N365FE

Part: SLIDE — FAILED (L1 DOOR) · airframe 91,101 hrs · 39,156 cycles

L1 DOOR SLIDE LIGHT FOUND ON DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL 52-10-03. PERFORMED RESISTANCE CHECK PER MEL 25-61-01 OF DOOR SLIDE ELECTRICAL JACK. RESISTANCE READ APPROX .5 OHMS. R&R L1 DOOR SLIDE ASSY REF MM 25-61-01-2.

Part: SWITCH — MALFUNCTIONED (L1 DOOR) · airframe 91,094 hrs · 39,153 cycles

ON PREFLIGHT L1 DOOR SLIDE CIRCUITRY LIGHT REMAINS ILLUMINATED. WHILE TRYING TO COMPLY WITH MEL 25-61-01 FOR THE "PRESS-TO-TEST" INDICATION, METHOD "A", THE TEST FAILED STEP 1A 4B, DISCONTINUED WITH MEL 25-61-01 PROCEDURES AND RETURNED L1 DOOR BACK TO ITS ORIGINAL CONFIGURATION. L1 DOOR SLIDE PRESSURE INDICATOR PRESS TO TEST SWITCH IS TESTING NORMAL, REF MM 25-61-03-5. CONTINUITY CHECK IS OK, REF FIM 25-61-00-2. OK FOR SERVICE.

Part: CABLE — DEFORMED (R1 DOOR) · airframe 90,102 hrs · 38,572 cycles

R1 DOOR CLUTCH RELEASE CABLE HAS DEFORMATION AND KINKING AT FWD CABLE END. REMOVED AND REPLACED THE R1 DOOR CLUTCH RELEASE CABLE IAW AMM 52-11-12.

Part: CABLE — BROKEN (L1 DOOR) · airframe 89,965 hrs · 38,495 cycles

L1 DOOR AFT CABLE IS BROKEN AND WRAPPED AROUND SPOOL. UNABLE TO OPEN OR CLOSE DOOR WITHOUT DAMAGING OTHER COMPONENTS. R & R THE CABLE IAW AMM 52-10-02-2.

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 88,652 hrs · 37,717 cycles

BS 595 BULKHEAD WEB AT LONGERON 41L HAS A .800 IN CRACK AT THE UPPER FASTENERS HOLE COMMON TO THE TEE CAP. INSTALLED REPAIRED PER SRM 53-40-00

Part: FLOOR SUPPORT — CORRODED (BS 1887) · airframe 88,652 hrs · 37,717 cycles

MAIN DECK BS 1881, RBL 27 FLOOR SUPPORT IS CORRODED.. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG WSP0711.

Part: PANEL — DELAMINATED (NR 2 INLET) · airframe 88,652 hrs · 37,717 cycles

#2 ENGINE INLET (PICKLE BARREL) PANEL AJC7068 IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL 2.

Part: FITTING — CRACKED (WING TO BODY) · airframe 88,652 hrs · 37,717 cycles

CAC BAY LT CTR WING TO FUSELAGE HAIRPIN FITTING UPPER AFT FASTENER AREA HAS 0.500 CRACK. REPAIRED IAW SRM 53-30-00 FIG 7 VOL 1.

Part: FITTING — CRACKED (BS 1156) · airframe 88,652 hrs · 37,717 cycles

LEFT BS 1156 SUGAR SCOOP FITTING HAS THREE CRACKS ON HORIZONTAL LEG BETWEEN LONGERONS 38 AND 39L. REMOVED AND REPLACED FITTING IAW DWG. AYB 7000-1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 88,652 hrs · 37,717 cycles

CAC BAY LWR SKIN, BETWEEN STA 1079 TO STA 1099 LONGERON 52 TO LONGERON 51R, HAS CORROSION AND SHEAR RIVET. REPAIRED PER DWG AGA3097 AND SRM 53-20-00.

Part: SHEAR TIE — CORRODED (BS 1079-1099) · airframe 88,652 hrs · 37,717 cycles

CAC BAY LOWER SKIN, BETWEEW BS 1079 TO 1099 LONGERON 51TO 52R HAS CORROSION AND SHEAR RIVET. REPLACED CORRODED SHEAR TIE IAW DWG. ADA 0112.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 88,652 hrs · 37,717 cycles

FWD CARGO COMP STA 595 AT LONGERON 36L PRESSURE BULKHEAD SUSPECT CRACK. REPAIRED PER SRM 53-40-00 FIG 4.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 88,652 hrs · 37,717 cycles

FWD CARGO BAY PRESSURE BULKHEAD AT BS 595, LWR TEE CAP UPPER TANG CRACKED BETWEEN TWO FASTENERS AND PROPAGATING TO THE EDGE BETWEEN L39L AND L40L. REPAIRED IAW EA. 8-5310-T0330353.

Part: TEE FITTING — CRACKED (BS 595) · airframe 88,652 hrs · 37,717 cycles

FWD CARGO BAY BS 595, LONGERON 36L CRACKED. REPAIRED PER EA. 8-5310-T0330353.

Part: CAP — CRACKED (FUSELAGE) · airframe 88,652 hrs · 37,717 cycles

FWD CARGO, COMPARTMENT STA 595 LONGERON 39R SUSPECT CRACK. AFTER EVALUATION , FOUND TEE CAP CRACKED. REPAIRED TEE CAP PER EA 8-5310-T0330385

Part: SKIN — CRACKED (RT WING) · airframe 88,652 hrs · 37,717 cycles

RIGHT WING NR 7 SLAT TRACK CUTOUT O/B CORNER CRACKED. REPAIRED IAW SRM 57-10-00, FIG.104 A , VOL. I

Part: OXYGEN MASK — UNSERVICEABLE (COCKPIT) · airframe 88,641 hrs · 37,713 cycles

COCKPIT PORTABLE OXYGEN MASK FOUND DRY-ROTTED. REMOVED AND REPLACED COCKPIT PORTABLE OXYGEN MASK IN REF TO AMM 35-30-01-4. ACFT OK FOR SERVICE.

Part: DOOR — CRACKED (LT MLG) · airframe 88,188 hrs · 37,462 cycles

ON T/O, HAD UNSAFE, RED LIGHT, GEAR UP. LEFT MAIN CYCLED GEAR. GEAR DOWN, 3 GREEN, CYCLE D UP, UNSAFE LT MAIN, ACFT DIVERTED. REPLACED LT MLG DOOR.

Part: CRANK ASSY — DEFECTIVE (BRAKE SYSTEM) · airframe 87,880 hrs · 37,295 cycles

CAPTAIN DURING POST FLIGHT DEBRIEF REPORTED, RT BRAKE PEDAL EXCESSIVE TRAVEL & SLOW TO ACTUATE. R & R CAPTAINS RT BRAKE FEATHERING CRANK IAW EA 8-2720-TO324787.

Part: CONTACT — UNSECURE (L1 DOOR) · airframe 87,326 hrs · 37,026 cycles

FOUND LI DOOR SLIDE PRESS TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C EXPIRATION 20 NOV 15. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. L1 DOOR SLIDE PRESS TEST SWITCH INOP. DURING REQ MEL PROCEDURE TEST FOUND LOOSE GROUND, SECURED CONTACT, OPS. TEST NORMAL REF AMM 25-61-03-5-0..

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 872 hrs · 36,987 cycles

DURING DESCENT PASSING THROUGH 16000 FEET THE CAPTAINS WINDSHIELD STARTED CRACKING. NEITHER PILOT NOTICED ANY BIRD IMPACT OR OTHER EXTERIOR FORCE THAT COULD HAVE CAUSED IT. R & R CAPTAINS LT WINDSHIELD IAW MM 56-11-00-2. REINSTALLED WINDSHIELD WIPER ARM IAW MM 30-43-25-4. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 868 hrs · 36,765 cycles

R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST SWITCH INOPERATIVE. R & R RT REMOTE SLIDE PACK PRESS INDICATOR. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 868 hrs · 36,720 cycles

EMERGENCY LIGHT BATTERY 1 LO LVL 1 ALERT DURING EMER LIGHT TEST ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS PWR SUPPLY PER AMM 33-51-01-4. OPS CHECKS GOOD PER AMM 31-51-01-5. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 867 hrs · 36,691 cycles

LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW, ILLUMINATED DURING PREFLIGHT. ARMED EMERGENCY LIGHTS AND THE MESSAGE DID NOT RETURN. EMERGENCY LIGHTS TESTED GOOD IAW AMM 33-51-00-5.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 866 hrs · 36,622 cycles

EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT ON EAD DURING EMERGENCY LIGHT PREFLIGHT TEST.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 864 hrs · 36,496 cycles

MAIN ENTRY DOOR SLIDE 1L DOES NOT TEST. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. R & R LIGHT BULBS. FOUND PUSH SOCKET FALLING APART NEEDS TO BE REPLACED. APPLIED MEL

Part: DOOR — OUT OF ADJUST (L1) · airframe 862 hrs · 36,433 cycles

THE L1 DOOR WILL NOT CLOSE. WHEN ATTEMPTING TO CLOSE THE DOOR THE TOP OF THE DOOR POPS INWARD ABOUT 10 INCHES. COMPLETED ADJUSTMENT TEST OF L1 DOOR PER AMM 52-11-00-5.

Part: SUPPORT — OUT OF POSITION (MLG) · airframe 86,159 hrs · 36,349 cycles

DURING RAISING GEAR AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP, RED LIGHT IN BOTH CONFIG PAGE & INDICATOR ABOVE GEAR HANDLE, DID NOT FEEL ADVERSE YAW OR NOISE THAT ONE MIGHT EXPECT WITH ONE GEAR DOWN. GEAR INDICATED DOWN WITH THREE GREEN FOR LANDING. REMOVED & INSTALLED THE BRAKE HOSE TORQUE BRACKET ON RT GEAR IAW AMM 32-11-02-2, ALIGNED BRAKE LINES & CONDUIT'S ON RT MLG. JACKED ACFT IAW AMM 7-11-00-2-0 & PERFORMED GEAR SWING SEVERAL TIMES. ALL INDICATIONS NORMAL. INSPECTED GEAR & WW NO DEFECTS NOTED. OK TO CONTINUE.

Part: SPAR — DAMAGED (LT WING) · airframe 86,150 hrs · 36,343 cycles

FOUND HOLE ON LT WING REAR LOWER SPAR TO BE DIFFERENT. COMPLY WITH EA 8-5710-T0313003 PT 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,150 hrs · 36,343 cycles

UPPER CARGO COMPARTMENT STATION 1422, RBL8 SEAT TRACK IS DAMAGED .552 BEYOND LIMITS IAW SRM 53-70 VOL 1 PAGE 21. SEAT TRACK SECTION REPLACED IAW SRM 53-70-00 VOL 1.

Part: PANEL — GOUGED (LT WING) · airframe 86,150 hrs · 36,343 cycles

LEFT WING LOWER WING HINGE PANEL 551DB HAS GOUGE ON INNER SECTION FROM FLAP VANE CONTACT. REPAIRED HINGE PANEL 551DB AS REQUIRED IAW SRM 51-71-00 VOL II.

Part: ACCESS PANEL — DELAMINATED (LT HORIZ STAB) · airframe 86,150 hrs · 36,343 cycles

LEFT HORIZONTAL STAB TE ACCESS PANEL 334HB HAS DELAMINATION INNER OTBD SECTION OF PANEL. REPAIR PANEL 334HB IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (LT WING) · airframe 86,150 hrs · 36,343 cycles

PANEL 541AB AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED IAW SRM 51-71-00 VOL II.

Part: PANEL — DELAMINATED (RT WING) · airframe 86,150 hrs · 36,343 cycles

RIGHT WING ROOT PANEL ARC0446-502 IS DELAMINATED. REPAIRED PANEL ARC0446-502 AS REQUIRED IAW SRM 51-71-00 VOL II.

Part: BULKHEAD WEB — CRACKED (NLG WW) · airframe 86,150 hrs · 36,343 cycles

NOSE WW LT SIDEWALL SKIN HAS A FOUR INCH CRACK AT BS 485. REPAIRED IAW SRM 53-30-00 FIG 6

Part: SKIN — DAMAGED (TE FLAP) · airframe 86,150 hrs · 36,343 cycles

RIGHT INBD FLAP INBD LE HAS DAMAGE. REPAIRED IAW SRM 57-10-00 & DWG SG 10570001.

Part: PANEL — DELAMINATED (LT WING) · airframe 86,150 hrs · 36,343 cycles

PANEL ARC0446-503 AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED PANEL ARC0446-503 AS REQUIRED IAW SRM 51-71-00 VOL II.

Part: BRACKET — CRACKED (TE FLAP) · airframe 86,150 hrs · 36,343 cycles

LEFT OTBD FLAP, INBD HINGE FWD ATTACH POINT FITTING, Z BRACKET CRACKED ON INBD SIDE. R & R CRACKED BRACKET IAW SRM 51-31-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,150 hrs · 36,343 cycles

MAIN DECK STATION 1015 LBL 47 SEAT TRACK DAMAGED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-7--00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,150 hrs · 36,343 cycles

MAIN DECK STATION 750 LBL 47 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL I.

Part: DOUBLER — CRACKED (MLG WW) · airframe 86,150 hrs · 36,343 cycles

CENTER LANDING GEAR WW BAY BS 1381, X=31.50 DOUBLER IS CRACKED. REMOVED AND REPLACED DOUBLER.

