N556FE

Part: ENGINE — STALLED (LEFT) · airframe 90,860 hrs · 35,924 cycles

ON CLIMBOUT, PASSING FL 290 FELT 2 FIRM JOLTS WITH YAW TO THE LT ENG INDICATIONS NORMAL IN COCKPIT. FELT LIKE COMPRESSOR STALL ON NR 1 ENG. ENG RPM'S AT THE TIME WERE ATS CET 101 PERCENT. REMOVED AND REPLACED NR 3 ENG. LEAK AND OPS CHECKED GOOD. ACFT OK FOR FLIGHT.

Part: CONNECTOR — UNSECURE (R1 SLIDE) · airframe 90,571 hrs · 35,777 cycles

R1 DOOR SLIDE LIGHT DOES NOT TEST. RESEATED CONNECTOR ON BACK OF PRESS TO TEST SWITCH R1 DOOR. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 90,404 hrs · 35,689 cycles

DURING CRUISE, NR 2 ENG OIL QTY STARTED DROPPING 1 GAL EVERY 8 MIN. WHEN QUANTITY HIT 3 AND AMBER, WE ALSO GOT AN ENG 2 OIL PRESSURE LOW ALERT AND IT STAYED ON WITH ENG THROTTLE AT IDLE. SHUTDOWN ENGINE IAW QRH. CREW VERBAL ON DEBRIEF: ENGINE WAS ALREADY AT IDLE WHEN LOW OIL PRESSURE ALERT CAME ON. TIME LOW OIL ALERT WAS ON, WAS LIMITED TO QRH RUN TIME. VERIFIED AT OIL QTY IS LOW BY MORE THAN 10 QTS. FOUND A LARGE QTY OF OIL COLLECTED IN CTR AFT BODY AND COMING FROM BREATHER EXHAUST ON LT CORE COWL. OIL WAS ALSO STREAMING DOWN LT CORE COWL. SUSPECT LUBE AND SCAVENGE PUMP. IAW P/P, ENGINEER HAS APPROVED REMOVAL OF THE NR 2 ENGINE. REMOVED AND INSTALLED NR 2 ENGINE IAW WORKCARDS 71T1101 AND 71T1701. LEAK CHECK AND RUN CHECKS GOOD PER JRH. MAX POWER ASSURANCE RUN GOOD.OK FOR SERVICE.

Part: SHUNT — LOOSE (EMERGENCY POWER) · airframe 90,387 hrs · 35,679 cycles

EMERG PWR TEST FAIL ON PREFLIGHT EPCU FAULTS "BATTERY/INTFC" REF FIM 24-30-19. TERMINAL ON SHUNT S4-1 LOOSE AND ARCING. S4-1 REPLACED SHUNT S4-1, REF WDM 24-08-01, SHT 3 AND SWPM. ALSO R & R EPCU REF AMM. FINAL CLOSED.

Part: FRAME — CRACKED (PRESSURE BLKHEAD) · airframe 90,322 hrs · 35,643 cycles

CAC, FWD PRESSURE BULKHEAD RT SIDE MAIN FRAME CRACKED ALLTHE WAY THROUGH AT BS 1157 BETWEEN LONGERON 27R AND 28R. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS AND TREATED PARTS IN ACCORDANCE WITH EA 8-5310-142572. INSTALLED PARTS AND SEALED AS REQUIRED PER SRM 53-30-00.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 90,213 hrs · 35,584 cycles

DURING CRUISE FL360 F/O'S MCDU BLANKED OUT FOR APPROX 1 MINUTE THEN CAME BACK ON. THEN WE SMELLED ELECTRICAL FIRE/FUMES. PULLED F/O, MULTI-FUNCTION DISPLAY UNIT NR 2 CB RT EMERGENCY AC BUSS, ODOR/FUMES WENT AWAY. R & R THE MULTIFUNCTION CONTROL UNIT IAW THE AMM 31-65-01-4. TESTED GOOD IAW 31-65-01-5. NO ODORS. OK FOR CONTINUED SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 90,078 hrs · 35,519 cycles

EMERGENCY EXIT SIGNS INOP. RELEASED FOR SERVICE IAW MEL: 33-50-02, WHEN SHAKING HARNESS BY L1 DOOR LIGHTS COME ON, BUT UNABLE TO FIND EXACT CAUSE AT THIS TIME. REPLACED L1 DOOR "EXIT" LIGHT ASSY. ACCOMPLISHED ADJ AND TEST IAW MM 33-50-00-5.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 87,267 hrs · 34,098 cycles

LANDING MEM, 18R 3 UNSAFE (RED) GEAR LIGHTS WITH GEAR HANDLE DOWN, 3 UNSAFE ON CONFIG PAGE, QRH PROCEDURE DEPLOY ALT GEAR EXTENSION AND RECEIVED 3 GREEN SAFE (CONFIG AND GEAR). NOSEWHEEL STEERING RIGHT LIMITED TO 25 DEG.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 87,011 hrs · 33,971 cycles

CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS A CRACK ALONG UPPER EDGE ACROSS THREE RIVETS ENDING AT STIFFENER, FWD OF PNEUMATIC DUCT. (VERIFIED CRACK USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. SEE JPF WORK STEP SIGNOFFS.

