N359FE

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 86,515 hrs · 31,039 cycles

UPON ARRIVAL AFTER A/C WAS PARKED AT GATE WAS NOTIFIED BY FLT CREW THEY HAD A FIRE INDICATION IN THE FWD LWR CARGO COMPT BUT DID NOT DISCHARGE FIRE BOTTLE. HAVE FWD AGENT DISCH LIGHT FLASHING ON OVER HEAD PNL ALSO HAVE ON AIR PAGE DISCH CARGO AGENT. INSP'D LWR CARGO COMPT FIRE EXT'S IN CAC FOR DISCHARGE. NO DISCHARGE WAS FOUND AND BOTH BOTTLES ARE OK FOR CONT'D SVC AT THIS TIME IAW MM 22-26-01. RESET C/B'S FOR MSC AND PERFORMED ADJ/TEST FOR MSC IAW MM 31-42-01-5 NO FAULTS FOUND AT THIS TIME. ALSO PERFORMED RTS OF MSC AND NO FAULTS NOTED IN MSC. OVERHEAD FWD DISCH LIGHT AND DISCH CARGO AGENT LIGHTS WENT OUT. CARGO FIRE TEST WAS ACCOMPLIHED AND SYSTEM OPS CKS NORMAL ON GRND NOW. A/C IS OK FOR CONT'D SVC AT THIS TIME.

Part: LATCH — OUT OF ADJUST (RT MLG DOOR) · airframe 86,513 hrs · 31,037 cycles

AFTER LEVEL OFF AT FL 350 THE RIGHT MAIN PRIMARY AND SECONDARY INDICATIORS WENT RED WITH GEAR HANDLE UP. RAN QRH AND ALL LITES WERE GREEN WITH HANDLE DOWN. WHEN HANDLE RAISED IAW QRH LIGHTS ILLUMINATED. LIGHTS REMAINED ON WITH HANDLE UP UNTIL DESCENDING THRU ABOUT 12000 FT & 250 IAS. WHEN GEAR HANDLE LOWERED FOR LANDING, ALL PRIMARY & SECONDARY LIGHTS WERE GREEN. CHECKED RT MLG DOOR ACTUATOR ADJUSTMENT, CHECKED GOOD, INSTALLED, TORQUED, & SAFETIED ROD END BOLT IAW AMM 32-34-01-2, FOUND RT MLG DOOR LATCH SLIGHTLY TOUCHING HOOK, ADJUSTED LATCH IAW 32-34-03-2, R & R RT GEAR UP & DOOR LATCH PROX SENSORS IAW 32-61-15-5, SWUNG GEAR, ALL NORMAL. PERFORMED EMERGENCY EXTENSION, OPS CHECKS NORMAL.

Part: SHEAR TIE — CORRODED (BS 825) · corrosion level 2 · airframe 86,256 hrs · 30,883 cycles

FWD CARGO BILGE STA 825 49R TO 50R CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP AT STA 825 STR 49R TO 50R IAW SRM 51-31-01. CORROSION FOUND OUT OF LIMITS IAW SRM 51-40-02. MAJOR REPAIR

Part: SHEAR TIE — CORRODED (BS 808) · corrosion level 2 · airframe 86,256 hrs · 30,883 cycles

FWD CARGO BILGE AREA AT STA 808 SHEAR CLIP SECTON CORRODED AND ANGLE. REMOVED CORROSION FROM SHEAR CLIP AND ANGLE CLIP FOUND TO BE OUT OF LIMITS IAW SRM 51-40-02. REMOVED AND REPLACED BOTH SHEAR CLIPS AND ANGLE CLIP AT STA 808 48R TO 47R IAW SRM 51-31-01. MAJOR REPAIR

Part: SKIN — CORRODED (BS 1197-2007) · corrosion level 2 · airframe 86,256 hrs · 30,883 cycles

WASTE TANK COMPARTMENT STA 1997-2007 LONGERON 46R - 47R FUSELAGE SKIN HAS CORROSION REMOVED CORROSION IAW SRM 53-20-00 FIG 4 OUT OF LIMITS FABRICATED AND INSTALLED DOUBLER REPAIR. IAW SRM 53-20-00 FIG 4 AT STA 1997 - 2007. CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1191-1531) · airframe 86,256 hrs · 30,883 cycles

MAIN DECK COMPARTMENT STA 1191-1531 SEAT TRACK X=75.25 HAS SCRATCHES AND GOUGES AS MARKED. REPAIRED MAIN DECK COMPARTMENT STA 1191 - 1531 X= 75.25 IAW SRM 53-70-00 FIG 1. (SEAT TRACK REPLACED). MAJOR REPAIR

Part: SKIN — CHAFED (FWD CARGO DOOR) · airframe 86,256 hrs · 30,883 cycles

LOWER FWD CARGO DOOR AFT FRAME SIDEWALL HAS CHAFE MARK. REMOVED AND REPLACED DOUBLER AND TRIPLER PER SRM 53-50-00. CAT "A" MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 86,256 hrs · 30,883 cycles

WASTE TANK COMPARTMENT STA 2007 CEILING AREA BL0 FLOOR STRUCTURE HAS CORROSION REMOVED FLOOR SUPPORT IAW SRM 51-31-01. CHECK LIMITS. EXCEEDS 10% ALLOWABLE DAMAGE IAW SRM 53-00-01 FIG 1A. LOCATED AND DRILLED NEW FLOOR SUPPORT P/N WSP0711-543 BATCH # 0003397793. INSTALLED FLOOR SUPPORT IAW SRM 51-31-01. MAJOR REPAIR

