N68051

Part: TARGET — SHEARED (RT MLG) · airframe 77,980 hrs · 35,047 cycles

AFTER GEAR WAS EXTENDED THE RT GEAR INDICATED UNSAFE ON BOTH PRIMARY NS SECONDARY SYSTEMS. ON LOW APPROACH TOWER OBSERVED GEAR APPEARED DOWN. COMPLIED WITH THE QRH & LANDED WITHOUT INCIDENT. UPON INSPECTION OF RT GEAR, FOUND TARGET SENSOR PLATE SHEARED FROM LANDING GEAR. INSTALLED TARGET ON RT TRUCK IAW AMM 32-61-15-4. PERFORMED ADJUSTMENT & TEST OF GEAR DOWN LOCK SENSORS IAW AMM 32-61-15-5, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SLIDE ARM) · airframe 77,393 hrs · 34,783 cycles

R1 DOOR DISARM LIGHT INOPERATIVE. REMOVED AND REPLACED R1 DISARMED INDICATOR LIGHT ASSY IAW AMM 20-30-08-2 AND SMP. OPS CHECKED NORMAL.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,244 hrs · 34,710 cycles

CAC AFT PRESSURE BULKHEAD ABOVE SYSTEM NR 2 DUCT HAS A APPROX 15 INCH CRACK. REPAIRED IAW EA 8-5310-T-0301508.

Part: SKIN — CRACKED (RT WING) · airframe 77,244 hrs · 34,710 cycles

RIGHT WING SKIN CRACKED, MIGRATING AT XORS 348 FWD OF INBD AILERON. REPAIRED IAW EA 8-5710-T0301500.

Part: SPAR — CRACKED (RT WING) · airframe 77,244 hrs · 34,710 cycles

RIGHT WING REAR LOWER SPAR HAS A CRACK AT XORS 402-452. REPAIRED IAW EA 8-5710-T03001500.

Part: CHARGER — INOPERATIVE (EMERGENCY POWER) · airframe 76,392 hrs · 34,261 cycles

BATTERY CHARGER INOPERATIVE MESSAGE DISPLAYED, EMERGENCY POWER TEST FAILED AS WELL. TROUBLESHOT IAW MM 24-30-00-0-2. BATTERY CHARGER FAILED. R & R BATTERY CHARGER UNIT IAW MM 24-30-00-0-2 & PERFORMED SATISFACTORY OPS CHECK. EMERGENCY POWER TEST SATISFACTORY IAW MM 24-30-00-5. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (ZONE 100) · airframe 76,029 hrs · 34,071 cycles

AFT UPPER CORNER OF NR 2 ACM EXHAUST CRACKED. REPAIRED CORNER ACM EXHAUST AS REQUIRED IAW SRM 53-20-00, FIG 2.

Part: STRUCTURE — CRACKED · airframe 76,029 hrs · 34,071 cycles

CRACK ON INBD SIDEWALL 30 INCHES FWD OF BS 1521 AND 20 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-157357.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 76,029 hrs · 34,071 cycles

LT MLG WW SIDEWALL CRACKED 20 INCHES AFT OF BS 1381 AND 7 INCHES DOWN AND A CRACK 17 INCHES AFT OF 1381 5.5 INCHES DOWN. REPAIRED CRACK REF EA 8-5310-157358, REV B.

Part: SKIN — CRACKED (ZONE 100) · airframe 76,029 hrs · 34,071 cycles

AFT UPPER CORNER OF NR 1 ACM EXHAUST CRACKED. INSTALLED DOUBLER AND TRIPLER ON AFT UPPER COUNER OF NR 1 ACM EXHAUST USING SRM 53-20-00 AS A REF.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 76,029 hrs · 34,071 cycles

LEFT FWD CORNER OF NOSE WW CRACKED. REPAIRED CRACK AND INSTALLED DOUBLERS IAW SRM VOL I 53-50-00, FIG 25.

Part: SPAR — DAMAGED (RT WING) · airframe 74,822 hrs · 33,462 cycles

WHILE ACCOMPLISHING EO 8-5710-7-5007, PT 2 MISDRILLED HOLE WHILE REMOVING FASTENERS. REPAIRED MISDRILLED HOLES BY REWORKING IAW EA 8-5710 -150976. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,822 hrs · 33,462 cycles

CTR CARGO FLOOR SUPPORT AT STA 1521 Y "0" HAS CORROSION. REMOVED ROLLER TRAY FOR ACCESS. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1B. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR PARTS IAW SRM 53-00-1 FIG 7, SHEET 3, INSTALLED ROLLER TRAY IAW SRM 51-31-01. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (BS 1964-1975) · airframe 74,822 hrs · 33,462 cycles

AFT CARGO BILGE AREA BETWEEN STA 1964 AND STA 1975 AND FROM LONGERON 48 - 47R INTERCOASTAL WEB HAS A CRACK. R & R INTERCOSTAL IAW SRM 51-31-01 AND REPAIRED PARTS. FABRICATED IAW SRM 53-16-01, REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 879-940) · corrosion level 2 · airframe 74,822 hrs · 33,462 cycles

UPPER CARGO SEAT TRACK 8R , F.S 879 TO 940, TRACK CORRODED BELOW LOBES BLENDED OUT CORROSION IAW SRM 53-70-00, FIG 5, MAT LOSS .023. OUT OF LIMITS. CUT OUT AND REPLACED DISCREPANT SECTION OF SEAT TRACK IAW SRM 53-70-01, FIG 1, SRM 51-31-01 .