Part: WEB — CRACKED (ZONE 700) · airframe 87,011 hrs · 33,971 cycles

CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS CRACK COMING FROM HOLE FOR THERMOCOUPLE. THIS CRACK HAS BEEN STOP DRILLED TWICE AND IS CRACKED PAST SECOND STOP DRILL. (VERIFIED CRACKED USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. WORK C/W PER JPF STEPS 1 THRU 10 FOR REPAIR OF CRACK.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,920 hrs · 32,966 cycles

CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 1521 LONGERON 50R TO 49R. REMOVED CORROSION ON T-CHORD IAW MD/DC10 SRM 51-21-01 VOL II PAGE 1, DAC DWG AEA 0018,ORIG. THICKNESS .200 REMAINING THICKNESS .177,.023 REMOVED. REMOVAL LIMITS OF T- CHORD ARE GOOD IAW EA 8-5310-112948. REMOVED AND REPLACED 4 END FITTINGS IAW MD/DC10 SRM 51-33-01 PAGE 1 VOL II AN 51-35-01 PGE 1 VOLII.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 15121, BETWEEN LONGERON 51L AND 52. REMOVED, REPLACED AND INSTALLED 2 EACH ANGLES AT 51L TO 52 AT FS 1521 IAW MD/DC10 SRM 51-33-01 VOL II PAGE 1.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON SHEAR TIE/LONGERON AT STA 15012 LONGERON 50L. REMOVED, FABRICATED AND INSTALLED NEW SHEAR-TIE/ FRAME IAW MD/DC10 SRM51-33-01 VOL II , 53-00-01 FIG 1B VOLI , 51-35-01 VOLII AND DWG AEA0273 REV G.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO1840. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW MD/DC10 SRM 51-31-01 VOLII AND 51-21-01 VOLII AND DWG AGA3855.

Part: SKIN — DENTED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

AFT SKIN DENTED AT APPROXIMATELY THE 5:00 POSITION ON FRAME AND IS 18 INCHES OF RVSM (CENTER PLATE). THIS SDR REPLACES (SDR#07-2123) REPAIRED SKIN IAW EA 8-55330-112937 FUSELAGE-SKIN REPAIR AT STA 851-913 L36R-L48R.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENTIAL ANGLE AT STA 152 LONGERON 50R TO 49R. REMOVED, FABRICATED AND INSTALLED 4 EACH ANGLES 49R TO 50R IAW MD/DC10 SRM 51-33-01 VOLII AND 51-35-01 VOLII PAGE 1.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 51L. REMOVED, FABRICATED AND INSTALLED NEW END FITTINGS IAW MD/DC10 SRM51-33-01 VOLII.

Part: SKIN — CORRODED (BS 1501-1521) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW MD/DC10 SRM 51-35-01 VOLII. SKIN REPLACED ON N/R N00616 EA8-5330-112939 (FUSELAGE SKIN REPAIR AT STA 1381- 1531, L48L-L48R REPAIR) W/O 36633,"SDR" 07-2147.

Part: SKIN — CORRODED (ZONE 700) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-10 SRM 51-35-01 VOL II.

Part: INTERCOSTAL — CORRODED (BS 1381-1401) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON INTERCOSTAL ABOVE LONGERON 52 R STA 1381 TO 1401. REMOVED AND REPLACED INTERCOSTAL IAW DC/MD-10 SRM 51-33-01 VOL II.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.

Part: LONGERON — CORRODED (ZONE 700) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CORROSION ON LONGERON END FITTING AT STA 1521, L48R CLG WHEEL/WELL. REMOVED AND REPLACED LONGERON END FITTINGS L48R IAW DC-10/MD-10 SRM 51-35-01 VOL. II.

Part: LONGERON — CORRODED (ZONE 700) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON LONGERON END FITTING STA 1501 TO STA 1521 LONGERON 51L TO 52L REMOVED AND REPLACED LONGERON END FITTING L52R IAW DC/MD-10 SRM 51-33-01 VOL II.

Part: LONGERON — CORRODED (ZONE 700) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

FOUND CORROSION ON LONG END FITTINGS AT STA 1521 LONG 48L CLG WHEEL WELL. REMOVED AND REPLACED L48L END FITTINGS IAW DC/MD-10 SRM 51-33-01 VOL. II.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.

Part: LONGERON — CORRODED (BS 1501-1521) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L REMOVED CORROSION ON LONGERON END FITTING AND FOUND TO BE WITHIN LIMITS IAW DC/MD10-10 SRM53-00-01 FIG 1B VOL 1. ORIGINAL THICKNESS 0.130" MATERIAL LOSS 0.007", MATERIAL REMAINING 0.123". ALODINED PRIMED AND PAINTED FITTING IAW DC/MD10-10 SRM 51-21-01 VOL 2.

Part: LONGERON — CORRODED (BS 1501-1521) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1, AND 51-35-01 VOL 2. FABRICATED LONGERON SECTION AND REPAIR SPLICES IAW MD10-10 SRM 53-00-01 FIG 9 VOL 1, AND 51-21-01 VOL 2.

Part: LONGERON — CORRODED (BS 1501-1521) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9 VOL 1, AND 51-35-01 VOL 2. FABRICATED LONGERON SECTION AND REPAIR SPLICES IAW MD10-10 SRM 53-00-010 FIG 9 VOL 1 AND 51-21-01 VOL 2.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,916 hrs · 32,965 cycles

MAIN CABIN SEAT TRACK AT RBL - 8 AT STA 1199 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. FABRICATED SEAT TRACK AND SPLICE REPAIR IAW DC/MD 10 SRM 53- 70-00 VOL I FIG 5. INSTALLED IAW DC/MD 10 SRM 51-31-01 VOL II.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,916 hrs · 32,965 cycles

MAIN CABIN SEAT TRACK AT RBL-27, AT STA 1059 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PGS 1-6A AND DC/MD 10 SRM 51-21-01 VOL II PGS 1-46.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,916 hrs · 32,965 cycles

