N370FE

Part: WARNING SYSTEM — FALSE ACTIVATION (R1 DOOR) · airframe 83,441 hrs · 35,042 cycles

WHEN CLOSING UP PRIOR TO PUSH, R1 DOOR DISARMED. LIGHT REMAINS ILLUMINATED WHEN DOOR IS ARMED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 834 hrs · 35,021 cycles

SEAT TRACK LOBE DAMAGED, INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. INSTALLED FLOOR PANELS & CARGO LOADING SYS IAW AMM 53-21-08-2, ANCRA 25-50-66.

Part: COMBINING BOX — DEFECTIVE (COCKPIT) · airframe 829 hrs · 34,775 cycles

TWENTY MINUTES AFTER DEPARTURE STARTED TO NOTICE LIGHT SMOKE, HAZE & ODOR. DETERMINED SOURCE MOST LIKELY FROM HUD WITH EFVS ON. TURNED EFVS OFF & ODOR, SMOKE & HAZE STOPPED. RELEASED FOR SERVICE IAW MEL 31-61-04-01 CATEGORY C, EXPIRATION 17JUL 15. HUD SYS INOPERATIVE, EFVS APPROACH NOT AUTHORIZED. R & R OPU & COMBINER IAW MM 31-82-02-4, 31-82-03-4 & 31-82-4-5.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 829 hrs · 34,772 cycles

AT FL 380 WE ENCOUNTERED ACRID SMOKE IN THE COCKPIT. PERFORMED QRH PROCEDURE TO CLEAR SMOKE. SMOKED CLEARED AFTER 10 - 15 MINS. REPLACED OLD COALESCER BAGS WITH NEW BAGS IAW AMM 21-54-03-2. REFER TO WRI 26-12 4858 FOR FURTHER DETAILS & INSTRUCTIONS.

Part: BATTERY — FAILED (CABIN) · airframe 829 hrs · 34,744 cycles

DURING EMER LIGHT TEST LEVEL 1, EMER BAT 1 LO. REMOVED & INSTALLED EMER LIGHTING BATTERY POWER SUPPLY. OK FOR CONTINUED SERVICE.

Part: ADIRU — FAILED (NR 2) · airframe 828 hrs · 34,722 cycles

NOTICED APPROXIMATELY 2000 FT DIFFERENCE BETWEEN NR 1 AND 2 MCDU DURING PROFILE DESCENT WITH F/O FLYING. SWITCHED AUTOPILOTS TO GET BACK ON PROFILE. AFTER BLOCK-IN IRU NR 2 SHOWED 14.8 DIRIFT & 15 GROUND SPEED. REPLACED THE NR 2 ADIRU, ACOMPLISHED TESTS IAW AMM 34-43-03-4. OPS CHECKED NORMAL AND ACCOMPLISHED AUTOLAND RTS ON FCC 1 AND FCC 2 IAW AMM 22-00-00-5 OPS CKS NORMAL NO DEFECTS NOTED RVSM AND LLM OPS NORMAL.

Part: INDICATOR — DAMAGED (CABIN) · airframe 825 hrs · 34,536 cycles

SOCKET ASSEMBLY FOR R1, DOOR DISARM, LIGHT IS BROKEN. R & R INDICATOR ASSEMBLY IAW SMP 20-00-00. OPERATIONS NORMAL.

Part: INDICATOR — DAMAGED (CABIN) · airframe 825 hrs · 34,536 cycles

SOCKET ASSEMBLY FOR L1 DOOR DISARM LIGHT IS BROKEN. R & R LT FWD ENTRY DOOR DISARM LIGHT SOCKET ASSEMBLY IAW LMMS SM 52-11-0 S1-S2 & IPC 52-11--75-02 ITEM 420. TESTED NORMAL ON GND.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 825 hrs · 34,493 cycles

EMERGENCY POWER TEST FAILED TWICE DURING PREFLIGHT. ASSOCIATED BATTERY CHARGER INOPERATIVE MINUTES LATER. REPLACED BATTERY CHARGER IAW MM 24-34-02-2-0. OPERATIONS CHECKED NORMAL.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 81,946 hrs · 34,159 cycles

RIGHT OTBD FLAP VANE UPPER SURFACE OTBD OF OTBD TRACK HAS CHAFED. RT OTBD FLAP VANE UPPER SURFACE REPAIRED IAW SRM 57-53-01. EA 8-5750-T0312136 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT OTBD FLAP VANE UPPER SURFACE CHAFED RSC TRACKING ISSUED. MAJOR REPAIR.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 81,946 hrs · 34,159 cycles

RIGHT WING INBD FLAP VANE INBD UPPER SURFACE THE REPAIR DOUBLER IS CHAFED WITH PAINT OVER. REPAIRED RT WING INBD FLAP VANE UPPER SURFACE IAW SRM 57-00-01, SRM 51-71-00 & SRM 51-23-10. EA 8-5750-T0312137 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT WING INBD FLAP VANE INBD UPPER SURFACE RSC TRACKING ISSUED. MAJOR REPAIR.

Part: DUCT — CRACKED (NR 1 PYLON) · airframe 81,946 hrs · 34,159 cycles

PANEL 437DR, NR 1 PYLON HEAT EXCHANGE DUCT, INNER WALL CRACKED. REMOVED FASTENERS IAW SRM 51-35-01 FOR ACCESS TO WELD SUPPORT ANGLES. INSTALLED FASTENERS IAW SRM 51-35-01. WELDED NR 1 PYLON HEAT EXCHANGE DUCT ON T14 1095275 IAW EA 8-5450-T0311727 REV NR PS P1. MINOR REPAIR.

Part: PANEL — CRACKED (NR 1 PYLON) · airframe 81,946 hrs · 34,159 cycles

NUMBER 1 PYLON PRE COOLER PANEL 437DR RIB STIFFENERS TOP & BOTTOM SIDES, INCLUDING FWD & AFT FLANGES, FOUND CRACKED WELDED AREAS. VERIFIED PANEL 437DR SECONDARY STRUCTURE IAW EA 8-5450-T0311730 STEP 1. WELDED RIB STIFFENERS TOP & BOTTOM SIDES & FWD & AFT FLANGES ON T14 1095276 IAW EA 8-5450-T0311730 REV NO A PS P1. MINOR REPAIR.

