N921FT

Part: TRANSMITTER — FAILED (ENGINE EPR) · airframe 66,174 hrs · 14,778 cycles

ON TAKEOFF ROLL, CREW REPORTED NR 3 ENGINE EPR WOULD NOT ADVANCE ABOVE 1.2 EPR, FULL TRAVEL OF THROTTLE HAD NO EFFECT. TAKEOFF ABORTED AT 80 KTS IAS EPR ON NR 3 STAYED AT 1.2 UNTIL ENGINE SHUTDOWN. REPLACED EPR TRANSMITTER, PERFORMED LEAK CHECK AND RAN ENGINE. ALL PARAMETERS NORMAL.

Part: TRANSMITTER — FAILED (NR 3 EPR) · airframe 66,147 hrs · 14,774 cycles

ON CLIMB, NR 3 ENGINE EPR STARTED DECREASING AT FL310 EPR IND., ON DESCENT IT READ HIGH (1.24 AT 150 WITH THRUST LEVERS IDLE) (CORRECTIVE ACTION) REPLACED EPR TRANSMITTER IAW MM 77-11-00 AND DEFERRED OPS CHECK IAW DDPG 77-4.

Part: SKIN — CORRODED (RT WING) · airframe 66,109 hrs · 14,768 cycles

CORROSION ON RT UPPER SKIN AFT OF REAR SPAR WS 560 TO 575. REMOVED CORROSION & REPAIRED IAW BOEING REPAIR PROCEDURE 1-129539127-5 AND 8100-9.

Part: FITTING — CORRODED (LT WING) · airframe 66,109 hrs · 14,768 cycles

LEFT WING AT UPPER CHORD OF SPLICE FITTING OF WING REAR SPAR HAS CORROSION BETWEEN WS 553 AND WS 558. CORROSION BLENDED OUT IAW SRM 57-30-01. HFEC & ULTRASONIC INSPECTION OF AREA CONFIRMED REMOVAL OF CORROSION IAW NDT 06-7170 PT 6, 51-00-00 FIG 23, 12. D6-7170 PT4.

Part: SUPPORT BEAM — CRACKED (LT WING) · airframe 66,109 hrs · 14,768 cycles

LEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD CRACKED (APPROX 2 INCHES) AT WS 528.20, WBL 235.20.

Part: PANEL — CRACKED (SPOILER) · airframe 66,109 hrs · 14,768 cycles

LEFT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02.

Part: PANEL — CRACKED (SPOILER) · airframe 66,109 hrs · 14,768 cycles

LT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REPLACED NR 3 SPOILER ASSEMBLY IAW AMM 27-61-02.

Part: SWITCH — OUT OF ADJUST (T/REV STOW) · airframe 65,918 hrs · 14,728 cycles

NR 2 ENGINE REVERSER UNSTOW. ADJUSTED NR 2 REVERSER STOW SWITCH PER MM 78-31-00.

Part: MODULE — FAILED (TE FLAPS) · airframe 65,917 hrs · 14,727 cycles

DURING CRUISE, LEADING EDGE FLAP GROUP 1, 2, 3, 4 LEFT AND 1 RIGHT DISPLAY AMBER, GROUPS 1 & 2 LEFT ALSO DISPLAY GREEN. REPLACED MODULE OPS CHECK OK PER MM 27-88-00.

Part: ACTUATOR — FAILED (CARGO DOOR HOOK) · airframe 65,893 hrs · 14,722 cycles

SIDE CARGO DOOR HOOK ACTUATOR FAILED IN ELECTRICAL MODE. DEFERRED PER MEL 52-20.

Part: DOOR — MISSING (MLG) · airframe 65,608 hrs · 14,661 cycles

ON POSTFLIGHT WALKAROUND, FOUND LEFT BODY GEAR O/B SHOCK STRUT DOOR MISSING. REPLACED DOOR PER MM 32-14-06.

Part: CLAMP — FAILED (NR 1 ENGINE) · airframe 65,215 hrs · 14,585 cycles

NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE. OPS AND LEAK CHECK OK PER MM 36-13-00 AND 71-00-00.

Part: CLAMP — FAILED (PNEUMATIC SYS) · airframe 65,275 hrs · 14,585 cycles

CREW REPORTED NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE, MM 36-13-00. OPS AND LEAK CHECK OK MM 71-00-00.

Part: DATA CARD — FAILED (GPS) · airframe 64,629 hrs · 14,456 cycles

GPS DATA CARD FAILED. TRANSFERRED TO DMI 34058 PER MEL 34-27-2S.

Part: DOOR — MISSING (THRUST REVERSER) · airframe 64,517 hrs · 14,433 cycles

ON POST FLIGHT NR 3 ENGINE REVERSER PANEL MISSING. ACCOMPLISHED INTERIM REPAIR PER SRM 51-00-04 AND SRM 51-40-16, ALSO GMM 3-17-1. TRANSFERRED TO C/O ITEM 921-179.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 64,427 hrs · 14,412 cycles

NR 2 ENGINE THRUST REVERSER LIGHT CAME ON FLASHING AS ENGINE APPROACHED TAKE OFF EPR. DEFERRED T/R PER MEL NR 78-3-1B.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 64,388 hrs · 14,402 cycles

CREW REPORTED NR 1 ENGINE WOULD NOT MAKE TAKEOFF EPR. INSPECTED NR 1 ENGINE PER MM 71-00-00, OPENED MEL 77-4-1 FOR EPR UNRELIABLE.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 64,218 hrs · 14,360 cycles

ON PREFLIGHT FOUND BOTH SEAT TRACKS BROKEN ON THE F/O'S SEAT (AFT SEAT TRACK). REMOVED & REPLACED BOTH LT & RT AFT SEAT TRACKS PER AMM 25-11-00.

Part: PUMP — LEAKING (NR 2 HYD SYSTEM) · airframe 64,211 hrs · 14,359 cycles

DURING CLIMB NR 2 ENGINE OIL QTY DROPPED TO ZERO. AFTER 5 MINUTES OIL PRESSURE 40 PSI AND FLUCTUATING. OIL TEMPERATURE NORMAL. ENGINE SHUTDOWN. REPLACED EDP PER MM 29-141-05. LEAK AND OPS CHECK OK PER MM 29-11-05.

Part: THRUST REVERSER — INOPERATIVE (NR 4 ENGINE) · airframe 65,218 hrs · 14,360 cycles

NR 4 ENGINE THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. NR 4 ENGINE THRUST REVERSER DEACTIVATED PER MEL 78-01-2A. REF MM 78-31-00.

Part: PUMP — LEAKING (NR 2 HYD SYSTEM) · airframe 64,211 hrs · 14,359 cycles

LOSS OF NR 2 HYDRAULIC SYSTEM. HYDRAULIC QUANTITY WENT FROM 6.5 GALLONS TO ZERO IN LESS THAN 5 SECONDS. FOUND NR 2 ENG EDP CASING CRACKED. REMOVED NR 2 EDP PER MM 29-11-05 AND DEFERRED PER MEL 29-1A.

Part: SWITCH — MALFUNCTIONED (STAB TRIM IND) · airframe 64,048 hrs · 14,325 cycles

AT APPROXIMATELY 80 KNOTS TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AT OKO. STAB TRIM WAS AT THE EDGE OF THE GREEN BAN. CAPTAINS TRIM INDICATOR HAS NO CENTER INDEX. MAX THRUST WAS SET PRIOR TO BRAKE RELEASE AT TAKEOFF OKO. RESET GREEN BAND SWITCH PER MM 31-26-00.

Part: PULLEY — WORN (FLT CONTROLS) · airframe 64,048 hrs · 14,325 cycles

ON TAXI OUT, FLIGHT CONTROL CHECK REVEALED WHEN CONTROL WHEEL TURNED TO LEFT, NORMAL MOVEMENT OBSERVED. WHEN CONTROL WHEEL TURNED TO RIGHT IT STOPPED AT 10 DEGREES FOR 4-6 SECONDS THEN RETURNS SLOWLY TO NEUTRAL. FOUND CABLE PULLEY IN LT WHEEL WELL WORN. REPLACED PULLEY, PERFORMED AILERON AND AILERON TRIM SYSTEM TEST PER MM 27-11-00. ALL OPS NORMAL.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 64,017 hrs · 14,317 cycles

NR 3 HYD SYS LOST 2 GALS IN THIS FLIGHT FROM UAM-HIK. FOUND LINE LEAKING FROM CASE DRAIN FOR NR 3 EDP. REMOVED EDP DUE TO LEAK. ITEM TRANSFERRED TO DMI 33554 PER MEL 29-1A.

Part: DRAIN MAST — LEAKING (NR 3 ENGINE) · airframe 64,017 hrs · 14,317 cycles

NR 3 ENGINE HYD LEAK AT DRAIN MAST. FOUND HYD LEAK WITHIN LIMITS PER MM 29-11-00 FIG 601.

Part: PROXIMITY SWITCH — DAMAGED (NLG)

NOSE LANDING GEAR ALT SQUAT SWITCH FOUND DAMAGED. REPLACED NLG ALT SQUAT SWITCH PER MM 32-60-00.