MAIN CABIN SEAT TRACK AT LBL - 8 BETWEEN STA 1681 AND 1701 IS GOUGED BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PG 3. FABED SEAT TRACK AND 2 SPLICE HAT AND 2 PLATES IAW DC/MD 10 SRM 53-70-00 VOL I PG 3.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG - WHEEL WELL CAVITY,CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 152, LONGERON 50R TO 49R. [07-17-07] REMOVED,FABRICATED AND INSTALLED 4 EACH END FITTINGS 49R TO 50R IAW SRM 51-33-01 VOL II AND 51-35-01 VOL II PAGE 1.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 1521, BETWEEN LONGERON 51L AND 52. [07-17-07] REMOVED,FABRICATED AND INSTALLED IAW SRM 51-33-01.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE CIRCUMFERENTIAL ANGLE AT STA.1521, BETWEEN LONGERON 52 AND 51R. [07-13-07] REMOVED INTERCOSTAL AT LONG 51R, FS 1501-1521 IAW SRM 51-33-01 VOL2 PG1. REMOVED CORROSION ON TEE CHORD FS 1521 FROM LONG 51R-52R IAW SRM 51-21-01 PG1 VOL2 AND DAC DWG AEA0018. ORIGINAL THICKNESS 0.200", MATERIAL LOSS 0.032" REMAINING THICKNESS 0.168", FOUND TO BE WITHIN LIMITS IAW FEDEX EA 8-5310-112948 (FUSELAGE - STA 1521 BULKHEAD TEE CAP REPAIR). INSTALLED INTERCESTAL ON L51R FS 1501-1521 IAW SRM 51-33-01 VOL2 PG 1 & 51-35-01 VOL2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L. [07-13-07] REMOVED LONGERON 49L END FITTING IAW DC/MD10-10 SRM 51-33-01 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. ORIG THICKNESS 0.130", MATERIAL LOSS 0.007", REMAINING THICKNESS 0.123", FOUND TO BE WITHIN LIMITS IAW SRM 53-00- 01 FIG 1B, VOL 1 AND SRM 51-21-01 VOL 2. REINSTALLED LONGERON 49L END FITTING IAW SRM 51-33-01 VOL 2.

Part: SKIN — DENTED (ZONE 900) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

DENT IN FUSELAGE SKIN FWD OF R-1 DOOR SILL. REMOVED DENT, FABRICATED AND INSTALLED SKIN AND FILLER IAW DC/MD10 SRM 53-20-00 VOL I FIG 6 SHT 4, 53-10-00 VOL II PAGE 75 AND 53-20-00 VOL I PAGE 23.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR SURFACE AT STA 1441, LONGERON 51R TO 51L. SKIN SECTION FROM 1401 TO 1541 IS BEING REPLACED ON N/R N00616 ATTACHED EA 8-5330- 112939/FUSELAGE-SKIN SPLICE AT STA.1381-1531,L48LTO L48R-REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE SKIN BETWEEN LONGERON 51L AND 52 STA 1350 TO 1370. CLEANED AREA IAW DC/MD10 SRM51-21-01 PARA.22 VOL. II. NO CORROSION NOTED. MECH 7951 QC281

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CORROSION ON LONGERON 52 STA 1461 TO 1501,CLG WHEEL WELL CAVITY. [07-13-07] FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 51-33-01 VOL 2. FABRICATED NEW LONG SECTION IAW DAC DWG A4B7013 REV AC, AND REPAIR SPLICES IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1. REMOVED AND REPLACED CORRODED LONGERON SECTION WITH NEW SECTION AND SPLICES IAW MD10-10 SRM 51-33-01 VOL 2.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CLG WHEEL WELL CAVITY, CORROSION ON LONGERON 51R STA 1441 TO 1501. [07-13-07] FOUND TO BE WITHIN LIMITS IAW MD10-10 SRM 53-00- 01 VOL 1 , ORIGINAL THICKNESS 0.150, MATERIAL LOSS 0.010, REMAINING MATERIAL 0.140. SAT 1481 - 1521 FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL1, MATERIAL LOSS 0.045, REMAINING MATERIAL 0.105. FABRICATED LONGERON SECTION IAW DAC DWG A4B7013 REV AC, FABRICATED REPAIR SPLICE IAW MD10-10 SRM 50-00-01 FIG 9, VOL 1. INSTALLED REPAIR IAW MD 10-10 SRM 51-35-01 VOL 2.

Part: ANGLE — DENTED (ZONE 100) · airframe 84,916 hrs · 32,965 cycles

UPON REMOVAL OF LOWER TORQUE BOX WEB FOR SKIN REPLACEMENT ON N/R N00337, FOUND INNER CHORD ANGLE ADA0055-7 DENTED AT STA 886 JUST ABOVE L41 RIGHT. [07-17-07] REPAIRED PER EA 8-5310-112940.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CENTER LANDING GEAR WHEEL WELL,CORROSION ON FUSELAGE SKIN AT STA 1501 TO 1521, LONGERON 51R TO 50R. [07-17-07] REPLACED ON N00616 WITH EA 8-5330-112939.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CORROSION ON FUSELAGE SKIN INTERIOR AT STA 1441 TO 1481, LONGERON 50L TO 50R, CENTER LANDING GEAR WHEEL WELL CAVITY. [07-13-07] REMOVED AND REPLACED SKIN WITH NEW SECTION FS1391-1521, LONGERON 48L - 48R IAW FEDEX EA 8-5330-112939 (FUSELAGE SKIN REPAIR AT STA 1381 - 1531, L48L - L 48R - REPAIR)

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

LT O/B AILERON BULGING AT FASTENERS ON SKIN. [07-17-07] REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II . MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO 1840. [07-17-07] REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-31-01 VOL II, 51-21-01 VOL II AND DWG. 3855. MINOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · corrosion level 2 · airframe 84,916 hrs · 32,965 cycles

AFT SKIN DENTED AT APPROXIMATELY 5:00 POSITION ON FRAME AND IS WITHIN 18 INCHES OF RVSM (CENTER) PLATE. [07-17-07] REPAIRED SKIN IAW EA 8-5330-112937 MAJOR REPAIR.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 82,449 hrs · 31,919 cycles

ON APPROACH TO MEMPHIS, LOWERED GEAR HANDLE BUT GEAR DID NOT LOWER. BOTH GEAR INDICATING SYSTEMS SHOWED UNSAFE ON ALL 3 GEAR. RECYCLED GEAR AND GEAR WORKED NORMALLY LANDING UNEVENTFULLY. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IN REFERENCE TO MD- 10-10 M/M32-31-03-2, RIGGED IN REFERENCE TO MD10-10 M/M 32-31-01-5, AND PERFORMED ADJUSTMENT TEST IN REFERENCE TO MD10-10 M/M 32-30-00-5. OPS AND LEAK CHECKS GOOD.