Part: PANEL — CRACKED (NR 3 PYLON) · airframe 81,946 hrs · 34,159 cycles

NUMBER 3 ENG PYLON PANEL 487DL HAS CRACK FWD LOUVER RADIUS, MARKED. WELDED CRACK ON T14 1095278 ON NR 3 ENG PYLON PANEL 487DL MAT 321 DPS 10.225, AMS 5L80 ROD & ACCOMPLISHED IAW EA 8-5450-T0311732 REV NO PS P1. MINOR REPAIR.

Part: PANEL — CRACKED (NR 3 PYLON) · airframe 81,946 hrs · 34,159 cycles

NUMBER 3 ENG PYLON PANEL 487DL HAS CRACK LOWER LT CORNER OF PRE COOLER BOX, MARKED. REMOVED FASTENERS TO ACCESS CRACK IAW SRM 51-31-01. WELDED CRACK ON T14 1095277. REINSTALLED FASTENERS IAW SRM 51-31-01. ACCOMPLISHED WELD REPAIR IAW EA 8-5450-T0311731 REV NO PS P1. MINOR REPAIR.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 81,946 hrs · 34,159 cycles

LEFT INBD ELEVATOR TE UPPER SURFACE HAS DENT. EVALUATED DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 VOL 1 FIG 8 L = 2 INCHES, W = 4 INCHES. FABRICATED DOUBLER & FILLER IAW SRM 55-10-00 FIG 8 PG 15. INSTALLED FASTENERS IAW SRM 51-36-01. REPAIRED LT INBD ELEVATOR IAW SRM 55-10-00 FIG 8 VOL 1. MAJOR REPAIR.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 81,946 hrs · 34,159 cycles

L1 DOOR OUTER SKIN BOTTOM FWD CORNER HAS A NOTCH CUT OUT. TEMP REPAIR, FABRICATED DOUBLER MAT 2024-T3 .071C, BATCH 2021540 IAW SRM 52-10-00 FIG 12A SHEET 1. INSTALLED DOUBLER IAW SRM 52-10-00. ACCOMPLISHED EA 8-5210-T0311872 RSC FOR TRACKING. MAJOR REPAIR.

Part: DOUBLER — DAMAGED (LT WING) · airframe 81,946 hrs · 34,159 cycles

LEFT WING LE PANEL 518GB HAS ONE EACH ELONGATED FASTENER HOLE ON PANEL CUT OUT. R & R LT WING LE ACCESS PANEL 518GB LANDING DOUBLER WITH NEW PART. FABRICATED FROM 7075-T6, 0.090C BN 1885277 IAW 57-21-01 FIG 7 ITEM 33 & SRM 51-31-01. MAJOR REPAIR. .

Part: LONGERON — CORRODED (BS 735-755) · corrosion level 2 · airframe 81,946 hrs · 34,159 cycles

LOWER FWD CARGO COMPARTMENT LONGERON 52 CORRODED BETWEEN STATION 735 - 755. REPAIRED IAW SRM 53-10-00 FIG 2 SHEET 1. REMOVED CORROSION ON LONGERON & FOUND TO BE OUT OF LIMITS IAW SRM 53- 00-01 FIG 1 B. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,946 hrs · 34,159 cycles

AFT CARGO FLOORBEAM AFT FLANGE IS EXFOLIATED AT STATION 1841, PARALLEL TO LONGERON 51L. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. REPAIRED IAW SRM 53-00-01 FIG 7, MATERIAL USED 7075- T6 063 1498-200 PO 0002031082. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 81,946 hrs · 34,159 cycles

MCD FLOORBOARD STATION 1909 - 2007, RBL 36 HAS CRACKS. FABRICATED FLOOR PANEL ON T14 1093394, BATCH 2663757 IAW SRM 51-61-01 / SRZ-25-005. MAJOR REPAIR.

Part: FITTING — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 81,946 hrs · 34,159 cycles

AFT CARGO DOOR FRAME LOWER FWD CORNER FITTING IS CORRODED. REMOVED AND REPLACED THE CORNER FITTING IAW SRM 51-31-01. ADJUSTED, SAFTIED OPS CHECKED GOOD IAW AMM 52-33-00-0. MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 81,876 hrs · 34,106 cycles

1L DOOR LIGHT DOES NOT TEST. CHANGED BATTERIES IN L1 DOOR IAW SMP.

Part: SKIN — CRACKED (LT WING) · airframe 81,669 hrs · 33,966 cycles

DURING POST FLIGHT, FOUND A CRACK ON THE LT WING LE AT NR 4 SLAT, OTBD TRACK CUT OUT, LOWER, INBD RADIUS. HFEC INSPECTED SUSPECTED IAW NDTSPM 06-10 01 & VERIFIED THE CRACK TO BE A 3/8 - 1/2 INCH LONG. CUT OUT DAMAGED AREA IAW SRM. VERIFIED CRACK REMOVED USING HFEC IAW NDTSPM 06-10-01, NO INDICATIONS NOTED. INSTALLED DOUBLER IAW SRM 57-10-00 VOL 1 FIGURE 68.

Part: SKIN — CRACKED (LT WING) · airframe 81,669 hrs · 33,966 cycles

WHILE PERFORMING FCD, FOUND A CRACK ON NR 1 INBD SLAT TRACK SKIN CUT OUT LT WING. VERIFIED CRACK USING HFEC IAW NDTSPM 06-10-01. CRACK 1/2 INCH IN LENGTH. REMOVED CRACK. COMPLIED WITH HFEC INSPECTION, NO CRACKS FOUND. REPAIRED IAW EA 8-5710-F0308207. MAJOR REPAIR.