Part: THRUST REVERSER — MALFUNCTIONED (NR 4 ENGINE) · airframe 63,889 hrs · 14,290 cycles

NR 4 ENGINE THRUST REVERSER OPERATING LIGHT CAME ON IN FLIGHT. NO ADVERSE INDICATIONS. REPLACED PDU, NO HELP REV INOP. TRANSFERRED TO DMI 33496 PER MEL 78-2A. PLACARD INSTALLED.

Part: INDICATOR — NO INDICATION (NR 3 ENG EPR) · airframe 63,692 hrs · 14,246 cycles

NR 3 ENGINE HAS NO EPR INDICATION WHEN ACCELERATING. TRANSFERRED TO DMI 33386 PER MEL 77-04-1.

Part: THRUST REVERSER — DAMAGED (NR 1) · airframe 63,692 hrs · 14,246 cycles

ON POST FLIGHT, MAINTENANCE WALK AROUND, FOUND NR 1 RT REVERSER HALF HAS DAMAGE TO PREVIOUSLY REPAIRED AREA AT FWD EDGE BETWEEN 4 O'CLOCK AND 6 O'CLOCK. REPAIRED CARRIED OUT PER SRM 54-30-03 AND 54-03.

Part: STARTER — MALFUNCTIONED (NR 1 ENGINE) · airframe 63,526 hrs · 14,216 cycles

NR 1 ENGINE WOULD NOT TURN ON, PYLON VALVE & START VALVE INDICATES OPEN. REPLACED STARTER, OPS CHECK OK PER AMM 80-11-00.

Part: FLAP — MALFUNCTIONED (NR 2 LT) · airframe 63,347 hrs · 14,176 cycles

NR 2 LEFT LEADING EDGE WOULD NOT COME UP PNEUMATICALLY, OK ELECTRICALLY. RECYCLED FLAPS PNEUMATICALLY, NO HELP. TRANSFERRED TO DMI 33203.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 63,127 hrs · 14,134 cycles

NR 2 ENG THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON FORWARD ANNUNCIATOR PANEL ON POWER UP FOR TAKEOFF. REPEATED THRUST REVERSER LIGHT ON FLIGHT ENGINEER PANEL. LOCKED OUT REVERSER PER AMM 78-00-00, OPENED MEL 78-12A.

Part: ACTUATOR — MALFUNCTIONED (FUEL CONDITION) · airframe 63,127 hrs · 14,134 cycles

AFTER PUSHBACK, ON ENGINE START NR 1 ENGINE FUEL CONDITION ACTUATOR CIRCUIT BREAKER OPENED. REMOVED AND REPLACED NR 1 FUEL CONDITION ACTUATOR, ALL OPS NORMAL.

Part: SEAL — LEAKING (NR 1 ENGINE OIL) · airframe 63,006 hrs · 14,109 cycles

DURING CRUISE, NR 1 ENG OIL QTY GRADUALLY DECREASED, OIL PRESSURE & TEMP NORMAL, CLOSELY MONITERED OIL QTY, WHEN ZERO OIL PRESSURE INDICATED, GAUGE FLUCTUATED & OIL PRESSURE LIGHT FLICKERED, SHUTDOWN ENGINE, ENGINE FAILURE / SHUTDOWN CHECKLIST ACCOMPLISHED. OIL PRESSURE STAYED 20-30 PSI AFTER SHUTDOWN. INSPECTED NR 1 ENG, FOUND NR 1 EDP DRIVE SHAFT SEAL DETERIORATED. REMOVED AND REPLACED SEAL, PERFORMED INSP PER 72-00-00 & PERFORMED EDP TEST PER AMM 29-11-05.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 63,002 hrs · 14,108 cycles

VIA PHONE PATCH, CREW REPORTS 0 PSI/0 QTY ON NR 1 HYDRAULIC SYSTEM. INSTALLED TEMP FLEX LINE PER MM 20-11-18 & GMM 3-17-1, PLACED ITEM ON COI 921-163. LINE IS LOCATED AFT OF STATION 23600 ON LT SIDE.

Part: CLAMP — DAMAGED (HI STAGE VALVE) · airframe 62,846 hrs · 14,070 cycles

NR 3 ENGINE HIGH STAGE VALVE WILL NOT OPEN AT ALTITUDE WITH THRUST LEVER CLOSED. REPLACED CLAMP ON HIGH STAGE VALVE, OPERATIONAL CHECK & LEAK CHECK OK PER MM 36-11-00.

Part: LIGHT — INOPERATIVE (INSTRUMENT PANEL) · airframe 62,861 hrs · 14,070 cycles

TAT, SAT, IB FLAPS AND P-10 PANEL LIGHTS OUT, ALSO BACKGROUND HSI, CLOCK AND AIR SPEED IND. TRANSFERED TO DMI NR 32904 IAW MEL 33-1.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 62,777 hrs · 14,053 cycles

NR 3 THRUST REVERSER DAMAGED. PERFORMED INTEAM REPAIR IAW SRM 54-07-00. THRUST REVERSER REPAIR PLACARD ON COI NR 162. TRANSFERED TO DMI NR 32887 T/R DEACTIVATED IAW MEL 78-1-2.

Part: WEB — CRACKED (LT OB ELEVATOR) · airframe 62,700 hrs · 14,034 cycles

WEB CRACK FOR CENTER WEIGHT, LT OB ELEVATORS OB ACTUATOR ELEV STA 256. REMOVED CRACKED WEB IAW SRM 51-30-02, FABRICATED WEB IAW SRM 55-20-02, INSTALLED WEB IAW SRM 51-30-02.

Part: PACKING — LEAKING (NR 4 ENGINE) · airframe 62,727 hrs · 14,042 cycles

NR 4 ENGINE IN OIL QTY DROPPED FROM 10.5 GAL BEFORE START TO 8.5 GAL AT IDLE. ON APPROACH INDICATION WENT TO ZERO WITH PRESSURE FLUXUATION B/W 40 AND 25 PSI. REMOVED CSD FOR OIL LEAK, INSTALLED CSD WITH NEW O-RING, OPS CHECK OK, LEAK CHECK OK, OIL PRESSURE NORMAL, OK FOR SERVICE IAW MM 24-11-01.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,700 hrs · 14,034 cycles

CORROSION ON KEELBEAM 2 PLACES, AT BS 1332 AND STA 1319 RT SIZE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW MA NR A5349-01-02, WORK ACCOMPLISH ON T160-468.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,700 hrs · 14,034 cycles

CORROSION UPPER DECK SEAT TRACK BS 540-580 RBL 46.65-WL 310. REMOVED AND REPLACED SEAT TRACK FROM BS 530-660, IAW SRM 53-10-05-53-30-08-53-30-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,700 hrs · 14,049 cycles

SEAT TRACK CORRODED & CRACKED B/W STA 580-560 LBL 62 UPPER DECK. REMOVED DAMAGE SECTION OF SEAT TRACK FROM STA 530-620 IAW SRM 51-30-08. NEW SECTION OF SEAT TRACK INSTALLED PER SRM 51-40-02, 51-11-25.

Part: STIFFENER — CORRODED (ELEVATOR) · airframe 62,700 hrs · 14,049 cycles

STIFFENER CORRODED ON O/B SIDE ELEV, STA 406-5 LEFT HORIZONTAL STAB. REMOVED CORROSION FOUND OUT OF LIMIT PER SRM 55-20-01. REMOVED AND REPLACED STIFFENER AS PER SRM 51-30-02.

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 62,700 hrs · 14,034 cycles

LT WING IB MID FLAP IB FORE FLAP TRACK WBL535 CUT OUT IS CRACKED AT IB LEADING EDGE RIB. REMOVED CRACKED ANGLE IAW SRM 51-30-02, FABRICATED REPAIRED DOUBLER IAW SRM 51-40-02, FIG 2 TREATED AND PAINTED INST DOUBLER IAW SRM 51-30-02, INST ANGLE IAW SRM 51-30-02.

Part: SKIN — DELAMINATED (LT IB AILERON) · airframe 62,700 hrs · 14,034 cycles

LT IB AILERON DELAMINATED LOWER SIDE WBL500 2 PLACES. REPAIR 2EA DAMAGED AREA WITH FIBER GLASS IAW SRM 51-40-15, APPLIED CONDUCTIVELY COATING, PRIMED AND PAINTED.

Part: SKIN — ERODED (LT IB FORE FLAP) · airframe 62,700 hrs · 14,034 cycles

LT WING IB FORE FLAP UPPER TRAILING EDGE WBL235 EROSION MIDDLE SECTION. REMOVED DAMAGE, APPLIED FIBERGLASS OVERLAY IAW SRM 51-40-15, APPLIED ANTISTATIC TO REPAIR IAW SRM 51-40-15, PAINTED IAW SRM 51-40-15.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,700 hrs · 14,034 cycles

RT KEEL BEAM CORROSION FROM BS 1310 TO BS 1342. LT KEEL BEAM CORROSION FROM STA 1310 TO STA 1340. REPAIR IAW POLAR MA NR A5349-01-02.

