N567FE

Part: WIRE — CHAFED (EXTINGUISHER) · airframe 78,289 hrs · 28,150 cycles

NR 1 ENGINE FIRE AGENT LOW DURING CRUISE AND DECENT. CLEARED AFTER BLOCK IN TO GATE FOUND SHEILD ON WIRE TO P1-1261 WORN TO CENTER CONTACT IAW WDM 23-33-01. REPAIRED THE WIRE IAW SWP 20-10-01. OPS CHECKED IAW AMM 23-21-06-5. OK FOR SERVICE.

Part: FLOOR PANEL — CHAFED (BS 791) · airframe 78,286 hrs · 28,148 cycles

FLOOR PANEL AT BS 791 BETWEEN LBL 8.5 AND RBL 8.5 IS CHAFED AND WORN. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (BS 791) · airframe 78,286 hrs · 28,148 cycles

FLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (BS 791) · airframe 78,286 hrs · 28,148 cycles

FLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02 AND SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1256-1561) · airframe 78,286 hrs · 28,148 cycles

MAIN DECK LT SEAT TRACK AT LBL 47.5 BETWEEN BS 1256 AND 1561, HAD SEVERAL AREAS OF WEAR. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 FIG 2, DRAWING AFA 7433, SRM 51-31-01, SRM 51-31-01, 53-42-01 FIG 5 VOL II AND DRAWING AFA 7433. MAJOR REPAIR.

Part: ENGINE — FAULTY (NR 3) · airframe 772 hrs · 27,598 cycles

DURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMILAR TO 1 & 2 ENG, WHEN NR 3 THROTTLE WAS ADVANCED FROM IDLE, MODERATE VIBRATIONS WERE FELT. RAN COMPRESSOR STALL CHECKLIST & SHUTDOWN NR 3 ENG. ENG FAILED BORESCOPE INSPECTION. ENG IS APPROVED FOR REMOVAL BY ENGINEER. R & R NR 3 ENG IAW NR 3 ENG CHANGE WC 71T0101-3. OPERATIONS & LEAK CHECKED GOOD. OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (EVAC SLIDE) · airframe 770 hrs · 27,463 cycles

R1 REMOTE SLIDE PACK PRESSURE INDICATOR INOPERATIVE. REPLACED SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-03-2. OPERATIONS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 764 hrs · 27,102 cycles

AFTER PREFLIGHT SET UP, RECEIVED LEVEL 1 ALERT, EMER PWR ON, RETRIED EMER POWER CHECK WITH NO RESULTS. TROUBLESHOOT CHECKED IAW FIM 24-24-00. PULLED POWER FROM ACFT, DISCONNECTED BATTERY, RECONNECTED BATTERY IAW MM 24-34-01-4. RECONNECTED GND POWER & CYCLED ALL THREE FUEL LEVERS. PERFORMED RTS OF EPCU, TEST PASSED. EMER POWER OPERATIONS CHECKED OK.

Part: SUPPORT — CRACKED (LT WING) · airframe 75,922 hrs · 26,787 cycles

DURING OK TO CLOSE LT WING PANEL 531AT FOUND CRACKED AT BOTTOM FASTENER, APPROX 1 1/2 INCHES PROTRUDING ON THE FASTENER AT 2ND WEB RIB FROM STATION 118.200. REPAIRED SUPPORT PN ARB0647-1 IAW EA 8-5710-T0310822. THIS IS A STACK ANGLE REPAIR. MAJOR REPAIR.

Part: SKIN PANEL — DELAMINATED (RT WING) · airframe 75,922 hrs · 26,787 cycles

PANEL 635DR, OUTER SKIN HAS DELAMINATION ON OUTER SURFACE, APPROX AREA IS 4 INCHES X 6 INCHES. REPAIRED DELAMINATION TO OUTER SKIN & DOUBLER IAW SRM 51-71-00 PARA 17 B & IAW EA NR 8-5750-T0311007 P1 PANEL 635DR. MINOR REPAIR.

Part: SUPPORT — CRACKED (NR 1 COWLING) · airframe 75,922 hrs · 26,787 cycles

NUMBER 1 ENG OTBD CORE COWL, AFT HINGE FITTING, AFT FACE HAS GOUGES. REMOVED & INSTALLED GUSSET IAW SRM 51-31-01. REMOVED & INSTALLED HINGE FITTING IAW CMM 71-31-01. DURING REMOVAL FOUND SUPPORT CRACKED, WELDED CRACK IN UPPER SUPPORT RADIUS IAW EA 8-7110-T0310909 ON T14 1089145 ON NR 1 ENG OTBD CORE COWL. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,922 hrs · 26,787 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT HAS SEVERAL PLACES OF CORROSION BETWEEN STATION X=-56 & X=56 STATION Y-1964. REMOVED FLOOR SUPPORT IN AFT CARGO COMPARTMENT IAW SRM 51-31-01. FABRICATED NEW SUPPORT ON T14 1086876. INSTALLED NEW SUPPORT IAW SRM 51-31-01. MAJOR REPAIR. FLOOR SUPPORT WAS FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 1A, SH 3.

Part: SKIN — CHAFED (RT AILERON) · airframe 75,922 hrs · 26,787 cycles

RIGHT INBD AILERON LE SKIN LOWER SURFACE, ENTIRE LENGTH HAS CHAFED. R & R SKIN PN ARC1286-6 IAW SRM 51-31-01. FABRICATED SKIN ON STAM TRAVELER T14 1086055. TRACKED ON EA 8-5730-T0310879, RSC TRACKING ONLY. MAJOR REPAIR.

Part: SKIN — CORRODED (RUDDER) · corrosion level 2 · airframe 75,922 hrs · 26,787 cycles

UPPER AFT RUDDER, LT SIDE, EXTERNAL SURFACE AT UPPER STATIC BASE HAS CORROSION. R & R UPPER AFT RUDDER IAW AMM 27-20-02-4 & IAW WC E8-1110-7-4304 01. OPERATIONS CHECK IS GOOD IAW AMM 27-20-02-4. CLEARANCES WITHIN LIMITS IAW AMM 27-20-02-6. MINOR REPAIR.

Part: SKIN — CHAFED (RT AILERON) · airframe 75,922 hrs · 26,787 cycles

RIGHT INBD AILERON INBD LOWER LE SKIN HAS CHAFED. FOUND SKIN TO BE OUT OF LIMITS, ORIGINAL MATERIAL .040 INCHES, MATERIAL REMAINING .027 INCHES, MATERIAL LOSS .013 INCHES IAW SRM 57-00-01 FIG 1A SHEET 3. REMOVED INBD AILERON INBD LOWER LE IAW SRM 51-31-01. FABRICATED NEW SKIN ON T14 1086385. LOCATED & DRILLED NEW SKIN IAW SRM 51-31-01. INSTALLED NEW SKIN IAW SRM 51-31-01. RSC TRACKING ON EA 8-5730-T0310879 REV NR PS P1. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 75,922 hrs · 26,787 cycles

AFT CARGO COMPARTMENT TRACK HAS MULTIPLE SCRATCHES & SEVERAL SPOTS OF CORROSION AT STATION X=20, BETWEEN STATION Y 1781 - 1964. REMOVED CORROSION FROM AFT CARGO COMPARTMENT TRACK STA 1781-1964. FOUND TO BE OUT OF LIMITS AT 1841 WITH 100% MATERIAL LOSS IAW SRM 51-31-01, FIG. 1A. REPAIRED SEAT TRACK FROM 1821 - 1865 IAW SRM 53-70-00, FIG. 1. MAJOR REPAIR

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 75,922 hrs · 26,787 cycles

UPPER CARGO SEAT TRACK RBL 8, FS 1260 HAS 2 WORN LOBES. REMOVED DAMAGED & WORN SEAT TRACK & REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 AT FS 1260 RBL 8. FABRICATED SEAT TRACK REPAIR PARTS. SEAT TRACK PN S4929150, BAT 000287519, SPLICE HAT PN FX-SRM 53-70-00-2 ON T14 1085127, SPLICE PLATE PN FX-SRM53-70-00-1 ON T14 1085128. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,922 hrs · 26,787 cycles

AFT CARGO COMPARTMENT RT FLOOR SUPPORT HAS SEVERAL SPOTS OF CORROSION AT STATION X- -64 BETWEEN STATION Y 1781 - 1841. FLOOR SUPPORT FOUND OUT OF LIMITS, 100% MATERIAL LOSS, IAW SRM 53-00-01, FIG 1A, SH 3. R & R RT FLOOR SUPPORT IN AFT CARGO COMPARTMENT AT STATION X-64 BETWEEN STATION Y 1781 - 1841 IAW SRM 51-31-01. FLOOR SUPPORT FABRICATED FROM 7075-T6 050C ON T14 1085830. MAJOR REPAIR.

Part: SKIN — BULGED (TE FLAP) · airframe 75,922 hrs · 26,787 cycles

LEFT INBD FLAP HAS SKIN BULGE AT UPPER CTR TE. REPAIRED LT INBD FLAP IAW SRM 57-20-00 FIG 13. CURRENTLY BEING TRACKED ON EA 8-5710-T0310431. FABRICATED FILLER 2024-T3 BATCH 2550453 & DOUBLER 2024-T3 BATCH 264264. INSTALLED AT UPPER SKIN 177.300 TO 189.300. MAJOR REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 75,922 hrs · 26,787 cycles

UPPER CARGO SEAT TRACK LBL 8 FS 1401 HAS WORN LOBE. REMOVED SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-70-00, FIG 1. ORG MAT .260, LOSS .015, REMAINING MAT.245. FABRICATED REPAIR PARS: SEAT TRACK PN: 668105. SPLICE HATS ON T14/1085125, AND 2 EACH SPLICE PLATES ON T14/1085126. INSTALLED REPAIR PARTS AT LBL 8, STA 1401 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 75,922 hrs · 26,787 cycles

UPPER CARGO SEAT TRACK LBL 45 FS 755 HAS WORN LOBE. FOUND TO BE OUT OF LIMIT IAW SRM 53-70-00 FIG 5 SHEET1. REMOVED AND REINSTALLED FLOOR PANELS (FOM) IAW SRM 51-31-01. REMOVED WORN SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK P/N 60-10964 IAW SRM 53-70-00, REPAIR AT STA 755 LBL 45. MAJOR REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 75,922 hrs · 26,787 cycles

UPPER CARGO SEAT TRACK LBL 08, FS 1810 HAS WORN LOBE. REPAIRED SEAT TRACK AT STA 1810-1890, LBL 8 IAW ARM 53-70-00 FIG 1. SEAT TRACK P/N 60-10964. HAT T14/1085424, 1 EA SPLICE PLATE T14/1085430 PART MARK'S IAW GMM 7-0-1001-1. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,922 hrs · 26,787 cycles

AFT CARGO COMPARTMENT AFT INTERMEDIATE FLOOR SUPPORT BEAM HAS CORROSION AT STATION X=58, LT LONGERON 43 STATION Y 1781. REMOVED CORROSION FROM STA 1781 FLOORBEAM AT LONGERON 43, FOUND TO BE OUT OF LIMITS, 100% MATERIAL LOSS, IAW SRM 53-00-01, FIG 1A. REPAIRED FLOORBEAM 1781 IAW SRM 53-60-01, FIG 3, SH 1 & 2. MAJOR REPAIR.

