE, CRACKED AT LOWER SECTION, MARKED DOT 9, 2016-09-04. REPAIRED THE NR 2 ENGINE RT FAN COWL, FWD LANDING, A/C SIDE, IN REF TO SRM 54-10-00, FIG 20, SHEETS 1 THRU 5, VOL 1.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 85,800 hrs · 35,947 cycles

DURING OVERSPEED INSPECTION, FOUND RT INBD DETACHABLE ELEVATOR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED DENTS AREAS ON RT INBD DETACHABLE ELEVATOR UPPER SURFACE REF SRM 55-00-01, VOL 1.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

LT SIDE STA 595 T-CHORD AT LONGERON 39L HAS APPROXIMATELY 2" CRACK ON VERTICAL LEG, 2016-09-03 SECTION OF TEE CHORD WAS R & R AT STA 595 BETWEEN LONGERON 39L & 43L IN REF TO EA 8-5310-T0327401.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 85,800 hrs · 35,947 cycles

AFT FUSE, WASTE TANK COMPARTMENT STA 1967-1980 CENTERLINE SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES. AREAS MARKED, 2016-08-31. R & R CENTERLINE FLOOR SUPPORT BECAUSE OF CORROSION OUT OF LIMITS, PN: WSP0711-555 IAW SR DWG 10510131, INSTALLED FASTENERS IN REF TO SRM 51-31-01 FIG 1 VOL 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 85,800 hrs · 35,947 cycles

AFT CARGO COMPARTMENT: STA 1902-1967 CEILING, CENTERLINE SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES. AREAS MARKED, 2016-08-31. R & R FLOOR SUPPORT DUE TO CORROSION OUT OF LIMITS, PN: WSP0711-543 IAW SR DWG 10510131, INSTALLED FASTENERS IN REF TO SRM 51-31-01, FIG 1, VOL 2.

Part: FLOOR SUPPORT — CORRODED (BS 374-395) · corrosion level 2 · airframe 85,800 hrs · 35,947 cycles

BS 374-395 75 RBL 107 FLOOR SUPPORT SHOWS LIGHT SURFACE CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DRAWING ABA7341 AND SRM 51-31-01 FIG 2 VOL 2.

Part: LONGERON — CRACKED (NLG WW) · airframe 85,800 hrs · 35,947 cycles

NOSE GEAR WW .75 INCH CRACK LOCATED JUST BELOW THE LT TRUNNION AND ABOVE THE LT STRUT DOOR. CRACK WAS PREVIOUSLY STOP DRILLED BUT APPEARS NO REPAIR HAS BEEN ADDED. REPAIRED CRACK REF EA 8-5310-T0327817.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A ONE INCH CRACK. SECTION OF TEE CHORD R & R AT STA 595 BETWEEN LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0327400 AND SRM 53-40-00, FIG 25, SHEET 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

BS 595 PRESSURE BULKHEAD WEB AT LONGERON 43L HAS CRACK INDICATIONS. REPAIRED PRESSURE BULKHEAD WEB, 3 EA FASTENER HOLES IAW SRM 53-40-00, FIG 25, SHEET 2 AND SRM 51-39-01, VOL 1.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

FWD CARGO COMPARTMENT TEE BRACKET HAS A CRACK. LT SIDE AT BS 595 BULKHEAD BETWEEN LONGERONS 44-45L. R & R TEE BRACKET, LT SIDE AT THE 595 BULKHEAD BETWEEN LONGERON 44L AND 45L, PN: NCA6044-187 IN REF TO DWG NCA6044.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

RIGHT STA 595 T-CHORD LONGERON 39R HAS APPROXIMATELY 2" CRACK IN VERTICAL FLANGE. SECTION OF TEE CHORD WAS R & R AT STA 595 BULKHEAD BETWEEN LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0327400 AND SRM 53-40-00, FIG 25, SHEET 1 THRU 3.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS A 1.0 IN. CRACK. DAMAGED SECTION OF TEE CAP ON LT SIDE, STA 595 AT LONGERON 43L REPAIRED IAW EA 8-5310-T0327401 AND SRM 53-40-00, FIG 25, SHEET 1. SECTION OF TEE CHORD WAS R & R AT STA 595 BETWEEN LONGERON 39L AND 43L IN REF TO EA 8-5310-T0327401.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

AFT FUSELAGE WASTE BAY CEILING BS 1980 LBL 24 SEAT TRACK UNDERSIDE NUT CLIP HOLE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DWG SP10510131.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

BS 595 RT SIDE T-CAP ON THE AFT FASTENER ROW OF THE HORIZONTAL LEG BETWEEN LONGERONS 38-39R HAVE CRACK INDICATIONS. REAMED THE HOLES ON THE AFT ROW OF HORIZONTAL LEG IAW SPM 51-39-01, VOL 2 AND DPS 1.33. INSTALLED BUSHINGS.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

STA 595 RT SIDE T-CAP ON THE FORWARD FASTENER ROW OF THE HORIZONTAL LEG AT LONGERON 38 HOLE HAS CRACK INDICATIONS. REAMED HOLE LABELED-A REAMED HOLE A TO .277 ON THE FORWARD ROW OF HORIZONTAL LEG AT LONGERON 37R REF: SRM 51-39-01, FIG 1, VOL 2. INSTALLED REPAIR BUSHING IN HOLE A REF SRM: 51-39-01, FIG 1, VOL 2 AND DPS 1.33.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

STA 595, RT SIDE T-CAP ON THE AFT FASTENER ROW OF THE HORIZONTAL LEG BETWEEN LONGERON 38-39, 3 HOLES HAVE CRACK INDICATIONS. REAMED 3 HOLES ON THE AFT ROW OF HORIZONTAL LEG BETWEEN LONGERON 38 & 39. HOLES LABLED B, C & D REAMED TO .277, REF SPM: 51-39-01, VOL 2 AND DPS 1.33 AND INSTALLED BUSHINGS, BETWEEN 38 & 39R, IN REF TO: DPS 1.33.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,800 hrs · 35,947 cycles