Part: SKIN — CRACKED (RT WING) · airframe 85,808 hrs · 36,173 cycles

FOUND CRACKS ON RT WING FIXED LE UPPER SURFACE ANTI-ICE TELESCOPING DUCT CUT OUT. COMPLIED WITH EA 8-5720-T0309797 COMPLYING WITH SRM 57-40-01.

Part: BATTERY — INOPERATIVE (SLIDE RAFT) · airframe 84,887 hrs · 35,718 cycles

L1 DOOR EVACUATION SLIDE RAFT PRESS. INDICATOR LIGHT INOPERATIVE. REPLACED BATTERIES FOR L1 DOOR EVACUATION SLIDE RAFT PRESS TEST LIGHT, OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE IAW MM 25-61-01-2.

Part: LAMP — INOPERATIVE (ESCAPE SLIDE) · airframe 83,987 hrs · 35,271 cycles

R1 DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. REPLACED LAMP IAW 26-61-03-2, OPS CHECKED GOOD.

Part: DOUBLER — CRACKED (MLG WW) · airframe 83,803 hrs · 35,179 cycles

CLG W/W COMPARTMENT RT SIDEWALL CUTOUT DOUBLER CRACKED. REMOVED CRACKED DOUBLER, INSTALLED DOUBLER RT SIDE REF SRM 51-00-01, VOL 2 AND 51-33-01, VOL 2.

Part: DOUBLER — CRACKED (MLG WW) · airframe 83,803 hrs · 35,179 cycles

CLG W/W COMPARTMENT LT SIDEWALL CUTOUT DOUBLER CRACKED. R & R CENTER LANDING GEAR W/W LT SIDEWALL CUTOUT DOUBLER PN AEA0526U1.

Part: SPAR — CRACKED (ZONE 300) · airframe 83,422 hrs · 34,966 cycles

RT SIDE OF HORIZONTAL STAB REAR SPAR VERTICAL TANG HAS A CRACK EMANATING FROM FASTENER HOLE, UPPER ROW SECOND OTBD APPROX .375" LONG. (MKD) NEED TO COMPLY WITH WORK CARD STEP 8 B IN WORK CARD INSTRUCTIONS 55X1203ALI-P4 SEQ 140 STOP DRILLED CRACK WITH .250 HOLE IN VERTICAL TANG ONLY. REPAIRED IAW EA 8-5510-163774. PART 2 TO BE ACCOMPLISHED AT OR BELOW EVERY 250 FLIGHT CYCLES.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 83,422 hrs · 34,966 cycles

NR 3 ACM COMPARTMENT STA 565-595 OTBD CEILING WEB TO SKIN ATTACHING ANGLE CRACKED, CRACK RUNS FWD TO AFT IN ANGLE RADIUS APPROX 30 INCHES LONG. INSTALLED CUSP REPAIR ANGLE IAW SRM 53-40-00 VOL I,FIG 28.

Part: CONTROL PANEL — BURNED (COCKPIT) · airframe 83,414 hrs · 34,963 cycles

ELECTRICAL ODOR, LIKE HOT EQUIPTMENT, NOTICABLE IN THE COCKPIT. STRONGER ON THE CAPTAIN'S SIDE AND THE STRONGEST ON GROUND. ODOR APPEARS TO BE COMING FROM THE ELECTICAL SYS CONTROL PANEL. R & R ELECTICAL SYS CONTROL PANEL IAW AMM.

Part: FIRE BOTTLE — INOPERATIVE (NR 1 NACELLE) · airframe 82,486 hrs · 34,456 cycles

ALERTED TO "ENG FIRE ALERT LO" ON NR 1 ENGINE. POSSIBLY COINCEDENTAL, BUT ALERT OCCURED WITHIN 10 SECONDS OF STATIC DISCHARGE/LIGHTNING STRIKE. REMOVED AND REPLACED NR 1 FIRE BOTTLES IAW AMM 26-21-01-4, OPS CHECKED IAW AMM 26-21-01-5, INSTALLED NEW FIREX DISCHARGE CARTRIDGES IN NEW BOTTLES IAW AMM 26-21-05-4. ALL ITEMS OPS CHECKED NORMAL. ALSO PERFORMED THE OPS CHECK PER ENGINEERING ERS REQUEST 12-0018, AMM 26-21-07-5, ALL TESTS PASSED.

Part: INDICATOR — INOPERATIVE (R1 DOOR SLIDE) · airframe 82,468 hrs · 34,448 cycles

R1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING LIGHT INOPERATIVE. R & R R1 EVAC SLIDE PRESSURE TEST SYSTEM PER AMM 25-61-03-2-0. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (R1 SLIDE LIGHT) · airframe 81,397 hrs · 33,859 cycles

R1 DOOR SLIDE PRESS TO TEST LIGHT IS INOP. RELAMPED R1 ESCAPE SLIDE PRESSURE ASSIST BOTTLE PTT SWITCH IAW SMP'S, OPS CKD GOOD. ACFT OK FOR SERVICE.

Part: PUSH-PULL CABLE — INOPERATIVE (THROTTLE) · airframe 81,363 hrs · 33,842 cycles

ABOUT 1 HR FROM DESTINATION, AFTER 2.5 HRS INTO FLIGHT, ENG 2 THROTTLE WOULD NOT KEEP UP WITH 1 OR 3, HAD 7-8 ENG FAILS WHICH WE CLEARED. DECENDING INTO DESTINATION, MANUAL THROTTLES. TRIED TURNING ATS OFF 2-3 TIMES AND RE-ENGAGING, THROTTLE FROZEN AT 83 PERCENT N1. UPON TOUCHDOWN, SHUTOFF NR 2 FUEL LEVER, CLEARING RUNWAY, NR 2 THROTTLE LEVER PERFECTLY FREE TO MOVE FWD OR AFT. REPLACED NR 2 ENGINE PUSH/PULL CABLE.

Part: ECU — MALFUNCTIONED (NR 3 ENGINE) · airframe 80,816 hrs · 33,579 cycles

LEAVING FL 180 ON DESCENT NR 3 ENG RPM LOW INDICATION. N1 20 PERCENT,N2 50 PERCENT, EGT 400. NO OBVIOUS DAMAGE TO ENGINE. ATTEMPTED RE-START AND ENGINE RE-STARTED BUT INDICATIONS ONLY WENT BACK TO N1 20 PERCENT, EGT 400, AND N2 50 PERCENT. ENG HUNG THERE WITH NO FURTHER INCREASE IN RPM. SHUTDOWN ENGINE AND LANDED. REMOVED AND REPLACED THE MAIN ENG CONTROL AND THE FUEL PUMP.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 80,172 hrs · 33,257 cycles

FL 360 FWD CARGO SMOKE INDICATION ILLUMINATED.COMPLIED WITH PHASE 1, DISCHARGED BOTTLE, INDICATION WENT AWAY. COMPLIED WITH CHECK LIST.DECLARED EMERGENCY. LANDED IN OKC. ACFT RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-01-B CATEGORY: C EXPIRATION: 10JUL09 ALSO COMPLIED WITH E.A 8-2620-129625 PART 1. REMOVED AND REPLACED NR 1 AND NR 2 LWR FIREX BOTTLES IAW MM 26-22-01-4. REPLACE ALL FWD LOWER CARGO COMPARTMENT SMOKE DETECTORS IAW AMM REF 26-14-01-4 (4 EACH) AND TEST IAW AMM REF 26-14-01-5. ALL TEST NORMAL. RETURNED ACFT TO SERVICE.

Part: SENSOR — FAILED (ENGINE TEMP) · airframe 79,897 hrs · 33,127 cycles

NR 1 ENG OIL TEMP HIGH LEVEL 3 ALERT. CAME BACK DOWN & FLUCTUATED THROUGHOUT FLIGHT. JUST PRIOR TO DESCENT WENT 178 RED BOXED. SHUTDOWN IAW QRH. WINDMILLED ABOUT 25 MIN. OIL PRESS SLIGHTLY LOW WHEN RUNNING, ABOUT 45 PSI WINDMILLING. TEMP CAME DOWN AT SHUTDOWN. CHECKED OIL TEMPS IN AIU. NR 2 ENG TEMP 47DEG & STEADY. NR 3 ENG TEMP 47DEG & STEADY. NR 1 ENG 86 DEG - 98 DEG FLUXUATING. INSPECTED NR 1 OIL TEMP BULB CONNECTOR. FOUND GROUND WIRE NOT FASTENED & CONNECTOR LOOSE & RUBBER DEBRIS LODGED INSIDE. REMOVED PINS & GROUND WIRE FROM CONNECTOR & DIRECTLY PINNED WIRES TO BULB & CLAMPED GROUND WIRE TO ENGINE. NR 1 ENG OIL TEMP INDICATES A STEADY 15 DEG WITH NO FLUXUATION.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 79,425 hrs · 32,908 cycles

DURING LAND ROLLOUT, ACFT HAD NO RT BRAKES. RECYCLED AND THEN HAD PARTIAL RT BRAKE. I HELD POSITION AND CONTACTED MAINTENANCE, TURNED ANTI-SKID OFF AND TAXIED TO RAMP. SEVERAL APPLICATIONS (8) AND FOUND BRAKE SAT. ANTI-SKID, OFF. WHEN RT BRAKE WORKED SECOND TIME ACFT HAD AGGRESSIVE RT YAW. BLED BOTH BRAKE SYSTEMS IN REF TO MM CH 32-44-04-2 AND 32-43-01. INSPECTED DBCV'S CHECKED RIG IN REF TO MM 32-44-00-2. NO DISCREPANCIES NOTED. SERVICED NR 1 HYD REF MM 12-13-02. AS PRECAUTIONARY REMOVED AND REPLACED ANTI SKID CONTROL BOX REF MM 32-45-01-2. ACFT REQUIRES TAXI CHECK. PERFORMED TAXI CK REF JRH. PERFORMED EASY AND AGGRESSIVE BRAKE APPLICATIONS, ACFT HELD CENTERLINE W/SMOOTH AND EVEN OPERATION. OK FOR SERVICE.

Part: BRACKET — BENT (NR 3 NACELLE) · airframe 78,173 hrs · 32,334 cycles

NR 3 ENGINE INBD AND OUTBD CENTER T/R ALIGNMENT PADS ARE BENT. REMOVED AND REPLACED IAW SRM 51-35-02; VOL II AND EM-78-32-03; REPAIR 17. VERIFIED GAP AND LATCH CHECKS GOOD AT THE NR 3 T/R IAW AMM 78-32-11-2.

Part: WEDGE — CRACKED (ZONE 600) · airframe 78,173 hrs · 32,334 cycles

RIGHT OUTBD AILERON T/E WEDGE IS CRACKED ALONG THE EDGE AT THE INBD END. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 57-20-00; FIG 10; VOL I. FABRICATED A NEW WEDGE SECTION AND ZEE ANGLE IAW SRM 57-20-00; FIG 10; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-35-01; VOL II.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 78,173 hrs · 32,334 cycles

RIGHT WING FUEL PANEL 635 BT; INTERNAL SURFACE HAS AREAS OF CORROSION. FABRICATED FUEL PANEL P/N IAW DAC DWG ARB 0872-38 AND PART MARKED.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 78,173 hrs · 32,334 cycles

RIGHT HORIZONTAL STABILIZER UPPER SKIN INBD SECTION FWD OF THE AFT SPAR IS GOUGED. REPAIRED IAW SRM 55-00-01 VOL I.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 78,173 hrs · 32,334 cycles

LEFT WING INBD L/E, NR 1 SLAT TRACK FWD ATTACHMENT TO SLAT TRIM PANEL AFT SUPPORT "C" CHANNEL HAS FASTENERS LOOSE. UPON FURTHER INVESTIGATION FOUND SIDE BRACKET ON THE SLAT TRACK ATTACHMENT CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET REF DC/MD-10 SRM 51-35-01; VOL II. REINSTALLED SLAT TRACK ATTACHMENT REF DC/MD-10 SRM 51-31-01; VOL II. SLAT TRACK COVER TO BE ADJUSTED ON WORK CARD 27X8501.

Part: PANEL — CHAFED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LEFT WING OUTBD L/E PANEL NR 527 AB INNER SURFACE IS CHAFED AT THE END OF THE ACCESS DOOR HINGE. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER IAW SRM 57-00-01 VOL I & 57-31-01 VOL III. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. ASSEMBLED IAW SRM 51-35-01 VOL II. PAINTED IAW SRM 51-21-01 VOL II.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING INBD FLAP PANEL 644 AB IS DISBONDED. REPAIRED PANEL 644 AB BY REMOVING DAMAGED OUTER SKIN; INNER AND OUTER DOUBLERS. FABRICATED AND BONDED NEW SKIN; INNER AND OUTER DOUBLERS IAW DAC DWG NR ARC 2991; TPS 101, REV E AND FEDEX EA 8-5750-118470 TITLED "WINGS - INBD FLAP NR 1 ROLLER ACCESS COVER PANEL". FABRICATED AND INSTALLED NEW -33 STIFFENER IAW DAC DWG ARC 2991 AND FEDEX EA 8-5750-118470 TITLED "WINGS INBD FLAP NR 1 ROLLER ACCESS COVER PANEL".

Part: SKIN — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING INBD FLAP LOWER SURFACE AT STA XIFH 162 TO XIFH 175 FROM THE FRONT SPAR PLANE TO THE REAR SPAR PLANE HAS 3 EA DENTS THAT REQUIRE REPAIR. CUT OUT DAMAGE IN REF TO SRM 57-10-00 FIG 85 VOL I. FABRICATED DOUBLERS IN REF TO SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED DOUBLERS IN REF TO SRM 51-21-01 VOL II. INSTALLED DOUBLERS IN REF TO SRM 57-10-00 FIG 85 VOL I & 51-35-01 VOL II. PAINTED AREAS IN REF TO SRM 51-21-01 VOL II.