Part: BULKHEAD WEB — CRACKED (MLG WW) · airframe 73,868 hrs · 25,618 cycles

CENTER LANDING GEAR WHEEL WELL SPACE, LT WALL, UPPER AFT CORNER HAS THREE CRACKS. TWO RUNNING THROUGH RIVETS AND ONE COMING FROM A HOLE DOUBLER. VERIFIED USING HFEC AND REPAIRED IN REF TO JPF'S AND SRM 53 -00-01, VOL I.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 73,442 hrs · 25,379 cycles

CARGO DOOR SKIN MISREPAIRED. REPAIRED AS PER EA 8-5230-159867.

Part: FRAME — MISREPAIRED (BS 1986 L46 L/R) · airframe 73,442 hrs · 25,379 cycles

FRAME FOUND MISREPAIRED AT BS 1986 BETWEEN L46 L/R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: FRAME — MISREPAIRED (BS 1975 L46L - 4) · airframe 73,442 hrs · 25,379 cycles

FRAME FOUND MISREPAIRED AT BS 1975 BETWEEN L46L-49R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 1701 L39-42R) · airframe 73,442 hrs · 25,379 cycles

CENTER CARGO DOOR FRAME FWD CUT OUT SKIN MISREPAIRED AT BS 1701 BETWEEN LONGERON 39 AND LONGERON 42 RT. REPAIR CARRIED OUT PER SRM 53-50-00 FIGURE 26 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: FLOORBEAM — MISREPAIRED (BS 808) · airframe 73,442 hrs · 25,379 cycles

FORWARD CARGO BAY FLOORBEAM BS 808, "X"= -22 TO "X" = -35 MISREPAIRED. REPAIRED AS PER EA 8-5310-159866. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 1220-1234) · airframe 73,442 hrs · 25,379 cycles

SKIN APPROX STATION 1220 TO STATION 1234 BETWEEN LONGERON 51 LT AND LONGERON 51 RT MISREPAIRED. REPAIRED IAW EA 8-5330-160977

Part: LONGERON — CRACKED (BS 808) · airframe 73,442 hrs · 25,379 cycles

ON REMOVAL OF FUSELAGE SKIN, FOUND LONGERON 49 LT CRACKED AT BS 808. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115

Part: LONGERON — MISREPAIRED (BS 780-825) · airframe 73,442 hrs · 25,379 cycles

LONGERON 51 LT MISREPAIRED, BETWEEN STA 780 AND STA 825. REPAIRED IAW SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON — MISREPAIRED (BS 826-840) · airframe 73,442 hrs · 25,379 cycles

LONGERON 52 LEFT MISREPAIRED BETWEEN BS 826 AND 840. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON — MISREPAIRED (BS 780-825) · airframe 73,442 hrs · 25,379 cycles

LONGERON 51 RT MISREPAIRED BETWEEN BS 780 AND 825. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON — MISREPAIRED (BS 808-825) · airframe 73,442 hrs · 25,379 cycles

LONGERON 50 LEFT MISREPAIRED BETWEEN BS 808 AND 825. REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (NR 3 SLAT) · airframe 73,442 hrs · 25,379 cycles

LT WING NR 3 SLAT AFT SKIN INBD OF NR 7 TRACK MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 98. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: RIB — MISREPAIRED (ZONE 500) · airframe 73,442 hrs · 25,379 cycles

LT WING AILERON LOWER SKIN RIB MISREPAIRED, REPAIRED IAW EA 8-5750-160989, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

LEFT WING INBD FLAP ASSY UPPER SURFACE MID SEGMENT STA XIFH 165, FOUND CRACKED. FOUND CRACKED. CRACKED SKIN AT LEFT HAND WING INBOARD FLAP ASSEMBLY UPPER SURFACE MID SEGMENT TRIMMED AND CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 98. CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: FUEL CELL — CORRODED (CENTER WING) · corrosion level 2 · airframe 73,442 hrs · 25,379 cycles

CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 40. AFTER CORROSION REMOVAL, FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CORRODED (BS 1139) · airframe 73,442 hrs · 25,379 cycles

CORROSION BETWEEN FUSELAGE SKIN AND BARE STRAP AT BS 1139, BETWEEN LT STRINGER 46 AND 45. REPAIRED IAW SRM 53-20-00, FIG 18 AND FIG 6, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 73,442 hrs · 25,379 cycles

BULK CARGO DOOR EXTERIOR SKIN LOWER FORWARD CORNER DAMAGED. CARRIED OUT REPAIR AS PER EA 8-5230-162350 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: FUEL CELL — CORRODED (CENTER WING) · corrosion level 2 · airframe 73,442 hrs · 25,379 cycles

CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, LBL 102. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. ORIGINAL MATERIAL THICKNESS = 0.220 INCH, REMAINING MATERIAL THICKNESS = 0.185 INCH, MATERIAL REMOVED = 0.035 INCH AND FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (ELEVATOR) · airframe 73,442 hrs · 25,379 cycles

HORIZONTAL STABILIZER INBD ELEVATOR UPPER SKIN FROM XE 148 TO XE 153 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (LT WING LE SLAT) · airframe 73,442 hrs · 25,379 cycles

LT WING NR 8 SLAT INBD LOWER SKIN MISREPAIRED. LT WING NR 8 SLAT R & R AMM 27-80-01-04, REV 14.3. OPS AND GAP CHECK CARRIED OUT IAW AMM 27-80-01-04, REV 14.3 FOUND SATISFACTORY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ELEVATOR) · airframe 73,442 hrs · 25,379 cycles

LT INBD ELEVATOR UPPER SKIN XE 111.75 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 1 SLAT AFT SKIN MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL I, REV 99. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 5 SLAT AFT SKIN MISREPAIRED. REPAIRED IAW EA 8-5100-162351. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,442 hrs · 25,379 cycles

CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 1. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (ELEVATOR) · airframe 73,442 hrs · 25,379 cycles

HORIZONTAL STABILIZER DETACHABLE ELEVATOR UPPER SKIN AT XE 50 RT MISREPAIRED. REPAIRED IAW SRM 51-35-02, VOLUME II, REV 98 AND EA8-5520-162352. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — DENTED (ZONE 100) · airframe 73,442 hrs · 25,379 cycles

LOWER FUSELAGE SKIN, APPROX STATION 1964, LONGERON 40 LT, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6 SHEET 3 VOL I, REV 98. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-20-00, FIG 6, SHEET 3, VOL I, REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — DENTED (ZONE 100) · airframe 73,442 hrs · 25,379 cycles

LOWER FUSELAGE SKIN, APPROX STATION 1966, LONGERON 40 LEFT, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6, SHEET 3, REV 98. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-20-00, FIG 6, SHEET 3, REV 98. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 115.

Part: SKIN — DENTED (BS 963) · airframe 73,442 hrs · 25,379 cycles

LOWER FUSELAGE AFT OF FORWARD CARGO DOOR CUTOUT APPROXIMATELY STATION 963 BETWEEN LONGERON 33, RT AND LONGERON 34, RT FOUND DENT. REPAIRED IAW SRM 53-50-00, FIG 26, VOLUME I, REV 98. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING L/E INNER SKIN MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-160976, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SEAT TRACK — CORRODED (BS 475) · corrosion level 2 · airframe 73,442 hrs · 25,379 cycles

FORWARD CABIN SEAT TRACK FOUND WITH CORROSION AT BS 475, RBL 27.5. REMOVED AND REPLACED FROM BS 421 TO 625 RBL 27.5 AS PER SRM 51-31-01 VOLUME II REVISION 98. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: PANEL — CORRODED (ZONE 200) · airframe 73,442 hrs · 25,379 cycles

FORWARD CABIN RIGID CARGO BARRIER LOWER ATTACHMENT PANEL, NR 6 FROM LT FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 98. ORIGINAL MATERIAL THICKNESS = 0.385 INCH. REMAINING MATERIAL THICKNESS = 0.348 INCH. MATERIAL REMOVED = 0.037 INCH FOUND WITHIN LIMIT AS PER SRM 51-21-01 VOLUM,E II REVISION 98 AND DRAWING WSP0785 REVISION B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (NR 2 SLAT) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 2 SLAT OTBD AFT SURFACE STA XIS 358 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 57-10-00 FIGURE 31 VOLUME I REVISION 99.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 73,442 hrs · 25,379 cycles

LT WING FIXED L/E COMPARTMENT UPPER BEADED DOUBLER BETWEEN STATION XOS 667 AND STATION XOS 673 FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5730-160984, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: RIB — CRACKED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

INTERIOR RIB XIFH 243, CRACKED. REMOVED AND REPLACED PER E.A. 8-5750-160991 STEP 5,

Part: RIB — DENTED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

FOUND INTERIOR RIB AT STATION XIFH 165 DENTED. REMOVED AND REPLACED PER E.A. #8-5750-160991 STEP 3.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

WITH INBD FLAP ASSY OTBD HINGE PIVOT BEARING REMOVED. FOUND FORWARD HINGE PIVOT HOLE INBD SPOT FACE CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMIT IAW CMM 57-44-07, REV 56, ORIGINAL THICKNESS: 0.486", MATERIAL REMOVED :0.017", REMAINING THICKNESS: 0.469", MINIMUM THICKNESS LIMIT: 0.450". REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 4 SLAT AFT SURFACE, STATION XOS 633 MISREPAIRED. REPAIR ACCOMPLISHED IAW SRM 57-10-00 FIG 31, VOL I, REV 98. EO 8-5100-7-5001 B2, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100 REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 4 SLAT AFT SURFACE STATION XOS 612, MISREPAIRED. REPAIRED IAW SRM 57-10-00 FIGURE 31, VOLUME I, REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 73,442 hrs · 25,379 cycles

RT WING, NR 4 SLAT AFT SURFACE STATION XOS 623 MISREPAIRED. REPAIR ACCOMPLISHED IAW SRM 57-10-00, FIG 31, VOLUME I, REV 98. EO 8-5100-7-5001 B2 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (SPOILER) · airframe 73,442 hrs · 25,379 cycles

RT WING NR 1 SPOILER PANEL LOWER SURFACE MISREPAIRED. SPOILER PANEL REPLACED IAW AMM 27-60-01-4, REV 14.3. CLEARANCE CHECK AND OPS TEST CARRIED OUT IAW AMM 27-60-01, REV 14.3 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (NR 1 SPOILER) · airframe 73,442 hrs · 25,379 cycles

RIGHT WING NR 1 SPOILER UPPER SURFACE XISP 226 MISREPAIRED. SPOILER PANEL REPLACED IAW AMM 27-60-01-4, REV 14.3. REPAIR CLASSIFIED AS MINOR GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (LT WING AILERON) · airframe 73,442 hrs · 25,379 cycles

LT WING OTBD AILERON LOWER SURFACE AT XOA 907 MISREPAIRED. REPAIRED IAW SRM 57-10-00, VOL 1, FIG 2, REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CHAFED (ZONE 100) · airframe 73,442 hrs · 25,379 cycles

