N498US

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,439 hrs · 51,003 cycles

PDX- EMERGENCY EXIT SIGN OVER COCKPIT ENTRANCE HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DETECTOR — INOPERATIVE · airframe 40,309 hrs · 50,886 cycles

PDX - LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,211 hrs · 50,794 cycles

PDX - THE AFT 3 CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED THE NUMBER 7 BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 40,191 hrs · 50,778 cycles

PDX - LEFT AND RIGHT AFT EVACUATION LIGHTS ON FUSELAGE WING/BELLY ARE INOPERABLE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 39,901 hrs · 50,536 cycles

BOI - FORWARD CABIN EXIT SIGN HAS BULBS BURNED OUT. REPLACED EXIT SIGN CIRCUIT BOARD IAW F-28 MAINTENANCE MANUAL, 33-50-00, PAGE 412 AND 413. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,336 hrs · 50,024 cycles

PDX- FORWARD FACING EXIT SIGN AT ROW 9 HAS 3 LIGHTS BURNED OUT. REMOVED AND REPLACED EXIT SIGN AS REQUIRED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 39,216 hrs · 49,914 cycles

PDX - FLIGHT CREW REPORTED SMALL HOLE AT INBOARD SECTION OF RIGHT WING FLAP. REPAIRED HOLE AS PER FOKKER STRUCTURAL REPAIR MANUAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 39,047 hrs · 49,742 cycles

SEA - ESCAPE PATH LIGHTING FOUND INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WITH SPLICE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,890 hrs · 49,597 cycles

SEA - THE EXIT SIGN ABOVE THE FLIGHT COMPARTMENT DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 38,714 hrs · 49,443 cycles

PDX- NR 1 COFFEE POT CIRCUIT BREAKER POPPED. F/A REPORTED SLIGHT ELECTRICAL SMELL. REMOVED AND REPLACED NR 1 COFFEE POT. RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTACLE — DEFECTIVE (GALLEY) · airframe 38,714 hrs · 49,443 cycles

SMF- ELECTRICAL SMELL IN GALLEY. NR 1 COFFEE CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 HOT JUG RECEPTICAL. INSPECTED, CLEANED AND LUBED NR 2 RECEPTICAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 39,818 hrs · 49,517 cycles

SEA - EXIT LIGHT GALLEY OVERHEAD INOP. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — ODOR (APU BAY) · airframe 38,501 hrs · 49,234 cycles

PDX- OIL SMELL IN CABIN. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: OIL TANK — ODOR (APU) · airframe 38,499 hrs · 49,234 cycles

BOI- STRONG FUEL SMELL IN FORWARD CABIN AND GALLEY AREA. REMOVED AND REPLACED APU OIL TANK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 38,499 hrs · 49,234 cycles

PDX- CABIN AND COCKPIT BOTH HAVE STRONG ODOR OF FUEL. ACCOMPLISHED BLEED AIR SYSTEM BLOWOUT OF BOTH AIR CONDITIONING PACK SYSTEMS DURING ENGINE RUN-UP. NO FURTHER FUEL ODOR NOTICED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 38,261 hrs · 49,012 cycles

SEA-#2 OVERHEAD EXIT SIGN HAS INOPERATIVE BULBS. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,260 hrs · 49,012 cycles

SEA - UPON INSPECTION, FOUND NR 2 OVERHEAD EXIT SIGN TO HAVE INOPERATIVE LAMPS. REMOVED AND REPLACED LAMP BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — INOPERATIVE (TAIL) · airframe 38,176 hrs · 48,941 cycles

MSO-CABIN FILLED WITH SMOKE, PROBABLE CAUSE IS APU.REMOVED AND REPLACED APU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 38,132 hrs · 48,895 cycles

SEA - GROUND PERSONEL FOUND RED WARNING LIGHT ILLUMINATED ON CARGO AREA SMOKE DETECTOR. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — DISLODGED (SEAT 9) · airframe 38,039 hrs · 48,821 cycles

SEA - EXIT LIGHT COVER AT SEAT 9B BECAME DISLODGED. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 37,537 hrs · 48,357 cycles

GEG - FORWARD CABIN EXIT SIGN WAS FOUND TO HAVE SEVERAL LAMPS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,844 hrs · 47,686 cycles