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 74,822 hrs · 33,462 cycles

LT INBD FLAP LOWER SURFACE HAS MULTIPLE DENTS FROM INBD END TO OTBD END. DENT LOCATED 28" FROM L/E AND 82" FROM INBD EDGE, D= O.150", DIA= 10.0" FOUND OUT OF LIMITS IAW SRM 57-10-00, FIG. 48, REPAIRED AREA IAW SRM 57-10-00, FIG 4, REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 1901) · corrosion level 2 · airframe 74,822 hrs · 33,462 cycles

AFT CARGO FLOORBEAM AT STA 1901, LBL 40 TOP AND BOTTOM SURFACE HAS CORROSION. REMOVED CORROSION. ORIG MAT .063. MAT LOSS IS .031. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1B. FABRICATED FILLER AND REPAIR ANGLE. REPAIRED AFT CARGO FLOORBEAM IAW SRM 53-00-010 FIG. 8

Part: FLOORBEAM — CORRODED (BS 1901) · airframe 74,822 hrs · 33,462 cycles

AFT CARGO FLOORBEAM AT STA 1901, RBL 13 UPPER FLANGE HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE, REPAIR SPLICE AND REINSTALLED EXISTING STIFFNER IAW SRM 51-31-01, PARTS FABRICATED PER SRM 53-00-01, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 74,822 hrs · 33,462 cycles

CENTER WING LOWER SKIN BS 1368 (REAR SPAR AREA) CORRODED AT 2EA. LOCATIONS, 12" AND 36" OTBD OF LT KEELBEAM. REMOVED CORROSION ON CENTER WING LWR SKIN IAW EA 8-5710-152431.

Part: BUNGEE — FAILED (LT SPOILER) · airframe 72,873 hrs · 32,510 cycles

DURING T/O FELT LT TURNING TENDENCY THAT INCREASED WITH SPEED. (AFTER CLEAN UP). AP WOULD NOT HOLD LEVEL FLIGHT AND HAD APP 5 DEGREES (UNITS OF AILERON RUDDER TO HAVE CONTROL OF AC. RETURN TO DEPARTURE DUE TO MALFUNCTION. FOUND LT SPOILER MIXER 2-3 BUNGEE BROKEN. R & R CAM FOLLOWER SPRING ON 2 & 3 SPOILER LATERAL CONTROL MIXER IAW STANDARD MX PRACTICES. PERFORMED A LATERAL FLIGHT CONTROL FUNCTION/SYMMETRY CHECK IAW AMM 27-60-00-5 STEP 3D48 A-E; FOUND LATERALS FUNCTION NORMAL IN CLEAN WING AND TAKEOFF CONFIGURATION.

Part: SPRING — DAMAGED (SPOILERS) · airframe 72,560 hrs · 32,370 cycles

AT FL 340 APPROX 50 MIN INT FLT W/ PNEU SYS 2 MEL(ED) INOP (SYS CONFIGURED W/ 1-2 ISOL ON & NR 2 PACK & BLEED OFF) GOT AIR SYS 2 OFF FOLLOWED BY LVL 3 AIR MANF 2 FAIL. AIR MANF 2 FAIL SOON CLEARED BUT PNEU SYS 2 SCHEMATIC & OVERHEAD MANF LIGHT REMAINED RED EVEN AFTER SHUTDOWN. R & R CAM FOLLOWER SPRING ON 2&3 SPOILER LATERAL CONTROL MIXER IAW SRM. NO ADJUST OR CHANGES TO CABLE/PUSHROD RIGGING MADE TO FACILITATE REPAIR. PERFORMED VISUAL INSP OF SPOILER LATERAL CONTROL MIXER ASSY`S (2) & CONTROL SECTORS; NO FURTHER DISCREPANCIES NOTED. PERFORMED A LATERAL FLT CONTROL FUNCTION/SYMMETRY CHECK IAW AMM 27-60-00-5 STEP 3D48 A-E; LATERALS FUNCTIONED NORMAL IN CLEAN WING & TAKEOFF CONFIG.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 72,225 hrs · 32,230 cycles

FLAPS SETTINGS WERE 8,8/6,8. ROLL TENDENCY BEGAN AT APPROX 80 KTS AND ENDED AT LIFTOFF. INSPECTED DRIVE MECHANISM CABLES AND PULLIES IN CTR ACCY COMPARTMENT. PERFORMED A VISUAL INSP OF THE ALL SLAT CABLES, PULLIES, BRACKETS FOR BEING LOOSE OR DAMAGED. NO DEFECTS.

Part: DOUBLER — UNKNOWN (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

EXTERNAL FUSELAGE EXISTING EXTERNAL DOUBLER. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

UPPER MAIN CARGO DOOR FOUND DEEP INTERGRANULAR CORROSION ON TOP OF LOWER DOOR JAMB, UNDER SPOOL FITTING NR 6. ACCOMPLISHED EA NR 8-5310-111456.

Part: DOUBLER — UNKNOWN (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

EXISTING DOUBLER ON EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I.

Part: LONGERON — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

FWD CARGO COMPT BILGE ON LONGERON LT SIDE FOUND CRACKS. REPAIRED LONGERON IAW SRM 53-10-00 VOL 1 FIG 5 SHT 1.

