N389FE

Part: SPRING — MISSING (SENSOR) · airframe 85,339 hrs · 36,575 cycles

UNSAFE GEAR INDICATION ILLUMINATED DURING DESCENT FOR THE RIGHT MAIN GEAR, UNSAFE INDICATION ON BOTH THE GEAR PANEL AND SYNOPTIC. COMPLIED WITH QRH, INDICATION WENT AWAY AFTER SLOWING BELOW 230KTS. NORMAL EXTENSION DURING APPROACH AND LANDING . PSEU TEST PASSED, PSEU FAULT HISTORY DISPLAYED A SENSOR FAULT FOR RIGHT GEAR UP AND LATCHED A & B SENSOR DISSAGREE. INSTALLED MISSING SPRINGS IAW AMM 32-60-7560, CYCLED MAIN LANDING GEAR, VERIFIED ALL GEAR INDICATIONS TO BE NORMAL IAW AMM 32-61-02. ALL SENSORS AND TARGETS READ WITHIN LIMITS IAW AMM 32-61-15-5, ACFT OK FOR SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED (LE) · airframe 84,800 hrs · 36,286 cycles

ON SLECTION OF FLAPS 35 FOR LANDING, A LEVEL 2 ALERT FOR SLAT DISAGREE CAME ON. DUE TO PROXIMINTY TO AIRPORT, A GO AROUND WAS INITIATED AND THEN THE ALERT WENT AWAY. F/O ALSO SUSPECTS FLAP/SLAT HANDLE DID NOT FULLY SETTLE IN DETENT. PERFORMED GVI OF THE FLAPS/SLATS IAW MM 27-50-00, NO DEFECTS NOTED AT THIS TIME. PERFORMED RTS OF THE FLAPS IAW MM 22-00-00-5, AND NO FAULTS NOTED AT THIS TIME

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,438 hrs · 36,052 cycles

DURING EMERGENCY LIGHT TEST, HAD A LEVEL ONE EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LOOP — WORN (NR 2) · airframe 84,407 hrs · 36,030 cycles

LEVEL 3 AIR MANIFOLD NR 2 FAILED DURING CLIMBOUT. TROUBLESHOT THE NR 2 LOOP MANIFOLD IAW FIM 36-23-00-2, AND SSM 36-23-00. CHECKED RESISTANCE ON D1-17 AND FOUND GOOD. LOOP IS DISCONNECTED BETWEEN LOOP D1-17 AND LOOP D1-13 FOR TROUBLESHOOTING. FOUND D1-38 FORWARD LOOP TO BE OUT OF LIMITS. REMOVED AND REPLACED THE LOOP D1-38 AMM 36-23-02-4.

Part: FUEL CONTROL — FAILED (NR 1 ENGINE) · airframe 83,967 hrs · 35,761 cycles

AFTER SHUTTING DOWN THE NR 1 ENGINE FOR A FUNCTIONAL CHECK. FUEL FLOW EGT AND N2 PROGRESSED NORMAL DURING START, BUT THE N1 WOULD NOT ADVANCE PAST 28%. ADVANCING THROTTLE DID NOT CHANGE ANY NR 1 ENGINE PARAMETERS UNTIL REACHING 10,000 FT, AT WHICH TIME THE THROTTLE ADVANCE CAUSED N1 TO ACCERLATE AND RESPOND NORMALLY. FL230 SPEED 230 KNOTS N1=28, EGT-400, N2-56.4, FUEL FLOW 530. REMOVED AND REPLACED THE NR 1 ENGINE MEC IAW AMM 73-20-01-2, ADJUSTED IAW AMM 71-00-00-5, RAN ENGINE IAW JRH 5-7, LEAK AND OPS CHECKED GOOD IAW JRH 7-7.

Part: SEAT TRACK — WORN (BS 1089-1169) · airframe 83,964 hrs · 35,759 cycles

MAIN DECK LBL 9 SEAT TRACK DAMAGED FROM BS 1089 TO 1169. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — WORN (BS 1089-1169) · airframe 83,964 hrs · 35,759 cycles

MAIN DECK SEAT TRACK DAMAGED BS 1089 TO 1169, LBL 9. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 83,964 hrs · 35,759 cycles

LEFT WING NR 10 SLAT TRACK CUT OUT AFT INBOARD DOOR CORNER HAS A .200 INCH CRACK. REPAIRED THE SKIN IAW SRM 57-10-00 FIG 68 SHEET 2/3 VOL 1

Part: ACCESS DOOR — CRACKED (LT WING) · airframe 83,964 hrs · 35,759 cycles

LEFT WING SLAT ACTUATOR ACCESS DOOR, FWD INBOARD CONER HAS A .100 INCH CRACK. REPAIRED IAW SRM 57-10-00, VOL I, FIG 104, SHEET 2. MAJOR REPAIR.

Part: SKIN — CRACKED (LT WING) · airframe 83,964 hrs · 35,759 cycles

LEFT WING NR 10 SLAT TRACK CUTOUT AFT INBD DOOR CORNER HAS A .200 INCH CRACK. REPAIRED IAW SRM 57-10-00, VOL I, FIG 68, SHEET 2 & 3.

Part: HINGE — CRACKED (BS 1448) · airframe 83,964 hrs · 35,759 cycles

LEFT MAIN GEAR DOOR CENTER HINGE IS CRACKED. REMOVED AND REPLACED THE HINGE ASSY IAW SRM 51-31-01, VOL 2, & DRAWING ANB7093.

Part: STRUCTURE — CORRODED (BS 1273) · airframe 83,964 hrs · 35,759 cycles

UPPER MAIN DECK, BS 1273 AND LBL TO RBL OF CENTER WING TOP BOX SHOWS NUMEROUS CORRODED SPOTS. REPAIRED IAW EA. 8-5730-T0331280.

Part: FITTING — CRACKED (BS 1443) · airframe 83,964 hrs · 35,759 cycles

LEFT MAIN GEAR DOOR FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-31-05, VOL 2, AND DRAWING ANB7134.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 83,964 hrs · 35,759 cycles

LEFT MAIN GEAR DOOR INNER SKIN IS CRACKED. REMOVED AND REPLACED THE SKIN IAW SRM 52-00-01, FIG 9, SHEET 1, VOL 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,964 hrs · 35,759 cycles

MAIN CARGO DECK, STA 1962 RT O/B FLOOR TRACK CORRODED. REPAIRED TRACK PER SRM 53-70-00 FIG 18.

Part: SEAT TRACK — WORN (BS 1135) · airframe 83,964 hrs · 35,759 cycles

MAIN DECK, BS 1135, LBL 9 SEAT TRACK DAMAGED. R & R THE SEAT TRACK SPLICE IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (BS 1140) · airframe 83,964 hrs · 35,759 cycles

MAIN DECK BS 1140 9LBL SEAT TRACK DAMAGED. R & R SEAT TRACK SPLICE IAW SRM 53-70-00, FIG 1.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 83,964 hrs · 35,759 cycles

RIGHT WING, ACCESS PANEL 641LB IS DELAMINATED. REPAIRED THE ACCESS PANEL IAW SRM 51-71-00, VOLUME 2, PAGE 39, PARAGRAPH 3, AND DRAWING ARC0357.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 83,964 hrs · 35,759 cycles

MAIN CABIN, SEAT TRACK AT STA 630 IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1A VOL1.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 83,964 hrs · 35,759 cycles

UPPER RT HORIZ STAB, SHOW HAILS / TOOL MARK APPROX 1" X 1" X .25" 5121819. CUT OUT DAMAGE AND INSTALLED A DOUBLER AND FILLER IAW SRM 55-00-01 VOL I FIG 3 SHEET 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 83,964 hrs · 35,759 cycles

MAIN DECK, SEAT TRACK AT STA 637, RBL 9 IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1A VOL1.

Part: ACCESS DOOR — CRACKED (LT WING) · airframe 83,964 hrs · 35,759 cycles

LEFT WING SLAT ACTUATOR ACCESS DOOR FWD INBOARD CORNER HAS A .100 INCH CRACK. REPAIRED IAW SRM 57-10-00 VOL1 FIG 104 SHEET 2.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 83,964 hrs · 35,759 cycles

LEFT MLG DOOR INBD INTERIOR LANDING IS CRACKED NEAR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED THE LANDING IAW SRM 52-00-01, FIG 9, SHEET 1, VOL 1, PG.42.

Part: SHAFT — SHEARED (RT HORIZ STAB) · airframe 82,454 hrs · 35,010 cycles

RIGHT SIDE HORIZONTAL STABILIZER, CONSTANT BEARING INSPECTION REVEALED, OTBD SIDE LOAD STRUT NUT & LUBE WASHER ARE LOOSE & OUT OF POSITION. R & R THE SHAFT, SLEEVE & LUBE WASHER.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 82,446 hrs · 35,006 cycles

ON PREFLIGHT, FIRST OFFICERS OXYGEN MASK FAILED MIC TEST. R & R MASK STOWAGE BOX IAW MM 35-13-04-4, OPERATIONS NORMAL.