Part: DOOR — CRACKED (MLG) · airframe 62,474 hrs · 13,983 cycles

LEFT WING GEAR INBOARD SHOCK STRUT DOOR LEADING EDGE HAS CRACK. REPLACED DOOR.

Part: DRIVE UNIT — MALFUNCTIONED (NR 1 LE FLAP) · airframe 62,096 hrs · 13,898 cycles

NR 1 L/E FLAP REQUIRES ALTERNATE PROCEDURE TO EXTINGUISH IN TRANSIT LIGHT. R&R NR 1 L/E DRIVE UNIT PER MM 27-81-03.

Part: TRANSMITTER — FAILED (EPR) · airframe 62,026 hrs · 13,880 cycles

NR 1 ENG WOULD NOT PRODUCE TAKEOFF THRUST OF 1.53 EPR. DROPPED TO 1.45 EPR AT FWD THROTTLE STOP. ABORTED T/O. REPLACED EPR TRANSMITTER PER MM 77-11-02. ENGINE GROUND OPS CHECK OK PER MM 71-00-11 TEST NR 9.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 62,010 hrs · 13,876 cycles

N4 T/R ARMED LIGHT ON DURING TAXI. OPENED MEL 78-06-A, CONFIRMED REVERSER STOWED.

Part: SEAL — BROKEN (N2 ENG DUCT) · airframe 61,977 hrs · 13,867 cycles

LEFT WING L/E OVERHEAT LIGHT ON. REPLACED BROKEN SEALS ON L/E DUCT INBOARD OF NR 2 ENG AND BY THE NR 3 PDU OPS AND LEAK CHECK OK PER MM 36-11-01 AND 26-18-01.

Part: FAN BLADE — BROKEN (NR 3 ENGINE) · airframe 61,977 hrs · 13,867 cycles

NR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED.

Part: INTAKE — DELAMINATED (NR 2 NACELLE) · airframe 61,977 hrs · 13,867 cycles

NR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COWLING.

Part: PANEL — CRACKED (LT WING) · airframe 61,977 hrs · 13,867 cycles

LEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL.

Part: PITOT HEAD — FAULTY (RIGHT) · airframe 61,890 hrs · 13,846 cycles

RIGHT AUX PITOT PROBE FAULT LIGHT ON. REMOVED AND REPLACED RIGHT AUX PITOT PROBE GROUND TEST & LEAK CHECK OK.

Part: CLAMP — FAILED (NR 2 ENG) · airframe 61,854 hrs · 13,839 cycles

WHILE IN CLIMB FL 29-30 NR 2 ENG FIRE WARNING ON HANDLE AND BOTH FIRE LOOPS CAME ON. ENG SHUT DOWN AND A/C DIVERTED TO NRT. REMOVED AND REPLACED NOSE COWL ANTI-ICE CLAMP. LEAK CK OK IAW MM 30-21-00.

Part: FUEL CONTROL — LEAKING (NR 2 ENGINE) · airframe 61,176 hrs · 13,710 cycles

ON ENG START NR 2 ENGINE ACCELERATED TO HIGH IDLE 75 PERCENT N2. REMOVED AND REPLACED NR 2 ENG FCU AND THE TT2 SENSOR UNIT IAW 73-21-01 AND AMM 73-21-04, OPS CK AND LEAK CHECK SATISFACTORY.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 61,141 hrs · 13,701 cycles

OUTBOARD T/E FLAPS LEFT SIDE STOPPED AT 4 DEGREES, RT SIDE STOPPED AT 10 DEG. REPLACED FLAP POS INDICATOR, OPS CHECK OK PER MM 27-58-00.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYSTEM) · airframe 61,088 hrs · 13,692 cycles

LT WING RT REAR ANTI-SKID WARNING LIGHT ILLUMINATED ON P-2 PANEL. REPLACED ANTI-SKID CONTROL UNIT AND TRANSDUCER IAW MM 32-41-00. SYSTEM CHECK GOOD.

Part: BOLT — SHEARED (BULKHEAD) · airframe 60,893 hrs · 13,653 cycles

BODY STATION 2360 - (AFT PRESSURE BULKHEAD) TWO SHEARED BOLTS AT STRINGERS 11R & 20R. REPLACED BROKEN BOLTS - DETAILED VISUAL INSPECTION AND TORQUE CHECK REMAINING BOLTS - FOUR BOLTS FOUND BOTTOMED OUT. ADDED WASHERS AND RETORQUED PER SB 747-53A2474.

Part: SUPPORT ANGLE — CRACKED (RT TE FLAP) · airframe 60,893 hrs · 13,653 cycles

RIGHT I/B MID FLAP O/B L-SUPPORT ANGLE CRACKED 5 INCHES. REPAIR CARRIED OUT IAW SRM 51-40-03.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,892 hrs · 13,653 cycles

RBG - WING TO BODY SEAL - HYDRAULIC GANG CLAMP SUPPORT BLOCK CORRODED. REMOVED AND REPLACED SEAL BLOCK SUPPORT BLOCK PER SRM 51-10-01. CORROSION REMOVED WITH SEAL BLOCK. BASIC STRUCTURE NOT CORRODED.

Part: PANEL — CRACKED (TE FLAP) · airframe 60,893 hrs · 13,653 cycles

RIGHT O/B MID FLAP, I/B LOWER AREA HAS A 12 INCH CRACK IN LOWER PANEL. FIBERGLASS REPAIR CARRIED OUT ON LOWER AREA OF MID FLAP AS PER SRM 51-40-09.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,893 hrs · 13,653 cycles

LBG - WING TO BODY FLAP TORQUE TUBE - LOWER GANG SEAL - SUPPORT BLOCK CORRODED - LEVEL ONE. REPLACED SUPPORT BLOCK PER SRM 51-10-01.

Part: THRUST REVERSER — DEPLOYED (NR 2 ENGINE) · airframe 60,786 hrs · 13,631 cycles

NR 2 ENG THRUST REVERSER DEPLOYED ON T/O ROLL AT 80 KTS. NR 2 ENG T/R DEACTIVATED PER DDPG 78-1 AND MM 78-31-00. ACCOMPLISHED HIGH ENERGY STOP HEAT DAMAGE CONDITIONAL INSP PER MM 5-51-10.

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 60,619 hrs · 13,597 cycles

ON MX PREFLIGHT, ON NR 3 ENG INSIDE REVERSER AREA FOUND DELAMINATION. PERFORMED REPAIR WITHIN 10 CYC - COI 921-150 ISSUED.

Part: HOSE — CHAFED (NR 1 ENGINE) · airframe 60,480 hrs · 13,567 cycles

ON MECHANIC PREFLIGHT FOUND HYD FLUID LEAKING FROM NR 1 ENG. REPAIRED PRESSURE LINE IAW 20-11-05 PERFORMED LEAK CHECK IAW 29-11-00.

Part: VALVE — MALFUNCTIONED (NR 3 PYLON) · airframe 60,153 hrs · 13,495 cycles

NR 3 ENG PYLON VLV WOULD NOT OPEN. REMOVED AND REPLACED PYLON VLV IAW 36-11-00, LEAK CHECK OK.

Part: CONNECTOR — DIRTY (T/E FLAP) · airframe 60,153 hrs · 13,495 cycles

FLAP POS INDICATOR. CLEANED FLAP POS CONNECTOR, OPS CHECK FLAPS PER MM 27-51-00. CHECK OK.

Part: INU — MALFUNCTIONED (NR 2) · airframe 59,957 hrs · 13,452 cycles

NR 2 INU HAD RED WARNING LIGHT CODE 02-50-42 (NR 3 WAS ALREADY DEFERRED). RE-RACKED NR 2 INU, PERFORMED REALIGNMENT & RESET FAULT CODES AS PER WC M3400-002.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,670 hrs · 17,749 cycles

BODY GEAR W/W STA 1394 - STA 1416 1 INCH CRACK INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1.

Part: ACCESS PANEL — CRACKED (NR 3 PYLON) · airframe 72,670 hrs · 17,749 cycles

NR 3 PYLON STRUT ACCESS PANEL 453FL CUTOUT CRACKED. REPAIRED PER SRM 54-34-03 FIG 2.3.

Part: SKIN — CRACKED (LT WING) · airframe 72,670 hrs · 17,749 cycles

LEFT WING NR 2 STRUT 11B, SKIN CRACKED. FUEL EMERGENCY DRAIN REPAIRED PER SRM 54-34-03 FIG 23.

Part: ACCESS PANEL — CRACKED (NR 3 PYLON) · airframe 72,670 hrs · 17,749 cycles

NR 3 PYLON ACCESS PANEL CUTOUT LWR AFT CORNER CRACKED. REPAIRED PER SRM 54-34-03 FIG 23.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,670 hrs · 17,749 cycles

BODY GEAR W/W STA 1438 1460 1 INCH CRACK AT INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1.

Part: WEB — CRACKED (TE FLAP) · airframe 72,670 hrs · 17,749 cycles

RIGHT WING INBOARD MID FLAP INBOARD WEB CRACKED. SPRING ROD CUT OUT, REPAIRED PER SRM 51-40-02 FIG 01.

