N949DN

Part: DOOR — DAMAGED (CABIN) · airframe 45,053 hrs · 37,338 cycles

DAMAGE FOUND ON DOOR AT ARRIVAL. INSPECTED, EVALUATED AND PERFORMED TEMPORARY REPAIR IAW ERA 564228-14. PERMANENT REPAIR PERFORMED ON L1 DOOR IAW ERA 564228-14, RV O.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,803 hrs · 36,589 cycles

RIGHT SKIN CRACKED VERTICAL STABILIZER. REPAIRED IAW ERA 556419-14.

Part: SKIN — CRACKED (NLG DOOR CUTOUT) · airframe 43,803 hrs · 36,589 cycles

CRACK AT LEFT FUSELAGE SKIN, NOSE LANDING GEAR STRUT DOOR FORWARD AND AFT HINGE CUTOUTS. REPAIRED IAW SRM 53-30-01.

Part: DOUBLER — CRACKED (BS 1460) · airframe 43,803 hrs · 36,589 cycles

CRACK AT BS 1460, DOUBLER, LONGERON 2R. REPLACED IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 902) · airframe 43,803 hrs · 36,589 cycles

FRAME BS 902 CRACKED. REPLACED THE FRAME.

Part: BRACKET — CRACKED (BS 1520) · airframe 43,803 hrs · 36,589 cycles

RIGHT AIR BOX WEB ANGLE BRACKET CRACKED, BS 1520. REPLACED THE BRAKET.

Part: BRACKET — CRACKED (BS 1520) · airframe 43,803 hrs · 36,589 cycles

RIGHT AIR BOX WEB ANGLE BRACKET CRACKED, BS 1520. REPLACED THE BRACKET.

Part: BRACKET — CRACKED (HANDRAIL) · airframe 43,803 hrs · 36,589 cycles

HANDRAIL BRACKET CRACKED, BS 1520 BULKHEAD FORWARD SIDE. REPLACED THE BRACKET.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,398 hrs · 36,355 cycles

FLIGHT ATTENDANT REPORTED AND ELECTRICAL ODOR DURING FLIGHT. TURNED OFF GALLEY POWER AND THE ODOR DISSIPATED. ODOR WAS LIMITED TOE FORWARD GALLEY. MAINTENANCE INSPECTED GALLEY. COMPLIED WITH NO GO ODI PREVENTION PROGRAM. PERFORMED DUCT BURNOUT AND RAN BOTH PACKS WITH GALLEY POWER ON. OPERATION CHECKS GOOD.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 42,908 hrs · 36,084 cycles

L1 DOOR SLIDE HAS GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE IAW MM.

Part: DOOR — DAMAGED (CABIN) · airframe 42,429 hrs · 35,808 cycles

DAMAGE TO FORWARD AFT LOWER CORNERS OF L1 DOOR. EDGE FLANGE. REPAIRED IAW SRM 52-01-01.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 42,032 hrs · 35,575 cycles

LEFT HORIZONTAL STABILIZER UPPER REAR SPAR AFT BARREL NUT HOLE CRACK. REMOVED AND REPLACED STABILIZER ASSEMBLY IAW AMDS 5510-4001.

Part: JACKSCREW — DAMAGED · airframe 42,032 hrs · 35,575 cycles

GROOVE WEAR ON JACKSCREW THREAD. COMPLIED WITH PRI/ERA 551394-14AD.

Part: LUG — CORRODED (HORIZONTAL STAB) · airframe 42,032 hrs · 35,575 cycles

AFT SUPPORT RIGHT FITTING ON HORIZONTAL SUPPORT OUTBOARD LUG CORRODED. COMPLIED WITH PRI/ERA 551207-14. (LP# 270936)

Part: SKIN — PUNCTURED (BS 240) · airframe 43,803 hrs · 36,589 cycles

FUSELAGE SKIN LEFT BS 240, STRINGER 18L PUNCTURED. REPAIR ACCOMPLISHED.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 41,669 hrs · 35,342 cycles

EMERGENCY LIGHT ABOVE AFT CABIN DOOR RIGHT SIDE, FLICKERS ON AND OFF. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY. OPERATION CHECKS NORMAL. (LP# 8720256)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,777 hrs · 34,821 cycles

DAMAGE TO NOSE FUSELAGE UPPER SKIN PANEL. REPAIRED IAW ERA 534440-14, SECTION I .

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,777 hrs · 34,821 cycles

DAMAGE TO RT SERVICE DOORS SURROUNDING SKIN PANEL. REPAIRED IAW ERA 534439-14, SECTION I.

Part: SKIN — DENTED (NOT REPORTED) · airframe 40,777 hrs · 34,821 cycles

DENT AND CREASE ON UPPER SKIN PANEL. REPAIRED IAW ERA 534431, SECTION I.