Part: FRAME — GOUGED (TAILCONE) · airframe 78,173 hrs · 32,334 cycles

TAIL CONE RIGHT UPPER PATIO DOOR HINGE FRAME IS GOUGED, MATERIAL ID 2024-T3; PO 600955.2 PER DC/MD-10 SRM 53-52-01; VOL III. ALODINED AND PRIMED PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER PER DC/MD-10 SRM 53-00-01; VOL I.

Part: SKIN — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT OUTBD FLAP LOWER SURFACE AT STA XOFH 703 HAS A DENT. CHECKED DENT, NOTED CREASES. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; FIG 48; VOL I. MATERIAL ID FOR THE REPAIR DOUBLER IS 2024-T3, 0.050, PO 610199.1. FABRICATED DOUBLER IAW DC/MD-10 SRM 57-10-00; FIG 85; VOL I. ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01 PGS 21 THRU 24 AND 51-21-02; VOL II. INSTALLED IAW DC/MD-10 SRM 51-35-01; VOL II.

Part: SKIN — CHAFED (NR 2 COWLING) · airframe 78,173 hrs · 32,334 cycles

NR 2 ENGINE LEFT FAN COWL INNER SKIN CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS & REPAIR AREA, LAYED UP REPAIR, VACUUM BAGGED REPAIR, CURED REPAIR, PERFORMED POST CURE INSPECTION, INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II.

Part: SKIN — CHAFED (NR 2 COWLING) · airframe 78,173 hrs · 32,334 cycles

NR 2 ENGINE RIGHT FAN COWL INNER SKIN IS CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS FOR BONDING, BONDED REPAIR; INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I. PRIMED IAW SRM 51-21-01 VOL II.

Part: SKIN PANEL — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

LEFT INBD FLAP LOWER SURFACE FWD PANEL 2ND FROM THE OUTBD END HAS 1 DENT. REMOVED LEFT FLAP LOWER SURFACE PANEL TO FOM IN REF TO DC/MD-10 SRM 51-31-01; VOL II. REPAIRED GOUGED DENT IN REF TO DC/MD-10 57-00-01; FIG 1 A; SHEET 2. INSTALLED PANEL IN REF TO DC/MD-10 SRM 51-31-01; VOL II.

Part: FITTING — CRACKED (RT WING) · airframe 78,173 hrs · 32,334 cycles

STRINGER BUTTERFLY FITTING NR 43 IS CRACKED APPROX 1/2 TOTAL LENGTH ON THE RIGHT WING, STA XORS 372. THE FITTING IS INSIDE THE FUEL TANK AT STRINGER 43, RIB XORS 372. REMOVED & REPLACED FITTING REF SRM 51-33-01; VOL II

Part: WEDGE — DAMAGED (LT ELEVATOR) · airframe 78,173 hrs · 32,334 cycles

LEFT OUTBD ELEVATOR T/E WEDGE IS DISBONDED AND CRACKED. REPAIRED T/E WEDGE IAW DC/MD-10 SRM 55-30-00; FIG 1; VOL I.

Part: COVER — CHAFED (SLAT TRACK) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING 1 SLAT TRACK COVER FWD END IS CHAFED. REMOVED DAMAGED COVER. LOCATED AND DRILL HOLES IN THE NEW COVER REF DC/MD-10 SRM 51-31-01; VOL II INFO: ADJUSTMENTS TO BE PERFORMED ON FEDEX W/C NR 27X8501.

Part: LINER — WORN (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

LINER OF APU INTAKE HAS SOME EROSION TAKING PLACE ON THE LOWER HALF. APU LINER AT THE INTAKE WAS FOUND TO BE WITHIN SERVICEABLE LIMITS AND TO BE TRACKED AT B-CHECK INTERVALS IAW FEDEX EA 8-4920-119704.

Part: SKIN — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT INBD FLAP LOWER SURFACE FWD PANEL; 2ND FROM THE INBD END HAS SEVERAL DENTS. REMOVED PANEL IAW DC/MD-10 SRM 51-31-01; VOL II. DEPTH OF THE DENTS ARE 0.125 THRU 0.325 USING DEPTH GAUGE T8492C. ORIGINAL THICKNESS OF THE SKIN IS 0.040 IAW DC/MD-10 SRM 57-52-01; FIG 1; VOL III. DENTS ARE OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01; PG 2; VOL I. FABRICATED REPAIRS (3 EA) IAW DC/MD-10 SRM 57-10-00; VOL I. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED REPAIRS IAW DC/MD-10 SRM 57-52-01; VOL I. TOP COATED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED PANEL IAW DC/MD-10 SRM 51-51-31-01; VOL II.

Part: INTERCOSTAL — GOUGED (R1 DOOR) · airframe 78,173 hrs · 32,334 cycles

ON THE R-1 DOOR, LOWER, FWD AND AFT INTERCOSTALS ARE GOUGED. FOUND TO BE WITHIN LIMITS IAW SRM 52-00-01 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED 2 EA INTERCOSTALS IAW SRM 51-31-01 VOL III & 51-33-01 VOL III.

Part: RETAINER — GOUGED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

FWD CARGO PIT ENTRANCE; UPPER RIGHT CORNER CEILING RETAINING STRIP IS GOUGED. REMOVED DAMAGED RETAINING STRIP IAW DC/MD-10 SRM 51-31-01; VOL II; PG 1. FABRICATED NEW STRIP IAW DAC DWG ADA 7132; REV H. ALODINED AND PRIMER IAW DC/MD -10 SRM 51-21-01; VOL II; PGS 21 AND 24. PART MARKED FX-ADA7132-27 IAW FEDEX GMM 7-0-1000. INSTALLED IAW DC/MD-10 SRM 51-31-01; VOL II; PG 1.

Part: RUB STRIP — CHAFED (ZONE 300) · airframe 78,173 hrs · 32,334 cycles

LEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. REMOVED GOUGES ON THE PANEL IAW DC/MD-10 SRM 55-00-01; VOL I. FOUND TO BE WITHIN LIMITS IAW DC/MD-10-10 SRM 55-00-01; VOL I AND UT GAUGE T8225P; CAL DATE 12-19-08. REMOVED AND REPLACED WORN THROUGH RUB STRIP IAW DC/MD-10-10 SRM 51-31-01; VOL II; PG 1.

Part: BRACKET — CRACKED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

BRACKET CRACKED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00414. REMOVED BRACKET IAW SRM 51-31-01 VOL II. FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-10 VOL II. INSTALLED NUTPLATE IAW SRM 51-35-01 VOL II.

Part: PANEL — CHAFED (ZONE 400) · airframe 78,173 hrs · 32,334 cycles

NR 3 PYLON LT TOP PANELS 487CL & 487 BL INTERIOR IS CHAFED. BLENDED DISCREPANT AREAS ON THE NR 3 PYLON PANEL 487 CL WHERE CHAFING WAS PRESENT IAW SRM 54-00-01. CHECKED LIMITS IN DISCREPANT AREA IAW THE FOLLOWING SRMS 54-00-01 VOL I & 54-31-02 VOL III. ORIGINAL THICKNESS 0.090, MATERIAL LOSS 0.023. REMAINING MATERIAL 0.067 ON PANEL (OUT OF LIMITS). FABRICATED A REPAIR DOUBLER IAW SRM 54-00-01 VOL III. TREATED, PRIMED & INSTALLED DOUBLER IAW SRM 51-21-01 VOL II & 51-31-01 VOL II.

Part: BRACKET — CRACKED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

BRACKET CRACKED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00009. REMOVED BRACKET IAW SRM 51-31-01 VOL II. FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED NUTPLATES IAW SRM 51-35-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FS 1840 LBL 19 FLOORBOARD SUPPORT IS CORRODED. CUT OUT DAMAGE IAW SRM 53-00-01; FIG 8 VOL I. FABBED REPAIR DOUBLERS & FILLER PER SRM 53-00-01 FIG 8 SHEET 2 VOL I. ALODINED & PRIMED REPAIR DOUBLERS & FILLER PER SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED REPAIR DOUBLERS & FILLER PER SRM 51-33-01 PG 34 VOL II & SRM 53-00-01 FIG 8 SHEET 2 VOL I.

Part: COVER — CHAFED (L/E SLAT) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING NR 2 SLAT TRACK COVER FWD END IS CHAFED. REMOVED TRACK COVER IAW SRM 51-31-01; VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL II. MACHINED NR 2 SLAT TRACK COVER IAW DWG ARB 1379; REV G. FORMED SLAT TRACK COVER TO CONTOUR IAW SRM 51-10-00; VOL II. DRILLED UP SLAT TRACK COVER IAW SRM 51-31-01; VOL II. ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED SLAT TRACK COVER IAW SRM 51-31-01; VOL II.

Part: SKIN — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT INBD FLAP LOWER SURFACE AT STE XIFH 255 HAS A DENT. DEPTH OF THE DENT IS .225. ORIGINAL THICKNESS OF THE SKIN IS 0.040. OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; FIG 1A; VOL I. USED DEPTH GAUGE TWS 8358A IAW DC/MD-10 SRM 57-00-01; FIG 1 A; VOL I. REMOVED DAMAGED AREA OF THE SKIN IAW DC/MD-10 SRM 57-00-01; FIG 4; VOL I. FABRICATED REPAIR IAW DC/MD-10 SRM 57-00-01; FIG 4; VOL I. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II AND INSTALLED IAW DC/MD-10 SRM 57-00-01; FIG 4.

Part: BRACKET — CHAFED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

BRACKET CHAFED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00009. REMOVED BRACKET IAW SRM 51-31-01; VOL II. FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED NUTPLATE IAW SRM 51-35-01; VOL II.

Part: STANCHION — CHAFED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

TAIL CONE LEFT PATIO DOOR HOLD OPEN STANCHION IS WORN FROM FRETTING. REPLACED TUBE ASSEMBLY IAW AMM 52-46-02-2.

Part: PANEL — CHAFED (HORIZ STAB) · airframe 78,173 hrs · 32,334 cycles

LEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. BLENDED CHAFED AREA. ORIGINAL MATERIAL 0.071; REMOVED 0.015; REMAINING MATERIAL 0.056 IAW DC/MD-10 SRM 54-00-02; VOL I. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 54- 51-02; VOL III. FABRICATED DOUBLER IAW DC/MD-10 SRM 54-00-01; VOL I AND DC/MD-10 SRM 54-51-02; VOL III. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. ASSEMBLED DOUBLER IAW DC/MD-10 SRM 51-35-01; VOL II.

Part: SKIN — CHAFED (ZONE 300) · airframe 78,173 hrs · 32,334 cycles

RIGHT HORIZONTAL STABILIZER PANEL NR 346 BB IS GOUGED AND HAS CORROSION. REMOVED AND REPLACED RUB STRIP SKIN IAW SRM 51-31-01 VOL II PG 1.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 78,173 hrs · 32,334 cycles

NR 3 ENGINE OUTBD T/R UPPER INNER FAIRING IS CRACKED. VERIFIED CRACK PER NTSPM 06-10-11-001. REMOVED DAMAGE IAW ESPM 78-32-01. LOCATED & DRILLED HOLES IAW ESPM 78-32-03. FABBED DOUBLER IAW ESPM 78-32-03. ALODINED & PRIMED DOUBLER IAW DC/MD- 10 SRM 51-21-01; VOL II. INSTALLED NEW FAIRING IAW ESPM 78-32-03.

Part: WEB — CORRODED (NR 1 COWLING) · airframe 78,173 hrs · 32,334 cycles

NR 1 ENGINE WEB APPEARS TO HAVE CORROSION JUST FWD OF THE HYD FILTER BOWLS. REPAIRED WEB IN REF TO EA 8-7220-118465 .

Part: SHEAR TIE — DAMAGED (BS 899) · airframe 78,173 hrs · 32,334 cycles

FWD PIT; FS 899 SHEAR TIE AT L49L TO L51R HAS DOUBLE DRILLED HOLES. FABRICATED NEW SECTION OF THE SHEAR TIE & SHEAR TIE SPLICE SPLICE IAW DWG ADA 0112; REV P & SRM 53-30-00 VOL I FIG 10. ALODINED, PRIMED & PAINTED IAW SRM VOL II PG 8. PART MARKED IAW GMM 7-0-1000.

Part: PANEL — CHAFED (ZONE 500) · airframe 78,173 hrs · 32,334 cycles

LEFT WING LOWER INBD L/E PANEL 516 HB IS CHAFED ALONG THE EDGE. BLENDED THE AREA IAW SRM 57-00-01; VOL I. ORIGINAL MATERIAL .090; MATERIAL REMOVED .020; MATERIAL REMAINING .070 TOOL NR T8225P. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01; VOL I. ASSEMBLED PANEL; DOUBLER AND FILLER IAW SRM 51-35-01; VOL II. PAINTED PANEL AND DOUBLER IAW SRM 51-21-02; VOL II.

Part: ANGLE — CRACKED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

ANGLE REQUIRES FABRICATION; ANGLE IS CRACKED. FABRICATED ANGLE IAW DWG AFA 3866. ALODINED & PRIMED ANGLE IAW DC/MD-10 SRM 51-21- 01; VOL II. INSTALLED ON JOB CARD N00128.

