N270UP

Part: DOUBLER — CRACKED (RT WING LE) · airframe 65,866 hrs · 18,436 cycles

INSPECTION TYPE: C3, MAJOR REPAIR. RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPX. STA XOS-635. REMOVED, FABRICATED, REPAIRED THE CRACKED BEADED DOUBLER AT STA XOS-635 IAW SRM 57-40-02 REPAIR 15 FIG 205, REV 69.01. (MAJOR)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 65,866 hrs · 18,436 cycles

INSPECTION TYPE:C3BULGE UNDER MOONMAT CENTER OF COURIER AREA AT STA X=0.00 BETWEEN Y=411 - Y=441.REMOVED, REPAIRED CORROSION AT SEAT TRACK AT STA X=0.00 AND BETWEEN Y=411 - Y=441 IAW EA 011-5320-01-A9799 IR , DATED 01/10/2023 AND UPS EO MD11-5310-85649-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,300 hrs · 18,138 cycles

INSPECTION TYPE:NAR1 DOOR PRESSURE LIGHT DOES NOT ILLUMINATE DURING PREFLIGHT TEST. DEFERRED SLIDE PRESSURE TEST INDICATIONS SYSTEM PER MEL 25-61-2 DMP C/WRELAMPED THE PTT SWITCH REF AMM 25-61-04. OPS TEST OK, PLACARD REMOVED.

Part: DOOR — INOPERATIVE (DOOR) · airframe 65,290 hrs · 18,132 cycles

INSPECTION TYPE:NA** SDR FILED OPEN** R1 DOOR SLIDE REMOTE PRESSURE TEST BUTTON INOP. DEFERRED REMOTE R1 SLIDE PRESSURE TEST FUNCTION IAW MEL 25-61-2. ASSIGNED M786461 PLACARD INSTALLED & DMP C/W.

Part: NONE — NONE (FUSELAGE) · airframe 64,783 hrs · 17,854 cycles

INSPECTION TYPE:NA** ATB SDR FILED** NO EMERGENCY DEC'D**A/C LANDED W/OUT INCIDENT** LEVEL 2 "AIR SYS 3 PRES LO" AIR TURN BACK DUE TO ICING COND AT DEST.R&R HIGH STAGE MANIFOLD PRESSURE SENSOR PER AMM 36-12-04-000-801, OPS CHECK, SYSTEM CHECK NORMAL, FOB BEFORE ENG. RUN 39,800 FOB AFTER ENG RUN 39,000 IPC 36-11-20-04

Part: NONE — INOPERATIVE (DOOR) · airframe 64,398 hrs · 17,687 cycles

INSPECTION TYPE:N/ATEST LT. ON R1 ENTRY DOOR INOP.DEFERRED PER MEL 25-61-2 & ACCOMPLISHED DMP 25-61-2 R1 SLIDE PRESS. OK. ASSIGNED M-764325. EACH FLT RE-INSP. REQ. REPLACED BATTERIES REF 25-61-04 OPS NML.

Part: SKIN — CRACKED (BS 535 L33R) · airframe 63,966 hrs · 17,488 cycles

INSPECTION TYPE:N/AFUSELAGE SKIN CRACK AT RIGHT SIDE AIR CONDITIONING DOOR OPENINGACCOMPLISH FUSELAGE SKIN REPAIR IAW EO 80909-B

Part: CABLE — BROKEN (PAX DOOR) · airframe 63,724 hrs · 17,364 cycles

WHILE CLOSING THE LEFT SIDE CREW ENTRANCE DOOR, ONE OF THE CABLES BROKE. R&R L1 DOOR AFT LOWER DRIVE CABLE PER MM 52-11-03, PRIOR TO RIG/ OPS CHECK FOUND DAMAGED SPRING AND FRAYED CABLE. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1 M746276 ASSIGNED, PLACARD INSTALLED. PN ON/OFF 54913809CW16420REPLACED UPPER SPRING CARTIAGE ASSY & LOWER PULLEY SPRING, REF 52-11-03. ADJUSTED CABLES, REF AMM 52-11-02..

Part: SENSOR — FAILED (ANTI-ICE) · airframe 63,500 hrs · 17,248 cycles

INSPECTION TYPE:NA**ATB - SDR FILED OPEN - NO EMERG DECLARED - NO EQUIP USED.** LVL 1 ANTI -ICE SENSOR FAIL AT FL240 ON CLIMBOUT. MEL 36 10 2 1 DEFER PNEU SUPPLY 1 DMP C/W.

Part: CASE — CRACKED (#1 ENGINE FAN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C NR 1 ENGINE FAN CASE IS CRACKED AT 5 O'CLOCK POSITION JUST AFT OF NOSE COWL ANTI-ICE VALVE. REPAIRED CRACKED NR 1 ENGINE FAN CASE AT 5 O'CLOCK POSITION IAW UPS EO 4000-7230-79031-A. MINOR

Part: HINGE — CORRODED (LT O/B FLAP) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: C2 LT WING OUTBOARD FLAP OUTBOARD HINGE BORE HAS CORROSION. REPAIRED CORRODED LT OUTBOARD FLAP OUTBOARD HINGE BORE, IAW VT-SAA EA 011-5740-01-A8829 REV I/R AND UPS EO MD11-5740-79149-A. (MINOR)

Part: HINGE — CORRODED (RT O/B FLAP) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: C2 RT WING OUTBOARD FLAP INBOARD HINGE LOWER LUG BORE CORRODED. REPAIRED CORRODED RT OUTBOARD FLAP INBOARD HINGE LUG BORE, IAW VT-SAA EA 011-5740-01-A8834 REV I/R AND UPS EO MD11-5740-79170-A. (MINOR)

Part: LUG — GOUGED (RT WING AILERON) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT OUTBOARD AILERON ACTUATOR ATTACH FITTING LUGS ARE GOUGED. REPAIRED GOUGED RT OUTBOARD AILERON ACTUATOR ATTACH FITTING LUGS, IAW VT-SAA EA 011-5751-01-A8822 REV IR AND UPS EO MD11-5750-79096-A. (MINOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0788-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 36 - X= 47.5 IAW VT-SAA EA 011-5320-01-A8824 REV IR AND UPS EO MD11-5310-79107-A. MINOR

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE:2CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 AND X= -57.5.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70 AND X= -57.5 IAW VT-SAA EA 011-5310-01-A8835 REV. I/R AND UPS EO MD11-5340-79191-A. (MAJOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0789-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 47.5 - X= 62.1 IAW VT-SAA EA 011-5320-01-A8812 REV IR AND UPS EO MD11-5310-79073-A. MINOR

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 52 IS CORRODED AT STA. 5-11.REPAIRED CORRODED LONGERON 52 BETWEEN STA. 5-0 TO 5-32 IAW VT-SAA EA 011-5310-01-*A8818 REV. I/R AND UPS EO MD11-5310-79192-A. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: C2 MAIN CABIN SEAT TRACK CORRODED AT STA 421-443 RBL X-27.50. REMOVED, FABRICATED AND REPLACED CORRODED SEAT TRACK, IAW SRM 51-31-01, 51-33-01 VT-SAA EA 011-5310-01-A8808 I/R AND UPS EO MD11-5310-79153-A. (MINOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE :2 C FLOOR PANEL NR WSP0790-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 62.1 - X= 73.3 IAW VT-SAA EA 011-5320-01-A8807 REV IR AND UPS EO MD11-5310-79067-A. MINOR

Part: DOUBLER — CHAFED (TAIL CONE) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C TAIL CONE RT UPPER PRODUCTION DOUBLER REPAIR FILLER HAS DEEP CHAFE DAMAGE. REMOVED AND REPLACED CHAFED TAIL CONE RT UPPER PRODUCTION DOUBLER REPAIR FILLER, IAW UPS EO MD11-5350-66790-A. (MINOR)

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT WING LOWER SKIN FUEL ACCESS PANEL 636AB LANDING HAS 2 EA CRACKS. REPAIRED 2 EA CRACKS ON RT WING LOWER SKIN FUEL ACCESS PANEL 636AB LANDING, IAW MD-11 SRM 57-20-02, REPAIR 5, FIGURE 201. (MINOR)

Part: LONGERON — CORRODED (CAC) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LONGERON 47 LT HAS CORROSION AT STA 6-90 AND 6-100. REPAIRED CORRODED LONGERON 47 LT BETWEEN STA. 6-70 TO 6-100, IAW SRM 53-00-05 REPAIR 1 FIG 201 & 202. (MAJOR)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT WING INBOARD FLAP NR 2 ROLLER ACCESS COVER IS DENTED AND GOUGED AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0. REPAIRED DENTED RT INBOARD FLAP NR 2 ROLLER ACCESS COVER AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0, IAW SRM 57-00-01 REPAIR 1 FIG 201. (MAJOR)

Part: FLOOR SUPPORT — CRACKED (CENTER CARGO BAY) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE :2 C CENTER CARGO FLOOR SUPPORT IS CRACKED AT STA 1521 BETWEEN LBL 25 & RBL 25. R & R CRACKED CENTER CARGO FLOOR SUPPORT AT STA 1521 BETWEEN LBL 25 - RBL 25 IAW MD-11 SRM 51-35-01. MINOR

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0785-502 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 27.5 - X= 36 IAW VT-SAA EA 011-5310-01-A8809 REV. IR AND UPS EO MD11-5310-79066-A. MINOR

Part: SEAT TRACK — CORRODED (COURIER AREA) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C COURIER AREA SEAT TRACK IS CORRODED BETWEEN STA 400.34 TO 481.0 AND X= -36. REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA 400.34 TO 481.0 AND X= -36, IAW DWG WSP0826 AND SRM 51-31-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD. CARGO) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LOWER FWD CARGO INTERCOSTAL IS CRACKED AT STA 6-50 AND LONG 43L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0785-502 IS CORRODED. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X=0 - X= -8.50 IAW VT-SAA EA 011-5320-01-A8814 REV IR AND UPS EO MD11-5310-79059-A. MINOR

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WING LOWER SKIN FUEL ACCESS PANEL 536AB LANDING HAS 4 CRACKS. REPAIRED 4 EA CRACKS ON LT WING LOWER SKIN FUEL ACCESS PANEL 536AB LANDING, IAW MD-11 SRM 57-20-02, REPAIR 5, FIGURE 201. (MINOR)

Part: TEE FITTING — CRACKED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: C2 MAIN CABIN LONGERON 15L TEE ANGLE IS CRACK AT STA 1341. REMOVED,FABRICATED AND REPLACED CRACKED LONG 15L TEE ANGLE, IAW SRM 51-33-01, 51-35-01 AND DWG AEA7568-21 (MINOR).