Part: DOUBLER — DAMAGED (BS 180-200) · airframe 39,966 hrs · 34,317 cycles

DEFORMED INTERNAL PRODUCTION DOUBLER BETWEEN BS 180-200, LONGERON 9-11R AT RT SERVICE DOOR SURROUNDING SKIN PANEL. REPAIRED IAW ERA 541592-14, REV O.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 39,889 hrs · 34,274 cycles

ON ARRIVAL, REPORTED DAMAGE TO LOWER LT CORNER OF L1 DOOR. REPAIRED IAW SRM 52-01-01.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 38,663 hrs · 33,538 cycles

VERTICAL STABILIZER LT SKATE ANGLE CRACKED. DOUBLER REPAIRED IAW SRM 55-30-05.

Part: LONGERON — CRACKED (BS 1475) · airframe 38,663 hrs · 33,538 cycles

LONGERON 2L CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14.

Part: SKIN — CRACKED (BS 1475) · airframe 38,692 hrs · 33,552 cycles

SKIN CRACKED, AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, FIG 16 AND PRI/ERA 537342-14, REV O.

Part: SKIN — CRACKED (BS 1475) · airframe 38,663 hrs · 33,538 cycles

SKIN CRACKED AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, RIG 16 AND ERA 537336-14, REV O.

Part: SKIN — CRACKED (BS 1494) · airframe 38,692 hrs · 33,552 cycles

FUSELAGE SKIN CRACKED, BS 1494, BETWEEN STRINGERS 3 - 4R. REPAIRED IAW SRM 53-00-01.

Part: SKIN — CRACKED (BS 1475) · airframe 38,663 hrs · 33,538 cycles

FUSELAGE SKIN CRACKED, BS 1475, L2R. REPAIRED IAW ERA 537336.

Part: SHEAR TIE — CRACKED (BS 1475) · airframe 38,663 hrs · 33,538 cycles

SHEAR TIE CRACKED BS 1475, STR 2R. SHEAR TIE REPLACED.

Part: SKIN — DAMAGED (BS 148-218) · airframe 38,078 hrs · 33,184 cycles

DAMAGED AREA ON FUSELAGE SKIN AT BS 148-218, L8R AND L12R. DISCREPANCY ADDRESSED ON NONROUTINES IAW ERA 534431-14, REV O. LP 1900490.

Part: DEPRESSOR — BENT (SERVICE DOORWAY) · airframe 38,078 hrs · 33,184 cycles

SEAL DEPRESSOR IS BENT, RT FORWARD SERVICE DOOR FUSELAGE CUTOUT, AFT UPPER CORNER. ACCOMPLISHED PERMANENT REPAIR IAW ERA 534438-14, REV O. LP 1897337.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 38,078 hrs · 33,184 cycles

RIGHT FORWARD SERVICE DOOR JAMB IS DENTED AT AFT UPPER CORNER. ACCOMPLISHED PERMANENT REPAIR IAW ERA 534438-14, REV O. LP 1897335.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 38,078 hrs · 33,184 cycles

FORWARD SERVICE DOOR EXTERNAL SKIN HAS DENT WITH GOUGE ON UPPER SIDE. ACCOMPLISHED PERMANENT REPAIR ON FORWARD SERVICE DOOR EXTERNAL SKIN UPPER IAW ERA 534435-14, REV O. LP 1897331.

Part: PIN — DISLODGED (L1 DOOR SLIDE) · airframe 35,515 hrs · 31,544 cycles

BOTTOM PARACHUTE PIN ON L1 DOOR SLIDE PACK DISCOVERED TO BE DISLODGED. TOP PIN ALMOST DISLODGED. MAINTENANCE R & R L1 DOOR SLIDE ASSEMBLY.

Part: SHEAR TIE — DAMAGED (BS 240) · airframe 34,616 hrs · 30,996 cycles

SHEAR TIE DAMAGED, BS 240, BETWEEN L17-18L. R & R DAMAGED SHEAR TIE IAW SRM 51-30-00.

Part: ACM — OVERSERVICED (LEFT) · airframe 34,185 hrs · 30,718 cycles

EXPERIENCED A PLASTIC ODOR COMING FROM THE AIR CONDITIONING SYS ON CLIMBOUT THROUGH 15000 FT. ODOR DISSIPATED AND THEN REOCCURRED ON DESCENT BELOW 10000 FT. PERFORMED TROUBLESHOOTING IAW FIM WITH PACKS ON. NO ODOR NOTED IN CABIN. FOUND LEFT ACM OVER SERVICED. RESERVICED TO PROPER LEVEL. PERFORMED DUCT BURNOUT IAW AMM. NO ODOR OR HAZE NOTED.

Part: SKIN — DENTED (PAX DOOR) · airframe 33,873 hrs · 30,515 cycles

SMALL DENT ON FORWARD CABIN DOOR EDGE DISCOVERED BY GATE CREW. MADE REPAIRS IAW SRM 52-01-01. OK FOR SERVICE.

Part: RELEASE CABLE — CORRODED (TAILCONE) · airframe 33,793 hrs · 30,459 cycles

TAILCONE RELEASE CABLE HAS CORROSION ON ALL CLEVIS COMMON TO YOKE, Y1567-895. R & R TAILCONE RELEASE CABLE NR 547 IAW AMM. RII COMPLIED WITH.