Part: SKIN — UNKNOWN (ZONE 500) · airframe 68,734 hrs · 30,687 cycles

EXISTING REPAIR LT WING I/B FLAP LOWER SKIN. REPAIRED IAW SRM 57-00-01 VOL 1 FIG 1A SHT 2.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

EXISTING DOUBLER EXTERNAL SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1, SRM 51-00-01 VOL 1 AND DWG NCA6012.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.50" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL 1 FIG 10.

Part: BEAM — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

FWD CARGO COMPT ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.

Part: PANEL — CRACKED (ZONE 300) · airframe 68,734 hrs · 30,687 cycles

DURING INSPECTION OF UPPER INTERIOR SKIN PANELS OF STB HORIZONTAL SECTION FOUND 1 PANEL P/N 7207-1 WITH CRACK. ACCOMPLISHED EA NR 8-5510-96123.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 68,734 hrs · 30,687 cycles

CLG WHEEL WELL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL 1.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.75" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL1 FIG 10.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT TUNNEL ON SHEAR CLIP NR 2 CRACKS. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1.

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 68,734 hrs · 30,687 cycles

EXISTING SEAT TRACK SPLICE REPAIR MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-00 VOL 2 PAR 6.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CLG WHEEL WELL AREA CRACK 8.5" LONG ON VERTICAL BULKHEAD WEB. REPAIRED CRACK IAW SRM 53-00-01 FIG 10 VOL 1.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT BILGE ON "T" CAP ANGLE UNDER CHANNEL ON BLKHD FOUND CRACK 1" LONG. REPAIRED TEE IAW SRM 53-00-01 VOL 1 FIG 9 SHT 3.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT ON CHANNEL FOUND CORROSION. REPAIRED CHANNEL IAW SRM 53-70-00 VOL 1 FIG 7 SHT 5.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 68,734 hrs · 30,687 cycles

MAIN CABIN CRACK 1' LONG ON SEAT TRACK. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.

Part: BULKHEAD — CRACKED (ZONE 300) · airframe 68,734 hrs · 30,687 cycles

AFT FUSE COMPT FOUND 1 CRACK 1" LONG ON "T" VERTICAL ANGLE AFT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 9 VOL 1.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

MAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

EXISTING DOUBLER EXTERNAL SKIN. REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.

Part: SKIN — UNKNOWN (RT WING) · airframe 68,734 hrs · 30,687 cycles

EXISTING REPAIR RT WING O/B FLAP LOWER SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL 1.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 68,734 hrs · 30,687 cycles

CLG WHEEL WEEL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 3 VOL 1.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 68,734 hrs · 30,687 cycles

NLG W/W FOUND 1 CRACK .50" LONG ON RT SIDE VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-30-00 FIG 6 SHEET 4 VOL 1.

Part: WEB — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

COCKPIT CRACK .25" LONG ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 VOL 1 FIG 4 SHT 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

MAIN CABIN ON SEAT TRACK FOUND 1 SEVERE CORROSION WITH EXFOLIATION AND 6 ELONGATED HOLES, DISCREPANCY FOUND DURING ACF MODIFICATION. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 68,734 hrs · 30,687 cycles

NLG W/W FOUND 6 CRACKS ON RT SIDE VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-40-00 FIG 34 VOL 1.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 68,734 hrs · 30,687 cycles

AFT FUSE ATTIC ZONE FOUND 1 CRACK ON SHEAR TIE UPPER VERTICAL BULKHEAD LT SIDE. REPAIRED IAW SRM 53-30-00 FIG 2B VOL 1.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 68,734 hrs · 30,687 cycles

CLG WHEEL WELL AREA CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

CTR CARGO COMPT BILGE ON CAP ANGLE FOUND MODERATE CORROSION WITH EXFOLIATION. REPAIRED CAP IAW SRM 53-30-00 VOL 1 FIG 8.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

COCKPIT CORROSION WITH EXFOLIATION ON MEMBRANE AND 1 CRACK.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 68,734 hrs · 30,687 cycles

RT WING LWR SURFACE FOUND DEEP NICKS ON INT SKIN OF SLAT NR 2. TRIMMED OUT DAMAGED PORTION INT SKIN. INSTALLED FILLER AND REPAIRED DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,734 hrs · 30,687 cycles

LT DETACHABLE UPPER SKIN FOUND 1 CRACK AND 10 RIVETS LOOSE RIVETS. REPAIRED SKIN IAW SRM 55-10-00 VOL 1 FIG 8 AND REPLACED FASTENERS IAW SRM 51-35-02 VOL 2 PAR 12-10.

Part: MEMBRANE — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,734 hrs · 30,687 cycles

COCKPIT CORROSION CON EXFOLIATION ON MEMBRANE, AND 1 CRACK.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 68,734 hrs · 30,687 cycles

AFT FUSE COMPT FOUND 1 CRACK ON HORIZONTAL WEB AFT SIDE VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 VOL 1 FIG 10.

Part: INSULATION — BURNED (ZONE 100) · airframe 67,186 hrs · 29,830 cycles

IN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERELY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC DUCT. REPLACED INSULATION BLANKETS PER REF: MM 25-28-00. NEED LEAK CHECK 97846. LEAK CHECKED #1 SYSTEM PNEUMATIC DUCT AT CAC, LT SIDE PER MM 36-14-02-1-1 . MX KM-97620 QC 97349

Part: PITOT TUBE — OBSTRUCTED (FIRST OFFICERS) · airframe 66,885 hrs · 29,689 cycles

REJECTED T/O 5L IND DUE TO ZERO AIRSPEED INDICATION IN F/O INDICATOR TEMP 24 DEG, WT=420,000, AIRSPEED AT REJECT=100KTS, RNWY 57 (FULL LENGHT), BRAKE COOLING TIME=64 MINS, TIME OF REJECT=21:59Z. FOUND F/O'S PITOT TUBE OBSTRUCTED. CLEARED OBSTRUCTION AND PURGED F/O'S PITOT SYSTEM AND PERFORMED LOW LEVEL PITOT STATIC SYSTEM CHECK F/O'S AIRSPEED INDICATOR, OPS CHECKS NORMAL.