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 C FLOOR PANEL WSP0785-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= -27.5 - X= -36 IAW VT-SAA EA 011-5310-01-A8810 REV IR AND UPS EO MD11-5320-79065-A. MINOR

Part: SEAT TRACK — CORRODED (COURIER AREA) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C COURIER AREA SEAT TRACK IS CORRODED BETWEEN STA 459.277 & 515.00 AND BETWEEN X=68 TO X=77.58. REMOVED, FABRICATED AND REPLACED SEAT TRACK, IAW DWG WSP0826-509 AND SRM 53-20-52. (MINOR)

Part: FLOOR SUPPORT — CORRODED (COURIER AREA) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C FLOOR PANEL SUPPORT UNDER LAV HAS HEAVY CORROSION. REMOVED AND REPLACED CORRODED FLOOR PANEL SUPPORT UNDER LAV BETWEEN STA 392-440 AND BETWEEN X= -8.5-X= -27.5, IAW MD-11 SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (RT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE RIB STIFFENER IS CRACKED AT OUTBOARD END OF ACCESS PANEL 618FB. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE RIB STIFFENER AT OUTBOARD END OF ACCESS PANEL 618FB, IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: SKIN — CRACKED (L/H WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE LOWER SKIN IS CRACKED AT STA XOS 500.00. REPAIRED CRACKED LT WING FIXED LEADING EDGE LOWER SKIN AT STA XOS 500.00, IAW SRM 57-40-01 REPAIR 17 FIG 201. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 685.94 TO 692.0. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 685.94 TO 692.0, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 661.71 TO 667.67. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 661.71 TO 667.67, IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SUPPORT — CRACKED (RT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT WING FIXED LEADOMG EDGE SUPPORT ANGLE OUTBOARD SIDE OF REFUELING CONTROL PANEL IS CRACKED INSIDE ACCESS PANEL 619CB. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE SUPPORT ANGLE OUTBOARD SIDE OF REFUELING CONTROL PANEL INSIDE ACCESS PANEL 619CB, IAW MD-11 SRM 51-35-01. (MINOR)

Part: FORMER — CRACKED (LT WING) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE FORMER IS CRACKED INBOARD OF NR 9 SLAT TRACK. REMOVED AND REPLACED CRACKED LT WING FIXED LEADING EDGE FORMER INBOARD OF NR 9 SLAT TRACK, IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: DOUBLER — GOUGED (FUSELAGE SKIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C EXTERIOR FUSELAGE SKIN REPAIR DOUBLER IS GOUGED AT STA 1153 AND BETWEEN L43R TO 45R. REPAIRED GOUGED EXTERIOR FUSELAGE SKIN REPAIR DOUBLER AT STA 1153 AND BETWEEN L43R TO 45R, IAW VT-SAA EA 011-5530-01-A8828 REV I/R AND UPS EO MD11-5330-79137-A. (MAJOR)

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT MLG WHEEL WELL OUTBOARD WEB HAS VERTICAL STIFFENER CRACKED 2ND FROM FWD END. REMOVED, FABRICATED AND REPLACED STIFFENER, IAW DWG ANB7203 AND SRM 51-35-01. (MINOR)

Part: CAP — CRACKED (UNDERWING PANEL) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT UNDERWING CANTED PANEL CAP IS CRACKED AT STA 1236.8 AND Z= -100. REPAIRED CRACKED LT UNDERWING CANTED PANEL CAP AT STA 1236.8 AND Z= -100, IAW UPS EO MD11-5310-78998-A. (MAJOR)

Part: SEAT TRACK — CRACKED (COURIER AREA) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C LT WHEEL WELL AFT OUTBOARD WEB HAS VERTICAL STIFFENER CRACKED 3RD FROM FWD. REMOVED AND REPLACED STIFFENER, IAW SRM 51-35-01. (MINOR)

Part: ATTACH FITTING — CRACKED (RT OB FLAP) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2 CR H OB FLAP IB HINGE ATTACH FITTING INSIDE FLAP IS CRACKED AT LOWER END. R & R RT OB FLAP IAW EO MD11-5750-959-D. MINOR

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: C2 MAIN CABIN COURIER FLOOR PANEL HAS CORROSION AT UPPER SKIN. REPAIRED CORRODED COURIER FLOOR PANEL UPPER SKIN, IAW VT-SAA EA011-5320-01-A8806 REV I/R AND UPS EO MD11-5320-79082-A. (MINOR)

Part: STIFFENER — CRACKED (RT MLG W/W) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE: 2C RT MLG WHEEL WELL OUTBOARD AFT 3RD STIFFENER FROM FWD IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG WHEEL WELL OUTBOARD AFT 3RD STIFFENER FROM FWD, IAW MD-11 SRM 51-31-01. (MINOR)

Part: SKIN — CRACKED (MAIN CABIN) · airframe 63,331 hrs · 17,145 cycles

INSPECTION TYPE:2CR-3 DOOR FWD. JAMB INNER SKIN IS CRACKED BETWEEN STA. 1256.75 TO 1250.75 AND BETWEEN DOOR STOPS 6 & 7.REPAIRED CRACKED R-3 DOOR FWD JAMB INNER SKIN BETWEEN STA. 1256.75 TO 1250.75 AND BETRWEEN DOOR STOPS 6 & 7 IAW VT-SAA EA 011-5310-01-A8816 REV. I/R AND UPS EO MD11-5330-79190-A. (MAJOR)

Part: BATTERY — LOW VOLTAGE (COCKPIT) · airframe 62,473 hrs · 16,763 cycles

INSPECTION TYPE:N/A EMERGENCY LIGHT BAT LOW. R&R EMERGENCY BATTERY IAW MM 33-50-00 & IPC 33-51-00 SYSTEM OPS CHECKS NORMAL. ESR: MM 33-50-00 & IPC 33-51-00.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 62,006 hrs · 16,566 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** L1 DOOR WONT ARM.DEFERRED L1 DOOR SLIDE INOP PER MEL 52-10-3-1-2-1-1. PLACARD INSTALLED.REPOSITIONED AIR& BAR PER MM 25-61-01, OPS CK GOOD. THIS CLEARS M 704223, DMP REVERSED.

Part: LIMIT SWITCH — OUT OF ADJUST (L1 DOOR) · airframe 61,990 hrs · 16,558 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** L1 DOOR WONT CLOSE COMPLETELY NOR ARM. FOUND CLOSED LIMIT SWITCH INTERMITTENT, CLOSED DOOR AND DEFERRED (ILLEG) MEL 52 10 3 1 2 1. DEFERRED ITEM CONTROL #M703778. NO DMP. PLACARD INSTALLED.REPLACED L1 DOOR CLOSED LIMIT SWITCH PER AMM 52-11-02, ADJUSTED THE CLOSED LIMITS SWITCH PER AMM 52-1-02-830-805 TO GAIN PROPER FIT. OPS CK GOOD, THIS CLEARS M 703878, PLACARD REMOVED ESR 52-11-20-01-005.

Part: TEST SWITCH — INOPERATIVE (R1 DOOR) · airframe 61,928 hrs · 16,529 cycles

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** R-1 DOOR EVAC SLIDE REMOTE PRESSURE . PRESS TO TEST IND. SYS. INOP. PLACED R-1 DOOR PRESS TO TEST IND. FOR DOOR EVAC SLIDE ON MEL # 25-61-2. C/W DMP 25-61-2. PLACARD INSTALLED M 702509 ASSIGNED.REPLACED PRESS TO TEST SWITCH PER AMM 25-61-04-400-801 OPS CK GOOD. THIS CLEARS DEFERRAL M 702509.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 61,922 hrs · 16,525 cycles

INSPECTION TYPE:NAL1 DOOR SLIDE WILL NOT ARM. DEFERRED L1 DOOR IAW MEL 53-10-3-1-2-1. PLACARD INSTALLED. M702390 OPENED.VERIFIED PROPER SLIDE & GIRT BAR INSTALLATION. ARMED & DISARMED SLIDE MULTIPLE TIMES. SYS CKS GOOD AT THIS TIME. ARM LIGHT & STATUS MSG OPERATE PROPERLY. REF AMM 25-61-15-400-801. THIS CLEARS M702390 & PLACARD REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 61,922 hrs · 16,525 cycles

INSPECTION TYPE:NALEVEL 1 CABIN DOOR FWD L ILLUMINATEDEXERCISED DOOR SLIDE HANDLE TO ARMED POSITION AND FWD L DOOR INDICATION CLEARED. REF 52-11-02

Part: DOOR — INOPERATIVE (L1) · airframe 61,747 hrs · 16,465 cycles

INSPECTION TYPE:N/ACABIN DOOR FWD L WILL NOT COMPLETLY CLOSEAFTER OPOERATIONAL TEST OF CREW REST IAW AMM 25-24-06-700-801 L1 PASSENGER DOOR SHOW NORMAL OPS. THIS CLEARS M699830

Part: CONTROL VALVE — INOPERATIVE (PRIMARY TRIM) · airframe 61,621 hrs · 16,406 cycles

INSPECTION TYPE:N/ADIVERSION - LEVEL 2 STAB OUT, TRIM CLIMBING OUT 4000' WITH A PILOT ON TRIM WORK PERFECT.DEFERRAL WAS APPLIED NOT KNOWING THE SOURCE OF THE STAB OUT MESSAGE HORIZONTAL STAB LVDTS WORKING NORMAL. FOUND #1 PRIMARY TRIM CONTROL VALVE FAULTY. R/R PRIMARY TRIM VALVE IAW AMM 27-43-40. OPS CK/LK CK GOOD. THIS CLEARS M697018

Part: ENGINE — FLAMED OUT (NR 2) · airframe 60,839 hrs · 16,093 cycles

NR 2 ENGINE FLAMED OUT ON DESCENT. EMERGENCY DECLARED. A/C TAKEN OUT OF SERVICE. RECEIVED A LEVEL 2 OIL PRESSURE MESSAGE. NR 2 ENG OIL PRESSURE GAUGE REMAINED NORMAL. ACCOMPLISHED ENGINE CHANGE PER TC 9103.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 60,838 hrs · 16,092 cycles

ENGINE 2 FLAME OUT ON DECENT. EMERGENCY DECLARED. PERFORMED WINDMILLING INSPECTION. PERFORMED EXTERNAL INSPECTION FOLLOWING EXPOSURE TO FIRE EXTINGUISHING AGENT. DID GVI OF ENGINE EXTERNAL COMPONENTS. DID BORESCOPE INSPECTION OF COMBUSTION CHAMBER, HPT BLADES & VANES STAGES 1,2 AND LPT STAGE BLADES. REPLACED FMV ON #2 ENGINE. LEAK AND OPS CHECK SATISFACTORY.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,817 hrs · 16,084 cycles

LEVEL 1 EMER 1 RT BATT LOW DURING TEST. R&R'D EMERGENCY POWER SUPPLY FOR EMERGENCY LIGHTING PER AMM 33-61-01-400-802. ESR: IPC 33-51-01-008

Part: ENGINE — FIRE (NR 2) · airframe 60,322 hrs · 15,861 cycles

EMERGENCY DECLARED - LEVEL 2 ENGINE OIL PRESS LOW ON ENGINE #2 2 PSI RED BOXED ON ENGINE INSTRUMENT. TOWER NOTIFIED US THAT ANOTHER UPS AIRCRAFT REPORTED A FIRE #2 ENGINE. TOWER NOTIFIED US AGAIN THAT WE NEEDED TO EVACUATE .R & R #2 ENG OIL PRESSURE TRANSMITTER PER AMM 79-33-01 OPS CHECK NORMAL.

Part: FUEL SYS — FLUCTUATES (NR 2 ENGINE) · airframe 60,109 hrs · 15,782 cycles

FUEL FLOW FLUCTUATED AFTER ENG START. FROM 2300 TO 800, THEN BACK TO 2300. THE#2 ENG N1 DISAPPEARED. A PRECAUTIONARY ENG SHUTDOWN WAS ACCOMP WITH THE LOSS OF OIL PRESSURE.FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS.