Part: SWITCH — INOPERATIVE (R1 DOOR) · airframe 820 hrs · 34,805 cycles

R1 DOOR SLIDE REMOTE PRESS INDICATOR TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. DEFERRED R1 SLIDE INDICATOR LIGHT C 7023854. R & R SWITCH IAW AMM 25-61-03-2. OPERATIONS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (LANDING GEAR) · airframe 815 hrs · 34,487 cycles

RT LANDING GEAR RED LIGHT ILLUMINATED AT FL330. DESCENDED TO FL270 & SLOWED TO 230 KTS IAW QRH. LIGHT REMAINED ON UNTIL PASSING FL20.5, GOOD INDICATIONS ON LANDING LIGHTS, 3 GREEN. FAULTED 317074 INTERMITTENT RT GEAR UP & LATCHED, AB SENSOR DISAGREE, FOUND RT MAIN GEAR UPLOCK SENSOR TARGET OUT OF ADJUSTMENT. ADJUSTED WITHIN LIMITS USING MM 32-61-15-4. PSEU RTS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (PUSH TO TEST) · airframe 812 hrs · 34,300 cycles

DURING PREFLIGHT CREW INFORMED MX L1 DOOR EMER SLIDE PUSH TO TEST DOOR LIGHT INOPERATIVE. REPLACED L1 REMOTE SLIDE PRESSURE INDICATOR AND BATTERY PACK ASSY.

Part: AILERON — CORRODED (RT WING) · airframe 81,065 hrs · 34,214 cycles

POPPED FASTENERS & SIGN OF CORROSION 24 INCHES OTBD OF THE INBD EDGE OF THE OTBD AILERON ON THE RT WING. REMOVED CORROSION & INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85.

Part: PANEL — DELAMINATED (NACELLE) · airframe 81,065 hrs · 34,214 cycles

PANEL 364 DR RT PICKLE BARREL HAS MINOR DAMAGE. REPAIRED PANEL 364 DR RT PANEL IAW SRM 51-71-00 VOL II.

Part: ANGLE — CRACKED (RT WING) · airframe 81,065 hrs · 34,214 cycles

RIGHT WING LE SLAT DRIVE ACCESS DOOR OTBD LANDING IS CRACKED AT PREVIOUS REPAIR DOUBLER. R & R ANGLE ARB1286-14 IAW DWG ARB1286 & SRM 51-31-01 VOL II.

Part: SKIN — CRACKED (RT WING) · airframe 81,065 hrs · 34,214 cycles

RIGHT WING LE PANEL LAND CRACKED BEHIND SLAT NR 3 NEXT TO SLAT TRACK NR 8. R & R LAND STRAP IAW DWG ARB1180 & SRM 51-31-01 VOL II.

Part: SKIN — CRACKED (RT WING) · airframe 81,065 hrs · 34,214 cycles

RIGHT WING, LE PANEL LAND CRACKED BEHIND SLAT NR 4 NEXT TO SLAT TRACK NR 9. REMOVED CRACKED LAND RT WING LE PANEL AS REQUIRED. INSTALLED NEW LAND RT WING LE PANEL IAW DWG ARB1180 & SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,065 hrs · 34,214 cycles

MAIN CABIN RT APPROX STATION 1219 RBL 80 FLOOR SUPPORT CORRODED. FABRICATED & INSTALLED FLOOR SUPPORT AEA0394-504 RT APPROX STATION 1129, RBL 80 IAW DWG NEA6018 & SRM 51-31-01 VOL II.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,065 hrs · 34,214 cycles

MAIN DECK STATION 1384 & 1389 LT 75.50 SEAT TRACK DAMAGED. WORK WITH NR 209. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,065 hrs · 34,214 cycles

MAIN DECK SEAT TRACK STATION 1250 LT 75.50 DAMAGED. REPAIRED IAW SRM 53-70-00 FIG 2 SHEET 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,065 hrs · 34,214 cycles

MAIN DECK STATION 1385 & 1395 RT 75.50 SEAT TRACK DAMAGED. REPAIRED DAMAGED SEAT TRACK AREA IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,065 hrs · 34,214 cycles

MAIN CABIN STATION 1270 SEAT TRACK DAMAGED AT LBL 75. REPAIRED IAW SRM 53 FIG 2 SHEET 1.

Part: LINK — FAULTY (LT MLG DOOR) · airframe 80,713 hrs · 34,022 cycles

LEFT MAIN GEAR SHOWED UNSAFE RED LIGHT AFTER TAKEOFF FOR BOTH PRIMARY & SECONDARY INDICATIONS. LG WAS CYCLED AT ALTITUDE IAW THE QRH WITH NO IMPROVEMENT. FOUND LT MAIN GEAR DOOR UP LATCH LINK NOT RETURNING TO LATCH POSITION. R & R LT MLG DOOR LINK, LINK BOLT & BUSHING IAW MM 32-34-03-2 & PERFORMED ADJUSTMENTS & MEASUREMENTS IAW MM 32-34-03-2. COMPLETED UP TO 3B STEP 28 TEST DOOR LATCH MECHANISM AS FOLLOWS. COMPLIED WITH MAIN GEAR DOOR LATCH MECHANISM TEST STEP 28 THRU COMPLETION IAW MM CHAP 32-34-03-2. NO FURTHER FAULTS NOTED.

Part: PIVOT — LACK OF LUBE (LT MLG) · airframe 80,641 hrs · 33,977 cycles

WHEN GEAR WAS RETRACTED AFTER TAKEOFF BOTH THE RED LT LIGHT ABOVE THE GEAR HANDLE & THE LIGHT ON THE CONFIG PAGE SHOWED AN INDICATION THAT THE LT MAIN GEAR WAS NOT EXTRACTED. HOWEVER THERE WAS NO DRAG OR ADVERSE HANDLING CHARACTERISTICS. SPEED WAS KEPT BELOW 230K & TWO MORE EXTENSIONS & RETRACTIONS WERE MADE WITH THE SAME RESULT. HOWEVER AFTER APPROX 5 MINS WHILE WE WERE RUNNING CHECKLISTS & PREPARING TO RETURN, THE LIGHT WENT OUT. TROUBLE SHOT & INSPECTED LT MLG HOOK ASSEMBLY FOR CRACKS, GOUGES & LOOSE HARDWARE, ALL WAS GOOD, HOWEVER FOUND MLG OR TARGET PIVOT ARM VERY STIFF. LUBED PIVOT & CHECKED TARGETS FOR SECURITY & ALL WAS GOOD. PROCEEDED TO DO MLG PROXIMITY SENSOR & TARGET ADJUSTMENT TEST, CHECKED BOTH LGUPLCHA & LGUPLCHB INDUCTANCE & BOTH WERE READING ABOVE 5.16 MHZ WITH GEAR UP. PROCEEDED TO CONDUCT A FULL GEAR SWING THROUGH 4 FULL UP & DOWN SWINGS, ALL INDICATIONS WERE GOOD IN BOTH THE UP & DOWN INDICATIONS. ACFT OK FOR SERVICE. IAW FIM 32--30-02, AMM 32-61-15-5 & AMM 12-21-01-3-2.

Part: LANDING GEAR — LACK OF LUBE (LEFT) · airframe 80,637 hrs · 33,976 cycles

LEFT MAIN GEAR WOULD NOT GIVE A SAFE UP INDICATION ON EITHER THE PRIMARY OR SECONDARY INDICATORS. COMPLIED WITH QRH WITH SAME RESULT. LUBRICATED LT & RT MLG IAW AMM 12-21-01-3-2. JACKED ACFT IAW AMM 07-11-00-2. PERFORMED EXTENSION & RETRACTION OF GEAR FOR 3 CYCLES NO FAULT FOUND IAW AMM 32-30-00-5 PAR 3. ACFT RESTORED TO NORMAL CONDITION & OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 80,698 hrs · 34,011 cycles

RIGHT WING NR 3 SLAT ANTI-ICE TELESCOPING DUCT CUT OUT IS CRACKED AT UPPER INBD & OTBD CORNERS. REPAIRED IAW EA 8-5710-T0308270.

Part: SKIN — CRACKED (LT WING) · airframe 80,698 hrs · 34,011 cycles

LEFT WING FIXED LE SKIN CRACKED AT THE PRESS REFUELING DOORWAY PANEL 518FB INBD FWD. REPAIRED IAW SRM 57-10-00 & EA 8-5710-T0308261 SEQ 231.

Part: SKIN — CRACKED (LT WING) · airframe 80,698 hrs · 34,011 cycles

LEFT WING FIXED LE SKIN CRACKED AT THE TAI DUCT CUT OUT TOP OTBD CORNER. REPAIRED IAW EA 8-5710-T0308271 PART 1.