Part: STRUCTURE — GROUND DAMAGE (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

DURING GROUND OPERATIONS OAN ACCIDENTALLY DAMAGE EXT FUSELAGE BETWEEN 1059/1039 LONG 32/33 LT SIDE. THE DIMENSION OF DAMAGE IS L= 4.17" W=3" D=0.114". BLENDED DAMAGE IAW SRM 53-00-01 VOL1 FIG 1A SHEET 3. PERFORMED US INSP FOUND MATERIAL THK 0.53". REPAIRED AND CUT OUT THE DAMAGE IAE SRM 53-20-00 SHEET 2 THRU 5 FIG VOL 1.

Part: LONGERON — CRACKED (BS 1978) · airframe 82,219 hrs · 31,802 cycles

LOWER FUSELAGE AFT CARGO STA 1978 LONG 49 RT FOUND 1EA CRACK LONG ABOUT 1" ON UPPER FLANGE OF LONGERON. TRIMMED OUT CRACKED PORTION OF LONGERON INSTALLED 2EA FILLERS AND 1EA ANGLE WITH HI LOCKS AND 2EA BOLTS IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1, BOLTS INSTALLED IAW SRM 51-38-01 PAGE 2A AND PAGE 4.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

RT HORIZONTAL STAB CENTER SECTION ON SKIN PANEL UPPER AFT SIDE FOUND 1 REPAIR DOUBLER DIM 16" BY 11" BEWTEEN STA XE 72 AND STA XE 83. STRIPPED PAINT IAW SRM 51-21-01 PAR 32C VOL 2. PERFORMED NDT INSPECTION IAW NDT SPM 06-10-01.006 AND 04-00-06 REPAIR PREVIOUSLY ACCOMPLISHED BY DWG SR10550004. RESTORED PAINT IAW SRM 51-21-01 VOL 2.

Part: FITTING — NICKED (WING) · airframe 82,219 hrs · 31,802 cycles

DURING ACCOMPLISHED NRC N00197, AFTER REMOVAL FITTING P/N ARC0329-1 FOUND ON ANGLE FITTING (ATTACHED ON WING REAR SPARE) DEEP NICK (LONG 7/16" LARGE 1/4" DEEP 3/32"). FABRICATED AND INSTALLED 1 BUSHING AND 1 ANGLE ON DAMAGED T/E BEAM LOWER CAP IAW EA# 8-5710-88857.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

DURING REMOVAL OF THE SKIN, FOUND 1 CRACK 1.25" LONG ON TEE CAP AT STA 595 Z-63 LT SIDE. ACCOMPLISHED IAW EA NR 8-5310-88854.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

LWR FUS ON SKIN FOUND REPAIR DOUBLER BTW STA 1219 AND 1289 FROM LONG 51 RT TO LONG 51 LT. REMOVED EXISTING DOUBLER IAW SRM 51-35-01 PAR 1-5 STRIPPED PAINT FROM AREA IAW SRM 51-21-01 VOL 2. INSPECTION AREA IAW NDI INSTALLED CONICAL WASHER AND INSTALL NEW DOUBLER IAW EA 8-5330-93219 AND INSTALLED SHEAR CLIP P/N F14383/9 IAW SRM 53-30-00 FIG 9 VOL 1.

Part: REPAIR — PROPER (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

CENTRAL CARGO COMPT FOUND REPAIR DOUBLER ON JUMB DOOR AT STA 1701 X-102 Z-46 RT SIDE. STRIPPED PAINT FROM DOUBLER IAW SRM 51-21-01, PERFORMED NDI AND GVI. THE REPAIR REWORKED IAW SRM 53-50-00 FIG 12 VOL 1. REPROTECTED AREA IAW SRM 51-21-01 PAR 2 AND THE REPAIR FOUND IN COMPLIANCE WITH SRM 53-50-00 FIG 12 VOL 1.

Part: REPAIR — IMPROPER (BS 879) · airframe 82,219 hrs · 31,802 cycles

LWR FUSELAGE LT SIDE ON SKIN FOUND 1 REPAIR EXISTING AT STA 879 BETWEEN L48 TO L43 . REMOVED PORTION SKIN AT STA 850 TO STA 900 BETWEEN L36 TO L48 LT SIDE IAW SRM 53-20- 00 FIG 17 PER EA NR 8-5330-90128. FABRICATED AND INSTALLED P/N' S F148375/3; -5; -7; -9; -11; - 13, -15; -17 IAW SRM 53-20-00 FIG 17 SHT 1-3-4-5-6-7 EA NR 8-5330-90128. REMOVED DAMAGED SHEAR CLIP AND TEAR CLIP. FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-30-00 FIG 9 AND FIG 18 VOL 1.

Part: DOOR FRAME — DAMAGED (BS 1841) · airframe 82,219 hrs · 31,802 cycles

IN THE AFT CARGO COMPT FOUND EXISTING ANGLE STIFFENER ON JAMB DOOR BETWEEN L37 TO L41 AT STA 1841 LT SIDE. REMOVED GUARD SUPPORT STRIPPED POINT PERFORMED NDI ACCOMPLISHED EA NR 8-5310-93211, REPROTECTED AREA AND REINSTALLED GUARD SUPPORT IAW SRM 51-31-01 PAR 6 VOL 2.