PDX - CENTER OVER HEAD CABIN EMERGENCY EXIT SIGN WAS REPORTED INOPERATIVE. REMOVED AND REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,844 hrs · 47,686 cycles

PDX - FORWARD CABIN EMERGENCY EXIT SIGN FOUND TO HAVE BURNT OUT LIGHT SEGMENTS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,731 hrs · 47,580 cycles

PDX-EVACUATION LIGHT AT SERVICE/EMERGENCY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND POWER WIRE FROM BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,731 hrs · 47,580 cycles

PDX- EVACUATION AND EMERGENCY LIGHTS ON FORWARD FLIGHT ATTENDANT PANEL INTERMITTANT. REMOVED AND REPLACED LIGHT ASSEMBLY IN FORWARD FLIGHT ATTENDANT PANEL.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 36,593 hrs · 47,440 cycles

GEG - UPON INSPECTION, FOUND FORWARD CABIN OVERHEAD EXIT SIGN WITH BURNT OUT SEGMENTS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — CRACKED (RUDDER) · airframe 36,579 hrs · 47,425 cycles

PDX- RUDDER LEADING EDGE RIB NR 4 HAS A CRACK APPROXIMATELY 1.25 INCH LONG LOCATED AT LEFT HAND SIDE OF RIB. REPAIRED IAW HORIZON AIR EA 4-55-217.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THREE DEEP CREASES IN VERTICAL SKIN LEFT SIDE BETWEEN FRONT SPAR AND SPAR I, BETWEEN RIB 5.0 AND 3.8. REPAIRED IAW HORIZON AIR EA 4-55-213.

Part: BEAM — DAMAGED (PRESS BULKHEAD) · airframe 36,579 hrs · 47,425 cycles

PDX- REAR PRESSURE BULKHEAD BEAM III REQUIRES REPAIRED IAW FOKKER SRM 53-02-18 AT AREA OF PREVIOUS REPAIR AT APPROXIMATELY BL 800 LEFT. REPAIRED IAW HORIZON AIR EA 4-53-1055 C.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP ON FRAME 17565 BETWEEN STRINGERS 8 - 9. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601A.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX-NUMEROUS DENTS 6 INCHES FROM FORWARD LOWER RADIUS OF AFT CARGO DOOR APERTURE. DENTS ARE IN AFT CARGO PIT DOOR APERTURE. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 51-31-01.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- STRINGER 71 FORWARD END HAS EDGE DAMAGE. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-01-01 PAGE 5.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP ON FRAME 17565 BETWEEN STRINGERS 7 - 5. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601A AND 53-01-13 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP ON FRAME 17565 BETWEEN STRINGERS 9 - 10. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- POSSIBLE CRACKS AT RIGHT VERTICAL CONNECTION ANGLE RADIATING FROM HI-LOKS AT SPAR II. REPAIRED IAW FOKKER SRM 55-31-00 FIGURE 1 AND 51-30-02.

Part: FRAME — TOOL DAMAGE (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS TOOLING DAMAGE TO CONNECTION ANGLE ON FRAME 16-2 AT STRINGER 34. REPAIRED IAW HORIZON AIR EA 4-53-1158.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A DENT IN THE EXTERIOR FUSELAGE SKIN APPROXIMATELY 3 INCHES FORWARD OF THE CUTOUT FOR ACCESS PANEL 41A, ALONG STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-02 FIGURE 1 AND 53-00-00.

Part: ATTACH FITTING — CRACKED (VERTICAL TO BODY) · airframe 36,579 hrs · 47,425 cycles

PDX- VERTICAL STABILIZER TO FUSELAGE LEFT HAND CONNECTION ANGLE IS CRACKED AT HI-LOK FASTENER, AT THE NR 2 INTERMEDIATE SPAR. REPAIRED IAW FOKKER SRM 55-31-00 FIGURE 1, 51-31-01 AND 51-31-02.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT FRAME 3820, 25 LEFT OF CL, BELOW FLOORBOARD SUPPORT. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-30-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- ONE DENT 2 INCHES LONG .035 DEEP 8 AFT FRAME 18075 ABOVE STRINGER 63. THIS DENT IS OUT OF LIMITS ASPECT RATIO IS 14 MUST BE GREATER THAN 30. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 AND 53-00-00.