Part: SENSOR — MALFUNCTIONED (MLG) · airframe 79,914 hrs · 32,810 cycles

ON GEAR RETRACTION, AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP AND LOCK ON BOTH THE PRIMARY AND SECONDARY INDICATORS. ON TOUCHDOWN, IT FEELS LIKE RT GEAR BOTTOMS OUT AS THE AIRPLANE SETTLES TO THE RUNWAY. CHECK WIRES IAW WDM 32-61-01, 32-61-03 AND TROUBLESHOT IAW FIM 32-30. FOUND NO DEFECTS. VISUALLY CHECK IN RT WHEEL WELL COMPARTMENT. NO DEFECTS NOTED. REMOVED BOLTS ON LT AND RT MLG LINK ASSY UPLOCK PROX SENSOR AND REMOVED TARGETS FORM DOWNLOCK PROX SENSORS. RAISED GEAR HANDLE UP AND LT AND RT RED LIGHTS EXTINGUISHED. RE-INSTALLED BOLTS ON LT AND RT MLG LINK ASSY UPLOCK AND TARGETS ON DOWNLOCK PROX SENSORS IAW MM 32-61-15-4. OPS CK NORMAL ON PSEU. ALL 3 GEAR PINS REMOVED.

Part: SENSOR — INOPERATIVE (MLG) · airframe 79,911 hrs · 32,808 cycles

WITH THE LANDING GEAR HANDLE UP, THE RT GEAR INDICATION NOT UP AND LOCK IN BOTH THE PRIMARY AND SECNDARY INDICATORS. (LIGHT RED) PERFORMED VISUAL INSP OF RT MLG UPLOCK PROX SENSOR AND NO DEFECTS NOTED, PSEU RTS PASSES NORMALLY, CHECKED PSEU SENSOR READOUT UNDER RIGGING AND FOUND "RG UP LCHA" HAS HIT 19 OUT OF 20 FLIGHTS. PERFORMED ADJUST CLEARENCE FOR PROX SENSOR AND TARGET IAW MM 32-61-15-4. THIS UPLOCK TARGET FOUND TO BE OUT OF LIMITS BY 50MM. R & R RT MAIN LANDING GEAR UP SENSOR. IAW MM 32-61-15-4, OPS CHECK NORMAL IAW PSEU.

Part: FUEL CONTROL — MALFUNCTIONED (ENGINE) · airframe 79,209 hrs · 32,420 cycles

FLEX PWR SET FOR 50 PERCENT, THROTTLES ADVANCED SMOOTHLY WHEN AUTOFLT SELECTED TO THE APPROPRIATE REDUCED PWR CHEVRON INDICATED SETTINGS ON THEN 1 GUAGE. THROTTLES CLAMPED NORMALLY PRIOR TO 80KTS. AFTER 80 KTS THE NR 3 ENGINE BEGAN NOTICEABLY SURGING WITH NR3 N1, N2 AND EGT FLUCTUATING WITH THE NR 3 THROTTLE CLAMPED AND NOT MOVING. SOON THEREAFTER THE NR 2 AND NR 1 THROTTLES BEGAN RETARDING TO COMPENSATE FOR THE N1 OVERSPEED ABOVE THE CHEVRON. TAKEOFF ABORTED BETWEEN 100 TO 110KTS. REPLACED NR 3 ENGINE FUEL PUMP PER M/M 73-12-01-2. ALSO REPLACED MAIN ENGINE CONTROL PER MM 73-20-01-2, BOTH LEAK CHECK GOOD ON WET MOTOR AND IDLE ENGINE RUN, WILL REQUIRE POWER TEST. COMPLIED WITH MAX POWER ASSURANCE RUN PER JRH AND ENGINE RUN FORM. ALL CHECKS WITHIN LIMITS, OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 78,043 hrs · 31,800 cycles

DURING SERVICE CHECK, FOUND L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER MISSING. INSTALLED NEW L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER IAW STANDARD PRACTICE.

Part: DOOR — INOPERATIVE (L1) · airframe 78,044 hrs · 31,801 cycles

DOOR L1 HAD NO POWER TO CLOSE AT CLOSEUP AND PUSHBACK. DOOR OPS CHECKED GOOD IAW MM 52-10-01-2-0.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 77,887 hrs · 31,704 cycles

RTO BELOW 80 KNOTS FOR LVL 1 ENG 2 EXCEEDANCE ALERT. MAX N2 101.1. PREVIEWED QRH FOR LVL1 AND RTO. ADVISED MX. RETURNED TO GATE. COMPLIED WITH VISUAL INSP OF NR 2 ENG EXHAUST AREA IAW AMM 72-00-00-6, NO DAMAGE NOTED. INSPECTED WHEELS TIRES BRAKES AND MLG DUE TO RTO IAW AMM 05-56-00-6 AND 05-57-00-6. NO DAMAGE NOTED. ACFT OK FOR SERVICE. BORESCOPED HPC AND HPT IAW AMM 72-00-00-6 AND FOUND NO LIMITING DEFECTS. INSTALLED BORESCOPE PLUGS ON NR 2 ENGINE. ACCOMPLISHED VSV STATIC RIG IAW AMM 73-20-01-2 PART A. ADJUSTED IAW 73-20-01-2, CHECKED GOOD OK FOR CONT SERVICE.

Part: CONNECTOR — CORRODED (ENGINE OIL) · airframe 77,726 hrs · 31,611 cycles

WE RECEIVED AN ENG 2 OIL FILTER, LEVEL 2 ALERT. FOLLOWING QRH ENG 2 WAS SHUTDOWN. REMOVED AND REPLACED THE SCAVANGE AND MAIN LUBE OIL FILTERS, NO CONTAMINATION WAS FOUND REF. AMM MD10-79-20-02 AND 79-20-01, LEAK CHECK WAS GOOD. COMPLETED A 5 MINUTES GROUND IDLE RUN TO SATISFY INFLIGHT SHUTDOWN REF. AMM MD10-72-00-00-6-1. REMOVED CONNECTOR FOR OIL DIFFERENTIAL SWITCH AND WAS GETTING THE AIU READING TO JUMP FROM NORMAL TO CLOGGED WHILE REMOVING THE CONNECTOR, AFTER CONNECTOR WAS REMOVED, ONLY A NORMAL READING WAS OBSERVED, RECONNECTED AND SHOOK THE CONNECTOR, NOW READING JUMPS FROM CLOGGED TO NORMAL, ALSO REF. FIM 79-35. CALLED AVI LINE FOR ASSIST WITH THE CONNECTOR OR WIRING ISSUE. REMOVED, AND UNTAPED, & DEPINNED CONNECTOR, INSPECTED WIRING. NO DEFECTS NOTED. FOUND FACE OF CONNECTOR AT PIN B SLIGHTLY CONTAMINATED OR CORRODED. REMOVED AND REPLACED CONNECTOR P1-8065 IAW WDM 79-34-01. RECONNECTED CONNECTOR, RAN #2 ENGINE PER JRH WHILE OBSERVING SENSOR READ OUT IN AIU 2 AND AIU 3 WITH NO FAULTS.