Part: BEAM — CRACKED (TE FLAP) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C LT WING O/B FLAP I/B FIXED FAIRING LOWER T BEAM IS CRACKED. REMOVED AND REPLACED LT WING O/B FLAP I/B FIXED FAIRING LOWER BEAM IAW SRM 51-35-01. (MINOR)

Part: FAIRING — CRACKED (NR 3 PYLON) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 3 PYLON AFT LOWER FAIRING AFT LOWER SKIN RT SIDE IS CRACKED PAST THE STOP DRILL. REPAIRED CRACKED NR 3 PYLON AFT LOWER SKIN RT SIDE IAW SRM 54-55-01 REPAIR 2. (MINOR)

Part: STRUT — CRACKED (CARGO BAY) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C CENTER CARGO COMP AT STA. 5-53 AND X=16 SUPPORT STRUT IS CRACKED. REMOVED, FABRICATED AND REPLACED STRUT AT STA. 5-53 AND X=16 IAW DWG ADA0033 AND SRM 51-35-01. (MINOR)

Part: WEB — CRACKED (LT WING) · airframe 39,018 hrs · 10,179 cycles

INSPECTION TYPE:4C LT OVER WING FUEL TANK UPPER AFT WEB IS CRACKED AT STA. 1372, X=80 AND Z=-54. REPAIRED CRACKED OVER WING FUEL TANK UPPER AFT WEB AT STA. 1372, X=80 AND Z=-54 IAW EO MD11-5710-71265-A. (MAJOR)

Part: STRUT — CRACKED (CARGO BAY) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C CENTER CARGO FLOORBEAM SUPPORT STRUT IS CRACKED AT STA. 5-53 LTH. REMOVED, FABRICATED AND REPLACED SUPPORT STRUT AT STA. 5-53 LT IAW DWG. ADA0033 AND SRM 51-35-01. (MINOR)

Part: SUPPORT — CRACKED (TE FLAP) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C LT WING O/B FLAP FIXED HINGE FAIRING SUPPORT IS CKACKED. REMOVED, FABRICATED AND REPLACED SUPPPORT TEE IAW DWG. ACA0547 AND SRM 51-31-01 & 51-35-01. (MINOR)

Part: SKIN — CRACKED (RT WING) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C RT WING L/E LOWER SKIN AT STA. XOS. 775 IS CRACKED AT SLAT TRACK NR 12. REPAIRED CRACKED RT WING L/E LOWER SKIN AT STA. XOS. 775 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA. XOS. 542-547. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER AT STA. XOS. 542-547 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CHAFED (TAILCONE) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C TAIL CONE RT UPPER PRODUCTION DOUBLER HAS DEEP WEAR IN NUMEROUS PLACES. REPAIRED TAIL CONE RT UPPER PRODUCTION DOUBLER CHAFE WEAR IAW EA 011-5320-01-7576 REV. IR AND EO MD11-5350-71259-A. (MINOR)

Part: WEB — CRACKED (THUST REVERSER) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 1 O/B T/R COWL AFT UPPER WEB IS CRACKED AT 12 O'CLOCK POS. REMOVED AND REPLACED NR 1 O/B T/R COWL AFT UPPER WEB IAW SRM 54-05-41. (MINOR)

Part: TRUNNION — CRACKED (NLG) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C RT NOSE TRUNNION FITTING IS CRACKED AT STA. 582.5, Z=-114 AND X=-24.0. REPAIRED CRACKED RT NOSE TRUNNION FITTING AT STA. 582.5, Z=-114 AND X=-24.0 IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 3 ENG. LT T/R AFT FIXED INNER BARREL UPPER SKIN IS CRACKED. REPAIRED CRACKED NR 3 ENG. LT T/R AFT FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7575 REV. I/R AND EO MD11-7830-71282-A. (MINOR)

Part: COWLING — CHAFED (NR 3 ENGINE) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 3 ENG. I/B FAN COWL FWD. DOOR HINGE FITTING HAS CHAFE DAMAGE. REPAIRED NR 3 ENG I/B FAN COWL FWD. DOOR HINGE FITTING IAW EA 011-7110-01-A7577 REV. I/R AND EO MD11-7110-71327-A. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 1 ENG. LT T/R AFT FIXED INNER BARREL UPPER SKIN HAS A CRACK. REPAIRED CRACKED NR 1 ENG. LT T/R AFT FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7574 REV. I/R AND EO MD11-7830-71281-A. (MINOR)

Part: BULKHEAD WEB — CRACKED (NR 1 COWLING) · airframe 60,085 hrs · 15,764 cycles

INSPECTION TYPE:4C NR 1 ENGINE NOSE COWL AFT BULKHEAD WEB IS CRACKED AT 3 O'CLOCK POS. REMOVED AND REPLACED CRACKED NR 1 ENG. NOSE COWL AFT BULKHEAD WEB AT 3 O'CLOCK POS. IAW CMM 71-11-05 REPAIR 7. (MINOR)

Part: FAIRING — DAMAGED (NR 3 PYLON) · airframe 60,081 hrs · 15,762 cycles

INSPECTION TYPE:4C NR 3 PYLON AFT LOWER WING FAIRING HAS 3 OVERSIZE HOLES. REPAIRED NR 3 PYLON AFT LOWER WING FAIRING IAW EO MD11-5450-71321-A. (MINOR)

Part: COVER — DAMAGED (R1 DOOR SLIDE) · airframe 59,792 hrs · 15,662 cycles

DURING AN OPS CHECK OF THE EMERGENCY PNEUMATIC SYSTEM, FUNCTION OF R1 DOOR SLIDE LOWER HINGE FLAP PANEL CONTACTED THE FLOOR AND BROKE OFF THE DOOR. THE SLIDE STILL FUNCTIONS NORMALLY. R & R R1 SLIDE COVER ASSY IAW AMM 25-61-15-400-801.

Part: FLAP — BROKEN (R1 DOOR) · airframe 59,792 hrs · 15,662 cycles

R1 DOOR LOWER HINGE SPRING PANEL REMOVED DUE TO DAMAGE. DURING OPS CHECK OF THE EMERGENCY PNEUMATIC FUNCTION OF THE R1 DOOR SLIDE, LOWER FLAP CONTACTED FLOOR AND BROKE OFF THE DOOR AND SLIDE FUNCTIONED NORMALLY.

Part: CYLINDER — EMPTY (R1 DOOR) · airframe 59,785 hrs · 15,655 cycles

R1 DOOR PNEUMATIC CYLINDER PRESSURE WAS AT ZERO PSI. COMPLIED WITH A LEAK CHECK IAW AMM 52-11-04-700-801 AND 12-25-04-600-801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,610 hrs · 15,598 cycles

DURING PREFLIGHT TEST, THE EMERGENCY LIGHT, AN ALERT EMERGENCY LIGHT BATTERY 1 LOW. REPLACED BATTERY PACK IAW AMM 33-51-01, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,935 hrs · 15,403 cycles

FOUND THE EMERGENCY LIGHT TEST FAILED. R & R THE BATTERY PACK IAW AMM 33-51-01/401. PERFORMED AN EMERGENCY LIGHT TEST, FOUND TO BE SATISFACTORY.

Part: CASE — DAMAGED (NR 2 ENG FAN) · airframe 58,646 hrs · 15,316 cycles

NR 2 RT FAN COWL DENTED OUT OF LIMITS. R & R THE FAN COWL IAW MM 71-12-01-000 & 400.

Part: CONTROL VALVE — MALFUNCTIONED (A/C PACK) · airframe 58,637 hrs · 15,310 cycles

AIR TURN BACK. DURING CLIMBOUT, A LEVEL ONE PACK 3 DISAGREE ALERT, THIS ALERT BECAME INTERMITENT. R & R THE A/C PACK FLOW CONTROL VALVE IAW MM 21-51-01-201, AND PACK OUTLET FLOW SENSOR IAW MM 21-53-03-401, OPS CHECKED GOOD.

Part: SMOKE GOGGLES — DAMAGED (RH COURIER SEAT) · airframe 58,504 hrs · 15,285 cycles

RIGHT COURIER SEAT SMOKE GOGGLES ARE DAMAGED. R & R THE SMOKE GOGGLES IAW MM 35-13-00.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 57,829 hrs · 15,087 cycles

SLIDE PRESSURE PRESS TO TEST LIGHT INOP ON LEFT CABIN DOOR. R&R INDICATOR LIGHT ASSY, OPS CK NORMAL PER MM 25-61-05.

Part: LAMP — INOPERATIVE (SLIDE PRESSURE) · airframe 57,285 hrs · 14,957 cycles

L1 SLIDE PRESSURE LIGHT IS INTERMITTENT. REPLACED THE LAMP IN THE REMOTE PRESSURE INDICATOR IAW AMM 25 61 04 401, OPS NORMAL.

Part: WARNING LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 57,112 hrs · 14,919 cycles

MLG DOOR SLIDE PRESSURE LIGHT INOPERATIVE. DOOR SLIDE PRESSURE GOOD.

Part: BUTTON — INOPERATIVE (L1 DOOR SLIDE) · airframe 56,814 hrs · 14,854 cycles

INSPECTION TYPE: L1, PUSH TO TEST SLIDE INOPERATIVE. REPLACED L1 DOOR SLIDE INDICATION LIGHT ASSY. OPS CHECKED OK IAW MM 25-61-04.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 56,795 hrs · 14,850 cycles

DURING POST FLIGHT WALK AROUND, A CRACK WAS FOUN IN THE LEFT INBOARD NR 1 SLAT. PERFORMED A REPAIR IAW EO MD11-5750-64740-A, AND SRM 57-40-01.

Part: INDICATOR — INOPERATIVE (ESCAPE SLIDE) · airframe 56,460 hrs · 14,775 cycles

R1 DOOR SLIDE TEST LIGHT WILL NOT TEST. R & R LOAD INDICATOR ASSY. OPS CHECKED GOOD IAW AMM 25-61-04.

Part: WARNING MESSAGE — ACTIVATED (AILERONS) · airframe 56,384 hrs · 14,751 cycles

LEVEL 2 ALERT. AILERON DEFLECT DISAGREE. DIVERTED.

Part: ACTUATOR — FAILED (R1 DOOR) · airframe 56,233 hrs · 14,718 cycles

THE R1 DOOR WILL NOT CLOSE. REPLACED THE R1 DOOR ACTUATOR ASSY IAW MM 52-11-01-401.

Part: WIRE — LOOSE (DOOR SWITCH) · airframe 56,233 hrs · 14,718 cycles

L1 DOOR ELECTRICAL FUNCTION INTERMITTENT. IAW AMM 52-11-02 FOUND WIRE LOOSE ON BACKUP TOGGLE SWITCH. TIGHTENED THE SWITCH, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (DOOR SLIDE) · airframe 56,233 hrs · 14,718 cycles

SLIDE RAFT PUSH TO TEST LOW PRESSURE INDICATOR INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD.