Part: RELEASE CABLE — BROKEN (TAILCONE) · airframe 33,793 hrs · 30,459 cycles

DURING SERVICE CHECK, TAILCONE RELEASE CABLE ASSY RUN HAS A BROKEN WIRE. MX R & R TAILCONE CABLE ASSY RUN IAW MM. OPS CHECKED GOOD.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

LEFT HORIZONTAL STAB CENTER BOX JOINT, ON THE UPPER INBD SKIN SURFACE, STA XH24234 HAS DETERIORATING, FASTENER INSTALLATION (14EA). CLEANED ALL LEFT BARRELL NUT HOLES. HOLES NR 6 AND NR 13 HAVE CORROSION. REAMED HOLES TO REMOVE CORROSION. FABRICATED AND INSTALLED BUSHING IAW ERA 513400-14.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

RT HORIZONTAL STAB CENTER BOX JOINT, ON THE UPPER INBD SKIN SURFACE AT STA XH24.234 HAS DETERIORIATING SURFACE FASTENER, SURFACE SEALING (12 EA). FOUND HOLES NR 10, 14, 18, AND 19 WITH CORROSION. REAMED HOLES 10 AND 14. LOCAL BLENDED HOLES 18 AND 19. FABRICATED BUSHING FOR 10 AND 14. INSTALLED ALL BUSHINGS IAW SRM 55-10-03, PARA 11. HFEC. NO DEFECTS NOTED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

HORIZONTAL STABILIZER, RT LOWER SURFACE FOURTH FROM AFT END HAS BARREL NUT PLUG PROTRUDING. INSPECTED AND FOUND CORROSION AT BARREL NUT HOLE, NR 32. REAMED HOLE AND LOCAL BLENDED REMAINING CORROSION IAW SRM 55-10-03, PARA 11. NO DEFECTS NOTED. FABRICATED, ALODINED, AND INSTALLED BUSHING IAW SRM 55-10-03, 51-10-03.

Part: SUPPORT ANGLE — DAMAGED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

HORIZONTAL STAB LEFT SUPPORT ANGLE AT REAR SPAR XE 167.953 HAS HEAVY EXFOLIATION. REMOVED DAMAGE SUPPORT ANGLE FROM LT HORIZONTAL STAB STA XE169.953. FABRICATED, ALODINED, PRIMED, TOPCOATED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-02, PARA 7 AND PARA 8, 551-10-05, PARA 1, 51-10-03, PARA 14 AND PARA 21 AND DWG 9918401- 165.

Part: SUPPORT ANGLE — DAMAGED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

RIGHT HORIZONTAL STAB SUPPORT ANGLE AT REAR SPAR STA XE 167.953 HAS HEAVY EXFOLIATION. REMOVED DAMAGED SUPPORT ANGLE FROM RT HORIZONTAL STAB, T/E ANGLE STA XE167.953. FABRICATED, ALONDINED, PRIMED, TOP COATED AND INSTALLED NEW ANGLE IAW SRM 51-30-05 PARA 7 AND PARA 8, 51-10-05, PARA 1, 51-10-03, PARA 21 AND 14 AND DWG 9918401-165.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 33,791 hrs · 30,457 cycles

HORIZONTAL STABILIZER LT LOWER SURFACE HAS SEVERAL BARREL NUT PLUGS THAT ARE DETERIORATED. CLEANED ALL BARREL NUT HOLES IAW SRM 51-20-00. FOUND 2 EA CORRODED. REMOVED 2 EA HOLES IAW 55-10-03, PARA II. HOLES NR 31 AND NR 37. REAMED TO ALLOWABLE LIMITS. FABRICATED BUSHING PO 2209283 AND INSTALLED IAW SRM 55-10-03, PARA 11. NO CRACKS NOTED. INSTALLED NR 31 AND NR 37 BOLTS.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 33,791 hrs · 30,457 cycles

MID CARGO DOOR FRAME HEADER BEAM STA 730-750 HAS CORROSION AROUND RIV-NUTS TASK 53-122-02. REMOVED CORROSION, OUT OF LIMITS. FABRICATED, ALODINED, PRIMED, TOP COATED AND INSTALLED REPAIR DOUBLER IAW 53-60-02.

Part: STIFFENER — DAMAGED (CENTER WING) · airframe 33,791 hrs · 30,457 cycles

CRACKED STIFFENER ABOVE CENTER WING BOX STA 883, LBL 44.5. CUT OUT DAMAGED FLANGE ON STIFFENER ERA 498192-14, MA REV A. NO DEFECTS NOTED. FABRICATED, ALODINED, PRIMED AND TOP COATED AND INSTALLED ALL REPAIR PARTS IAW ERA 498192-14, MA REV A.

Part: SKIN — CORRODED (BS 750) · airframe 33,791 hrs · 30,457 cycles

RIGHT FUSELAGE SKIN AT BS 750, 10 INCHES BELOW L27R IS CORRODED. REMOVED CORRODED BUTT SPLICE. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED DOUBLER AND FILLER IAW SRM 53-31-03 AND 51-20-00, VOL II.