Part: PUMP — FAILED (NR 2 ENGINE FUEL) · airframe 79,378 hrs · 33,289 cycles

NR 2 ENGINE FUEL FILTER ALERTED AT 80 KTS DURING TAKEOFF ROLL. ALERT OCCURED AT 98 PERCENT N1. REJECTED TAKEOFF. ALERT EXTINQUISHED AT THROTTLE REDUCTION. REMOVED FUEL FILTER AND DEBRIS SCREEN IAW 73-12-01-2. NR 2 ENGINE FUEL PUMP, MEC, AND FUEL OIL COOLER REMOVED. MATED FUEL PUMP AND MEC AS IAW MM 73-20-01-2. INSTALLED FUEL PUMP PACKAGE IAW MM 73-12-01-2.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 79,168 hrs · 33,166 cycles

2 INCH CRACK LT MLG WW INBD BULKHEAD 30 INCHES FWD OF AFT BULKHEAD AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED PER SRM 53-00-01, FIG 10, VOLUME I.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 78,648 hrs · 32,891 cycles

HORZIONTAL STAB CONSTANT SECTION RT SIDE AFT UPPER SPAR CAP FITTING, HAS A CRACK APPROX 1" IN LENGTH, JUST INBD OF ATTACH BOLT. R & R SECTION OF UPPER SPAR CAP REF EA 8-5510-163913.

Part: REGULATOR — INOPERATIVE (NR 2 ENGINE) · airframe 77,834 hrs · 32,454 cycles

FLIGHT LEVEL 340, LEVEL 3 AIR MANIFOLD 2 FAIL. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE PRESSURE REGULATOR VALVE, REF AMM 36-12-01-4.

Part: LOOP — MALFUNCTIONED (MANIFOLD) · airframe 77,769 hrs · 32,421 cycles

ON CLIMB OUT AT 14,000 FT HAD NR 2 MANIFOLD FAIL LEVEL 3 ALERT. INTERROGATED THE MCDU SYS AIU 1, AIU 2, PSC 1, PSC 2, AND MSC. ALSO REVIEWED CURRENT FAULTS. FOUND A FAV FAULT (CODE 361031). THE AIR SYNOPTIC PAGE SHOWS SYS NR 2 IN RED AND THE MANF LIGHT ON THE ASCP IS ILLUMINATED. MEM R AFTER FURTHER REVIEW, FOUND SYS NR 2 MANIFOLD FAIL IN AIU 1, 2, 3. R & R NR 2 MANIFOLD LOOPS D1-27A & D1-27B IAW MM 36-23-02-4. AFTER LOOP'S R & R. 'AIR SYS 2 FAIL' STILL DSPLAYED, AIR MANF TEST FAIL & AIU 1 CURRENT FAULTS SHOWED: NO LOOP 1A/1B INPUT RECEIVED DURING PREFLT TEST-P, NO LOOP 2 INPUT RECEIVED DURING PREFLT TEST-P NO LOOP 3 INPUT RECEIVED DURING PREFLT TEST-P. RECONNECTED MANIFOLD FAIL TEST BOX & VERIFIED MANIFOLD FAIL DETECT SYS ALL OK. R & R AIU 1. R-T-S OK. AIR SYS TEST NORMAL. NO ALERTS DISPLAYED. REF MM 31-43-02-4-0.

Part: CONTROLLER — MALFUNCTIONED (HYD SYSTEM) · airframe 77,125 hrs · 32,063 cycles

DURING CRUISE FL350, RECEIVED A MASTER CAUTION LEVEL 1 ALERT FOR HYD PUMPS. ALL 3 LEFT EDPS WERE IN THE OFF POSITION (NO PRESSURE AUTO MODE ). SELECTED HYD CONTROL SYS FROM AUTO MODE TO MANUALLY MODE AND ALL 3 LT PUMPS TURNED ON AND PRODUCED PRESSURE. SHUT ENGINES DOWN. ENGINE RUN WAS ACCOMPLISHED AGAIN. LOOKING FOR PRESSURE DECREASE AND INCREASE WITH 2-3 REVERSABLE MOTOR PUMP OFF. ALL LEFT PUMPS SELECTED OFF, AND RIGHT REMAINED ON, PRESSURE DROPPED AGAIN. 3 LEFT PUMPS SELECTED ON AND PRESSURE INCREASED. REMOVED AND REPLACED THE HSC PER MM 29-08-01. RAN ENG PER JRH. ENG DRIVEN PUMPS OPERATE NML LEFT ON, AND RT PUMPS IN ARMED POSITON. OPS NORMAL.

Part: MOTOR — LEAKING (STAB TRIM) · airframe 76,876 hrs · 31,918 cycles

"ON CLIMBOUT THROUGH APPROX FL180 RECEIVED LEVEL 1 ALERT "HYD 3 ELEV OFF". HYD SYNOPTIC SHOWED APPROX 3 GALS AND DECREASING. SOON AFTER RECEIVED LEVEL 2 ALERT "HYD 3 FAIL" AND QTY DECREASED TO 0.2 GAL. RAN "HYD SYS 3 FAIL" QRH PROCEDURE WITH AND EVENTUAL ALTERNATE GEAR EXTENSION. (DKM)". RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. HORIZONTAL STAB TRIM MOTOR 1 HSG FOUND TO BE CRACKED. REPLACED NR 1 STAB TRIM MOTOR UPTO 3.B.8 OPS AND LEAK CHECKS REQUIRED, REF MM 27-43-01-2. MEM R COMPLETED REPLACEMENT OF NR 1 STAB TRIM MOTOR, LEAK AND OPS CHECK GOOD, REF MM 27-43-01-2. NR 3 HYD SYS FILTERS CHANGED ON WRI 29-10/1262.

Part: UNKNOWN — INOPERATIVE (EMERGENCY POWER) · airframe 76,444 hrs · 31,698 cycles

EMERGENCY POWER TEST WILL NOT PASS. CYCLED FUEL LEVERS AND RAN EMERGENCY POWER TEST IN REF TO AMM 24-30-00-5-0. ALL CHECKS GOOD. RAN TEST SERVERAL TIMES PASSED EACH TIME.

Part: TERMINAL — BROKEN (R1 DOOR SLIDE) · airframe 76,092 hrs · 31,517 cycles

R1 DOOR SLIDE REMOTE PUSH TO TEST LIGHT/INDICATOR IS INTERMITTENTLY INOP. RELEASED FOR SERVICE IAW MEL: 25-61-01 CATEGORY: C EXPIRATION: 15DEC10 MEL 25-61-01:RT EVAC SLIDE REMOTE PRESS INDICATOR INOP IAW MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY." VERIFIED RT SLIDE PRESSURE TO BE WITH IN LIMITS IAW MEL MX PROCEDURE. FOUND RING TERMINAL BROKEN THAT ATTACHES TO "C" BATTERY HOLDER ASSY. RING TERMINAL ATTACHED WITH SOME TYPE OF RIVET ATTACHMENT TO THE BATTERY HOLDER. REQUIRES PART THAT HAS ALREADY BEEN ADDED. R & R REMOTE SLIDE PRESSURE INDICATOR IN REF TO AMM CH 25-61-03-2-0, PERFORMED ADJ/TEST IN REF TO AMM CH 25-61-03-5-0, OPS CHECKS GOOD.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 76,084 hrs · 31,510 cycles

(P2-38) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN AT STA 1411, X = 27 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. REMOVED, FABBED AND REPLACED SPLICE IAW SRM 53-70-00, FIG 1, VOL I.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 76,084 hrs · 31,510 cycles

(P2-45) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN FROM STA 1661 TO STA 1681, X = 47 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. REMOVED, FABBED AND REPLACED SPLICE AT STA 1661 - 1681, X = 47 IAW SRM 53-70-00, FIG 1, VOL I.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 76,084 hrs · 31,510 cycles

FWD PIT EXISTING "J " CHANNEL REPAIR AT STA 824 BETWEEN LONGERON 51L AND LONGERON 51R REQUIRES EVALUATION. VISUALLY INSPECTED REPAIR - FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR IAW SRM 53-30-00, FIG 5, VOL I. THIS IS A CLASS "B" REPAIR WITH A VISUAL INSPECTION DUE AT 43,510 CYCLES.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 76,084 hrs · 31,510 cycles

(P2-39) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN FROM STA 1371 TO STA 1411, X = 8.5 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. R & R SEAT TRACK SPLICES AT STA 1371 AND 1411, X = 8.5 IAW SRM 53-70- 00, FIG 1, VOL I.

Part: HINGE FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,084 hrs · 31,510 cycles

RT WING OTBD FLAP OTBD HINGE FITTING, LOCATION NR 3 FWD MOUNTING SURFACE CORRODED. ACCOMPLISHED REPAIR OF THE NR 3 MOUNT SURFACE OF THE OUTBD FLAP OUTBD HINGE FITTING IAW EA 8-5750-123566.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 76,084 hrs · 31,510 cycles

RT WING NR5 SPOILER UPPER SURFACE OTBD FWD REPAIR AND FOUND IT DELAMINATED. REMOVED EXISTING REPAIR AND INSTALLED A METAL BOND REPAIR, SEALED ALODINED PRIMED AND PAINTED IAW SRM 57-10-00, VOL I AND SRM 51-71-00, VOL II.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 76,084 hrs · 31,510 cycles

(P2-65) EXISTING MAIN CABIN SEAT TRACK SPLICE FROM STA 1321 TO 1351; LBL 107 IS REQUIRED TO BE CHECKED FOR CONDITION. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA DATA. REMOVED AND REPLACED IAW SRM 53-70-00, FIG 1, VOL I.