Part: TUBE — RUPTURED (NR 4 ENGINE) · airframe 59,142 hrs · 13,270 cycles

NR 4 ENG 13TH STAGE TURBINE CASE COOLING DUCT RUPTURED AND BLEW THRU LT REVERSER HALF. REPLACED 13TH STAGE COOLING DUCT & LT REVERSER HALF.

Part: SKIN — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

CRACK ON BS 360 RIGHT B/T STR 8 TO 10. DAMAGED AREA TRIMMED OUT, REINFORCED WITH SEGMENT AND SPLICE PER SRM 53-10-01 FIG 10 & 51-10-02 & 51-30-02.

Part: SKIN — CORRODED (RT WING) · airframe 58,800 hrs · 13,199 cycles

RT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9.

Part: SKIN — CORRODED (RT WING) · airframe 58,800 hrs · 13,199 cycles

RIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLER PER SRM 57-30-03 FIG -9.

Part: SKIN — CORRODED (RT WING) · airframe 5,880 hrs · 13,199 cycles

RIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLERS PER SRM 57-30-03 FIG -9.

Part: SKIN — CORRODED (RT WING) · airframe 5,880 hrs · 13,199 cycles

RIGHT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WAS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON SEAT TRACK STA 1817/LBL 98 WL 208. DAMAGE AREA TRIMMED OUT. REINFORCED WITH NEW SEAT TRACK PER SRM 53-10-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

STA 2320 / LBL 20 WL 208 CORROSION ON FLOORBEAM UPPER TEE. CORRODED AREA TRIMMED OUT, REINFORCED AREA PER SRM 53-11-25.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

STA 1817 / LBL 98 / WL 208 CRACK ON SEAT TRACK. DAMAGED AREA TRIMMED OUT, REINFORCED WITH NEW SEAT TRACK PER SRM 53-10-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LEVEL 1 CORROSION ON FLOORBEAM AND SEAT TRACK STA 1760-1880 LBLM & RBLM WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LEVEL 1 CORROSION FOUND ON FLOORBEAM STA 2320/LBL 20/WL 208. CORRODED AREA TRIMMED OUT. REINFORCED AREA PER SRM 53-11-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LEVEL 1 CORROSION FOUND ON UPPER LOBE MAIN DECK SEAT TRACK LBL 11 BWTN STA 1940-1960. CORRODED PORTION SEAT TRACK REMOVED. REINFORCED WITH NEW SEAT TRACK PER SRM 53-11-25 FIG.7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

UPPER LOBE MAIN DECK, CORROSION ON SEAT TRACK LBL 11 BETWEEN STA 1940-1960. CORRODED PORTION SEAT TRACK REMOVED, REINFORCED WITH NEW SEAT TRACK PER SRM 53-11-25 FIG -7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LEVEL 1 CORROSION FOUND ON FLOORBEAM STA 1800 LBL/RBL-5/WL 208. ACCOMPLISHED WORK PER SRM 51-40-03 FIG 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

STA 1760-1880 LBL & RBL 11 WL 208 CORROSION ON SEAT TRACK AND FLOORBEAM. DAMAGED AREA TRIMMED OUT, REINFORCED PER SRM 51-30-02 & 53-10-05 FIG 1 A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

STA 1800 LBL / RBL -5 / WL 2008 CORROSION ON THE FLOORBEAM UPPER CHORD. ACCOMPLISHED WORK PER SRM 51-40-03 FIG -3.

Part: DUCT — DELAMINATED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK AND DELAMINATION FOUND ON NR 1 ENG LT -C- DUCT LWR VERTICAL WEB. REPAIRED DUCT AS PER SRM 54-05-009 FIG 5.

Part: CLIP — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND UPPER DECK WALL ON CLIP 500 & 520 RT SIDE. STRAINER 8, 9, 10, 10A, 11 & 12. FABRICATED NEW CLIP PER SRM 57-40-03, 51-30-02 & 51-10-01.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 5,880 hrs · 13,199 cycles

NR 1 ENG LT C-DUCT LWR VERTICAL WEB CRACKED AND DELAMINATED. REPAIRED DUCT AS PER SRM 54-05-009.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON F/S 360 RH BWTN STR 8 TO STR 10. DAMAGE AREA TRIMMED OUT REINFORCED WITH SEGMENT AND SPLICE PER SRM 53-10-04, 51-10-02 & 51-30-02.

Part: PANEL — CRACKED (CABIN)

UPPER DECK SIDE WALL CRACKS ON CLIPS 500-520 RT SIDE STRINGER 8, 9, 10, 10A, 11A & 12. FABRICATED NEW CLIPS PER SRM 51-40-03, 51-10-02, 51-30-02, 51-11-01.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

UPPER LOBE DECK CRACK ON F/S RIGHT BETWEEN STR 8 TO STR 10A. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH SEGMENT, SPLICE AND STRAP PER SRM 53-10-04 FIG -10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON INTERCOSTAL BTWN LBL 25-LBL 45 AND SHEARED RIVETS ON FWD CARGO SEAT TRACK. DAMAGED INTERCOSTAL REMOVED NEW FABRICATED H/F 2024 T3 0050 THK PER SAMPLE PER SRM 59-10-21. PROTECTED AREA PER SRM 51-10-02 RIVETED PER SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

FWD CGR SHEARED RIVETS ON SEAT TRACK AND CRACK ON INTERCOSTAL BETWEEN LBL 25-LBL45. DAMAGED INTERCOSTAL REMOVED, NEW FABRICATED H/F 2024 T30.050 THK PER SAMPLE PER SRM 53-10-21. PROTECTED AREA PER SRM 51-10-02. RIVETED PER SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND UPPER LOBE DECK ON BETWEEN STR 8 TO STR 10A RT. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH SEGMENT, SPLICE AND STRAP PER SRM 53-10-04 FIG 10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON UPPER LOBE DECK F/S 520 RT BETWEEN STR 7 TO STR 10A. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH SEGMENT, SPLICED & STRAPPED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

FWD CGR SHEARED RIVETS ON SEAT TRACK & CRACK ON INTERCOSTAL BETWEEN LBL 25-LBL 45. DAMAGED INTERCOSTAL REMOVED NEW FABRICATED H/ 2024 T30.050 THK PER SAMPLER SRM 53-10-21. PROTECTED AREA PER SRM 51-10-02, RIVETED PER SRM 51-30-02.

Part: PANEL — CRACKED (CABIN) · airframe 5,880 hrs · 13,199 cycles

UPPER DECK SIDE WALL PANEL CRACK ON CLIP AT FRAME STA 500, STR 10, 10A, 11A, 12. NEW CLIP FABRICATED SRM 53-10-20 & SRM 51-40-03 FIG 4. PROTECTED PER SRM 51-10-02, RIVETS PER SRM 51-30-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

UPPER LOBE DECK CRACK ON F/S 520 RT BETWEEN STR 7 TO 10A. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH SEGMENT AND SPLICE STRAP.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK ON SEAT TRACK RH-25 STA 910. DAMAGED PORTION FLOOR TRACK REMOVED. NEW PORTION FABRICATION H/F 78-71511 EXTRU.BAC 1580-1658 PER SRM 58-11-25 FIG. 7R ANGLE PER SRM 51-40-02 (7075 T6 TM560). RIVETED PER SRM 51-30-02.

Part: INTERCOSTAL — TORN (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

LWR LOBE AFT CARGO SEVERAL TEARS, CORROSION & DISTORTION ON INTERCOSTAL BETWEEN STA 1900-1920 & RBL 58-LBL 58. DAMAGED INTERCOSTAL REMOVED, NEW SECTION FABRICATED & SRM 53-11-25, PROTECTED AREA PER SRM 51-10-02, RIVETED PER SRM 51-30-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LEVEL 1 CORROSION, DISTORTION AND SEVERAL TEARS FOUND LOWER LOBE AFT CARGO BTWN STATION STA 1800-1900, RH 58 LBL 58. DAMAGE INTERCOSTAL REMOVED AND FABRICATED HF 2024T3.0050 THK PER SAMPLE & SRM 53-11-25. PROTECTED AREA PER SRM 51-10-02. RIVETED PER SRM 51-3-02.

Part: PANEL — DELAMINATED (ELEVATOR) · airframe 5,880 hrs · 13,199 cycles

ELEV NR 334JB HONEYCOMB PANEL HAS A HOLE AND DELAMINATION. REPAIRED BY BONDING FIBERGLASS PLIES USING VACUUM BAG PER SRM 51-40-09.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

CRACK ON SEAT TRACK RBL-25 STA 910. DAMAGED PORTION FLOOR TRACK REMOVED, NEW PORTION FABRICATED H/F 7178-76511 EXTRU BAC 1520-1682 PER SRM 53-11-25 SRM 51-40-02 (7075T6 TMSGO) RIVETED PER SRM 51-30-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND FWD PRESSURE BULKHEAD OF F/S 140, 12:20 O'CLOCK. DAMAGED AREA TRIMMED OUT. REINFORCED AREA W/ STRAP & DOUBLER PER SRM 54-40-03, FIG. 2.