Part: CHAIN — MISSING (L1 DOOR) · airframe 86,256 hrs · 30,883 cycles

L1 DOOR EMERGENCY PNEUMATIC ACTUATION CHECK FAILED. FOUND L1 EMERGENCY AIR MOTOR CHAIN MISSING. REPLACED CHAIN IAW CMM 52-11-09. PNEUMATIC TEST CHECK GOOD IAW AMM 52-10-01-2

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 86,256 hrs · 30,883 cycles

AFT CARGO SEAT TRACK UPPER SURFACE HAS SCRATCHES, GOUGES, AND CORROSION AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 CAT "A" MAJOR REPAIR. SEAT TRACK FOUND OUT OF LIMITS FOR CRACK.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 86,256 hrs · 30,883 cycles

MAIN CARGO SEAT TRACK AT STA 999 POSITION X=-47.5 HAS MULTIPLE GOUGES. REMOVED DAMAGE ON SEAT TRACK STA 999 X= -47.5 IAW SRM 53-70-00 FIG 5. CHECKED LIMITS. MAXIMUM MATERIAL REMOVE IS .025 AFTER REWORK MATERIAL LOSS IS .045 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. FABRICATED NEW SEAT TRACK SECTION STA 979 TO 1039 P/N S49291507075-T6511 IAW SRM 57-70-00 FIG 1. INSTALLED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1. MAJOR REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,256 hrs · 30,883 cycles

AFT CARGO DOOR SILL LOWER SURFACE HAS CORROSION UNDER NUT PLATES 5 PLACES. REMOVED AND REPLACED AFT CARGO DOOR SILL LOWER SURFACE IAW SRM 51-31-01 AND SRM 51-35-01. MAJOR REPAIR.

Part: FIRE — DETECTED (APU) · airframe 86,251 hrs · 30,878 cycles

APU TAIL PIPE FIRE. SMOKE REPORTED BY OTHER AIRCRAFT. FIRE CRASH RESCUE INSPECTED AND FOLLOWED BACK TO RAMP. AFTER BLOCK IN AND CREW DEBRIEF INSPECTED AFT ENG AND APU COMPARTMENT. WITH NO SMOKE OR DAMAGED NOTED, BUT COULD SMELL A SMOKE ODOR. RESTARTED APU, DURING APU START, HAD AN EXHAUST PIPE FLAME. ABORTED START AND PULLED APU FIRE HANDLE. DID NOT DISCHARGE AGENT. INSPECTED APU AREA FOR FIRE DAMAGE, NO DAMAGE NOTED. RESET ALL PULLED C/B FOR APU RUN . STARTED APU 4 TIMES LAST 2 STARTS NO FLAMES RAN IAW JRH GOT A FLAME AT APU START 2 TIMES FLAME EXTINGUISHES IMMEDIATELY, NO EGT SPIKE NO ERRATIC FUEL FLOW, APU ISOLATION VALVE ON AIR FLOW OPS CHECKS NORMAL PACKS OPS CKS NORMAL EGT STAYS WITHIN LIMITS 394-398 C WITH ALL 3 PACKS RUNNING. NO HISTORY IN THE LAST 30 DAYS A/C OK FOR SERVICE IAW M/M 49-00-00-5.

Part: PITOT TUBE — DIRTY (PITOT/STATIC SYS) · airframe 85,902 hrs · 30,651 cycles

"SEL ELEV FEEL MAN" AND "SEL FLAP LIMIT OVRD" LVL MSGS CAME UP AFTER T/O. WE RAN AND COMPLIED WITH QRH. FO AIRSPEED WAS UNRELIABLE. FOUND BOTH CAPTAINS AND FO'S PITOT TUBES TO HAVE PLUGGED DRAIN HOLES. REMOVED AND REPLACED BOTH IAW MM 34-11-02-2. ALSO REF EA 8-3410-T0341438 FOR INCLUSION FOR USE OF P/N 851DK PITOT TUBE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 85,766 hrs · 30,566 cycles

EMER LT BAT 1 LO. T/S USING FIM 33-50-00-810 FOUND EMERG PWR SUPPLY AT FAULT. REMOVED AND REPLACED PWR SUPLY IAW MM 33-51-01-4 AND OPS CHECK PER 33-51-01-5 OPS VERIFED NORMAL. A/C OK FOR SERVICE.

Part: SKIN — NICKED (LT WING TE FLAP) · airframe 83,611 hrs · 29,328 cycles

LEFT WING INBD FLAP LOWER SURFACE NICKED. REPAIRED LOWER FLAP SKIN IAW SRM 57-10-00 FIG 85. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 83,611 hrs · 29,328 cycles

MAIN DECK CARGO BS 1501, RBL 68 FLOOR PANEL DELAMINATED & DENTED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,611 hrs · 29,328 cycles

MAIN DECK AREA LEFT SIDE BETWEEN STATION 1401-1421 STRINGER 19L LONGERON HAS CORROSION. LONGERON FOUND OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 1B. REMOVED AND REPLACED LONGERON IAW SRM VOL II 51-33-01 AND 51-31-01 AND DRAWING AEA0222. LONGERON FABRICATED ON T16/1236697 IAW DRAWING AEA0222. REPLACED LONGERON 19L AT STA 1401-1421. MAJOR REPAIR.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,611 hrs · 29,328 cycles