Part: CONTROL UNIT — MULTIPLE FAIL (ELECTRICAL SYS) · airframe 56,040 hrs · 14,671 cycles

NUMEROUS ELECTRICAL FAULTS (FCC 2 FAIL, AVIONICS OVERRIDE, DU DISPLAYS, A/C AND D/C TIE BUSSES) WHICH RESULTED IN DEGRADED NAVIGATION CAPABILITY. EMERGENCY DECLARED. REPLACED EPCU IAW AMM 24-08-01-400. CHECKED NORMAL. REPLACED OVERHEAD ELECTRICAL CONTROL PANEL AND DC BUSS TIE NR 2 RCCB

Part: SKIN — CORRODED (BS 2113-2163) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C,CORROSION FOUND ON THE FUSELAGE SKIN AT BS 2113 - 2163 BETWEEN LONGERONS 33 & 35R. REPAIRED THE SKIN IAW EO MD11-5330-63208A AND EA.011-5330-01-A6611, REV I/R.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, AFT CARGO BAY FLOORBEAM ANGLE HAS CORROSION BS 1841, LBL 13. REPAIRED THE FLOORBEAM ANGLE IAW EA 011-5310-01-A6604, REV. I/R AND EO MD11-5310-63206-A.

Part: SKIN — DENTED (R1 DOOR) · airframe 56,022 hrs · 14,668 cycles

TWO DENTS ON R1 DOOR BETWEEN BEAMS 4-5. REPAIRED IAW EA 011-5210-01-A6586 AND EO MD11-5210-63026-A.

Part: SKIN — WORN (BS 1139-1168) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, FUSELAGE SKIN HAS DEEP FRETTING WEAR BETWEEN BS 1139 - 1168 AND LONGERONS 43 - 45L. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG. 201. (MAJOR)

Part: SKIN — PUNCTURED (TAIL CONE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, TAIL CONE LOWER SKIN HAS A PUNCTURE AT BS 2224 - 2229. REPAIRED THE SKIN IAW EA 011-5350-01-A6597 AND EO MD11-5350-63071-A.

Part: SKIN — GOUGED (BS 1139-1168) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, FUSELAGE SKIN HAS DEEP FRETTING WEAR BETWEEN BS 1139 - 1168 & LONGERONS 43 - 45R. REPAIRED IAW SRM 53-40-01 REPAIR 3 FIG. 201. (MAJOR)

Part: LUG — WORN (THRUST REVERSER) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, THE UPPER SURFACE OF THE LOWER TRACK LUG OF THE NR 1 ENGINE LT THRUST REVERSER HAS WEAR DAMAGE. REPAIRED THE THRUST REVERSER IAW EA 011-7830-01-A6598 REV. I/R, AND EO MD11-7830-63117-A.

Part: FITTING — WORN (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER SIDE FITTING NR 6 HAS DEEP WEAR. REPAIRED FITTING IAW EA 011-5310-01-A6603 REV. I/R AND EO MD11-5340-63110-A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, LEFT INBD FLAP L/E UPPER SKIN HAS GOUGES AT XIFH215.3 & XIFH 217.3. REPAIRED IAW EA 011-5753-01-A6608 REV. I/R AND EO MD11-5750-63129-A.

Part: STANCHION — CORRODED · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, VERTICAL STANCHION AT BS 6-79 ABOVE LONGERON 48L HAS HEAVY CORROSION. REPAIRED THE STANCHION IAW EA 011-5310-01-A6583 REV. I/R AND EO MD11-5310-63122-A.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 2 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6593 REV. I/R AND EO MD11-5310-63070-A.

Part: BEAM — CRACKED (FWD CARGO) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, FWD CARGO BAY HORIZONTAL BEAM IS CRACKED AT BS 6-79 ABOVE LONGERON 43R. REMOVED, FABRICATED AND REPLACED THE BEAM IAW DWG ADA7667 AND SRM 51-33-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 1 HAS CORROSION. REMOVED AND REPLACED RCB FLOOR FITTING NR 1 IAW EO MD11-2520-58701-D. (MINOR)

Part: FITTING — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 4 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6593 REV. I/R AND EO MD11-5310-63070-A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 5 HAS HEAVY CORROSION. REMOVED AND REPLACED RCB FLOOR FITTING NR 5 IAW MD11-2520-58701-D. (MINOR)

Part: FITTING — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 3 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6594 REV. I/R AND EO MD11-5310-63078-A.

Part: BEAM — CRACKED (FWD CARGO BAY) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, BS 6-79 ABOVE LONGERON 43L, HORIZONAL BEAM HAS A TWO INCH CRACK. REMOVED, FABRICATED, AND REPLACED THE BEAM IAW DWG. ADA7667 AND SRM 51-33-01.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 HAS CORROSION. REPAIRED IAW EA 011-5340-01-A6599 REV. I/R AND EO MD11-5340-63091-A. (MINOR)

Part: SUPPORT ANGLE — CRACKED (BS 430) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, AVIONICS BAY BILGE FRAME SUPPORT ANGLE AT BS 430 LBL 2 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ABA8678, AND SRM 51-35-01.

Part: FRAME — CORRODED (BS 430) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, BAY FRAME ANGLE HAS CORROSION AT BS 430 RBL 2 - 9. REMOVED, FABRICATED AND REPLACED THE FRAME ANGLE IAW DWG ABA8678 AND SRM 51-35-01

Part: SKIN — CORRODED (BS 2104-2163) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C,AFT UPPER EXTERIOR SKIN HAS CORROSION BETWEEN BS 2104 & 2163.685, LONGERONS 11 - 13L. REPAIRED THE SKIN IAW EA 011-5330-01-A6600 REV. I/R AND EO MD11-5330-63118-A.

Part: PAN — GOUGED (CARGO DOOR) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, MAIN CARGO DOOR FWD. PAN IS GOUGED 23 INCHES FROM BOTTOM. REMOVED, FABRICATED AND REPLACED MAIN CARGO DOOR FWD LOWER PAN IAW DWG ACA7301 AND SRM 51-35-01 & N51-33-01. (MINOR)

Part: FRAME — CRACKED (BS 469) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, FUSELAGE FRAME AT BS 469.173, LBL 60 IS CRACKED. REPAIRED THE FRAME IAW SRM 53-10-07, REPAIR 1, FIG. 201.

Part: ANGLE — CORRODED (BS 475) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3CT, ANGLE CORRODED IN FWD E/E BAY BS 475 RBL 4.5. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG NCA6042, AND SRM 51-33-01.

Part: SKIN — CRACKED (TAILCONE DOOR) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, UPPER RT AFT TAILCONE PATIO DOOR SKIN CRACKED. REPAIRED SKIN IAW SRM 52-00-00, FIG 204.

Part: INTERCOSTAL — CORRODED (BS 475) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, E/E BAY BS 475, RBL 9-12 INTERCOSTAL HAS CORROSION. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL IAW DWG ABA7655 AND SRM 51-33-01.

Part: FUEL TANK — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, CENTER WING TANK UPPER SKIN HAS CORROSION AT RBL 89 TO 101.5 AT STRINGER 15. REPAIRED IAW EA 011 5730-01-A6596 AND EO MD11-5730-63200-A. (MAJOR)

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL 262GF HAS A PUNCTURE. REMOVED, FABRICATED AND REPLACED THE FLOOR PANEL IAW EO MD11-5320-27286-C.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, AFT CARGO COMP FLOOR SUPPORT ANGLE/FLOOR BEAM CAP STA 1841 LONG 42R IS CORRODED. REPAIRED CORRODED SUPPORT ANGLE AT STA 1841, LONG 42R IAW DWG AGA3857 AND SRM 51-35-01. (MINOR)

Part: SKIN — CORRODED (MAIN CABIN) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, SKIN HAS CORROSION ABOVE STRINGER 15. REPAIRED THE SKIN IAW EA 011-5730-01-A6609 REV. I/R AND EO MD11-5730-63128-A.

Part: SKIN — CORRODED · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, SKIN CORRODED ABOVE STRINGER 15. REPAIRED IAW EA 011-5730-01-A6591 REV. I/R AND EO MD11-5730-63084-A.

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 38L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, UPPER SKIN HAS CORROSION ABOVE STRINGERS 2, 3, & 4 AT RBL 105. REPAIRED CORRODED THE SKIN IAW EA 011-5730-01-A6595 REV. I/R AND EO MD11-5730-63085-A.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, NR 2 ENGINE LT THRUST REVERSER CORE COWL UPPER CLOSE-OUT WEB IS CRACKED. REMOVED AND REPLACED THE CLOSE-OUT WEB IAW SRM 54-05-41.

Part: STRUCTURE — CORRODED · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, STRUCTURE IS CORRODED ABOVE STRINGER 15. REPAIRED IAW EA 011-5730-01-A6590 REV. I/R AND EO MD11-5730-63082-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, SKIN HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5730-01-A6601 REV. I/R AND EO MD11-5730-63090-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, SKIN HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5730-01-A6602 REV. I/R AND EO MD11-5730-63089-A.

Part: INLET — GOUGED (NR 2 ENGINE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, NR 2 ENGINE INLET INNER SKIN HAS GOUGES AT THE 10:30 POSITION. REPAIRED IAW EA 011-5430-01-A6610 REV. I/R AND EO MD11-7110-63154-A.

Part: SKIN — CORRODED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RT WING UPPER SKIN HAS CORROSION AT XORS. 399 AND STRINGERS 11-12 AND XORS. 407 AND STRINGER 9. REPAIRED IAW EA 011-5730-01-A6607 REV. I/R AND EO MD11-5730-63181-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE :3C, RT WING REAR SPAR UPPER CAP HAS CORROSION AT XORS. 480 - 488. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6589 REV I/R, AND EO MD11-5710-63058-A.

Part: LONGERON — CRACKED (BS 1199-1219) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, MAIN CABIN BS 1199 - 1219, LONGERON 17R IS CRACKED. REMOVED AND REPLACED THE LONGERON IAW DWG AEA7530 AND SRM 51-33-01.

Part: SKIN — CORRODED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGHT UPPER WING SKIN HAS MULTIPLE AREAS OF CORROSION BETWEEN XORS 128.3 - 219.3 AND BETWEEN STRINGERS 13 - 17. REPAIRED THE RT WING UPPER SKIN IAW EA 011-5730-01-A6606 REV. I/R AND EO MD11-5730-63115-A.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON SPLICE FITTING 11R IS CRACKED AT STA 1321. REMOVED, FABRICATED AND REPLACED LONGERON SPLICE FITTING 11R AT STA 1321 IAW DWG AEA7600 AND SRM 51-33-01. (MINOR)

Part: TEE FITTING — CRACKED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RT WING T/E REAR FALSE SPAR VERTICAL TEE ANGLE IS CRACKED FWD OF INBD AILERON. REMOVED AND REPLACED THE VERTICAL TEE ANGLE IAW SRM 51-33-01. )

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, NR 1 PYLON ACCESS FAIRING SUPPORT ANGLE IS CRACKED AT BOTH ENDS. REMOVED, FABRICATED AND REPLACED THE SUPPORT ANGLE IAW DWG AUB7564 AND SRM 54-05-41.

Part: FORMER — CRACKED (TAIL CONE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, TAIL CONE RT SIDE FORMER HAS SEVERAL LARGE CRACKS. REPAIRED IAW SRM 53-80-07 REPAIR 1 FIG. 201.

Part: SPAR — CRACKED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C RT WING T/E REAR SPAR LOWER SILL IS CRACKED AT XORS. 472. REPAIRED IAW EA 011-5710-01-A6587 REV. I/R AND EO MD11-5720-63077-A.

Part: TEE FITTING — CRACKED (TE FLAP) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT WING O/B FLAP I/B HINGE FWD FAIRING SUPPORT TEE IS CRACKED. REMOVED, FABRICATED AND REPLACED RT O/B FLAP I/B HINGE FAIRING SUPPORT TEE IAW DWG ARC0745 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: SKIN — CHAFED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E SKIN IS CHAFED BETWEEN XIS 171.8 - 178.8. REPAIRED IAW EA 011-5730-01-A6580 REV. I/R AND EO MD11-5730-62990-A.