BS 595 RT SIDE TEE CAP ON THE UPPER FASTENER ROW OF THE VERTICAL LEG AT LONGERON 37 HAS CRACK INDICATIONS. REAMED IAW SRM 51-33-01, VOL 2 COMPLIED WITH HFEC INSPECTION IAW NDTSPM, TP-MDC-93KO393, NO DEFECTS NOTED. INSTALLED A BUSHING IAW SRM 51-39-01 VOL 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 85,800 hrs · 35,947 cycles

RIGHT WING INBD T/E FLAP UPPER SURFACE MID-SPAN AREA, SHOWING ONE DENT SPOT. REPAIRED IAW SRM 57-10-00 FIG 85 SHEET 2.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 85,598 hrs · 35,827 cycles

PASSING 11,000 FT, DURING DESCENT AT 250 KTS AT 2, 45 AFTER TACKOFF, EXPERIENCED FUME EVENT. ALL 3 BLEEDS ON, ISOL VALVES CLOSED AND PACKS 1 AND 3 ON. FUME EVENT ODOR WAS VERY STRONG, HUMID MUSTY SMELL. R & R NR 1 AND NR 3 COALESCER BAGS IAW AMM 21-54-03-2. RAN PACK SYSTEMS WITH NO FUMES. OPS CHECK GOOD.

Part: RIVET — SHEARED (NR 1 ENGINE) · airframe 85,368 hrs · 35,720 cycles

ON POST FLIGHT WALK AROUND FOUND NR 1 ENG CONICAL NOZZLE PLUG, AFT SECTION, MISSING. FOUND ALL RIVETS SHEARED AROUND AFT SECTION OF CONICAL NOZZLE PLUG. SEE ATTACHED PHOTOS. ONE REPLACED EXHAUST PLUG.

Part: CONNECTOR — DEFECTIVE (BRAKE TEMP) · airframe 85,309 hrs · 35,700 cycles

AFTER TAKEOFF, RECEIVED LEVEL 2, BRAKE OVERHEAT, MAX TEMP 692. LEVELED OFF AT 17,000 SLOWED, LOWERED GEAR FOR 10 MINUTES. RAISED GEAR, TEMP STARTED TO RISE. DIVERTED & LOWERED GEAR AT FL 200, LANDED FLAPS 50. R & R NR 6 BRAKE TEMP CONNECTOR IAW AMM 20-30-02-2-0. OPERATIONS CHECKED GOOD. BRAKE TEMP INDICATIONS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,628 hrs · 35,354 cycles

ON DESCENT, DUE TO RUNWAY CHANGE, EXTENDED LG AT 235 KTS, ONCE ON DESCENT RETRACTED GEAR AT 220 KTS, BOTH MAIN GEAR INDICATED UNSAFE UP ON RETRACT. EXTENDED GEAR & GOT 3 GREEN. PERFORMED A TEST OF PSEU SENSORS, ALL INDICATED OKAY. THERE WERE NO CURRENT FAULTS LISTED IN THE PSEU. VISUALLY INSPECTED ALL UP & DOWNLOCK & UPLOCK TARGETS & SENSORS, NOTHING ABNORMAL FOUND. CONSULTED WITH MOCC & WAS INFORMED THIS IS AN SDR. THE ONLY MM ADJUSTMENT TEST PROCEDURE REQUIRES A GEAR SWING. STILL RESEARCHING A POSSIBLE MM IAW MX. COMPLIED WITH IAW MM CH 32-61-15-5 FOR PROX SENSORS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,628 hrs · 35,354 cycles

ON DESCENT, DUE TO RNWY CHANGE, EXTENDED LG AT 235 KTS, ONCE ON DESCENT RETRACTED GEAR AT 220 KTS, BOTH MAIN GEAR INDICATED UNSAFE, UPON RETRACTION EXTENDED GEAR & GOT 3 GREEN. JACKED ACFT IAW AMM 07-11-00-2. PERFORMED MLG PROXIMITY SENSORS & TARGET TEST IAW AMM 32-61-15-5. ALL READINGS WITHIN LIMITS, GEAR EXTENDED & RETRACTED. PERFORMED LG EXTENSION & RETRACTION TIMED ACTUATION TEST IAW AMM 32-30-00-5. RETRACT TIME WAS 10 SECONDS WITH HYD OPERATIONS CHECKED GOOD. RETRACTED GEAR 8 TIMES, NO DISCREPANCIES NOTED. LANDING GEAR INDICATION OPERATIONS CHECKED GOOD. PERFORMED DETAILED VISUAL INSPECTION OF MLG PROXIMITY SENSORS. NO FAULTS FOUND.

Part: STRUCTURE — UNKNOWN (STAB) · airframe 839 hrs · 34,922 cycles

STABILIZER LT UPPER SPAR CAP & SKIN REPAIR. SHORING COMPLY WITH EA 8-5510-T0315116 REV NR A POS P1.

Part: INTERCOSTAL — CRACKED (BS 1953-1964) · airframe 83,465 hrs · 34,675 cycles

AFT CARGO BAY AFT WASTE TANK AREA BS 1953 - 1964 INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED A NEW PART IAW DWG AGA3225.

Part: SKIN — DAMAGED (NR 2 SPOILER) · airframe 83,465 hrs · 34,675 cycles

RIGHT WING NR 2 SPOILER TOP SURFACE DAMAGED. REPAIRED IAW SRM 57-00-01 FIGURE 4 SHEET 1.

Part: SKIN — DAMAGED (RT WING NR 5) · airframe 83,465 hrs · 34,675 cycles

RIGHT WING NR 5 SPOILER PANEL TOP SKIN DAMAGED. REPAIRED IAW SRM 57-00-01 FIGURE 4 SHEET 1.