LOWER FUSELAGE RT SIDE FORWARD OF STATIC PORT APPROXIMATE STA 859, LONGERON 42R FOUND SHORT PITCH AND CHAFING. CARRIED OUT REPAIR IAW EA 8-5330-159852 PART 1. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 115.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 73,442 hrs · 25,379 cycles

SKIN MISREPAIRED BS 886 BETWEEN LONGERONS 39 TO 42 RT. REPAIRED IAW EA 8-5330-159852. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

INBD LOWER SEGMENT UPPER SURFACE FORWARD EDGE STA XIFH 237 OF LT WING TE FLAP, MISREPAIRED. REPAIR CARRIED OUT PER E.A. 8-5750-160987 PART 1 STEP 2.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 73,442 hrs · 25,379 cycles

LT WING INBD AILERON LOWER SURFACE AT XIA 329 MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 01, VOL 1, REV 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: RIB — MISREPAIRED (RT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

RIB MISREPAIRED AT RT WING INBD FLAP L/E AT XIFH 240. REMOVED AND REPLACED PER E.A. 8-5750-160991.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

LT WING INBD FLAP ASSY, OTBD LOWER SEGMENT UPPER SURFACE FORWARD EDGE STATION XIFH 249 MISREPAIRED. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 99. E.O. #8-5100-7-5001 B2 PART 2

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 73,442 hrs · 25,379 cycles

SKIN MISREPAIRED AT RT WING INBD FLAP UPPER XIFH 243. REPAIR ACCOMPLISHED PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 99

Part: SKIN — MISREPAIRED (NR 5 SLAT) · airframe 73,442 hrs · 25,379 cycles

LT WING NR 5 SLAT INNER SKIN AT XOS 722 MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL 1, REV 98 & EO 8-5100-7-5001B2, PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 72,557 hrs · 24,907 cycles

WHEN CONDUCTING EMERGENCY LIGHT TEST, EMERGENCY LIGHT BATTERY 1 LOW, ILLUMINATED. REPLACED THE EMERGENCY LIGHT TEST BATTERY POWER SUPPLY IAW THE MM 33-51-01-4. OP CHECKED GOOD.

Part: BULB — FAILED (OIL TEMP) · airframe 71,739 hrs · 24,498 cycles

DURING CLIMB AT FL295, CLIMBING TO FL310 REC'D LEVEL II ALERT " ENG NR 1 OIL TEMP HIGH "TEMP INDICATED 203 DEG INITIALLY. AFTER SHUTDOWN TEMP CLIMBED TO 237 DEG. DURING DESCENT TEMP AVERAGED APPROX 160-165 DEG, EMERGENCY DECLARED. NO FUEL DUMPED. GENERAL VISUAL ON NR 1 ENGINE INLET AND TAILPIPE FOUND DAMAGE OR DEFECTS. DURING CREW DEBRIEF NR 1 OIL TEMP WAS ERRATIC AND GIVING INTERMITTENT OIL TEMP HIGH ALERTS. NR 1 ENGINE OIL TEMP CONTINUED TO READ HIGH AND FLUCTUATE LONG AFTER BLOCK-IN. R & R NR 1 ENGINE OIL TEMP SENSOR REF; MM 79-32-01-2. TEMP INDICATING NORMAL , DRY MOTOR LEAK CHECK GOOD. STILL NEEDS LAST STEP (9) OF MM 79- 32-01-2 COMPLIED WITH TO CLOSE WRITE-UP. COMPLIED WITH LAST STEP (9) OF AMM CH 79-32-01-2, OPS CHECKS NORMAL. ALSO RAN ALL ENGINES IN REF TO JRH FOR 10 MINUTES ON THE GROUND TO COMPARE NR 1 ENGINE TO THE OTHER 2, OIL TEMPS RESPECTIVELY WERE NR1-66C, NR 2-72C, NR 3-68C. ALSO COMPLIED WITH AMM CH 72-00-00-6-1 PARA E/2 AND PARA F. ALSO VERIFIED OPERATION FROM FIM FAULT CODE 79-32-03. ALL OPS CHECKS WERE NORMAL. ACFT OK FOR SERVICE. FINAL, CLOSED

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,707 hrs · 24,485 cycles

EMERGENCY LIGHT COVER MISSING ABOVE RT ACCESS TO INSPECT R-1 DOOR PNEUMATIC PRESSURE. SEARCHED COURIER AREA AND COULD NOT LOCATE. WILL REQUIRE NEW LENS REF IPC 33-53-01-02 ITEM NR 050 MPN PA71440. PLACING ON ORDER. . INSTALLED LIGHT COVER REF AC/MX SMP'S. FINAL CLOSED.

Part: UNKNOWN — MULTIPLE FAIL · airframe 71,149 hrs · 24,180 cycles

SIGNIFICANT STATIC DISCHARGE EXPERIENCED WHICH RESULTED IN MOMENTARY WX RADAR FAILURE AND LVL ONE "ENG FIRE AGNT LO". AGT 1 LO & AGT 2 LOW ILLUMINATED FOR ENGS 1 & 3 AND AGT 2 LO ILLUMINATED FOR ENG 2. COMPLIED WITH LIGHTENING INSPECTION REF MM 05-53-00-6 STEPS A THRU J COMPLETED.

Part: SKIN — DENTED (BS 1881-1898) · airframe 70,955 hrs · 24,070 cycles

FUSELAGE SKIN DENTED LT STA 1881 - 1898 AT LONGERON 36L. SIDEWALL PANELS REMOVED TO FOM IAW SRM 51-31-00, VOL II. DISPLACED INSULATION TO FOM IAW AMM 25-20-00. DENT OUT OF LIMITS IAW SRM 53-20-00, VOL I. FABRICATED REPAIR PARTS IAW SRM 53-20-00, FIG 6, VOL I. INSTALLED IAW SRM 53-20-00, FIG 6, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 70,955 hrs · 24,070 cycles

RT WING L/E UPPER SKIN INTERNAL BEADED DOUBLER HAS CRACKS EXTENDING BEYOND THE REPAIR DOUBLER (8 PLACES ) AT XORS 570. CUT OUT BEADED DOUBLER AND FABRICATED DOUBLER, FILLER AND REPAIR ANGLES IAW EA 8-5710-123547 "WINGS - RT WING L/E BEADED DOUBLER CRACKED - REPAIR". ALODINED AND PRIMED DOUBLER, FILLER AND REPAIR ANGLES IAW SRM 51-21-01, VOL II. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES IAW EA 8-5710-123547 "WINGS - RT WING L/E BEADED DOUBLER CRACKED - REPAIR".

Part: SPAR CAP — CRACKED (RT WING) · airframe 70,955 hrs · 24,070 cycles

RT WING SPAR LOWER CAP AT STA XORS 345.750; ALL (6) HOLES SHOW CRACK INDICATIONS. COMPLIED WITH EA 8-5710-123545,

Part: SKIN — BENT (CARGO DOOR) · airframe 70,955 hrs · 24,070 cycles

LOWER EXTERNAL FUSELAGE; FWD CARGO DOOR; FWD EDGE OF DOOR CUTOUT IS BENT AT FS 879 BETWEEN LONGERONS 42R & 43R.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1039; 85 INCHES RIGHT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1039, 85" RH OF C/L IAW SRZ25-005 REV. H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL IS PUNCTURED AT STA 1521 RBL 65 INCHES. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1521, 65" RT OF C/L IAW SRZ25-005 REV.H. REMOVED AND REINSTALLED FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1461; 85 INCHES RIGHT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1461 IAW DWG SRZ 25-005, REV "H". REMOVAL ACCOMPLISHED IN HANGAR ON N/R N00448.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139; 15 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1139, 15" LT OF C/L IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV. E SH 4.

Part: FLOOR PANEL — PUNCTURED (BS 800) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 800; 78 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 800, 78" LT OF CTR IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOORBOARD AND APPLIED HOT MELT IAW AMM 53-21-08-02.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 820; 15 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA. 820 IAW SRZ 25-005 REV. H INSTALLED FLOORBOARD IAW MM 53-21-08-2 PG. 2 STEP 3,4 APPLIED HOT MELT IAW DC/MD10-1053-21-08-2 PG.4 STEP 4,5 INSTALLED PLACARD/DECAL IAW DWG. 81608 REV.E SHT.4

Part: FLOOR PANEL — PUNCTURED (BS 1039) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1039; 55 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1039, 55" RT OF CTR IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOOR PANEL AND APPLIED HOT MELT IAW AMM 53-21-08-02. INSTALLED PLACARD IAW DWG 81608, REV "E".

Part: FLOOR PANEL — PUNCTURED (BS 820) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 820; 78 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 800, 78" LT OF CTR IAW DWG SRZ 25-005, REV "H". R & R FLOOR PANEL AND APPLIED HOT MELT IN GAPS IAW AMM 53-21-08-02. INSTALLED PLACARD IAW DWG 81608, REV "E".

Part: FLOOR PANEL — PUNCTURED (BS 1375) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1375; 55 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1375, RBL.55 IAW SRZ25-005, REV H, INSTALLED FLOORBOARD IAW MM 53-21-08-2, APPLIED HOT MELT IAW MM 53-21-08-2, PG 4, STEP A4,5. INSTALLED PLACARD IAW DWG 81680, REV E, SH 4.

Part: FLOOR PANEL — PUNCTURED (BS 820) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 820; C/L FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 820, BL.0 IAW SRZ25-005 REV H, INSTALLED FLOORBOARD IAW MM 53-21-08-2, APPLIED HOT MELT IAW MM 53-21-08-2, PG 4, STEP A 4,5.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL IS PUNCTURED AT STA 1521; 15 INCHES RT OF C/L. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1521, 15" RH OF C/L IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1701, LBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1910) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1910, LBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV. H. INSTALLED NEW FLOOR PANEL IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOOR PANEL IAW DWG.81608 REV. E SH 4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1701, LBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1270) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1270; 80 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1270, RBL 80 IAW SRZ25-005 REV H, INSTALLED FLOORBOARD IAW MM 53-21-08-2, APPLIED HOT MELT IAW MM 53-21-08-2 PG 4 STEP A4,5. INSTALLED PLACARD IAW DWG 81680, REV E, SH.4.

Part: FLOOR PANEL — PUNCTURED (BS 780) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 780; 60 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 780, 60" LT OF CTR IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOOR PANEL AND APPLIED HOT MELT IAW AMM 53-21-08-02. INSTALLED PLACARD IAW DWG 81608, REV "E".

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1621 RBL 65 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139; 65 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1139, 65" LH OF C/L IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. ANCRA 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139 C/L FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1139, B/L 0 IAW SRZ25-005 REV. H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV. E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1139) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139 LBL 85 . FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1139 IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOOR PANEL AND APPLIED HOT MELT IAW AMM 53-21-08-02.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139; 15 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1139, 15" RT OF C/L IAW SRZ25-005 REV.H. REINSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1841 C/L IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV. H. INSTALLED NEW FLOOR PANEL IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOOR PANEL IAW DWG. 81608 REV. E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139; 85 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1139, 85" RH OF C/L IAW SRZ25-005 REV.H. REMOVED AND INSTALLED FLOORBOARD IAW MM 53- 21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 920) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 920; 80 INCHES LEFT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 920, 80" LT OF CTR IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOOR PANEL AND APPLIED HOT MELT IAW AMM 53-21-08-02. INSTALLED PLACARD IAW DAC DWG 81608, REV "E".