Part: SPAR — CRACKED (LT WING) · airframe 65,522 hrs · 28,981 cycles

FUEL LEAK LT WING REAR SPAR AREA AT XORS STATION 346 LOWER CHORD ANGLE. INSPECTED AREA WITH HFEC AND DETECTED A CRACK INDICATION ALONG HORIZONTAL FLANGE INTO RADIUS AND UP VERTICAL FLANGE. TOTAL LENGTH OF CRACK IS APPROXIMATELY 4.650 INCH.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 65,466 hrs · 28,949 cycles

AFTER T/O AT 800 FT, HAD FLAP DISAGREE LIGHT ILLUMINATE . RUN RED TABS AND THE LIGHT DID NOT GO OUT. DUMPED APPROX. 20K OF FUEL. FLAPS EXTENDED THE LIGHT GOES OUT. THERE WERE NO ABNORMAL FLT CHARACTERISTICS WITH FLAPS CYCLING OR EXTENDED. T/S PER TAFI 27-50-00 H-VOLTAGE CHECKS AT TERMINALS S3-12 AND S3-43 ARE NORMAL, TAFI POINTS AT FLAP POS. INDICATOR. MEL: A/C RELEASED FOR SERVICE PER MEL/CDL: 27-06-01 CATEGORY: C EXPIRATION: 24SEP04 MEL 27-06-01: INBD FLAP DISAGREE FLAG - INOP. VERIFY AND RECORD IN AML/EAML FLAP OPERATION AND SYMMETRY PRIOR TO EACH DEPARTURE.

Part: PANEL — DAMAGED (ZONE 400) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5410-78219, PYLON HORIZONTAL ENGINE PYLON LT ACCESS PANEL REPAIR. COMPLIED WITH EA 8-5410-78219.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

FLOOR PANEL SUPPORT CORRODED LWR FWD PIT FS 819 RIGHT SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 AND SRM 51-35-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

AFT FUSE LEFT SIDE BANANA PANEL HAS CORROSION. REMOVED AND REPLACED PANEL IAW SRM 51-31-01.

Part: BRACKET — CORRODED (ZONE 500) · airframe 65,001 hrs · 28,730 cycles

LEFT I/B FLAP IDLER ARM ATTACH FITTING IS CORRODED. REMOVED BUSHINGS FOR ACCESS IAW M/M 20-20-07, REMOVED CORROSION BY REAMING TO 1.079, OUT OF LIMITS IAW DWG ARC2761. REMOVED AND REPLACED FITTING IAW SRM 51-35-01 AND 51-31-01. LOCATED AND DRILLED 4EA MOUNT HOLES IAW DWG ARC2761. REAMED TO 378. PAINTED FITTING IAW SRM 51-21-02.

Part: RETAINER — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

AFT CARGO COMPT DOOR SILL DOOR SEAL RETAINER AFT LWR CORNER AFT SIDE CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-35-01, SRM 51-41-01, SRM 51-33-01.

Part: RIB — GOUGED (SLAT) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN LEADING EDGE SLAT RIB ARB1092-1. COMPLIED WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN WING LEADING EDGE SLAT RIB ARB1092-1.

Part: CHANNEL — ELONGATED (VERTICAL STAB) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5530-78221 STABILIZERS VERTICAL. RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC7265-2. COMPLIED WITH EA 8-5530-78221 STABILIZERS VERTICAL RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC 7265-2.

Part: RIB — GOUGED (NR 1 SLAT TRACK) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. COMPLIED WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-78220A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR. COMPLIED WITH EA 8-5750-78220 A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR.

Part: PULLEY BRACKET — DAMAGED (RUDDER) · airframe 65,001 hrs · 28,730 cycles

RUDDER CABLE QUADRANT INSIDE ACCESS PNL 364BR UPPER AND LOWER ARMS GUIDE PIN HOLES ELONGATED AND PINS FALLING OUT/MISSING. REMOVED AND REPLACED PULLEY BRACKET AND PULLEY IAW MM 20-50-02-2, CHECKED TENSIONS IAW MM 27-20-00-5 AND MM 27-20-00-6 AT MAE.

Part: RUB STRIP — WORN (NR 2 COWLING) · airframe 65,001 hrs · 28,730 cycles

NR 2 ENG RIGHT FAN COWL AFT EDGE RUB SEAL WORN. REMOVED AND REPLACED RUB SEAL STRIP IAW SRM 51-31-01 AT MAE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

AFT CARGO COMPT DOOR SILL FLOOR BOARD SUPPORT IS CORRODED STA 1801 TO 1841. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-01 AND SRM 51-35-01 AT MAE.

Part: STATIC PORT — OUT OF TOLERANCE (PITOT/STATIC SYS) · airframe 65,001 hrs · 28,730 cycles

RT PRIMARY STATIC PORT FAILED THE CONVEXITY AND CONCAVITY CHECK ALONG PLANE LINE-A. REMOVED AND REPLACED RT STATIC PORT PRIMARY IAW MM 34-11-02 AT MAE.

