N261UP

Part: DOOR — FAULTED (MAIN ENTRY) · airframe 80,553 hrs · 15,770 cycles

INSPECTION TYPE:NAMAIN ENTRY DOOR UPON ARRIVAL WOULD NOT OPEN ELECTRONICALLYPERFORMED OPS CHECK OF L1 DOOR OPS CHECKS PASSED FOUND EXTENDED AND NEEDED TO BE STOWED FOR OPERATION REF AMM 52-10-01

Part: SEAT — OUT OF POSITION (COURIER) · airframe 80,364 hrs · 15,679 cycles

L1 ENTRY DOOR LIFT BAR CONTACTS COURIER SEAT WHEN CLOSING, ADJUSTED COURIER SEATS AFT. PERFORMED OPS TEST OF L1 DOOR REF AMM 52-10-01, PB 201 DOOR NO LONGER MAKES CONTACT. THIS CLEARS M792141

Part: DISK — CRACKED (ZONE 500)

INDICATION IN BORE A ZONE CORNER, AMPLITUDE 2020MV. GE ENGINE SHOP MANUAL (ESM) EVALUATION/REJECTION LIMIT IS 1500MV.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,039 hrs · 15,498 cycles

INSPECTION TYPE:NAEMERG LIGHT LO BATT MSG DURING TESTREPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS TEST GOOD. IPC33-51-10-01 ITEM 005J

Part: SUPPORT ANGLE — CORRODED (AFT CARGO) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:1CAFT CARGO FLOOR BEAM SUPPORT ANGLE CORRODED AT X=3,Y=1841.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT ANGLE IAW VT-SAA EA 011-5310-01-A9512 REV I/R AND UPS EO MD11-5310-83234-A BY P.LAU (AR-830967) DATED 03/25/2022 (MAJOR).

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:C1AFT CARGO COMPARTMENT STEP UP AT STA 1841 HAS A CRACKED STIFFENER AT LONGERON 48L.REMOVED,FAB, REPLACE THE CRACK STIFFENER IAW DWG AGA7170 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (R/H WING) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 679.8 TO 685.9.REPAIREDCRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 679.85 TO 685.9 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (R/H WING) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692.0 TO 703.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 692.0 TO 703.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205 . (MAJOR)

Part: FORMER — CRACKED (RT WING L/E) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:1CRT WING FIXED L/E FORMER CRACK AT STA. XOS=667.79.REPAIRED RT WING FIXED L/E CRACKED FORMER AT STA. XOS=667.79 IAW VT-SAA EA 011-5754-01-A9516 REV I/R AND UPS EO MD11-5710-83236-A BY P.LAU (AR-830967) DATED 03/25/2022 (MAJOR).

Part: FORMER — CRACKED (L/H WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:4CL/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS. 584.891.REPAIRED CRACKED L/H WING FIXED L/E FORMER AT STA. XOS. 584.891 IAW VT-SAA EA 011-5740-01-A9515 REV. I/R AND UPS EO MD11- 5710-83235-A. (MAJOR) REF FAA FORM 8100-9 BY P. LAU (AR830967) DATED 03/28/2022.

Part: DOUBLER — CRACKED (R/H WING) · airframe 79,811 hrs · 15,356 cycles

INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 763.3 TO 768.2.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 763.3 TO 768.2 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: NONE — INOPERATIVE (DOOR) · airframe 79,644 hrs · 15,252 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR**L1 DOOR WILL NOT OPEN ELECTRICALLY. DEFERRED PER MEL 52-10-3-1-2-1-2. M768556 ASSIGNED, PLACARD INSTALLEDREPLACED S2-730 LOCK REL SOL, R2-177 DOOR ACT RELAY PER AMM 52-10-06 & 20-30-00 W/ REF IPC 52-34-01-01-911. RAN ALL WIRING PER WDM & LAMM 52-11. FOUND OPEN CIRCUIT AT C/P P1-385 PINS A & B LEVER ACT SW S1-211. REMOVED DEBRIS FROM BEHIND COURIER SEATS & FULLY STOWED SEAT ASSY CLOSING SEAT OPS CK GOOD. PER AMM 52-10-01. CLEARS M768556. PLACARD RMVD.