Part: PANEL — DELAMINATED (ELEVATOR) · airframe 58,800 hrs · 13,199 cycles

DELAMINATION AND A HOLE FOUND LT ELEVATOR 334JB HONEYCOMB PANEL. REPAIRED BY BONDING FIBERGLASS PLIES PER SRM 51-40-09.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

LOWER LOBE AFT CARGO DISTORTION ON FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900 - 1920. DAMAGE PORTION FLOOR TRACK REMOVED. NEW PORTION FABRICATED H/F 7178-T65H EXTRU BAC 1580-1688 PER SRM 53-11-25, FIG 7. ANGLE 7075-T6 THS 60-1350 PER SRM 51-40-02. RIVETED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (ELEVATOR) · airframe 5,880 hrs · 13,199 cycles

ELE LEFT NR 334 ML HONEYCOMB PANEL INBOARD SURFACE HAS DELAMINATION. REPAIRED BY BONDING FIBERGLASS PLIES USING VACCUM BAG PER SRM 51-40-09.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

FWD PRESSURE BULKHEAD FOUND CRACK ON F/S 1HR 12:30 O'CLOCK. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH STRAP & DOUBLER PER SRM 51-40-03 FIG-2.

Part: PANEL — DELAMINATED (ELEVATOR) · airframe 58,800 hrs · 13,199 cycles

DELAMINATION FOUND LT ELEVATOR 334ML HONEYCOMB PANEL, INBOARD SURFACE. REPAIRED BY BONDING FIBERGLASS PLIES PER SRM 51-40-09.

Part: FLOOR SUPPORT — DISTORTED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

LWR-LOBE AFT CRG DISTORTION ON THE FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900-1920. DAMAGED PORTION FLOOR TRACK REMOVED, NEW SECTION INSTALLED PER SRM 53-40-02 & PER SRM 51-30-02.

Part: PANEL — CRACKED (CABIN) · airframe 5,880 hrs · 13,199 cycles

UPPER DECK SIDE WALL CRACK ON THE CLIPS AT FRAME STA 500/L AT CONNECTION TO STR 10, 10A, 11A, 12. CRACKED CLIPS REMOVED AND NEW FABRICATED 7075 TG 0.050 THK PER SRM 53-10-20 & SRM 51-40-03 FIG -4. PROTECTED PER SRM 51-10-02 AND INSTALLED RIVETS PER SRM 51-30-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACKS FOUND ON 2 BRACKETS AT FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1800-1920, "LOWER LOBE AFT CARGO". CRACKED BRACKETS REMOVED. NEW FABRICATED HF 7075T651 PER SRM 53-11-25 & PER SAMPLE. PROTECTED W/ ANODIZE PER SRM 51-10-02. FASTENER INSTL PER SRM 51-30-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON BRACKET AT FLOOR TRACK SUPPORT RBL-25 BETWEEN STA 1900-1920, "LOWER LOBE AFT CARGO." CRACKED BRACKET REMOVED. NEW FABRICATED HF 7075T651 PER SRM 53-11-25 & PER SAMPLE. PROTECTED W/ ANODIZE PER SRM 51-10-02. FASTENER INSTL PER SRM 51-30-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 5,880 hrs · 13,199 cycles

LWR LOBE AFT CRG CRACK ON BRACKET AT FLOOR TRACK SUPPORT RBL-25 BETWEEN STA 1900-1920. CRACKED BRACKET REMOVED, NEW BRACKET FABRICATED PER SRM 53-11-25, ANODIZE PER SRM 51-10-02, FASTENERS INSTALLED PER SRM 51-30-02.

Part: CLIP — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACK FOUND ON CLIP AT FRAME STA 500/R AT CONNECTION TO STR 10-10A-11A-12. UPPER DECK SIDEWALL PANEL. NEW CLIP FABRICATED PER SRM 53-10-20 & SRM 51-40-03, FIG. 4. PROTECTED PER SRM 51-10-02, RIVETS PER SRM 51-30-02.

Part: CLIP — CRACKED (FUSELAGE) · airframe 58,800 hrs · 13,199 cycles

CRACKS FOUND ON THE CLIP AT FRAME STA 500/L, UPPER DECK SIDEWALL, AT CONNECTION TO STR 10-10A-11A-12. CRACKED CLIPS REMOVED & NEW ONES FABRICATED HF 7075T6 0.050 THK PER SRM 53-10-20 & SRM 51-40-03, FIG. 4. PROTECTED PER SRM 51-10-02 & INSTALL RIVETS PER SRM 51-30-02.

Part: BRACKET — CRACKED (FLOOR SUPPORT) · airframe 5,880 hrs · 13,199 cycles

LWR-LOBE AFT CRG CRACKS ON TWO BRACKETS AT THE FLOOR TRACK SUPPORT LBL-25 BETWEEN STA 1900-1920. CRACKED 2 BRACKETS REMOVED, NEW BRACKETS FABRICATED PER SRM 53-11-25 & PER SAMPLE PROTECTED WITH ANODIZE PER SRM 51-10-02, FASTENERS INSTALLED PER SRM 51-30-02.

Part: SEAL — CRACKED (KRUGER FLAP) · airframe 66,004 hrs · 17,647 cycles

CRACK FOUND WHILE CHECKING FLAP TO PYLON SEAL ON BACK SIDE OF NR 16 KRUEGER FLAP, RT WING, APPROX 4 INCHES INBOARD OF OUTBOARD SEAL. CRACK RUNS FROM LWR EDGE UP 12 INCHES. NR 16 KRUEGER FLAP PANEL REMOVED AND REPLACED IAW MM 27-81-01.

Part: PANEL — DAMAGED (SPOILER) · airframe 58,377 hrs · 13,103 cycles

ON POST-FLT INSPECTION, NR 9 SPOILER PANEL WAS FOUND TO BE DAMAGED (POSSIBLE DELAMINATION). REMOVED & REPLACED NR 9 SPOILER PANEL IAW AMM 27-61-00. OPERATIONAL CHECK SATISFACTORY.

Part: DOOR — CRACKED (CABIN) · airframe 57,640 hrs · 12,954 cycles

CRACK 7/8" LONG FOUND AT #5 RH CABIN DOOR, STATION 2231, BELOW STRINGER 25R. CRACK STOP DRILLED IAW SRM 51-10-01 & REPAIR CARRIED OUT IAW SRM 53-10-04, FIG 4.

Part: INU — FAILED (COCKPIT) · airframe 57,523 hrs · 12,929 cycles

DOUBLE INS FAILURE WHILE EN ROUTE. NR 3 INS HAD WARNING LIGHT, ACTION CODE 02, MALFUNCTION CODE 56 - BECAME 35 MILES OFF TRACK (CODES CLEARED) NR 3 INS HAD RED WARNING LIGHT, ACTION CODE 01, MALFUNCTION CODES 13, 31, 34, 35, 36, 42, 50 & 62. F/O'S ADI RED FLAG. INS TURNED OFF. REMOVED & REPLACED BOTH NR 3 & 2 INS NAV UNITS. OPS CHECK ON BOTH UNITS NORMAL PER MM 34-41-03.

Part: SWITCH — FAULTY (NR 3 ENGINE) · airframe 56,725 hrs · 12,758 cycles

OIL FILTER BYPASS LIGHT ON NR 3 ENGINE ILLUMINATED DURING CRUISE ON AIRWAY A450 EN ROUTE FROM GUM TO HNL AT 1715Z. NR 3 ENGINE SHUT DOWN IAW ABNORMAL PROCEDURE 6-15-10. LANDING WAS UNEVENTFUL. INSPECTION DETERMINED INTERNAL FAILURE IN PRESSURE SWITCH AS CAUSE. REMOVED AND REPLACED OIL PRESS BYPASS SWITCH, REPLACED OIL FILTER AND INSPECTED MAG PLUGS. OPS CHECKED GOOD IAW MM 71-00-00.

Part: TAILPIPE — CRACKED (NR 1 ENGINE) · airframe 56,668 hrs · 12,747 cycles

FOUND NR 1 ENGINE TAIL PIPE INNER SLEEVE, CRACK APPROX 1 INCH LONG AT 6 O'CLOCK POSITION AND APPROX 18 INCHES FROM FWD CONE L/E. CRACK IS 6.5 INCH LONG FOUND ON OUTER SKIN OF EXHAUST CONE INNER BARREL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,499 hrs · 12,712 cycles

DURING A-CHECK FOUND MAIN CEILING EMERGENCY LIGHT INOP STATION 500. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-07. OPS CHECKED SATISFACTORY.

Part: LIGHT — FALSE INDICATION · airframe 79,259 hrs · 18,598 cycles

#4 REVERSER LIGHT CAME ON DURING TAKE OFF ROLL. RETURNED TO RAMP. AMBER IN-TRANSIT LIGHT FLASHES. VERIFIED #4 ENG. T/R CORRECTLY LOCKED OUT AS PER MM 78-30-01 PROCEDURES AS PER CREW REQUEST. ALL FOUND O.K.