Part: RUB STRIP — WORN (NR 3 COWLING) · airframe 65,001 hrs · 28,730 cycles

NR 3 ENG LT CORE COWL FWD RUB STRIP WORN. REMOVED AND REPLACED RUBSTRIP IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE.

Part: STRUCTURE — CRACKED (RT ELEVATOR) · airframe 65,001 hrs · 28,730 cycles

RIGHT ELEVATOR DROOP T/E OUTBOARD T/E CORNER IS CRACKED. REMOVED AND REPLACED T/E SECTION IAW SRM 51-35-01 AT MAE.

Part: RUB STRIP — DAMAGED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

RIGHT INBOARD FLAP OUTBOARD HINGE FITTING FWD FAIRING CHAFE STRIP IS DAMAGED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-31-01 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINER UNIT IS CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINER UNIT CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINERS UNIT IS CRACKED 2EA STA 1600 TO 1681. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

RETAINER BALL UNIT CRACKED STA 635-695. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

RETAINER BALL UNIT IS CRACKED STA 610 TO 635. REMOVED AND REPLACED RETAINER STA 610 TO 635 IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE.

Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL MAT IS DAMAGED AT STA 615 TO 775 MCD. REMOVED AND REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINER UNIT CRACKED STA 615 TO 635 13 EA. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 65,001 hrs · 28,730 cycles

RIGHT MLG W/W AFT O/B WEB VERT STIFFENER UPPER END BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINER UNIT CRACKED STA 699-745. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: CLIP — BROKEN (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

MCD, RT VENT PNL FAIRING CLIPS BROKEN AT STA 615. REMOVED AND REPLACED BROKEN CLIPS IAW SRM 51-21-02 AT BFM/MAE.

Part: LOCK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

TWO EA 80464-10 LOCK ASSY CORRODED. REMOVED AND REPLACED LOCK ASSY IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

RETAINER BALL UNIT CRACKED STA 615-675. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE.

Part: PANEL — DAMAGED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5740-77422 WINGS - INBOARD FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY. COMPLIED WITH EA 8-5740-77422 WINGS - FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

RETAINER BALL UNIT CRACKED STA 745-785. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

CONVEYOR ASSY ON BOTTOM SIDE CORRODED. REPLACED CONVEYOR IAW ANCRA MM 25-50-33 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINER UNIT CRACKED STA 1501. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

MCD FLOOR SUPPORT CORRODED AT FS 1300 LBL 80. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-31-01 AT MAE.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 65,001 hrs · 28,730 cycles

BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE.

Part: FITTING — DAMAGED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK. COMPLIED WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK AT MAE.

Part: PLATE — GOUGED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO DOOR CUTOUT FWD JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-21-02 AT MAE.

Part: CLIP — BROKEN (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT OUTBOARD FLAP, INBOARD WING MOUNTED HINGE, FWD OUTBOARD FAIRING SUPPORT STR CLIP BROKEN. REMOVED AND REPLACED CLIP RIGHT OUTBOARD INBOARD HINGE FWD OUTBOARD FAIRING SUPPORT IAW SRM 51-31-01, 51-25-01, DPS 3.69 REV E DWG ARC0744 2020T- 3 .071.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 65,001 hrs · 28,730 cycles

RIGHT MLG W/W AFT WEB FWD BULB SEAL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED ANGLE SUPPORT AND WEB IAW SRM 51-35-01 AT MAE.

Part: PRESSURE BLKHD — CORRODED (LT MLG WW) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

LEFT MLG W/W AFT BULKHEAD IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD SKIN PANEL IAW SRM 51-31-01 AT MAE.

Part: FLAP TRACK — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

LEFT I/B FLAP TRACK MOUNT HOLES CORRODED. REMOVED AND REPLACED FLAP TRACK IAW CMM 57-52-01 AT MAE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO SEAT TRACK IS CORRODED AROUND FLOOR BOARD FASTENER HOLES STA 1219 RBL 74-86. REMOVED AND REPLACED SECTION OF SEAT TRACK AND SPLICES IAW SRM 53-20-00-01 AT MAE.

Part: PLATE — GOUGED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO DOOR CUTOUT AFT JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE.

Part: RETAINER — WORN (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT O/B FLAP, O/B WING MOUNTED HINGE, AFT O/B BULB SEAL RETAINER ON BULLET FAIRING ARE WORN. FAB NEW RETAINER ON MAE TRAVLER T4/434038, INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2.

Part: PLATE — GOUGED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO DOOR CUTOUT AFT JAMB HAS A GOUGED SCUFF PLATE. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE.

Part: RETAINER — DAMAGED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT O/B FLAP O/B WING MOUNTED HINGE, AFT I/B BULB SEAL RETAINER ARE DAMAGED ON BULLET FAIRING. FAB NEW RETAINER ON MAE TRAVLER T4/433934. INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2.

Part: STOP FITTING — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-77430 WINGS - OUTBOARD FLAP INBOARD UP-STOP FITTING CORROSION REWORK, LEFT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-77430.

Part: RIB — WORN (RT WING) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5710-77424 WINGS - REWORK OF RIGHT NR 7 SLAT TRACK OUTBOARD RIB ARB1868. COMPLIED WITH EA 8-5710-77434.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 537AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL. REMOVED AND REPLACED IAW SRM 51-31-01AT MAE.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 538BB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE.