Part: REPAIR — IMPROPER (BS 879-939) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND NR 3 SPLICE REPAIR ON LONG NR 52 BETWEEN STA 879-939. REMOVED SPLICE IAW SRM 53-10-00 VOL 1. STRIPPED PARTS IAW SRM 51-21-01. PERFORMED INSPECTION RESTORED PAINT IAW SRM 51-21-01 VOL 2. REINSTALLED PARTS IAW SRM 53-10-00.

Part: REPAIR — IMPROPER (BS 879-919) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND NR 2 SPLICE REPAIR ON LONG NR 51 BETWEEN STA 879-919 RT SIDE. REMOVED SPLICE AND PORTION LONGERON IAW SRM 53-10-00 VOL1 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. PERFORMED NDT INSPECTION RESTORED PAINT IAW SRM 51-21-01 VOL 2. REINSTALLED SPLICE AND PORTION LONGERON IAW SRM 53-10-00 VOL 1.

Part: SKIN — CORRODED (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

LOWER FUSELAGE ON SKIN PANEL FROM LONG LT TO LONG 48 RT: FOUND PITTING CORROSION BTW STA Y=1941 AND STA Y=1129. REMOVED CORROSION ON BELLY SKIN IAW SRM 51-21-01 PAR 33 PAG 26-27. REMOVED RESIDUAL CORROSION AND BLENDOUT AREA BTW LONG 50 TO LONG 50 IAW SRM 51-21-01 PAR 34. PERFORMED INSPECTION IAW NDI SPM 04. REPAIRED AREA IAW OUT OF LIMITS IAW SRM 53-40-00 FIG 14 VOL 1 AND IAW SRM 53-40-00 FIG 14 AND FIG 20 VOL 1. INSTALLED REPAIR CHANNEL, 13 AND FILLER IAW SRM 53-00-01 VOL1 FIG 7 AND FIG 9.

Part: SKIN — UNSECURE (LT WING) · airframe 82,219 hrs · 31,802 cycles

ACCESS PANEL LT WING P/N 525 AT FOUND SKIN UNGLUED. REBONDED AND REPAIRED PANEL IAW SRM 57-10-00 FIG 71 VOL 1 AND DWG ARB1111 DPS 1.07- 2 TYPE 2. FABRICATED PART IAW DETAIL PART TRAVELER N02362 AND SRM 57-10-00 FIG 71 VOL 1.

Part: REPAIR — UNKNOWN (BS 2122) · airframe 82,219 hrs · 31,802 cycles

UPPER AFT FUSELAGE COMPT STA 2122 ON LWR ANGLE OF BULKHEAD FOUND 1 ANGLE REPAIR AT X30. PERFORMED INSPECTION RESTORED HL 64-6 H/L IAW SRM 51-33-01 PG 34/47 VOL 2.

Part: REPAIR — IMPROPER (BS 1256) · airframe 82,219 hrs · 31,802 cycles

FOUND PASSENGERS DOOR 3 LT FOUND 1 EXISTING REPAIR ON FWD JAMB WEB AT STA 1256 BETWEEN LONG 26-27 LT SIDE. REMOVED EXISTING REPAIR, INSPECTED AREA, INSTALLED BUSHING REF EA NR 8-5310-92335. INSTALLED NEW DOUBLER P/N FC148913-3 PER SRM 53-50-00 FIG 19 VOL 1 AND EA NR 8-5310-92335.

Part: WEB — CORRODED (BS 350) · airframe 82,219 hrs · 31,802 cycles

COCKPIT AREA FOUND SEVERE CORROSION WITH EXFOLIATION ON WEB AT STA 350 X47 Z - 10.925. REMOVED CORROSION IAW SRM 53-00-01 VOL 1 FIG 1B, MATERIAL REMOVED IS OUT OF LIMIT CUT DAMAGED SECTION OF WEB IAW 53-00-01 FIG 10 SHT 4.

Part: SKIN — DENTED (BS 383-374) · airframe 82,219 hrs · 31,802 cycles

NOSE RT SIDE ON SKIN FROM STA 383 TO STA 374 UPPER LONG 36 FOUND 1EA DENT (LENGTH 1.65 INCH DEPTH 0.075 INCH) AND 1EA DENT (LENGTH 0.315'' DEPTH 0.028''). PERFORMED NDI INSPECTION NO CRACK FOUND. REFORMED DENT IAW SRM 51-10-00 AND FABRICATED DOUBLER IAW DETAIL PART TRAVELER F148061-3/N000061. INSTALLED INTERNAL DOUBLER IAW SRM 53-20-00 FIG 13 DET H.

Part: SKIN — CORRODED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING REAR SPAR AT STA XORS 338 FOUND CORROSION EXFOLIATION ON UPPER SKIN PANEL SUPPORT. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2 VOL 1.

Part: LONGERON — DAMAGED (BS 2122-2163) · airframe 82,219 hrs · 31,802 cycles

UPPER INTERNAL FUSELAGE AFT BODY FOUND NR1 LONGERON REPAIRED BETWEEN STA 2122 TO STA 2163 AT LONG 51 RT SIDE. REPAIRED IAW EA 8-5310-90131.

Part: SKIN — CORRODED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING REAR SPAR AT STA XORS 308 FOUND EXFOLIATION CORROSION IN THE UPPER SKIN PANEL SUPPORT. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 FOUND OUT OF LIMITS. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 82,219 hrs · 31,802 cycles

LT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3.