Part: FLANGE — CRACKED (NR 2 ENGINE) · airframe 52,980 hrs · 11,966 cycles

NR 2 ENG R FLANGE CRACK AT 05:00 & 06:00 O''CLOCK POSITIONS. NR 2 ENG COOLING TURBINE CRACKED AT 10:00 O''CLOCK POSITION. REPAIRED PER EM 72-53-01 REP 24.

Part: FLANGE — CRACKED (NR 4 ENGINE) · airframe 52,980 hrs · 11,966 cycles

NR 4 ENG R FLANGE CRACK AT 7 O''CLOCK POSITION ON LIGHTENING HOLE. NR 2 ENG TURBINE COOLING CRACKED AT 10 O''CLOCK POSITON. REPAIRED PER MM 72-09-71, REP 8.

Part: SUPPORT BRACKET — CRACKED (NR 3 ENGINE) · airframe 52,980 hrs · 11,966 cycles

NR 3 ENG TURBINE CASE WALL COOLING DUCT SUPPORT BRACKET AT 2:30 & 7 O'CLOCK POS CRACK NR 4 ENG RT L DUCT LOWER DOOR LATCH PANEL HINGE LOOSE. REPLACED PER EM 72-09-71, REP 8, MM 72-50-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,933 hrs · 11,957 cycles

LEVEL 1 CORROSION AT EXT SKIN LOWER LOBE SURFACE CORRODED BS 2360 S-40R AND BS 2380 S-516. LEVEL 1 CORROSION REPAIRED PER SRM 51-10-22.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,933 hrs · 11,957 cycles

LEVEL 1 CORROSION AT ACCESS DOOR 315AL FWD AND AFT EDGE SURFACE. LEVEL 1 CORROSION REPAIRED PER SRM 51-10-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,933 hrs · 11,957 cycles

LEVEL 1 CORROSION EXT SKIN LOWER LOBE SURFACE CORRODED AT BS 2488 S-51R AND BS 2638 S-49L. LEVEL 1 CORROSION REPAIRED PER SRM 51-10-02.

Part: TIRE — FAILED (LT MLG)

ON LANDING, NR 6 MAIN WHEEL ASSY BLEW CAUSING MINOR DAMAGE TO LEFT BODY GEAR INNER DOOR. BOTH NR 5 AND NR 6 MAIN WHEELS CHANGED, AS WELL AS NR 7 WHEEL WHICH HAD FLAT SPOT. MINOR REPAIR WAS CARRIED OUT ON LEFT BODY GEAR INNER DOOR PER SRM. LEFT BODY GEAR STRUT FOUND LOW. LEFT BODY GEAR SERVICED PER MM.

Part: DOOR — DAMAGED (LT MLG)

ON LANDING, NR 6 MAIN WHEEL ASSY BLEW CAUSING MINOR DAMAGE TO LEFT BODY GEAR INNER DOOR. BOTH NR 5 AND NR 6 MAIN WHEELS CHANGED, AS WELL AS NR 7 WHEEL WHICH HAD FLAT SPOT. MINOR REPAIR WAS CARRIED OUT ON LEFT BODY GEAR INNER DOOR PER SRM. LEFT BODY GEAR STRUT FOUND LOW. LEFT BODY GEAR SERVICED PER MM.

Part: CLIP — CRACKED (BS 320, 280, 340)

FOUND CRACKS ON VERTICAL BEAM CLIPS NOSE WHEEL WELL STRUCTURE LEFT SIDE AT BS 320, 280, 340. REPAIRED CLIPS PER SRM 51-30-02.

Part: HINGE — CORRODED (CARGO DOOR)

LEVEL 1 CORROSION FOUND AFT CARGO DOOR HINGE. AREA CLEANED PER SRM 51-10-01 AND TREATED.

Part: SKIN — DAMAGED (RT TE MIDFLAP)

RIGHT HAND OUTBOARD MID FLAP UPPER SURFACE INBOARD HAS DAMAGE. FIBERGLASS REPAIR PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (FUSELAGE)

FUSELAGE LOWER SIDE LEFT SIDE AIR CONDITIONING FAIRING PANEL NR 192 HAS DELAMINATION. FIBERGLASS REPAIR PER SRM 51-40-09.

Part: SKIN — DAMAGED (RT TE FLAP)

RIGHT WING RIGHT HAND AFT FLAP UPPER SURFACE O/B SIDE IS BROKEN. FIBERGLASS REPAIR IAW SRM 51-40-09.

Part: CLIP — CRACKED (BS 300-340)

FOUND CRACKS ON VERTICAL BEAM CLIPS NOSE WHEEL WELL STRUCTURE RIGHT SIDE STA 300-340. CLIPS REPAIRED IAW SRM 51-10-02.

Part: FAIRING — BROKEN (RT WING/BODY)

RIGHT WING AFT WING TO BODY FAIRING NEAR INBOARD FLAP IS BROKEN. FIBERGLASS REPAIR IAW SRM 51-10-09.

Part: HINGE — CORRODED (CARGO DOOR)

LEVEL 1 CORROSION FOUND ON FWD CARGO DOOR HINGES. AREA CLEANED AND TREATED IAW SRM 51-10-01 AND 51-10-02.

Part: PANEL — DELAMINATED (LT WING)

LEFT WING LOWER SURFACE TRAILING EDGE PANEL BELOW NR 3 SPOILER HAS DELAMINATION. FIBERGLASS REPAIR IAW SRM 51-40-09.

Part: SKIN — BROKEN (NR 8 SPOILER)

RIGHT WING NR 8 SPOILER LEADING HAS BROKEN PIECE. FIBERGLASS REPAIR IAW SRM 51-40-09.

Part: FRAME — CRACKED (BS 440)

FOUND CRACK AT UPPER CHORD FRAME STA 440 RIGHT SIDE BETWEEN STR 13 AND 14. FABRICATED CHORD IAW SRM 53-10-20 FIG 31 AND INSTALLED PER SRM 51-30-02.

Part: SKIN — DENTED (LT HORIZ STAB)

LEFT HAND HORIZONTAL STABILIZER LEADING EDGE IS DENTED IN 2 PLACES. DENTED AREAS REPAIRED IAW SRM 51-40-01.

Part: SKIN — DAMAGED (NR 5 SPOILER)

FOUND LEFT WING NR 5 SPOILER UPPER SURFACE DAMAGED. BONDED NEW SKIN AND DOUBLER PER SRM 51-40-06.

Part: SKIN — DELAMINATED (LT TE FLAP)

LEFT INBOARD LOWER FLAP LOWER SURFACE FOUND DELAMINATED. FIBERGLASS REPAIR IAW SRM 51-40-09.

Part: VALVE — MALFUNCTION (NR 2 BRAKE SYST)

DURING TAXI, CAPT FOUND RIGHT SIDE BRAKES INOP WITH EITHER BRAKE SYSTEM 4 OR 1 SELECTED. ALL HYD PRESS IND NORMAL (3,000 LBS). PROBLEM REMAINS WITH ANTI-SKID ON OR OFF. SELECTED BRAKE SYS TO RES BRAKES (SYS 2) FULL BRAKES CAME ON WITHOUT TOUCHING BRAKE PEDALS. REMOVED RT NORMAL SYSTEM BRAKE METERING VALVE. INSTALLED IN RT RESERVE. BRAKE METERING VALVE IN THE NORMAL POSITION. NORMAL SYSTEM OPS CHECK NORMAL PER MM 32-41-03. REMOVED RES BRAKE VALVE AND INSTALLED NEW VALVE, OPS SYSTEM CHECK NORMAL. NO LEAKS IAW MM 32-41-14.

Part: PACK — MALFUNCTIONED (NR 2)

NR 2 PACK UNCONTROLLABLE IN AUTO AND MANUAL MODE. DUE TO INOP NR 3 PACK ON DMI, HAD TO RETURN TO HKG. INTERCHANGE NR 2 AND NR 3 PACK CONTROLLERS BYPASS VALVE AND TEMP SENSOR AND NR 3 PACK OPS NORMAL.

Part: FIRE WARNING — ACTIVATED (CARGO COMPT)

ON TAKEOFF ROLL, MAIN DECK CARGO FIRE WARNING 1 ILLUMINATED WITH BELL. ABORTED TAKEOFF AND EMERGENCY CHECKLIST CARRIED OUT IAW AOM VOL 1. ON TAXI IN, THE SAME WARNING CONTINUALLY CAME ON WITH NO SMOKE. NOTE: ACFT LOADED WITH LIVE CATTLE. FOUND 1A DETECTOR CAUSING SPURIOUS WARNING. DEACTIVATED AND TRANSFERED TO DMI PER MEL 26-11.

Part: PANEL — CRACKED (RT WING)

TOP OF RT WING L/E PANEL I/B OF NR 3 ENG PYLON SURFACE CRACKED JUST BESIDE PREVIOUS REPAIR. REMOVED DAMAGED AREA AND REPAIRED AREA IAW SRM 51-40-12.

Part: COWL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE O/B T/R COWL T/E INSIDE SKIN CRCKED AT LOWER TRAILING EDGE. REMOVED AND REPLACED WEB IAC SRM 51-10-01 AND 51-30-02.