Part: CLIP — CRACKED (RT WING) · airframe 65,001 hrs · 28,730 cycles

TWO CLIPS CRACKED INSIDE NR 3 FUEL TANK PLATE 634AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE.

Part: RUB STRIP — GOUGED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638BB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED FOR PANEL 538AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 536CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

C/W 8-5710-77408, WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR, P/N ARB3799-2. COMPLIED WITH EA 8-5710-77408 WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR P/N 3799-2 AT MAE.

Part: RUB STRIP — GOUGED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638AB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE.

Part: CLIP — CRACKED (LT FUEL TANK) · airframe 65,001 hrs · 28,730 cycles

TWO CLIPS CRACKED INSIDE FUEL TANK PLATE 534AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5740-77420 WING - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0154-2). COMPLIED WITH EA 8-5740-77420 LEFT INBOARD FLAP - O/B HINGE BRACKET CORROSION REPAIR (P/N ARC 0154-2) FABRICATED BUSHING ON TRAV 432592 AT MAE.

Part: RUB STRIP — GOUGED (LT WING) · airframe 65,001 hrs · 28,730 cycles

LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 533AT. REMOVED AND REPLACED RUB STRIP IAW SRM 51-31-01AT MAE.

Part: GUIDE — CRACKED (THRUST REVERSER) · airframe 65,001 hrs · 28,730 cycles

NR 2 ENGINE RIGHT REVERSER LWR FWD T-TRACK GUIDE CRACKED LWR ATTACHMENT. REMOVED AND REPLACED BRACKET IAW SRM 51-35-01.

Part: RUB STRIP — GOUGED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 636CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-42-04 AT MAE.

Part: HINGE — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5740-77431 WINGS-RT OB FLAP, OUTBD HINGE ASSY P/N ARC0503 PIVOT BORE REWORK. COMPLIED WITH EA 8-5740-77431 WINGS-RT OB FLAP, OB HINGE ASSY P/N ARC0503 PIVOT BORE REWORK AT MAE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR, P/N A NB7393-501. COMPLIED WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR P/N ANB7393-501 AT MAE.

Part: RUB STRIP — GOUGED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 637AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-42-04 AT MAE.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5740-77418 WINGS RT INBD FLAP, FWD HINGE ASSY PIVOT BORE CORROSION. COMPLIED WITH EA NR 8-5740-77418 WINGS-LT IB FLAP, FWD HINGE ASSY PIVOT BORE CORROSION, PART 1 ONLY. COMPLIED WITH AS STATED IN UPDATE.

Part: FITTING — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-77424 WINGS LT IB FLAP-OB HINGE BRACKET SIDE BRACE REPAIR (P/N ARC0182-1) COMPLIED WITH EA 8-5750-77424 (WINGS-LT IB FLAP- OB HINGE BRACKET SIDE BRACE REPAIR (PN ARC 018 2-1) AT MAE.

Part: FITTING — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-77425 WINGS-LT IB FLAP, ROLLER FITTING ATTACH HOLES CORRODED AT MAE(PART 1 INTIAL IS COMPLIED WITH AND WILL REQUIRE A FOLLOW UP ACTION TO BE COMPLIED WITH. COMPLIED WITH AS STATED IN UPDATE.

Part: MOUNT BRACKET — BENT (COCKPIT) · airframe 65,001 hrs · 28,730 cycles

CAPTAINS ESCAPE ROPE MOUNT BRACKET IS BENT. CLOSING ACTION ON 05/25/04 ON N/R N00025. REMOVED AND REPLACED CAPTAINS ESCAPE ROPE MOUNT BRACKET IAW SRM 51-31-01.

Part: PANEL — WORN (NACELLE) · airframe 65,001 hrs · 28,730 cycles

PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01.

Part: SUPPORT — CHAFED (NR 3 PYLON) · airframe 65,001 hrs · 28,730 cycles

ENGINE NR 3 THROTTLE CABLE PYLON SUPPORT IS CHAFING AGAINST THE ENGINE CASING. REMOVED AND REPLACED CABLE SUPPORT GUIDE P/N AUH7030-1 IAW SRM 51-33-01.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 65,001 hrs · 28,730 cycles

RIGHT WING L/E LOWER L/E SUPPORT BRACKET IS CRACKED AT IT'S AFT END RT WS XORS 835. REMOVED AND REPLACED RT WING L/E SUPPORT BRACKET AT WS XORS 835 INBOARD OF SLAT TRACK 15 IAW SRM 51-31-01 AND SRM 51-35-01.

Part: PANEL — WORN (NACELLE) · airframe 65,001 hrs · 28,730 cycles

PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01.

Part: HINGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-77414, WING - OUTBOARD FLAP, REWORK OF POSITION INDICATION HOLE IN ARC1991 HINGE. COMPLIED WITH EA 8-5750-77414.

Part: HINGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5750-77413 WING - RT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-77412.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

COMPLY WITH EA 8-5310-77410 FUSELAGE MAIN FRAME - MINOR DEVIATION TO SRM SEAT TRACK SPLICE. COMPLIED WITH EA 8-5310-77410.

Part: HINGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. COMPLIED WITH EA 8-5750-77415, WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE.