MAIN DECK AREA LEFT SIDE BETWEEN STATION 1381-1401 STRINGER 17L LONGERON HAS CORROSION. LONGERON FOUND OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 1B. REMOVED AND REPLACED LONGERON IAW SRM VOLII 51-31-01 AND 51-33-01 AND DRAWING AEA 0220-1. LONGERON FABRICATED ON T16/1236701 IAW DRAWING AEA 0220-1. ORIGINAL LONGERON THICKNESS .090 AFTER REWORK .071, OUT OF LIMITS IAW SRM 53-00-07. INSTALLED NEW LONGERON STA 1381-1401 STR 17L IAW SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1841) · corrosion level 2 · airframe 83,611 hrs · 29,328 cycles

BROKEN NUTPLATES AND CORROSION UNDER NUTPLATES AT AFT CARGO FLOORBEAM UPPER TEE BS 1841 LT TO RT END. REMOVED CORROSION IAW SRM 51-00-01. AND FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR IAW SRM 53-00-01 FIG. 7. INSTALLED THE REPAIR IAW SRM 51-31-01. MAJOR REPAIR.

Part: LONGERON — CORRODED (BS 1321-1341) · corrosion level 2 · airframe 83,611 hrs · 29,328 cycles

MAIN DECK AREA, LT SIDE BETWEEN BS 1321 AND 1341 LONGERON 17L HAS CORROSION. REMOVED THE CORROSION IAW SRM 51-21-01 VOL II. FOUND OUT OF LIMITS IAW SRM 51-00- 01 VOL I. REMOVED AND REPLACED THE LONGERON IAW SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 83,598 hrs · 29,319 cycles

DURING ENGINE SHUTDOWN WE RECEIVED A FIRE WARNING IN THE LOWER FORWARD CARGO COMPARTMENT. FIRED THE AGENT. THERE WAS NO EVIDENCE OF A FIRE/SMOKE IN THE FWD LOWER COMPARTMENT. THERE WAS A OVERVOLTAGE MSG IN THE EPCU CURRENT FAULTS. FIREX DISCHARGE SQUIB MPN: 876296-3 CPN: 0028922.

Part: SKIN — CRACKED (BS 1871) · airframe 82,791 hrs · 28,884 cycles

DURING WALK AROUND, FOUND WHAT APPEARS TO BE 1/2 CRACK & PUNCTURE IN FUSELAGE, LOCATED ABOUT 8 FEET AFT OF AFT LOWER CARGO DOOR. CRACK & PUNCTURE IS PROTRUDING OUTWARD. REMOVED CORROSION DAMAGE IAW SRM 53-20-00. REQUIRES HFEC OF CUT OUT AREA TO INSURE ALL DAMAGE IS REMOVED IAW SRM 53-20-00. PERFORMED HFEC OF REMOVED DAMAGE AREA IAW NTSPM 06-10-01 001 PROCEDURE 1 NO ADDITIONAL DEFECTS NOTED. INSTALLED REPAIR DOUBLER & TRIPLER IAW SRM 53-20-00 REF EA 8-5330-T0323644 & ERS 16-01113. ACFT RETURNED TO SERVICE IAW EA 8-5330-T0323644 P1.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 82,483 hrs · 28,732 cycles

DURING COCKPIT SET UP, HAD FWD AGENT DISCHARGE LIGHT FLASHING ALONG WITH DISCHARGE AGENT ON EAD, FOLLOWED BY FIRE ALERT. FIRED BOTH BOTTLES, ACFT WAS LOADED UNABLE TO VERIFY. TROUBLE SHOT & FOUND THAT THE MSC SOFTWARE HAD GLITCHED. PULLED & RESET CB'S FOR MSC. MSC OPERATION RTS PASSED IAW MM 31-42-01-5. R & R BOTH CARGO FIRE EXTINGUISHER CONTAINERS IAW MM 26-22-01-4. OPERATIONS CHECKED NORMAL.

Part: PANEL — DAMAGED (L1 DOOR) · airframe 814 hrs · 28,139 cycles

SMALL DAMAGE, APPROX 1.5" X 1.5", FOUND ON UPPER AFT SIDE OF COVER PANEL INSIDE OF L1 DOOR. REPAIRED DAMAGE TO L1 DOOR COVER.

Part: FUSE — CRACKED (HYD SYSTEM) · airframe 81,047 hrs · 27,904 cycles

HYD 3 FAIL LEVEL 2 AFTER GEAR DOWN ON APPROACH, ALL HYD FLUID EMPTIED & LEAKED FROM HYD SYS 3 AFTER GEAR LOWERED. PUMPS NOT TURNED OFF. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM32-31-06-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK SEAT TRACK AT STATION 1140 RBL 48 HAS DAMAGE. R & R NEW SEAT TRACK IAW SRM 53-70-00 FIG 2.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL STATION 1401 - 1421 L17 LONGERON HAS EXFOLIATION CORROSION. REPLACED LONGERON AEA0220-521 IAW DWG AZA0220.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL STATION 1361 - 1381 L17 LONGERON HAS EXFOLIATION CORROSION. REPLACED LONGERON AEA 0220-503 IAW DWG AZA0220.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL STATION 1381 - 1401 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL STATION 1441 - 1461 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL STATION 1461 - 1481 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 80,965 hrs · 27,856 cycles

LEFT LG WELL HYD LINE SUPPORT, CRACK IS EMANATING FROM MOUNT BOLT LOCATED FWD OF THE GEAR STRUT UP STOP. REMOVED CRACKED BRACKET & INSTALLED A NEW SERVICEABLE BRACKET IAW SRM 51-31-01 VOL II.