Part: COWL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE I/B T/R COWL T/F INSIDE SKIN CRACKED LOWER TRAILING EDGE. REMOVED AND REPLACED WEB IAW SRM 51-10-01 AND 51-30-02.

Part: FITTING — CRACKED (LT WING)

LEFT WING FLYING PANEL CRACKED FWD LEFT ATTACH FITTING. REMOVED AND REPLACED LT FLYING PANEL IAW SRM 51-10-01, RIG CHECKED GOOD IAW MM 57-20-01.

Part: COWL — LOOSE (NR 3 ENGINE)

NR 3 NOSE COWL SEVERAL RIVETS LOOSE AND NOT SEATED PROPERLY IN PREVIOUS REPAIR FWD RING AT 5 O'CLOCK POSITION. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, REPAIRED NOSE COWL IAW SRM 54-31-03 ROHR SRM.

Part: FAIRING — DAMAGED (LT TE FLAP)

LEFT WING O/B FLAP I/B FWD FAIRING HAS SEVERAL HOLES IN NOSE SECTION. POTTED HOLES, FABRICATED FIBERGLASS OVERLAYS AND BONDED THEM TO REPAIR AREA IAW SRM 51-40-15.

Part: RAIL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE R-RAIL CRACK FOUND AT 6 O'CLOCK POSITION. WELDED AND STRESS RELIEVED IAW PW MM 72-53-01.

Part: PANEL — DAMAGED (RT WING)

PANEL ON RT WING FWD OF FLYING HAS HOLE CENTER AFT. REPAIRED DAMAGE BY APPLYING FIBERGLASS FILLERS AND DOUBLERS AND COATING IAW SRM 51-40-15.

Part: COWL — DAMAGED (NR 3 ENG)

#3 NOSE COWL RING INNER SURFACE DAMAGED AT 11 OCLOCK POSITION. REPAIRED DAMAGED AREA IAW SRM 54-10-01.

Part: R RAIL — CRACKED (NR 3 ENGINE)

#3 ENGINE R RAIL CRACKED LEFT SIDE AT 7 OCLOCK POSITION. WELDED, STRESS RELIEVED IAW PW MM 72-53-01.

Part: PANEL — CRACKED (RT WING)

TOP OF R/H WING L/E PANEL JUST I/B OF #4 ENG PREVIOUS REPAIR FOUND CRCKED. SANDED OFF PREVIOUS REPAIR CUT SKIN BACK TO A 6X6 INCH CUTOUT, CLEANED AREA APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: ACTUATOR — FAILED (LT MLG)

LEFT BODY GEAR DID NOT RETRACT. RED GEAR LIGHT AND RED DOOR LIGHT IN UP, NO GEAR GREEN LIGHT. GEAR HANDLE OFF, BODY GEAR THEN SHOWED DOWN AND LOCKED WITH DOOR OPEN. REMOVED AND REPLACED LT BODY GEAR LOCK ACTUATOR, PERFORMED EXTENSION AND RETRACTION OF BODY GEAR PER MM 32-33-15.

Part: SKIN — DENTED (BS 680)

FUSELAGE DENTED AFT OF FORWARD CARGO DOOR STATION 680. FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-03.

Part: STRUCTURE — DAMAGED (CARGO DOORWAY)

A/C EXPERIENCED GROUND DAMAGE AT FWD EDGE AFT CARGO DOOR CUTOUT. DAMAGE EXTENDED INTO SKIN, INTERNAL BEAR STRAP, STA 1800 AND STA 1810 FRAME AND STRINGER 31R AND 32R. REPAIRED IAW POLAR AIR CARGO MA 5310-26:02.

Part: OIL TANK CAP — MISSING (NR 4 ENGINE)

FOUND NR 4 ENGINE OIL CAP MISSING. INSPECTED ENG FOR CAP. DRAINED OIL AND SERVICED. INSTALLED NEW CAP, OPS AND LEAK CHECK OK IAW MM 79-11-00.

Part: BRACE — CHAFED (NR 1 PYLON)

NR 1 PYLON O/B SIDE DIAGONAL BRACE CHAFED FWD END. EDDY CURRENT C/W PER NDT PART 6 54-40-03 WITHIN LIMITS PER SRM 54-40-01. BLEND OUT AREA SHOT PEENED AND TREATED PER SRM 54-40-01 AND 51-70-00.

Part: DOOR — CHAFED (NR 4 PYLON)

NR 4 PYLON O/B SAILBOAT DOOR CHAFED. SANDED DOWN CHAFED AREA, APPLIED POTTING COMPOUND, SANDED DOWN AND PRIMED/PAINTED PER SRM 51-70-00.

Part: DOOR — CHAFED (NR 1 PYLON)

NR 1 PYLON O/B SIDE OF SAILBOAT DOOR CHAFED FWD END. SANDED OUT CHAFED AREA, APPLIED POTTING COMPOUND, SANDED AND REPAINTED PER SRM 51-70-00.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING AIRCRAFT SERVICING, DYNAIR HIGHLIFT FELL ONTO LEFT HAND STABILIZER. REPAIRED PER POLAR MA 5510-02:01.

Part: WARNING LIGHT — ILLUMINATED (LT/RT MLG)

LEFT WING AND RIGHT WING PRIMARY AND ALTERNATE TILT LIGHTS ON. ALSO, LEFT AND RIGHT WING LANDING GEAR DOOR PRIMARY AND ALTERNATE LIGHTS ON WHEN THE GEAR HANDLE PLACED TO THE OFF POSITION. LEFT AND RIGHT WING TILT AND DOOR SENSORS CHECKED OK, GEAR RETRACTION AND EXTENSION CHECKED NORMAL PER BOEING MAINTENANCE MANUAL 32-32-00, 32-33-00 AND 32-34-00 UNABLE TO DUPLICATE FAULT.

Part: BRACE — CHAFED (NR 4 PYLON)

NR 4 ENGINE PYLON SAIL AREA DIAGONAL BRACED CHAFED FWD END LT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER 54-40-01 ZONE 3. EDDY CURRENT C/W, NO CRACKS NOTED PER NDT 54-40-08 PART 6. BLENDED OUT CHAFED AREA, SHOT PEENED AND TREATED PER SRM 54-40-01.

Part: BRACE — CHAFED (NR 1 PYLON)

NR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED 2 PLACES LT SIDE. CHAFE WITHIN LIMITS ZONE 3 PER SRM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6. BLENDED OVER CHAFE AREA SHOT PEENED AND TREATED PER SRM 54-40-01.

Part: BRACE — CHAFED (NR 1 PYLON)

NR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED FWD RT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER ZONE 3 SRM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6, NO CRACKS FOUND. BLENDED OUT CHAFED AREA AND TREATED AREA PER SRM 54-40-01.

Part: VANE CONTROL — FAILED (NR 4 ENGINE)

NR 4 ENGINE HAD COMPRESSOR STALL AFTER THROTTLES RETARDED AT TOP OF DESCENT. EGT INCREASED TO 490 DEGREES. INFLIGHT SHUT DOWN ACCOMPLISHED. INFLIGHT START ATTEMPTED, LIGHT OFF EGT INCREASING, LOW N2, LOW FUEL FLOW AND EGT INCREASING TO 480 DEGREES. SHUT DOWN ENGINE. REPLACED FUEL CONTROL UNIT PER BOEING MAINTENANCE MANUAL 73-21-01. AFTER FUEL CONTROL CHANGE, REPLACED ENGINE VANE CONTROL PER BOEING M/M 75-31-02. ENGINE VANE CONTROL CONFIRMED AS CAUSE OF STALL.

Part: BRACE — CHAFED (NR 1 PYLON)

CHAFING DAMAGE ON NR 1 PYLON DIAGONAL BRACE FORWARD END LOWER SIDE CAUSED BY HYD DOOR FORWARD LATCH CLEARANCE. REPAIRED PER SRM 51-10-01.

Part: LINE — CHAFED (PYLON)

EDP PRESSURE LINE CHAFFING INTO INBOARD SIDE LINK ASSY ON FORWARD SIDE BY CLAMP BLOCK. REPLACED LINE REF SB 54-2158A PYLON MOD.

Part: COWL — PUNCTURED (NR 4 ENGINE)

PUNCTURE/SLIGHT HEAT DAMAGE TO NR 4 (RT) OUTBD FAN COWL. REPAIRED PER SRM 51-04-40-06.

Part: COWL — CRACKED (NR 2 ENGINE)

DELAMINATED HOLD OPEN ROD ON FWD LWR PANEL OF NR 2 ENG LT FAN COWL. REPAIRED IAW ROHR LETTER MEM 97-0866. HOT BOND IAW SRM 51-40-06.

Part: COWL — DELAMINATED (NR 3 ENGINE)

DELAMINATED INNER LOWER COVER OF RT FAN REVERSER COWL ON NR 3 ENGINE. INJECTED AND BONDED IAW SRM 54-31-03 FIGURE 1.

Part: COWL — DELAMINATED (NR 2 ENGINE)

DELAMINATED NR 2 ENG LT FAN COWL FWD LOWER PANEL ABOVE HOLD OPEN ROD. REPAIRED PER SRM 51-40-06 AND ROHR MEM 97-0866.