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1375; 15 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1375, 15" RH OF C/L IAW SRZ25-005 REV. H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL A STA 1621 RBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG.81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1841, LBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1841, LBL 15 IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 820; 30 INCHES RT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.820 , 30" RT OF C/L IAW SRZ25-005 REV H. REMOVED AND INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1460) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1460, C/L IS PUNCTURED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1701, LBL 65 IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1139) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1139; 85 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1139; 85" LT OF C/L IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD IAW AMM 53-21-08-2. APPLIED HOT MELT IAW AMM 53-21-08-2.

Part: FLOOR PANEL — PUNCTURED (BS 1881) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1881, LBL 15 IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL IAW SRZ25-005 REV.H, INSTALLED FLOORBOARD IAW 53-21-08-2, APPLIED HOT MELT IAW MM 53-21-08-2 PG.4 STEP A 4,5. INSTALLED PLACARD IAW DWG. 81680 REV. E SH.4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1199 C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1199, B/L 0 IAW SRZ25-005 REV. H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG ANCRA 81608 REV. E SH4.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1375; 15 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1375, 15" LT OF C/L IAW SRZ25-005 REV. H. REMOVED AND REINSTALLED FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2 P.4 PAR.5. APPLIED PLACARD ON FLOORBOARD IAW DWG. 81608 REV.E SH4.

Part: FLOOR PANEL — PUNCTURED (BS 1039) · airframe 70,955 hrs · 24,070 cycles

MAIN CARGO COMPARTMENT STA 1039; 80 INCHES LT OF C/L; FLOOR PANEL IS PUNCTURED. FABRICATED NEW MAIN CARGO FLOOR PANEL AT STA 1039, 80" LT OF CTR IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED FLOORBOARD AND APPLIED HOT MELT IAW AMM 53-21-08-02.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CABIN SEAT TRACK IS GOUGED AT STA 1421 X 107.25. REPAIRED IAW SRM 53-70-00, FIG 1, VOL I. REMOVED AND INSTALLED AIR GRILLS TO F.O.M. IAW SRM 51-31-01, VOL II.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MAIN CABIN SEAT TRACK IS GOUGED AT STA 1448 X 107.25. SEAT TRACK WAS REPLACED ON NON- ROUTINE N00773.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 70,955 hrs · 24,070 cycles

RT WING INBD FLAP LOWER SKIN IS DENTED. CHECKED ALL DENTS IAW MD/DC10 SRM 57-10-00, FIG 48, PG 162A, VOL I. ALL DENTS BETWEEN XIFH 192 TO XIFH 199 AND YIFH 39 TO YIFH 51 ARE WITHIN LIMITS. DENT AT XIFH 201 AND YIFH 72 IS CREASED OUT OF LIMITS. BLENDED OUT GOUGES IN DENTS AT STA XIFH 171; YIFH 62 AND XIFH 172.5 ; YIFH 59.9 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01, FIG 1-A, SHEET 3, PG 5. ORIGINAL MATERIAL THICKNESS IS 0.040. REMAINING THICKNESS IS 0.025 / 0.022. REMOVED 0.015 / 0.018. CUTOUT DAMAGED AREAS AND REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, PG 12.

Part: FITTING — CRACKED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MCD NR 3 SPOOL HAS A CRACK INDICATION AT HOLE "B". REMOVED AND REPLACED CRACKED SPOOL FITTING IAW SRM 51-31-01, VOL II. "B" HOLE ON THE SPOOL FITTING RERQUIRES A NEW BUSHING. NEW BUSHING FABRICATED AND INSTALLED IAW SRM 53-50-00, FIG 17, VOL I. REMOVED WEB, CLIPS, AND FLOORBEAM ATTACH BRACKETS STA 655 TO 675 FOR ACCESS. REINSTALLED WEB , CLIPS AND FLOORBEAM ATTACH BRACKETS IAW SRM 51-31-01, VOL II.

Part: FITTING — CRACKED (ZONE 200) · airframe 70,955 hrs · 24,070 cycles

MCD NR 7 SPOOL HAS 2 CRACK INDICATIONS AT HOLE "B". REMOVED CRACKED NR 7 SPOOL FITTING FROM FUSELAGE STA 755 IAW SRM 53-50-00. REMOVED WEBS AT 2 EA, AND ATTACHMENTS FROM STA 755 TO 775. REMOVED FLOORBEAM TO FUSELAGE ATTACHMENTS, PLATES, ANGLES AND INTERCOSTALS AT 3 EA. RECEIVED NEW SPOOL FITTING P/N AFA 7132-1, PO 685280.3. REAMED TO 0.453 FOR FINAL DIAMETER , SPOT FACED 4 EA HOLES IAW DWG AFA7132, REV "B". ALODINED AMD PRIMED SPOT FACED AREAS IAW SRM 51-20-01, VOL II. INSTALLED SPOOL FITTING IAW SRM 53-50-00. INSTALLED FLOORBEAM, INTERCOSTALS 2 EA, WEBS 3 EA AND SIDE WALL SUPPORT PANEL BEAM IAW SRM 51-33-01.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,955 hrs · 24,070 cycles

MCD NR 1 SPOOL HAS A CRACK INDICATION AT HOLE "B". REMOVED AND REPLACED CRACKED SPOOL FITTING IAW SRM 51-31-01, VOL II. "B" HOLE ON THE SPOOL FITTING REQUIRES A NEW BUSHING. NEW BUSHING FABRICATED AND INSTALLED IAW SRM 53-50-00, FIG 17, VOL I. REMOVED WEB, CLIPS, AND FLOORBEAM ATTACH BRACKETS AND REINSTALLED WEB , CLIPS AND FLOOR BEAM ATTACH BRACKETS IAW SRM 51-31-01, VOL II.

Part: FITTING — CRACKED (CARGO DECK) · airframe 70,955 hrs · 24,070 cycles

MCD NR 6 SPOOL HAS A CRACK INDICATION AT HOLE "B".

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 70,955 hrs · 24,070 cycles

FORWARD CARGO COMPARTMENT FLOOR BEAM IS CRACKED; RIGHT HAND SIDE OF THE MIDDLE ROLLER TRAYS AT FS 808 TO FS 808. REPAIRED FWD CARGO PIT FLOOR BEAM AT STA 808; RBL 32 IAW MD/DC10 SRM 53-00-01, FIG 7, PG 23, VOL I.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 XF IS PUNCTURED. (SECOND AFT) FABRICATED NEW FLOOR PANEL NR123XF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 CD IS DENTED. FABRICATED NEW FLOOR PANEL NR 123 CD IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 BD IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR 123 BD IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 YF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR 123 YF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 ZF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR 123 ZF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 UF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR123 UF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 SF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR123 SF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 DD IS GOUGED. FABRICATED NEW FLOOR PANEL NR 123 DD IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 LF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR 123 LF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 ED IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR 123 ED IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 WD IS DELAMINATED & PUNCTURED. FABRICATED NEW FLOOR PANEL NR123 WF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 70,955 hrs · 24,070 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 123 XF IS DELAMINATED. FABRICATED NEW FLOOR PANEL NR123 XF IAW DWG SRZ 25-005, REV "H".

Part: LOOP — FAULTED (BLEED AIR) · airframe 69,246 hrs · 23,214 cycles

PASSING 16000 FT ON CLIMB-OUT GOT AIR SYST 2 OFF, FOLLOWED BY LEVEL 2 AIR MANIFOLD 2 FAIL. NR 2 PACK WAS SELECTED OFF AT THE TIME AND NR 2 BLEED WAS ON. PER QRH LAND AT NEAREST SUITABLE AIRPORT. PERFORMED AIR SYSTEM DECAY CHECK REF AMM 36-00-01-5. TEST PASSED. ISOLATED FAULT TO NO LOOP 2 INPUT RECEIVED REF MEL 36-23-01-02.

Part: PANEL — DENTED (FUSELAGE) · airframe 68,012 hrs · 22,624 cycles

FILLET PANEL NR 152 LT IS DENTED. REPAIRED DAMAGED AREAS (2 EACH) BY REPLACING THE CORE AND APPLYING WET FIBERGLASS OVERLAYS IAW DC/MD-10 SRM 51-62-01; VOL II AND SRM 51-43-01; VOL II; PARA 16. RESTORED SURFACE FINISH IAW DC/MD-10 SRM 51-21-02; VOL II. REMOVED AND REINSTALLED THE PANEL IAW DC/MD-10 SRM 51-31-01; VOL II.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

RIGHT WING RUEL TANK TANK PLATE/PANEL 634 BT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVED CORROSION FROM THE FLANGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I; PG 217. MACHINED A NEW 634 BT PANEL IAW DAC DWG ARB0872, REV "AV". ALODINED, PRIMED AND PAINTED 634 BT DC/MD-10 SRM 51-21-01, VOL II AND SRM 51-21- 02, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI IAW DPS 4.707 AND DAC DWG ARB 0872, REV "AV", NO CRACKS NOTED.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

LEFT WING FUEL TANK PLATE/PANEL 531 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED NEW FUEL PANEL IAW DAC DWG ARB0872, REV "AV".

Part: PANEL — WORN (ZONE 500) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

LEFT WING FUEL TANK PLATE/PANEL 535 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS, GOUGES AND TWO FASTENER HOLES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I, PG 217. MACHINED A NEW PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE, PRIMER AND PAINT IAW DAC DWG ARB0872, REV "AV" AND DC/MD-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI IAW DPS 4.707AND DAC DWG ARB0872, REV "AV", NO CRACKS NOTED.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

RIGHT WING FUEL TANK PLATE/PANEL 633 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED NEW FUEL PANEL IAW DAC DWG ARB0872, REV "AV".

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

RIGHT WING FUEL PLATE/PANEL 635 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVED DAMAGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL II, PG 217. MACHINED A NEW 635 AT PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE, PRIMER AND PAINT IAW ARB0872, REV "AV" AND DC/MD-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI PER DPS 4.707 AND DAC DWG ARB0872, REV "AV", NO CRACKS NOTED.

Part: PANEL — WORN (ZONE 500) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING TANK PLATE/PANEL 639 CB HAS ELONGATED FASTENER HOLE AND FOUND TO BE OUT OF LIMITS IAW DC/MD SRM 57-10-00, VOL I. MACHINED A NEW PANEL IAW DAC DWG ARB0975-33, REV "AY". FPI IAW DPS 4.707 AND DAC DWG ARB0975, REV "AY". NO CRACKS NOTED. APPLIED ALODINE, PRIMER AND PAINT IAW DAC DWG ARB0975, REV "AY" AND DC/MD-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 68,012 hrs · 22,624 cycles

LEFT WING FUEL TANK PLATE / PANEL 534 CT; INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION; NICKS & GOUGES. REMOVED DAMAGE FROM THE PANEL & FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; VOL I; PG 217. MACHINED A NEW 534 CT PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE; PRIMER & PAINT IAW DAC DWG ARB0872, REV "AV" & DC/MD-10 SRM 51-21-02; VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI PER DPS 4.707 & DAC DWG ARB0872, REV "AV". NO CRACKS NOTED.