Part: STRUCTURE — CRACKED (NR 2 NACELLE) · airframe 80,965 hrs · 27,856 cycles

NUMBER 2 ENG INLET NOSE COWL CRACKED AT INNER STRUCTURE BETWEEN 3 & 4 O'CLOCK POSITION. R & R NOSE COWL IAW AMM 54-22-01-2.

Part: WEB — CRACKED (BS 1841) · airframe 80,965 hrs · 27,856 cycles

CENTER CARGO BS 1841, RT WEB HAS SMALL CRACK. REMOVED, FABRICATED & INSTALLED NEW WEB.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,965 hrs · 27,856 cycles

MAIN DECK RT SIDEWALL LONGERON 17, EACH FRAME BAY HAS A SEPARATE LONGERON, CORRODED, A TOTAL OF 10 LONGERONS FROM STATION 1159 TO 1481. REMOVED CORROSION WITHIN LIMITS PER SRM 53-00-01 FIG 1B AND REPLACED LONGERONS THAT EXCEEDED LIMITS IAW BLUEPRINT SPECIFICATIONS. REF SDR 14-2677, 14-2993, AND 14- 2994 FOR NR'S 366, 368, AND 366.

Part: SKIN — GOUGED (LE SLAT) · airframe 80,965 hrs · 27,856 cycles

LEFT WING NR 4 SLAT LOWER TE SURFACE HAS DEEP GOUGE BY NR 9 TRACK. REPAIRED GOUGE IAW SRM 57-00-01 FIGURE 4 SHEET 2.

Part: FRAME — CORRODED (BS 970) · airframe 80,965 hrs · 27,856 cycles

FORWARD CARGO BILGE CORROSION AT BS 970 STRINGER 51L. REMOVED AND REPLACED THE FRAME IAW DWG ADA0078 AND SRM 53-10-00 FIG. 2 VOL 1.

Part: LONGERON — CORRODED (BS 979) · airframe 80,965 hrs · 27,856 cycles

FORWARD CARGO BILGE BS 979 LONGERON 51L HAS CORROSION. REPAIRED LONGERON 51L IAW SRM 53-10-00 FIG 2 VOL 1

Part: LONGERON — CORRODED (BS 1481-1501) · airframe 80,965 hrs · 27,856 cycles

MAIN DECK BS 1481 - 1501 LONGERON 18R HAS CORROSION. REMOVED CORROSION WITHIN LIMITS IAW SRM 53-00-01 FIG 1B

Part: FRAME — CORRODED (BS 1781) · corrosion level 2 · airframe 80,965 hrs · 27,856 cycles

CENTER CARGO BILGE FRAME HAS CORROSION AT BS 1781 JUST ABOVE LONGERON 45R, BENEATH AFT END OF ROLLER TRAY. REPAIRED IAW SRM 53-60-01 AND SRM 53-60-01.

Part: SKIN — CORRODED (BS 1841) · airframe 80,965 hrs · 27,856 cycles

AFT CARGO BAY BILGE BS 1841, SKIN HAS A LIGHT SURFACE CORROSION AROUND FINGER DOUBLER BETWEEN L47-48R. CLEANED CORROSION IAW SRM 51-21-01 VOL II. PERFORMED UT NDT INSPECTION & VERIFIED REMAINING MATERIAL THICKNESS FOUND TO BE WITHIN IAW SRM 53-20-00 VOL 1.

Part: SKIN — CORRODED (BS 1841) · airframe 80,965 hrs · 27,856 cycles

AFT CARGO BAY BILGE, CORROSION FOUND BETWEEN LONGERON 47-48R BS 1841. CLEANED & TREATED SURFACE CORROSION IAW SRM 51-21-01 VOL II. PERFORMED UT NDT & VERIFIED REMAINING MATERIAL FOUND TO BE WITHIN LIMITS IAW SRM 53-20-00 VOL 1 FIG 13 SHEET 28.

Part: FRAME — CORRODED (BS 1841) · airframe 80,965 hrs · 27,856 cycles

CENTER CARGO BILGE FRAME HAS CORROSION AT BS 1841 JUST ABOVE LONGERON 46L. REMOVED CORROSION IAW SRM 51-21-01, VOL II

Part: PUMP — BYPASSING (CARGO HEAT) · airframe 80,373 hrs · 27,552 cycles

NR 2 AIR MANIFOLD FAIL ILLUMINATED AT 17,000 FT DURING CLIMB OUT WITH CLIMB POWER SET. FOLLOWED QRH PROCEDURE, LIGHT EXTINGUISHED WITH THROTTLE RETARDED BELOW 95%. PERFORMED NR 2 PNEUMATIC SYS DECAY CHECK IAW MM 36-00-01-5, SYS FAILED TEST. SHOULD BE 20 SECONDS TO DECAY FROM 20 PSI DOWN TO 15 PSI, IT ONLY LASTED 9 SECONDS. FOUND AFT CARGO HEAT JET PUMP VALVE BYPASSING INTERNALLY, REMOVED & REPLACED THE VALVE IAW MM 21-41-04-4. OPS CHECKED NORMAL, DECAY PASSED BY 30 SECONDS.