Part: CABLE — BENT (NR 2 VSV) · airframe 77,185 hrs · 31,324 cycles

STARTED T/O ROLL NR 2 THROTTLE WAS SLOW TO ACHIEVE TAKEOFF POWER. AFTER ACHIEVING TAKEOFF POWER NR 2, N1 ROLLED BACK TO 10 O'CLOCK ON THE GAUGE AND ENGINE FAIL CAME ON AROUND 90 KTS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM 75-31-01-2. REMOVED AND REPLACED NR 2 ENGINE FAN SPEED SENSOR PER AMM 77-11-01-2. CLOSED NR 2 ENGINE FAN, REVERSER AND CORE COWLS AND PATIO DOORS. COMPLIED WITH MAX POWER ASSURANCE CHECK AND ENGINE ACCELERATION CHECK PER MD-10 JRH. COMPLETED ENGINE RUN. ALL PARAMETERS NORMAL.

Part: MEC — FAILED (NR 2 ENGINE) · airframe 77,185 hrs · 31,324 cycles

ON TAKEOFF, NR 2 ENGINE DID NOT REACH T/O, N1 WITH THROTTLE ALIGNED WITH NR1 AND NR3. THROTTLE WAS MOVED SLIGHTLY FWD MANUALLY, AND N1 ROLLED BACK. ENGINE FAIL LIGHT ILLUMINATED, TAKEOFF REJECTED AT 85KTS. INSTALLED FUEL PUMP/MEC IAW MM 73-20-01-2. PERFOMED STEPS B 1-29. STEP 29 C/W IAW MM 75-31-01-5. ACCOMPLISHED LEAK CHECK, IDLE CHECK AND FLIGHT IDLE CHECK, ADJUSTED FLIGHT IDLE 1 TURN CLOCKWISE, THEN ACCOMPLISHED THE MAXIMUM POWER ASSURANCE CHECK/RUN PER MM 71-00-00-5 AND JRH.. ALL PARAMETERS FOUND TO BE WITHIN LIMITS MPA FORM FAXED TO MOCC. NR 2 ENGINE COWLING AND WORK PLATFORM CLOSED AND SECURED PER 71-00-00-2.

Part: FLOOR PANEL — PUNCTURED (BS 1841) · airframe 77,094 hrs · 31,271 cycles

AFT CARGO PIT FLOOR PANEL LT SIDE AT STA 1841 IS PUNCTURED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ25-005, REV "H" AND DWG SRZ 25-011, REV "C". REMOVED AND RE-INSTALLED FLOOR PANEL IAW SRM 51- 31-01, VOL II.

Part: CHANNEL — CORRODED (BS 1521) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

CTR CARGO COMPARTMENT AT BS 1521, LBL 56, CHANNEL IS CORRODED. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED "J" CHANNEL IAW DAC DWG 2929469. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM 53-00-01, FIG 9, VOL I.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 77,094 hrs · 31,271 cycles

FWD CARGO PIT FLOOR PANEL 127 UF IS CRACKED. (BS. 791 - 2ND INBD) FABRICATED FLOOR PANEL 127 UF IAW SRZ 25-005, REV H. INSTALLED FLOOR PANEL 127 UF IAW SRM 51-31-01, VOL II.

Part: SKIN — DENTED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

RT EXTERIOR FUSELAGE SKIN PRIMARY STATIC PORT CONTROLLED AREA HAS 5 EA DENTS. REPAIRED RT PRIMARY STATIC PORT CONTROLLED AREA DENTS, 5 EACH IAW EA 8-5330-123564, REV "IR" 10-1-10, ALL DENTS FOUND TO BE WITHIN LIMITS EA 8-5330-123564, REV "IR" 10-1- 10, AND AMM 34-11-01-2. NO FURTHER ACTION REQUIRED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

CENTER CARGO COMPARTMENT BILGE AREA INTERCOSTAL IS CORRODED AT BS 1724; RBL 3. REMOVED ROLLER TRAY TO F.O.M. IAW MD/DC10 SRM 51-31-01, VOL II. REMOVED VHF ANTENNA TO F.O.M. REMOVED INTERCOSTAL TO F.O.M. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNESS 0.071. MATERIAL REMOVED 0.021. MATERIAL REMAINING 0.050. FABRICATED INTERCOSTAL IAW DAC DWG ACA 3011, REV "F". ALODINED, PRIMED AND PAINTED INTERCOSTAL IAW SRM 51-31-01, VOL II. INSTALLED INTERCOSTAL IAW SRM 51-33-01, VOL II. INSTALLED ROLLER TRAY IAW SRM 51-31-01, VOL II. INSTALLED VHF ANTENNA IAW AMM 23-12-05-04. PERFORMED OPS CHECK ON ANTENNS IAW AMM 23-12-05-04.

Part: TUBE — CRACKED (THRUST REVERSER) · airframe 77,094 hrs · 31,271 cycles

NR1 ENG LT THRUST REVERSER GREEN COOLING TUBE IS CRACKED. R & R NR1 ENG LT THRUST REVERSER COOLING TUBE IAW AMM70-00-00; AMM 78-32-14; 70-32-01; SRM 51-21-01 AND SRM 51-41-01.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 77,094 hrs · 31,271 cycles

AFT PIT FLOORBOARD 187 GF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD PANEL 187 GF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: FLOORBOARD — PUNCTURED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

AFT PIT FLOOR BOARD 187 HF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD 187 HF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: LONGERON — CRACKED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

FWD CARGO BAY LONGERON 52 BETWEEN STA 859 AND STA 755 HAS A CRACKED FASTENER HOLE. FABRICATED NEW LONGERON IAW DWG ADA 3064 AND SRM 51-10-02, FIG 1, VOL III. ALODINED, PRIMED AND PAINTED LONGERON 52 IAW SRM 51-21-01, VOL II. INSTALLED LONGERON 52 IAW SRM 51-33-0; SRM 51-31-01, VOL II; DWG NDA 6014 AND DWG ADA 3064.

