AVIATION ADVISOR, INC.

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.

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.

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,

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.

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

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.

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

FUSELAGE SKIN DENTED. REPAIRED PER SRM 53-04.

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

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

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

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

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

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

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

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

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

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.

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

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

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

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

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

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

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

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

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

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

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

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