N369FE

Part: FIRE BOTTLE — LOW (NR 2 NACELLE) · airframe 75,719 hrs · 31,179 cycles

ENG FIRE AGNT LO ALERT AND ENG 2 AGT 1 LOW LIGHT DURING CRUISE FOUND NR 2 ENG 1 FIRE BOTTLE LOW PRESS SWITCH BAD, REPLACED NR 2 ENG NR1 FIRE BOTTLE, LIGHT EXT. CHECKS OK

Part: VALVE — ACTIVATED (OVERPRESSURE) · airframe 75,636 hrs · 31,134 cycles

"AIR SYS 1 OFF" ANNUNCIATED. AFTER ABOUT A MINUTE GOT "AIR MANF 1 FAIL" LEVEL 3 ALERT. COMPLIED WITH QRH. DIVERTED, DURING DECENT, AIR MANF 1 FAIL ALERT CAME ON SEVERAL TIMES. INTERIGATED MCDU FOUND NO FAULTS IN AIU , VIA, OR PSC1, PERFORMED RTS ON PSC1 AND PASSED. OPENED NR1 ENG AND APPLIED AIR TO SYS FOUND LEAK ON OVERPRESSURE VALVE. REPLACED CLAMPS WITH NO HELP, INSTALLED NEW VALVE AND LEAK CHECKED GOOD. REF AMM 78-31-03-2. PERFORMED DECAY TEST REF 36-00-01-5 TEST PASSED. RAN NR 1 ENG FOR 20 MIN TOTAL AND 5 MINS, AT FLIGHT IDLE, NO FAULTS ON ENGINE RUN. ENG RUN PERFORMED BY EMP 485450. CLOSED NR1 COWLINGS REF AMM 71-00-00-5.

Part: RELIEF VALVE — FAILED (CABIN PRESSURE) · airframe 74,615 hrs · 30,635 cycles

AT FL 310 RECEIVED LEVEL 3 "CABIN ALTITUDE" ALERT WITH NO OTHER NOISE OR INDICATIONS. ENG A/I WAS ON. FOLLOWED QRH AND COULD NOT (WITH 3 PACKS) MAINTAIN INDICATED CABIN ALTITUDE TO BELOW 10,000 FT. CABIN ALTITUDE INDICATED CLIMB WITH DDP AT APPROX 9.1. COULD NOT CONTROL CABIN ALT IN AUTO OR MANUAL. REMOVED AND REPLACED AFT UPPER POS PRESS RELIEF VALVE. VALVE OPS CK OK. REF MM 21-34-01-4. ALSO, REMOVED AND REPLACED CPAM. OPS CK STILL REQ REF MM 21-31-08-4.

Part: SKIN — CRACKED (ZONE 300) · airframe 72,855 hrs · 29,814 cycles

FROM J/C SP10270016-7000-10J OTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I AND SRM 55-20-00 FIG 4 VOL I.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 72,855 hrs · 29,814 cycles

OUTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE.

Part: NONE — NONE (NONE) · airframe 72,855 hrs · 29,814 cycles

MAIN CABIN L4 PASSENGER DOOR UPPER INTERNAL JAMB EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5310-115295A.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 10 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA FOUND CORROSION WITH EXFOLIATION ON LONGERON, REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5.

Part: BEAM — CRACKED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 VOL I FIG 3.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT SUMP AREA FOUND CORROSION WITH EXFOLIATION, SEE NRC N00315, N00316, N00294, N00253. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5 SHEET 1.

Part: INTERCOSTAL — DAMAGED (LT WING) · airframe 72,855 hrs · 29,814 cycles

LT WING L/E INTERNAL STRUCTURE ON HORIZONTAL INTERCOSTAL EXISTING ANGLE REPAIR. REPLACED INTERCOSTAL IAW DWG ARB2408 AND ARB1333.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,855 hrs · 29,814 cycles

INT CAC CRACK ON FRAME. PERFORMED FRAME REPAIR IAW SRM 53-30-00 VOL I FIG 7.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA FOUND CRACK ON LONGERON, SEE NRC N00293, N00294, N00295, N00297. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1-2.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 72,855 hrs · 29,814 cycles

DURING STB INSP FOUND PANEL P/N 7206-1 AND P/N 7207-1 OF CONSTANT SECTION SKIN PANEL PLANKS, SEE ATTACHED SHEET FOR BEST DETAIL. CRACK IS IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-99384.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,855 hrs · 29,814 cycles

MAIN CABIN R1 DOOR FWD JAMB DURING PERFORM OAN J/C SP10240272-7001-2J FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-00-01 VOL I FIG 8.