Part: FAILSAFE — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

CAC FRAME FAILSAFE ANGLE IS CORRODED STA 1119; LONGERON 51 RT. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1-B, VOL II. REMOVED INTERCOSTALS AT STA 1119 TO 1099; RBL 6 AND LONGERON 51 TO F.O.M. IAW SRM 51-30-0, VOL II. MATERIAL ID FOR REPAIR FILLER 7075-0 0.071, PO 692456.1 IAW DWG AAA7046 AND SRM 51-10-02, FIG 1, VOL III. MATERIAL ID FOR REPAIR ANGLE 7075-0 0.080, PO 927975.4 IAW SRM 53-30-00, FIG 5, VOL I. HEAT TREATED REPAIR FILLER AND ANGLE TO 7075-T6, LOAD HT100610-6. FABRICATED REPAIR FILLER AND REPAIR ANGLE IAW SRM 51-10-02, FIG 5, VOL 1. ALODINED AND PRIMED REPAIR FILLER AND ANGLE IAW SRM 51-21-01, VOL II. INSTALLED REPAIR FILLER, ANGLE AND INTERCOSTAL AT STA 1099 TO 1119; RBL 6 AND LONGERON 51 IAW SRM 51-30-01, VOL II.

Part: FLOOR PANEL — DEBONDED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

CTR ACCESSORY COMPARTMENT LT STEP IS DEBONDED. REMOVED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW SRM 51-31-01, VOL II. FABRICATED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW DWG SRZ 25-005, REV "H". INSTALLED NEW PANEL IAW SRM 51-31-01, VOL II.

Part: SEAT TRACK — DAMAGED (BS 775) · airframe 77,094 hrs · 31,271 cycles

MAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 775 RBL 8. REMOVED AND RE-INSTALLED FLOOR BOARD PANEL LBL 0 TO RBL 27 AT STA 615 - 775. MATERIAL ID NEW SEAT TRACK 49291150-12000, PO 617966.1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. VOL I. OK TO PRIME, ALODINE ATPAINT IAW SRM 51-21-01, VOL II. (OUT OF SEQUENCE) FABRICTED SEAT TRACK, SPLICE PLATE IAW MD/DC10 SRM 53-70- 00, VOL I.

Part: SKIN — GOUGED (BS 999) · airframe 77,094 hrs · 31,271 cycles

FWD CARGO DOOR CUTOUT, AFT SKIN DOUBLER AT APPROXIMATELY STA 999; STRINGER 40 IS GOUGED AND MISSING MATERIAL. REMOVED DOUBLER IAW MD/DC10 SRM 51-31-01, VOL II. GENERATED RFTS N370FE-28-43009 MATERIAL ID TO FABRICATED A NEW DOUBLER IS 2024-T3 0.125, PO 674650.3 IAW SRM 53-50-00, FIG 8, VOL I. FABRICATED NEW DOUBLER IAW MD/DC10 SRM 53-50-00, FIG 8, VOL I. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01, VOL II AND SRM 51-21-02, VOL II. INSTALLED NEW DOUBLER IAW SRM 53-50-00, FIG 8, VOL I AND SRM 51-31-01, VOL II.

Part: WEDGE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT OTBD FLAP SEC WEDGE PANEL, INBD TOP SKIN REQUIRES REPLACEMENT BECAUSE OF CORROSION. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II. FABRICATED 1 EA DOUBLER IAW DWG ARC 1953, REV "J". FABRICATED -34 AND -35 TEE CAPS IAW DWG ARC 1953, REV "J". INSTALLED SKIN ASSY AND REPAIR IAW SRM 51-31-01, VOL II.

Part: BRACKET — CORRODED (BS 1701) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

CTR CARGO PIT FRAME AND CLIP (LWR SIDE) HAS CORROSION FROM BS 1701 TO BS 1702; LONGERON 44R. REMOVED BRACKET IAW SRM 51-35-01, VOL II. FOUND TO BE OUT OF LIMITS. FABRICATED NEW BRACKET IAW DWG AFA0043. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED BRACKET IAW 51-33-01, VOL II. CLEANED AREA IAW SRM 51-21-01, VOL II. NO CORROSION NOTED ON FRAME.

Part: GUSSET — CRACKED (BS 1480-1482) · airframe 77,094 hrs · 31,271 cycles

MAIN CABIN INTERNAL FRAME GUSSET IS CRACKED BETWEEN BS 1480 AND BS 1482, STRINGER 16R - STRINGER 17R. FABRICATED NEW CHANNEL IAW DWG 88277. HEAT TREATED CHANNEL FROM 7075-0 TO 7075-T6 PER DWG AWE 7017, REV "AH" AND IAW DPS 7.0. LOCATED AND DRILLED NEW CHANNEL IAW SRM 51-31-01, VOL II. ALODINED AND PRIMED IAW SRM 51-21- 01, VOL II. INSTALLED CHANNEL IAW SRM 51-31-01, VOL II.

Part: CHANNEL — CORRODED (BS 1521) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

CTR CARGO COMPARTMENT CHANNEL IS CORRODED BELOW THE CARGO FLOOR AT BS 1521, RBL 56. REMOVED DAMAGED J-CHANNEL IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. MATERIAL ID FOR REPAIR ANGLE AND ZEE ANGLE IS 7075-T6511, PO 299853.1 IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED J-CHANNEL IAW DWG S2929469. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM 53-0-01, FIG 9, VOL I.

