Aviation Advisor, Inc.

Sanction: $5,000 · case closed 2014-08-26

Part: REGULATOR — LEAKING (ZONE 200) · airframe 4,337 hrs · 3,437 cycles

N533CM 525B-0182 WAS IN ROUTE FROM MIA TO C29. WHILE IN ROUTE AND ON DESCENT AT 34,000 FEET CREW REPORTED AIRCRAFT DEPRESSURIZATION FOLLOWED BY EMER PRESS ANNUNCIATOR ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO KMKE. THIS WAS A PART 135 TRIP WITH 1 PASSENGER ON BOARD. CREW LANDED THE AIRCRAFT SAFELY.

Part: AUTOPILOT SYS — CORRUPTED · airframe 1,095 hrs · 713 cycles

AIRCRAFT DEPARTED, ENGAGED AUTOPILOT IN CLIMB, EXPERIENCED A RAPID PITCH UP AND LEFT ROLL, AUTOPILOT SELF DISENGAGED, PILOT LEVELED AIRCRAFT AND FOLLOWED CHECKLIST PROCEDURES FOR TROUBLESHOOTING AND VERIFICATION OF ANY OTHER MALFUNCTIONS, DECIDED TO DIVERT FROM INTENDED DESTINATION, AND LANDED WITHOUT INCIDENT.

Part: FDU — INTERMITTENT (NR 2 ENGINE) · airframe 1,912 hrs · 1,419 cycles

AIRCRAFT ENTERED DECENT FROM 44,000 FT, TO 38,000 FT, THE NR 2 ENGINE FLAMED OUT, EMERGENCY PROCEDURES WERE FOLLOWED AND EMERGENCY DECLARED, AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT, THE NR 2 ENGINE FUEL DELIVERY UNIT WAS SENT FOR INSPECTION,

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 4,144 hrs · 2,774 cycles

WINDSHIELD FAULT LIGHT ILLUMINATED APPROX 30 SECONDS PRIOR TO PILOTS SEEING CRACK IN LOWER RT COPILOTS WINDSHIELD, DECLARED EMERGENCY AND DECENDED TO A SAFE DEPRESSURIZED ALTITUDE IAW ACFT PROCEDURES, PROBABLE CAUSE BROUGHT ON BY FAILED ELECTRICAL HEATING ELEMENT IN WINDSHIELD, WINDSHIELD REPLACE AT SERVICE CENTER.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 1,429 hrs · 994 cycles

CREW EXPERIENCED LOSS OF PRESSURIZATION/ERRATIC OPERATION, WAS ABLE TO CONTROL IN MANUAL MODE.

Part: SKIN — DAMAGED (BS 229-264) · airframe 51,611 hrs · 27,104 cycles

DENT IN FUSELAGE APPROX 4' FROM L1 DOOR AND 2' BELOW WINDOW BELT REMOVED DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR SECTION OF SKIN FINGER DOUBLERS SKIN SPLICE STRAP STRAPS IAW MD80 SRM 53 04 FIG 12C.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY PULLED LOOSE. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED PANEL WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR PANEL WITH GLASS CLOTH PER SRM 51-90-0.

Part: WEB — CORRODED (BS 170-199) · corrosion level 2 · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR MEMBRANE CORRODED. CUT OUT DAMAGED AREA AND INSTALLED REPLACEMENT WEB PER SRM 51-70-4 AND 51-30-2.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-5.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.

Part: SKIN — DAMAGED (BS 1253-1263) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN CREASED AT PRIOR REPAIR. REMOVED EXISTING REPAIR DOUBLER RECONTOURED SKIN AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-04.

Part: SKIN — DENTED (BS 1266-1278) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN DENTED AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION AND PREVIOUS REPAIR DOUBLER PER SRM 53-04.

Part: SKIN — DENTED (PAX DOOR) · airframe 50,504 hrs · 26,544 cycles

FORWARD ENTRY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 50,504 hrs · 26,554 cycles

CUSP WEB CRACKED. REPLACED WEB PER SRM 51-10-4 AMD 51-30-2.

Part: SKIN — DENTED (BS 207-255) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN DENTED. REPAIRED PER SRM 53-04.

Part: VANE — CHAFED (TE FLAP) · airframe 50,504 hrs · 26,554 cycles

LEFTHAND WING OUTBOARD FLAP INBOARD VANE TRAILING EDGE IS CHAFED. REPAIRED DAMAGED AREA WITH BONDED FILLER AND DOUBLER PER SRM 51-70-2.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO DOOR CUTOUT LOWER BEAM CORRODED ON LOWER OUTBOARD FLANGE. REPLACED BEAM PER SRM 51 10 4 AND 51 30 5.

Part: SHEAR TIE — CORRODED (BS 693) · airframe 46,594 hrs · 24,688 cycles

FOUND FRAME SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 04 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1307-1322) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.

Part: WEB — CORRODED (BS 1155-1212) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO BAY THRESHOLD WEB CORRODED. REPLACED WEB PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: LONGERON — CORRODED (BS 1260-1320) · airframe 46,594 hrs · 24,688 cycles

FOUND LONGERON CORRODED. REPLACED DAMAGED SECTION OF LONGERON PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1307-1322) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 2.

Part: FRAME — CORRODED (BS 1322 S29LT RT) · airframe 46,594 hrs · 24,688 cycles

FOUND FRAME CORRODED. REPLACED DAMAGED SECTION OF FRAME BY INSTALLING FOUR REPAIR ANGLES AND FOUR SPLICE PLATES PER SRM 53 03 FIG 2A.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO DOOR DENTED ON UPPER HALF. REPLACED DAMAGED SECTION OF DOOR SKIN BY INSTALLING EXTERNAL SPLICE PLATE AND TWO FINGER DOUBLERS PER ALASKA AIR EA 5230 01312.

Part: SHEAR TIE — CORRODED (BS 1155) · airframe 46,594 hrs · 24,688 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1150-1155) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.

Part: CUSP WEB — CORRODED (BS 1098-1117) · airframe 46,594 hrs · 24,688 cycles

FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 05 FIG 96 AND 51 01 PARA 3 B.

Part: CUSP WEB — CORRODED (BS 1098-1117) · airframe 46,594 hrs · 24,688 cycles

FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 51 70 4.

Part: SHEAR TIE — CORRODED (BS 1174) · airframe 46,594 hrs · 24,688 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: SKIN — CORRODED (BS 1329-1334) · airframe 46,594 hrs · 24,688 cycles

FOUND FUSELAGE SKIN CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 04.

Part: SKIN — DENTED (BS 1252-1257) · airframe 46,594 hrs · 24,688 cycles

FOUND FUSELAGE SKIN DENTED. COLD WORKED DAMAGED SECTION. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SEA LINE CHECK, AFT EXIT, CATWALK, PATH EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR AND REPLACED LIGHT. LIGHT THEN OPERATED PROPERLY. (M)

Part: FLOOR PANEL — FRAYED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: FLOOR PANEL — FRAYED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FUSELAGE DENTED NEAR RIGHT ENGINE COWL DRAIN MAST. COLD WORKED AND INSTALLED REPAIR DOUBLER. (M)