Part: ANGLE — CHAFED (MLG DOOR) · airframe 36,579 hrs · 47,425 cycles

PDX- ANGLE IS CHAFED THROUGH WHERE THE RIGHT HAND INBOARD MAIN LANDING GEAR DOOR AFT OUTBOARD EDGE CONTACTS THE FUSELAGE FAIRING. REPAIRED IAW HORIZON AIR EA 4-57-410.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LOOSE AND SMOKING HI-LOKS AT RIGHT HAND VERTICAL CONNECTION ANGLE SPAR II. REPAIRED IAW FOKKER SRM 51-30-02.

Part: SKIN — GOUGED (PAX DOOR) · airframe 36,579 hrs · 47,425 cycles

PDX- GOUGES ON MAIN CABIN DOOR AND MAIN CABIN DOOR APERTURE AFT OF HINGE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3 AND 51-10-4 PAGES 8-9.

Part: DOOR FRAME — MISDRILLED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SERVICE/EMERGENCY DOOR UPPER DOOR FRAME TORSION BOX AT STATION 3870 HAS DRILL HOLES IN BOX. REPAIRED IAW HORIZON AIR EA 4-53-1173 AND FOKKER SRM 51-31-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN THE CONNECTION ANGLE ON THE FORWARD SIDE OF FRAME 17565 AND STRINGER 50. REPAIRED IAW FOKKER SRM 53-10-05 FIGURE 602.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS AN AREA WITH DELAMINATION ON UNDERSIDE OF LEFT HAND INBOARD FLAP, NEAR TRAILING EDGE AT APPROXIMATELY STATION 2100. REPAIRED IAW FOKKER SRM 51-70-0.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD CARGO DOOR APERTURE ON AIRCRAFT SIDE HAS CHAFING (AFT UPPER SIDE). REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-01-01 PAGE 3.

Part: RIVET — WRONG PART (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- NON-SRM GROUP OF RIVETS INSTALLED IN 6 X 6 AREA OF NOSE LANDING GEAR BAY RIGHT HAND SIDEWALL FORWARD OF FRAME 2650. OUT OF 19 RIVETS, 6 ARE OVERLAPING. REPAIRED IAW HORIZON AIR EA 4-53-11-66.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 36,579 hrs · 47,425 cycles

PDX- CENTER CARGO DOOR AT FORWARD APERTURE HAS CHAFING. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-01-01 PAGE 3.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- ONE DENT 21/4 LONG AND .060 DEEP, 8 AFT OF FRAME 18075 BETWEEN STRINGERS 68 AND 69 UNDER OBLIQUE FRAME 16-2. THIS DENT IS OUT OF LIMITS, ASPECT RATIO IS 16, MUST BE GREATER THAN 30 PER SRM 53-01-00. REPAIRED IAW FOKKER SRM 53-02-03 FIGURE 3 AND 53-00-00.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LIGHT CORROSION AT AFT CABIN SPLICE ANGLE LOCATED AT FRAME 15205 AND STRINGER 18. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LIGHT CORROSION AFT CABIN SPLICE ANGLE, LOCATED AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 51-10-01 PAGE 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS AN AREA WITH DELAMINATION ON UNDERSIDE OF LEFT HAND INBOARD FLAP, NEAR TRAILING EDGE AT APPROXIMATELY STATION 2800. REPAIRED IAW FOKKER SRM 51-70-00.

Part: SKIN — CRACKED (OVERWING EXIT) · airframe 36,579 hrs · 47,425 cycles

PDX - LEFT HAND OVERWING EXIT DOOR HAS CRACKS ON OUTER SKIN AT RADIUS. REPAIRED IAW FOKKER SRM 51-31-05, 52-02-03 AND 51-31-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- EXFOLIATION CORROSION ON THE RIGHT HAND INBOARD SEAT TRACK 11 INCHES AFT OF FRAME 9805 ON TOP OF TRACK. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SKIN — CHAFED (OVERWING EXIT) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OVERWING EXIT DOOR OUTER SKIN IS CHAFED ON TOP. REPAIRED IAW FOKKER SRM 52-01-01 AND 51-10-4.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- TWO CHAFED AREAS ABOVE LEFT AFT OVERWING EXIT. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5. REFER TO HORIZON AIR EA 4-53-1159 FOR FASTENER INSTALLATION.