Part: NONE — NONE (DOORS) · airframe 79,622 hrs · 15,241 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** L1 DOOR DOES NOT WORK FROM INSIDE SWITCH. DEFERRED IAW MEL 52-10-3-1-2-1-2. L1 DOOR DOES NOT OPEN/CLOSE ELECTRICALLY.T/S PER WDM 52-11-01, FOUND GIRT BAR SWITCH S1-1090 STICKING, FREED UP SWITCH & PERFORMED OPS CK PER AMM 52-10-01-700-801. THIS CLEARS M768045, PLACARD REMOVED.

Part: NONE — NONE (DOOR) · airframe 79,622 hrs · 15,241 cycles

INSPECTION TYPE:N/AL1 DOOR DOES NOT OPERATE. DEFER L1 DOOR PER MEL 52-10-3-1-2-1, PLACARD INSTALLED, ITEM #M767960.OPERATED DOOR MULTIPLE TIMES FROM INSIDE AND OUTSIDE SWITCHES. NO FAULTS NOTED, DEFERRAL CLEARED.

Part: NONE — NONE (DOORS) · airframe 79,559 hrs · 15,214 cycles

INSPECTION TYPE:NAL1 DOOR INOP.OPS CHECK L1 DOOR IAW AMM 52-10-00. OPS CHECK GOOD M766663 CLEARED.

Part: LIGHT — NONE (CABIN) · airframe 79,353 hrs · 15,088 cycles

INSPECTION TYPE:N/AR1 MED FLOOR EMERGENCY LIGHT INOPR&R BULBS @ R1 MED FLOOR EMERGENCY LIGHT OPS CHECK GOOD REF AMM 33 50 00

Part: DOOR — INOPERATIVE (L1) · airframe 79,101 hrs · 14,916 cycles

INSPECTION TYPE:NAL1 DOOR ELECTRIC MODE INOP. OPENED DOOR PNUMATICALLY. ELECTRONIC FUNCTION RESTORED. ITEM DEFERRED IAW MEL 52-10-3-1-2-1-1FOUND L1 DOOR BOTTLE DEPLETED. RESET & SERVICED BOTTLE AS REQ AMM 12-54-04 LEAK CHECK BOTTLE & FITTING. NO LEAKS NOTED. THIS CLEARS DEFERRAL. PLACARD REMOVED.

Part: EVAS UNIT — NO TEST (COCKPIT) · airframe 79,101 hrs · 14,916 cycles

INSPECTION TYPE:NAWHILE PREFORMING TC-9197 EVAS TEST BOTH LH AND RH EVAS UNITS FAIL BLOWER TEST. WILL NOT RUN. MANUAL SWITCH ON CKS OK. ACCOMP. DMP 25-68-1 REMOVED AND PROCESSED. DEFERRED UNDEER MEL 25-68-1 CONTROL NUMBER M747080. PLACRD INSTALLED.INSTALLED NEW EVAS BOXES ON CAPTAIN & COPILOTS SIDES OF SEATS. IAW AMM 05-69-00, OPS CHECK GOOD. M747080 CLOSED. DMP REVERSED, PLACARD REMOVED. ESR IAW 25-60-00-90-001 & 002.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 78,973 hrs · 14,842 cycles

EMER LT BATT / LOW ON PREFLIGHT. ACCOMPLISHED M743368 ASSIGNED PLACARD INSTALLED.REPLACED EMERGENCY BATTERY REF AMM 33-51-01-000-802, OPS CK GOOD. REVERSED DMP.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 78,731 hrs · 14,667 cycles