Part: SKIN — UNKNOWN (ZONE 600) · airframe 76,084 hrs · 31,510 cycles

EXISTING FLUSH REPAIR ON THE RT, NR 1 SLAT INNER SKIN, INBD UPPER CORNER REQUIRES A "MAJOR / MINOR" DETERMINATION AND EVALUATION TO ENSURE THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD DOUBLER IAW SRM 51-31-01, VOL II. FABRICATED NEW DOUBLER IAW SRM 57-00-01, FIG 4, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM 57-00-01, FIG 4, VOL I.

Part: SKIN — UNKNOWN (ZONE 600) · airframe 76,084 hrs · 31,510 cycles

EXISTING EXTERNAL DOUBLER REPAIR ON THE RIGHT WING L/E FWD SURFACE OF THE TIP AT STA XW 937. REPAIR REQUIRES EVALUATION FOR "MAJOR / MINOR" DETERMINATION AND TO ENSURE THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR IAW SRM 57-00-01, FIG 4, VOL I. REMOVED AND REINSTALLED POSITION LIGHT LENS FOR ACCESS IAW AMM 33-44-00-4, OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 76,084 hrs · 31,510 cycles

CTR ACCESSORY COMPARTMENT, INBD SLAT DRIVE CONTROL RETENTION MECHANISM (LT SIDE) HAS 2 SHEARED MECHANICAL FUSES.

Part: HINGE — WORN (ZONE 100) · airframe 76,084 hrs · 31,510 cycles

FWD TWO LOBES ON FUSELAGE SIDE OF THE CENTER CARGO DOOR ARE OUT OF LIMITS AT 0.346, LIMIT IS 0.343. REAMED FWD 2 LOBES TO 0.410 IAW SRM 52-10-00, FIG 8, SHEET 1, VOL I. MACHINED / FABRICATED 2 EA REPAIR BUSHINGS IAW SRM 52-10-00, FIG 8, SHEET 1, VOL I. INSTALLED 2 EA. BUSHINGS IN FWD 2 LOBES IAW SRM 52-10-00, FIG 8, SHEET 1, VOL I.

Part: LONGERON — CORRODED (BS 1021-1029) · airframe 76,084 hrs · 31,510 cycles

FORWARD CARGO COMPARTMENT BILGE LONGERON REPAIR ANGLE IS CORRODED FROM FS 1021 TO FS 1029; STRINGER 52. REMOVED CORROSION AND FOUND MATERIAL LOSS TO EXCEED ALLOWABLE LIMITS. REPAIRED LONGERON IAW SRM 53-10-00, FIG 2, VOL I.

Part: DRIVE ASSY — SHEARED (SLATS) · airframe 76,084 hrs · 31,510 cycles

CENTER ACCESSORY COMPARTMENT, INBD SLAT DRIVE CONTROL RETENTION MECHANISM (LT SIDE) HAS TWO SHEARED MECHANICAL FUSES. REMOVED AND REPLACED INBD SLAT DRIVE CONTROL MECHANISM SHEAR MECHANICAL FUSES REF CMM 27-83-09 AND AMM 27-83-08-2.

Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 76,084 hrs · 31,510 cycles

CENTER CARGO BAY FLOORBOARD 183HF DELAMINATED. FABRICATED FLOORBOARD 183 HF IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 76,084 hrs · 31,510 cycles

CENTER CARGO BAY FLOORBOARD 183PF IS DELAMINATED. FABRICATED CENTER CARGO BAY FLOORBOARD 183 PF IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 76,084 hrs · 31,510 cycles

CENTER CARGO BAY FLOORBOARD 183GF DELAMINATED. FABRICATED FLOORBOARD 183 GF IAW DWG SRZ 25-005, REV "H".

Part: STOP FITTING — SHEARED (L1 DOOR) · airframe 76,084 hrs · 31,510 cycles

L-1 DOOR; FWD SIDE; 5TH DOOR STOP UP; IS SHEARED OFF. R & R THE L-1 STOP FITTING (5TH UP FROM THE BOTTOM) IAW SRM 51-31-01, VOL I. REMOVED AND RE-INSTALLED THE L-1 DOOR SLIDE AND ADJUSTED THE L-1 DOOR STOPS IAW AMM 52-11-03-2, AMM 25-61-01 AND AMM 52-11-00-5.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 76,084 hrs · 31,510 cycles

RT OTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS AND 1 MISSING FASTENER AFT OF THE INBD FLAP HINGE FITING ALONG THE T/E. REMOVED WORKING FASTENERS IAW SRM 57-20-00, FIG 11, VOL I. FABRICATED BEARING STRAPS, APPLIED ALODINE AND PRIMER IAW SRM 51-21-01, VOL II. INSTALLED IAW SRM 57-20-00, FIG 11, PG 38, VOL I. PAINTED IAW SRM 51-21-01, VOL II. INSTALLED ONE MISSING FASTENER IAW SRM 57-20-00, FIG 11, VOL I.

Part: FITTING — MISINSTALLED (NR 1 PYLON BLKHD) · airframe 76,084 hrs · 31,510 cycles

NR 1 PYLON AFT BULKHEAD FITTING HAS 12 EA FASTENERS ALONG THE UPPER FLANGE SPINNING. ACCOMPLISHED EA 8-5450-123559.

Part: SKIN — LOOSE (RT WING TE FLAP) · airframe 76,084 hrs · 31,510 cycles

RIGHT OUTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS JUST IND OF THE NR 2 FLAP TRACK CENTER AREA. REMOVED WORKING FASTENERS IAW SRM 51-35-20, VOL II. FABRICATED 5 EA REPAIR DOUBLER STRIPS. ALODINED TREATED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED IAW SRM 57-20-00, PG 38, VOL I AND SRM 51-35-01, VOL II. PAINT TOUCH UP IAW SRM 51-21-02, VOL II. SEALED PER SRM 51-40-01, VOL II.

Part: SKIN — WORN (ZONE 600.) · airframe 76,084 hrs · 31,510 cycles

RIGHT OUTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS AFT OF THE INBD FLAP HINGE FITTING. REMOVED WORKING FASTENERS IAW SRM 57-20-00, FIG 11, VOL I. FABRICATED BEARING STRAPS, MATERIAL ID 2024-T3 0.050 IAW SRM 57-20-00, FIG 11, VOL I. APPLIED ALODINE AND PRIMER IAW SRM 51-21-01, VOL II. INSTALLED IAW SRM 57-20-00, FIG 11, PG 38, VOL I.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 76,084 hrs · 31,510 cycles

LT WING INBD LOWER FLAP LOWER SKIN IS DENTED 5" FROM THE T/E FROM WS XIFH 296 TO WS XIFH 300. REMOVED DAMAGED AREA; FABRICATED DOUBLER AND FILLER IAW SRM 57-00-01, FIG 4, SHEET 2, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. PAINTED IAW SRM 51-21-02, VOL II. INSTALLED DOUBLER AND FILLER IAW SRM 57-00-01, FIG 4, SHEET 2, VOL I.

Part: SKIN — WORN (NR 6 SLAT) · airframe 76,084 hrs · 31,510 cycles

RT WING NR 6 LEADING SLAT LOWER SURFACE HAS WORN SPOTS. REMOVED DAMAGE AND EVALUATED AREA IAW SRM 57-00-01, VOL I. AREA WAS FOUND OUT OF LIMITS. REMOVED DAMAGE IAW SRM 51-71-00, VOL II. FABRICATED AND INSTALLED REPAIR IAW SRM 57-00-01, VOL I, AND SRM 51-31-01, VOL II. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. TOP COATED IAW SRM 51-21- 00, VOL II.

Part: SPAR CAP — CRACKED (LWS 345.75) · airframe 76,084 hrs · 31,510 cycles

LT WING REAR SPAR AT STA XORS 345.750, 3 EA FASTENER HOLES ON THE OTBD SIDE HAS CRACK INDICATIONS. REPAIRED CRACKED HOLES IAW EA 8-5710-123557.

Part: PSEU — LOOSE (MLG) · airframe 73,959 hrs · 30,480 cycles

ON ARRIVING KONT AFTER EXTENDING GEAR RECEIVED 3 UNSAFE GEAR INDICATING ON PANEL AND CONFIG PAGE RECYCLED GEAR HANDLE AND RECEIVED ALL GREEN GEAR INDICATION SHGN 08 MAY 09 01:11. ON T R PER CREW DEBRIEF ALL THREE GEARS WERE DOWN WITH RED IND. T/R PER THE FIM 32-30-03 , FOUND PSEU LOOSE IN RACK, RESECURED IN RACK, PSEU TESTED PER MM 31-71-01-2. ALL TESTS GOOD, NO HISTORY FOUND, A/C OK TO CONTINUE.

