N950DN

Part: ENGINE — FAILED (NR 2) · airframe 45,964 hrs · 37,142 cycles

RIGHT ENGINE COMPRESSOR STALL. RETURNED TO DEPARTURE. RIGHT ENGINE FAILED HPC BORESCOPE. REPLACED THE NR 2 ENGINE IAW AMDS 7100-4637-RH.

Part: PIN — DISENGAGED (EVAC SLIDE) · airframe 45,849 hrs · 37,075 cycles

DURING W/C 2561-2001 FOUND PARACHUTE PINS TO BE DISENGAGED ON L1 DOOR. SLIDE REQUIRES CHANGE. R&R L1 DOOR SLIDE PER W/C 2561-464.

Part: BRAKE — FIRE (MLG) · airframe 45,528 hrs · 36,887 cycles

SHIP 9250 - BRAKE/TIRE - NUMBER 4 BRAKE SMOKING/FLAMES UPON ARRIVAL. FUSE PLUGS BLOWN, TIRES FLAT. CORRECTIVE ACTION: REPLACED NUMBER 3 AND 4 WHEEL ASSEMBLIES. REPLACED NUMBER 4 BRAKE. INSPECTED AXLE WITH NO DAMAGE NOTED. PERFORMED ANTISKID WHEEL SPIN UP TEST. NO FAULTS. (LP#4210456)

Part: MOTOR — FAILED (FAN) · airframe 44,593 hrs · 36,362 cycles

STRONG BURNING ODOR IN THE GALLEY, TURN OFF THE GALLEY POWER AND THE ODOR DISAPPEARED. FOUND THE FIRST CLASS LAVATORY SMOKE DETECTOR FAN MOTOR SEIZED AND EXTREMELY HOT. REPLACED THE FAN IAW AMM WDM 23-17.

Part: RUB STRIP — DAMAGED (ACCESS PANEL) · airframe 43,595 hrs · 35,763 cycles

FUEL TANK ACCESS PANEL 520DT RUBSTRIP IS DAMAGED. INSTALLED A NEW RUBSTRIPS AND NUT CHANNEL IAW SRM 57-10-05.

Part: SUPPORT ANGLE — CRACKED (SPOILER) · airframe 43,595 hrs · 35,763 cycles

CRACKED SUPPORT ANGLE ON LEFT WING OUTBOARD SPOILER. REMOVED AND REPLACED IAW SRM 51-30-05, 51-30-02 AND DWG 9957465.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,595 hrs · 35,763 cycles

DENT LOCATED IN RVSM CONTROLLED AREA, STA 446, L27R-28R. OUT OF LIMITS. REPAIRED IAW SRM 53-31-02.

Part: DOOR FRAME — CRACKED (BS 45) · airframe 43,595 hrs · 35,763 cycles

NOSE LANDING GEAR WHEEL WELL CUTOUT FRAME CRACKED, BS 45, LEFT SIDE. REPAIRED IAW SRM 53-90-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,595 hrs · 35,763 cycles

SKIN CRACKED AT RIGHT HAND AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED FUSELAGE SKIN AT RIGHT HAND AFT NOSE LANDING GEAR DOOR AFT HINGE CUT OUT IAW SRM 53-30-01.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 43,595 hrs · 35,763 cycles

LEFT HAND VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-30-02 AND 51-30-05.

Part: FRAME — CRACKED (NLG WW) · airframe 43,595 hrs · 35,763 cycles

NOSE LANDING GEAR WHEEL WELL CUTOUT FRAME CRACKED, STA 45 RIGHT HAND SIDE. REMOVED AND REPLACED FRAME IAW SRM 51-30-05, 51-30-02 AND DWG 991008.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,266 hrs · 35,587 cycles

FOUND AFT VENTRAL STAIR DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-237 AND BATTERY CHARGER BASE. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,636 hrs · 35,257 cycles

CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY IAW MM. OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 41,668 hrs · 34,728 cycles

CENTER OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. FOUND CONNECTOR P1-2312 WITH A PUSHED BACK CONTACT. SECURED CONTACT INTO POSITION. OPERATION CHECKS OKAY. (LP# 9272344)

Part: SKIN — LOOSE (VERTICAL STAB) · airframe 41,592 hrs · 34,672 cycles

FOUND 15 FASTENERS LOOSE AND COUNTERSINKS WORN OUT OF LIMITS, VERTICAL STABILIZER LEADING EDGE. COMPLIED WITH PRI/ERA 552194-14AD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,221 hrs · 34,444 cycles

EMERGENCY PATH LIGHTS AT TAIL STAIRS GO OUT AFTER 5 SEC. R & R BATTERY PACK AT THE DROP DOWN CEILING LOCATION ABOVE F/A SEAT. LIGHTS OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,166 hrs · 34,412 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED THE BATTERY PACK IAW MM. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,431 hrs · 34,005 cycles

EMERGENCY FLOODLIGHTS ALONG CATWALK OUT. REPLACED BATTERY PACK IAW MM. OPERATION CHECKS GOOD.