Part: SKIN — CORRODED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, THE LT WING UPPER SKIN HAS CORROSION AT STRINGER 1 BETWEEN XORS. 980 - 983. REPAIRED THE SKIN IAW EA 011-5730-01-A6584 REV. I/R, AND EO MD11-5730-63059-A.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, LT MLG WW O/B BULKHEAD VERT STIFFNER ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED LT MLG WW STIFFNER ANGLE IAW DWG ANB7203 AND SRM 51-31-01. (MINOR)

Part: DOOR FRAME — CRACKED (L3 DOORWAY) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, THE L3 DOOR FRAME INNER SKIN IS CRACKED AT BS 1254, RBL 18. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG. 201.

Part: SKIN — WORN (TAIL CONE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, TAIL CONE EXTERNAL SKIN HAS DEEP GOUGED AT BS 2165.6, RBL 36.5. REPAIRED TAIL CONE AT SAID LOCATION IAW EA 011-5320-01-A6581 REV. I/R AND EO MD11-5350-62966-A.

Part: BARRIER — CRACKED (BS 488) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL HAS A CRACK AT BS 488.812, RBL 42. REPAIRED BARRIER WALL IAW SRM 53-20-53 REPAIR 1 FIG. 201.(MAJOR)

Part: SKIN — CORRODED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, LT WING UPPER SKIN HAS CORROSION AT STR 6 BETWEEN STA XORS 956.8 AND XORS 960. REPAIRED CORRODED LT WING UPPER SKIN AT STR 6 BETWEEN STA XORS 956.8 TO 960 IAW EA 011-5730-01-A6585 REV I/R AND EO MD11-5730-63020-A. (MINOR)

Part: SKIN — WORN (DOOR) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, LEFT PATIO DOOR INTERNAL SKIN AFT END HAS DEEP WEAR. REMOVED, FABRICATED, AND REPLACED THE SKIN IAW DWG AKC7820 AND SRM 51-35-01.

Part: THRUST REVERSER — CRACKED (NR 1 ENGINE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, NR 1 ENGINE INBD THRUST REVERSER CORE COWL EXTERIOR SKIN IS CRACKED ABOVE AFT UPPER LATCH. REPAIRED THRUST REVERSER COWL IAW SRM 54-00-00 REPAIR GENERAL FIG. 204.

Part: FRAME — WORN (FUSELAGE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT PATIO DOOR FRAME HAS DEEP WEAR. REMOVED, FABRICATED AND REPLACED RT PATIO DOOR FRAME (AFT) IAW DWG AKC7820 AND SRM 51031-01. (MINOR)

Part: STRINGER — CRACKED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E UPPER STRINGER AT STA XOS.666 IS CRACKED. REPAIRED CRACKED RT WING FIXED L/E UPPER STRINGER AT STA XOS 666 IAW SRM 57-40-03 REPAIR 2 FIG 202. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT WING INNER BEADED DOUBLER IS CRACKED AT STA XOS 695. REPAIRED CRACKED RT WING INNER BEADED DOUBLER AT STA XOS 692-698 IAW SRM 57-40-05 REPAIR 15 FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT WING INNER BEADED DOUBLER IS CRACKED AT STA XOS 661-667. REPAIRED CRACKED RT WING INNER BEADED DOUBLER AT STA XOS 661-667 IAW SRM 57-40-02 REPAIR 15 FIG 203. (MAJOR)

Part: FORMER — CRACKED (NR 1 ENGINE) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, NR 1 ENG LT T/R CORE COWL AFT UPPER FORMER IS CRACKED. REMOVED AND REPLACE LT T/R CORE COWL AFT UPPER FORMER IAW SRM 54-05-41. (MINOR)

Part: SUPPORT ANGLE — CRACKED (NR 3 PYLON) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, NR 3 PYLON FAIRING SUPPORT ANGLE IS CRACKED AT THE AFT OF PRE COOLER. REMOVED, FABRICATED, AND REPLACED THE FAIRING SUPPORT ANGLE IAW DWG AUB7564 AND SRM 54-05-41.

Part: FORMER — CRACKED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E RIB/FORMER IS CRACKED AT STA XOS 559. REMOVED, FABRICATED AND REPLACED RIB/FORMER IAW DWG ARB1162 AND SRM 51-33-01. (MINOR)

Part: STRAP — CRACKED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E SKIN INNER SPLICE STRAP CRACKED AT XOS 789. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT STRAP IAW DWG ARB3954, SRM 51-33-01, AND 51-35-01.

Part: SKIN — DENTED (R1 DOOR) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, EXTERIOR SKIN OF R1 DOOR DENTED BETWEEN BEAM 4-5 FWD. AND AFT EDGES. REPAIRED THE SKIN IAW EA 011-5210-01-A6586 REV. I/R AND EO MD11-5210-63026-A.

Part: SKIN — CRACKED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E LOWER SKIN IS CRACKED AT XOS 775. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, LT WING L/E SKIN FOR SLAT TRACK CUTOUT AT STA XOS 720 IS CRACKED. REPAIRED CRACKED LT WING L/E SKIN FOR SLAT TRACK CUTOUT AT STA XOS 720 IAW SRM 57-40-02 REPAIR 7 FIG 201. (MAJOR)

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE: 3C, NR 2 PYLON LT LOWER SKIN HAS DAMAGED FASTENERS. REPAIRED THE SKIN IAW EA 011-5450-01-A6588 REV. I/R AND EO MD11-5430-63001-A.

Part: FAIRING — DELAMINATED (LE SLAT) · airframe 56,022 hrs · 14,668 cycles

INSPECTION TYPE:3C, RT WING NR 1 SLAT FILLET FAIRING/PERFORMANCE FAIRING IS DELAMINATED. REPAIRED RT WING NR 1 SLAT FILLET/PERFORMANCE FAIRING IAW SRM 57-40-70 REPAIR 2. (MINOR)

Part: ACTUATOR — MALFUNCTIONED (L1 DOOR) · airframe 55,389 hrs · 14,508 cycles

ENTRY DOOR WILL NOT CLOSE OR OPEN FULLY. R & R THE ACTUATOR IAW AMM 52-11-01-401. OPS CHECKED GOOD. OK FOR SERVICE 52-11-025-05-525

Part: COAX — FAILED (TCAS) · airframe 55,207 hrs · 14,469 cycles

SHORTLY AFTER TAKEOFF, TCAS FAILED. RETURNED TO DEPARTURE. REPLACED BOTH J2 AND J4 COAX CABLES. TCAS OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 54,821 hrs · 14,357 cycles

EMERGENCY POWER SUPPLY BATTERY FAILED TEST. R & R THE BATTERY PACK IAW AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,289 hrs · 13,920 cycles

LEVEL 1 EMERGENCY LIGHT BATTERY NR 1 LOW, LIGHT ILLUMINATED. R & R THE BATTERY PACK IAW MM 33-51-01. OPS NORMAL IAW MM 33-51-01-700-802.

Part: LOUVER — DETACHED (THRUST REVERSER) · airframe 53,289 hrs · 13,920 cycles

FOUND NR 2 ENGINE LEFT T/R LOUVER HAS DEPARTED ACFT AND CAUSED COMPOSITE AND S/M DAMAGE TO LT T/R. REPAIRED NR 2 ENGINE LT T/R INNER BARREL IAW EO 7830-59016A, PARA 6A. STEPS 1-3. C/W STEPS 4 AND 5 REF EO 7830-59016B. PERMANENT REPAIR COMPLETED IAW EO 7830-59016C.

Part: INDICATOR — NO TEST (R1 DOOR SLIDE) · airframe 52,630 hrs · 13,726 cycles

R-1 DOOR SLIDE PRESS INDICATOR WILL NOT TEST. R & R ESCAPE SLIDE BATTERIES AND LAMPS. OPS CHECKED GOOD.

Part: BUTTON — INOPERATIVE (L1 DOOR) · airframe 51,836 hrs · 13,532 cycles

L1 DOOR PRESS TO TEST SLIDE, PRESS INDICATION INOPERATIVE. DEFERRED IAW MEL 25-61-2. DMP 25-61-2 ACCOMPLISHED. R & R REMOTE PRESSURE INDICATOR ASSY IAW MM 25-61-04. THIS CLEARS M547344, EFF SOURCE REF 25-61-05-01-165.

Part: STRINGER — CRACKED (LT WING) · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE:3C, LT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIR LT WING STRINGER 15 BETWEEN XORS433- 455 IAW EA 011-5710-01-A5721, REV IR AND EO MD11-5710-56725-A.

Part: STRUCTURE — CRACKED (LT WING) · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE: 3C, LT WING LOWER T/E FILLER STRIP, SILL, CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SILL STRIP IAW DWG ARC7008, SRM 51-31-01, 53-33-01.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL 261KF PUNCTURED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO 5320-27386C, 5320-38342B AND DWG AEA0181.

Part: STRINGER — CRACKED · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE:3C, CENTER WING TANK, STRINGER 48 CRACKED AT XCW17. REPAIRED STRINGER 48 BETWEEN XCW17 AND -47 IAW EA 011-5710-01-A5717, REV IR AND EO 5710-56724-A.

Part: STRINGER — CRACKED · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE:3C, CENTER WING TANK STRINGER 47 CRACKED AT XCW 46.5, 17, -17. REPAIRED CTR WING STRINGER 47 IAW EA 011-5710-01-A5716, REV IR AND EO MD11-5710-56723-A.

Part: STRINGER — CRACKED · airframe 51,836 hrs · 13,532 cycles

INSPECTION TYPE:3C, CENTER WING TANK STRINGER 48 CRACKED, XCW-46, REPAIRED CTR WING TANK STRINGER 48 BETWEEN XCW17 AND -46 IAW EA 011-5710-01-A5717, REV IR AND EO 5710-56724-A.

Part: CONTACT — OUT OF ADJUST (BATTERY RETAINER)

RT ENTRY DOOR SLIDE WILL NOT TEST. ADJUSTED CONTACTS ON BATTERY RETAINER. OPS CHECKED GOOD IAW AMM 25-61-04-000.

Part: CONTROL LEVER — LACK OF LUBE (MLG)

LANDING GEAR HANDLE LOWERED FOR LANDING. HANDLE STUCK IN DETENT POSITION. CLEANED AND LUBRICATED LANDING GEAR CONTROL LEVER SHAFT IAW 32-31-00-00. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

OVERHEAD EMERGENCY LIGHT AFT OF R1 DOOR INOPERATIVE. REPLACED THE LAMP AND TESTED IAW MM 33-52-04-400 AND MM 33-52-04-700-801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING EMERGENCY LIGHT TEST, FOUND EMERGENCY LIGHT BATTERY 1 LOW ALERT MESSAGE. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY AND OPS TEST PASSED IAW AMM 33-51-01-400-802. EFF SOURCE REF IPC 33-51-01-05, ITEM 15.

Part: FITTING — CRACKED (LT WINGLET) · airframe 49,219 hrs · 12,784 cycles

INSPECTION TYPE:1C, LT LOWER WINGLET AFT ATTACH FITTING CRACKED. ACCOMPLISHED PERMANENT REPAIR BY REMOVING AND REPLACING LT WING LOWER WINGLET FWD AND AFT ATTACH FITTINGS IAW EA 011-5740-01-A4971, REV I/R AND EO'S MD11-5740-52499-A AND MD11-5720-27680-C, APPX D.