Part: PANEL — DAMAGED (NR 2 ENGINE) · airframe 73,025 hrs · 30,064 cycles

NR 2 ENGINE AT THE 5:00 POSITION; LIP RING PANEL LEFT FAN COWL OPEN / CLOSE IS DELAMINATED / CRACKED & GOUGED WITH LOOSE & SHEARED FASTENERS. REMOVED; FABRICATED & REPLACED THE LOWER SKIN PANEL & ANGLE IAW SRM 51-31-01, 51-35-01, 51-24-01 & 55-31-01 & DWG AJC7415; REV BK. ANGLE MARKED IAW GMM 7-0-1000.

Part: FITTING — CRACKED (ZONE 100) · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DOOR LOWER JAMB FITTING NR 2 AT HOLE " B ' SHOWED INITIAL CRACK INDICATION. AFTER REAMING HOLE " B " TO .519 AND ACCOMPLISHMENT OF E.O. 9-5230-7-5000. NO FURTHER INDICATION EXISTS AT THIS TIME. MACHINED 2 REPAIR BUSHINGS IAW SRM 53-50-00. REPAIRED HOLE " B " AT THE NR 2 FITTING LOCATION IN REFERENCE WITH SRM 53-50-00.

Part: SUPPORT — WORN (NR 2 FAN COWL) · airframe 73,025 hrs · 30,064 cycles

THE NR 2 FAN COWL LT; LOWER MATING AREA; FOUND FWD LEFT ANGLE SUPPORT WORN TO A KNIFE EDGE. FABRICATED & REPLACED ANGLE SUPPORT IAW DWG AJC 7415, SRM 51-35-01, SRM 51-21-01 & SRM 51-31-01. REMOVED & RE-INSTALLED PARTS TO FACILITATE MAINTENANCE IAW SRM 51-31-02 & AMM 71-10-01-2 & 20-50-01. NR 2 ENGINE STARTER DUCT LEAK CHECK GOOD IAW AMM 71-00-00-4-0.

Part: FRAME — CRACKED (LT WING) · airframe 73,025 hrs · 30,064 cycles

LEFT WING FIXED L/E COMP FORMER IS CRACKED ADJACENT TO THE FRONT SPAR UPPER T-CAP AT XOS 751 APPROX MATERIAL ID FOR THE REPAIR ANGLE IS 0.063, 17-7 PF CRES ANNEALED REF DC/MD-10 SRM 57-20-00. FORMED THE REPAIR ANGLE REF DC/MD-10 SRM 51-10-00; VOL II. RECEIVED ANGLE FROM HEAT TREAT; LOCATED & DRILLED REF DC/MD-10 SRM 51-21-01; VOL II. INSTALLED REPAIR ANGLE REF DC/MD-10 SRM 57-20-00; VOL I.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,025 hrs · 30,064 cycles

STA 1501 SHEAR TIES AT LONGERONS 51R TO 51L ARE CRACKED. REMOVED DAMAGED SHEAR TIE AT FS 1501 FROM LONGERON 45R TO 45L. FABRICATED NEW ONE P/N AEA 0273-19 IAW DAC DWG AEA 0273. LOCATED & DRILLED UP NEW ONE IAW DAC DWG AEA 0273. ALODINE & PRIMED IAW SHEAR TIE IAW DC/MD-10 SRM 51-21-01; PG 21 - 24; VOL II. APPLIED TOP COAT OF PAINT IAW DC/MD-10 SRM 51-21-01 PG 8; VOL II. PART MARKED NEW PART FX AEA 0273-19 IAW FEDEX GMM 7-0-1001. RE-INSTALLED NEW SHEAR TIE IAW DC/MD-10 SRM 51-35-01 PG 1; VOL II.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

FORWARD LOWER CARGO ROLLER TRAY HAS CORROSION ON THE ATTACH ANGLE LOWER SURFACE AT FS 879, RBL 5 INCH - 8 INCH. COMPLIED WITH THE REPAIR TO THE ROLLER TRAY ATTACH ANGLE AT STA 879; RBL 8; FWD CARGO COMPARTMENT IAW DC/MD-10 SRM 53-00-01; VOL I; FIG 7.

Part: HINGE — WORN (LT WING TE FLAP) · airframe 73,025 hrs · 30,064 cycles

LEFT WING INBD FLAP OUTBD HINGE FWD HALF OUTBD FACE LOWER EDGE HAS WEAR MARKS IN 5 SPOTS JUST INBD OF THE NUTPLATES. REMOVED HINGE FAIRING IAW SRM 51-31-01. BLENDED WORN AREAS, FOUND TO REQUIRE REPAIR IAW SRM 51-44-07. BLEND AREA IS 0.065. FABRICATED REPLACEMENT CLIPS & SHIMS IAW SRM 57-20-00. ALODINED, PRIMER & PAINTED REPAIR PARTS & BLENDED AREAS IAW SRM 51-21-10. INSTALLED ANGLES IAW SRM 57-20-00. RE-INSTALLED HINGE FAIRING IAW SRM.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 2 HAS CRACK INDICATIONS AT HOLES A, C AND D. REMOVED & REPLACED FITTING IN REF TO SRM 51-33-01. REPAIRED HOLES IN UPPER BEAM IN REF TO SRM 53-50-00.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 4 HAS A CRACK INDICATION AT HOLE C.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 7 HAS CRACK INDICATIONS AT HOLES B AND D. REMOVED & REPLACED FITTING IN REF TO SRM 51-33-01. REPAIRED UPPER BEAM IN REF TO SRM 53-50-00.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 3 HAS A CRACK INDICATION AT HOLE A. REMOVED & REPLACED FITTING IN REF TO SRM 51-38-04. REPAIREDUPPER BEAM IN REF TO SRM 53-50-00.

Part: INTERCOSTAL — CRACKED (BS 910 L43R) · airframe 73,025 hrs · 30,064 cycles

FWD LOWER CARGO LONGERON 43R INTERCOSTAL AT STA 910 IS CRACKED. REPAIRED INTERCOSTAL, LONGERON 43 RT IAW SRM 53-00-01.

Part: SEAT TRACK — CORRODED (ZONE 300) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BEWTEEN STA 1800 AND STA 1860, LBL 105. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00. FABRICATED CHANNEL IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED CHANNEL REPAIR IAW SRM 53-70-00. REMOVED & REPLACED FLOOR PANEL IAW AMM 53-21-01-8.

Part: FITTING — GOUGED (BS 1997 L50L) · airframe 73,025 hrs · 30,064 cycles

FOUND WASTE COMPARTMENT BS 1997, LONGERON 50L, INBD AND OUTBD SIDES ARE GOUGED. REMOVED LONGEROON END FITTING IN REF TO SRM 51-33-01. SMOOTHED OUT THE GOUGES IN REF TO SRM 53-00-01. AREA IS OUT OF LIMITS IN REF TO SRM 53-00-01. LOCATED; DRILLED & DEBURRED NEW AJC 7236-517 LONGERON END FITTING IN REF TO SRM 51-33-01. APPLIED TOP COAT IN REF TO SRM 51-21-01. INSTALLED LONGERON END FITTING IN REF TO SRM 51-33-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BEWTEEN STA 1361 AND STA 1391, LBL 27. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-70-00. FABBED A NEW SECTION IAW SRM 53-42-01 AND SRM 53-70-00. ALODINED & PRIMED SECTION IAW SRM 51-21-01. INSTALLED NEW SECTION IAW SRM 53-70-11 & SRM 51-31-01. REMOVED & RE-INSTALLED FLOOR PANELS IAW AMM 53-21-01-08.

