N323FE

ATA 3610

Part: SEAL — FAILED (ANTI ICE DUCT) · airframe 74,813 hrs · 17,675 cycles

NR 3 PNEU MANIFOLD FAILURE LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER T/O (NR 3 PNEU SUPPLY ON DUE TO WING ANTI-ICE REQUIRED FOR T/O). PHASE IS ACCOMPLISHED. QRH PROCEDURES COMPLETED. LIGHT WENT OUT IMMEDIATELY AS NR 3 PNEU SUPPLY SELECTOR WAS TURNED OFF. NR 3 PNEUMATIC PRESSURE DROPPED TO 5 PSI. FOUND TELESCOPING DUCT SEALS BLOWN. REMOVED AND REPLACED SEALS PER SMP. ALSO, REMOVED AND REPLACED ANTI- ICE SHUTOFF VALVE AND PNEU MANIFOLD FAULT COMP AS PRECAUTIONARY. TOOK ACFT TO HIGH POWER AND RAN ACFT PER JRH TO TAKEOFF POWER WHILE TESTING ANTI-ICE SYSTEM. NO FAULTS NOTED. POST RUN, NO FAULT BALLS TRIPPED ON MANIFOLD FAULT COMP. ALL WORK DONE IAW DC-10-30 TAFI 36-23-00.

ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED AT STA 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL 2. FABRICATED REPAIR PARTS IAW DC10 SRM 53-20-00 FIG 6 VOL 1 AND DC10 SRM 53-33-01 VOL 2 FIG 2. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2.

ATA 5753

Part: WEDGE — DENTED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN IAW DC10 SRM 51-40-02 VOL 2.

ATA 5414

Part: SKIN — CRACKED (RT WING PYLON) · airframe 74,211 hrs · 17,263 cycles

NR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLER & FILLER IAW DC10 SRM 54-00-01 VOL 1, INSTALLED REPAIR IAW DC10 SRM 54-00-01 VOL 1.

ATA 5753

Part: RIB — CRACKED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW RIB IAW DAC DWG ARC 2340. INSTALLED RIB IAW DC10 SRM 51-35-01 VOL 2 AND DC10 SRM 51-35-02 VOL 2.

ATA 5753

Part: SKIN — CRACKED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. REINSTALLED TRAILING EDGE WEDGE IAW DC10 SRM 51-31-01 VOLUME 1.

ATA 5751

Part: SKIN — DENTED (AILERON) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW DC10 SRM 57-00-01 VOLUME 1. INSTALLED REPAIR DOUBLER IAW DC10 SRM 51-35-01 VOLUME 2.

ATA 5751

Part: SKIN — DENTED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIMITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10 SRM 51-30-01 VOLUME II. TWO DENTS ON FORWARD UPPER SURFACE AND TWO DENTS ON AFT UPPER SURFACE DAMGE REMOVED AND FABRICATED REPAIRS FOR FOUR REPAIRS IAW 57-00-01 VOLUME I. INSTALLED REPAIRS IAW DC10 SRM 51-35-01 VOLUME II, SRM 51-33-01 VOLUME II AND SRM 51-35-02 VOLUME II. REFERANCE NR N00193.

ATA 5753

Part: VANE — DELAMINATED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAULED VANE RIGHT HAND INBOARD FLAP VANE IAW FEDEX WORKCARD E-8- 5750-7-5002 C PT4.

ATA 5310

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

CORROSION AND FLAKING PAINT AND PRIMER AT STATION 1821, LONGERON 51L-51R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 58-00-01 VOL I. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC10 SRM 53-30-00 VOL I, 51-21-01 VOL 2 AND 53-30-00 VOL I.

ATA 5315

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 74,211 hrs · 17,263 cycles

FLOORBEAM CRACKED UNDER CENTER ROLLER TRAY AT ATTACH POINT STATION 840 LBL 2. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 53-00-01 VOL I, 53-00-01 VOL I, AND 51-21-01 VOL 2.

ATA 5315

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 652 IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-12-01 VOL 3, 53-00-01 VOL I AND 51-21-01 VOL 2.

ATA 5753

Part: VANE — DAMAGED (ZONE 500) · airframe 74,211 hrs · 17,263 cycles

LEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND INBOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-5002 C PT3.

ATA 5522

Part: SKIN — DENTED (ZONE 300) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND OUTBOARD ELEVATOR HAS NUMEROUS DENTS ON UPPER SURFACE. CHECKED DENTS HIGHEST READING 97887.111, DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-80-01. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 55-10-00 VOL I AND 51-21-01 VOL 2. RECORDED NEW WEIGHT 836.87 ON WEIGHT DATA TAG, WITHIN LIMITS, (ELEVATOR DOES NOT REQUIRE REMOVAL) IAW DC10 SRM 55-20-00 VOL 2. REPLACED TAG IAW DC 10 SRM 55-20-00 VOL 2.

ATA 5754

Part: TRACK — CHAFED (NR 9 SLAT) · airframe 74,211 hrs · 17,263 cycles

RIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE 1 PARAGRAPH 2 VOL 3 AND 57-00-01 VOL I FIG 1A, PARAGRAPH 5. FABRICATED AND INSTALLED OUTER SLAT SKIN REPAIR IAW DC10 SRM 57-10-00 VOL I FIGURE 30 PARAGRAPH 1-5 AND 107.