Part: SKIN — CRACKED (OVERWING EXIT) · airframe 36,579 hrs · 47,425 cycles

PDX- RIGHT HAND AFT OVERWING EXIT DOOR UPPER AFT CORNER IS CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 51-31-01, 52-02-03 AND 51-31-05.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- TWO CHAFED AREAS ABOVE LEFT FORWARD OVERWING EXIT. REFER TO HORIZON AIR EA 4-53-1159.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CHAFED AREA ABOVE RIGHT AFT OVERWING EXIT. REPAIRED IAW HORIZON AIR EA 4-53-1160, AND FOKKER SRM 53-01-01 PAGE 5.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACKED CONNECTION ANGLE AT FRAME 32-2 AND STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5.

Part: BRACKET — CRACKED (WINDOW POST) · airframe 36,579 hrs · 47,425 cycles

PDX- CENTER WINDOW POST BEAM TO THE FPB BRACKET, UPPER RIGHT HAND BRACKET FLANGE IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1172.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FUSELAGE SKIN HAS MINOR CORROSION PITS UNDER NAV/COM UPPER ANTENNA BASE PLATE. REPAIRED IAW WORK CARD 4-420.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 36,579 hrs · 47,425 cycles

PDX- RIGHT HAND UPPER ANTI-UPFLOAT CABLE IS CHAFING ON THE NR 1 LIFTDUMPER OUT HYDRAULIC LINE B-NUT DIRECTLY ABOVE THE NR 2 MAIN LANDING GEAR. THE CABLE HAS APPROX 50 PERCENT WEAR. REPAIRED IAW FOKKER SRM 27-11-00 PAGE 512.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD BELLY SKIN HAS CORROSION UNDER LOWER VHF COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4, COMPLIED WITH HORIZON AIR EA 4-53-1161.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- VERTICAL GILL LINER SUPPORT ANGLE IN FORWARD CARGO PIT AT FRAME 4175 HAS CHAFED AGAINST THE AFT SKIN OF THE NOSE LANDING GEAR STRUT PRESSURE BOX HUMP. REPAIRED IAW HORIZON AIR EA 4-53-1164.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FUSELAGE SKIN IS CRACKED APPROXIMATELY 3.4 AT STRINGER 55 AND FRAME 3050, BELOW AND AFT OF PILOT''S ''D'' WINDOW. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, 53-02-02 AND 53-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE IS EXFOLIATED IN TWO SPOTS BETWEEN FRAMES 4900 AND 5305. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 53-40-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- AFT FUSELAGE SKIN CORROSION UNDER NR 2 DME ANTENNA MOUNT. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: CLIP — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK IN FRAME CLIP, FRAME 13815B BETWEEN STRINGERS 2 & 3. REPAIRED IAW FOKKER SRM 53-02-13 AND FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN A CLIP REPAIR AT FRAME 41-2 AND STRINGER 31. REPAIRED IAW FOKKER SRM 51-30-02 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN THE CLIP REPAIR ON FRAME 20075 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 4 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CLIP AT FRAME 3050 AND STRINGER 17 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK IN FRAME CLIP, FRAME 13815B, BETWEEN STRINGERS 73 & 72. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP REPAIR ON FRAME 41-2 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-30-02 AND 51-31-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SERVICE/EMERGENCY DOOR UPPER APERTURE IS WORN ON FORWARD AND AFT SIDE. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — GOUGED (FUSELAGED) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE IN CENTER OF TRACK AT STATION 8515. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04, PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LIGHT CORROSION ON THE RIGHT HAND INBOARD SEAT TRACK LOCATED 6.5 INCHES AFT OF FRAME 15205. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD CARGO BAY FRAME 6805 HAS CORROSION IN FRAME GROOVE AREA. REPAIRED IAW HORIZON AIR EA 4-53-1147.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FUSELAGE SKIN DENTED BELOW LEFT STUBWING, BELOW STRINGER 17 BETWEEN FRAME 16060 AND FRAME 16660. REPAIRED IAW HORIZON AIR EA 4-53-1155 AND FOKKER SRM 53-01-01 PAGE 8.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK HAS NICKS FROM FRAME 9805 TO FRAME 14285. REPAIRED IAW FOKKER SRM 53-40-01, 53-01-01, AND 51-10-4 PAGE 8.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FUSELAGE SKIN DENTED FROM INSIDE, BELOW LEFT STUBWING AT STRINGER 20 FORWARD OF FRAME 16660. REPAIRED IAW HORIZON AIR EA 4-53-1154 AND FOKKER SRM 53-01-01 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK OUTBOARD FLANGE HAS CORROSION FROM STATION 9305. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- NICK .001 INCH DEEP ACROSS TOP INBOARD OF LEFT HAND SEAT TRACK AT STATION 16202 AND FRAME 13815B. REPAIRED IAW FOKKER SRM 53-40-01 AND 51-10-4 PAGE 8.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD CARGO BAY FRAME 6805 ABOVE STRINGER 74 CROSS CONNECTION HAS TWO NUT PLATES WITH EXFOLIATION CORROSION ON THE UNDERSIDE. REPAIRED IAW HORIZON AIR EA 4-53-1147.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN THE CONNECTION ANGLE ON THE AFT SIDE OF FRAME 50-2 AND STRINGER 25. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 11794 FRAME 10346. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER 51-10-4, PAGE 8, PARAGRAPH 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 8565. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-4.