Part: SKIN — DENTED (BS 1009) · airframe 82,219 hrs · 31,802 cycles

LWR FUS RT SIDE ON SKIN: BTW LONG 37 AND LONG 38 FOUND AT STA 1009 NR 1EA DENT (LENGTH 1,063 INCH X DEPTH 0,082 INCH) AND AT STA 1006 FOUND 1EA DENT (DEPTH 0,161 INCH X LENGTH 2 INCH) BTW LONG38 AND LONG 39 AT STA Y=1007 FOUND NR1 DENT (LENGTH 1.57 INCH X DEPTH 0,102 INCH). REPAIRED SKIN IAW SRM 53-20-00 FIG 6 SHEET 3/4 VOL1.

Part: SKIN — DAMAGED (BS 1921-2007) · airframe 82,219 hrs · 31,802 cycles

LOWER FUSELAGE RIGHT SIDE ON SKIN BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT FROM STA Y= 1921 AT STA Y= 2007 FOUND NR 1 NEW SKIN PANEL WITH 200 SCREW AND ONE SPLICE REPAIR DOUBLER. CHECKED MATERIAL AND THK. THE REPAIR IS IN COMPLIANCE WITH SRM 53-20-00 FIG 17 SHEET 1 VOL 1.

Part: FLOORBEAM — CRACKED (BS 1256) · airframe 82,219 hrs · 31,802 cycles

MAIN CABIN INTERNAL FUSELAGE FOUND NR 1 CRACK LONG 2" ON FLOORBEAM AT STA Y= 1256 X= 107. REPAIRED WITH NEW SECTION OF FLOORBEAM AND SPLICE IAW SRM 53-00-01 FIG 9 VOL 1.

Part: SKIN — SCRATCHED (BS 1721-1741) · airframe 82,219 hrs · 31,802 cycles

UPPER FUSELAGE LT SIDE FOUND 1 SCRATCH (6" LONG ) ON SKIN BTWN AT STA Y= 1721 AND Y=1741 CLOSE OUT LONGERON 5. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 7 VOL 1.

Part: HINGE FITTING — GOUGED (TE FLAP) · airframe 82,219 hrs · 31,802 cycles

FLAP I/B FITTING HINGE OUTBOARD FOUND DEEP NICK ON INSIDE HOLES ACTUATOR AND LIGHT COROSION ON SURFACE AROUND OF THE HOLE. INSTALLED OVERSIZED BUSHING IAW CMM 57-52-01.

Part: SKIN — DENTED (BS 735-755) · airframe 82,219 hrs · 31,802 cycles

LOWER FUSELAGE NOSE LT SIDE FOUND NR 1 DENT (1.18" BY 0.067") ON SKIN AT BETWEEN STA Y=735 AND STA Y= 755 CLOSE OUT LONGERON 38. INSTALLED TITANIUM FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 7 VOL 1.

Part: SKIN — DENTED (BS 447) · airframe 82,219 hrs · 31,802 cycles

LOWER FUSELAGE NOSE LT SIDE FOUND NR 1 DENT (1.5" X 0.080") ON SKIN AT STA Y= 447. INSTALLED TITANIUM FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 5 VOL 1.

Part: FRAME — CRACKED (BS 469) · airframe 82,219 hrs · 31,802 cycles

AV COMPT FOUND NR 1 CRACK (1" LONG ) ON FRAME AT STA Y= 469 X= 75. INSTALLED FRAME REPAIR IAW SRM 53-30-00 FIG 5 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RIGHT WING FIXED LEADING EDGE AT STA XORS 672 ZONE 625 FOUND RIB CRACK. REPAIRED FORMER INSTALLED REPAIR CLIP ARB1291-38 AND SRM 57-20-00 FIG.1 SHEET 4, 6 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RIGHT WING FIXED LEADING EDGE AT STA XORS 655 ZONE 625 FOUND RIB CRACK. REPAIRED FORMER INSTALLED REPAIR ANGLE -36 AND SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 114 ZONE 515 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 2 VOL I, INSTALL REPAIR ANGLE -43.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 949 ZONE 627 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 5 AND 6 VOL I.

Part: SKIN — BUCKLED (BS 295-285) · airframe 82,219 hrs · 31,802 cycles

LWR FUSELAGE NOSE AREA LT SIDE FROM STA 295 TO 285 FOUND BUCKLING SKIN WITH NR 3 DENT (0.286"X1"), (0.176"X1"), (0.080"X1 1/4). INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 4.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 650 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 626 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 644 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 530 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 542 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 762 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I, INSTALL REPAIR ANGLE -35.

Part: FITTING — CRACKED (BS 1159) · airframe 82,219 hrs · 31,802 cycles

CAC FOUND ONE FITTING AT STA 1159 BETWEEN L=38 AND L=39 RT SIDE ONE CRACK 3 INCH LONG. REPAIR IAW SRM 53-40-00 FIG 8.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 522 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 512 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I, INSTALL REPAIR ANGLE -35.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 340 ZONE 618 FOUND RIB CRACK (4" LONG). REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 2 AND 3 VOL I.

Part: SKIN — DENTED (BS 879-899) · airframe 82,219 hrs · 31,802 cycles

LWR FUSELAGE RT SIDE ON SKIN FOUND DENT (1.2" BY 0.106") BETWEEN Y=899 AND Y=879 LONGERON 37-38. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 347 ZONE 518 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I , INSTALL REPAIR ANGLE -35.