Part: LONGERON — CORRODED · airframe 73,025 hrs · 30,064 cycles

CENTER PIT LONGERON 50R OUTBD SIDE HAS CORROSION ON THE INNER FLANGE. REMOVED LT & RT AFT ADF PANELS IAW SRM 51-31-01. REMOVED 2 FRAME SECTIONS; 4 EA SPLICES AND 4 EA SUPPORTS IAW SRM 51-33-01 & SRM 51-35-01. REMOVED DAMAGED LONGERON FITTING 50R IAW SRM 51-35-01. LOCATED AND DRILLED NEW LONGERON FITTING & INSTALLED FITTING & SUBSTRUCTURE IAW SRM 51-35-01. INSTALLED ADF PANELS IAW SRM 51-31-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO SEAT TRACK HAS CORROSION BETWEEN STA 994 AND 1010, LBL 27. REMOVED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-70-00. LOCATED & DRILLED FOR CHANNEL IAW SRM 53-70-00. REMOVED FLOOR PANEL IAW AMM 53-21-01-8. INSTALLED CHANNEL STRAP IAW SRM 53-70-00. INSTALLED FLOOR PANEL IAW AMM 53-21-01-8.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK IS GOUGED AT STA 880; LBL 8. BLENDED GOUGES, EXCEEDS LIMITS. REMOVED FLOOR PANELS AT BS 775-969 LBL 28 & RBL 28 IAW SRM 51-31-01 VOL II. REMOVED SEAT TRACK FROM BS 860-900 LBL 8 IAW SRM 51-31-01 VOL II. FABBED SEAT TRACK IAW SRM 53-70-00 VOL I. ALODINED & PRIMED THE SEAT TRACK IAW 51-21-01 VOL II. INSTALLED SEAT TRACK IAW SRM 51-31-01 VOL II. INSTALLED FLOOR PANELS IAW SRM 51-31-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1321 AND STA 1351, LBL 107. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-70-00. FABBED NEW TRACK, 2 HAT SPLICES & 2 SPLICE PLATES IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED NEW SECTION IAW SRM 53-70-00. REMOVED & RE-INSTALED GRILL MOUNT & DECOMPRESSION PANEL IAW SRM 51-31-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN CARGO DECK SEAT TRACK HAS CORROSION BETWEEN STA 1151 AND 1173, LBL 27. REMOVED DAMAGED SECTION OF SEAT TRACK. FABRICATED A REPAIR SECTION; SPLICE & SPLICE PLATE AND INSTALLED IAW SRM 51-21-01. REMOVED & RE-INSTALLED FLOOR BOARDS INBD AND OUTBD OF LBL 27 BS 1099-1239 IAW SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 1480-1540) · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1480 AND 1540, LBL 107. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED SEAT TRACK IAW SRM 51-31-01. REPAIRED SEAT TRACK IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. REMOVED & RE-INSTALLED FLOOR PANEL IAW AMM 53-21-02-2. REMOVED & RE-INSTALLED AIR GRILLS IAW AMM 53-23-02-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 73,025 hrs · 30,064 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN BS 1330-1341, LBL 27. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG SHEETS 1&2 NOTE 5. FABBED A NEW SECTION IAW SRM 53-42-01 & SRM 53-70-00. ALODINED & PRIMED SECTION IAW SRM 51-21-01. INSTALLED NEW SEAT TRACK SECTION AT BS 1311-1371 LBL 27 IAW SRM 53-70-00 & SRM 51-31-01. REMOVED & RE-INSTALLED FLOOR PANELS IAW AMM 53-21-01-8.

Part: LONGERON — CRACKED (ZONE 100) · airframe 73,025 hrs · 30,064 cycles

CENTER WHEEL WELL LONGERON 52 IS CORRODED AT FS 1481. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED NEW SECTION OF LONGERON, LOCATED, & DRILLED IAW DWG AYB 7013. FABRICATED LONGERON SPLICES. LOCATED & DRILLED IAW SRM 53-00-01. ALODINED & PRIMED NEW SECTION OF LONGERON & SPLICES IAW SRM 51-21-01. APPLIED TOP COAT OF PAINT IAW SRM 51-21-01. PART MARKED IAW GMM 7-0-1001. INSTALLED LONGERON & SPLICES IAW SRM 53-00-01 & SRM 51-33-01.

Part: FRAME — NONE (ZONE 200) · airframe 70,984 hrs · 29,122 cycles

EXISTING FRAME REPAIR MAIN CABIN PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: SKIN — NONE (ZONE 100) · corrosion level 2 · airframe 70,984 hrs · 29,122 cycles

EXISTING REPAIR EXTERNAL FUSELAGE. PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: LONGERON — NONE (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

EXISTING LONGERON SPLICE REPAIR FWD CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUESTED BY EO 8-5100-7-5001 P2.

Part: FRAME — NONE (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

EXISTING FRAME REPAIR INTERNAL FUSELAGE CAC PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

EXISTING REPAIR EXT FUSELAGE REPLACED REPAIR PER SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

EXISTING SKIN REPAIR EXT FUSELAGE FWD JAMB AFT CARGO DOOR APPLIED SEALANT IAW SRM 51-41-01 VOL 2 AND APPLIED PRIMER IAW SRM 51-21-01 VOL 2.

Part: LONGERON — NONE (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

EXISTING 3 EA LONG SPLICE REPAIR AFT CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P.2.

Part: SEAT TRACK — WORN (BS 1199) · airframe 70,984 hrs · 29,122 cycles

MAIN CABIN DEEP WEAR ON SEAT TRACK. REPAIRED SECTION OF SEAT TRACK IAW SRM 53-70-00 PAGE 4 VOL 1.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 70,984 hrs · 29,122 cycles

DURING INSP OF HORIZ STAB CONSTANT SECTION SKIN PANEL, FOUND THREE LOWER INTERIOR SKIN PNLS WITH CRACK, P/N 7205-1, P/N 7204-1, P/N 7206-1. SEE ATTACHED SHEET FOR ALL REF (INSPECTION FINDING FORM). REPAIRED IAW EA NR 8-5510-96121.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 70,984 hrs · 29,122 cycles

FWD CARGO COMPT BILGE AREA FOUND 1 CRACK ON TEE CAP OF BLKHD. REPAIRED IAW EA NR 8-5310-96124.

Part: RIB — CRACKED (ZONE 500) · airframe 70,984 hrs · 29,122 cycles

RT WING LOWER RIB CHORD HAS 2 CRACKED LUGS CRACKS EXTEND ABOVE HORIZONTAL FLANGE OF CHORD. REPAIRED IAW SRM 57-20-00 FIG 21 SHT 1 VOL 1.

Part: BALANCE WEIGHT — CORRODED (ZONE 300) · corrosion level 2 · airframe 70,984 hrs · 29,122 cycles

RT OUTB ELEVATOR BALANCE WEIGHT WITH PAINT REMOVED AND LIGHT CORROSION. REPLACED BALANCE WEIGHT IAW CMM 55-21-01.

Part: BULKHEAD — CRACKED (ZONE 100) · corrosion level 2 · airframe 70,984 hrs · 29,122 cycles

RT MLG W/W FOUND 2 CRACKS ON VERTICAL BULKHEAD DOUBLER. TRIMMED AREA, FAB AND INSTALLED WEB, SPLICE, FILLER IAW SRM 53-00-01 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E INTERNAL ZONE FOUND 1 CRACK 0.75" LONG ON RIB. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING DURING INSPECTION WITH EO NR 8-5100-7-5001 P2 FOUND 1 CRACK 1" LONG ON UPPER SKIN OF O/B FLAP. REPAIRED SKIN IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: BULKHEAD — BROKEN (BS 1119) · airframe 70,984 hrs · 29,122 cycles

FOUND A STRUT OF BULKHEAD BROKEN. REPAIRED STRUT IAW SRM 53-00-01 FIGURE 2 SHT 2 VOL 1.

Part: SKIN — CRACKED (TE FLAP) · airframe 70,984 hrs · 29,122 cycles

RT WING T/E DURING INSPECTION WITH EO 8-5100-7-5001 P2 FOUND 1 CRACK .25" LONG ON LOWER SKIN OF OUT'B FLAP. REPAIRED SKIN IAW SRM 57-00-01 FIGURE 4 SHT 2 VOL 1.

Part: BEAM — CORRODED (BS 1099 S43L) · airframe 70,984 hrs · 29,122 cycles

FOUND CORROSION WITH EXFOLIATION ON BEAM AT STA 1099 LONGERON 43 LT. REPAIRED BEAM IAW SRM 53-60-01 FIGURE 3 VOL 1.

Part: TEE FITTING — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E FOUND 1 CRACK 1" LONG ON FIXED TEE. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1.

Part: TEE FITTING — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E FOUND 1 CRACK ON FIXED TEE 1" LONG. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1.

Part: SKIN — DAMAGED (BS 959) · airframe 70,984 hrs · 29,122 cycles

EXTERNAL FUSELAGE SKIN DAMAGED CUT OUT AFT JAMB LOWER FWD CARGO DOOR. REPAIRED SKIN IAW SRM 53-20-00 FIGURE 6 SHT 3-6 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E EXTERNAL SKIN FOUND 1 CRACK 1.5" LONG. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 2 VOL 1.

Part: BULKHEAD — CRACKED (BS 1491) · airframe 70,984 hrs · 29,122 cycles

RT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED BLKHD IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL.1.

Part: RIB — CRACKED (RWS 720) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E INT ZONE FOUND 1 CRACK 0.50" LONG, ON RIB WITH OLD REPAIR. REMOVED OLD REPAIR, AND PERFORMED NEW REPAIR IAW SRM 57-20-00 FIGURE 1 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 70,984 hrs · 29,122 cycles

LT WING L/E CRACK LONG 0.75" ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1.

Part: FRAME — CRACKED (BS 421) · airframe 70,984 hrs · 29,122 cycles

FWD AVIONIC COMPT CRACK 6" LONG ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIGURE 5 SHT 1-2 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E ON EXTERNAL SKIN FOUND 1 CRACK 1" LONG. REPAIRED CRACK ON L/E SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1.