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- BRACE BETWEEN FRAME 16660 AND 16060 IS DENTED ABOVE STRINGER 33, 2 TO 3 INCHES FORWARD OF FRAME 16660. REPAIRED IAW HORIZON AIR EA 4-53-1156 AND FOKKER SRM 51-11-4 PAGE 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK FLANGE INBOARD HAS CORROSION FROM STATION 16495 FRAME 4285 TO STATION 11253 FRAME 9805. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS CORROSION FROM STATION 11253 FRAME 9805 TO STATION 4850 FRAME 4900. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN RADIUS OF RIGHT HAND INBOARD SEAT TRACK 7 INCHES FROM FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS SEVERAL SMALL AREAS OF PITTING CORROSION LOCATED BETWEEN FRAMES 3820 AND 4610. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSIN IN RADIUS OF THE RIGHT HAND INBOARD SEAT TRACK 5 INCHES AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE ON INBOARD FLANGE AT CAMLOC RECEPTICLE STATION 8405. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04, PAGE 9 AND FOKKER SRM 53-01-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CHAFING DAMAGE TO LOWER AFT CORNER OF MAIN CABIN DOOR APERTURE. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-01-01 PAGE 3 AND 5.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK HAS NICKS FROM FRAME 4900 TO FRAME 4805. REPAIRED IAW FOKKER SRM 53-40-01 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK IS CHAFED ON OUTBOARD FLANGES BETWEEN STATIONS 12414 AND 12224. REPAIRED IAW FOKKER SRM 53-01-01, 53-40-01 AND 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK AFT OF FRAME 3820. REPAIRED IAW FOKKER SRM 50-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX-LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE IN TOP FLANGE AT OUTBOARD STATION 8770. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 202, PARAGRAPH 4B, STEP 6 AND FOKKER SRM 51-10-04, PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND SEAT TRACK HAS CORROSION AT STATION 15263 (FRAME 13815). REPAIRED IAW FOKKER SRM 51-10-4, 53-40-01 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND SEAT TRACK HAS CORROSION AT STATION 14323, FRAME 12875. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE ON OUTBOARD SIDE FLANGE AT STATION 8435. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-04, PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK, CORROSION LOCATED APPROXIMTELY 5 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE IN OUTBOARD FLANGE AT STATION 9050. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 51-10-4, PARAGRAPH 4B.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS GOUGE IN TOP OF TRACK AT STATION 9545. REPAIRED IAW FOKKER SRM 53-40-01 AND FOKKER SRM 53-01-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CHAFING DAMAGE TO LOWER FORWARD CORNER OF MAIN CABIN DOOR APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, 53-01-01 PAGE 3 AND 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN RIGHT HAND INBOARD SEAT TRACK 6 INCHES AFT OF FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND INBOARD SEAT TRACK HAS CORROSION AT STATION 13853, FRAME 12405. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN CENTER OF RIGHT HAND INBOARD SEAT TRACK, 8 INCHES AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FRETTING CORROSION LEFT HAND AND RIGHT HAND FLOOR PANEL SUPPORT FLANGES OF THE RIGHT HAND INBOARD SEAT TRACK, BETWEEN FRAMES 8305 AND 9305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN CENTER OF RIGHT HAND INBOARD SEAT TRACK AT FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SEVERAL AREAS OF LIGHT FRETTING CORROSION ON FLOOR PANEL SUPPORT FLANGES OF THE RIGHT HAND OUTBOARD SEAT TRACK, BETWEEN FRAMES 7305 AND 9305B. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION ON THE INBOARD UPPER FLANGE OF THE RIGHT HAND INBOARD SEAT TRACK LOCATED APPROX 7 FT AFT OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04 AND 53-40-01.