Part: COWL — DELAMINATED (NR 3 ENGINE)

DELAMINATED NR 3 ENG RT FAN REVERSER COWL INNER LOWER COVER. INJECTED CORE PER 54-31-08 FIG 1.

Part: SUPPORT — CORRODED (BS 2340)

LEVEL 1 CORROSION ON FLOOR SUPPORT FRAME AT STATION 2340, RBL 20 TO RBL 40. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1660)

LEVEL 1 CORROSION ON FAIRING SUPPORT FRAME AT STATION 1660, LBL 50 TO RBL 82. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 2300)

LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT ANGLE AT STATION 2300, RBL 63. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: FILLET — CRACKED (BS 1416)

CRACK ON FILLET AT STATION 1416, LBL 11. REPLACED FILLET PER BOEING SERVICE BULLETIN 53-2227.

Part: SUPPORT — CORRODED (BS 1000)

LEVEL 1 CORROSION ON FAIRING SUPPORT RIB AT STATION 1000, RBL 60. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1540)

LEVEL 1 CORROSION ON FAIRING SUPPORT FRAME AT STATION 1540, LBL 42 TO RBL 46. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1485)

LEVEL 1 CORROSION RIGHT WING LOWER SKIN AT WING STATION 1485 FRONT SPAR AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 57-10-01.

Part: SUPPORT — CORRODED (BS 1550-1620)

LEVEL 1 CORROSION AND TEAR ON FAIRING SUPPORT FRAME BETWEEN STATIONS 1550 AND 1620, BL 0. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01, REPAIRED DAMAGE PER SRM 53-50-02.

Part: DOOR — DELAMINATED (RT MLG)

DELAMINATED RIGHT WING GEAR INBOARD STRUT DOOR. REPAIRED DELAMINATION PER BOEING SRM 51-40-06.

Part: INTERCOSTAL — CORRODED (BS 1770)

LEVEL 1 CORROSION ON FRAME INTERCOSTAL AT STATION 1770, RBL 45. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1114)

LEVEL 1 CORROSION ON FAIRING SUPPORT RIB AT STATION 1114, LBL 64. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 2300-2320)

LEVEL 1 CORROSION ON HOUSING SUPPORT OF DRAIN MAST BETWEEN STATIONS 2300 AND 2320, RBL'S 46 TO 49. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1280)

LEVEL 1 CORROSION ON RIGHT WING LOWER SKIN AT FRONT SPAR, WING STATION 1280. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: INTERCOSTAL — CORRODED (BS 1915)

LEVEL 1 CORROSION ON FRAME INTERCOSTAL AT STATION 1915, LBL 1 TO LBL 20. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1580)

LEVEL 1 CORROSION ON FAIRING SUPPORT FRAME AT STATION 1580, LBL 58 TO RBL 50. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1280)

LEVEL 1 CORROSION ON RIGHT WING REAR SPAR LOWER SKIN BETWEEN WING STATIONS 1280 AND 1364. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1370)

LEVEL 1 CORROSION ON RIGHT WING LOWER SKIN AT FRONT SPAR, WING STATIONS 1370 TO 1454. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 880)

LEVEL 1 CORROSION ON FAIRING SUPPORT FRAME AT STA 880 BETWEEN LBL 40 AND RBL 40. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 1150)

LEVEL 1 CORROSION TO RIGHT WING LOWER SKIN AT REAR SPAR, BETWEEN WING STATIONS 1150 AND 1200. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1620)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STATION 1620, RBL 0 TO 40. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 1924)

LEVEL 1 CORROSION ON FLOOR SUPPORT ANGLE AT STATION 1924, LBL 35. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: PANEL — DELAMINATED (NR 4 SPOILER)

DELAMINATION ON NR 4 SPOILER PANEL. REPAIRED DELAMINATION PER BOEING SRM 51-40-06.

Part: FLAP TRACK — CORRODED (NR 4 TE FLAP)

LEVEL 1 CORROSION ON LEFT WING NR 4 FLAP TRACK BEARING PLATE. REMOVED CORROSION AND TREATED PER BOEING OVERHAUL MANUAL 57-52-70.

Part: SKIN — CORRODED (BS 1180)

LEVEL 1 CORROSION ON FUSELAGE SKIN AT STATION 1180, RBL 96. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1906)

LEVEL 1 CORROSION ON FLOOR SUPPORT AT STATION 1906, RBL 40. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 2280-2320)

LEVEL 1 CORROSION ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 2280 AND 2320, L AND RBL 13. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-24.

Part: SUPPORT — CORRODED (BS 1174)

LEVEL 1 CORROSION ON FAIRING SUPPORT RIB AT STATION 1174, RBL 50. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 2280)

LEVEL 1 CORROSION ON FLOOR SUPPORT FRAME AT STATION 2280, LBL 41. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 2340)

LEVEL 1 CORROSION ON FLOOR SUPPORT AT STATION 2340, LBL 28 TO LBL 50. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 1980)

LEVEL 1 CORROSION ON FLOOR SUPPORT ANGLE AT STATION 1980, RBL 53. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — DAMAGED (LT TE FOREFLAP)

DAMAGE TO LEFT WING INBOARD FOREFLAP TRAILING EDGE OUTBOARD, CORNER SPLIT. REPAIRED DAMAGE PER BOEING SRM 51-40-09.

Part: FITTING — CRACKED (RT TE FOREFLAP)

CRACKED OUTBOARD FITTING ON RIGHT OUTBOARD TRAILING EDGE FOREFLAP. FABRICATED AND INSTALLED FITTING PER BOEING SRM 51-30-02.

Part: FLOOR BEAM — CORRODED (BS 2320)

LEVEL 1 CORROSION ON FLOORBEAM AT STATION 2320, RBL 23. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: FLOOR BEAM — CORRODED (BS 228)

LEVEL 1 CORROSION ON FLOORBEAM UPPER SURFACE AT STATION 228, LBL 50. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 2360)

LEVEL 1 CORROSION ON FLOOR SUPPORT AT STATION 2360, LBL 17. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (WS 550)

LEVEL 1 CORROSION TO RIGHT WING LOWER SKIN AT FRONT SPAR, BETWEEN WING STATIONS 550 AND 560. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 2300)

LEVEL 1 CORROSION ON FLOOR SUPPORT AT STATION 2300, RBL 34. REMOVED CORROSION AND TREATED PER BOEING 51-10-01.

Part: SUPPORT — CORRODED (BS 1350-1360)

LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT BETWEEN STATIONS 1350 AND 1360, LBL 10. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: THRESHOLD — CORRODED (CARGO DOOR)

LEVEL 1 CORROSION ON BULK CARGO DOOR THRESHOLD, STATION 1980. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: BRACKET — CORRODED (BS 2300)

LEVEL 1 CORROSION ON BRACKET UNDER FLOOR SUPPORT AT STATION 2300, RBL 12. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — DELAMINATED (NR 6 SPOILER)

DELAMINATION ON NR 6 SPOILER TRAILING EDGE. REPAIRED DELAMINATION PER BOEING SRM 51-40-06.

Part: SKIN — CORRODED (BS 1694)

LEVEL 1 CORROSION ON LEFT FUSELAGE EXTERIOR SKIN AT STATION 1694, STRINGER L36. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: ANGLE — CORRODED (BS 2280)

LEVEL 1 CORROSION ON FLOOR SUPPORT ANGLE AT STATION 2280, RBL 3. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: PANEL — DENTED (NR 4 SPOILER)

DENT ON NR 4 SPOILER PANEL. REPAIRED DENT PER BOEING SRM 51-40-09.

Part: FLAP TRACK — CORRODED (NR 4 TE FLAP)

LEVEL 1 CORROSION ON LEFT WING NR 4 FLAP TRACK UPPER SURFACE AT BEARING PLATE AREA. REMOVED CORROSION AND TREATED PER BOEING OVERHAUL MANUAL 57-52-70.

Part: FLOORBEAM — CORRODED (BS 2340)

LEVEL 1 CORROSION ON FLOORBEAM FRAME AT STATION 2340, LBL 14 TO LBL 40. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 1180)

LEVEL 1 CORROSION ON LOWER FUSELAGE SKIN AT STA 1180, RBL 96. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 860)

LEVEL 1 CORROSION ON LOWER FUSELAGE REINFORCEMENT SUPPORT AT STA 860 AND LBL 39. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: INTERCOSTAL — CORRODED (BS 920-1000)

LEVEL 1 CORROSION ON FAIRING SUPPORT INTERCOSTAL BETWEEN STA 920 AND 1000, LBL 4. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1000)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STA 1000, LBL 60. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 820)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STA 820, RBL 0. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1174)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STA 1174, RBL 50. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: BRACKET — CORRODED (BS 840)

LEVEL 1 CORROSION ON CENTER LINE LOWER FUSELAGE SKIN BRACKET AT BS 840. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1000)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STA 1000, RBL 108. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1114)

LEVEL 1 CORROSION ON FAIRING SUPPORT AT STA 1114, LBL 64. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01.