Part: SILL — CORRODED (BS 879-886) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD.

Part: SILL — CORRODED (ZONE 800) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD. REPAIRED AREA IAW SRM 53-50-00 FIG 1 VOL I.

Part: LONGERON — CRACKED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.

Part: LONGERON — CRACKED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

ENTRY WAY, DURING REMOVAL FLOOR PANELS WITH OAN J/C MD10-0600C220-1JR FOUND SEVERE EXFOLIATION CORROSION INTERNAL SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I.

Part: DOUBLER — DAMAGED (L/E SLAT) · airframe 72,855 hrs · 29,814 cycles

RT WING NR 1 SLAT EXTERNAL SKIN EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-10-00 FIG 84 VOL I.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 72,855 hrs · 29,814 cycles

PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN JC SP10530208-2JR, FOUND CRACK ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

LT WING INBD AILERON CORROSION BOTTOM UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION ON MEMBRANE AND CRACK 2" LONG. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND MODERATE CORROSION AND CRACK 2" LONG ON MEMBRANE. REPLACED WEB SECTION IAW SRM 53-00-01 VOL I FIG 10.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA HAS CRACK ON CAP TEE OF BULKHEAD. REPAIRED AREA IAW EA 8-5310-99388.

Part: SKIN — CRACKED (ZONE 400) · airframe 72,855 hrs · 29,814 cycles

PYLON NR 1 EXT SKIN FOUND CRACK ON SKIN UPPER SIDE RT. 10-25-07 REPAIRED PYLON SKIN IAW SRM 51-00-01 VOL I FIG 100 & SRM 54-00-01 VOL I FIG 2B.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION (OUT OF LIMIT) ON MEMBRANE AND CRACK. REPLACED WEB SECTION IAW SRM 53-00-01 FIG 10 VOL I.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 72,855 hrs · 29,814 cycles

NLG W/W FOUND CRACK ON LT VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 72,855 hrs · 29,814 cycles

RT WING TIP CRACKS, 1.5" LONG ON EXTERNAL SKIN XW 928, YW 799. CONTINUED CRACK ON INT OLD REPAIR ON FRAME XW 928, YW 799. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.

Part: SKIN — DAMAGED (BS 427) · airframe 72,855 hrs · 29,814 cycles

R1 PASSENGERS DOOR DEFORMATION OLD REPAIR ON UPPER FWD CORNER EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00 FIG 12A VOL I.

Part: PAN — CRACKED (DOOR FRAME) · airframe 72,855 hrs · 29,814 cycles

LOWER CENTER CARGO DOOR CRACK LONG .250" AND DEFORMATION ON LWR FORWARD CORNER. 11-07-07 REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1& 2.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 72,855 hrs · 29,814 cycles

RT W/W CRACK 0.5" LONG ON VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00-01 VOL I FIG 10.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 72,855 hrs · 29,814 cycles

CTR W/W SPACE CRACK ON VERTICAL BULKHEAD. PERFORMED REPAIR IAW SRM 53-00-01 VOL I FIG 4.

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING L/E CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.

Part: RIB — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING INTERNAL L/E ON UPPER RIB FOUND CRACK 0.70" LONG. REPAIRED RIB IAW SRM 57-20-00 FIG 1 VOL I.

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING L/E INTERNAL CRACK LONG 0.50" ON INTERCOSTAL. 10-10-07 REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 72,855 hrs · 29,814 cycles

CTR W/W SPACE: CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 4 VOL I.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 72,855 hrs · 29,814 cycles

LT WING OUTBOARD FLAP CORROSION UNDER UPPER SKIN. 10-11-07 REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 85.