Part: STANCHION — CORRODED (BS 1964) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

AFT CARGO BAY BS 1964 CTR STANCHION LOWER LT SIDE CORROSION. FABRICATED NEW STANCHION IAW DWG AGA3224, SRM 51-00-01 VOL 1 & SRM 51-21-01 VOL 2.

Part: STANCHION — CORRODED (BS 1953 BULKHEAD) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

AFT CARGO BAY AFT BULKHEAD VERTICAL STANTION BS 1953 LBL 22 UPPER AREA UNDER CAM-LOC RECEPTACLES HAS CORROSION. MANUFACTURED AFT BULKHEAD STANTION IAW DWG NGA6030.

Part: WEB — CRACKED (BS 1139-1159) · airframe 83,465 hrs · 34,675 cycles

MAIN CABIN LONGERON 27L BETWEEN BS 1139 - 1159 HAS A WEB CRACKED. FABRICATED & INSTALLED WEB IAW DWG ACA0259 & SRM 51-35-01 VOL 2.

Part: SKIN — DAMAGED (NR 4 SPOILER) · airframe 83,465 hrs · 34,675 cycles

RIGHT WING NR 4 SPOILER TOP SKIN DAMAGED. REPAIRED IAW SRM 57-00-01 FIG 4 SHEET 1.

Part: INTERCOSTAL — CRACKED (BS 1975) · airframe 83,465 hrs · 34,675 cycles

AFT CARGO AFT WASTE TANK AREA BS 197, L48 INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW IAW DWG AGA3225, HEAT TREATED IAW DWG AGA3225.

Part: FLOOR SUPPORT — CORRODED (BS 1701) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

CENTER CARGO BAY BS 1701 LBL 50 FLOOR SUPPORT CORRODED. FABRICATED NEW FLOOR SUPPORT IAW DWG AFA3865.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 83,465 hrs · 34,675 cycles

RIGHT WING NR 3 SPOILER PANEL TOP SURFACE DAMAGED. REPAIRED IAW SMR 57-00-01 FIG 4 SHEET 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

AFT CARGO COMPARTMENT STATION 1964, BILGE FRAME AFT SIDE RT L51 LOWER SHEAR CLIP EXFOLIATION CORROSION. FABRICATED SHEAR TIE IAW DWG AGA0022-65. HEAT TREATED SHEAR TIE IAW DPS 7.00-1. R & R CORRODED SHEAR TIE IAW DWG AGA0022.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

AFT FUSELAGE WASTE TANK AREA STATION 1986 BILGE CTR LINE AFT SIDE OF FRAME. SHEAR CLIP EXFOLIATION CORROSION. REMOVED SHEAR CLIP IAW SRM 51-31-01 VOL 2. REPLACED SHEAR TIE IAW DWG AGA3787. HEAT TREATED SPLICE ANGLE IAW DPS 7.00-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 83,465 hrs · 34,675 cycles

AFT FUSELAGE WASTE TANK AREA STATION 1975 BILGE CTR LINE SHEAR CLIP AFT SIDE OF FRAME EXFOLIATION CORROSION. REMOVED SHEAR CLIP IAW SRM 51-31-01 VOL 2. FABRICATED SHEAR TIE IAW DWG AGA3183. HEAT TREATED SHEAR TIE IAW DPS 7.00-1. REPLACED SHEAR TIE IAW DWG AGA3183.

Part: SKIN — DENTED (FUSELAGE) · airframe 83,465 hrs · 34,675 cycles

LOWER FUSELAGE LT 36 INCHES AFT OF OTBD PITOT STATIC TUBE BULGE IN SKIN, INTERNAL DENT. REPAIRED AREA IAW SRM 53-40-00 FIGURE 15 SHEET 4.

Part: SPAR CAP — CRACKED (LT WING) · airframe 83,465 hrs · 34,675 cycles

LEFT WING REAR SPAR LOWER CAP HAS A 3 INCHES VERTICAL CRACK AT STATION XORS 425 ADJACENT TO THE CTR FASTENER & THROUGH THE LOWER FASTENER OF THE VERTICAL FLANGE & TERMINATING JUST BEYOND THE RADIUS. CRACK REPAIRED PER EA 8-5710-T0309874. THE REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (LT WING) · airframe 83,239 hrs · 34,564 cycles

LEFT WING SLAT DRIVE MECHANISM DOOR INBD LE CRACKED TO RIVET. REMOVED PANEL 518DB FOR SHEET METAL ACCESS. REMOVED REQUIRED FASTENERS & TRIMMED OUT CRACK IAW SRM 51-30-00 VOL 2 & SRM 57-10-00 REPAIR. NEEDS HFEC FOR CRACK CONTAINMENT. FABRICATED FILLER PO 16433962 7075-T6 090 & DOUBLER PO 2111898 .063 6AL-4V TITANIUM. REPAIR DOUBLER & FILLER PLUG OK TO INSTALL. INSTALLED REPAIR IAW TEMP EA 8-5710-T0308209. COMPLIED WITH EA 8-5710-T0308209 WINGS & BASIC WING STRUCTURE & LT WING LE SKIN AT XOS 490 CRACKED. OK FOR CON'T SERVICE.

Part: FIRE WARNING — ILLUMINATED (NR 2 ENGINE) · airframe 82,059 hrs · 33,951 cycles

DURING TAXI IN TO RAMP, RECEIVED A FIRE INDICATION ON THE NR 2 ENGINE. PULLED THE FIRE HANDLE AND FIRED ONE BOTTLE AND INDICATION OF FIRE WENT AWAY. FIRE HANDLE DID NOT ILLUMINATE.

Part: BULKHEAD — CRACKED (BS 1521) · airframe 81,487 hrs · 33,626 cycles

INBD BULKHEAD CRACKED 29 INCHES FWD OF BS 1521 AND FOUR INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD AREA IAW SRM 53-00-01.