Part: PANEL — CHAFED (ZONE 600) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING LOWER L/E PANEL 616 HB IS CHAFED ALONG THE EDGE. CLEANED RIGHT WING LOWER L/E PANEL 616 HB TO EVALUATE DAMAGE AND PANEL WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. PANEL REQUIRED A SRM REPAIR. FABRICATED REPAIR DOUBLER IAW DC/MD-10 SRM 57-00-01; VOL I. TREATED; PRIMED AND TOPCOATED DOUBLER IAW 51-21-01; VOL II. INSTALLED REPAIR DOUBLER IAW SRM 51-31-01; VOL II.

Part: FRAME — DAMAGED (BS 899) · airframe 78,173 hrs · 32,334 cycles

FWD PIT; FS 899, L51L FRAME HAD DOUBLE DRILLED HOLES. REPAIRED IAW SRM 53-00-01 VOL. I FIG. 10.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 78,173 hrs · 32,334 cycles

NR 2 ENGINE LT T/R TRANSLATING SLEEVE AFT LOWER FAIRING IS CRACKED AT THE FWD CORNER. THE CRACK WAS PREVIOUSLY STOP DRILLED BUT HAS PROGRESSED BEYOND THE STOP DRILL. REMOVED FAIRING IAW SRM 51-35-01; VOL II. LOCATED & DRILLED HOLES IN THE SUBSTRUCTURE IAW SRM 51-31-01; VOL II. INSTALLED SUBSTRUCTURE IAW SRM 51-35-01 VOL II. INSTALLED FAIRING IAW SRM 51-35-01 VOL II.

Part: FITTING — CRACKED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

FITTING REQUIRES FABRICATION; FITTING IS CRACKED. FABRICATED FITTING IAW SRM 51-31-01; VOL II & DWG AFA 3866. ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED ON JOB CARD N00128.

Part: SEAL — CRACKED (NR 2 NACELLE) · airframe 78,173 hrs · 32,334 cycles

NR 2 ENGINE LEFT CORE COWL SKIRT FAIRING SPRING SEALS ARE CRACKED. REMOVED & REPLACED THE SPRING SEAL IAW SRM 51-35-01; VOL II.

Part: PANEL — DENTED (TE FLAP) · airframe 78,173 hrs · 32,334 cycles

LEFT INBD FLAP, LOWER INBD PANEL (P/N ARC 2991-1) IS DENTED AND DEFORMED. THE ACCESS DOOR WITHIN THE PANEL IS MOST DIFFICULT TO CLOSE. REMOVED & REPLACED DOOR HUNGE IAW SRM 51-31-01 VOL II. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. PAINTED IAW SRM 51-21-02 PG 8 VOL II.

Part: PANEL — CHAFED (NR 1 NACELLE) · airframe 78,173 hrs · 32,334 cycles

NR 1 PYLON PANEL NR 439 AL IS CHAFED. REMOVED WEB IAW SRM 51-31-01 VOL II. LOCATED, DRILLED & DEBURRED NEW WEB IAW SRM 51-35-01 VOL II. INSTALLED WEB IAW DWG AUG 7107; REV P.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOORBOARD AT RBL 48 TO 76; BS 615 TO 675 IS SOFT AND SPONGY. EVALUATED FLOOR PANEL INSTALLED INSERTS. FOUND PANEL TO BE SOLID PER FEDEX SRZ 25-005 REV F. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: CLAMP — CRACKED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

IN THE AFT FUSELAGE COMPARTMENT, UPPER TORQUE BOX AREA, ABOVE LONGERON 4R HAS A CRACKED ELECTRICAL CLAMP. REMOVED ELECTRICAL CLIP THAT WAS DAMAGED IAW SRM 51-35-01 VOL II. REMOVED DAMAGED AREA ON THE CLIP IAW SRM 53-00-01 VOL I PG 4B VIEW A. ALODINED & PRIMED ELECTRICAL CLIP IAW SRM 51-21-01 VOL II. INSTALLED CLIP IAW SRM 51-35-01 VOL II.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOORBOARD AT RBL 9 TO 28; BS 615 TO 735 IS SOFT AND SPONGY. EVALUATED THE FLOOR PANEL AND FOUND IT TO BE SOLID IAW FEDEX SRZ 25-005; REV F. SDR SUMITTED IN ERROR- ADMINISTRATOR.

Part: HINGE — WORN (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

FWD CARGO DOOR CONTROL PANEL DOOR HINGE HAS EXCESSIVE PLAY. REMOVED FWD CARGO DOOR CONTROL PANEL DOOR TO FOM PER DC/MD-10 SRM 53-31-01; VOL II. RECEIVED NEW HINGE P/N 2999325N, AND P/N ADA 3469-7, PO 544680.1. ALODINED HINGE PER SRM 51-21-01; PARA 31; VOL II. INSTALLED CONTROL PANEL DOOR PER SRM 51-31-01; VOL II.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOORBOARD AT RBL 48 TO 76; BS 615 TO 675 IS SOFT AND SPONGY. EVALUATED FLOOR PANEL INSTALLED INSERTS. FOUND PANEL TO BE SOLID PER FEDEX SRZ 25-005 REV F. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FLOOR PANEL — DAMAGED (BS 630) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOOR PANEL AT STA 630; LBL 95 IS PUNCTURED. REMOVED LEFT OVER DAMAGED MATERIAL; CLEANED THE AREA AND FILLED IAW FEDEX SRZ 25-005 REV F.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOORBOARD AT LBL 76 TO 108; BS 506 TO 590; PREVIOUS REPAIR AT THE FWD END IS DISBONDED. REPAIRED MAIN CABIN FLOORBOARD WITH FILLER AT LBL 76 TO 108; BS 506 TO 590 AS REQUIRED IAW FEDEX DC/MD-10 DWG SRZ 25-005; REV F. REPAIRED THE DELAMINATION OF THE FWD END PREVIOUS REPAIR IAW FEDEX DC/MD-10 SRM 51-62-01.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOORBOARD AT LBL 48 TO 76 FROM BS 506 TO 590 HAS A PUNCTURED UPPER SKIN. REPAIRED MAIN CABIN FLOOR PANEL AT LBL 48 TO 76; BS 506 TO 590 WITH FILLER AS REQUIRED IAW FEDEX DC/MD-10 DWG SRZ 25-005, REV F.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 78,173 hrs · 32,334 cycles

RT WING NR 8 SLAT LOWER EXTERIOR SKIN IS DENTED. CUT OUT DAMAGED SKIN IAW SRM 57-10-00 FIG 11 VOL I. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00 FIG 41 VOL I. FABRICATED DOUBLERS, 2 SEALS, SPLICE PLATE, FILLER & 4 EACH SUPPORTS IAW SRM 57-10-00 FIG II VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED REPAIR IAW SRM 51-35-02 VOL II.

Part: FLOORBOARD — CRACKED (BS 755) · airframe 78,173 hrs · 32,334 cycles

MAIN CABIN FLOOR PANEL AT STA 755; LBL 5 IS CRACKED. REPAIRED CRACK IAW FEDEX SRZ 25-005 REV F.

Part: FRAME — CORRODED (BS 899) · airframe 78,173 hrs · 32,334 cycles

FWD LOWER CARGO BILGE J-CHANNEL IS CORRODED AT BS 899 BETWEEN STR 51L AND STR 51R. REMOVED CORROSION FROM THE LOWER FRAME CAP (J CHANNEL) IAW SRM 51-21-01 VOL II PG 28 & FOUND MATERIAL LOSS EXCEEDED ALLOWABLE LIMITS. ORIGINAL THICKNESS 0.071, MATERIAL REMAINING 0.054 IAW SRM 53-00-01 VOL I FIG 1A. REPAIRED LOWER FRAME CAP IAW SRM 53-30-00 VOL I FIG 5 & DAMAGED SHEAR TIE SECTION IAW SRM 53-30-00 VOL I FIG 10.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RT INBD FLAP HAS HAIL DAMAGE; SEVERAL DENTS ON THE LOWER SURFACE. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RIGHT WING INBD FLAP T/E WEDGE IN REF TO SRM 51-31-01 VOL II.

Part: SKIN — DAMAGED (TAILCONE) · airframe 78,173 hrs · 32,334 cycles

TAIL CONE UPPER AFT SKIN HAS 3 HOLES (LT AFT EDGE). REPAIRED HOLES PER SRM 53-00-01; VOL I. DOUBLER PER SRM 53-00-01; VOL I AND SRM 53-52-01; VOL III; PO 483358.1. ALODINED AND PRIMED PER SRM 51-21-01; VOL II. INSTALLED PER SRM 53-00-01; VOL I AND SRM 51-31-01; VOL II.

Part: CHANNEL — CRACKED (NR 1 PYLON) · airframe 78,173 hrs · 32,334 cycles

NR 1 PYLON PANEL NR 437 DR HAS A CRACKED CHANNEL. REMOVED CHANNEL IAW AMM 51-31-01 VOL II. FABRICATED CHANNEL IAW SRM 51-10-00 FIG 2 VOL II & DWG 7054, REV J. HEAT TREATED CHANNEL IAW TPS 1003. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. PART MARKED CHANNEL IAW DWG FX AUB 7054-5; REV J & GMM 7-0-1000. INSTALLED CHANNEL IAW SRM 51-31-01 VOL II.

Part: SKIN — CRACKED (RT AILERON) · airframe 78,173 hrs · 32,334 cycles

RT OUTBD AILERON LOWER SKIN FWD EDGE IS CRACKED. REMOVED SKIN PANEL IAW SRM 51-31-01; VOL II. FABRICATED IAW SRM 57-00-01 FIG 4 PARA 12 VOL I. HEAT TREAT IAW TPS 1003 REV A. LOCATED & DRILLED HOLES IAW SRM 51-35-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED DOUBLER REPAIR & SKIN PANEL IAW SRM 51-25-01 VOL II. INSTALLED COVERS IAW SRM 51-31-01 VOL II.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 78,173 hrs · 32,334 cycles

FWD LOWER CARGO BILGE INTERCOSTAL IS CORRODED BETWEEN BS 1059 AND 1079; LBL 57. FOUND CRACK, REMOVED ANGLE & FITTING IAW SRM 51-35-01 VOL II. FABRICATED ANGLE & FITTING ON N/R N00806 & N00807 IAW DWG AFA 3866. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. FABRICATED INTERCOSTAL WEB IAW DWG AFA 3866. TREATED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED INTERCOSTAL, ANGLE & FITTING IAW DWG AFA 3866 & SRM 51-33-01; VOL II. MINOR REPAIR.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RT OUTBD FLAP LOWER SKIN HAS HAIL DAMAGE; SEVERAL DENTS. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RT WING OUTBD FLAP INBD HINGE FAIRING TO WEDGE BRACKETS IN REF TO SRM 51-31-01 VOL II. REMOVED & INSTALLED 3 EA T/E WEDGES IN REF TO SRM 51-31-01 VOL II.

Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 78,173 hrs · 32,334 cycles

NR 3 ENGINE OUTBD T/R LOWER OUTBD FAIRING IS DAMAGED, (MISSING FWD EDGE). REMOVED FAIRING IAW MANUAL 70-13-01. DRILLED NEW PANEL IAW MANUAL 70-13-01. INSTALLED NEW FAIRING IAW MANUAL 70-13-01.

Part: STRINGER SPLICE — CORRODED (BS 1056 S45L) · airframe 78,173 hrs · 32,334 cycles

FWD LOWER CARGO BILGE STR 45L U-CHANNEL HAD CORROSION AT BS 1056. REMOVED CORROSION; ORIGINAL MATERIAL .070; MATERIAL REMAINING .050 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01; VOL I. REMOVED AND REPLACED SPLICE CLIP IAW SRM 51-33-01; VOL II, P/N AGA 3185-1, PO 612787.1.

Part: PANEL — CHAFED (ZONE 500) · airframe 78,173 hrs · 32,334 cycles

LT WING T/E UPPER SURFACE OF THE MOST INBD FIXED PANEL AFT EDGE HAS CHAFING WEAR ABOVE THE INBD FLAP VANE INBD EDGE. TRIMMED WORN EDGE IAW SRM 57-00-01. REPAIRED PUNCTURED AREA BY BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. REMOVED CORROSION, ALODINED & PRIMED IAW 57-00-01 VOL I. CHECKED DENTS ON THE UPPER & LOWER SURFACES AND FOUND THEM TO BE WITHIN LIMITS IAW SRM 51-71-00 VOL II.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RT OUTBD FLAP T/E WEDGE IS DELAMINATED. REMOVED T/E SECTION IAW SRM 51-35-01 VOL II. LOCATED, DRILLED & DEBURRED NEW T/E SECTION IAW SRM 57-20-00 FIG 10 VOL I. INSTALLED T/E SECTION IAW SRM 57-20-00 FIG 10 VOL I.

Part: PANEL — CRACKED (RT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RT INBD FLAP AFT INBD EDGE IS CRACKED. REMOVED, LOCATED, DRILLED & INSTALLED T/E TIP IAW SRM 51-35-02, VOL II. REMOVED, INSTALLED & CHECKED PER AMM 27-50-01-4.

Part: RUB STRIP — WORN (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

LT WING FLAP FWD SIDE L/E RUB STRIP IS WORN IN AREAS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. REMOVED RUB STRIPS IN REF TO SRM 51-35-01 VOL II. DRILLED, DEBURRED, & COUNTERSUNK NEW RUB STRIP IN REF TO SRM 51-31-01 VOL II. INSTALLED RUB STRIP IN REF TO SRM 51-35-01 VOL II.