Part: SUPPORT — CORRODED (BS 1840) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

AFT CARGO COMPARTMENT AREA SEAT TRACK SUPPORT IS CORRODED AT THE TRACK ATTACH POINT; BS 1840, RBL 20. REMOVED CORROSION ON THE SEAT TRACK SUPPORT IN THE AFT CARGO COMPARTMENT AT THE TRACK ATTACH POINT BS 1841, RBL 20. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1A & FIG 1B. DISASSEMBLED SEAT TRACK AT RBL 20 FROM STA 1781 TO STA 1853 TO F.O.M. IAW SRM 51-31-01, VOL II. CUTOUT DAMAGED SECTION OF THE SUPPORT ANGLE IAW MD/DC10 SRM 53-00-01, FIG 8, VOL I. FORMED, DRILLED & DEBURRED REPAIR PARTS IAW SRM 53-00-01, FIG 8, VOL I . ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED REPAIR IAW SRM 53-00- 01, FIG 8, VOL I. ASSEMBLED SEAT TRACK IAW SRM 51-31-01, VOL II.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 77,094 hrs · 31,271 cycles

CRACK FOUND LT WING INTERNAL LOWER STRINGER 36 BUTTERFLY CLIP AT XORS 402.00. REMOVED AND REPLACED BUTTERFLY CLIP IAW DWG ARB2176 AND EA 8-5710-123558.

Part: FLOOR SUPPORT — DAMAGED (BS 1801) · airframe 77,094 hrs · 31,271 cycles

AFT CARGO COMPARTMENT AREA FLOOR PANEL SUPPORT FRAME HAS A DOUBLE DRILLED HOLES AT BS 1801, RBL 40. MATERIAL ID'S ANGLE PO NR 456452.1, STRAP PO NR652554.2 & FILLER PO NR652554.2 IAW SRM 53-00-01, FIG 9, VOL I. REMOVED DAMAGE AND FABBED REPAIR PARTS IAW SRM 53-00-01, FIG 9, VOL I. ALODINE AND PRIMED IAW SRM 51-21-01, VOL II. INSTALL REPAIR IAW SRM 53-00-01, FIG 9, VOL I.

Part: DUCT — CORRODED (NR 2 ENGINE INTA) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

NR2 ENGINE INLET DUCT INTERIOR SKIN IS CORRODED; FASTENERS SHEARED AND IS CORRODED INSIDE PANEL 362 DOOR (RT), STA 222. REMOVED AND REPLACED INLET SKIN IAW MD/DC10 SRM 51-31-01, VOL II AND DWG AJC7288, REV "D".

Part: WEDGE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT OUTBD FLAP, NR 2 WEDGE LOWER SKIN AND FINGER DOUBLER IS CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 3 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSY.

Part: SKIN — BULGED (BS 824 L52) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

FUSELAGE SKIN BULGED AT STA 824, LONGERON 52. REMOVED DAMAGED SKIN AND TEAR STRAPS. FABBED NEW SKIN SECTION, TEAR STRAPS AND END SPLICE IAWDWG NDA 6014 AND SRM 53-20-00, FIG 17, VOL I. ALODINED, PRIMED AND PAINTED PARTS IAW SRM 51-21-01, VOL II. INSTALLED PARTS IAW DWG NDA 6014 AND SRM 51-31-01AND SRM 51-33-01, VOL II.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 5; INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OTBD FLAP; INBD HINGE FITTING; SIDE LOAD FITTING MOUNTING SURFACE CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 7 FWD BOLT HOLE CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5; OUTBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 2 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 3; BORE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE; LOCATION NR 5 INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 3; OUTBD BORE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; BARREL NUT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAPS) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3, OTBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5; INBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 4; INBD LUG FACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 5 BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAPS) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE; LOCATION NR 2 OUTBD BORE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; LOCATION NR 6 OTBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 4 OUTBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (ZONE 600) · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 5 OUTBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5; INBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAPS) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 4; INBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 6; INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 3 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 6; INBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR4; OTBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 7 AFT BOLT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: LONGERON — CORRODED (BS 824 L50R/L) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

FWD CARGO COMPARTMENT BILGE AREA LOWER TEAR STRAP N AND SKIN HAS CORROSION AT FRAME 824; LONGERON 50R - LONGERON 50L. FABRICATED AND INSTALLED NEW LONGERONS IAW DAC DWG ADA 3064 AND NDA 6014. LOCATED AND DRILLED NEW SHEAR TIES IAW DAC DWG NDA 6014; SRM 51-23-01 AND SRM 51-31-01, VOL II. SKIN WAS REPLACED ON JOB CARD NR N00646. LONGERON SPLICE IAW SRM 53-10-00, FIG 2, VOL I (L51L). SEE SRM 53-10-00, FIG 2, SHEET 2 , VOL I FOR DAMAGE TOLERANCE INSPECTION REQUIREMENTS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 4 BORE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5; INBD LUG FACE INNER SURFACE CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 2; INBD BORE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5 INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 6; OUTBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; SIDE LOAD FITTING; AFT BOLT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 4 INBD LUG FACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR7 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5 OTBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 6; INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 3 INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5 INBD LUG FACE OUTER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 3 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; SIDE LOAD FITTING; MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OTBD FLAP; INBD HINGE FITTING; SIDE LOAD FITTING FWD BOLT HOLE CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 7 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OTBD FLAP; INBD HINGE FITTING; SIDE LOAD FITTING AFT BOLT HOLE CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 7; AFT BOLT HOLE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 6; INBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 7; FWD BOLT HOLE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; LOCATION NR6 OTBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5; OUTBD LUG FACE INNER SURFACE CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR3; OTBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR3; INBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 6; OUTBD BUSHING IS WORN. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 5 INBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 5 INBD LUG FACE OUTER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 2 OUTBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

LT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 5; OTBD BUSHING IS WORN. REPLACED THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; OUTBD HINGE FITTING; LOCATION NR 5; OUTBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 6 OTBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; INBD HINGE; SIDE LOAD FITTING; FWD BOLT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 2 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE; LOCATION NR 6 INBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 2; OUTBD BORE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 4 INBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RIGHT WING OUTBD FLAP; INBD HINGE; LOCATION NR 5 OUTBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3; MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

RT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3; INBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,094 hrs · 31,271 cycles

LEFT WING OUTBD FLAP; INBD HINGE FITTING; LOCATION NR 4; OUTBD LUG FACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

FWD CARGO BAY FLOOR PANEL 123DF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED FLOOR PANEL 123 DF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