Part: VENT — OPEN (CARGO DOOR) · airframe 81,341 hrs · 33,549 cycles

LEVEL 2 ALERT "CARGO DOOR FWD B" "CARGO DOOR FWD A" AT BLOCKING FOUND FWD LOWER CARGO VENT DOOR OPEN, OPENED AND CLOSED FWD LOWER CARGO DOOR, DOOR OPERATED AND CLOSED NORMAL, REF AMM 52-31-00-0, ACFT OK FOR SERVICE.

Part: LATCH — BROKEN (MLG DOOR) · airframe 81,164 hrs · 33,440 cycles

AFTER TAKE OFF, RT MAIN GEAR WOULD NOT RETRACT. CONFIRMED BOTH ON PRIMARY AND SECONDARY INDICATIONS NO PROBLEMS OR UNSAFE INDICATIONS WITH GEAR DOWN AND LOCKED. AIRSPEED NEVER EXCEEDED 220 KIAS INSPECTED RT MLG, FOUND RT MLG DOOR LATCH ASSY BROKEN OFF DOOR CASTING. REMOVED AND REPLACED RT MLG DOOR IAW AMM 32-14-01-2 UP TO ITEM "7B". TRIMMED MLG DOOR FOR CLEARANCE REF MM32-14-01. ADJUSTED RT MLG DOOR CYLINDER PER MM 32-14-01-2 UP TO AND INCLUDING STEP 8(L). INSTALLED RIGHT MAIN GEAR DOOR LATCH ROLLER LINK AND ADJUSTED PER MM 32-34-03-2. CONTINUED ON WITH GEAR/DOOR RETRACTION CHECK PER MM 32-14-01-2 UP TO AND INCLUDING STEP 3D(15). OPS CHECKED RT MLG DOOR IAW 3D(14) A&B AND 16 THRU STEP 24 OPS CHECK GOOD AT THIS TIME AND ALL CHECKS AND CLEARANCES GOOD REF AMM 32-14-01-2,32-34-03-2-1,32-34-03-2, WORK INSTRUCTION WORK CARD PART 1 EO 8-5280-7-5000 AND ERS 12-06074.

Part: SUPPORT FITTING — CRACKED (BS 1501) · airframe 80,856 hrs · 33,265 cycles

RT MLG WHEEL WELL AFT OTBD CORNER, LOWER REINFORCING STRUCTURE HAS A CRACKED SUPPORT FITTING AT BS 1501. R & R CRACKED SUPPORT FITTING IAW SRM 51-31-01, FOUND STIFFENER CRACKED, REMOVED STIFFENER, FABRICATED AND INSTALLED STIFFENER IAW SRM 51-31-01, VO.I, FOUND CRACKED WEB ANGLE (RIB), REMOVED RIB AND FABRICATED NEW ANGLE (RIB)AND INSTALLED IAW SRM 51-31-01, VOL I, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — MISREPAIRED (BS 695) · airframe 80,856 hrs · 33,265 cycles

SKIN AT BS 695 S2L MISREPAIRED. REPAIRED IAW SRM 51-31-01, 53-20-00 AND 51-21-02.

Part: SKIN — MISREPAIRED (BS 960-1019) · airframe 80,856 hrs · 33,265 cycles

SKIN MISREPAIRED AT BS 960 TO 1019 L36 TO 41R. REPAIRED IAW SRM 53-20-00, FIG.6 VOL.I

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 80,856 hrs · 33,265 cycles

RT WING FLAP, OUTBD HINGE FITTING, HAS PITTING CORROSION. REMOVED CORROSION IAW CMM 57-44-09. FOUND TO BE WITHIN LIMITS IAW CMM 57-44-09.

Part: FRAME — CRACKED (BS 1159) · airframe 80,856 hrs · 33,265 cycles

FOUND BS 1159 FRAME LOWER LEG CRACKED THROUGH WIDTH OF THE FLANGE ON RT SIDE.

Part: BULKHEAD — CRACKED (LT MGL WW) · airframe 80,856 hrs · 33,265 cycles

LEFT MLG WHEEL WELL INBD BULKHEAD HAS 2 SMALL CRACKS TOWARDS THE TOP AT BS 1400 NEXT TO FLT RECORDER ACCELEROMETER. REMOVED CRACK IAW SRM 53-00-01, FIG.11, NDT CHECKED AND FOUND CRACK FREE, FABRICATED REPAIR PARTS IAW SRM 53-00-01, FIG.11 AND EA 8-5710-160678, INSTALLED ALL REPAIR DOUBLERS IAW SRM 53-00-01, APPLY PAINT IN REPAIR AREA IAW SRM 51-21-02, REAPPLIED CIC PER AMM 51-20-00-02, REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — MISREPAIRED (LT MLG WW) · airframe 80,856 hrs · 33,265 cycles

DURING REPAIR ASSESSMENT EVALUATION OF THE LT MAIN GEAR WHEEL WELL INBD BULKHEAD AFT UPPER SKIN. SUPPORT INTERCOSTAL FOR ACCUMLATOR WAS MISREPAIRED. REMOVED REPAIR ANGLE WITH NO EDGE DISTANCE IAW SRM 51-31-06. FABRICATED NEW REPAIR ANGLE IAW SRM 53-00-01. INSTALLED NEW REPAIR ANGLE IAW SRM 51-31-01. REINSTALLED ACCUMLATOR SUPPORT BRACKET IAW SRM 51-31-01. MAJOR REPAIR.

Part: ROLLER TRAY — GOUGED (CARGO BAY) · airframe 80,856 hrs · 33,265 cycles

FWD LOWER CARGO COMPT FS 959, BL 28L, ROLLER TRAY GOUGED GOING THROUGH TRAY. CHECKED LIMIT OF PREVIOUS REPAIR IN ROLLER TRAY AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 1A, FABRICATED REPAIR DOUBLER IAW SRM 53-00-02, FIG 4, VOL I AND INSTALLED IAW SRM 53-00-01. REPAIR CLASSIFIED AS MAJOR.