Part: SKIN — CRACKED (RT WING LE) · airframe 72,855 hrs · 29,814 cycles

L/E RT WING CRACK ON EXTERNAL SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING L/E CRACK ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

EXT FUSELAGE RT SIDE FOUND DENT .45" BY .25" DEEP 0.027" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

EXT SURFACE RT SIDE FOUND DENT 2" BY 1" DEEP 0.062" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.

Part: SCOOP — CRACKED (ZONE 100) · airframe 72,855 hrs · 29,814 cycles

INT CAC CRACK ON SUGAR SCOOP. REPAIR AREA IAW SRM 53-40-00 VOL I FIG 8.

Part: SKIN — CRACKED (ZONE 500) · airframe 72,855 hrs · 29,814 cycles

LT WING L/E CRACK ON EXTERNAL LOWER SKIN.

Part: SKIN — CRACKED (ZONE 600) · airframe 72,855 hrs · 29,814 cycles

L/E RT WING CRACK ON EXTERNAL SKIN L/E .

Part: SENSOR — MALFUNCTIONED (STALL WARNING) · airframe 70,941 hrs · 28,782 cycles

PDIS: ON ROTATION FOR TAKEOFF BOTH STICK SHAKERS ACTIVATED AND REMAINED ON WITH NORMAL AIRCRAFT INDICATIONS, NORMAL FEEL, AIRSPEED INDICATORS ALL THE SAME & NORMAL. FLAPS RETRACTED NORMALLY. SLATS LEFT EXTENDED. CAPTAIN AND F/O STICK SHAKER CB'S PULLED. RETURNED FOR NORMAL LANDING. FOUND NR 1 AOA PROBE VERY STIFF, DIFFICULT TO ROTATE BY HAND. REMOVED AND REPLACED AUTO PITCH TRIM COMPUTER. REMOVED AND REPLACED BOTH LT AND RT ANGLE OF ATTACK SENSORS PER MM 22-33-01-2. PERFORMED SELF TEST OF BOTH NR 1 AND NR 2 AT/SC COMPUTERS PER MM 22-33-01-2 CHECK OK. RETURNED TO SERVICE.

Part: PEDAL — BROKEN (BRAKES) · airframe 70,828 hrs · 28,728 cycles

CAPTS RT BRAKE PEDAL WILL NOT ACTUATE THE BRAKES. FOUND THE CTR TORQUE TUBE BRACKET FOR THE CAPTS RT PEDAL BROKEN. MPN ABH7271-501 INSTALLED SERVICEABLE BRACKET (SETS PARKING BRAKE) BRAKE PEDALS OPERATE NORMAL AND PARKING BRAKE SETS AND RELEASES NORMAL. INSTALLED BRACKET PER DC-10 SMP.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 69,761 hrs · 28,142 cycles

COMPLY WITH EA 8-5750-55451, RT OB FLAP FLAP VANE SUPPORT CORROSION REWORK. CLOSING ACTION ON 03/08/05. ON N/R S00013. COMPLIED WITH EA 8-5750-55451.

Part: RIB — GOUGED (ZONE 500) · airframe 69,761 hrs · 28,142 cycles

COMPLY WITH EA 8-5710-55459, REWORK OF GOUGES IN WING LEADING EDGE RIB PN NRD6037-1. CLOSING ACTION ON 03/09/05. ON NR S00019. COMPLIED WITH EA 8-5710-55459.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 69,761 hrs · 28,142 cycles

COMPLY WITH EA 8-5750-55448 WINGS - FLAP VANE SUPPORT CORROSION REWORK LT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-55448.

Part: THRUST REVERSER — GOUGED (ZONE 500) · airframe 69,761 hrs · 28,142 cycles

COMPLY WITH EA 8-7830-55453 TITLE EXHAUST THRUST REVERSER - REWORK OF GOUGE ON T/R SUPPORT FITTING. COMPLIED WITH EA 8-7830-55453.