Part: COWLING — DAMAGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 ENGINE INBD FAN COWL HAS A SMALL PUNCTURE. REPAIRED DAMAGED AREA BY FABRICATING AND BONDING A FILLER AND DOUBLER IAW DC/MD-10 SRM 54-00-01, FIG 4, VOL I. RESTORED THE SURFACE FINISH IAW DC/MD-10 SRM 51-21-01, VOL II, 51-21-01; VOL II AND 51-41-01, VOL II.

Part: FAIRING — DAMAGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 PYLON STRINGER FAIRING NR 489 AL LOWER FRAME HAS MULTIPLE DRILLED HOLES ON BOTH SIDES. REPLACED FAIRING NR AUB 7107-46, PO 619490.1 IAW DAC DWG 6 NR AUB 7107, REV "P".

Part: FAIRING — DELAMINATED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 PYLON STRINGER FAIRING NR 489 A, LOWER SECTION OF THE FAIRING IS DELAMINATED AND COMING APART. FAIRING 489 AL WAS REPLACED ON FEDEX N/R N00610.

Part: SKIN — DENTED (ZONE 600) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING NR 2 SLAT L/E HAS A DENT. CUT OUT DAMAGED AREA OF SLAT. FABRICATED DOUBLER AND FILLER IN REF TO DC/MD-10 SRM 57-10-00, FIG 43 VOL II. REMOVED RUB STRIP FROM THE NR 2 SLAT IAW DC/MD-10 SRM 51-35-01, VOL II. REMOVED NR 3 SLAT TRACK IN REF TO DC/MD-10 SRM 51-31-01, VOL II. ALODINED AND PRIMED IN REF TO DC/MD-10 SRM 51-21-01, VOL II. INSTALLED DOUBLER AND FILLER IN REF TO DC/MD-10 SRM 51-35-02, VOL II. INSTALLED RUB STRIP AND SLAT TRACK COVER IN REF TO DC/MD-10 SRM 51-35-01, VOL II AND 51-35-02, VOL II.

Part: RUB STRIP — GOUGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 ENGINE INBD CORE COWL UPPER RUB STRIP IS WORN (GOUGED). REMOVED THE DAMAGED RUB STRIP IAW SRM 51-35-01 VOL II. FABRICATED PER DWG NSL 6061, REV "BC". PRIMED & PAINTED IAW SRM 51-21-01; PG 21; 51-23-01; VOL II. INSTALLED IAW 51-23-01; VOL II.

Part: RIB — WORN (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON STRINGER FOR PANEL 439 AL FWD LEFT LANDING IS WORN. REMOVED FWD RIB IAW SRM 51-31-01; VOL II & 51-35-01; VOL II. DRILLED UP NEW RIB IAW DWG AUB 7107, REV F & SRM 51-31-01; VOL II. INSTALLED NEW RIB IAW SRM 51-31-01, VOL II & 51-35-01; VOL II.

Part: HINGE — DAMAGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL NR 437 HL HAS A BROKEN HINGE. BLENDED DOUBLER ORIGINAL MAT .100 REMOVED .030 REMAINING .070 FOUND TO BE OUT OF LIMITS IAW DC/MD10 SRM 57-00-01 VOL I FABBED -177 DOUBLER IAW DC/MD10 DWG. AUB7108 REV AN ALODINED AND PRIMED DOUBLER IAW DC/MD10 SRM 5121-01 VOL II. PART MARKED DOUBLER FEDEX GMM 7-0-1000. INSTALLED -177 DOUBLER AND HINGE IAW DC/MD10 SRM 51-31-01 VOL II.

Part: PANEL — CHAFED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL 437 EL IS CHAFED AT THE HINGE AND THE HINGE IS WORN. REMOVED AND REPLACED P/N AUB7038-37 HINGE ASSY AUB7038-39 HINGE IAW DC10/MD 10 SRM 51-35-01 VOL II; BLENDED AREA IAW DC/MD10 SRM 54-00-01 VOL I; FOUND TO BE OUT OF ALLOWABLE LIMITS IAW DC/MD10 SRM 54-00-01 VOLI; MAT ID 2024-T3 .090 IAW DC/MD10 SRM 54-00-01 VOL I; FABBED DOUBLER IAW DC/MD10 SRM 54-00-01 VOL I; ALODINED AND PRIMED DOUBLER IAW DC/MD10 SRM 51-21-01 VOLII; INSTALLED DOUBLER IAW DC/MD10 SRM 51-35-01 VOL II.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 68,012 hrs · 22,624 cycles

LT HORIZ STAB DROOP ELEVATOR UPPER AND LOWER SKIN HAVE WORKING FASTENERS NUMEROUS PLACES. REMOVED FSATENERS; HOLES IN THE SKIN & RIB DAMAGED. REMOVED DAMAGED RIB & SKIN. ALODINED; PRIMED & TOP COATED IAW SRM 51-21-01; VOL II. INSTALLED DOUBLER; FILLERS AND ANGLE IAW SRM 55-10-00; VOL I & 55-20-00; VOL I.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL NR 438 CL, INNER CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED A NEW CHANNEL REF DC/MD-10 SRM 51-31-01, VOL II.

Part: SEAL — BENT (NR 3 PYLON) · airframe 68,012 hrs · 22,624 cycles

NR 3 PYLON ACCESS PANEL NR 488 DR, SPRING SEAL IS BENT. REMOVED 2 SEALS IAW SRM 51-35-01; VOL II. FABBED 2 SEALS IAW SRM 51-10-00; VOL II; FIG 1 & 51-31-01; VOL II; FIG 2. PART MARKED PER GMM 7-0-1001. INSTALLED SEALS IAW SRM 51-35-01; VOL II.

Part: PANEL — DAMAGED (NR 1 PYLON) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL 483 GL HAS 1 FASTENER HOLE WALLOWED OUT. ANNEALED TITANIUM IAW E.A. 8-5480-116981. FORMED & FABBED IAW DWG AUB 7036. REMOVED & INSTALLED DRAIN TUBE IAW E.A. 8-5480-116981. INSTALLED IAW SRM 51-35-01. LOCATED & DRILLED HOLES IAW SRM 51-31-01. INSTALLED IAW SRM 51-31-01.

Part: SKIN — DENTED (ZONE 300) · airframe 68,012 hrs · 22,624 cycles

LEFT STABILIZER DROOP ELEVATOR UPPER SURFACE HAS DENTS. SIX DENTS WITHIN LIMITS IAW DC/MD-10 SRM 51-80-01, VOL II. ONE DENT OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01; VOL II. MATERIAL ID FOR DOUBLER IS 2024-T3, 0.03, PO 485358.1 IAW DC/MD-10 SRM 55-00-01, VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, VOL II. INSTALLED DOUBLER IAW DC/MD-10 SRM 55-00-01, VOL I.

Part: FAIRING — CHAFED (RT WING TE FLAPS) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING INBD FLAP TRACK FAIRING NR 641 DL AFT EDGE IS CHAFED. BLENDED AREA; PERFORMED D.P.I. AODINED & PRIMED IN REF TO FEDEX E.A. 8-5720-116982" REMOVED & INSTALLED FAIRING IN REF TO SRM 51-31-01; VOL II.

Part: PANEL — CHAFED (RT WING) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING T/E PANEL NR 645 BB L/E IS CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. RECEIVED NEW PART. DRILLED, DEBURRED AND COUNTERSUNK IN REF TO SRM 51-31-01; VOL II.

Part: SKIN — DAMAGED (RT WING) · airframe 68,012 hrs · 22,624 cycles

RIGHT SKIN LEADING EDGE SKIN LOWER SURFACE IS KNIFE EDGED AT THE CUTOUT FOR THE ANTI-ICE "T" DUCT. BLENDED DAMAGED AREA. ORIGINAL MATERIAL 0.063 IAW DWG ARB1284, REV "AC". MATERIAL LOSS 0.045. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATED IAW DWG ARB1284, REV "AC". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21-24 VOL II. INSTALLED IAW SRM 51-35-01 & 51-33-01; VOL II.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 68,012 hrs · 22,624 cycles

LEFT WING LEADING EDGE FIRE BOTTLE COMPARTMENT ACCESS PANEL IS CHAFING AROUND THE CONTACT SURFACE. REPAIRED PANEL BY BLENDING CHAFED AREA & CHECKING LIMITS IAW SRM 57-00- 01; VOL I. BLENDED AREAS FOUND TO BE OUT OF LIMITS. REMOVED PANEL IAW SRM 51-31-01; VOL II. FABRICATED & BOUNED REPAIR DOUBLER IAW SRM 51-71-00; VOL II & EA 8-5720-118487. INSTALLED IAW SRM 51-31-01; VOL II.

Part: SEAL — WORN (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 2 ENGINE CORE COWL FWD UPPER SPRING SEAL HAS HOLES WORN THROUGH THE SEALS. REMOVED & REPLACED THE UPPER SPRING SEAL IAW DC/MD-10 SRM 51-35-01; VOL II.

Part: ACCESS PANEL — CHAFED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 PYLON ACCESS PANEL NR 487 HR HAS FASTENERS ON A PREVIOUS REPAIR THAT ARE CHAFED IN HALF WITH ELONGATED HOLES AND NO ED AND BARE METAL. FABRICATED NEW PANEL IAW DWG AUB 7108 REV AN. ALODINED & PRIMED PANEL IAW SRM 51-21-01; VOL II. PART MARKED PANEL ASSY IAW GMM 07-0-1000.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 68,012 hrs · 22,624 cycles

RIGHT SIDE NR 1 PYLON LOWER AFT FAIRING HAS A CRACK APPROX 2 INCHES LONG. REMOVED & INSTALLED FAIRING IN REF TO SRM 51-31-01 VOL II. REMOVED DAMAGE; FABRICATED REPAIR AND INSTALLED REPAIR IN REF TO SRM 54-00-01 FIG 26 VOL I & SRM 51-33-01 VOL II.

Part: ADAPTER — WORN (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 ENGINE OUTBD CORE COWL L/E RUB STRIP IS WORN IN SEVERAL AREAS. BLENDED WORN AREAS. MATERIAL LOSS 0.065. FOUND TO BE OUT OF LIMITS IAW AMM 71-13-01-02 & DWG S2929517. REMOVED & REPLACED RUB STRIP ASL 0040-1. IAW SRM 51-35-01; VOL II & DWG ASL 0040 REV "NC".

Part: SKIN — CRACKED (ZONE 600) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING FIXED LEADING EDGE CAVITY UPPER SKIN DOUBLER IS CRACKED AT STA XFS 669, OUTBD OF THE NR 10 SLAT TRACK. FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00; FIG 71; VOL I. PRIMED REPAIR DOUBLER IAW SRM 51-21-01; VOL II AND 51-35-01; VOL II.