Part: SENSOR — FAILED (AIR MANIFOLD) · airframe 80,072 hrs · 32,853 cycles

AIR MANIFOLD 2 FAIL ENROUTE. REPLACED SENSING ELEMENT D1-49C.

Part: O-RING — CUT (HYD SYSTEM) · airframe 79,383 hrs · 32,454 cycles

HYD 3 ELEV OFF ALERT, HYD QUANTITY DECREASED AT 1GAL/30MIN HYD 3 QUANT LO AND HYD FAIL. ALTERNATE GEAR EXTENTION USED. UPON BLOCKED IN, HYD QUANTITY SHOWING :NR 1 = 7.1, NR 2 = 6.7 & NR 3 = 1.4 ; NR 3 RESERVOIR QTY POINTER SHOWING BELOW SERVICEABLE LEVEL. FOUND O-RING CUT AND PROTRUDING ON THE PRIMARY TRIM CONTROL VALVE. REPLACED O-RING IN REF TO AMM 27-43-03-4. LEAK AND OPS CHECKS GOOD. SERVICED HYDRO AND STOWED EMERGENCY GEAR EXTEND HANDLE. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: ROLLER — OUT OF ADJUST (RIGHT MLG) · airframe 78,609 hrs · 32,046 cycles

AFTER T/O ON GEAR RETRACTION WE HAD A UNSAFE RIGHT MAIN GEAR INDICATION. PUTTING GEAR DOWN, RECEIVED 3 GREEN INDICATION. ADJUSTED ROLLER LINK WITH REQUIRED WASHERS TO OBTAIN DESIREABLE END PLAY GAP, REF AMM 32-34-03-2.

Part: FRAME — CRACKED (BS 348 S28R) · airframe 78,454 hrs · 31,955 cycles

FUSELAGE - FWD AVIONICS COMPARTMENT STA 348 FRAME AT LONGERON 28 RT FOUND CRACKED. FUSELAGE - FWD AVIONICS COMPARTMENT STA 348, FRAME AT LONGERON 28 RT. R & R IAW SRM 51-31-01, VOL II, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 2007, 'X' = 28 AFT FUSELAGE FLOOR SUPPORT STRUCTURE FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 96. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING WSP0711, REVISION E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 110.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 78,454 hrs · 31,955 cycles

RT WING INBD FLAP INBD AFT SEGMENT UPPER SURFACE FOUND DENTED AT MID AREA. DENT AREA AT RIGHT HAND WING INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE MID SKIN AREA CARRIED OUT DOUBLER REPAIR AS PER SRM 57-10-00 FIGURE 85 VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 110.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 1907, 'X' = -25 AFT FUSELAGE FLOOR SUPPORT STRUCTURE FOUND WITH CRACKED. CABIN - STA 1907, 'X' = -25 AFT FUSELAGE FLOOR SUPPORT 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: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 1887, 'X' = -27.50 AFT FUSELAGE FLOOR SUPPORT STRUCTURE FOUND WITH CORROSION. CABIN - STA 1887, 'X' = -27.50 AFT FUSELAGE FLOOR SUPPORT 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: WEDGE — DENTED (ZONE 300) · airframe 78,454 hrs · 31,955 cycles

RT INBD ELEVATOR T/E WEDGE FOUND DENT. RIGHT HAND INBOARD ELEVATOR TRAILING EDGE WEDGE DENT MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 55-00-01 FIGURE 4 VOLUME I, REVISION 96. DEPTH = 0.089 INCH LENGTH = 1 INCH X 2 INCH. WEDGE REPAIRED AS PER SRM 55-30-00 FIGURE 2 VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 110.

Part: SKIN — CRACKED (ZONE 500) · airframe 78,454 hrs · 31,955 cycles

LT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CUT-OUT. EXTERIOR SKIN FOUND CRACKED. REPAIRED AS PER EA 8-5710-140445, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 110.

Part: SKIN — CRACKED (ZONE 600) · airframe 78,454 hrs · 31,955 cycles

RT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CUT-OUT. EXTERIOR SKIN FOUND CRACKED. RT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CRACKED CUT-OUT EXTERIOR SKIN REPAIRED IAW EA 8-5710-140444, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 78,454 hrs · 31,955 cycles

RT WING REFUELLING DOOR CUT OUT OTBD SUPPORT BEAM FOUND CRACKED. REPAIRED IAW EA 8-5710-140442, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (BS 1381) · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 1381, "X" = 8 SEAT TRACK LUG DAMAGED. DAMAGED SEAT TRACK TRIMMED OFF AND REMOVED IAW SRM 53-70-00, FIG 1 VOL I, REV 96. NEW SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-70-00, FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (BS 1381) · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 1381, "X" = -8 SEAT TRACK LUG DAMAGED. DAMAGED SEAT TRACK TRIMMED OFF AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I, REV 96. NEW SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-70-00, FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (BS 884) · airframe 78,454 hrs · 31,955 cycles

CABIN - STA 884, "X" = 47 (M884, AMJ POS 3L) SEAT TRACK ASSY LUG FOUND DAMAGED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01 VOL II, REV 96. NEW SEAT TRACK AT STA 766 TO STA 887, "X" = 47 FABRICATED AND INSTALLED IAW SRM 53-70-00, FIG 1 VOL I, REV 96. REPAIR CLASSIFIED IAW GMM 6-2-100, REV 110.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 78,454 hrs · 31,955 cycles