Part: PANEL — CRACKED (BS 939-959) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND ONE SUMP PANEL BETWEEN Y=939 AND Y=959 LT SIDE WITH CRACK 2 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 4.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 632 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 510 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 644 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I , INSTALL REPAIR ANGLE -37.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 719 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 610 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 6737 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE L WING FIXED L/E COMPT AT STA XORS 917 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 5 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 735 ZONE 518 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 921 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET5 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 873 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 662 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I, INSTALL REPAIR ANGLE -35.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 660 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 789 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 755 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: LONGERON — CORRODED (BS 1781-1561) · airframe 82,219 hrs · 31,802 cycles

CNTR CARGO COMPT TUNNEL AREA LT SIDE FROM STA 1781 TO 1561 LONGERON 38 LT FOUND CORROSION. INSTALLED REPAIR LONGERON IAW SRM 53-10-00 FIG 2A SHEET 1, 2 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 933 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I.

Part: SKIN — CRACKED (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND ON STRUCTURE AT STA 1102 X= -57 RT SIDE QTY 1 CRACK LONG HALF INCH. SMOOTH AND BLENDED OUT CRACK IAW SRM 53-00-01 FIG 1A VOL 1. INSTALLED CHANNEL REPAIR IAW SRM 53-00-01 FIG 2 SHEET 2 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 917 ZONE 627 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 5 VOL I. INSTALL REPAIR ANGLE -36.

Part: WEB — CRACKED (ZONE 200) · airframe 82,219 hrs · 31,802 cycles

COCKPIT FOUND 1 CRACK 2" LONG ON WEB AT STA 304 X=-27 Z= -2.925 AND MODERATE CORRSION AT STA 313 X=-39 Z=-2.925. REMOVED CORROSION IAW SRM 51-21-01 AND PROTECT AREA IAW SRM 51-21-01. CUT DAMAGED PORTION OF WEB AND REPAIRED IAW SRM 53-00-01 FIG 4 SHEET 2.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

ACCESS PANEL LT WING 516ET FOUND 2 CRACK ON ANGLE INTERNAL SKIN. REMOVED EXISTING REPAIR AND REPAIR STIFFENERS IAW SRM 51-35-01 PAG 1-13 AND 51-33- 01 PAGE 34-47 AND SRM 57-10-00 FIG 23 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 731 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND ON FLOORBEAM AT STA 979 X=-97 RT SIDE CRACK LONG 1/2 INCH. CUT DAMAGED PORTION BEAM. REPLACED SECTION IAW SRM 51-35-01 PAGE 1-13 VOL II. REPLACED BRACKET ADA0144-27 AND REPAIRED IAW 53-00-01 FIG 9 SHEET 8.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 638 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I. INSTALL REPAIR ANGLE -38.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 559 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I.

Part: RIB — CRACKED (ZONE 300) · airframe 82,219 hrs · 31,802 cycles

LT HORIZ STAB TIP INTERNAL SIDE FOUND CRACK 1 INCH LONG ON RIB FROM THE EDGE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 688 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I. INSTALL REPAIR ANGLE -35.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 795 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

NOSE AREA RT SIDE BETW Y=285 AND Y=295 UNDER LONGERON 27 FOUND 1 DENT 0.512"X0.043") ON SKIN. REPAIRED DENT IAW SRM 51-10-00 VOL II. PERFORMED NDI INSPECTION: FOUND OK AND INST DOUBLER IAW SRM 53-20-00 VOL 1 FIG 13 SHEET 5.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 690 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 911 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I, INSTALL REPAIR ANGLE -35.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 815 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: SKIN — DENTED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LEFT WING LWR SURFACE INBOARD AILERON FOUND QTY 1 DENT AT STA XW 373. INSTALLED EXT DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

THE RIGHT WING FIXED L/E COMPT AT STA XORS 514 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 767 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 518 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1.3 AND 4 VOL I. INSTALL REPAIR ANGLE -38.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 600 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I. INSTALL REPAIR ANGLE -35.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED L/E COMPT AT STA XORS 761 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

IN THE RT WING FIXED L/E COMPT AT STA XORS 684 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36.

Part: SKIN — CRACKED (ZONE 300) · airframe 82,219 hrs · 31,802 cycles

LT HORIZ STAB LEADING EDGE INBOARD FOUND CRACK 2 INCH LONG ON OUTBOARD EDGE LWR SIDE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL III.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

IN THE RIGHT WING FIXED LEADING EDGE, AT XORS 347, ZONE 618, FOUND RIB CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-20-00, VOL I, FIG 1, SHT 1, 3 AND 4.

Part: SKIN — DENTED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING I/B FLAP STRUCTURE AT XIFH 195.300 TO XIFH 189.300 FOUND DENT IN THE LWR EXTERNAL SKIN DIAMETER 2.36 INCH BY .275 INCH DEEP AND FOUND DEFORMATION ON STRUCTURE. CUT DAMAGE SECTION OF SKIN; CHECKED AND REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I.

Part: SKIN — NICKED (ZONE 300) · airframe 82,219 hrs · 31,802 cycles

RT I/B ELEVATOR UPPER SURFACE FOUND NICK BETWEEN STA XE 225 AND XE 238. ACCOMPLISH EXTERNAL DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL I.

Part: CHANNEL — CORRODED (BS 959-979) · airframe 82,219 hrs · 31,802 cycles

FWD CARGO COMPT FOUND HEAVY CORROSION BETWEEN STA 959-979 WITH CRACK LONG 4 INCH. CUT DAMAGE SECTION ON CHANNEL AND REPAIRED IAW SRM 53-70-00 FIG 7 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

IN THE LT WING FIXED LEADING EDGE AT STA XORS 743 FOUND RIB CRACK. REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 AND INSTALLED REPAIR ANGLE.

Part: ACCESS PANEL — WORN (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-10-00 FIG 10A VOL I.