AFT PIT FLOOR PANEL NR 187 AF HAS NUMEROUS PUNCTURES. FABRICATED AFT PIT PANEL 187 AF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

AFT CARGO BAY FLOOR PANEL 187CF IS PUNCTURED IN SEVERAL PLACES. FABRICATED FLOOR PANEL 187 CF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: FLOOR PANEL — PUNCTURED (TAILCONE) · airframe 77,094 hrs · 31,271 cycles

TAIL CONE LWR CTR FLOOR PANEL IS PUNCTURED IN SEVERAL PLACES. FABRICATED TAILCONE LT LOWER CENTER PANEL IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

AFT PIT FLOOR PANEL NR 187 EF HAS NUMEROUS DENTS AND PUNCTURES. FABRICATED AFT PIT PANEL 187 EF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

CENTER PIT FLOOR PANEL 183 XF HAS EDGE DAMAGE AND FASTENER HOLE DAMAGE. FABRICATED CENTER PIT PANEL 183 XF IAW FEDEX DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 77,094 hrs · 31,271 cycles

CENTER CARGO BAY FLOOR PANEL, NR 183DF HAS SEVERAL DAMAGED INSERTS. FABRICATED CENTER CARGO BAY FLOOR PANEL 183 DF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 77,094 hrs · 31,271 cycles

AFT CARGO BAY FLOOR PANEL NR 187DF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED AFT CARGO BAY FLOOR PANEL 187 DF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".

Part: FLOOR PANEL — DENTED (BS 1361) · airframe 77,094 hrs · 31,271 cycles

MAIN CABIN FLOOR PANEL IS DENTED AT STA 1361; RBL 75.5 TO RBL 107.25. REPAIRED DENT ON FLOOR PANEL 252KFIAW SRM 53-60-00, FIG 7; VOL 1.

Part: FLOOR PANEL — CRACKED (TAILCONE) · airframe 77,094 hrs · 31,271 cycles

TAIL CONE; RIGHT PATIO DOOR FLOOR PANEL IS CRACKED. FABRICATED TAIL CONE RIGHT PATIO DOOR PANEL IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 77,094 hrs · 31,271 cycles

FWD PIT FLOOR PANEL 123GF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED FLOOR PANEL 123 GF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — WORN (TAILCONE) · airframe 77,094 hrs · 31,271 cycles

TAIL CONE; AFT PATIO DOOR HAS HONEYCOMB EXPOSED. FABRICATED TAIL CONE AFT ACCESS DOOR IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.

Part: FLOOR PANEL — CRACKED (TAIL CONE) · airframe 77,094 hrs · 31,271 cycles

TAIL CONE LT UPPER FLOOR PANEL IS CRACKED. FABRICATED PANEL FOR TAIL CONE LT UPPER IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.

Part: FLOORBOARD — DAMAGED (BS 1059-1089) · airframe 77,094 hrs · 31,271 cycles

FWD PIT FLOORBOARD AT STA 1059-1089 LT, INBD HAS DAMAGE AROUND FASTENER HOLE ON THE EDGE. FABRICATED FWD PIT PANEL 127 UF; STA 1059 TO STA 1089 IAW SRZ 25-005, REV "H".

Part: FITTING — CRACKED (CARGO DOOR) · airframe 77,094 hrs · 31,271 cycles

MCD NR 5 SPOOL HAS A CRACK INDICATION AT HOLE "D". REMOVED AND REPLACED THE NR 5 SPOOL FITTING IAW SRM 51-31-01, VOL II AND SRM 51-33-01, VOL II. MACHINED AND INSTALLED BUSHING IN HOLE "D" IAW SRM 53-50-00, VOL I.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 77,094 hrs · 31,271 cycles

MCD NR2 SPOOL HAS A CRACK INDICATION AT HOLE "C". REMOVED SPOOL FITTING NR 2 IAW SRM 51-31-01, VOL II. MATERIAL ID IAW MD/DC10 SRM 53-50-00, FIG 17, VOL I. INSTALLED NEW SPOOL FITTING IAW SRM 51-33-01, VOL II, PERFORMED HFEC IAW NATSPM 06-10-01.003 ON 4 EA. MOUNT HOLES. NO CRACKS FOUND USING TNAT0010-1. MACHINED 11 EA. REPAIR BUSHINGS IAW SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-1213556. BUSHING OD DIAMETER CHECK FOR PROPER INTERFERENCE FIT OF 0.0005 - 0.0015 IAW EA 8-5310-123556. INSTALLED BUSHING IAW SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123556.

Part: COVER — CRACKED (BS 1256 S16-17L) · airframe 77,094 hrs · 31,271 cycles

MAIN CABIN INTERIOR COVER PLATE IS CRACKED AT BS 1256, FROM STRINGER 16L TO STRINGER 17L. REMOVED AND REPLACED COVER PLATE IAW SRM 51-33-01, VOL II AND SRM 53-50-00, FIG 19, VOL I.

Part: HANDLE — MALFUNCTIONED (ZONE 200) · airframe 76,711 hrs · 31,104 cycles

ON FINAL, GEAR HANDLE PLACED DOWN & PRIMARY INDICATIONS WERE ALL THREE RED AND ALL THREE GEAR SHOWED RED ON CONFIG PAGE. RETRACTED GEAR & RAN QRH. ALL GEAR THEN EXTENDED NORMALLY. SUSPECT GEAR HANDLE NOT ALL THE WAY IN ON FINAL. ALL INDICATIONS OPS CK NORMAL REF PER MM 32-60-00-0. FOUND LARGE AMOUNT OF DUST IN LANDING GEAR LEVER ASSY. GEAR HANDLE SLIDER WAS SLOW TO RETRACT, CAUSING THE GEAR UNSAFE LIGHTS(RED)TO STAY RED. CLEANED DUST/DEBRIS FROM SLIDER AND SWITCHES FROM LEVER ASSY. LUBED SLIDER ON GEAR HANDLE. INSTALLED GEAR PINS AND CHECKED POSITION LIGHT WITH GEAR HANDLE- ALL CHECKS GOOD. GEAR PINS REMOVED.