Part: BRACKET — CHAFED (THRUST REVERSER) · airframe 65,001 hrs · 28,730 cycles

NR 3 ENG O/B TR FEED BACK YOKE BRACKET CHAFED. REMOVED AND REPLACED FEEDBACK YOKE IAW SRM 51-31-01 AT MAE.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

LEFT O/B FLAP BOTH I/B AND O/B ROLLER CARRIAGES HAVE WORN AREAS AND CORROSION. REPLACED CARRIAGES ON W/C E 8- 5750-7-5000 PT 3 AT MAE.

Part: DAMPENER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

LWR FWD CARGO DOOR COUNTER BALANCE DAMPENER IS CORRODED. REMOVED AND REPLACED COUNTER BALANCE DAMPENER IAW MM 52-31-07-2 AT MAE.

Part: BRACKET — CHAFED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

RIGHT I/B SIDE LOAD ROLLER BRACKET IS WORN/CHAFED. REPLACED BRACKET ON W/C E8-5750-75002 PT 2 AT MAE.

Part: HEAT EXCHANGER — CRACKED (A/C BAY) · airframe 65,001 hrs · 28,730 cycles

NR 3 HEAT EXCHANGER HAS CRACK ON INSIDE. REPLACED HEAT EXCHANGER IAW MM 21-53-01-2 AT MAE.

Part: FITTING — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

LEFT I/B FLAP SIDE LOAD ROLLER FITTING HAS CORROSION IN BORES AND IS CHAFED. REPLACED FITTING ON W/C E8-5750-7-5002 PT 1 AT MAE.

Part: DRIVE ASSY — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

RIGHT I/B FLAP DRIVE ARM I/B BEARING FACE IS PITTED. REPLACED DRIVE ARM ON WC E8-5750-7-5002 PT 2 AT MAE.

Part: MOUNT — CORRODED (T/E FLAP) · corrosion level 2 · airframe 65,001 hrs · 28,730 cycles

RIGHT I/B FLAP SIDE LOAD ROLLER FITTING MOUNT IS CORRODED. REPLACED ASSY ON WC E 8-5750-7- 5002 AT MAE.

Part: SPINDLE — WORN (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

LEFT O/B FLAP I/B ROLLER SPINDLE IS WORN AND IS CORRODED. REMOVED AND REPLACED SPINDLE ON W/C E 8-5750-7-5000 PT 3.

Part: STOP FITTING — WORN (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

LEFT WING O/B FLAP O/B STOP WORN AND MISSING. REMOVED AND REPLACED STOP AT MAE.

Part: HINGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

C/W EA8-5740-77406, RIGHT INBOARD FLAP, AFT HINGE ASSY ARC 2512, PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77406 RIGHT INBOARD FLAP, AFT HINGE ASSY, PIVOT BORE CORROSION CW PT1 ONLY.

Part: STOP — GOUGED (ZONE 500) · airframe 65,001 hrs · 28,730 cycles

LT WING O/B FLAP, O/B FLAP TRACK STOP GOUGED. REMOVED AND REPLACED TRACK STOP IAW MM 20-50-02-2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CABIN SEAT TRACK LBL 27 FS 1119 IS CRACKED. REPLACED SEAT TRACK IAW SRM 53-70-00 AT MAE.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO DECK SEAT TRACK GOUGED AT LBL 47.25 FS 1740. REMOVED AND REPLACED DAMAGED TRACK AT FS 1740 LBL 47.25 IAW SRM 53-70-00 FIG 1 & 51-31-01 AT MAE.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

RIGHT O/B FLAP BOTH I/B AND O/B CARRIAGES HAVE CORROSION IN ROLLER MOUNT HOLES. REPLACED I/B AND O/B ROLLER CARRIAGES TO BE INSTALLED ON EO 8-5750-7-5000 AT MAE.

Part: ROD — DAMAGED (THRUST REVERSER) · airframe 65,001 hrs · 28,730 cycles

ENGINE NR 3 OUTBOARD T/R HOLD OPEN ROD SAFETY PIN IS ELONGATED. REMOVED AND REPLACED ENGINE NR 3 RT T/R HOLD OPEN ROD IAW SRM 51-31-01 AT MAE.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 65,001 hrs · 28,730 cycles

STA 1450 RIGHT MAIN LANDING GEAR W/W AFT OUTBOARD WEB VERTICAL STIFFENER LOWER END CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01 AT MAE.

Part: THRU BOLT — WORN (TAIL CONE) · airframe 65,001 hrs · 28,730 cycles

TAIL CONE RIGHT HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED TAIL CONE RIGHT HINGE THRU BOLT IAW MM 53-52-00-2 AT MAE.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CABIN RIGHT UPPER GILLINER SUPPORT BRACKETS ATTACHED TO FRAMES FS 635 AND 655 ARE BROKEN. REMOVED AND REPLACED CLIPS AT STA 635 AND 655 IAW SRM 51-35-01, FABBED FROM 2024-T3 .063C BATCH 702499 DRWG D10-25-073 AT MAE.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 65,001 hrs · 28,730 cycles

MAIN CARGO DECK SEAT TRACK GOUGED AT STATION 820 TO 970 LBL 47.25. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AT MAE.

Part: WINDOW — SCRATCHED (CABIN) · airframe 65,001 hrs · 28,730 cycles

SIDE OF FUSELAGE FWD OF RIGHT WING FWD WINDOW HAS SCRATCHES. REMOVED AND REPLACED RT CABIN WINDOW FWD OF WING IAW MM 56-20-00-2 AT MAE.

Part: SPINDLE — CORRODED (T/E FLAP) · airframe 65,001 hrs · 28,730 cycles

RIGHT O/B FLAP I/B ROLLER SPINDLE WORN AND HAS CORROSION. REMOVED AND REPLACED SPINDLE IAW W/C E 8-5750-7-5000 AT MAE.