Part: DRAIN — CORRODED (ZONE 100) · airframe 69,761 hrs · 28,142 cycles

COMPLY WITH EA 8-5310-55454, FUSELAGE MAIN FRAME BULK CARGO DOOR LWR JAMB SILL CORROSION REPAIR (P/N AFA3248). CLOSING ACTION ON 02/28/05. ON N/R S00015, COMPLIED WITH EA8-5310-55454.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR) · airframe 69,213 hrs · 27,871 cycles

BEFORE TAKEOFF FLIGHT, CONTROL CHECKS WERE NORMAL. ROTATION FELT SLIGHTLY HEAVIER THAN NORMAL. DURING ACCELERATION AND CLEAN UP, ELEVATOR BECAME VERY DIFFICULT TO MOVE. ACTED AS IF AUTOPILOT MIGHT BE ON, BUT NO CB'S POPPED. DUMPED 5000 LBS AND RETURNED TO MEM. PERFORMED ELEVATOR MOVEMENT TEST WITH NO NOTICEABLE STIFFNESS. FOUND FAULT BALLS ON ELF/FL PROGRAMMER FOR FL ACTUATOR FOR NR 2 PROGRAMMER. FOUND FAULT BALLS ON BOTH PITCH COMP FOR COMPUTER, ACTR A, AND ACTR B. PERFORMED BI TE CK ON BOTH CONTROLLERS BOTH PASSED. REMOVED AND REPLACED ELEVATOR LOAD FEEL DUPLEX ACT. IN REFERENCE TO DC-10-10 M/M 27-32-01-2, OPS CHECKED GOOD.

Part: SUPPORT — DAMAGED (T/E FLAP) · airframe 67,461 hrs · 26,911 cycles

RIGHT INBOARD FLAP-INBOARD FLAP SUPPORT OVERSIZED HOLE REPAIR P/N 7170, COMPLY WITH EA 8-5750-72263 ENT BY: 497234 RPT BY: 497234 FACT 21AUG03 15:14 BFM R COMPLIED WITH EA 8-5750-72263 ENT BY: 497191 RPT BY: 497191.

Part: TRACK — GOUGED (THRUST REVERSER) · airframe 67,461 hrs · 26,911 cycles

COMPLY WITH EA 8-7832-72262 EXHAUST-THRUST REV- GOUGE REPAIR LOWER TEE TRACK P/N 9019M20P06 ENT BY: 497234 RPT BY: 497234 FACT 19AUG03 13:13 BFM R COMPLIED WITH EA 8-7832-72262 EXHAUST- THRUST REV- GOUGE REPAIR LOWER TEE TRACK P/N 9019M20PO6 ENT BY: 497191 RPT BY: 497191.

Part: HINGE BRACKET — DAMAGED (T/E FLAP) · airframe 67,461 hrs · 26,911 cycles

WINGS- OUTBOARD FLAP (RT) INBOARD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/N ARC0502 ENT BY: 497239 RPT BY: 497239 FACT 19AUG03 13:22 BFM R COMPLIED WITH EA 8-5750-72261, WINGS- OUTBOARD FLAP (RT)- INBOARD HINGE BRACKET- ACTUATOR ATTACH HOLE REPAIR P/N ARCO502 ENT BY: 497191 RPT BY: 497191.

Part: HINGE BRACKET — DAMAGED (T/E FLAP) · airframe 67,461 hrs · 26,911 cycles

COMPLY WITH EA 8-5750-72256- WINGS- RIGHT OUTBOARD FLAP INBOARD HINGE ASSY-ARC 1984--PIVOT BORE REWORK ENT BY: 39014C RPT BY: 39010C FACT 21AUG03 15:11 BFM R COMPLIED WITH EA 8-5750-72256 ENT BY: 497191 RPT BY: 497191.

Part: DUCT — DAMAGED (NR 3 A/C PACK) · airframe 67,461 hrs · 26,911 cycles

AIR CONDITIONING- NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019. FACT 18AUG03 22:55 BFM R COMPLIED WITH EA 8-2150-72259 AIR CONDITIONING NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019 AT MAE.

Part: HINGE — GOUGED (TAILCONE) · airframe 67,461 hrs · 26,911 cycles

DOORS - SERVICE - TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC7011-1. COMPLY WITH EA 8-5240-72249 REV NR POS ENT BY: 402783. FACT 18AUG03 23:02 BFM R COMPLIED WITH EA 8-5240-72249 DOORS - SERVICE- TAIL CONE- PATIO DOOR HINGE REPAIR P/N AKC 7011-1 AT MAE.