HFEC INSP CARRIED OUT, FOUND CRACK AT LT HORIZ STABILIZER UPPER OUTER REAR SPAR CAP AFT BARREL NUTS HOLE NR36, LENGTH APPROX 0.75 IN AND DEPTH APPROX 0.75 INCH FROM EDGE OF THE HOLE LOOKING FWD 12 O'CLOCK. CRACK REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOLUME II, REVISION 96. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 110.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 78,454 hrs · 31,955 cycles

CABIN: BETWEEN STA 740 AND STA 770, "X" = 47 SEAT TRACK LUG FOUND DAMAGED. SEAT TRACK REMOVED IAW SRM 51-31-01 VOLUME II, REV 96. NEW SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 78,454 hrs · 31,955 cycles

CABIN: STA 735, "X" = 8 SEAT TRACK LUG FOUND DAMAGED. TRIMMED OFF AND REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 96. NEW SEAT TRACK AND SPLICE FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 110.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 78,454 hrs · 31,955 cycles

CABIN: STA 755, "X" = -8 SEAT TRACK LUG FOUND DAMAGED. DAMAGED SEAT TRACK TRIMMED OFF AND REMOVED IAW SRM 53-70-00 FIGURE 1, VOLUME I, REV 96. NEW SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-70-00 FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — DAMAGED (BS 635) · airframe 78,454 hrs · 31,955 cycles

STA 635, "X" = 47 SEAT TRACK LUG FOUND DAMAGED. SEAT TRACK REMOVED IAW SRM 51-31-01, VOL II, REV 96. NEW SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-70-00 FIG 1, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: PUMP — CRACKED (NR 2 HYD SYS) · airframe 76,362 hrs · 30,939 cycles

HYD 2 FAIL LEVEL 2 ALERT DURING CRUISE. TEMP 117 C DEG, QTY -0-. BEFORE, WE HAD HYD 2 OFF LEVEL ONE ALERT, NORMAL QTY, WITH TEMP 112 C DEG, FOLLOWED QRH. TROUBLE SHOT AND FOUND LT EDP CASE CRACKED. REMOVED REPLACED LT & RT EDP DUE TO NR 2 HYD SYS LOST OF FLUID, REF AMM 29-11-01-2. ALSO REPLACED ALL ENGINE MANIFOLD HYD FILTERS, FOUND ALL FILTER CLEAN. SERVICED SYS NR 2 HYD AS REQ REF AMM 29-01-00. MOTOR ENGINE, LEAK AND OPS CHECKED OK REF JRH. CLOSED NR 2 ENGINE AMM REF 71-10-00.

Part: TIRE — FAILED (MLG) · airframe 73,721 hrs · 29,695 cycles

PDIS: NOTIFIED BY DEPT CONTROL TOWER AFTER T/O THAT PROBABLY HAD A TIRE FAILURE AT OR APPROACHING ROTATION. SLT VIBRATION FELT-LIKE FROM NOSE TIRES. GEAR RETRACTED NORMALLY. DUMPED-15K FUEL. RTN TO MEM, LDG 18C W/FLAPS 50. STOPPED ON RWY. FAILED TIRE RT TRK. FOUND NR 3 TIRE BLOWN. REMOVED AND REPLACED NR 3 TIRE PER MD10-10 AMM. REPAIRED DAMAGE.

Part: BOLT — SHEARED (NR 1 PYLON) · airframe 73,257 hrs · 29,482 cycles

NR 1 ENG PYLON FWD LOWER ATTACH FITTING/TOMBSTONE HAS 2 BOLTS PULLED, OUT/SHEARED AT 3:00 O`CLOCK AND 9:00 O`CLOCK POSTION. REMOVED LOWER PLUG PLATE AND 6EA. BOLTS IN REFERANCE TO MM 54-00-01-4. INSPECTED ALL 6EA BOLT HOLES AND FOUND NO CORROSION. INSTALLED 6 EA. NEW BOLTS, PLUG PLATE AND RETAINER IAW MM 54-00-01-4.

Part: CLIP — MISINSTALLED (THROTTLE CABLE) · airframe 71,718 hrs · 28,819 cycles

NO CONTROL OVER NR 1 ENGINE. NO THROTTLE RESPONSE. DURING TROUBLESHOOTING FOUND THAT THROTTLE ONLY BINDS AFTER THRUST REV LEVER HAS BEEN PULLED UP. FOUND THAT THE THROTTLE TURNBUCKLE BEHIND THE AFT AVI RACK IS GETTING HUNG UP IN CABLE RUN 121 (NOSE WHEEL STEERING) THE POPPING- NOISE THAT WAS REFERRED TO WAS THE CABLE SNAPPING BACK INTO PLACE. FOUND NR 1 THROTTLE TURNBUCKLE SAFETY CLIP NOT FULLY INSTALLED, CAUSING SAFETY CLIP TO GRAB STEERING CABLE WHEN THROTTLE WAS MOVED FWD. INSTALLED SAFETY CLIP PER MD10 SMP. INSPECTED CABLES NO DAMAGE NOTED. RAN NR 1 ENG PER MD10 JRH. ALL INDICATIONS NORMAL.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,265 hrs · 28,192 cycles

SKIN BULGING AT RIVETS, POSSIBLE CORROSION AND STRESS CRACK CORROSION. REMOVED FUSELAGE SKIN WITH CORRODED AREAS FROM FS 775-879 STR 50L-50R AND REPLACED WITH NEW SKIN PANEL PER SRM. PASSED LEAK CHECK TEST ON REPLACED AREA.