Part: PRECOOLER — LEAKING (NR 2 ENGINE) · airframe 80,353 hrs · 27,540 cycles

AIR MANIFOLD NR 2 FAIL, PERFORMED DECAY CHECK IAW AMM 36-00-02-5 & 36-00-01-5 WITH APU & NR 2 ENG, BUT STILL FAILED. CHECKED NR 2 PACK FLOW CONT VALVE, FWD, CENTER & BULK CARGO BAY JET PUMPS, SHUTOFF VALVES & DUCTING, NR 2 START VALVE & DUCTING, NR 2 ENG BLEED VALVE, PRESSURE REGULATOR, THRUST REVERSER OVER PRESSURE SHUTOFF VALVE, MOTORCYCLE VALVE & DUCTS, NO LEAK NOTED. WHILE NR 2 MANIFOLD WAS PRESSURIZED, IN THE PROCESS OF CHECKING THE PRE COOLER ABOVE NR 2 ENGINE FOR LEAKS. COMPLETED INSTALLATION OF NR 2 ENGINE PRECOOLER ASSEMBLY IAW MM 36-12-01-4, LEAK CHECKED GOOD ON GROUND IAW MM 36-10-00 & 36-13-01-4, NO LEAKS NOTED, ACFT OK FOR SERVICE.

Part: SHEAR TIE — CORRODED (BS 1975 L50 L-R) · airframe 78,370 hrs · 26,434 cycles

AFT WASTE TANK AREA, STA 1975 BETWEEN LONGERON 50 AND 50 RT SHEAR TIE SHOWING EXFOLIATION. REMOVED CORRODED SHEAR TIE AND REPLACED WITH NEW SHEAR TIE IAW SRM 51-21-00 VOL II.

Part: FIRE BOTTLE — LOW (NR 3 NACELLE) · airframe 78,262 hrs · 26,377 cycles

ENGINE FIRE AGENT LOW, AT GATE AFTER ENGINE SHUTDOWN. REMOVED AND REPLACED NR 3 ENGINE FIRE DISCHARGE BOTTLES IAW MM 26-21-01-4. PERFORMED ALL ADJ/TEST'S PER MM 26-21-06/ 26-21-01. FOUND BRACKET BROKEN ON PNEUMATIC BLEED DUCT CAUSING UNRESTRAINED FLEX DUCT JOINT SEAL HOUSING TO LEAK. DUCTS SEPARATED BEYOND THE NORMAL RANGE. REPLACED BROKEN STANDOFF BRACKET.

Part: FILTER — CONTAMINATED (SCAV PUMP) · airframe 76,022 hrs · 25,190 cycles

ABOUT 10 MINS AFTER T/O, NR1 ENG OIL QTY DECREASED TO 0. PRESS AND TEMP REMAINED NORMAL FOR ABOUT 10 MINS. THEN PRESS DECREASED AND INCREASED OUT OF NORMAL RANGE. SHUT ENG DOWN BEFORE PRESS REACHED RED LINE AND OR TEMP HIT YELLOW LINE. FOUND TGB SCAV IN FILTER SCREEN CLOGGED WITH PHENOLIC MATERIAL. REMOVED AND REPLACED NR 1 ENGINE IAW WORK CARDS 71T0101-1 AND 71T0701-1. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.

Part: TRANSMITTER — FAILED (ENGINE OIL) · airframe 76,019 hrs · 25,188 cycles

OIL QUANTITY DROPPED TO ZERO AFTER TAKEOFF ON ENGINE 1, OIL PRESSURE STARTED FLUCTUATING -10-20 PSI AND OIL TEMP CLIMBED TO 130 (NR2 100, NR3 105. SHUTDOWN ENGINE AND RETURNED. DID NOT NOTICE OIL PRESSURE ON WINDMILLING ENGINE. DURING 20 MIN OF FLIGHT BACK IN. RELEASED FOR SERVICE IAW MEL: 79-31-01, CATEGORY: B EXPIRATION: 23NOV10 "MEL 79-31-01: ENG NR 1 OIL QTY INDICATION- INOP. BEFORE EACH TAKEOFF, SERVICE OIL TANK TO FULL AND RECORD IN AML/EAML." R& R AND INSPECTED SCAVENGE OIL FILTER IAW MM 79-20-02-2. INSPECTED SCAVENGE INLET STRAINERS AND CHIP DETECTORS IAW MM 79-20-05-2. ALL CLEAN, NO METAL. IAW REQUEST R & R OIL PRESSURE TRANSMITTER IAW MM 79-33-01-2-0, AND ALSO OIL QTY TRANSMITTER IAW MM 79-31-01-2-0. RAN ENGINE IAW JRH, LEAK AND OPS CHECK NORMAL. OK FOR SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 75,840 hrs · 25,104 cycles

DURING TEST FLIGHT AT 15,500' & 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT AND EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/RED TABS AND MADE UNEVENTFUL LANDING. SDR CLOSED DUE FILED PREVIOUSLY, SEE SDR 10-4074 AND 10-4075.

Part: DRIVE SYSTEM — CRACKED (SLATS) · airframe 75,840 hrs · 25,104 cycles

DURING TEST FLIGHT AT 15,500'& 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT & EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/RED TABS AND MADE UNEVENTFUL LANDING. FOUND LH OB SLAT DRIVE MECHANISM FAILED AND HYDRAULIC LINES RUPTURED.REMOVED AND REPLACED LT OB SLAT DRIVE MECHANISM IAW AMM 27-83-02-1. REPAIRED HYDRAULIC LINES IAW AMM 20-10-01-2 ON SNR S0009 WRI 29-10/7212.MINOR REPAIR.LEAK AND OPS CHECKS GOOD.