Part: FLOORBOARD — DAMAGED (MAIN CARGO DECK) · airframe 49,219 hrs · 12,784 cycles

INSPECTION 1C, INSERT MISSING FLOORBOARD 261CF. FABRICATED NEW FLOORBOARD IAW EO MD11-5320-27386-C, APPENDIX A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW ILLUMINATED DURING EMERGENCY LIGHT TEST. R & R BATTERY IAW MM 33-51-01-000-802 AND 33-51-01-400-802. OPS CHECKED GOOD IAW MM 33-51-01-700-802.

Part: BATTERY — WARNING LIGHT (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY ONE LOW MESSAGE. TROUBLESHOT IAW FIM 33-51-00. EMERGENCY LIGHT TEST PASSED IAW AMM 33-51-00. SYS OK.

Part: LINE — CRACKED (HYDRAULIC SYS)

FL360, OBSERVED LEVEL 1 HYD 3 1 ELEV OFF 3-2 NRMP INOP. NR 3 HYD QTY LOW, EMERGENCY DECLARED. R & R LINE ASSY IAW MM 20 50 01 & 32 43 20 . NO LEAKS NOTED AT THIS TIME. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (R1 DOOR SLIDE)

R1 DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN PUSHED. LAMPED R1 DOOR EVAC SLIDE REMOTE PUSH TO TEST PRESS IND SWITCH. OPS CHECKS NORMAL IAW MM 25-6-104. THIS CLEARS M490654.

Part: LONGERON SPLICE — CRACKED (BS 1129 L2L) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE:4C, LONGERON 2L SPLICE FITTING CRACKED AT BS 1129. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING AT BS 1129 L2L IAW DWG ADA8413 & SRM 51-33-01.

Part: FAIRING — CRACKED (NR 3 NACELLE) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, NR 3 PYLON LOWER AFT FAIRING FOUND WITH A CRACK PROPAGATING FROM PREVIOUS STOP-DRILL REPAIR NEAR YPN297. REPAIRED NR 3 PYLON LOWER AFT FAIRING IAW EA 011-5450-01-A4215 REV IR AND UPS EO MD11-5450-48454-A.

Part: INTERCOSTAL — CRACKED (NR 2 NACELLE) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE:4C, NR 2 ENGINE INTAKE DUCT STRUCTURAL INTERCOSTAL CRACKED, RT SIDE, YTN 121.865. REPAIRED INTERCOSTAL IAW EA 011-5530-01-A4197 REV IR AND EO MD11-5530-48451-A. MAJOR REPAIR.

Part: SKIN — CORRODED (CENTER WING) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, CENTER WING UPPER EXTERIOR SKIN CORRODED IN MAIN CABIN SUBFLOOR ABOVE STRINGER 15 AT LBL 114 F/STA 1227 (XCW103-109). REPAIRED CORROSION ON CENTER WING UPPER SKIN ABOVE S15 BETWEEN XCW103-109 IAW STA SA EA 011-5730-01-A4214, REV IR & EO MD11-5730-48406-A.

Part: SKIN — CORRODED (WING CENTER SECT) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, CENTER WING UPPER EXTERIOR SKIN CORRODED IN MAIN CABIN SUBFLOOR ABOVE STRINGER 15 RBL102, NEAR F/STA 1227 (XCW 97-101). REPAIRED CORROSION ON CENTER WING UPPER SKIN ABOVE S15 BETWEEN XCW 91-101 IAW EA 011-5730-01-A4212 REV IR & EO MD11-5730-48413-A.

Part: INTERCOSTAL — CRACKED (NR 2 NACELLE) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, NR 2 ENGINE INTAKE DUCT STRUCTURAL INTERCOSTAL CRACKED, LT SIDE, YTN 121.865. REPAIRED INTERCOSTAL IAW EA 011-5530-01-A4197 REV IR AND EO MD11-5530-48451-A (MAJOR).

Part: SEAT TRACK — CRACKED (BS 1421 LBL 9) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, SEAT TRACK LOWER FLANGE CRACKED AT BS 1421, LBL 9. REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 1, FIG 201.

Part: SKIN — CORRODED (CENTER WING) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, CENTER WING UPPER SKIN IN MAIN CABIN SUBFLOOR CORRODED NEAR BS 1234 RBL 83 (STA XCW -81 BETWEEN S14 & S15). REPAIRED CORRODED CENTER WING UPPER SKIN AT XCW -81 BETWEEN S14 AND S15 IAW EA 011-5730-01-A4213 REV IR AND EO MD11-5730-48439-A.

Part: LONGERON — CORRODED (BS 1049 L52) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, LONGERON 52 CORRODED AT BS 1049. REPAIRED LONGERON 52 BETWEEN BS 1029-1069 IAW STASA EA 011-5310-01-A4218 REV IR, EO MD11-5310-48469-A, AND SRM 53-00-05, REPAIR 1, FIG 1 FAA 8100-9.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, CRACKED RIB IN NR 2 PYLON PANEL 437BL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FORMER IN PANEL 437BL IAW DWG AUB7583 AND SRM 51-35-01.

Part: LONGERON — CORRODED (BS 1049 L52) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, LONGERON 52 CORRODED AT BS 1049. FABRICATED AND INSTALLED REPLACEMENT SECTION OF L52 BETWEEN BS 1029 & 1129/6-0 IAW EA 011-5310-01-A4218, REV IR, EO MD11-5310-48469-A, AND SRM 53-00-05, REPAIR 1, FIG 201.

Part: ATTACH FITTING — GOUGED (CARGO BARRIER) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, RIGID CARGO BARRIER ATTACH FITTING NR 4R GOUGED. REPAIRED RCB ATTACH FITTING 4R IAW EA 011-5310-01-A4217 REV IR AND EO MD11-5310-48388-A.

Part: ATTACH FITTING — GOUGED (CARGO BARRIER) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, RIGID CARGO BARRIER ATTACH FITTING NR 3LH GOUGED. REPAIRED RCB ATTACH FITTING NR 3L IAW EA 011-5310-01-A4217 REV IR AND EO MD11-5310-48388-A.

Part: RIB — CRACKED (BS 1341) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, WING-TO-BODY PANEL SUPPORT RIB CRACKED ON LT SIDE OF FUSELAGE EXTERIOR AT STA 1341. REMOVED FABRICATED AND INSTALLED REPLACEMENT RIB AT LT SIDE STA 1341 IAW DWG ANB 7142 AND SRM 51-35-01.

Part: ATTACH FITTING — GOUGED (CARGO BARRIER) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, RIGID CARGO BARRIER ATTACH FITTING NR 4L GOUGED. REPAIRED RCB ATTACH FITTING NR 4L IAW EA 011-5310-01-A4217 REV IR AND EO MD11-5310-48388-A.

Part: SKIN — CRACKED (LT WING) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, NDT INSPECTION OF ALI 57.23.01.2, FOUND 10 CRACKS AT FASTENER HOLES AROUND CUT-OUT FOR LT WING LOWER ACCESS PANEL 536AB BETWEEN XORS 683-713. REPAIRED LT WING LOWER SURFACE PANEL CUT-OUT BETWEEN XORS 683-713 IAW EA 011-5730-01-A4187 REV IR, EO MD11-5730-48347-A, AND SRM 57-20-02, REPAIR 5.

Part: SKIN — CRACKED (LT WING) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, NDT INSPECTION OF ALI 57.23.01.2 FOUND CRACKS AROUND 4 FASTENER HOLES FOR LT WING ACCESS PANEL 536AB BETWEEN XORS 683-713. REPAIRED LT WING LOWER SURFACE PANEL IAW EA 011-5730-01-A4188 REV IR, EO MD11-5730-48311-A AND SRM 57-20-02, REPAIR 5, REV 50.

Part: BOLT — SHEARED (VERTICAL STAB) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, VERTICAL STAB LT SIDE NR 4 BANJO CARRY-THROUGH FITTING 6 SHEARED BOLTS. REPAIRED VERT STAB LT SIDE NR 4 BANJO FITTING BOLTS IAW EO MD11-5530-46641-A.

Part: MEMBRANE — CRACKED (BS 359 BL 0) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, COCKPIT SUBFLOOR MEMBRANE CRACKED BELOW RT OTBD SEAT. REPAIRED COCKPIT SUBLOOR MEMBRANE BS 355-366, LBL13 TO RBL13 IAW SRM 53-10-51 REPAIR 1, FIG 201.

Part: FRAME — CORRODED (BS 1996) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, FRAME BS 1996.75 CORRODED BETWEEN L51L -L51R. REPAIRED FRAME IAW EA 011- 5310-01-A4203 REV IR & EO MD11-5310-48442-A.

Part: SEAT TRACK — CORRODED (BS 2007) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, SEAT TRACK CORRODED IN MAIN CABIN BS 2007 AT RBL 107. REPAIRED SEAT TRACK BETWEEN BS 1831-2007, IAW SRM 53-00- 52. REPAIR 6, FIG 201 AND REPAIR 1, FIG 201.

Part: WEB — CRACKED (DOOR FRAME) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE:4C, R3 INTERNAL DOOR FRAME WEB CRACKED AT LOWER AFT LIGHTNING HOLE. REPAIRED INTERIOR WEB IAW SRM 53-40-15, REPAIR 3, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XFS 700. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS698-703 IAW EO MD11-5730-42916-D AND SRM 57-40-02, REPAIR 9, FIG.203

Part: SKIN — DENTED (BS 879) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, FUSELAGE DENT BS 879, 11.5 INCHES FWD OF LOWER CARGO DOOR. LONGERON 41.5. ACCOMPLISHED EA 011-5330-01-A4205 I/R, EO MD11-5330-48480-A.

Part: MOUNT — CHAFED (NR 2 PYLON) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, AFT ENGINE MOUNT BULKHEAD CHAFED. REPAIRED IAW EA 011-5410-01-A4202 REV IR & EO MD11- 5430-48396-A.

Part: WEB — CRACKED (DOOR FRAME) · airframe 46,791 hrs · 12,113 cycles

INSPECTION TYPE: 4C, R3 DOOR FRAME FWD INTERIOR WEB CRACKED AT LOWER LIGHTNING HOLE. REPAIRED R3 DOOR JAMB INTERIOR WEB STA 1250-1256 IAW MD11-SRM 53-40-15, REPAIR 3, FIG 201.

Part: LEAD — DISCONNECTED (FIRE LOOP)

ENGINE 2 FIRE LEVEL THREE ALERT AOM CHECKLIST ACCOMPLISHED. ALERT REMAINED DISPLAYED. AIR TURN BACK. EMERGENCY DECLARED. TROUBLESHOT IAW FIM 26-11-00-1, FIG 103. FOUND PYLON "A" LOOP DETECTOR HAS OPEN CIRCUIT. LEADS TO NR 2 ENG PYLON "A" LOOP DETECTOR DISCONNECTED AT LEADS IAW AMM 26-11-03-4. R & R LOOP IAW 26-11-03-4.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION)

AT APPROX 10 MINUTES INTO FLIGHT, THE FLIGHT CREW REPORTED NR 2 ENGINE FIRE INDICATION AND DIVERTED. 1 FIRE BOTTLE WAS BLOWN AND THE INDICATION WENT AWAY. DISCOVERED THE FAULT TO BE WITH IN THE NR 2 FDCU AND REPLACED IT IAW THE AMM. THE FIRE BOTTLE WAS REPLACED AND A WIND MILL INSPECTION WAS COMPLETED AND THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY BATTERY 1 LOW, DISPLAYED DURING TEST. EMERGENCY LIGHTING BATTERY POWER SUPPLY, REPLACED IAW AMM 33-51-01-4. OPS CHECKED GOOD IAW AMM 33-51-01-5.