Part: SPAR CAP — DAMAGED (ZONE 600) · airframe 70,265 hrs · 28,192 cycles

A TEMPORARY REPAIR (PER S/B DC10-57A137) INSTALLED BY A PREVIOUS OPERATOR ON THE RT REAR SPAR LOWER CAP AT STATION XORS 417.00 REQUIRES REPLACEMENT. E.A. 8-5710-86514 PROVIDES INSTRUCTIONS FOR THE REPLACEMENT OF THE TEMPORARY WITH A PERMANENT REPAIR. THE PERMANENT REPAIR SPLICES IN A NEW SECTION OF LOWER SPAR CAP PER DRAWING SR10570019-7007. LAX (FEDEX) HEAVY MAINTENANCE IS ACCOMPLISHING EA (CLASSIFIED AS MAJOR REPAIR. COMPLIED WITH FEDEX W/C 57X1205 ALI-PT . 2, PT. 4, AND PT. 6. ACCOMPLISHED PERMANENT REPAIR AS PER EA 8-5710-86514 (SEQ #773).

Part: PROBE — MALFUNCTIONED (TAT) · airframe 68,949 hrs · 27,605 cycles

TAT PROBE HEAT ALERT AFTER TAKEOFF CB POPPED. RETURNED TO MEM. REMOVED AND REPLACED TAT PROBE IAW MD-10 AMM 34-16-02-2. OP CHECKS GOOD.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,413 hrs · 27,348 cycles

ORIGINAL NON-ROUTINE N00905 LOST. L3 DOOR HAS 2 EA FWD STOP FITTINGS CRACKED. GENERATED RFTS NR 396FE-2931081, REMOVED 1 EA CRACKED BEAM PN ADA 3752-1 REMOVED 10 EA STIFFENERS, DRILLED NEW BEAM PN 3752-1, INSTALLED NEW BEAM PN ADA3752-1, INSTALLED 10 EA STIFFENERS IAW SRM 51-35-01 VOL LL,D-DWG ADA 3752, VERIFIED CRACK ON 2ND BEAM, DYE PENETRATE: NO CRACK FOUND, ALODINED AND PRIMED IAW ASTME 1417-99 AND SRM 51-21-01 VOL LL.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROXIMATELY 5 OCLOCK POSITION 13 7/10 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED APPROX .014. REWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20-00, NO CRACKS FOUND. CHECKED LIMITS, FOUND WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -0.004, FOUND TO BE WITHIN LIMITS IAW MM 34-11-01-2. REF N/R N00224.

Part: ROLLER — WORN (ZONE 600) · airframe 68,413 hrs · 27,348 cycles

RT IB FLAP TRACK LOWER LOAD ROLLER WORN. REMOVED AND REPLACED LOWER LOAD ROLLER ON RT IB FLAP TRACK. INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H DUE 12-08-04. REF. N/R 00645

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROXIMATELY 8 O’CLOCK POSITION 17 1/2 INCHES FROM CENTER OF RIGHT HAND PRIMARY STATIC PORT, NEAR CARGO DOOR EDGE, THE SKIN IS DIMPLED OUT OF LIMITS. CHECKED LIMITS, LIMITS DEPTH WAS .012 INCHES, BLENDED GOUGE IAW DC10 SRM 53-00-01 VOL I. INSTALLED RIVET IAW DC10 SRM 53-20-00 VIL I, ALODINED AND PRIMED AREA OF SKIN IAW DC10 SRM 51-21- 01 VOL II. PERFORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -.001, FOUND TO BE WITHIN LIMITS IAW MD10 MM 34-11-01-2. DAMAGE LOCATED AT FS 880 AT LONGERON 42R. REF N/R N00226.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 68,413 hrs · 27,348 cycles

NR 3 PYLON RT FAN REVERSER TOP CRACKED AND GOUGED AT STATION Y172. REPAIRED THRUST REVERSER FAIRING IAW EA 8-7830-77612. REMOVED AND INSTALLED SKIRT PANEL IAW SRM 51-35-01 VOL II. REF N/R N00555.

Part: SKIN — CRACKED (ZONE 400) · airframe 68,413 hrs · 27,348 cycles

NR 2 PYLON AFT TRAILING EDGE WEDGE NEEDS TO BE RAN. REMOVED TRAILING EDGE ASSY AND SKIN ASSY IAW SRM 51-35-01 VOL II AND SRM 51-31-01 VOL II. FABRICATED NE TRAILING EDGE ASSY IAW DWG AVB7021, ASSEMBLED TRAILING EDGE IAW SRM 51-35-01 VOL II, INSTALLED TRAILING EDGE ASSY IAW SRM 51-35-02 VOL II, FABRICATED NEW SKIN IAW DWG AVB7091, INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II AND 51-31-01 VOL II. FOR ADDITIONAL WORK SEE N/R N01063, N00716, N01061, N01062, N00717, N01064 AND N01065. REF N/R N01024.

Part: PANEL — CORRODED (ZONE 500) · airframe 68,413 hrs · 27,348 cycles

CORROSION ON MATING SURFACE OF PANEL 541BB. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .032 INCHES, 7075-T6 IAW DRW NR ARC0267. MATERIAL THICKNESS AFTER BLEND OUT .020 INCHES, PART OUT OF LIMITS IAW DC10 SRM 57- 00-01 VOL I. RECIEVED NEW PANEL P/N ARC0267-503 IAW DAC DWG. DRW NR ARC0267. LOCATED, DRILL AND COUNTERSUNK FASTENER HOLES IAW SRM 51-31-01 VOL II. REF N/R N00123.