Part: ACCESS PANEL — WORN (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LEFT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 809 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 516 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING TIP AT XW 912 FOUND NR 1 RIB CRACK. ACCOMPLISH ANGLE REPAIR IAW SRM 57-00-01 FIG 3 SHEET 2 VOL I. REMOVED AND REINSTALLED PLUG ON WEB IAW SRM 51-41-01 FIG 5 VOL II.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 519 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 927 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET, 3, 5 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 1011 FOUND NR 1 RIB CRACK. ACCOMPLISHED FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 5, 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 594 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 821 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 504 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 656 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 677 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 694 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LEFT WING FIXED LEADING EDGE AT XORS 487 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 849 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 749 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3,4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 706 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 700 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 980 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 5, 6 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 509 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 531 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1SHEET 4, 6 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 638 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 860 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4; 6 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 402 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 615 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT STA 750 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.

Part: SKIN — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 469 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 454 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 490 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 352 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT STA XORS 768 FOUND NR 1 RIB CRACKED. REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4/6 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING L/E AT XORS 526 FOUND RIB CRACKED. ACCOMPLISHED WING OB EDGE FORMER REPAIR IAW SRM.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 485 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: FRAME — WORN (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

AIR COND COMPT LT SIDE FOUND WORN FRAME AT STA 588 X=64. TRIMMED WORN AREA AND REPAIR IAW SRM.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 457 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

THE RIGHT WING FIXED LEADING EDGE AT STA 756 FOUND NR 1 RIB CRACK. ACCOMPLISHED FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

THE RIGHT WING FIXED LEADING EDGE AT STA 816 FOUND RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LEFT WING FIXED LEADING EDGE AT XORS 452 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT STA XORS 810 FOUND NR 1 RIB CRACK. REPAIRED FORMER INSTALLED CLIP IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT STA XORS 936 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER, FILLER AND DOUBLER REPAIR IAW SRM.

Part: FASTENER — WRONG PART (ZONE 100) · airframe 82,219 hrs · 31,802 cycles

AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED IAW SRM.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 696 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 457 FOUND NR 1 RIB CRACK. INSTALLED FILLER IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 742 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 831 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 598 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT STA XORS702 FOUND NR 1 RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM AND REPAIR ANGLE.

Part: RIB — CRACKED (ZONE 600) · airframe 82,219 hrs · 31,802 cycles

RT WING FIXED LEADING EDGE AT XORS 733 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.

Part: STRUCTURE — DAMAGED (ZONE 200) · airframe 82,219 hrs · 31,802 cycles

MAIN CABIN INTERNAL FUSELAGE FOUND NR 2 HOLES DIAM. 0.25 INCH TOO CLOSE AT STA 1561, LONGERON 8 LT SIDE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM.

Part: RIB — CRACKED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING FIXED LEADING EDGE AT XORS 481 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR.

Part: SKIN — DENTED (ZONE 500) · airframe 82,219 hrs · 31,802 cycles

LT WING LOWER SURFACE ON IB AILERON: FOUND NR 1 DENT ( LENGTH 0.87 INCH ; DEPTH 0.094 INCH) AND FOUND NR 1 DENT (LENGTH 0.63 INCH ; DEPTH 0.027 INCH) AT STA XW 343 CUT DAMAGED PORTION OF LOWER SKIN AND REPAIRED IAW SRM.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 82,219 hrs · 31,802 cycles

UPPER FUSELAGE INTERNAL AFT BODY FOUND 1EA LONGERON REPAIRED BTW STA 2122 TO STA 2163 LONGERON 50 LT SIDE. REPAIRED IAW SRM 53-00-01 FIGURE 7 VOL.1.

Part: ATTACH ANGLE — DAMAGED (VERTICAL STAB) · airframe 82,219 hrs · 31,802 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE RT SIDE FOUND 1EA EXTERNAL DOUBLER REPAIR. REPAIRD IAW SRM 55-20-00 FIGURE 3 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 582. FABRICATED ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: SKIN — DAMAGED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING TIP FOUND 1EA EXTERNAL DOUBLER REPAIR ON EXTERNAL SKIN. REPAIRED IAW SB 57-27

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 82,219 hrs · 31,802 cycles

HORIZONTAL STAB CONSTANT SECTION FOUND 1EA DOUBLER REPAIR ON AFT BLKHD AT STA 2123 X=-40 RT SIDE. REPAIRED IAW SB 55A028 AND DWG SR10550007.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

DISCREPANCY: RH WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 470. CORRECTIVE ACTION: FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: SKIN — DAMAGED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING INB'D L/E FOUND 1EA EXTERNAL DOUBLER REPAIR ON SKIN AT XORS 87. REPAIRED IAW SRM 57-10-00 FIGURE 40 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 940. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1 EA ANGLE REPAIR ON RIB AT XORS 930. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB XORS 917. REPAIRED IAW SRM 57-00-01 FIGURE 3 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT;B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 567. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 460. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: SKIN — DAMAGED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING OUT'B L/E FOUND 1EA DOUBLER REPAIR ON SKIN AT XORS 506. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIGURE 68 VOL.1.

Part: BULKHEAD — DAMAGED (HORIZONTAL STAB) · airframe 82,219 hrs · 31,802 cycles

DISCREPANCY: HORIZONTAL STABILIZER CONSTANT SECTION FOUND 1EA DOUBLER REPAIR ON AFT BLKHD AT STA 2123 X=40 LH SIDE. CORRECTIVE ACTION: REPAIRED IAW SB 55A028 AND DWG SR10550007.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 577. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

DISCREPANCY: RH WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB XORS 572. CORRECTIVE ACTION: FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.

Part: RIB — DAMAGED (LT WING) · airframe 82,219 hrs · 31,802 cycles

LT WING L/E INTERNAL STRUCTURE FOUND 1 EA ANGLE REPAIR ON RIB XORS 577. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIG. 1 VOL.1.

Part: RIB — DAMAGED (RT WING) · airframe 82,219 hrs · 31,802 cycles

RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA REPAIR ANGLE ON RIB XORS 465. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1.