Part: ATTACH BRACKET — CRACKED (NLG) · airframe 78,173 hrs · 32,334 cycles

NOSE LANDING GEAR RT LANDING LIGHT SUPPORT/ATTACH BRACKET IS CRACKED AT THE LOWER EDGE. REMOVED CRACKED BRACKET LOCATION AND DRILLED THE NEW BRACKET. INSTALLED NEW BRACKET REF SRM 51-31-01; VOL II.

Part: RIB — CRACKED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED INBD OF THE NR 15 SLAT TRACK. REMOVED AND REPLACED RIB ARB-4352-35, PO 612712.1 IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR.

Part: PANEL — CORRODED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING T/E UPPER SURFACED FIXED PANEL LOWER SURFACE SKIN HAS CORROSION AND DELAMINATION JUST ABOVE THE OUTBD FLAP TRACK. REPAIRED IAW DWG ARC0822, TPS 1001 REV E & EA 8-5710-7-116966.

Part: PANEL — CHAFED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING L/E PANEL 517 AB OUTER SKIN EDGE IS CHAFED AND CRACKED. BLENDED AREA IAW SRM 57-00-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 VOL I. CUT OUT DAMAGED AREA IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER & FILLER IAW 57-00-01 VOL I. ALODINED, PRIMED & PAINTED IAW SRM 51-21-01 & 51-21-02 VOL II. INSTALLED DOUBLER & FILLER IAW SRM 51-35-01 VOL II.

Part: RIB — CRACKED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING L/E INTERNAL RIB UPPER AFT EDGE REPAIR DOUBLER IS CRACKED INBD OF THE NR 16 SLAT TRACK. REPAIRED RIB & INSTALLED CUP ARB 1292-39, PO 612641.1; IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR.

Part: SKIN — DENTED (LLT AILERON) · airframe 78,173 hrs · 32,334 cycles

LT WING; FOUND 2 DENTS ON THE INBD AILERON LOWER SURFACE SKIN IN THE FWD OUTBD EDGE AREA. CHECKED DENT, FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01 VOL II AT STA XIA 350. FABRICATED IAW SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21-24 VOL II. INSTALLED IAW SRM 51-21-01 VOL II.

Part: RIB — CRACKED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED OUTBD OF NR 12 SLAT TRACK. INSTALLED REPAIR ARB-4352-35, PO 612903.1 IAW SRM 57-20-00 FIG 1 VOL I & 53-33-01 VOL II. MINOR REPAIR.

Part: SKIN — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

LT WING INBD FLAP FWD SURFACE HAS MANY DENTS. REMOVED & INSTALLED 2 FLAP WEDGES IN REF TO SRM 51-31-01 VOL II.

Part: PANEL — DELAMINATED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

LT WING OUTBD FLAP PANEL 536 HL; CORNER IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGED SKIN FABRICATING A SKIN, PLUG & DOUBLE. HOT BONDED REPAIR & REFINISHED IAW SRM 51-71-00.

Part: PANEL — DENTED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

RT WING OUTBD FLAP; INBD PANEL NR 636 BR IS DENTED IN SEVERAL PLACES. REPAIRED RT WING OUTBD FLAP INBD PANEL 636 BR BY CHECKING LIMITS ON THE DENTS IAW SRM 51-80-01 VOL II. REMOVED DAMAGED AREAS FOUND TO BE OUT OF LIMITS. PERFORMED DOUBLER REPAIR AT THE OUTER SKIN BY METAL BONDING IAW SRM 51-71-00 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. SEALED IAW SRM 51-41-01 VOL II & RESTORED FINISH IAW SRM 51-21-02 VOL II.

Part: PANEL — CHAFED (LT AILERON) · airframe 78,173 hrs · 32,334 cycles

LT WING INBD AILERON L/E INBD SURFACE CLOSE OUT PANEL HAS CHAFING WEAR. LT WING INBD AILERON L/E INBOARD SURFACE CLOSE OUT PANEL WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 57-00-01 VOL I. FABRICATED, TREATED & PRIMED IAW THE FOLLOWING SRM`S 57-00-01 VOL I & 51-21-01 VOL II. INSTALLED REPAIR DOUBLER IAW SRM 51-31-01 VOL II. REINSTALLED PANEL IAW SRM 51-31-01 VOL II.

Part: PANEL — CHAFED (T/E FLAP) · airframe 78,173 hrs · 32,334 cycles

LT WING INBD FLAP FWD L/E PANEL IS CHAFED AT THE OUTBD HINGE AREA. BLENDED CHAFFED AREA & FOUND OUT OF LIMITS IAW SRM 57-00-01 VOL I, ORIGINAL THICKNESS 0.080. REMAINING MATERIAL 0.020. MATERIAL REMOVED 0.060. FABRICATED SKIN & INNER DOUBLER IAW DWG ARC 3152, REV M. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. REMOVED & REPLACED SKIN PANEL IAW SRM 51-31-01 VOL II. PAINTED SKIN PANEL IAW SRM 51-21-01 VOL II.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 78,173 hrs · 32,334 cycles

CENTER PIT FLOOR PANEL 183 KF HAS CRACKED SKIN AND THE EDGES ARE DELAMINATED. FABRICATED A NEW CTR PIT FLOOR BOARD IAW DWG SRZ 25-005; REV E. PART MARKED NEW PANEL IAW GMM 7-0-1000.

Part: STRUCTURE — DEBONDED (LT MLG DOOR) · airframe 78,173 hrs · 32,334 cycles

LT MLG STRUT DOOR; LOWER AFT END HAS THE METAL EDGE PROTECTOR DISBONDING. LT MLG STRUT DOOR WAS REPLACED. ALL WORK WAS ACCOMPLISHED ON N00122.

Part: DOOR — CORRODED (LT MLG) · airframe 78,173 hrs · 32,334 cycles

LT MLG STRUT DOOR LOWER CORNER HAS CORROSION. DOOR WAS REPLACED & ALL WORK WAS ACCOMPLISHED ON W/C N00122.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 EF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 3 187 EF. LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET AND LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 KF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 KF; POTTED EDGES; COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS AND FABRICATED TOP SHEET. LAY-UP PLACED UNDER VAC BAG; COMPLETED CURE; COUNTERED SINK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: DOOR — DELAMINATED (LT MLG) · airframe 78,173 hrs · 32,334 cycles

LT MLG STRUT DOOR EXTERNAL DOUBLER IS DISBONDING. LEFT MLG STRUT DOOR WAS FOUND TO REQUIRE REPLACEMENT. REMOVED & REPLACED LT MLG STRUT DOOR & ADJUSTED THE DOOR FOR PROPER FIT & FAIR LIMITS ON GEAR RETRACTION IAW AMM 32-14-01-2. PERFORMED THE FUNCTIONAL CHECK LISTED ON THE JPF STEP 8.

Part: BRACKET — CRACKED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING OUTBD FLAP FWD HINGE; POSITION TRANSMITTER SUPPORT BRACKET IS CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-33-01 & 51-35-01; VOL II. FABRICATED IAW DWG ARC0873 REV 6. ALODINED & PRIMED IAW SRM 51-21-01 PGS 24 THRU 24 VOL II. INSTALLED IAW SRM 51-33-01 & 51-31-01 VOL III.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 HF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 HF. LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: SKIN — DENTED (BS 820 S37L) · airframe 78,173 hrs · 32,334 cycles

DENTED; EXTERNAL SKIN AT STA 820; BELOW LONGERON 37L. REPAIRED AREA OF SKIN AT STA 820; BELOW LONGERON 37L IN REFERENCE WITH SRM 53-20-00 VOL I FIGURE 13. EXTERNAL DOUBLER HAS A EDGE DISTANCE TO HEIGHT RATIO OF 211 THAT IS WITHIN LIMITS IAW SRM 53-00-02 VOL II FIGURE 1 SHEET 2. MINOR REPAIR

Part: FLOOR PANEL — FAILED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 DF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 DF; POTTED EDGES; COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS AND FABRICATED TOP SHEET. LAYED UP TOP SHEET UNDER THE VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C.

Part: PANEL — CHAFED (RT WING) · airframe 78,173 hrs · 32,334 cycles

RT WING LOWER T/E PANEL NR 651 BB AT THE OUTBD FLAP IS CHAFED ON THE INBD INNER SKIN. REPAIRED IAW SRM 51-71-00 VOL II & DWG ARC 0781. REMOVED & INSTALLED PANEL & SEAL IN REF TO SRM 51-31-01 VOL II.

Part: FRAME — BENT (BS 791 S49-50R) · airframe 78,173 hrs · 32,334 cycles

FWD LOWER CARGO BILGE J-CHANNEL HAS BENT EDGE AT BS 791 BETWEEN STR 49R AND STR 50R. REPAIRED THE FRAME J-CHANNEL IN REFERENCE WITH SRM 53-30-00 VOL I FIGURE 5. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 BF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 BF; POTTED EDGES; COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS; FABRICATED TOP SHEET LAYED UP UNDER VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005 REV F AND 25-011 REV C.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 JF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 JF. POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP TOP SHEET UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: HINGE — DAMAGED (LT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

FRAGMENTS ARE MISSING FROM THE INBD PIANO HINGE ON PANEL 551 CB LT WING T/E LOWER SURFACE. REMOVED PANEL IAW SRM 51-31-01; VOL II. REMOVED HINGED PANEL IAW SRM 51-33-01 VOL II. LOCATED & DRILLED HOLES IAW SRM 51-33-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED PANEL & HINGE IAW SRM 51-31-01 & 51-33-01 VOL II. PAINTED IAW SRM 51-21-01 PG 8 VOL II.

Part: PANEL — GOUGED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LT WING LOWER SURFACE HINGED PANEL 551 DB UPPER SURFACE IS GOUGED AND BENT ON THE AFT MID SECTION. REPAIRED IAW SRM 51-71-00 VOL II. ALODINED & PRIMED REPAIR AREA IAW SRM 51-21-01 VOL II. SEALED REPAIR IAW SRM 51-71-00 & 51-71-01 VOL II. PAINTED REPAIR IAW SRM 51-21-01 VOL II. REMOVED & INSTALLED THE SEAL RETAINER & PANEL 551 DB IN REF TO SRM 51-31-01 VOL II.

Part: PANEL — CRACKED (RT WING) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING UPPER L/E PANEL NR 617 CT IS CRACKED IN 2 PLACES. PERFORMED HFEC PER NDT SPM 06-10-09-09. MARKED CRACKS. STOP DRILLED CRACKS. FABBED DOUBLERS REF SRM 57-10-00 VOL I. ALODINED & PRIMED REF SRM 51-21-01 VOL II. INSTALLED DOUBLERS REF SRM 51-35-01 VOL II. PAINTED REF SRM 51-21-01 VOL II.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 GF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 GF; POTTED EDGES; COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG COMPLETED CURE; COUNTER SUNK HOLES AND NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 AF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 AF; LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET AND LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 CF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 CF. LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 78,173 hrs · 32,334 cycles

AFT PIT FLOOR PANEL NR 187 FF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 FF. LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR.

Part: LINER — CRACKED (CARGO DOOR) · airframe 78,173 hrs · 32,334 cycles

FWD CARGO DOOR LINER LOWER EDGE CRACKED OUT AT THE FASTENER HOLES; PREVIOUS REPAIR IS DELAMINATING WITH WASHERS PULLING THROUGH. APPLIED FIBERGLASS OVERLAY REPAIR IAW SRM 51-43-01; VOL II.

Part: ACOUSTIC PANEL — BROKEN (NR 1 ENGINE) · airframe 78,173 hrs · 32,334 cycles

NR 1 ENGINE INTAKE BLACK SOUND SUPPRESSION FWD LIP IS BROKE AT THE 10:30 POSITION. REMOVED PANEL IAW MM 72-23-01. REPAIRED IAW MM 72-23-01. RESTORED FINISH IAW SRM 51-21-02 VOL II. REINSTALLED SUPPRESSION PANEL IAW AMM 72-23-00.

Part: LINER — DELAMINATED (CARGO DOOR) · airframe 78,173 hrs · 32,334 cycles

THE FWD CARGO DOOR LINER HAS A PREVIOUS REPAIR THAT IS DELAMINATING ON THE AFT EDGE. APPLIED FIBERGLASS OVERLAY REPAIR IAW SRM 51-43-01 VOL II.

Part: PANEL — DELAMINATED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LEFT WING LOWER T/E PANEL NR 541 NB IS DELAMINATED. REPAIRED IAW SRM 51-71-00; VOL II.

Part: PANEL — DEBONDED (LT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

LEFT WING INBD FLAP FAIRING NR 535HL HAS AREAS OF DISBOND. REPAIRED BY FABRICATING & BONDING THE INNER & OUTER SKINS; INNER & OUTER DOUBLERS & CORE IAW TPS 1001, REV E & EA 8-5720-118479,

Part: SKIN — CHAFED (ZONE 500) · airframe 78,173 hrs · 32,334 cycles

CHAFED INTERIOR SKIN REPAIR DOUBLER ON PANEL NR 535 DL. REMOVED DAMAGED DOUBLER. CLEANED & PREPPED AREA. FABRICATED NEW DOUBLER & FILLER. APPLIED A HOT BOND, SEALED EDGES WITH SEALANT. PRIMED & PAINTED IAW SRM 51-71-00 VOL II.

Part: PANEL — DELAMINATED (RT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING OUTBD FLAP; INBD PANEL NR 635 DL IS DELAMINATED. FABRICATED & BONDED PANEL IAW EA 8-5720-118478.