Part: NOSE COWL — DENTED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 ENGINE NOSE COWL L/E HAS A DENT AT THE 6-7 O'CLOCK POSITION. NR 1 ENGINE NOSE COWL DENTS FOUND TO BE OUT OF LIMITS DUE TO DREASE IAW SRM 54-11-00; VOL I. REMOVAL AND REPLACEMENT ACCOMPLISHED ON N/R N00284.

Part: NOSE COWL — CORRODED (NR 1 NACELLE) · airframe 68,012 hrs · 22,624 cycles

NR 1 ENGINE NOSE COWL L/E HAS NUMEROUS AREAS OF PITTED CORROSION ALONG THE ENTIRE CIRCUMFERENCE OF EXTERNAL SKIN. REMOVED THE CORROSION IN REF TO DC/MD-10 SRM 51-21-01; VOL II AND FOUND TO BE OUT OF LIMITS IN REF TO DC/MD-10 SRM 54-00-01; VOL I. REMOVED & REPLACED THE NR 1 ENGINE NOSE COWL REF MD-10-10 AMM 71-11-00-2. PERFORMED AN ANTI ICE OPS CHECK. OP'S CHECKED GOOD.

Part: SUPPORT ANGLE — CRACKED (RT WING LE) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING LEADING EDGE CAVITY PANEL SUPPORT ANGLE IS CRACKED, OUTBD OF THE NR 8 SLAT TRACK. REMOVED FORMER IAW SRM 51-35-01 & 51-33-01; VOL II. FABRICATED PER DWG ARB1162, REV "S". ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24. INSTALLED IAW SRM 51-35-01 & 51-33-01; VOL II.

Part: SKIN — DENTED (TAILCONE) · airframe 68,012 hrs · 22,624 cycles

THE TAILCONE, RIGHT SIDE EXTERNAL SKIN HAS A DENT. REMOVED THE DAMAGE FROM THE RIGHT SIDE EXTERNAL SKIN OF THE TAILCONE IAW SRM 53-00-01; PGS 46 & 50; VOL I. FABRICATED REPAIR DOUBLER; ALODINED; PRIMED AND TOP COATED IAW SRM 51-21-01; VOL II.

Part: DEPRESSOR — CRACKED (LT MLG DOOR SEAL) · airframe 68,012 hrs · 22,624 cycles

LT MLG WW OUTBD SEAL DEPRESSOR FOR THE MAIN GEAR DOOR IS WORN AND CRACKED. SEAL LAND WAS WORN & CRACKED RENDERING IT UNSERVICEABLE. REMOVED SEAL LAND IAW SRM 51-35-01. FABRICATED A NEW SEAL LAND IAW DWG ARC0467. HEAT TREATED SEAL LAND IAW TPS 1003. CONDUCTIVITY LOAD 35.2 / 35.5; HT050208-2. PART MARKED SEAL LAND ARC0468-107FX IAW GMM 7-0-1000. INSTALLED SEAL LAND IAW SRM 51-31-01.

Part: SKIN — GOUGED (ZONE 600) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING T/E OUTBD FLAP, INBD TRACK, INBD SIDE, SKIN HAS A GOUGE. REMOVED PLATE DAMAGE IAW SRM 51-25-01; VOL II. FABRICATED IAW DWG ARC 2009, REV Y. ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21 & 24. INSTALLED IAW SRM 51-35-01 VOL II. PART MARKED IAW GMM 7-0-1000. PAINTED IAW SRM 51-21-02; VOL II; PG 8.

Part: CASE — GOUGED (NR 3 EXIT) · airframe 68,012 hrs · 22,624 cycles

NR 3 ENGINE FAN EXIT CASE FLANGE AT THE FAN HOLD OPEN ROD SUPPORT BRACKET HAS A GOUGE ON THE FLANGE. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO ENGINE MANUAL 72-23-01 PG 311. WELDED REPAIR AREA IN REF TO ENGINE MANUAL 72-23-01 REPAIR 01. ALODINED 7 PRIMED IN REF TO SRM 51-21-01; VOL II. FPI IN REF TO SPM 70-32-01. NO DEFECTS NOTED.

Part: BRACKET — CRACKED (ZONE 700) · airframe 68,012 hrs · 22,624 cycles

LT MLG W/W OUTBD SEAL DEPRESSOR FOR THE MAIN GEAR DOOR IS WORN & CRACKED. SEAL LAND WAS WORN & CRACKED RENDERING IT UNSERVICEABLE. REMOVED SEAL LAND IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID TO FAB SEAL LAND IS 7075-0, PO 550418.3 IAW DWG ARC0468, REV AW. FABRICATED NEW SEAL LAND IAW DWG ARC0467, REV AW. HEAT TREATED SEAL LAND TO 7075-6 IAW TPS 1003, REV A. CONDUCTIVITY LOAD 35.2 / 35.5; HT050208-2. APPLIED ALODINE & PRIMER IAW SRM 51-21-01; VOL II. PART MARKED SEAL LAND ARC0468-107FX IAW GMM 7-0-1000. INSTALLED SEAL LAND IAW SRM 51-31-01; VOL II.

Part: PLATE — GOUGED (ZONE 500) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING T/E OUTBD FLAP, INBD TRACK, INBD SIDE, THE SUPPORT FOR PANEL NR 635 DL IS GOUGED. REMOVED PLATE DAMAGE IAW SRM 51-31-01; VOL II. FABBED NEW PLATE IAW DWG ARC 2009, REV Y. ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24. PART MARKED IAW GMM 7-0-1000. INSTALLED IAW SRM 51-35-01 VOL II. INSTALLED PANEL 635 FL IAW SRM 51-35-01 VOL II.

Part: RUB STRIP — WORN (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 ENGINE OUTBD CORE COWL UPPER T/E CHAFE STRIP IS WORN. BLENDED AREA; ALODINED; PRIMED AND PAINTED IN REF TO EA 8-7110-118486.

Part: RUB STRIP — WORN (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 ENGINE INBD CORE COWL FWD CHAFE STRIP IS WORN IN SEVERAL PLACES. REMOVED THE ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II. DRILLED AND LOCATED NEW ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II AND DWG ASL 0040 REV J. INSTALLED NEW ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II AND DWG ASL 0040, REV J.

Part: PANEL — CHAFED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 3 PYLON PANEL 487 FL IS CHAFING AT THE INNER SURFACE. BLENDED OUT. ORIGINAL MATERIAL 0.071 IAW SRM 54-51-02; VOL III. MATERIAL REMOVED 0.027. MATERIAL REMANING 0.044; AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01; VOL I; WTG T8225P. REMOVED THE SEAL RETAINER TO F.O.M.IAW SRM 51-31-01; VOL II. FABRICATED A REPAIR DOUBLER IAW SRM 54-00-01; VOL I. ALODINED & PRIMED IAW SRM 51-21-01; PGS 21 & 34; VOL II. INSTALLED DOUBLER REPAIR IAW SRM 51-35-01; VOL II. INSTALLED THE SEAL RETAINER IAW SRM 51-31-01; VOL II.

Part: SKIN — DENTED (NR 3 NOSE COWL) · airframe 68,012 hrs · 22,624 cycles

NR 3 ENGINE NOSE COWL HAS DENTS ON THE EXTERNAL SKIN AT APPROX 5 O'CLOCK POSITION. REWORKED SKIN IN REF TO EA 8-5410-116980.

Part: DOOR — DAMAGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL NR 437LL, INNER SURFACE HAS CHAFED THROUGH. NR 1 PYLON PANEL NR 437 LL REQUIRES AN SRM REPAIR. IAW DC/MD-10 54-51-01; VOL III; PG 3. FABRICATED REPAIR DOUBLER & FILLER IAW SRM 54-00-01; VOL I. ALODINE & PRIMED REPAIR DOUBLER & FILLER IAW SRM 51-21-01; VOL II. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 51-31-01; VOL II.

Part: RIB — DAMAGED (NR 1 PYLON) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL 437EL HAS A DAMAGED RIB. REMOVED REPLACED RIB NR AUB7079-9 PO NR 577666.3 IAW DC/MD 10 SRM 51-35-01 VOL II.

Part: COWLING — WORN (NR 3 ENGINE) · airframe 68,012 hrs · 22,624 cycles

NR 3 ENG LT CORE COWL INNER SURFACE OF LEADING EDGE WORN. REMOVED ASL 0040-0 ADAPTER. LOCATED & DRILLED HOLES IAW SRM 51-35-01 & ASL 0040. INSTALLED ASL 0040 ADAPTER IAW SRM 51-35-01 & ASL 0040. PAINTED IAW SRM 51-23-01.

Part: PANEL — DENTED (RT WING) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING LOWER I/B T/E PANEL 641EB HAS SEVERAL DENTS. REPAIRED ( 3 EA ) DAMAGED AREAS BY FABRICATING & BONDING A CORES; FILLERS & DOUBLERS IAW SRM 51-71-00 VOL II.

Part: PANEL — DAMAGED (ZONE 400) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON 437ER HAS DAMAGED FASTENER HOLES. FABBED DOUBLER TO REPAIR FASTENER HOLE DAMAGE REF DC/MD-10 SRM 54-00-01; VOL III. ALODINED & PRIMED DOUBLER REF DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER REF DC/MD-10 SRM 51-35-01; VOL II.

Part: RETAINER — CRACKED (NR 1 PYLON) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL 437AR SEAL RETAINER IS CRACKED. REMOVED & REPLACED THE SEAL RETAINER IAW SRM 51-31-01; VOL II.

Part: SKIN — DAMAGED (RT WING) · airframe 68,012 hrs · 22,624 cycles

RIGHT WING UPPER I/B L/E PANEL 618AT INNER SKIN IS DAMAGED. REMOVED DAMAGED SECTION INNER SKIN IAW SRM 57-10-00. FABRICATED FILLERS 2 EA AND A REPAIR DOUBLER IN REF TO SRM 57-10-00. PRIMED REPAIR PARTS IN REF TO SRM 51-21-01. INSTALLED FILLERS AND REPAIR COUBLER IN REF TO SRM 51-35-01.

Part: RETAINER — CRACKED (NR 1 PYLON) · airframe 68,012 hrs · 22,624 cycles

NR 1 PYLON PANEL 437HL HAS A CRACKED SEAL RETAINER. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-31-01 VOL II.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 68,012 hrs · 22,624 cycles

TAIL CONE, PATIO DOOR, LATCHING MECHANISM, LT SIDE, INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL FROM THE TAIL CONE IAW SRM 51-35-01; VOL II. HEAT TREATED IAW DWG HT 042808-6, TESTED 58-60 ON RWD. FABRICATED NEW INTERCOSTAL IAW DWG AKC 7150. ALODINED & PRIMED THE INTERCOSTAL IAW SRM 51-21-01 VOL II. INSTALLED THE INTERCOSTAL IAW SRM 51-31-01 VOL II.