Part: DOOR FRAME — CORRODED (BS 1817-1821) · airframe 71,660 hrs · 28,745 cycles

EXFOLIATING CORRSIONON P/N AFA3931-501 CARGO DOOR JAMB LOWER FITTING STA 1875 TO 1821 FROM CLOGGED DRAIN HOLES. REMOVE CORROSION AND OPENED DRAIN HOLES IN AFT UPPER TORQUE BOX AT FS 1827 IAW MD/DC10 SRM 53-00-01 FIG 1B VOL II AND EA 8-5310-94486.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 70,702 hrs · 28,348 cycles

DURING FLIGHT EXPERIENCED EXHAUST SMELL IN COCKPIT AND MAIN CABIN. ATTEMPTED TO ISOLATE SOURCE BY TURNING OFF BLEEDS ONE AT A TIME FOR 5 MINUTES EACH. DID SAME FOR PACKS, SMELL CONTINUED. RETURNED TO MEMPHIS. REMOVED AND REPLACED ALL THREE A/C PACK WATER SEPARATOR BAGS. RAN ENGINES AT 40% N1 WITH ALL PACK ON FOR 15 MINUTES WITH NO ODORS. ALL THREE SOCKS REMOVED WERE EXTREMELY DIRTY. ACFT OK FOR CONTINUED SERVICE. CHECKED APU BLEED AIR DUCT FOR EVIDENCE OF OIL LEAK AND NO LEAKS NOTED. THEN PERFORMED AN ENGINE RUN AT POWER SETTINGS FROM IDLE TO MAX POWER WITH ALL PACKS RUNNING AND WITH PACKS ISOLATED WITH NO FUMES AT ANY TIME DURING A 45 MINUTE ENGINE RUN.

Part: FITTING — CORRODED (ZONE 700) · airframe 68,993 hrs · 27,587 cycles

WINGS-MAIN FRAME-DOOR ASSY-MLG STRUT WING FITTING ATTACH HOLE. COMPLIED WITH EA 8-5710-55481.

Part: HINGE — GOUGED (ZONE 800) · airframe 68,993 hrs · 27,587 cycles

COMPLY WITH EA 8-5240-55471, DOORS-SERVICE-TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011 LT. CLOSING ACTION ON 04/15/05. ON N/R S00013. COMPLIED WITH EA 8-5240-55471.

Part: HINGE — GOUGED (ZONE 800) · airframe 68,993 hrs · 27,587 cycles

COMPLY WITH EA8-5240-55472-DOORS-SERVICE-TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011 RT. CLOSING ACTION ON 04/15/05. ON N/R S00014. COMPLIED WITH EA 8-5240-55472.

Part: SKIN — BULGED (ZONE 500) · airframe 68,993 hrs · 27,587 cycles

COMPLY WITH EA 8-5750-55478,WINGS-LT INBD FLAP-UPPER SKIN BULGE REPAIR AT XIFH=183.3 (P/N ARC2369-503). BFM R COMPLIED WITH EA8-5750-55478-WINGS LT INBOARD FLAP, UPPER SKIN BULGE REPAIR AT XIFH 183.3 (P/N ARC2369-503).

Part: BRACKET — CHAFED (ZONE 700) · airframe 68,993 hrs · 27,587 cycles

COMPLY WITH EA8-5310-55469, FUSELAGE-MAIN FRAME-BRACKET ASSY NOSE RETRACT CHAFE REPAIR (P/NACA0007-1). CLOSING ACTION ON 04/12/05. ON N/R S00011. COMPLIED WITH EA8-5310-55469.

Part: FITTING — CORRODED (ZONE 600) · airframe 68,993 hrs · 27,587 cycles

COMPLY WITH EA8-5750-55470, WINGS-RT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR P/N ARC1984. CLOSING ACTION ON 04/12/05. ON N/RS00012. COMPLIED WITH EA 8-5750-55470.

Part: ENGINE — STALLED (NR 1) · airframe 68,867 hrs · 27,530 cycles

ON DESCENT FROM 36,000 TO 35,000 AND AGAIN DESCENT TO 34,000 FT NR 1 ENGINE COMPRESSOR STALLED AND N1, N2 WENT TO LESS THAN IDLE, RESTARTED EACH TIME AND HAD MUCH COMPRESSOR STALLS. ENGINE WAS THEN SHUT DOWN. BOROSCOPE INSPECTED NR 1 ENGINE FOR STALLS, FOUND DAMAGE IN 1ST STAGE HPC BLADES HAS TEARS AND EVIDENCE OF RUBBING ON LEADING EDGES, 3RD STAGE HAS TORN BLADE, 4TH STAGE HAS SEVERE TIP CLANG, ALSO 5TH STAGE HAS SEVERE TIP CLANG. REQUIRES ENG CHANGE. INFO 02MAR05 APPROVED THIS ENGINE FOR CHANGE DUE TO THE DAMAGE AND TIP CLANG.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 67,384 hrs · 26,834 cycles

HORIZONTAL STABILIZER CONSTANT SECTION AND OUTBOARD SKIN PANELS CRACKED. P/N ALC7442-1, ALC7206-1, ALC7208-1. PANELS REPLACEMENT/REPAIR PER SB 55-16 IAW FEDEX EA 8-5510-72225.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 65,131 hrs · 25,747 cycles

LEFT INBOARD FLAP OUTBOARD HINGE FITTING BOTTOM INBOARD ATTACH BOLT TO REAR SPAR BOX FITTING HAS RUST EMANATING FROM BETWEEN THE FITTING AND SPAR TANG.

Part: CONTROL VALVE — FAULTY (T/E FLAP) · airframe 64,764 hrs · 25,569 cycles

AFTER T/O 9L FLL FLAP TAPES REMAIN IN T/O POS WITH HANDLE 0 EX. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE PER MM 27-52-02-2.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 64,262 hrs · 25,375 cycles

ON T/O, A/C WOULD NOT HOLD PRESSURE.

Part: TRANSMITTER — DAMAGED (LEFT OUTBOARD)

00-350 ON LD FLAP INDICATOR SHOW LEFT INBD FLAP LESS THAN SEL AT 35 DEGREES POSITION. R&R LEFT OUTBOARD TRANSMITTER PER IAW DC10-10 MM 27-54-03-2. OK FOR SERVICE.