Part: TEE FITTING — CRACKED (RT WING) · airframe 70,984 hrs · 29,122 cycles

RT WING L/E 1 EA CRACK 1" LONG ON FIXED TEE. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 70,984 hrs · 29,122 cycles

LT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL 1.

Part: BULKHEAD — CRACKED (BS 495) · airframe 70,984 hrs · 29,122 cycles

RT AIR COND. COMP. CRACK 2" LONG ON EXTERNAL REPAIR ON VERTICAL BLKHD. REPAIRED IAW FEDEX E.A 8-5320-94639 PART 2.

Part: VERTICAL BEAM — CRACKED (BULKHEAD) · airframe 70,072 hrs · 28,598 cycles

NLG WHEEL WELL RIGHT VERTICAL SUPPORT BULKHEAD CRACKED AT STA Y485 APP 6' C/W EA 8-5320-94639 PART 1. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PART 2 FOLLOW UP ACTION TO BE COMPLIED WITH AT NEXT C-5 CHECK.

Part: CSD — FAILED (NR 2 GENERATOR) · airframe 69,352 hrs · 28,217 cycles

NR 2 ENGINE GENERATOR WILL NOT COME ON LINE, HAS 0 VOLTS AND 0 FREQUENCES. REMOVED AND REPLACED NR 2 ENGINE CSD IAW DC10 M/M 24-11-09-2. SERVICED NR 2 CSD IAW DC10 M/M 24-10-00. OPS CHECK GOOD IAW DC10 M/M 24-11-09 .

Part: LONGERON — CORRODED (BS 1958-1998) · airframe 69,352 hrs · 28,217 cycles

AFT PIT STA 1958 LONG 50L SPLICE IS CORRODED ALL THE WAY TO STA 1998. REMOVED LONG SECTION AND SPLICE IAW DC10 SRM 53-10-00 VOL, 51-35-01 VOL11. MACHINED LONG SECTION AGA7742-19 IAW DAG AGA7742 DALF E7946A. MACHINED LONG SECTION AGA 3104-1 IAW DAC DAG AGA3104 CAL NR E7946A. LOCATED AND DRILLED 2EA, LONG AND 6 SPLICE SECTIONS IAW DAC DAG NR AGA7742. ALODINE AND PRIMED LONGERONS AND SPLICES IAW DC10 SRM 51-21-01 VOL 11. INSTALLED 2 LONG AND 6EA SPLICES IAW SRM 51-33-01 VOL 11.

Part: SPLICE — CORRODED (BS 1711-1721) · airframe 69,352 hrs · 28,217 cycles

CTR LOWER CARGO COMPT STA 1711 TO STA 1721 L48R CORRODED AT INBOARD SIDE AROUND FASTENER. REMOVED CORRODED SPLICE IAW DC10 SRM 51-33-01 VOL 11. FABBED SPLICE IAW DAC DWG AFA 3113. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 11. INSTALLED SPLICE IAW DC10 SRM 51-33-01 VOL 11. MAJOR REPAIR.

Part: SPLICE — CRACKED (ZONE 100) · airframe 69,352 hrs · 28,217 cycles

CTR PIT STA 1704-1715, OUTBOARD SECTION OF L48R SPLICE, CRACKED (FITTING). REMOVED CRACKED SPLICE IAW DC10 SRM 51-31-01 VOL II. FABBED SPLICE FITTING IAW DAC DWG AFA 3113. REMOVED INTERCOSTAL FOR ACCESS IAW DC10-SRM 51-35-01 VOL II AND 51-33-01 VOL II, INSTALLED SPLICE FITTING IAW DC10- SRM 51-33-01 VOL II. REINSTALLED INTERCOSTAL IAW DC10-SRM 51-33-01 VOL II AND DC10 SRM 51-35-01 VOL II; MAJOR REPAIR, N/R 00887.

Part: SPLICE — CORRODED (BS 775) · airframe 69,352 hrs · 28,217 cycles

FWD LOWER PIT STA 775 L52 LONGERON SPLICE CORRODED AFT END. REMOVED FASTENERS AT LONGERON SPLICE STA 755 L52. NO CORROSION FOUND. ALODINE AND PRIMED LONG SPLICE IAW DC10 SRM 51-21-01 VOL 1. PAINTED LONG SPLICE IAW DC10 SRM 51-21-02 VOL 11. FABRICATED LONG END CAP IAW DC10 DWG 3064. INSTALLED LONG END CAP IAW DC10 SRM 51-33-01 VOL 11.

Part: CONTROL VALVE — LEAKING (HYD SYSTEM) · airframe 69,352 hrs · 28,217 cycles

EVIDENCE OF HYDRAULIC LEAK AT I/B SLAT CONTROL VALVE IN CAC COMPARTMENT. REMOVED AND REPLACED I/B SLATE CONTROL VALVE IAW DC10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2.

Part: SKIN — CORRODED (BS 1480-1521) · airframe 69,352 hrs · 28,217 cycles

CENTER GEAR WELL BILGE AREA LIGHT CORROSION ON SKIN AND DETERIORATED PAINT FS 1480 TO FS 1521. REPAIRED AREA IAW FEDEX EA 8-5330-91291, N/R N00316.

Part: CONTROL VALVE — LEAKING (HYD SYSTEM) · airframe 69,352 hrs · 28,217 cycles

RT O/B SLAT CONTROL VALVE LEAKING AT SPLINE SHAFT. REMOVED AND REPLACED RT O/B SLATE CONTROL VALVE IAW DC 10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2.

Part: STRINGER — CORRODED (BS 1510) · airframe 69,352 hrs · 28,217 cycles

CENTER GEAR WHEEL WELL BILGE AREA AT STRINGER 52 STA 1510 IS CORRODED. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 11. FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. REPAIRED LONGERON IAW DC10 SRM 53-00-01 FIG 9 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 11. INSTALLED LONG IAW DC10 SRM 51-33-01 VOL11. MACHINED LONG IAW DAC DWG AYB7013 REV C.

Part: LONGERON — CORRODED (BS 791) · airframe 69,352 hrs · 28,217 cycles

FWD LOWER PIT STA 791 L52 LONGERON END CAP CORRODED. REMOVED DAMAGED END CAP IAW DC10 SRM 51-35-01 VOL 11. MAT ID FOR NEW END CAP FOUND TO BE 7075-0 .063" PO 495488.1 IAW DAC DWG ADA3064 AND FED-EX EA8-5310-92565. FORMED END CAP FITTING IAW DAC DWG3064. HEAT TREATED END CAP. ALODINE AND PRIME IAW DC10 SRM 51-21-01 VOL 11. PAINTED IAW DC10 SRM 51-21-02 VOL 11. INSTALLED END CAP FITTING IAW DC10 SRM 51-33-01 VOL 11.

Part: CABLE — CORRODED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 143 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1445 N RBL 37. REMOVED, REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00-2 . OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 .

Part: CABLE — CORRODED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 143 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1445 RBL37. REMOVED REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM. OPS CHECK GOOD.

Part: CABLE — CORRODED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 148 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1450 RBL37. REMOVED, REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00. OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 .

Part: CABLE — CORRODED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 144 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPARTMENT FLOOR STA 1450 RBL 37. REMOVED, REPLACED, ADJUSTED LEFT HAND BRAKE CONTROL SYSTEM, OPS CHECK GOOD IAW DC10-10 M/M 32-44-00-2 .

Part: CABLE — CORRODED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 147 RUSTY AT PULLEY BEND BELOW MAIN CARGO COMPT FLOOR STA 1450 RBL37. REMOVED REPLACED ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00-2. OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 .

Part: CABLE — DAMAGED (BRAKE) · airframe 69,352 hrs · 28,217 cycles

BRAKE CABLE NR 148 AT PULLEY BEND UNDER MAIN CARGO CARGO FLOOR STA 1450 RBL 37. REMOVED, REPLACED, AND ADJUSTED LT BRAKE CONTROL SYSTEM. OPS CHECK GOOD .