Part: SLAT SYSTEM — MALFUNCTIONED (LE SLATS) · airframe 75,840 hrs · 25,104 cycles

DURING TEST FLIGHT AT 15,500' AND 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT & EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/RED TABS AND MADE UNEVENTFUL LANDING.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 75,837 hrs · 25,100 cycles

LT DROOP ELEVATOR FWD LATCH BROKEN. REMOVED AND REPLACED 2 BROKEN LATCHES P/N H2188-1 IAW SRM 51-31-01. FOUND CRACK ON LOWER SKIN, TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 2024 T3 .050 BATCH NR 1795T93 IAW SRM 55-00-01 FIG 3 AND SRM 55-22-01 FIG. 9. INSTALLED REPAIR DOUBLER IAW SRM 51-31-01.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 75,837 hrs · 25,100 cycles

LEFT OUTBD FLAP UPPER SKIN IS DAMAGED, LOCATED OUTBD OF CENTER HOIST POINT. REMOVED AND REPLACED LEFT OUTBD FLAP UPPER SKIN IAW SRM 51-31-01 AND SRM 57-10- 00, MAJOR REPAIR, THIS IS CLASS B REPAIR AND REQ. REPECTIVE INSP IAW SRM 57-10-00 FIG. 7, SHEET 2.

Part: FITTING — CHAFED (NR 2 NACELLE) · airframe 75,837 hrs · 25,100 cycles

INSIDE NR 2 PRECOOLER COMPARTMENT, RIGHT SIDE FRAME SUPPORTS CHAFED. BLENDED FRAME SUPPORTS PER SRM 54-20-00 AND E.A. 8-5450-142268. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 75,837 hrs · 25,100 cycles

THE LT WING OTBD FLAP , SECOND FROM INBD WEDGE SEGMENT UPPER SKIN, HAS AN APPROX 2" LONG CRACK IN THE FWD MID SECTION AT APPROX STA OF 565.

Part: SEAT TRACK — GOUGED (BS 1688) · airframe 75,837 hrs · 25,100 cycles

SEAT TRACK LBL 48 BETWEEN FS 1688 HAS A GOUGE ON CROWN AREA. FABRICATED SEGMENT OF SEAT TRACK ON TRAVELER T10/853974 AND REPAIR PARTS ON TRAVELER T10/853972. INSTALLED SEAT TRACK AND REPAIR IAW SRM 53-70-00. CLASSIFED AS A MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1389) · airframe 75,837 hrs · 25,100 cycles

SEAT TRACK LBL 48 AT FS 1389 HAS SHARP EDGES ON BOTTOM PORTION OF CROWN. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-70-00. FABRICATED NEW SEAT TRACK SECTION ON TRAVELER T10/853975 AND REPAIR PART ON TRAVELER T10/853973. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,837 hrs · 25,100 cycles

CENTER CARGO COMPARTMENT VHF-3 ANTENNA MOUNT CORRODED AND SURROUNDING SKIN. BLENDED AREA IAW SRM 51-21-01 ORIG. MAT. .071 AFTER REWORK .066. .005 MAT LOSS IS WITHIN LIMITS IAW SRM 53-00-01. CLASSIFIED AS A MINOR REPAIR.

Part: FRAME SPLICE — CRACKED (BS 1996 L27L) · corrosion level 2 · airframe 75,837 hrs · 25,100 cycles

UPPER CABIN, LONGERON 27L, FRAME SPLICE 1996L HAS COOROSION AND CRACKS THROUGH FASTENERS. CLEANED AREA AT FRAME SPLICE STA. 1996 AND LONGERON 27L IAW AMM 12-22-02-7. PERFORMED HFEC INSPECTION IAW NTSM 06-10-01. NO CORROSION OR CRACKS FOUND. NO REQUIREMENT FOR SDR REPORTING.

Part: WIRE — DAMAGED (INTERFACE UNIT) · airframe 74,840 hrs · 24,609 cycles

ACFT AIR TURNBACK, NR 2 EGT SHOWED AMBER "X"ON CLIMBOUT. SPORADICALLY CAME BACK WITH ERRATIC READINGS. RTB AFTER CONFORMATION WITH MOCC. REMOVED AND REPLACED AIU'S 1 & 3. WAITING HIGH POWER RUN. REPAIRED WIRE 2H2704F22 GOING TO R5-8212 PIN B WITH BLUE SPLICE IAW SWP MANUAL. WIRE HAS TEMP REPAIR IAW EA 8-7720-137795 AND WILL HAVE PERMANENT REPAIR DURING NEXT C CHECK.

Part: DIVERTER — BENT (APU DOOR) · airframe 70,584 hrs · 22,623 cycles

PDIS: ADVISED BY GROUND MARSHALLER APU DOOR WAS OPEN AT BLOCK IN. DURING POST FLIGHT WALK AROUND NOTICED APU ACCESS DOOR WAS OPEN. LANDING WAS SMOOTH. FACT: INSPECTED DOOR AND DOOR LATCH'S ASSY,REF AMM 52-45-01-2. LATCH ASSY'S CK NORMAL. DOOR TRAILING EDGE FAIRING IS BENT AND INTERFERRING WITH CLOSING OF DOOR. SHEET METAL DEPT REPARIED FAIRING. DOOR CLOSES AND LATCHES NORMALLY. RETURNED TO SERVICE.