Part: PANEL — DELAMINATED (RT WING) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING LOWER T/E PANEL NR 641LB IS DELAMINATED. REPAIRED PANEL BY FABRICATING & BONDING SKINS, CORE, DOUBLERS AND PHENOLIC FILLER IAW EA 8-5720-118473; DWG ARC0357 & TPS 1001, REV E.

Part: INTAKE — DAMAGED (LT ENGINE) · airframe 78,173 hrs · 32,334 cycles

NR 1 ENGINE INTAKE AT THE 8:30 POSITION; ABLATIVE COATING IS MISSING. REMOVED DAMAGE, APPLIED SEALANT TO REPAIR & CURED IAW ENGINE MANUAL 72-22-01 REPAIR 10.

Part: PANEL — DEBONDED (RT WING) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING PANEL NR 641 EB; CORNER IS DISBONDED. RESTORED TO ORIGINAL IAW SRM 51-71-00, 51-21-01 & 51-21-02 VOL II.

Part: PANEL — DELAMINATED (RT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING OUTBD FLAP INBD FAIRING PANEL NR 636 DR IS DELAMINATED. REPAIRED IAW DWG ARC 2232, TPS 1001 REV E & EA 8-5750-116970. RESTORED FINISH SRM 51-21-02; VOL II.

Part: PANEL — DELAMINATED (ZONE 600) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING UPPER L/E PANEL NR 618 BT IS DELAMINATED. REPAIRED PANEL IAW DWG ARB1100, TPS 1001 REV E & EA. 8-5710-116969.

Part: LINER — CRACKED (CARGO DOOR) · airframe 78,173 hrs · 32,334 cycles

FWD CARGO DOOR LINER IS CRACKED AT THE LOWER CORNER OF THE ACTUATOR ARM CUTOUT. APPLIED FIBERGLASS OVERLAY REPAIR IAW SRM 51-43-01; VOL II.

Part: SKIN — DENTED (ZONE 600) · airframe 78,173 hrs · 32,334 cycles

PANEL NR 541 CR EXTERNAL SKIN IS DENTED AND GOUGED. REPAIRED DENT & GOUGED PANEL BY REMOVING THE DAMAGE AT THE OUTER SKIN SECTION. FABRICATING & BONDING A REPAIR SKIN SECTION & DOUBLER IAW SRM 51-71-00 VOL II. ALODINED & PRIMED REPAIR AREA IAW IAW 51-21-01 VOL II. SEALED REPAIR IAW SRM 51-71-00 VOL II. RESTORED THE FINISH TO THE REPAIR AREA IAW SRM 51-21-01 VOL II.

Part: SKIN — GOUGED (TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RIGHT WING OUTBD FLAP INBD HINGE FAIRING PANEL NR 635 BR INNER SKIN IS GOUGED. REPAIRED IAW SRM 51-71-00, VOL II, PARA 17. ALODINDE, PRIMED & PAINTED IAW SRM 51-71-00, VOL II.

Part: PANEL — CRACKED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LEFT WING OUTBD L/E PANEL 527 AB OUTBD END ACCESS DOOR HINGE MOUNT IS CRACKED. REMOVED & REPLACED THE HINGE IAW SRM 51-35-01 VOL II.

Part: PANEL — DELAMINATED (RT WING TE FLAP) · airframe 78,173 hrs · 32,334 cycles

RT WING OUTBD FLAP HINGE PANEL NR 636GL IS DELAMINATED ON THE INNER SURFACE. REPAIRED PANEL & FABRICATED & BONDED NEW INNER & OUTER SKINS IAW DWG ARC2012, TPS 1001 REV E & EA 8-5750-116964.

Part: RETAINER — GOUGED (LT WING) · airframe 78,173 hrs · 32,334 cycles

LEFT WING INBD T/E PANEL 541 GB SEAL HOLDER IS GOUGED. REMOVED GOUGED SEAL RETAINER AND REPLACED IAW SRM 51-35-01 VOL II. MINOR REPAIR.

Part: WEDGE — CRACKED (RT AILERON) · airframe 78,173 hrs · 32,334 cycles

THE RT OUTBD AILERON T/E WEDGE IS CRACKED AND THE AFT EDGE IS SEPARATED. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 57-20-00 FIG 10 VOL I. FABRICATED A NEW WEDGE SECTION & ZEE ANGLE IAW SRM 57-20-00 FIG 10 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. REMOVED 3 STATIC DISCHARGE WICK BASES IAW AMM 23-00-00-2. INSTALLED WEDGE SECTION; ZEE ANGLE & 3 STATIC DISCHARGE WICK BASES IAW SRM 51-35-01 VOL II 57-20-00 FIG 10 VOL I & AMM 23-60-00-2.

Part: SLAT — DENTED (ZONE 600) · airframe 78,173 hrs · 32,334 cycles

THE NR 8 SLAT HAS NUMEROUS L/E DENTS ALONG THE ENTIRE SPAN. REMOVED & REPLACED NR 8 SLAT. EXTEND & RETRACTED SLATS SEVERAL TIMES. NO BINDING & GAP CHECK GOOD PER AMM 27-80-01-4.

Part: SKIN — DEPARTED (RT AILERON) · airframe 78,173 hrs · 32,334 cycles

RT OUTBD AILERON UPPER SKIN HAS NUMEROUS DENTS. MEASURED DEPTH IS .056. FOUND TO BE WITHIN LIMITS IAW SRM 51-80-01; PROCEDURE "F" PG 1 VOL II. MINOR REPAIR

Part: WHEEL — FAILED (MLG) · airframe 77,974 hrs · 32,228 cycles

PDIS: DURING TAKEOFF FELT VIBRATION LEFT THE GEAR DOWN. CONFIRMED WITH TOWER FOUND RUBBER ON RUNWAY. DUMPED 82,000 POUNDS OF FUEL AND DID EMERGENCY RETURN. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY, WHICH BLEW UP AT 152 KTS ON TAKEOFF FROM EWR. INSPECTED AREA AROUND RT GEAR, NO DAMAGE NOTED EXCEPT FOR A PIECE OF THE MLG FOLLOWUP DOOR IS MISSING. REMOVED AND REPLACED RT MAIN GEAR DOOR LOWER PANEL IAW AMM 20-50-02-2. NO ADJUSTMENT REQ FOR THIS PART ON THE MAIN GEAR DOOR. OK TO CONTINUE.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 76,657 hrs · 31,608 cycles

DURING NORMAL LG EXTENSION, COCKPIT PANEL GEAR LIGHTS AND SD CONFIG LIGHTS INDICATED RED, ALL 3 LG LIGHTS WERE RED ON BOTH INDICATORS. ALTERNATE EXTENSION RESULTED IN 3 GREEN ON BOTH PANEL (COCKPIT PANEL AND CONFIG SD). WHEN THE LG HANDLE WAS PLACED DOWN, IT FELT LIKE THE GEAR EXTENDED, BUT NO GREEN INDICATIONS, RED LT WAS ON IN LG HANDLE; LG NOT DOWN WARNING SOUNDED; "LANDING GEAR" IN ESSENTIAL ITEMS BOX PRIOR TO ALTERNATE EXTENSION. REMOVED AND REPLACED LANDING GEAR HANDLE SWITCH S1- 431 PER MM 32-31-02-2. JACKED A/C AS PER MM 07-11- 00-2, AND PERFORMED GEAR SWING PER MM 32-30-00-0 AL INDICATIONS ARE NORMAL.

Part: SKIN — DAMAGED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING CRACK 1" LONG AT STA 480 ON L/E SKIN. REPAIRED IAW SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — DAMAGED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING FOUND 1 CRACK ON DOOR SKIN LONG.1.25". REPAIRED IAW SRM 57-10-00 FIGURE 8 VOL.1.

Part: SKIN — DAMAGED (RT WING) · airframe 75,721 hrs · 31,216 cycles

RT WING UPPER SKIN AT STA XORS 160 HAS A DOUBLER REPAIR 19" BY 11". CUT OUT ORIGINAL DOUBLER IAW SRM 57-10-00 FIGURE 44 VOL 1 AND ACCOMPLISHED FEDEX EA 8-5710-99717.

Part: SKIN — DAMAGED (L/E SLAT) · airframe 75,721 hrs · 31,216 cycles

LT WING, SLAT NR 2, AT STA XORS 264,THE EXTERNAL SKIN UPPER SIDE HAS A DOUBLER REPAIR (4 INCHES X 3 INCHES ). REMOVED EXISTING REPAIR TO EVALUATE DAMAGE IAW SRM 51-30-01 VOL 2. CLEANED AREA IAW SRM 51-41-01-VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER NR F177208/N01208-1 FILLER, F177208/N01208-3 SPLICE, F177208/N01208-5 SPLICE AND IAW EA NR 8-5760-97870.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 75,721 hrs · 31,216 cycles

ON NR 1 PYLON FOUND 1 EA CRACK 1.25 INCH LONG ON UPPER WEB AT STA YN 310. REMOVED PUSH PULL CABLES IAW MM 76-11-02-2 PAR 3, DISASSEMBLIED PIPES IAW MM 20-10-01-2, 28-00-01-2, REMOVED PULLEY, BRACKETS IAW SRM 51-31-02 VOL 2, MM 20-50-02-2, DISASSEMBLIED WEB AND 19 STIFFENERS IAW SRM 51-35-01 VOL 2 PAR 1/5 AND SRM 51-31-01 VOL 2 PAR 20. CLEANED, REPAIR AREA IAW MM 12-22-01-7. PERFORMED REPAIR IAW SRM 54-20-00 VOL 1 FIG 20. INSTALLED PUSH PULL CABLES, INSTALLED PIPES, INSTALLED PULLEYS, BRACKETS. PERFORMED TEST FOUND OK IAW MM 76-11-02-2, 20-10-01-2, 28-00-01-2 IAW SRM 51-31-02 VOL 2, MM 20-50-02-2.

Part: SKIN — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

FOUND LT WING TIP UPPER SIDE AT STA XW925 HAS REPAIR DOUBLER (12 BY 5) AND TRIPLER(6.5 BY 4). REMOVE PANEL IAW SRM 51-31-01 VOL2. REMOVED 2 DOUBLER IAW SRM 51-31-01VOL 2. REMOVED SEALANT IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDT SPM 8. FOUND CRACK. INSTALLED REPAIR IAW FX EA 8-5760-97869 REINSTALLED PANEL IAW SRM 57-31-01 VOL 2. FABRICATED PARTS IAW DETAIL PART TRAVEL N01214-3 DOUBLER AND N01214-5 FILLER IAW FX EA8-5760-97869. SEALED AREA IAW SRM 51-4-01 VOL 2.

Part: WEB — CORRODED (CARGO DOOR) · airframe 75,721 hrs · 31,216 cycles

AFTER REMOVAL LINER OF FWD CARGO DOOR FOUND SEVERE CORROSION ON WEB AROUND HOLES BETWEEN STA 959 AND STA 899. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2, REMAIN MATERIAL THK .050". IS OUT OF LIMITS IAW SRM 52-00-01 FIG 1A SHT 3 VOL 1. INSTALLED AN EXTERNAL DOUBLER IAW SRM 52-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00695-3 FILLER AND N00695-5 REPAIR DOUBLER IAW SRM 52-00-01 FIG 4 SHT 2 VOL 1.

Part: WEB — CORRODED (CARGO DOOR) · airframe 75,721 hrs · 31,216 cycles

AFTER REMOVAL LINER OF FWD CARGO DOOR FOUND CORROSION WITH EXFOLIATION ON WEB AT STA 969. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 REMAIN MATERIAL THK .035" OUT OF LIMITS IAW SRM 52-00-01 FIG 1A SHT 3 VOL 1. TRIMMED OUT DAMAGED PORTION OF WEB, AND INSTALLED FILLER REPAIR DOUBLER IAW SRM 52-00-01 FIG 4 SHT 2 VOL1 FAB PART IAW DETAIL. PARTS TRAVELLER N00694-5, DOUBLER AND N00694-3 FILLER IAW SRM52-00-01 FIG 4 SHT2 VOL 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

AIR COND COMPT LT SIDE CRACK FOUND 1" LONG ON ANGLE AT STA 545 X= 70. TRIM AND REMOVED CRACK ON JAMB IAW SRM 51-35-01 PAGE 1/13 VOL 2 AND DWG ACA3805. INSTALLED NEW JAMB SECTION IAW DWG ACA3805 AND SPLICE IAW SRM 53-00-01 FIG 8 SHT2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER NR F176681 N00681 AND IAW SRM 53-00-01 FIG 8 SHT2 VOL 1.

Part: SPLICE — CRACKED (NR 3 PYLON) · airframe 75,721 hrs · 31,216 cycles

DURING GENERAL OPENING PYLON 3 RE OAN J/C ACCESS PNL ENG PYLON 3 FOUND 1 EA CRACK 1 INCH LONG ON SPLICE OF FAIRING 488DL (REMOVED PART). PERFORMED STOP DRILL HOLE AND FABRICATED & INSTALLED ANGLE IAW SRM 51-35-01 PAGE 1/13 REF SRM 54-00-01 FIG 2B SHT 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

AFT CARGO COMPT AT STA 1940 X= 20 EXISTING REPAIR ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW DWG AGA 3855.