INSPECTION TYPE: N/A DURING TAXI, NR 2 ENGINE FLAMED OUT, ALL ENGINE PARAMETER ROLLED BACK. NO FCC FAULTS ON ECU 2A ON 2B FAULTS, PER FON MTS NORMAL START, PER MD11 AMM 71-00-00. OPERATIONS TEST GOOD AT THIS TIME.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C AFT CARGO LT LOWER BILGE FRAME SHEAR TIE CHORD CRACKED AT STA 1841. REMOVED, FABRICATED AND INSTALLED SHEARTIE IN LT LOWER BILGE STA 1841 IAW SRM 51-35-01. (MINOR)

Part: SKIN — GOUGED (TE FLAP) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C WHILE INSTALLING THE LEFT MAIN LANDING GEAR FIXED BRACE ASSEMBLY, GEAR STAND DOOR OPENED AND CONTACTED THE LEFT I/B FLAP LOWER SKIN. REPAIRED GOUGED LT I/B FLAP LOWER SKIN BETWEEN XIFH 190 AND XIFH 213.05 IAW EA 011-5750-01-A8184 AND EO MD11-5750-76889-A. (MAJOR)

Part: FRAME — CRACKED (BS 469) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:C3AFT AVI COMP BILGE AREA L/H CANTED FRAME IS CRACKED AT STA 469.173.ACCOMPLISHED PERMANENT REPAIR ON CRACKED CANTED FRAME IN AFT AVIONICS COMPARTMENT AT STA 469.173 IAW MD11 SRM 53-10-07 REPAIR 1 FIGURE 201 REV. 66. (MAJOR)

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CFUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IS CRACKED.REPAIRED CRACKED FUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IAW SRM 53-10-07 REPAIR 1 FIG. 201. (MAJOR)

Part: SKIN — CORRODED (BS 2140-2163) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRT AFT FUSELAGE EXTERIOR SKIN HAS CORROSION BETWEEN STA 2140 - 2163.ACCOMPLISH PERMANENT REPAIR ON CORRODED RT AFT FUSELAGE SKIN BETWEEN STA 2140 - 2163 IAW MD-11 SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR SEAT TRACK STA 1381 -1521 X=8.50 HAS CORROSION.REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1371 AND 1531 X=8.50 IAW SRM 53-00-52 REPAIR 1 FIG 201 AND EA 011-5310-01-A8188 , EO MD11-5310-76615A. (MAJOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C SEAT TRACK IS CORRODED BETWEEN STA 1401-1521 AT X=8.50. REMOVED AND REPLACED SEAT TRACK IAW EA 011-5310-01-A8188 REV IR AND EO MD-11-5310-76615-A. (MINOR)

Part: SEAT TRACK — CORRODED (BS 1401-1501) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C, MAIN CARGO RT FLOOR AREA SEAT TRACK HAS CORROSION BETWEEN STA 1401 TO STA 1501 X= -75.25REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1391 AND 1531 X= -75.25 IAW SRM 53-00-52 REPAIR 1 FIG 201 , EA 011-5310-01-A8188 AND EO MD11-5310-76615-A. (MAJOR)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

3C MAIN CABIN RT FLOOR AREA AT STA 1481 FLOOR PANEL LANDING SUPPORT HAS SURFACE CORROSION. REMOVED CRACKED SUPPORT. FABRICATED AND INSTALLED IN MAIN CABIN RT FLOOR AREA AT STA 1481 IAW SRM 51-33-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

3C FWD CARGO COMPARTMENT. LT SIDE BILGE INTERCOSTAL, BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME HAS A CRACK. REMOVED CRACKED INTERCOSTAL. FABRICATED AND INSTALLED BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME IAW SRM 51-31-01.