Part: CONTROL CABLE — STUCK (NR 2 THROTTLE) · airframe 64,900 hrs · 28,691 cycles

NR 2 THROTTLES STUCK AT 91 PERCENT N1 FL310 SHUTDOWN ENGINE AT 6000 HIGH THROTTLE BROKE FREE ON TAXI IN. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE IN REF TO DC10 MM 76-11-01-2 RIG CHECKED GOOD. INSTALLED ALL SCREWS ON NR 2 ENGINE ACCESS PANELS, CLOSED WORK PLATFORM, AND PERFORMED AN ENGINE RUN FOR 5 MINUTES. MOVED THROTTLE TO BREAKAWAY THRUST AND THROTTLE MOVEMENT WAS SMOOTH AND RESPONDED WELL. ACFT OK FOR SERVICE.

Part: MOTOR — FAILED (R1 DOOR) · airframe 62,070 hrs · 27,579 cycles

R-1 DOOR PNEU DRIVE MOTOR FAILED EMERGENCY ACTUATION TEST (SPLINE SHAFT SEPARATED FROM MOTOR).

Part: ENGINE — MALFUNCTIONED (NR 2)

VIBRATION NOTED INCREASED WITH POWER CHG ON ENG NR 2. POWER REDUCED TO IDLE AND AC RETURN TO MEM. SWAPPED AC PACKS WITH NO CHG IN VIBRATION ALL ENG AND HYD IND NORM. *S/D* REMOVED AND REPLACED NR 2 ENG IAW W/C 71T1101 & 71T1701. NR 2 ENG GROUND CKS NORMAL.

Part: RETRACT MECH — MALFUNCTION (TE FLAPS)

AFTER T/O FROM PHX AND FLAPS SELECTED UP, FLAPS STOP RED AT 100. FLAPS SELECTED TO 150 AND AFTER ABOUT TWO MINUTES, THE FLAPS WENT DOWN TO 150. FUEL WAS DUMPED TO LANDING WEIGHT AND A 500 FLAP LANDING WAS MADE AT PHX. FLAPS OPERATED NORMALLY TO 300 AFTER 150 FLAPS WERE REACHED. PERFORMED INSPECTION OF LEFT AND RIGHT FLAP AREAS. RAN FLAPS SEVERAL TIMES WITH NO FAULTS. FLAP HANDLE AND INDICATION TAPE RAN TOGETHER. CHECKED INDICATION AS PER TAFI 27-50-00 PG 110.

Part: SPAR CAP — CRACKED (LT HORIZ STAB)

LT HORIZONTAL STABILIZER, UPPER FWD SPAR CAP AFT TANG HAS CRACK INDICATION IN FASTENER HOLE AT EXISTING FILLER LOCATION, THAT BEING THE O/B FASTENER. REPAIRED CRACK IN REFERENCE TO SRM 55-20-00 FIG 9 AND 10, PER EA 8-5510-27035A.

Part: SKIN — CRACKED (LT STAB)

CRACK INDICATION ON LT STAB L/E AT UPPER FWD TANG. CRACK EXTENDS ITSELF ACROSS FASTENER HOLE APPROX 1.25 INCH IN LENGTH. CRACK LOCATION IS 5 INCHES I/B OF CLOSURE RIB AREA. REPAIRED CRACK IN REF TO SRM 55-20-00 FIG 9 AND 10. ALSO, PER EA 8-5510-21035A.

Part: SPAR CAP — CRACKED (HORIZ STAB)

CRACK IN HORIZONTAL STABILIZER OUTER RT SECTION, UPPER AFT SPAR CAP AFT BARREL NUT HOLE ADJACENT TO OPERATING BULKHEAD. CRACK MEASURES .3125 INCH INTO HOLE AND THEN PROGRESSES FWD .3750 INCH LONG. CRACK WAS REWORKED PER AN ELLIPTICAL SHAPE AND CALCULATED, AREA EQUALS .387 SQ PER S/B A55118 A MAXIMUM OF .92 IS ALLOWED.

Part: ANGLE — CORROSION (WING CENTER SECT)

L/LT WW FWD BULKHEAD TOP OF WING CENTER BOX SECTION, REMOVABLE PANEL HAS HEAVY CORROSION, APPROX 10 INCHES O/B OF VERTICAL KEEL BEAM WEB. REMOVED CORRODED ANGLE, CLEANED, TREATED AND PRIMED UPPER WING SURFACE THAT MATES WITH ANGLES REF 51-00 VOL 11 SRM, OK TO INSTALL ANGLE. INSTALLATION COMPLETED AS PER SRM 53-00-01.

Part: STRUCTURE — DAMAGED (RT ELEVATOR)

STRUCTURAL FAILURE ON RT ELEVATOR UPPER SURFACE, APPROX 3 INCHES LONG BY 3 INCHES WIDE AND HAD COLLAPSED APPROX .5 INCHES, DOES NOT APPEAR TO BE FROM IMPACT. THIS GOES ACROSS 4 RIBS AND IS LOCATED APPROX 2 FEET FROM O/B END OF ELEVATOR. ITEM FOUND DURING B-CHECK MX. REMOVED AND REPLACED O/B ELEVATOR IAW MM 27-20-02, PERFORMED ELEVATOR CHECK PER MM 27-30-02 PG 601 TO 603.