Part: PRESSURE SENSOR — FAULTED (PNEUMATIC SYS) · airframe 68,785 hrs · 21,882 cycles

NR 2 MANIFOLD FAIL LEVEL ONE ALERT AFTER TAKEOFF. PERFORMED NR 2 PNEUMATIC SYSTEM DECAY CHECK PER MD-10-10 AMM SUPP 36-00-01-5. DECAY CHECK PASSED WITH 23-25 SECONDS. ITEM PLACED ON MEL. REMOVED AND REPLACED NR 2 PNEUMATIC REGULATING PRESSURE SENSOR, RTS PSC 2. RETURNED TO SERVICE.

Part: SKIN — DAMAGED (WING) · airframe 68,161 hrs · 21,613 cycles

NUMEROUS SCRATCHES AND SEVERAL DENTS TO THE ARB0934-1 AND ARB0933-1 LOWER SKIN PANELS AS WELL AS STRINGER 34L STA XORS 919 AND STRINGER 52L DENTED AT XORS 883. DENTS IN STRINGERS REPAIRED PER EA 8-5710-91321. WNGS - DENTS IN STRINGER 34L AT STA XORS 919 AND 52L AT STA XORS 883. DENTS IN LOWER SKIN PANELS ARB 0934-1AND ARB0933-1 REPAIRED PER EA 8-5710-91319. WINGS - LOWER SKIN DAMAGE BETWEEN XORS 845 AND 933 - REPAIR.

Part: SKIN — DENTED (BS 1975-1986) · airframe 68,161 hrs · 21,613 cycles

LT FUSELAGE SKIN 20" AFT OF AFT PIT DOOR HAS 3 EACH DENTS FS1975-1986, LONGERON 37L-38L. REPAIRED FUSELAGE SKIN IAW DC10 SRM 53-20-00 VOL II. SEE FEDEX SNRM N00137 OF WORK ORDER 00031297.

Part: SKIN — DENTED (ZONE 100) · airframe 68,161 hrs · 21,613 cycles

RIGHT PRIMARY STATIC PORT CONTROLLED AREA AT 5 O'CLOCK 10 INCHES FAILED MISMATCH. READS .0115 INCH. REWORKED DENT AREA AND FABRICATED INTERNAL REPAIR DOUBLER IAW DC10 SRM 53-20-00 FIG 13 VOL I. ALODINED AND PRIMERED IAW DC10 SRM 51-21-01 VOL II. PERFORMED RVSM WAVINESS CHECK ON REWORKED AREA IAW MD10-10 MM 34-11-01-02, FOUND TO BE WITHIN TOLERANCE. SEE FEDEX SNRM N00116 OF WORK ORDER 00031297.

Part: FLOOR SUPPORT — CRACKED (BS 1521) · airframe 68,161 hrs · 21,613 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT STRUCTURE AT FS1521, L46L-44L, SUPPORT ANGLE CRACKED. FABED NEW ANGLE IAW DAC DRAWING AEA0341-15. REPLACED IAW SRM 51-35-01 VOL II. ALODINED AND PRIMERED IAW SRM 51-1-21 VOLII. SEE SNRM N00525 OF WORK ORDER 00031297.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,161 hrs · 21,613 cycles

FUSELAGE SKIN DENTED FS 1810 L30R DOT J7004. REWORKED DENT IAW DPS 2.70 AND DC10 SRM 51-10-00 VOL 1. ENETRANT INSPECTION IAW DPS 4.707 NO DEFECTS FOUND. REMOVED GOUGE IAW DC10 SRM 53-00-01 VOL II. ORIGINAL THICKNESS .071 2024-T3. REMAINING THICKNESS .064 FOUND WITHIN LIMITS IAW DC10 SRM 53-35-01 VOL III. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II.

Part: STRUCTURE — CRACKED (SPOILER) · airframe 68,161 hrs · 21,613 cycles

LT WING NR 1 SPOILER TRAILING EDGE CRACKED LATERALLY OB AND AFT OF ACTUATOR. REMOVED AND REPLACED LT WING NR 1 SPOILER PANEL IAW MD10MM 27-60-01-4. CHECKED CLEARANCES IAW MD10-MM 27-60-01-6. SEE SNRM N00298 OF WORK ORDER NR 00031297.

Part: RADOME — DELAMINATED (FUSELAGE) · airframe 68,161 hrs · 21,613 cycles

RADOME, DELAMINATED/SWELLING ON INTERNAL SKIN FS 239. REMOVED AND REPLACED RADOME IAW MD10-10 MM 53-51-00-2 AND 20-50-02-2. SNRM N00335 OF WORK ORDER NR 0031297.

Part: SKIN — GOUGED (ZONE 100) · airframe 68,161 hrs · 21,613 cycles

LOWER FUSELAGE, FWD CARGO DOOR CUTOUT HAS FOREIGN OBJECT DAMAGE TO SKIN AT AFT CORNER, LONGERON 39R TO 42R STA 959. REPAIRED DAMAGED AREA IAW DC10 SRM 53-50-00 FIG 26 VOL I SHEET 3.