Part: BRACKET — CRACKED (BS 1159) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CCAC COMPARTMENT STA 1159 TRUSS BRACKET AT LONGERON 27 RH IS CRACKED IN 2 PLACES.REMOVED CRACKED TRUSS BRACKET, FABRICATED AND INSTALLED BETWEEN STA 1139 AND 1159 AT LONGERON 27 RH IN CAC COMP. IAW MD11 SRM 51-30-01 AND DRAWING AFA7605. (MINOR)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C AFT CARGO BILGE AREA LOWER FRAME SUPPORT HAS A CRACK AT STA 1841 ABOVE LONGERON 43. REMOVED CRACKED FRAME SUPPORT, FABRICATED AND INSTALLED IN AFT CARGO AT STA 1841 ABOVE LONGERON 43 IAW SRM 51-35-01 AND DWG AGA7098. (MINOR)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CAFT CARGO DOOR JAMB LWR AFT ANGLE SUPPORT IS CORRODED.REMOVED, FABRICATED AND INSTALLED ZEE ANGLES ON AFT CARGO DOOR JAMB IAW SRM 51-31-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CCENTER CARGO COMP R/H INTERCOSTAL UNDER Z FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED CENTER CARGO COMP R/H INTERCOSTAL BETWEEN STA 5-11 AND STA 5-32 IAW SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CCENTER CARGO COMP MRH INTERCOSTAL UNDER Z-FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IN CENTER CARGO COMP BETWEEN STA 5-11 - 5-32. IAW SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (BS 1761-1781) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CCENTER CARGO COMP L/H SIDE INTERCOSTAL UNDER Z-FRAME BETWEEN STA 1761 AND 1781 HAS A CRACK.REMOVED, FABRICATED CRACKED INTERCOSTAL AND INSTALLED IN CETER CARGO LH SIDE UNDER Z-FRAME BETWEEN STA 1761 AND 1781 IAW DRAWING ACA7046 AND AMM 20-50-02-910-801. (MINOR)

Part: SKIN — GOUGED (LT HORIZ STAB) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C LT HORIZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 391.933 AND XFS 397.749 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

3C SUB FLOORBEAM AT APPROX STATION 6 - 73, LONGERON 43, LT CORNER IS CRACKED AT ITS ANGLE CHANGE. REMOVED CRACKED SUB FLOORBEAM, FABRICATED AND INSTALLED AT STATION 6 - 73, LONGERON 43 LT IAW SRM 51-31-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CFWD CARGO RT SIDE BILGE INTERCOSTAL BETWEEN STA 6-30 AND 6-50 CRACKED AT AFT UPPER SIDE.REMOVED , FABRICATED AND INSTALLED INTERCOSTAL AT FWD CARGO BETWEEN STA 6-30 AND 6-50 IAW SRM 51-33-01 AND DRAWING ACA7049. ( MINOR)

Part: SKIN — GOUGED (LT HORIZ STAB) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C LT HORZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 351.215 AND XFS 357.032 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).

Part: SUPPORT FRAME — CRACKED (RT WING / BODY) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR/H WING TO BODY AT STRINGER 31 RH HAS VERTICAL ATTACHMENT SUPPORT FRAME CRACKED.REMOVED, FABRICATED CRACKED SUPPORT FRAME AND INSTALLED AT RH WING TO BODY AT STRINGER 31 IAW DRAWING ANB7143 AND SRM 51-35-01. (MINOR)

Part: ANGLE — CRACKED (FAIRING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CL/H UPPER WING TO BODY FAIRING ATTACH FRAME HAS BOTTOM L-ANGLE CRACKED AT STA 1401.REMOVED FABRICATED AND INSTALLED L-ANGLE AT L/H WING TO BODY FRAME AT STA 1401 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRH UPPER WING TO BODY AREA UNDER R3 DOOR AT LONGERON 28 RH HAS CORROSION.REPAIRED LONGERON 28 RH AT STA 1300 IAW EA 011-5300-01-A8170 I/R AND UPS EO MD11-5300-76521-A ( MINOR)