Part: SKIN PANEL — DAMAGED (LT WING) · airframe 68,012 hrs · 22,624 cycles

LEFT WING LOWER INBD L/E PANEL 517 AB HAS DAMAGED ATTACHED HOLES. FABRICATED DOUBLER & FILLER IAW SRM 57-00-01 VOL I. ALODINED; PRIMED AND TOPCOAT PAINTED SRM REPAIR IAW SRM 51-21-01 VOL II. INSTALLED SRM REPAIR DOUBLER & FILLER IAW 57-31-01 VOL II.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 68,012 hrs · 22,624 cycles

TAIL CONE, PATIO FLOOR; DOOR; DELAMINATED. FABRICATED NEW PATIO FLOOR DOOR; POTTED EDGES, COMPLETED CURE & SANDED THE EDGE POTTING, INSTALLED INSERTS; APPLIED NON-SKID. PART MARKED PANEL; REMOVED HARDWARE FROM THE OLD PANEL & REINSTALLED THE HARDWARE ON THE NEW PANEL IAW DWG SRM 25-005; REV F.

Part: WINDOW — OPEN (COCKPIT) · airframe 65,895 hrs · 21,638 cycles

REJECTED T/O FOR F/O OPEN WINDOW 90KTS. OPEN AND RECLOSED WINDOW LOCKED AND LATCHED A/C OK TO CONTINUE.

Part: SKIN — DAMAGED (BS 507-530) · airframe 65,464 hrs · 21,453 cycles

DURING STRIPPED PAINT DAMAGED FUSELAGE EXT RT SIDE THE PACK NR 3 DOOR SCRATCH ABOUT 59" FROM STA 507 TO STA 560 BTWN L41-42. REMOVED PACK NR 3 PARTS TO GAIN ACCESS IAW MM 21-53-20-4, MM 21-53-02-2, MM 20-50-02. PERFORMED INSP, NO CRACK FOUND, PERFORMED MAP REQUIRED ON RWK AREA ATTACHED SHT. REMOVED RUST HINGES IAW SRM 51-21-01 VOL2. APPLIED CADPLAT IAW ACM7626, REMOVED SKIN FOUND CORROSION EXFOLIATION. REPAIRED FAB AND INST ON FRAMES IAW SRM53-00-01 FIG8 SHT1-3-4 VOL 1 SEE DET PART TRAVELER F170777-7-13-15-21-3-5. INSTALLED SKIN AND DOUBLER IAW DWG NCA6052. REPAIRED ANGLE LONG 48 RT IAW SRM53-10-00 VOL1 FIG 6. FAB PART IAW DETAIL PART TRAVELER F170777 AND IAW SRM 53-10-00 VOL 1 FIG6.

Part: FITTING — CRACKED (AILERONS) · airframe 65,464 hrs · 21,453 cycles

FOR CUSTOMER REQUEST REPLACE 1" CRACKED LT I/B AILERON FITTING P/N ARC0329-1. REMOVED LT INBD AIL IAW MM27-10-01-4. REMOVED ACTUATOR IAW MM27-13-01-4. REMOVED AND REPLACED BEARING DMD14-18D1-501 IAW MM57-44-01-2 BEARING DMD12-12B1-501 IAW MM57-44-01-2. HOLES DRILLED IAW SRM51-35-01 PAG1/13 VOL2. AFTER DRILL WR O/B HOLE SUPPORT RESULT WITHOUT MIN 2 EA EDGE DIST FROM SUPP LWR ED ACTUAL ED IS 0.30" INSTEAD OF .375" ATTACHED SKETCH. DURING SUPPORT INST FOUND CRACK LONG 6" LWR TEECAP AT STA XW 315,00 ATTACHED SKETCH, CAP CUT AT XW275 IAW EA NR 8-5710-103692 AND SRM 57-00-01 FIG11. CAP SECT FAB AND INSTALLED P/N F170826-3;-5;-7 IAW EA#8-5710-103692 AND SRM 57-00-01 VOL1 FIG 11. REINST INBD AILERON IAW MM27-1

Part: SHEAR TIE — CORRODED (BS 1257) · airframe 65,464 hrs · 21,453 cycles

CENTER WING LOWER BARREL SECTION. CORROSION ON FRAME TO SKIN LOWER ANGLES BETWEEN LONGERONS 50L-51L ON THE FWD SIDE AND LONGERONS 50L-51L, 51L-52L ON THE AFT SIDE OF FRAME 1257.4 NOT POSSIBLE TO REMOVE CORROSION NEED TO REMOVED FRAME FOOT AS CORROSION GOES UNDER FRAME BTWN LONG NR 50L AND LONG NR 51L STA 1257. REMOVED FRAME IAW SRM 51-33-01 P34/47 VOL2. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2, ORIG THK 0.071" MAT REMA .069" BTWN LONG NR 51L-52L, WITHIN LIMITS IAW SRM 53-00-01 FIG1A SHT4 BTWN LONG NR 50L AND LONG NR 51L MAT REMA .044" 38 PERCENT MAT REMOVED OUT LIMITS IAW SRM 53-00-01 FIG 1A SHT4 AND FIG 1B VOL1. DAMAGED FLANGE TRIMMED OUT REPAIR FRAME FABRICATED F171058-3. INSTALLED IAW SRM53-00-01

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

FWD CARGO COMPT FOUND 3 CRACKS ON CHANNEL BTWN STA 879 AND STA 959 X = 58 LT. REMOVED RAIL CHANNEL IAW SRM 51-31-02 VOL 2 PAR 2-5, CUTE CHANNEL SECTION AT STA 879 TO STA 939 X =58,00 LT IAW SRM 53-70-00 VOL 1 FIG 7 SHT 5. INSTALLED NEW CHANNEL N00252-3 AND SPLICE -7 WITH ANGLE -17 AND -5. INSTALLED BLIND RIVET FASTENER ON VERTICAL FLANGE ON -17 IAW SRM 53-70-00 VOL 1 FIG 7 SHT 5 AND SRM 51-38-01 VOL 2. REINSTALLED RAIL CHANNEL IAW SRM 51-31-02 VOL 2 PAR 2-5.

Part: SKIN — CORRODED (RT WING) · airframe 65,464 hrs · 21,453 cycles

RT WING LWR SKIN TANK AT XORS 250 ON DOUBLER BEAVER TAIL FOUND SEVERE CORROSION WITH EXFOLIATION. REMOVED CORROSION IAW SRM 57-00-01 FIG 8 SHT 3 4 VOL 1. REMOVED FASTENERS IAW SRM 51-34-01 PAGE 1/7 VOL 2. RECORDED RESIDUAL MTL. THK AND VERIFIED REWORK LIMITS IAW SRM 57-00-01 FIG 8 SHT 3 4 VOL 1. ACCOMPLISHED EA NR 8-5710-99397.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 65,464 hrs · 21,453 cycles

RT WING INB FLAP L/E EXISTING REPAIR AT STA XIFH240. EXISTING REPAIR REMOVED IAW SRM 57-30-00 VOL 2. FOUND RIB DISTORTED AND ILLEGAL REPAIR. REMOVED O/B SKIN AND CUT OUT SECTION. REMOVED 3 RIBS AND EXISTING ANGLE REPAIR IAW SRM 51-30-00 VOL 2. RIB P/N F172340-12 CUT TOO SHORT ON FITTING (NO ED). INSTALLED NEW 4 RIBS AND CUP IAW SRM 51-33-01 VOL 2 PAGE 34/47 AND DWG ARC2417, ARC3009 AND ARC2413. FABRICATED PARTS DETAIL PARTS TRAVELER NR F172340 AND DWG ARC2412 NEW SKIN FABRICATED AND INSTALLED IAW SRM 51-30-00 VOL 2 AND FEDEX EA, SEE DET PARTS TRAV N02340 / F172340. RUB STRIPS P/N FX-ARC2395-27 AND 29 INSTALLED IAW SRM 51-30-00 VOL 2.

Part: SKIN — DAMAGED (BS 1841 L50-51L) · airframe 65,464 hrs · 21,453 cycles

AFT CARGO INTERNAL FUSELAGE AT STA 1841 BETWEEN LONGERONS NR 50 AND 51 LT REPAIR ON CAP. EXISTING REPAIR REMOVED. CAP SECTION CUT BETWEEN LONGERONS NR 47 AND 48. CAP SECTION AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-30-00 FIG 5 AND DWG AGA3789. SEE DETAILED PARTS TRAVELERS N01317/ F172317.

Part: DOOR FRAME — MISREPAIRED · airframe 65,464 hrs · 21,453 cycles

MAIN CABIN R3 PASSENGER DOOR JAMB AT STA 1256 LONGERON NR 27 EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA NOT FOUND INSTALLED 2 FASTENERS IAW SRM 53-50-00 FIG 19 SHT 1. INSTALLED 2 MISSING FASTENERS IAW SRM 53-50-00 FIG 19 SHT 1. PERFORMED INSPECTION IAW EA NR 8-5310-99735 PART 1.

Part: DOOR FRAME — MISREPAIRED · airframe 65,464 hrs · 21,453 cycles

INTERNAL FUSELAGE CAC AREA AT STA 1156 TO 1158 BETWEEN LONGERONS 31 TO 28 LT SIDE EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA FOUND INSTALLED BOLTS INSTEAD OF HI-LOCKS IAW SRM 53-30-00 FIG 7 VOL 1. INSTALLED FASTENERS IAW SRM 53-30-00 FIG 7 VOL 1. PERFORMED INSPECTION IAW FEDEX EA NR 8-5330-99374 PART 1.

Part: RIB — BROKEN (LWS 320) · airframe 65,464 hrs · 21,453 cycles

LT WING ON L/E DROP FOUND INTERNAL RIB BROKEN AT STA XW 320. INNER SKIN AND INTERCOSTAL REMOVED IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND SRM 51-35-01 PAGE 1/13 VOL 2. CRACKED SECTION TRIMMED AND REPAIRED IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. REMOVED PARTS REINSTALLED IAW SRM 51-31-01 PAGE 36 /41 VOL 2 AND SRM 51-35-01 PAGE 1/13 VOL 2. MISSING NUT PLATE INSTALLED IAW SRM 51-35-01 PAGE 1/13 VOL 2.

Part: DOOR FRAME — MISREPAIRED (BS 1305) · airframe 65,464 hrs · 21,453 cycles

MAIN CABIN R3 PASSENGER DOOR JAMB AT STA 1305 LONGERON NR 27 EXISTING REPAIR. INSPECTION OF EXISTING REPAIR CARRIED OUT IAW ED 8-5100-7-5001 P2. FOUND 2 FASTENERS NOT INSTALLED ( SEE JPF N00742). FASTENERS INSTALLED IAW SRM 53-30-00 FIG 19. PERFORMED INSPECTION IAW EA NR 8-5310-99735.