ATA 5711

Part: SPAR — DAMAGED (ZONE 600) · airframe 74,211 hrs · 17,283 cycles

RIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLISHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OUTBOARD HOLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8-5750-7-5000 PART 2 IAW EA 8-5710-77571.

ATA 5711

Part: SPAR — DAMAGED (ZONE 600) · airframe 74,211 hrs · 17,283 cycles

RT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLISHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OUTBOARD HOLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8- 5750-7-5000 PART 2 IAW EA 8-5710-77571. REFERENCE N/R N01153.

ATA 5315

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 775 IS CRACKED. REMOVED CENTER ROLLER TRAY FOR ACCESS. FABRICATED REPAIR FILLER ANGLE, REPAIR ANGLE AND CUT OUT DAMAGED AREA IAW DC10 SRM 53-00-01 VOL I. INSTALLED REPAIR PARTS AT STATION 775 FLOORBEAM IAW DC10 SRM 53-00-01 VOL I. REINSTALLED CENTER ROLLER TRAY AT STATION 606-879 IAW DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00368.

ATA 5320

Part: ANGLE — CRACKED (ZONE 300) · airframe 74,211 hrs · 17,263 cycles

ZONE 316 FORWARD UPPER BULKHEAD ANGLE IS CRACKED AT STATION 2164 BULKHEAD TO FUSELAGE SKIN ATTACH ANGLE AT RBL 8. PERFORMED DYE PEN CHECK, FOUND 1 INCH CRACK, REMOVED DAMAGED ANGLE AND INTERCOSTAL CLIPS IAW DC10 SRM 51-35-01 VOL II. FABRICATED AND INSTALLED REPAIR COMPONENTS (FILLER AND ANGLE) AND REINSTALLED INTERCOSTAL CLIPS IAW DC10 SRM 53-00-01 VOL I, DC 10 SRM 51-31-01 VOL II AND DAC DWG AJC7615. REFERENCE N/R N00348.

ATA 5754

Part: SKIN — GOUGED (NR 8 SLAT) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC10 SRM 57-10-00 VOL I, 51-21-01 VOL 2, AND 51-33-01 VOL 2.

ATA 5753

Part: ANGLE — CRACKED (ZONE 500) · airframe 74,211 hrs · 17,263 cycles

LEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-35-01 VOL 2, 51-33-01 VOL 2. FABRICATED ANGLE AND INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL 2 AND DAC DWG ARC 2227.

ATA 5315

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

FWD CARGO PIT FLOORBEAM AT BS 652 IS CRACKED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS LOCATED AND DRILLED IAW DC10 SRM 53-00-01 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 53-00-01 VOL 1.

ATA 5311

Part: FRAME — CORRODED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01.

ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER IS DENTED AT FS 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL I PAGE 6116 NR 2. FABRICATED REPAIR COMPONENTS IAW DC10 SRM 53-20-00 FIG 6 VOL 2 AND DC10 SRM 53-33-01 VOL 3 FIG 2 AND DC10 SRM 51-20-01 VOL 2, INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2.

ATA 5311

Part: FRAME — CORRODED (ZONE 100) · airframe 74,211 hrs · 17,263 cycles

AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01.

ATA 5797

Part: WIRE HARNESS — ARCED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED AND REPLACED WIRE BUNDLE IAW DC10 MM 20-30-01-2.

ATA 5720

Part: RUB STRIP — CORRODED (ZONE 500) · airframe 74,211 hrs · 17,263 cycles

LEFT WING FUEL PANEL 536DD LANDING RUB STRIP HAS CORROSION AND PITTING LOWER WING. REMOVED CORRODED RUB STRIP IAW DC10 SRM 51-35-01 VOL 2. FOUND LANDING CORRODED, TRIMMED OUT CORRODED AREA AND FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER, 2 EACH SHIMS AND FILLERS IAW DC10 SRM 57-10-00 VOL I. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 57-10-00 VOL I. INSTALLED RUB STRIP AND GANG CHANNEL IAW DC10 SRM 51-35-01 VOL 2 AND 51-42-04 VOL 2.

ATA 5753

Part: BRACKET — BROKEN (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BROKEN BRACKET IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW BRACKET IAW DAC DWG ARC 2149. INSTALLED BRACKET IAW DC10 SRM 51-35-01 VOL 2, RE-ASSEMBLED STRUCTURE IAW DC10 SRM 51-35-01 VOL 2.

ATA 5753

Part: WEDGE — DENTED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. REMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 2, FABRICATED NEW SKIN IAW FED-EX EA 8-57-50-77573 AND DC10 DAC DWG ARC 1949. INSTALLED NEW SKIN IAW DC10 SRM 51-40-2 VOL 2. REINSTALLED WEDGE IAW DC10 SRM 51-40-2 VOL 2.

ATA 5753

Part: WEDGE — DENTED (ZONE 600) · airframe 74,211 hrs · 17,263 cycles

RT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10 SRM 57-21-01 VOL 2 AND DC10 SRM 51-40-01 VOL 2.