Part: BEAM — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FWD CARGO COMPT CRACK 0.25 INCH LONG ON BEAM AT STA 1099 X=-58. REPAIRED BEAM IAW SRM 53-00-01 FIG 2 SHT 2 VOL 1. INSTALLED NEW CLIP-9 PICK UP EXISTING HOLE AND FASTENER IAW DWG ADA3645, REINSTALL CHANNEL IAW SRM 51-31-01 PAGE 36/41 VOL 2.

Part: BUSHING — DAMAGED (NR 3 PYLON) · airframe 75,721 hrs · 31,216 cycles

PYLON 3 FOUND SLEEVE WEAR AND FITTING CLEVIS WITH HOLES BUSHING OVALIZED. CHECKED DIAMETER CLEVIS FITTING, AND VERIFIED SLEEVE DIAMETER IAW CMM 20-20-06 FIG 5 REF SRM 57-20-00, CLEVIS FITTING REMOVAL IAW MM 57-00-00-2. REWORKED HOLES, FABRICATED/INSTALLED REPAIR BUSHING IAW CMM 20-20-06 FIG 5 REF SRM 57-00-00 FIG2. INSTALLED CLEVIS FITTING IAW MM 57-00-00-2 REF SB A57-106, AND INSTALLED SLEEVE BUSHING IAW MM 54-00-02-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

MAIN CABIN AT STA 1741 L13 RT SIDE ON FRAME FOUND CRACK 5 INCHES LONG. CUTTED FRAME SECTION BETWEEN LONG 10 AND 11 LT SIDE AND SPLICE INSTALLED NEW SECTION IAW SRM 53-30-00 FIG 5 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F176558- 3 FWD CHANNEL F176556-5A AFT CHANNEL AND AND F17656-7 SECTION FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

MAIN CABIN AT STA 1781 L13 LT SIDE ON FRAME FOUND CRACK 5 INCHES LONG. CUT FRAME SECTION BETWEEN LONGERONS 10 AND 11 LT SIDE AND SPLICE INSTALLED NEW SECTION IAW SRM 53-00-00 FIG 51 VOL 1. FABRICATED PART IAW DETAIL PARTS TRAVELER F176555-3 FWD CHANNEL F176555-5A AFT CHANNEL AND F176555-7S, FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL 1.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND CRACK LONG .750 INCH AT STA 1156 BETWEEN L39/L40 LT SIDE, INTERNAL CAC ON BULKHEAD AT X=-76, SIGNED POSITION AND STOPCRACK. SUGAR SCOOP REPAIRED IAW SRM 53-40-00 FIG 8 VOL 1.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND 2 EXTERNAL DOUBLER (DIM 13" BY 12") FROM STA 1841 TO STA 1851 BETWEEN L NR 36 RT AND L NR 38 RT. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01185 AND IAW SRM 53-20-00 FIG 6 VOL 1.

Part: UNKNOWN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

FOUND REPAIR DOUBLER CENTER FUSELAGE R3 DOOR JAMB AT STA 1250.750 AND STA 1256.750 BETWEEN LONGERON S26/27. REPLACED REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F177246-4 DOUBLER AND IAW SRM 53-50-00 FIG 19 DETAIL -3.

Part: UNKNOWN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

LEFT WING FIXED L/E LOWER SIDE, STA XOS 545 AT SLAT TRACK NR 8 CUTOUT, FOUND AN EXTERNAL REPAIR DOUBLER (5.5 X 3.5 INCHES). REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 6 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER N01207 AND IAW SRM 57-10-00 FIG 6 VOL 1.

Part: REPAIR — MISREPAIRED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND 2 EXTERNAL DOUBLERS (DIM 4" BY 12") ON FWD JAMB OF FWD CARGO DOOR STA 879 BETWEEN L NR 40 RT AND L NR 42 RT. PERFORMED GVI ON EXTERNAL DOUBLER ON FWD JAMB IS NOT COMPLIANCE WITH EA NR 8-5300-91121 CRITERIA BY EO NR 8-51-00-7-5001 PT1- BECAUSE 1 ROW HOLE MISSING. REMOVED 2 DOUBLERS IAW SRM 51-33-01 VOL 2 PAGE 34/47 AND SCUFF PLATE TO GAIN ACCESS IAW SRM 51-31-01 VOL 2. INSTALLED REPAIR IAW SRM 53-50-00 FIG 26 VOL 1. REINSTALLED SCUFF PLATE IAW SRM 51-41-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01157-1 REPAIR DOUBLER AND FILLER IAW SRM 53-50-00 FIG 26 VOL 1.

Part: UNKNOWN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

LT WING FIXED L/E LOWER SIDE, AT STA XOS 490, AT SLAT TRACK NR 7 CUT OUT, FOUND AN EXTERNAL DOUBLER (9" BY 6"). AFTER ASSESSMENT OF THE REPAIRED WAS DETERMINED THIS REPAIR COMPLIED WITH THE REQUIREMENTS OF SRW, REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 65.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND REPAIR DOUBLER CENTER FUSELAGE L3 DOOR JAMB AT STA 1250.70 AND 1256.750 BETWEEN LONGERONS 26 AND 27. REPLACED REPAIR IAW SRM 53-50-000 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01241-3 DOUBLER IAW SRM 53-50-00 FIG 19 DETAIL -3.

Part: SKIN — UNKNOWN (SLAT) · airframe 75,721 hrs · 31,216 cycles

LEFT WING SLAT NR 2, FOUND EXTERNAL REPAIR DOUBLER AT STA XORS 264 ON THE INTERNAL SKIN LOWER SIDE 12 X 10 INCHES. REMOVED EXISTING REPAIR TO EVALUATE DAMAGE IAW SRM 51-30-01 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER N01197 AND IAW SRM 51-30-01 VOL 2. INSTALLED REPAIR IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: UNKNOWN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

R1 DOOR EXISTING FLUSH REPAIR ON EXTERNAL SKIN. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 12 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELERF177260-4 DOUBLER F177260-2 FILLER AND IAW SRM 52-10-00 FIG 12A. VOL1

Part: SKIN — UNKNOWN (UNKNOWN) · airframe 75,721 hrs · 31,216 cycles

REMOVE AND REPLACE REPAIR IAW SRM 57-10-00 FIG 68. FABBRICATED PART IAW DETAIL PART TRAVELER N01231 AND SRM 57-10-00 FIG 68. REMOVE AND REPLACE REPAIR IAW SRM 57-10-00 FIG 68. FABBRICATED PART IAW DETAIL PART TRAVELER N01231 AND SRM 57-10-00 FIG 68.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

CTR CARGO COMPT, CRACK 2 INCHES LONG ON L44 RT AT STA 1671. REMOVED CHANNEL AND RAI IAW SRM 51-21-01 PAGE 34/41 VOL1. REMOVED INTERCOSTAL BTWN STA 1681 AND 1701. REMOVED FASTENERS ON FLOORBEAM IAW SRM 51-33-01 PAGE 36/41 AND 51-35-01 PAGE 1/13 VOL 2. CUT SHEAR CLIP AND CAP FRAME IAW SRM 51-35-01 PAGE 1/13 VOL2 AND SRM 53-30-00 FIG 10 VOL1 FABRICATED PART IAW DETAIL PART TRAVELER N/RN00109 AND SRM 53-30-00 FIG 5 VOL1. REPLACED LONGERON P/N AFA 3040U1 REINSTALLED REMOVED PARTS AND NEW SPLICES IAW SRM 53-30-00 FIG 5 VOL 1 AND SRM 51-35-01 PAGE 1/13 VOL 2.

Part: SKIN — UNKNOWN (FLAP) · airframe 75,721 hrs · 31,216 cycles

RT WING, OUTBD FLAP AT XOF 722,235 UPPER SKIN HAS A DOUBLER REPAIR (5.5" BY 2.5"). REMOVED AND REPLACED REPAIR IAW SRM 57-00-01 FIG 4. FABRICATED PART IAW SRM 57-00-01 DETAIL PART TRAVELER N01218 AND IAW SRM 57-00-01.

Part: UNKNOWN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

MAIN CABIN FOUND FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 9 LT AND 14 LT. REPLACED FASTENERS IAW SRM 53-30-00 FIG 05 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING L/E FOUND 1 CRACK 5 INCHES LONG ON EXT SKIN AND 1 CRACK .50 INCH ON TEE ANGLE INT SIDE AT STA XORS 511(SEE NRC N00324). REMOVED DOOR AND FASTENERS TO GAIN ACCESS IAW SRM 51-31-01 PAGE 36/41. PERFORMED HFEL INSP IAW NDI SPM 06-20-01 FOUND CRACK. REMOVED INTERNAL WEB AND RIVET SKIN AND RIB IAW SRM 51-35-01 PAGE 1/13. REMOVED TEE IAW DWG ARB 1137 AND SRM 51-35-01 PAGE 1/13 SRM 51-33-01 PAGE 34/47. FOUND P/N ARB1187-7 RIB BROKEN, REMOVED SLAT NR 4LH IAW MM 27-80-01-4. REPLACED DAMAGED HARDWARE IAW MM 27-80-01-4 AND INSTALLED SLAT NR 4 LT IAW MM 27-80-01-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

RIGHT WING FIXED L/E SKIN LOWER SIDE AT XOS 610, NEAR REFUELING DOOR CUTOUT CORNER HAS A REPAIR DOUBLER 5 X 2 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 51-30-00 VOL 2, FABRICATED PART IAW DETAIL PART TRAVELER N01230 AND SRM 51-30-00.

Part: SKIN — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING L/E EXT SKIN FOUND 1 CRACK .50 INCH LONG AT STA XORS558 (SEE NRC N00325). REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT1 VOL1. FABRICATED PART IAW DETAIL PART TRAVELER NR 324 AND IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1.

Part: SKIN — UNKNOWN (LT WING FLAP) · airframe 75,721 hrs · 31,216 cycles

LEFT WING OUTBOARD FLAP, LOWER SKIN AT STA XOF 722 HAS AN EXTERNAL DOUBLER REPAIR (23" BY 15"). REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 85 SHEET 1 2 3 4 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01212-3 DOUBLER IAW SRM 57-10-00 FIG 85 VOL 1.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND 1 FLUSH REPAIR (DIM2" BY 2") FROM STA1801 TO STA 1821 BETWEEN L =43 RT AND L=45 RT. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 6 VOL4. FABRICATED PART IAW DETAIL PARTS TRAVELER N01185 AND IAW SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — DAMAGED (RT WING) · airframe 75,721 hrs · 31,216 cycles

RIGHT WING FIXED L/E SKIN LOWER SIDE, AT STA XOS 912 HAS A REPAIR DOUBLER 5.5 X 4 INCHES. REMOVED REPAIR IAW SRM 57-30-00 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER N01228 AND IAW SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

LT WING FIXED LOWER SIDE, STA XORS 50 AT SLAT TRACK NR 1 CUT OUT, FOUND AN EXTERNAL REPAIR DOUBLER (7.5 BY 5). REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 68 VOL1. FABRICATED PART IAW DETAIL PART TRAVELER N01201 AND IAW SRM 57-10-00 FIG 68 VOL 1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 75,721 hrs · 31,216 cycles

FOUND EXISTING FRAME REPAIR (35"X 5") AT STA 449 FROM X=-22. REPLACED 4EA SPLICES WITH NEWS P/N F177133-3-5-7-9 PER SRM 53-00-01 VOL 1 FIG 8. REPLACED CLIP P/N ABA7366-21 IAW SRM 51-35-01 VOL 2 PG 1/13. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01133 AND IAW SRM 53-00-01 VOL 1 FIG 8 AND IAW SRM 51-35-01 VOL 2 PG 1/13.

Part: REPAIR — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

FOUND EXISTING DOUBLER AND ANGLE REPAIR ON SKIN AND FRAME AT STA 330 LT SIDE. PERFORMED GVI ON DOUBLER AND FRAME REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1 INITIAL INSPECTION PERFORMED IAW EA #8-5330-95700.

Part: RIB — CRACKED (RT WING) · airframe 75,721 hrs · 31,216 cycles

RT WING L/E FOUND CRACK .50" LONG ON RIB INSIDE L/E AT STA XOS 969. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1.

Part: BULKHEAD — CRACKED (BS 490) · airframe 75,721 hrs · 31,216 cycles

FOUND 4 CRACKS 0.50" LONG NLG W/W ON LT BULKHEAD UNDER HEAD RIVETS AT STA 490.250. REPAIRED NOSE GEAR SUPPORT BEAM WEB IAW SRM 53-30-00 FIG 4-6-8 VOL 1. INTEGRATE IN THIS REPAIR ALSO 3 CRACKS REPORTED ON NRC N00680/F176680.

Part: FRAME — WORN (BS 590) · airframe 75,721 hrs · 31,216 cycles

AIR COND COMPT LT SIDE DEEP WEAR ON FRAME AT STA 590 X 63. TRIMMED OUT WORN SECTION OF FRAME, INSTALLED REPAIR DOUBLER IAW SRM 53-30-00 FIG 4 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F176660-3 REPAIR DOUBLER IAW SRM 53-30-00 FIG 4 AND 4A VOL 1.

Part: BULKHEAD — DAMAGED (BS 579) · airframe 75,721 hrs · 31,216 cycles

FOUND 1 CRACK NLG W/W 0.50" LONG ON LT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 579. REPAIRED NLG W/W WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176651/N00651.

Part: BULKHEAD — CRACKED (BS 579) · airframe 75,721 hrs · 31,216 cycles

FOUND 1 CRACK NLG W/W 0.50" LONG ON RT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 579. REPAIRED NLG W/W WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176650/N00650.