Part: ROLLER — WORN (TE FLAP TRACK) · airframe 68,413 hrs · 27,348 cycles

RIGHT HAND INBOARD FLAP MID TRACK ROLLER WORN. REMOVED AND REPLACED MID TRACK ROLLER ON RIGHT HAND INBOARD TRACK. INSTALLED AND TORQUED IAW FEDEX EA 8-5750-80957 TW 8381H DUE 12-08-04.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROXIMATELY 1 O`CLOCK POSITION, 15 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, THE SKIN IS DIMPLED. REWORKED DENT IAW DC 10 SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20- 00, NO CRACKS FOUND, DENT WITHIN LIMITS IAW MD 10-10 MM 34-11-01-2. PERFORMED INSPECTION OF NOTED DISCREPANT AREA. MEASUREMENT IS .004, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00229

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AFT LOWER CARGO, LOWER AFT CORNER OF DOOR CUT OUT, CLOSE OUT ANGLES CORRODED. REMOVED CORROSION IAW SRM 53-00-01 VOL I, FOUND TO BE OUT OF LIMITS. REMOVED ANGLES IAW SRM 51-31-01 VOL II PAGE 1. FABRICATED ANGLES IAW DAC DRG. AGA3881 AND AGA3857. LOCATED, DRILLED AND DEBURRED IAW SRM 51-31-01 VOL I PAGE 3. ALODINE AND PRIMED IAW MD 10- SRM 51-21-01 VOL II, PAGE 21. INSTALLED ANGLES IAW MD10 SRM 51-35-01 VOL II PAGE 1-3. REF N/R N00654.

Part: COUNTERWEIGHT — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,413 hrs · 27,348 cycles

LT OB AILERON BALANCE WEIGHTS, 5 EACH HAVE CORROSION AND CAD PLATING MISSING. REMOVED AND REPLACED WEIGHT ASSEMBLY IAW CMM 57051-07, SB 57919. REMOVED CORROSION FROM HOLE AND INSTALLED BUSHING IAW SB 57-117 AND CMM 57-51-02 AND EA 8-5750-77610. FLAP PEENED AND DYE PENETRANT INSPECTION OF HOLES IAW EA 8-5750-77610. REF N/R N00777.

Part: COUNTERWEIGHT — CORRODED (ZONE 600) · airframe 68,413 hrs · 27,348 cycles

RT WING TRAILING EDGE OB AILERON BALANCE WEIGHTS CORRODED AND 50 PERCENT OF PROTECTIVE PAINT IS MISSING. REMOVED AND REPLACED WEIGHT ASEMBLY IAW SB 57-119 AND CMM 57-51-02. REMOVED AND INSTALLED BUSHINGS IAW CMM 57-51-02, SB 57-119 AND EA 8-5750-77610. FLAP PEENED AND DYE PENETRANT INSPECT HOLES IAW EA 8-5750-77610. REF. N/R N00407

Part: ROLLER — WORN (ZONE 600) · airframe 68,413 hrs · 27,448 cycles

RT IB FLAP TRACK UPPER LOAD ROLLER WORN. REMOVED RT IB FLAP TRACK UPPER LOAD ROLLER AND REPLACED INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H, DUE 12-08-04. REF N/R N00646.

Part: SKIN — CHAFED (ZONE 600) · airframe 68,413 hrs · 27,348 cycles

RIGHT HAND WING LEADING EDGE SKIN HAS CHAFFING MARKS FROM NR 4, 5, 6 & 7 LEADING EDGE SLATS, ALSO TEFLON PAINT MISSING IN SOME AREAS. CHAFFING AREA IS BETWEEN STATION XOS 660 AND XOS 1005. BLENDED LEADING EDGE BEHIND SLAT NR 4 AND 7, FOUND TO BE OUT OF LIMITS AT XOS 600 AND XOS 594, IAW DC10 SRM 57-10-00 VOL I. FABRICATED DOUBLERS (2 EACH) IAW DC10 SRM 57-10-00 VOL I. ALODINED AND PRIMED DOUBLERS IAW DC10 SRM 51-21-01 VOL II. INSTALLED DOUBLERS IAW DC10 SRM 57-10-00 VOL I; DC10 SRM 51-33-01 VOL II AND DC10 SRM 51-35-01 VOL II. LEADING EDGE BEHIND SLATS 5 AND 6 WAS FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 VOL I.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

LOWER FORWARD CARGO DOOR CUTOUT AFT LOWER CORNER REPAIR TRIPLER DAMAGED. REMOVED TRIPLER REPAIR IAW MD10 SRM 51-33-01 PAGE 1 VOL I, FABRICATED NEW REPAIR TRIPLER IAW MD10 SRM 53-20-00 VOL I FIG 6 SHEET 5, ALODINE AND PRIMED IAW MD10 SRM 51-21-01 VOL II, PAGE 32. INSTALLED NEW TRIPLER IAW MD10 SRM 51-35-01 VOL II AND 51-33-01 VOL II. DAMAGE REPAIRED AT FS 959-990, LONGERON 38R TO 43R. REF N/R N00020.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROXIMATE 9 O’CLOCK POSITION 16 1/2 INCHES FROM RIGHT HAND PRIMARY STATIC, AT CARGO DOOR EDGE THE SKIN IS DAMAGED OUT OF LIMITS. POLISHED AREA, CHECKED LIMITS, FOUND TO BE WITHIN LIMITS .0042 IAW MD10 AMM 34-11-01-2. PERFORMED RVSM INSPECTION ON NOTED DISCREPANT AREA, MEASUREMENT IS .004, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2, REF N/R N00227.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROXIMATELY 11 0`CLOCK POSITION 14 4/5 INCHED FROM RIGHT HAND PRIMARY STATIC PORT, THE SKIN IS DIMPLED APPROXIMATELY .022 INCHES. REWORKED DENT IAW MD10 SRM 53-20-00 VOL I, PERFORMED HFEC IAW NDT MANUAL SPM 06-10-10 .001. NO CRACKS FOUND. DENT WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. PERFORMED RVSM INSPECTION OF THE NOTED DISCREPANT AREA, MEASUREMENT -0.001, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00228.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,413 hrs · 27,348 cycles

AT APPROX 7 O CLOCK POSITION 17.5 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED. APPROXIMATELY .060 INCHES. REWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED IAW NDT MANUAL 20-20-00, NO CRACKS FOUND, CHECKED LIMITS, WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED INSPECTION (RVSM) OF NOTED DISCREPANT AREA, READING -0.004, FOUND TO BE WITHIN LIMITS IAW MM 34-11- 10-2. REF. NR N00225.