Part: PANEL — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CL/H UNDERWING BARREL CANTED PANEL CRACKED AT STA X=1236.8 Z=100.ACCOMPLISHED PERMANENT REPAIR OF CRACKED LH UNDERWING BARREL CANTED PANEL AT STA 1236.8 IAW EO.MD11-5310-76331-A REV 05/18/2020. (MAJOR)

Part: BELTFRAME — DENTED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 695 LONGERON 12R. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN BELT FRAME AT STA 695 LONGERON 12R IAW EA 011-5310-01-A8171 REV I/R AND EO MD11-5310-76700-A. (MAJOR)

Part: SHEAR TIE — CRACKED (LEFT) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CCENTER WING TANK RH ACCESS ENTRANCE STRUTURE UPPER LH SHEAR TIE CRACKED.REMOVED, FABRICATED CRACKED SHEAR TIE AND INSTALLED IN CENTER WING TANK RH ACCESS ENTRANCE IAW DRAWING APB7351-2 AND MD-11 SRM 51-30-01. (MINOR)

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR3 DOOR AFT DOOR JAMB AT STA 1341 LONGERON 15R T-FITTING IS CRACKED,REMOVED, FABRICATED AND INSTALLED R3 DOOR AFT DOOR JAMB T-FITTING AT STA 1341 LONGERON 15R IAW DRAWING AEA7568. (MINOR)

Part: BELTFRAME — DENTED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 715 LONGERON 13R. CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON BELT FRAME IN MAIN CABIN AT STA 715 LONGERON 13R IAW EA 011-5310-01-A8168 REV I/R AND EO MD11-5310-76728-A. (MAJOR)

Part: BULKHEAD — DAMAGED (NR 1 PYLON) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C NR 1 PYLON INTERNAL BULKHEAD INSIDE ACCESS PANELS 438CR/DR HAS ELONGATED HOLE. REPAIRED ELONGATED HOLE ON NR 1 PYLON BULKHEAD WEB AT YWN 315.500 INSIDE ACCESS PANEL 438CR/DR IAW EA 011-5410-01-A8220 AND EO MD11-5410-76813-A. (MAJOR)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C MAIN CABIN L3 DOOR LWR FWD DOOR JAMB WEB CRACKED BETWEEN STA 1256.75 AND 1250.75 BETWEEN DOOR STOP 7 AND Z-19. CUTOUT DAMAGE, FABRICATED REPAIR DOUBLER AND ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN L3 DOOR JAMB BETWEEN STA 1256.75 AND 1250.75 BETWEEN DOOR STOP 7 AND Z-19 IAW EA 011-5310-01-2020 REV IR AND EO MD11-5310-76654-A. (MAJOR)

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CMAIN CABIN T-FITTING CRACKED AT AFT END AT STA 1341 LONGERON 15L AFT OF L3 DOOR.REMOVED, FABRICATED AND INSTALLED MAIN CABIN T-FITTING AT STA 1341 LONGERON 15L IAW DRAWING AEA7568. (MINOR)

Part: FRAME — WORN (TAILCONE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CTAIL CONE FRAME AT RH UPPER GUIDE PIN WORN THRU.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)

Part: FRAME — CRACKED (TAILCONE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CTAILCONE RH FRAME CRACKED AT MIDDLE GUIDE PIN.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-01 REPAIR 1 FIG 201. (MINOR).

Part: FRAME — WORN (TAILCONE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CTAILCONE FRAME AT LH MIDDLE GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)

Part: FRAME — WORN (TAILCONE) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:C3TAILCONE FRAME AT LH UPPER GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)

Part: STRINGER — CRACKED (LT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C LT WING STRINGER 40 IS CRACKED BETWEEN XORS 737.6 AND XORS 772.5.CUT OUT DAMAGE. FABRICATED REPAIR PARTS AND ACCOMPLISHED PERMANENT REPAIR ON LT WING STRINGER 4O BETWEEN STA XORS 737.6 AND XORS 772.5 IAW SRM 57-00-03 REPAIR 4, FIG 201 REV 66. (MAJOR)

Part: SKIN — CRACKED (TE FLAP) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C LT WING UPPER SURFACE T/E WEDGE SKIN IS CRACKED JUST O/B OF I/B AILERON. CUTOUT DAMAGE AREA AND ACCOMPLISHED PERMANENT REPAIR ON LT WING UPPER SURFACE T/E WEDGE SKIN JUST O/B OF I/B AILERON IAW SRM 57-50-01, REPAIR 6 FIG 202 REV-66 (MAJOR).