Part: RIB — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

FOUND 1 CRACK LT WING L/E INT SIDE 0.25" LONG ON RIB AT STA XORS 727. REPAIRED FORMER IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F176276/N00276 AND IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1.

Part: REPAIR — NONE (NONE) · airframe 75,721 hrs · 31,216 cycles

AFT CAC BULKHEAD STA 1159 FOUND DOUBLER AT X-83 AND DOUBLER AT X-84. PERFORMED GVI ON BULKHEAD CAC FOUND IN COMPLIANCE WITH CRITERIA BY EO #8-5100-7-5001 P1, INITIAL INSPECTION PERFORMED IAW EA NR 8-5330-95700.

Part: RIB — CRACKED (RT WING) · airframe 75,721 hrs · 31,216 cycles

FOUND RT WING L/E CRACK 0.50" LONG ON RIB INSIDE L/E AT STA XORS 643. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1.

Part: REPAIR — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

FOUND EXISTING DOUBLER AND ANGLE REPAIR ON SKIN AND FRAME AT STA 339 LT SIDE. PERFORMED GVI ON DOUBLER AND FRAME REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO #8-5100-7-5001 P1. INITIAL INSPECTION PERFORMED IAW EA NR 8-5330-95700.

Part: REPAIR — UNKNOWN · airframe 75,721 hrs · 31,216 cycles

FOUND EXISTING DOUBLER AND ANGLE REPAIR ON SKIN AND FRAME AT STA 321 LT SIDE. PERFORMED GVI ON DOUBLER AND FRAME REPAIR FOUND IN COMPLIANCE WITH CRITERIA BY EO NR 8-5100-7-5001 P1. INITIAL INSPECTION PERFORMED IAW EA #8-5330-95700.

Part: BULKHEAD — CRACKED (BS 1501) · airframe 75,721 hrs · 31,216 cycles

CLG W/W SPACE CRACK 1 INCH LONG ON RT VERTICAL BULKHEAD AT STA 1501 Z-37. PERFORMED HFEL INSP IAW NDT SPM 06-10-01 FOUND CRACK 1.3/8" LONG. TRIMMED OUT CRACKED PORTION ON WEB. REPAIRED IAW SRM 53-00-01 FIG 10 SHT 4 VOL 1. REMOVED AND INSTALLED NEW FITTING IAW DWG AEA0161. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176452-3 DOUBLER AND F176452-5 FILLER AND F176452-7 FILLER AND F176452-9 TAPERED FILLER IAW SRM 53-00-01 FIG 10 SHT 6 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 75,721 hrs · 31,216 cycles

RT WING L/E FOUND CRACK 1" LONG ON RIB INSIDE L/E AT STA XOS 923. REMOVED FASTENERS IAW SRM 51-33-01 PAGE 34-41. WRONG PART ARRIVED FROM BACKSHOP SCRAPPED WRONG PART. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176397-3A. REPAIR ANGLE AND F176397-6 FILLER IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1. INSTALLED NEW ANGLE IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1.

Part: BULKHEAD — DAMAGED (BS 490) · airframe 75,721 hrs · 31,216 cycles

FOUND CRACK NLG W/W 0.50" LONG ON RT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 490.250. REPAIRED NOSE GEAR SUPPORT BEAM WEB IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING L/E INT SIDE FOUND CRACK 0.25" LONG ON RIB AT STA XORS 884. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 39 SHT 2 SECTION B-B VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F176275/N00275 AND IAW SRM 57-10-00 FIG 39 SHT 2 SECTION B-B VOL 1.

Part: WEB — CRACKED (BS 2075) · airframe 75,721 hrs · 31,216 cycles

APU COMPT INT CRACK 1" LONG ON HORIZONTAL WEB AT STA 2075 X 29. TRIMMED OUT DAMAGED PORTION OF WEB AND INSTALLED REPAIR FILLER FORMED DOUBLER IAW SRM 53-00-01 FIG 8 SHT 1, FAB PART IAW DETAIL PART TRAVELER F176854-3 FILLER AND F176854-5 DOUBLER IAW SRM 53-00-01 FIG 8 SHT 1 VOL 1.

Part: REPAIR — UNKNOWN (BULKHEAD) · airframe 75,721 hrs · 31,216 cycles

LEFT MLG W/W 3EA CRACKS ON OLD REPAIR INBOARD BULKHEAD FROM STA 1471 TO STA 1481 Z-60. REMOVED EXISTING REPAIR IAW SRM 51-35-01 PAGE 1 VOL 2. PERFORMED INSP IAW NDI SPM06- 10-02 CONFIRMED SIGNED CRACK ON INSP AREA. ENLARGED CUT OUT TO ENG LOBE CRACK AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-01 FIG 10 SHT 6 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F176453-3 DOUBLE IAW SRM 53-00-01 FIG 10 SHT 6 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 75,721 hrs · 31,216 cycles

LT WING T/E FOUND 1EA CRACK 0.25 INCH LONG ON SKIN OF ISLAND LOWER SKIN AT STA XORS 486. TRIMMED OUT DAMAGED AREA AND REPAIRED SKIN IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176333-3 FILLER AND F176333-5 REPAIR DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: GEARBOX — CRACKED (NR 2 ENGINE) · airframe 74,747 hrs · 30,699 cycles

AT B - 9 CHECK TROUBLESHOOTING OIL LEAK ON NR 2 ENGINE S/N 451280, FOUND ACCESSORY GEARBOX, FUEL PUMP DRIVE PAD, HAD A 4 INCH CRACK, EMANATING FROM DRIVE PAD. DOCUMENTED ON B - 9 CHECK WORK PACKAGE, WORK ORDER 28833, NR 108. ENGINE REPLACED ON SEQ 324 WORK CARD. ENGINE OIL LEAK/CONSUMPT/SERVICE. CLOSED

Part: SKIN — CRACKED (ZONE 700) · airframe 74,300 hrs · 30,481 cycles

LT MLG DOOR HAS CRACKED SKIN AND DAMAGED HINGE FITTINGS PN.

Part: CONTROL UNIT — WILL NOT TEST (ZONE 700) · airframe 73,116 hrs · 29,872 cycles

ANTI-SKID FAILS (MULTIPLE REPEATS). REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING. FOUND SHORT AT RECEPTACLE R5-264. REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTI-SKID CONTROL UNIT FAULTY. REPLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD. INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWPM 20-31-03.

Part: CONTROL UNIT — FAILED (ZONE 700) · airframe 73,116 hrs · 29,872 cycles

ANTISKID FAILS (MULTIPLE REPEATS) REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING, FOUND SHORT AT RECEPTACLE R5-264, REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTISKID CONTROL UNIT FAULTY, REPLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD, INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWPM 20-31-03.

Part: DRUM — WRONG PART (ZONE 500) · airframe 73,116 hrs · 29,872 cycles

LT SLAT DRIVE MECHANISM FOLLOWUP CABLW DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACE DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSION CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2. FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC-10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1.

Part: SKIN — ERODED (ZONE 600) · airframe 73,116 hrs · 29,872 cycles

RIGHT HAND OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUT OUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1.

Part: SKIN — WORN (LT AILERON) · airframe 73,116 hrs · 29,872 cycles

LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 TO 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1.

Part: SKIN — CRACKED (ZONE 600) · airframe 73,116 hrs · 29,872 cycles

RT OUTBOARD AILERON INBOARD SUDE HAS SKIN SEPERATING AND CRACKED. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 TO 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSIN CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC-10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1.

Part: MOUNT — OUT OF POSITION (NR 3 ENGINE) · airframe 73,116 hrs · 29,872 cycles

NUMBER 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2.

Part: SKIN — WORN (LT WING AILERON) · airframe 73,116 hrs · 29,872 cycles

LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519.

Part: SKIN — CRACKED (ZONE 600) · airframe 73,116 hrs · 29,872 cycles

RT OUTBOARD AILERON INBOARD SIDE HAS SKIN SEPARATING AND CRACKED. VERIFIED MATERIAL ID FOR SKIN .032 INCH 2024-T3 PO 427557.2 AND DOUBLER .040 INCH 2024-T3 PO 434977.1 IAW DC-10 SRM 57-51-01 VOL 3. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 73,116 hrs · 29,872 cycles

NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVED DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AND DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB7025-13 IAW DRAWING AUB7025 AND AUB7034.

Part: DRUM — WRONG PART (SLAT DRIVE) · airframe 73,116 hrs · 29,872 cycles

LEFT HAND SLAT DRIVE MECHANISM FOLLOW UP CABLE DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACED DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9.

Part: ALTIMETER — MALFUNCTIONED (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOVED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1-1009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD.

Part: ALTIMETER — MALFUNCTIONED (ZONE 200) · airframe 73,116 hrs · 29,872 cycles

FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOVED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1-1009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD.

Part: SKIN — ERODED (ZONE 600) · airframe 73,116 hrs · 29,872 cycles

RT OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUTOUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1.

Part: MOUNT — WORN (ZONE 400) · airframe 73,116 hrs · 29,872 cycles

NR 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2.

Part: MOUNT — CORRODED (ZONE 400) · airframe 73,116 hrs · 29,872 cycles

NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVE DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AND DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB7025-13 IAW DRAWING AUB7025 AND AUB7034.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 69,967 hrs · 28,442 cycles

CLIMBING THROUGH FL200 THE NR 1 GEN OFF LIGHT CAME ON (AFTER LOSING THE NR 3 GEN ON T/O) RAN RED TABS. DISCONNECTED NR 1 GEN. TRIED UNSUCCESSFULLY TO START APU AT FL240, FL230, FL150, FL10. RETURNED TO MEM. APU STARTED ON TAXI IN. GROUND RAN ENGINES IAW DC-10 JRH CHAPT 5A. PERFORMED ENGINE GEN TEST IAW DC-10 JRH CHAPT 8. ALL TESTS PASSED. CHECKED SERVICE ON NR 1 CSD, CHECKS GOOD. STARTED APU 4 TIMES ON GROUND IAW DC-10 JRH CHAPT 3. ALL STARTS CHECKED GOOD. NO FAULTS FOUND AT THIS TIME. OK FOR CONTINUED SERVICE.

Part: MEC — FAILED (NR 2 ENGINE) · airframe 68,749 hrs · 27,850 cycles

ON DESCENT NR 2 ENG PWR LEVER FAILED TO CONTROL ENG PWR. SHUTDOWN ENG. REMOVED AND REPLACED NR 2 MAIN ENG CONTROL, FUEL PUMP, FUEL FILTER PER MM.

Part: FIRE LOOP — CHAFED (NR 2 ENGINE FAN)

00-362 DURING NR 2 ENGINE START, VALVE CLOSED. WE A GOT FIRE INDICATION ON NR 2 B-LOOP. R&R BOTTLE AND CLEANED CONNECTOR PLUG P1-8004 & P1-8006. R&R FAN FIRE DETECTOR LOOP A+B ASSY. CANNON PLUG P1-1255 NEEDS TO BE REPLACED.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AFTER T/O, RIGHT MAIN UNSAFE LIGHT WITH GEAR UP. COMPLIED WITH APPROPRIATE CKLIST, RT GEAR REMAIN UNSAFE UP. *S/D* REMOVED AND REPLACED SHEARED UPLOCK TARGET GEAR SWING AND OPS CK GOOD.

Part: CHANNEL — CORRODED (CARGO COMPT)

CENTER CARGO COMPT SUMP O/RAIN BILGE AREA. FOUND CORROSION ON WEB FROM STA 1741 TO STA 1788 STRG 49 RT. REMOVED FASTENERS AND CUTTED CHANNEL AT STA 1741. REMOVED CORRODED SECTION, REMOVED CORROSION, METAL PICK-UP WITHIN LIMITS ON WEB AND STRUCTURE AND TREATED PER SRM 51-21-01 AND SRM 53-00-01. INSTALLED 3 NEW CHANNEL SECTIONS WITH SPLICE PLATES AND FILLERS PER SRM 51-31-01 AND SRM 51-00-01. INSTALLED WITH NEW FASTENERS OVERSIZED. (JUNE 9, 1998)

Part: FLOOR — CRACKED (BS 1149)

N1326 STA-VCE: UPPER FUSELAGE INTERNAL RT SIDE, AT STA 1149 FOUND 2 EA CRACKS 2 LONG ON FLOOR WEB L27. REMOVED CRACKED FLOOR WEB AND REPLACED WITH A NEW ONE IAW SRM 51-41-01 AND 51-35-01. (11 JUNE 1998).

Part: SKIN — CORRODED (CARGO DOOR)

STA-VCE AFTER SCUFF PLATE REMOVAL ON LOWER CENTER CARGO DOOR IAW NRC N0933/F009933, FOUND LARGE AREA WITH SPREAD SEVERE CORROSION FROM STA 1701 TO STA 1781. MAJOR REPAIR PERFORMED REPAIR BY REPLACEMENT OF DAMAGED SKIN AND SPLICED IAW SRM 53-20-00, FIG 6. REMOVED CORROSION AND TREATED SKIN WITHIN ALLOWABLE LIMITS IAW SRM 51-21-01 AND 53-00-01 FIG 4. INSTALLED SCUFF PLATE.

Part: LONGERON — CRACKED (BS 2092)

STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 4 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998).

Part: LONGERON — CRACKED (BS 2092)

N1087 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 5 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-0. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998).

Part: LONGERON — CRACKED (BS 2092)

STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 9 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20 FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998).

Part: LONGERON — CRACKED (BS 2092)

N1088 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 8, LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998).