Part: LONGERON — CORRODED (BS 1961) · airframe 69,352 hrs · 28,217 cycles

CORROSION ON LONGERON L49L AT FS 1961 INBD VERTICAL LEG. REMOVED CORROSION ORIGINAL THICKNESS .068, REMAINING .051, REMOVED .071 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-0. REMOVED DAMAGED LONGERON IAW DC10 SRM 51-33-01 VOL 11. MACHINED NEW LONGERON SECTION AND SPLICE IAW DWG AGA3104 AND DC10 SRM 53-10-00 VOL II. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED IAW DC10 SRM 51-33-01 VOLII.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,352 hrs · 28,217 cycles

10" CRACK INSIDE SEAT TRACK FS 1830 TO FS 1840 7.5 RBL. FABRICATED TRACK AND SPLICE AND INSTALLED IAW DC10- SRM 53-70-00-VOL1 FIG 1, SRM 51-31-01 VOL 2 SEE NR N00980 OF WORK ORDER 00029899.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,352 hrs · 28,217 cycles

MAIN CABIN, SEAT TRACK AT RBL 27.5 IS CRACKED AT FS 1272. MANUFACTURED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE IAW DOUGLAS DWG NEA6022 SH2 REV AM AND DC10 SRM 53-70-00 VOL I. SEE FEDEX NONROUTINE N00323 OF WORK ORDER 00029899.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 69,352 hrs · 28,217 cycles

LOWER FUSELAGE STATION 808 FRAME HAS PUNCTURE DAMAGE FROM SKIN SIDE OF J-ANGLE AT LONGERON 51L. REMOVED DAMAGE, FABRICATED NEW ANGLE SECTION AND INSTALLED REPAIR SPLICE AND FILLER IAW DC10 SRM 53-30-00 FIG 5 VOL I.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 68,518 hrs · 27,801 cycles

ON TAKEOFF ROTATION A LOUD POP AND OUTER WINDSCREEN CRACKED, BEFORE LANDING THERE WERE 2 MORE POPS WITH FURTHER CRACKING. REMOVED AND REPLACED L1 WINDOW PER MM 56-11-00-2. OPS CHECK GOOD. ALSO REMOVED AND REPLACED LEFT WINDOW HEAT CONTROLLER PER MM 30-41-01-2, OPS CHECK GOOD.

Part: INDICATOR — INACCURATE (COCKPIT) · airframe 68,345 hrs · 27,693 cycles

A 70 KT DIFFERENCE BETWEEN CAPT & F/O MACH VMO FLAG INDICATOR. CAPT SHOWING 250 & F/O SHOWING 340 AT FL 260 MACH WARNING HORN WAS GOING OFF. ATB MHT. T/S SYSTEM PER TAFI 34-13-00 REPLACED NR 1 CADC AND MACH AIRSPEED INDICATOR. CLEANED PITOT LINES WITH NITROGEN NO OBSTRUCTIONS FOUND. PERFORMED PITOT TEST OF SYSTEM BOTH CAPT & F/O INDICATORS CHECK NORMAL. RETURNED TO SERVICE.

Part: DOUBLER — MISINSTALLED (FUSELAGE) · airframe 67,811 hrs · 27,417 cycles

DURING B SERVICE AT LAX AND RVSM UPGRADE, FOUND PREVIOUS SRM REPAIR INFRINGING UPON RT NORMAL STATIC PORT CONTROLLED AREA. SELECTED REPAIR IS NOT APPLICABLE TO SPEIFIC AREA PER EA 8-5320-77995. REPAIR WAS REMOVED AND APPROPRIATE REPAIR INSTALLED PER SRM 53-20-00, PAGE 93, SHT1, FIG 9. ALSO EA NR 8-5320-77995 IS C/W. ALSO, CHECK N/R #'S 6, 36, 37, 41 AND 42.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 67,733 hrs · 27,376 cycles

AFTER TAKEOFF, ALL GEAR INDICATIONS REMAINED UNSAFE AFTER GEAR HANDLE WAS RAISED AND CHECKED IN, BOTH FRONT AND BACK PANELS. FOLLOWED QRH, CYCLED THE GEAR AND ALL LIGHTS WENT OUT. CONTINUED FLIGHT. TROUBLESHOT IAW DC10 TAFI CHAPTER 32-30-00, FAULT CODE-AA. NO GEAR WARNING HORN WHEN GEAR HANDLE IS PULLED OUT, PROXIMITY ELECTRONICS UNIT DETERMINED TO BE BAD. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS HOUSING IAW DC10-10 MM CHAPTER 32-61-01-2. ALL TESTS/CHECKS PASSED.

Part: SPAR — DAMAGED (ZONE 300) · airframe 67,131 hrs · 27,040 cycles

COMPLY WITH EA 8-5510-75123 STABILIZER OVERSIZE HOLES IN HORIZ STAB CENTER SECTION AFT SPAR. COMPLIED WITH EA 8-5510-75123.

Part: FRAME — CRACKED (ZONE 200) · airframe 67,131 hrs · 27,040 cycles

INSIDE ATTIC-TAIL SECTION CANTED FRAMES AT Y-2046.00 Y-2069.44 AND Y-2092.88 ARE CRACKED. REMOVED DAMAGED CLIPS IAW SRM 51-30-01 AND SRM 51-31-01. LOCATED AND INSTALLED REPAIR CLIPS IAW SRM 51-31-01 AND SRM 51-33-01.

Part: BELLMOUTH — DELAMINATED (ZONE 400) · airframe 67,131 hrs · 27,040 cycles

COMPLY WITH EA 8-7110-75131 ENGINE BELL-MOUTH RING ASSY INTERIM REPAIR A/C N389FE. COMPLIED WITH EA 8-7110-75131.

Part: DOUBLER — WORN (RT TE FLAP) · airframe 67,131 hrs · 27,040 cycles

RIGHT INBOARD FLAP VANE OUTBOARD LEADING EDGE RUB STRIP IS GOUGED/ WORN ALL THE WAY THRU LOWER SURFACE. REMOVED AND REPLACED DOUBLER/RUB STRIP IAW SRM 51-31-01 & SRM 57-10-00.

Part: FLOOR PANEL — CORRODED (MAIN CARGO DECK) · airframe 67,131 hrs · 27,040 cycles

UPPER MAIN CARGO DECK STA 475 FLOOR PANEL AT NR 5 RCB FITTING EXFOLIATED. REMOVED AND REPLACED PANEL IAW SRM 51-31-01.

Part: RIB — GOUGED (ZONE 500) · airframe 67,131 hrs · 27,040 cycles

EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098-25. COMPLIED WITH EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098.25.

Part: BRACKET — CORRODED (RT TE FLAP) · airframe 67,131 hrs · 27,040 cycles

WINGS RIGHT OUTBOARD FLAP - OUTBOARD HINGE REWORK OF SIDE BRACE ATTACH HOLE. COMPLIED WITH EA 8-5740-75127 REWORKED SIDE BRACE ATTACHED HOLES, RIGHT OUTBOARD FLAP, OUTBOARD HINGE IAW EA 8-5740-75127 AT MAE.

Part: HINGE — CORRODED (ZONE 500) · airframe 67,131 hrs · 27,040 cycles

COMPLY WITH EA 8-5750-75126 WINGS - REWORK OF LEFT OUTBOARD FLAP, INBOARD FWD HINGE ASSY P/N ARC0502. COMPLIED WITH EA 8-5750-75126.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 67,131 hrs · 27,040 cycles

OUTBOARD FLAP - FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR P/N ARC2177. COMPLIED WITH EA 8-5750-75125.

Part: BRACKET — CORRODED (ZONE 600) · airframe 67,131 hrs · 27,040 cycles

WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-502. COMPLIED WITH EA 8-5740-75121.

Part: FITTING — CRACKED (ZONE 600) · airframe 67,131 hrs · 27,040 cycles

RIGHT INBOARD AILERON O/B HINGE SUPPORT FITTING CRACKED. REMOVED SUPPORT FITTING IAW M/M 53-23-01, RECEIVED SUPPORT FITTING WITH TRAVLER T4/414610, FIT AND DRILLED IAW SRM 51-35-01 AND INSTALLED SUPPORT FITTING IAW SRM 53-33-01.

Part: PRESSURE SWITCH — FAILED (PNEUMATIC SYS) · airframe 66,370 hrs · 26,661 cycles

PNEUMATIC SYSTEM 3 MANIFOLD FAILURE, IN FLIGHT. COMPLETED RED TABS, LIGHT WENT OUT. CREW REPORTED FAILURE OCCURRED ON DESCENT, APPX 30-40 MILES OUT. REMOVED AND REPLACED RIGHT WING PRESSURE SWITCH IAW MM. OPS CHECK NORMAL IAW TAFI.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

RT MLG RED TRANSITION LIGHT STAYED ON AFT RAISING GEAR, CYCLED LG PER RED TAB & LIGHT EXTINGUISHED, REPEAT.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

RT MAIN GEAR INDICATED ON RETRACTION, RECYCLED GEAR, WORKED OK, INDICATION ON BOTH FRONT AND REAR PANELS. PERFORMED TEST AT PROX BOX PER MM 32-61-01-2 CK GOOD. INSPECTED RT MLG, PROX SW AND TARGET, CK OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

ON DESCENT RT MLG RED LIGHT ILLUM ON BOTH PANELS. ACCOMP RED TAB PROC. FERRIED A/C TO IND.

Part: TARGET — INOPERATIVE (RT MLG DOOR)

01-124 RT MLG RED LIGHT ILLUMINATED ON BOTH PANELS AFTER TAKE OFF. RECYCLED PER RED TABS, REMAIN ILLUMINATED. R/R TARGET PER EO 8-3260-7-3304-B. AC OK FOR SERVICE.

Part: WEB — CRACKED (RT MLG WW)

DURING MAINTENANCE, A 3.75 INCH CRACK WAS FOUND ON RIGHT/CENTER WHEELWELL WEB. CRACK AFFECTED KEEL WEB UPPER SPLICE ONLY, P/N AEA0501. (X)