Part: SKIN — DENTED (BS 892 L40R) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:C3, LOWER FWD CARGO DOOR JAMB SKIN HAS A DENT AT STA 892, L40R. CUT OUT DAMAGED AREA, HFEC SURFACE AREA. FABRICATED AND INSTALLED A REP AIR FILLER AND 2 LAYER DOUBLER IAW EA 011-5330-01-A3366 AND EO MD11-5330-44030-A.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:C3, TAIL ENGINE AFT PYLON SKIN REPAIR, EO MD11-5410-42470-A. REMOVED & FABRICATED A STIFFNER, DOUBLER AND FILLER IAW EA 011-5410 -01-A3369-2. FABRICATED SPLICE IAW EA 011-5410-01-A3369 AND DWG AUB7 518 REV V. INSTALLED REPAIR PARTS IAW EA 011-5410-01-A3369. COMPLIED WITH EA 011-5410-01-A3369 AND EO MD11-5430-44035-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT STA.XOS792. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS789-795 IAW SMR 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: STRINGER — CRACKED (RT WING L/E) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT RIB/WEB STRINGER CRACKED AT STA XOS792. REPAIRED STRINGER BETWEEN XOS789-795 IAW SRM 57-40-03, REPAIR 2, FIG 201.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACK AT XOS 638. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203, EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT STA XOS701. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS698-703 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS670 REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS667-673 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACK AT XOS STA 613. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 2, FIG 203, AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, RT WING L/E COMPT BEADED DOUBLER CRACK IN 2 BAYS AROUND FASTENERS AT X OS STA 622 AND STA 626 JUST ABOVE FUEL. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: FORMER — CRACKED (LT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LEFT WING L/E COMPTARTMENT AT STA XOS 1026 RIB SUPPORT CRACKED AT AFT END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB SUPPORT IAW DWG ARB2920, SRM 51-31-01, AND SRM 51-33-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT AT APPROX XOS683 BEADED DOUBLER IS CRACKED AT 2 FASTENERS. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS679-685 IAW SRM 57-40-02. REPAIR 9 FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT AT APPROX STA XOS669 BEADED DOUBLER CRACKED AT ONE FASTENER. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS667-673 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT AT APPROX STA XOS649, BEADED DOUBLER CRACKED AT 1 FASTENER. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS643-648 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT AT APPROX XOS694 BEADED DOUBLER IS CRACKED AT ONE FASTENER. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS692-698 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: SKIN — CHAFED (LT WING L/E) · airframe 44,753 hrs · 11,566 cycles

INSPECTION TYPE:3C, LT TELESCOPING DUCT DOUBLER REPAIR HAS CHAFING DAMAGE ON INBD AND OTBD SIDES. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED REPAIR IAW STA-SA EA 011-5750-01-A3368 I/R AND EO MD11-5730-44029-A.

Part: SKIN — LOOSE (NR 2 NACELLE)

NR 2 ENG PYLON SKIN LOOSE RIVETS. REPAIRED IAW EO MD11-5410-42470-A.

Part: FLOOR PANEL — DELAMINATED (CABIN)

FLOOR PANEL DELAMINATED FWD OF GALLEY. FABRICATED NEW PANEL IAW MD11-5320-42456-A ON NRC 396932.

Part: RIB — CRACKED (RT WING L/E) · airframe 42,194 hrs · 10,962 cycles

INSPECTION TYPE:2C, FOUND RIB CRACKED AT RT WING L/E TELESCOPIC CUTOUT XOS 464 REF N/R 357008 IAW NDT VERIFICATION. REMOVED RIB, FABRICATED AND INSTALLED NEW RIB IAW DWG ARB1284.

Part: SKIN — CRACKED (RT WING L/E) · airframe 42,194 hrs · 10,962 cycles

INSPECTION TYPE:2C, RT WING L/E EXTERIOR SKIN, ANTI-ICE TELESCOPIC DUCT CUT OUT AT APPROX WS XOS 464-470 HAS 2 EA CRACKS IN CORNERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBER IAW SRM 57-40-01, REPAIR 10, FIG 201.

Part: WEB — CRACKED (RT WHEEL WELL) · airframe 42,194 hrs · 10,962 cycles

INSPECTION TYPE:2C, RT WHEEL WELL BETWEEN STA 1441 AND 1461 JUST NEXT TO DOOR ACTUATOR BEAM HAS UPPER WEB CRACKED. REMOVED WEB, FABRICATED, AND INSTALLED WEB IAW AEA0218 WT-00588.

Part: RIB — CRACKED (RT WING L/E) · airframe 42,194 hrs · 10,962 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E COMPARTMENT AT APPROX WW XOS 160 PANEL LANDING RIB CRACKED. REMOVED RIB, FABRICATED AND INSTALLED NEW RIB IAW DWG ARB1161.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT BAT 1 MESSAGE DURING TEST REF T/C 0001 STEP 18. R & R RECHARGEABLE BATTERY EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01-4. OPS GOOD IAW MM 33-51-01-5.

Part: POWER SUPPLY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS BATTERY LOW. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECK NORMAL.

Part: BOTTLE — DISCHARGED (L1 DOOR ASSIST)

L1 DOOR ACCUM DISCHARGED. SERVICED L-1 DOOR PNEUMATIC ASSIST BOTTLE PER MM 12-25-04-3, OPS CK GOOD.

Part: SKIN — DENTED (TE FLAP)

INSPECTION TYPE:N/A LT WING UPPER SKIN DENTED ON I/B FLAP. REPAIR PER EO MD-11-5750-33299A.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A PER EO MD11-5330-33297-A, REMOVE TRIPLER FROM REPAIR AT STATION 1741, BETWEEN STRINGER L43L AND L47L. REMOVED REPAIR DOUBLER/TRIPLER, FABRICATED NEW DOUBLER/TRIPLER, AND INSTALLED REPAIR PARTS IAW EO MD11-5330-33297-A.

Part: SKIN — DENTED (BS 1741 L45L) · airframe 39,387 hrs · 10,288 cycles

INSPECTION TYPE:1C FOUND DENT ON LWR LT FUSELAGE STA 1741 LONGERON L45 OUT OF LIMITS, REF N/R 342660. REMOVED DENT, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLERS, AND FINGER DOUBLER IAW MD-11 SRM 53-20-00 FIG 6 SHEETS 2 AND 3 AND UPS EO MD11-5330-18894-C.

Part: SKIN — MISREPAIRED (RH WINGLET) · airframe 39,387 hrs · 10,288 cycles

INSPECTION TYPE:1C RT WINGLET REQUIRE LE BULLNOSE REMOVED TO EVALUATE AND NDT EXISTING REPAIR, SEQ W4-01, REPAIR NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5720-31992-A.

Part: SKIN — CRACKED (LT WING) · airframe 39,387 hrs · 10,288 cycles

INSPECTION TYPE:1C LEFT WING TELESCOPIC DUCT CUTOUT UPPER CUTOUT CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-10-00 FIG 43 SHT 1-5.

Part: SKIN — GOUGED (NR 2 SLAT) · airframe 39,387 hrs · 10,288 cycles

INSPECTION TYPE:1C GOUGE POSSIBLE CRACK ON LOWER SURFACE OF RT NR 2 SLAT, STICKER 26- RH2. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-00-01 FIG 8.

Part: SKIN — DAMAGED (WINGLET)

INSPECTION TYPE:N/A WINGLET L/E SKIN DAMAGED. REPAIRED IAW EO MD11-5720-30288-C.

Part: PANEL — DELAMINATED (RT WING)

INSPECTION TYPE:N/A DELAMINATION DAMAGE ON RT WING I/B LEADING EDGE FILLET PANEL. C/W EO MD11-5730-31467-D REF NRC 268556 FOR JOB COMPLETION AND DEFERRAL CLEARING ACTION.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 39,013 hrs · 10,176 cycles

INSPECTION TYPE: S.V. NOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER, REPAIR DOUBLER AND STRAP IAW SRM 53-40-00 FIG 23 NOTE 9.

Part: STRUCTURE — CORRODED (BS 1009-1019) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:C4 WHILE GAINING ACCESS TO REPLACE A SHEARED FASTENER FOUND EXTENSIVE EXFOLIATION CORROSION BETWEEN L43R AND 45R, STA 1009 TO 1039. CORROSION DAMAGE REPAIRED PER EO 011-5310-29279-A AND EA 011- 5340-01-A1329, FINAL AND ADVANCED COPIES.

Part: FRAME — CRACKED (BS 1258) · airframe 37,098 hrs · 1,307 cycles

INSPECTION TYPE:4C CRACK AT FRAME TO FLOOR BRACKET AT FS 1258 RBL 106. REMOVED, FABRICATED, AND INSTALLED FRAME PER EO MD11-5310-29275-A DAC DWG AEA7605, MD-11 SRM 53-33-01, AND SAA EA 011-5310-01-A1340.

Part: SEAT TRACK — CORRODED (BS 475) · airframe 37,098 hrs · 1,307 cycles

INSPECTION TYPE:4C AT STA 475 FROM 0 BUTTLINE TO OUTBOARD AFT OF R1 DOOR AREA SEAT TRACK FOR RCB PANEL IS CRACKED (EXFOLIATED CORROSION). REMOVED, FABRICATED, AND REPLACED SEAT TRACK PER DWG WSP0826, SAA TRAVELER 79598420001, AND SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 495) · airframe 37,098 hrs · 1,307 cycles

INSPECTION TYPE:2C RCB LEFT FLOOR PANEL SUPPORT AT STA 495 CRACKED AND BUCKLING ON INBOARD SUPPORT AS WELL (EXFOLIATED CORROSION). REMOVED, FABRICATED, AND REPLACED SEAT TRACK PER DWB WSP0826 SAA TRAVELER 79598410001, AND SRM 51-33-01, 51-21-00.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C LEFT WING LE ACCESS PANEL LANDING AT NR 9 SLAT TRACK CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG.18.

Part: SKIN — CRACKED (RT WING LE) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C RT WING LE ACCESS PNL LANDING AT SLAT TRACK FITTING 9 STRINGER CRACKED. REMOVED CRACKED STRINGER DOUBLER. FABRICATED AND INSTALLED REPLACEMENT STRINGER DOUBLER IAW DWG ARB1180 AND MD-11 SRM 51-33-01.

Part: SKIN — CRACKED (LT WING LE) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C LEFT WING LE NR 14 SLAT TRACK CUT OUT CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 21 AND 51-33-01.

Part: SKIN — CRACKED (RT WING) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS669 CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED AND INSTALLED REPLACEMENT SPLICE STRAP IAW DWG ARB3954 AND MD-11 SRM 51-33-01.

Part: SKIN — CRACKED (LT WING LE) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C LEFT WING LE SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED CRACKED SKIN SPLICE STRAP. FABRICATED AND INSTALLED REPLACEMENT SKIN SPLICE STRAP IAW DWG ARB3954 AND 51-33-01.