Part: SKIN — DENTED (FLAP LE) · airframe 68,161 hrs · 21,613 cycles

DENT ON RIGHT HAND INBOARD FLAP LEADING EDGE AT XIFH 174-179. REPAIRED LEADING EDGE SKIN IAW DC10-10 SRM 57-00-01 FIG 4 VOL I. ALODINED AND PRIMERED IAW DC10-10 SRM 51-21-01 VOL. II. SEE FEDEX SNRM NR N00291 OF WORK ORDER NR 00031297.

Part: SKIN — DENTED (ZONE 600) · airframe 68,161 hrs · 21,613 cycles

RIGHT WING OUTBOARD FLAP LOWER SKIN, DENT AT XFS 651, 6 INCHES FROM AFT EDGE IS OUT OF LIMITS. REPAIRED IAW DC10 SRM 57-10-00 FIG 85 VOL I MECH. 2668 QC316 SEE FEDEX NON ROUTINE NR N00598 OF WORK ORDER 00031297.

Part: BALANCE WEIGHT — CORRODED (RT WING) · airframe 68,161 hrs · 21,613 cycles

RIGHT WING OUTBOARD AILERON BALANCE WEIGHT CORRODED. REMOVED AND REPLACED BALANCE WEIGHT IAW DAC DC10 CMM 57-51-02. CALCULATED NEW BALANCE WEIGHT IAW DC10 SRM 57-50-00 VOL I, SEE FEDEX NONROUTINE NR N00245 OF WORK ORDER NR 00031297.

Part: SKIN — DENTED (ZONE 600) · airframe 68,161 hrs · 21,613 cycles

RIGHT WING FLAP LOWER SKIN, DENT AT XFS 535, 12" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00597 OF WORK ORDER NR 00031297.

Part: SKIN — DENTED (ZONE 500) · airframe 68,161 hrs · 21,613 cycles

LEFT WING INBOARD FLAP LOWER SKIN DENT FILLED WITH SEALANT AT XW234-238, 31" FWD OF TRAILING EDGE. FOUND DENT TO BE OUT OF LIMITS, REPAIRED SKIN IAW DC10 SRM 57-00-00 VOL I. SEE FEDEX NONROUTINE NR N00295 OF WORK ORDER 00031297.

Part: SKIN — DENTED (ZONE 600) · airframe 68,161 hrs · 21,613 cycles

RIGHT WING FLAP LOWER SKIN DENT AT XFS 674, 22" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00599 OF WORK ORDER 00031297.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 67,980 hrs · 21,534 cycles

AIR TURN BACK, GOT A RED LEVEL 3 CARGO SMOKE WARNING AT 18,000. RAN QRH PROCEDURE AND WARNING QUIT, WARNING RETURNED ON SHORT FINAL TO TPA, MEL: ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-03-A CATEGORY: C EXPIRATION: NR 4 MAIN DECK CENTERLINE SMOKE DETECTORS INOP. FOUND NR 4 MAIN DECK SMOKE DETECTOR INTERMITTENT. CAP AND STOW ELECTRICAL CONNECTOR. AS PER MEL. REMOVED AND REPLACED NR 4 MAIN CARGO DECK CENTERLINE SMOKE DETECTOR PER MD10-10 M/M REF 26-15-01-4. OPS CHECK GOOD.

Part: RIB — DAMAGED (ZONE 600) · airframe 65,410 hrs · 20,388 cycles

C/W EA 8-5750-80579 WINGS RT INBOARD FLAP VANE TRACK OVERSIZE HOLE REPAIR AT XIFH 216.3 (P/N ARC2966). COMPLIED WITH EA 8-5750-80579.

Part: FITTING — CORRODED (ZONE 600) · airframe 65,410 hrs · 20,388 cycles

C/W EA 8-5740-79557 WINGS RIGHT AILERON SUPPORT ASSY CORROSION REPAIR P/N ARC0317- 502. COMPLIED WITH EA 8-5740-79557.

Part: SUPPORT — CORRODED (TE FLAPS) · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK ON RIGHT O/B FLAP.

Part: FITTING — CORRODED (ZONE 500) · airframe 65,410 hrs · 20,388 cycles

WINGS-OUTBD AILERON, ACTUATOR ATTACH FITTING REWORK. CLOSING ACTION ON 07/16/04. ON N/R S00014, COMPLIED WITH EA8-5750-79553.

Part: FITTING — CORRODED (ZONE 500) · airframe 65,410 hrs · 20,388 cycles

C/W EA 8-5750-79553 WINGS OUTBOARD AILERON, ACTUATOR ATTACH FITTING REWORK. COMPLIED WITH EA 8-5750-79553.

Part: SUPPORT — CORRODED (RH WING) · corrosion level 2 · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR. COMPLIED WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR AT MAE.

Part: WEB — DAMAGED (ZONE 400) · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-5450-79556 NACELLES / PYLONS NR 3 ENGINE PYLON WEB DAMAGE. COMPLIED WITH EA 8-5450-79556 NACELLES / PYLONS NR 3 ENGINE PYLON WEB DAMAGE.

Part: FITTING — CORRODED (RT OB FLAP) · corrosion level 2 · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177.

Part: FITTING — CORRODED (RT OB FLAP) · corrosion level 2 · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-5750-79549 WINGS RIGHT O/B FLAP I/B HINGE LUG CORROSION REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-79549 WINGS RIGHT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR (P/N ARC1984).

Part: MOUNT BRACKET — WORN (ACCESSORY GB) · airframe 65,410 hrs · 20,388 cycles

COMPLY WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET WEAR REPAIR. COMPLIED WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET AT MAE.