Part: CROSSBEAM — CRACKED (R3 DOOR) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR3 DOOR PLUG UPPER AFT CROSS BEAM IS CRACKED.REPLACED R3 DOOR PLUG UPPER AFT CROSS BEAM IAW SRM 51-35-01 DRAWING ADA3462. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 667.67-673.76.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 667.67 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOOR — GOUGED (A/C BAY) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CL/H A/C BAY ACCESS DOOR 113DL HAS A GOUGE ON INTERIOR AFT SIDE FLAT EDGE.ACCOMPLISHED PERMANENT REPAIR OF L/H AIRCONDITION DOOR INTERIOR AFT SIDE IAW EA 011-5200-01-A8164 AND EO MD11-5240-76587-A. {MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRT WING FIXED L/E SKIN BEADED DOUBLER IS CRACKED AT XOS-499.CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON RH WING LE SKIN BEADED DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CL/H WING L/E SPLICE DOUBLER IS CRACKED JUST O/B OF #12 SLAT TRACK.REPLACED LH WING L/E SPLICE DOUBLER IAW SRM 51-33-01 AND DRAWING ARB3954. (MINOR)

Part: SKIN — CRACKED (LT WING SLAT) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C, LT OTBD WING L/E SKIN IS CRACKED JUST OTBD OF NR 7 SLAT TRACK.ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-40-01 REPAIR 17 FIGURE 201 REV 66. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS. 774.8529.REPAIRED CRACKED R/H WING FIXED L/E LOWER SKIN AT STA. XOS. 774.8529 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E PANEL LANDING INTERNAL DOUBLER IS CRACKED AT STA. XOS. 906.REPAIRED CRACKED R/H WING FIXED L/E PANEL LANDING INTERNAL DOUBLER AT STA. XOS.906 IAW SRM 57-40-03 REPAIR 1 FIG. 201 (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 661 - 667.REMOVED DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 661 - 667 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)

Part: SKIN — CRACKED (LE SLAT) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CR/H WING #1 SLAT EXTERIOR SKIN IS CRACKED BETWEEN STA. 185-191.REPAIRED CRACKED R/H WING #1 SLAT EXTERIOR SKIN BETWEEN STA. 185-191 IAW SRM 57-40-01 REPAIR 8 FIG. 201. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRT WING FIXED L/E PANEL LANDING CRACKED AT XOS 615.REMOVED, FABRICATED AND INSTALLED RT WING FIXED L/E LANDING / DOUBLER BETWEEN STA XOS 602 - XOS 629 IAW DWG ARB1180 AND SRM 51-31-01. { MINOR }

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED AT XOS 789.REMOVED AND INSTALLED NEW SPLICE DOUBLER AT RT WING FIXED L/E SKIN AT XOS 789. IAW DRAWING ARB3954 AND MD11 SRM51-33-01. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,606 hrs · 14,572 cycles

INSPECTION TYPE:3C LT O/B WING L/E BEADED DOUBLER IS CRACKED JUST I/B OF NR 12 SLAT TRACK BETWEEN XOS 772 AND XOS 776. CUTOUT DAMAGE, FABRICATED PART AND ACCOMPLISHED PERMANENT REPAIR OF LT WING L/E BEADED DOUBLER O/B OF NR 12 SLAT TRACK BETWEEN XOS 772 AND XOS 776 IAW SRM 57-40-02 FIG 205 REPAIR 15 REV 66. (MAJOR)