Part: STRINGER — CRACKED (LT WING) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C LEFT WING LE ACCESS PNL LANDING XOS 550 STRINGER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 18 AND 51-33-01.

Part: STRINGER — CRACKED (RT WING) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C RT WING LE ACCESS PNL LANDING XOS 550 STRINGER DOUBLER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 18 AND 51-33-01.

Part: SKIN — CRACKED (RT WING) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS791 CRACKED. REMOVED CRACKED SKIN SPLICE. FABRICATED AND INSTALLED REPLACEMENT SKIN SPLICE IAW DWG ARB3954 AND MD-11 SRM 51-33-01.

Part: FITTING — CRACKED (LT WING LE) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C LEFT WING NR 16 SLAT TRACK IB FITTING CRACKED. REMOVED AND REPLACED NR 16 SLAT TRACK IB RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01.

Part: FITTING — CRACKED (RT WING LE) · airframe 37,098 hrs · 9,796 cycles

INSPECTION TYPE:4C RIGHT WING NR 16 SLAT TRACK FITTING IB CRACKED. REMOVED AND REPLACED NR 16 SLAT TRACK IB RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY POWER "OFF" LIGHT INOP. RELAMPED PER MM 33-00-00. OPS CHECK GOOD.

Part: SIGN — BROKEN (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT SIGN BROKEN. REINSTALLED EMERGENCY EXIT SIGN.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A UPON TEST EMERGENCY LT BATT 1 LO ANNUNCIATED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 1 PER AMM 33-51-01-4. OPS TEST PASS PER AMM 33-51-01-5.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST FAILED D354644 ASSIGNED. T/S PER FIM 33-51-02-00 & WDM 33-51-01, RESEATED & RESECURED R2-5700 (RELAY) & PERFORMED EMERGENCY LIGHT SYSTEM TEST. PASSED PER MM 33-50-00-5. THIS CLEARS M354644 AND PLACARD REMOVED.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY 1 LOW ALERT ON EMERGENCY LIGHTS TEST. RESET EMERGENCY LIGHT SWITCH. OPS CHECK OK. REF 33-50-00.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A LEVEL 1 ALERT EMERGENCY LIGHT BATTERY 1 LOW ALERT ON PREFLIGHT. PERFORMED R-T-S MSC PER FIM 33-51-00-1. OPS NORMAL.

Part: SWITCH — STICKING (L1 DOOR SLIDE)

L1 DOOR EVAC SLIDE REMOTE PRESS TEST INOP. C/O T/S AND FOUND SWITCH STICKY. ADJUSTED REMOTE PRESS TO TEST SWITCH AND REPLACED BATTERIES PER SMP WORKS NORMAL NOW M322380 CLOSED.

Part: WARNING LIGHT — FALSE ACTIVATION

AIR MAN 2 FAIL ALERT AND MAN FAIL LIGHT. T/S PER FRIM 36-23-06 BLOCK 5. REMOVED AND REPLACED MANIFOLD FAIL DETECTION CONTROLLER PER MM 36-23-00. PERFORMED RETURN TO SERVICE. NO FAULTS. RESET PSC CONTROLLERS. OPERATION NOW CHECKS NORMAL.

Part: MANIFOLD — FAILED (PNEUMATIC SYS)

MANIFOLD FAIL MESSAGE. T/S PER FIM 36-23-06 BLOCK 5 REMOVED AND REPLACED MANIFOLD FAIL DETECTION CONTROLLER PER MM 36-23-00. PERFORMED RETURN TO SERVICE NOT FAULTS RESET PSC CONTROLLERS. OPERATION NOW CHECKS NORMAL.

Part: SKIN — CORRODED (LT WING) · airframe 28,993 hrs · 8,425 cycles

INSPECTION TYPE:C2 LEFT WING TIP LWR SURFACE SKIN CRACKED .5 INCH LONG AND HAS HEAVY CORROSION AT XW 998. THE CORRODED AREA WAS TRIMMED OUT AND A FILLER AND DOUBLER WERE INSTALLED IAW SAA SK 270-894256 UPS ENG FILE MD11-57-20035, BOEING MSG 1-139605558-2 BOEING MSG 1-139605558-4, AND FAA FORM 8100-9.

Part: WARNING LIGHT — ILLUMINATED (AILERONS)

AILERON DEFLECTED DISAGREE MESSAGE. A/C WAS DIVERTED AND EMERGENCY WAS DECLARED. FUEL WAS DUMPED BELOW MAXIMUM LANDING WEIGHT TO 57000 POUNDS. REPLACED O/B AILERON DEFLECTION ACTUATOR UP TO SUB TASK 27-16-02-820-001 PG 8 PER MM 27-16-02-4. L/P 474801--COMPLETED STEPS 2, F (3) O FMM 27-16-02-4 TO END. COMPLETED ADJUSTMENT OF RT OB AILERON DEFLECTION ACTUATOR. SAFTIED BOTH JAM NUTS ON AILERON DEFLECTION ACTUATOR. [CLOSED]

Part: BRAKE ASSY — FAILED (LANDING GEAR)

DURING LANDING AUTOBRAKES FAILED TO DECELERATE THE A/C. AUTOSPOILERS DEPLOYED NORMALLY AND FULL REVERSE THRUST WAS APPLIED IMMEDIATELY MANUAL BRAKING, FULL SPOILERS AND FULL THRUST REVERSE WERE MAINTAINED. PERFORMED AUTO BRACK SYS IAW 32-44-00. NO DEFECT NOTED. SUSPECT FAULTY LT IBCW SEE L/ 414386. PERFORMED MAINT TAXI NO DEFECT NOTED SYS OPS CK SAT. OK FOR FURTHER FLIGHT. "BRAKE TEMP EVEN ACROSS LEFT/RIGHT."

Part: SMOKE GOGGLES — CRACKED (CABIN)

JUMP SEAT AREA RIGHT SIDE SMOKE GOGGLES NEED REPLACED LENS CRACKED. REPLACED SMOKE GOGGLES.

Part: SKIN — DELAMINATED (LT OB FLAP)

LEFT OUTBOARD FLAP DELAMINATED.

Part: SWITCH — INOPERATIVE (R1 DOOR SLIDE)

INSPECTION TYPE:N/A R-1 DOOR ESCAPE SLIDE BATTERY PACK LT PUSH TO TEST SWITCH LT INOP. RELAMPED, NO HELP (BAD SWITCH). FOUND IND LAMP HOUSING BASE BROKEN FROM HOUSING. REPLACED DOOR SLIDE IND IN REF TO MD11 WDM 25-61-01. LIGHT TESTS NORMAL.

Part: BUSS — FAILED (NR 1)

DURING FLT AT FL360 A/C BUS 1 FAILED & NUMEROUS C/B BEGAN TO POP. THE FOLLOWING ITEMS ALSO FAILED: NR 2 DU, CAPTS NAV GUIDANCE, NR 3 DU DISPLAYED INOPERATIVE FAIL, GROSS WEIGHT, FUEL QTY, CG X'D OUT, EPR NR 1; 2 INDICATORS OUT, UNABLE TO GET NR 1 TO OP STBY, F/F NR 1 OUT, OIL PRES NR 1 OUT, OIL QTY NR 3 OUT, NR 1 COMM FAILED, ACARS FAILED, TAIL R PUMP LO, TANK NR 1 FWD PUMP OFF, ATC 1 TRANSPONDER INOP, FUEL CONFIG, AUTO SLAT FAIL, NO AUTOL AND, AUX IRU FAILED, IRU AUX ON BATT, IRU BATT LO LT ON, AVIONIC FLOW LT ILLUMINATED, FUEL QTY ALERTS ON. REPLACED RCCB B1-174 PER MM 24-50-01. OPS NORMAL. THIS CLEARS ALL FAULTS

Part: LIGHT — WILL NOT TEST (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS WILL NOT TEST. DEFERRED PER MEL 33-50-2. REF M271306. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED NORMAL. THIS CLEARS M271306. REF LP675424

Part: LIGHT — WILL NOT TEST (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT TEST FAIL. PLACED ON DFRL M263353. OPS TESTED GOOD PER FIM 33/51/02. THIS CLEARS DFRL M263353.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT BATTERY LOW TEST FAIL. FOUND EMERGENCY PWR SELECTOR IN OFF SELECTED ARM OPS CK NORMAL IAW 33/51/01 & FIM 33/51/02.

Part: SMOKE DETECTOR — FAILED (CABIN)

CLIMBING THROUGH 26000 FT, CABIN SMOKE LEVEL 3 ALERT ILLUMINATED. 1 SENSOR TOP DECK. MECHANIC FOUND NR 3 SENSOR SHOWING FAILED. 0 STOCK MECHANIC DEFERRED IAW MEL REF M2 61900.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C, CABIN INTERIOR FOUND LONGERON SPICE L-24L BETWEEN STA 5-113 & STA 15 41 WITH CRACK AS MARKED. CRACKED LONGERON SPLICE L-24 BETWEEN STA 5-113 TO 1541. REMOVED PER SRM 51-33-01 VOL 2 REV 32. NEW STRINGER SPLICE FABRICATED AS DWG A5A7 112 AND PROTECTED PER SRM 51-21-01 VOL 2 REV 32. FAB LONGERON SPLICE, INSTALLED AS PER SRM 51-33-01 VOL 2 REV 32.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C, CABIN INTERIOR FOUND LONGERON SPICE L-18L BETWEEN STA 5-113 & STA 15 41 WITH CRACK AS MARKED. REMOVED CRACKED LONGERON SPICE L-18 BETWEEN STA 5-113 TO 1541 AS PER SRM 51-33-01 VOL 2 REV 32. NEW STRINGER SPLICE FAB AS PER DWG A5A7112, FAB LONGERON SPLICE, INSTALLED AS PER SRM 51-33-01 VOL 2 REV 32.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C CABIN CORROSION ON SEAT TRACK BETWEEN STA 1721-1761 AS MARKED ON X=8.5. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 32 AT SEAT TRACK STA 1721-1761, X-8.5 EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1 REV 32. DAMAGED PORTION OF SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED.

Part: SKIN — CORRODED (RT WING) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C, RT WING EXTERNAL SURFACE AT STA XORS 683-700 AFT STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MATERIAL REMOVED 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AS PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIED VISUAL INSPECTION ON BLEND OUT AREA CUT OUT AS PER EN1001-03. REWORKED AND PROTECTED AS PER SRM 51-21-01 VOL 2 REV 32.

Part: SKIN — CORRODED (RT WING) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT XORS 740-745 AFT OF STRUCTURE 1 FOUND CORRODED AT 2 PLACES AS MARKED. REMOVED MATERIAL 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AT XOR S 740-745 AS PER SRM 57-10-00 FIG 32 VOL 1 REV 32. REWORKED & PROTECTED AS PER SRM 51-21-01 VOL 2 REV 32.

Part: SKIN — CORRODED (RT WING) · airframe 22,206 hrs · 7,099 cycles

INSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT STA XORS 683-700 AFT OF STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MAT REMOVED 0.023 ORIGINAL THICK 0.200, FOUND OUT OF LIMIT PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIED VISUAL INSP ON BLEND OUT AREA CARRIED OUT PER EN1001-03, SHOT PEEN CUTOUT AS PER DPS4999 & REWORKED AREA REPROTECTED PER SRM 51-21-01 VOL 2 REV 32.