Part: WIRE HARNESS — FAILED (CABIN) · airframe 39,971 hrs · 33,732 cycles

ACFT EXPERIENCED A MOMENTARY CABIN FIRE EVENT DURING TAXIOUT TO THE RUNWAY. FIRE EXTINGUISHED AFTER ENGINES WERE SHUTDOWN AND NO FIRE EXTINGUISHER WAS USED. CREW REPORTED PRIOR TO TAKING THE RUNWAY THE F/O EFIS SCREENS FLICKERED AND THEN WENT BLANK FOLLOWED BY THE SOUND OF SEVERAL, 7 CIRCUIT BREAKERS POPPING. PASSENGERS WERE HEARD SHOUTING "FIRE" AND SPARKS/FLAMES WERE MOMENTARILY VISIBLE AT THE CEILING/OVERHEAD BIN AREA AT SEAT ROWS 26-27CDE. MAINTENANCE FOUND WIRE BUNDLES ABOVE SEAT ROW 27CDE SHORTED TO A BRACKET ON THE CEILING PANEL FOR RECEPTACLE R5-3360. WIRE REPAIRS WERE PERFORMED IAW SWPM CHAPTER 20-10 AND THE WDM. ALL SYSTEMS WERE OPERATIONALLY CHECKED AND TESTED IAW THEIR RESPECTIVE ATAS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,961 hrs · 33,727 cycles

AFT CABIN AND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK. OPERATION CHECKS GOOD.

Part: LANYARD — UNSECURE (L1 DOOR SLIDE) · airframe 39,505 hrs · 33,442 cycles

FOUND L1 DOOR SLIDE LANYARD UNSECURE. R & R L1 DOOR SLIDE.

Part: ATTACH FITTING — CORRODED (NR 2 SLAT) · airframe 38,314 hrs · 32,692 cycles

CORROSION ON INBD AND OTBD SLAT ATTACH FITTINGS. REMOVED AND INSTALLED NR 2 SLAT IAW AMDS 2700-4528-RH-02.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 37,062 hrs · 31,944 cycles

L1 DOOR SLIDE PINS PULLED ON SLIDE PACK. REPLACED L1 DOOR SLIDE IAW CARD 2561-01358-02A.

Part: SKIN — BENT (L1 DOOR) · airframe 36,544 hrs · 31,636 cycles

L1 DOOR LOWER FLANGE BENT ON FORWARD LOWER CORNER SKIN. STRAIGHTENED LOWER EDGE IAW SRM 52-01-01. NO ADDITIONAL REPAIR REQUIRED. OK FOR SERVICE.

Part: SKIN — DENTED (BS 1290-1307) · airframe 36,083 hrs · 31,341 cycles

DENT FOUND ON RT FUSELAGE BETWEEN BS 1290 - 1307, BETWEEN STRINGERS 22 AND 23 RIGHT.

Part: STRUCTURE — DENTED (L1 DOOR) · airframe 34,263 hrs · 30,194 cycles

SMALL DENT ON LOWER FORWARD EDGE ON L1 DOOR. STRAIGHTENED DENT IAW SRM 52-01.

Part: DOOR FRAME — CORRODED (MID CARGO) · airframe 32,979 hrs · 29,357 cycles

MID CARGO COMPARTMENT DOOR FRAME HAS SLIGHT CORROSION BS 695, LONGERON 28L. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED DOUBLER IAW SRM 51-10-03.

Part: SKIN — CORRODED (BS 864-883) · airframe 32,979 hrs · 29,357 cycles

REMOVAL OF WTB FAIRING RUB STRIPS REVEALED CORROSION ON FUSELAGE SKIN BETWEEN LONGERON 28R TO 29R FROM STA 864-883. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-31-01, 53-30-01, 51-10-03. ID REPAIR IAW PS 900-5-01, NR 4.