Part: SKIN — CRACKED (LWS 320) · airframe 65,464 hrs · 21,453 cycles

LT WING ON L/E DROP FOUND 1 CRACK .050" LONG ON SKIN UPPER SURFACE AT STA XW 320 AFTER REMOVE PLATE ( REMOVED PART AND SEE NRC N00169 ). SKIN REPAIRED WITH DOUBLER IAW SRM 57-10-00 FIG 55 SHT 1 AND 2 VOL 1. SEE DETAILED PARTS TRAVELER N01887/ F171887.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

FWD CARGO COMPT TUNNEL AREA FOUND 1 CRACK 3" LONG ON WEB OF FWD JAMB AT STA 879 BTWN LONG NR 36 RT AND LONG NR 37 RT. REPAIRED DOOR JAMB WEB IAW SRM 53-00-01 VOL 1 FIG 10 SHT 3, ( REF SRM 53-50-00 VOL 1 FIG 1 SHT 2 ). FABRICATED PART IAW DETAIL PARTS TRAVELER N00258/F170258 AND SRM 53-00-01 VOL 1 FIG 10 SHT 3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

WITH REFERENCE TO NRC N F01023, FOUND EXFOLIATION CORROSION ON LOWER SIDE OF FRAME UPPER FLANGE AT STATION 1768 X = - 39.5 CENTER CARGO COMPARTMENT AFT BULKHEAD. CORROSION REMOVED IAW SRM 51-21-01 PAR 35 VOL 2. ORIG MATERIAL THICKNESS .095" (SRM 53-15-01 FIG 6 VOL 2 ). RESIDUAL MATERIAL THICKNESS .047". PERCENTAGE MATERIAL REMOVED 50 PERCENT. OUT OF LIMIT IAW SRM 53-00-01 FIG 1B VOL1 (ALSO CRACKED). AREA TRIMMED OUT AND REPAIR FABRICATED AND INSTALLED IAW SRM 53-00-01 FIG 9 VOL1. SEE DETAILED PARTS TRAVELERS F170924. CHANNEL ETC REINSTALLED IAW MM 20-50-02-2. ( REMOVED FOR ACCESS).

Part: PANEL — CRACKED (HORIZ STAB) · airframe 65,464 hrs · 21,453 cycles

DURING NDT INSP ON HORIZ STAB, FOUND TWO PANEL P/N 7208-1 AND 7205-1 WITH CRACKS. SEE ATTACHED SHEET FOR ALL DETAIL. SHORING INSTALLED, OPENED ACCESS, REPLACED 2 PANELS AND REMOVED SHORING IAW SB DC10-55-16 GROUP 1 AND EA# 8-5510-96066.

Part: TEE FITTING — CRACKED (L/E SLAT) · airframe 65,464 hrs · 21,453 cycles

LT WING SLAT NR 2 FOUND 1 CRACK 0.50" LONG AT STA XIS 247 ON TEE CAP INT SIDE (REF NRC N00168 ). REMOVED AND REPLACED LT NR 2 SLAT ASSY IAW JC 57-40-01-056 AND MM 27-80-01-4.

Part: SKIN — DENTED (BS 510) · airframe 65,464 hrs · 21,453 cycles

LOWER FUSELAGE EXT: 1 DEEP DENT 1 INCH BY 1 INCH MAX DEEP .060 INCH ON RT SIDE EXT SKIN AT STA 510 STR NR 28 RT. REFORMED DENT IAW SRM 53-20-00 FIG 13 SHT 14 NOTE B. NDI INSPECTION IAW SPM 08, NO CRACK FOUND. INSTALLED INTERNAL FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1 AND SRM 51-35-01 PAGE 1/13 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER NR F170215/N00215 AND IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1.

Part: LONGERON — CRACKED (BS 1741-1761) · airframe 65,464 hrs · 21,453 cycles

CTR CARGO COMPT SUMP AREA FOUND 1 CRACK 1" LONG ON LONGERON NR 47 LT BETWEEN STA 1741 AND STA 1761. EXISTING LONGERON REMOVED ( P/N AFA30-78-1 ) IAW SRM 51-35 01 PAGE 1/13 VOL 2. NEW LONGERON SECTION, STRAPS AND SPLICE FABRICATED IAW EA NR 8-5310-100640 SEE DETAILED PARTS TRAVELERS N01164/F171164. INSTALLED REPAIR IAW SRM 51-33-01PAR 6-10 & 51-35-01 PAR 1-5 VOL 2. AREA TREATED IAW SRM 51-21-01 PAR 31-24.

Part: DOOR FRAME — CRACKED (BS 1305) · airframe 65,464 hrs · 21,453 cycles

ON SURROUNDING OF JAMB L3 DOOR FOUND 1 CRACK 1" LONG ON WEB UPPER SIDE AT STA 1305 BTWN LONG NR 16 AND LONG NR 15. DOUBLER FABRICATED AND INSTALLED IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1 SEE DETAILED PARTS TRAVELER N01746/F171746.

Part: SKIN — DENTED (BS 515 S29L) · airframe 65,464 hrs · 21,453 cycles

LWR FUSELAGE: 1 DEEP DENT 5" BY 4" MAX DEEP .120 ON EXT LT SKIN AT STA 515 STR NR 29 LT SIDE. PERFORMED DENT IAW SRM 53-20-00 FIG13 SHT14 VOL 1 NOTE B. NDI INSPECTION IAW SPM 6-10-04, NO CRACK FOUND REPAIRED SKIN WITH FINGER DOUBLER IAW SRM 53-20-00 FIG13 SHT 2A SHT 14 VOL 1 AND SRM 53-35-01. FABRICATED PART IAW DETAIL PART TRAVELER NR F171120/N01120 AND SRM 53-20-00 VOL 1 FIG13 SHT2A AND 14.

Part: BEAM — CRACKED (BS 919) · airframe 65,464 hrs · 21,453 cycles

1 CRACK 1" LONG ON BEAM FWD CARGO COMPT AT STA 919 X= -47. DISCONNECTED TORSION BAR IAW MM25-52-02-2. REPAIRED BEAM IAW SRM 53-60-01 VOL 1 FIG 3. REINSTALLED TORSION BAR IAW MM 25-52-02-2.

Part: FLOORBEAM — UNKNOWN (FUSLEAGE) · airframe 65,464 hrs · 21,453 cycles

INTERNAL FUSELAGE FWD CARGO COMPARTMENT AT STA 1099 LONGERON 44 LT SIDE APPROX REPAIR ON FLOORBEAM. REMOVED AND REPLACED BEAM IAW DWG AFA0039

Part: SKIN — DAMAGED (RT WING) · airframe 65,464 hrs · 21,453 cycles

RT WING L/E SLAT TRACK CUT OUT STA XOS 890 EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 65,464 hrs · 21,453 cycles

CENTER CARGO DOOR EXTERNAL SKIN LWR AFT CORNER EXISTING REPAIR REPAIRED IAW 52-10-00 FIG 17 VOL 1.

Part: SKIN — DAMAGED (LT WING) · airframe 65,464 hrs · 21,453 cycles

LT WING L/E SLAT TRACK CUT OUT STA XOS 610 EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 51-30-00 VOL II.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 65,464 hrs · 21,453 cycles

FOUND CENTER CARGO DOOR EXTERNAL SKIN LWR AFT CORNER EXISTING REPAIR REPAIRED IAW SRM 52-10-00 FIG 17 VOL 1.

Part: SKIN — DAMAGED (LT WING) · airframe 65,464 hrs · 21,453 cycles

LT WING L/E SLAT TRACK CUT OUT STA XOS 890 EXISTING REPAIR REPAIRED IAW SRM 57-10-00 FIG 49 AND 51-30-00 VOL II.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

EXTERNAL FUSELAGE AT STA 1871 TO 1891 BETWEEN LONGERONS 51 AND 52 RT SIDE EXISTING REPAIR REMOVED AND REPAIR IAW SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

EXTERNAL FUSELAGE AT STA 1900 TO 1921 BETWEEN LONGERONS 51 AND 52 RT SIDE EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1.

Part: BULKHEAD — CRACKED (RT WING) · airframe 65,464 hrs · 21,453 cycles

TRANSFERRED FROM NRC FC25018: RT WING XORS 345 AND STR 43 FOUND CRACK IN LOWER BULKHEAD CAP. TRIMMED CRACKED LEG AND INSTALLED REPAIR TEE IAW SRM 57-20-00 FIG 27 SHT 24 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F170897/ N00897 & SRM 57-20-00 FIG 27 SHT 24 VOL 1.

Part: CHANNEL — CRACKED (BS 899-919) · airframe 65,464 hrs · 21,453 cycles

FWD CARGO COMPT FOUND 1 EA CRACK 4 INCHES LONG ON CHANNEL BETWEEN STA 919 & STA 899 X= -16 RT. CUT CHANNEL AT STATIONS 919 & 899 AND INSTALLED SPLICE AND NEW CHANNEL SECTION IAW SRM 53-70-00 VOL 1 FIG 7 SHT 3. FABRICATED PART IAW DETAILS PARTS TRAVELER N00230/F170230 & SRM 53-70-00 VOL 1 FIG 7 SHT 3.

Part: FRAME — CRACKED (LT WING) · airframe 65,464 hrs · 21,453 cycles

LT WING L/E STA XORS 100 LOWER SECTION FOUND 1EA CRACK ON FORMER 1.5 INCH LONG. FORMER REPAIRED IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. MATING FACE OF FORMER NDI'D IAW NDT SPN 06-10-01. NO CRACK FOUND. AREA PROTECTED IAW SRM 51-21-01 VOL 2. FORMER RE-FIT IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1.

Part: FRAME — CRACKED (LT WING) · airframe 65,464 hrs · 21,453 cycles

LT WING L/E STA XORS 538 LOWER SECTION FOUND 2 EA CRACK ON FORMER 1 INCH AND 2.5 INCH LONG. CRACKED AREA TRIMMED OUT & DOUBLER & FILLER FABRICATED IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. REPAIR CARRIED OUT IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1.

Part: FRAME — CRACKED (LT WING) · airframe 65,464 hrs · 21,453 cycles

LT WING L/E STA XORS 164 LOWER SECTION FOUND 1EA CRACK ON FORMER 1 INCH LONG. FORMER REPAIRED IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. PARTS FABRICATED IAW SRM 57-00-01 SHT 2 VOL 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

AVIONIC COMPT FOUND SKIN AND FRAME DEFORMED AT STA 295 LT SIDE X=50. CUT PORTION OF SKIN DAMAGE, TRIMMED FRAMES DAMAGE, FABRICATED PARTS IAW DETAIL PARTS TRAVELERS AND SRM 53-20-00 VOL 1 FIG 11 SHT 182 NR N01477/F171477. INSTALLED NEW PARTS IAW SRM 53-20-00 FIG 11 SHT 1 AND SRM 53-40-00 FIG 15 SHT 4 VOL 1. RESTORED TOP COAT AND SEAL IAW TF 110 AND DPS 2.510-4.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

INTERNAL FUSELAGE AT STA 285 Z=30 APPROX LT SIDE FRAME REPAIR. REMOVED EXISTING CAP REPAIR, TRIMMED OUT AND INSTALLED NEW CAP, FABRICATED PART IAW DETAIL PART TRAVELER N02459 AND SRM 53-40-00 FIG 15 SHT 4 VOL 1.

Part: BEAM — CRACKED (FUSELAGE) · airframe 65,464 hrs · 21,453 cycles

ONE EACH CRACK 1.50 INCH LONG ON BEAM FWD CARGO COMPT AT STA 1099 X=-58. REPAIRED BEAM IAW SRM 53-60-01 VOL 1 FIG 3.