Part: CLIP — CRACKED (FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK IN FRAME CLIP, FRAME 13815A BETWEEN STRINGER 2 & 3. REPAIRED IAW FOKKER SRM 53-02-11 PAGE 2 FIGURE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LIGHT CORROSION NEAR NUT PLATE HOLE ON THE RIGHT HAND INBOARD SEAT TRACK 8 INCHES FROM FRAME 8805. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN CENTER AND IN THE RADIUS OF THE RIGHT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SEVERAL AREAS OF CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK BETWEEN FRAMES 4610 AND 4850. REPAIRED IAW FOKKER SRM 53-40-01 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN CENTER OF RIGHT HAND INBOARD SEAT TRACK AT FRAME 8305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS SEVERAL AREAS OF PITTING CORROSION LOCATED BETWEEN FRAMES 4850 AND 5305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FRETTING CORROSION ON LEFT HAND AND RIGHT HAND FLOOR PANEL SUPPORT FLANGES OF THE RIGHT HAND INBOARD SEAT TRACK BETWEEN FRAMES 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FRETTING CORROSION ON LEFT HAND AND RIGHT HAND FLOOR PANEL SUPPORT FLANGES OF THE RIGHT HAND INBOARD SEAT TRACK BETWEEN FRAMES 5805 AND 6305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN RADIUS OF RIGHT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LIGHT CORROSION ON THE OUTBOARD UPPER FLANGE OF THE RIGHT HAND INBOARD SEAT TRACK AT FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04 AND 53-40-01.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CHAFE DAMAGE IN CENTER OF THE RIGHT HAND INBOARD SEAT TRACK LOCATED 10.5 INCHES AFT OF FRAME 5305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SEVERAL GOUGES IN RIGHT HAND OUTBOARD SEAT TRACK LOCATED 2 INCHES FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- SEVERAL GOUGES IN RIGHT HAND OUTBOARD SEAT TRACK. DAMAGE IS LOCATED 8 INCHES AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- TWO GOUGES ON RIGHT HAND OUTBOARD SEAT TRACK. DAMAGE LOCATED 8.5 INCHES AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FRETTING CORROSION ON LEFT HAND AND RIGHT HAND FLOOR PANEL SUPPORT FLANGES ON THE RIGHT HAND INBOARD SEAT TRACK BETWEEN FRAMES 6305 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: CLIP — CRACKED (FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN A CLIP REPAIR AT FRAME 16-2 AND STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 FIGURE 4.

Part: CLIP — CRACKED (FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE IS A CRACK IN A CLIP AT FRAME 16-2 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 FIGURE 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FRETTING CORROSION ON LEFT HAND AND RIGHT HAND FLOOR PANEL SUPPORT FLANGES OF THE RIGHT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 AND 51-10-4.

Part: CLIP — CRACKED (FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK IN FRAME CLIP, FRAME 13815A BETWEEN STRINGERS 73 & 72. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND FOKKER SRM 51-31-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PITTING CORROSION IN CENTER OF RIGHT HAND INBOARD SEAT TRACK 4 INCHES AFT OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD CARGO BAY FRAME 9305A AND STRINGER 74 CROSS CONNECTION HAS TWO BROKEN OFF SCREWS IN NUT PLATES. UPON REMOVAL OF NUT PLATES FOUND CORROSION ON FRAME 9305A AND STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-1146.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- FORWARD CARGO BAY FRAME 7305 HAS CORROSION ON UNDERSIDE OF UPPER FLANGE AROUND NUT PLATES BETWEEN STRINGER 74 AND 1. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND 51-10-4.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- AFT SPAR RIB 3 AND 4 LOOKING THROUGH PANE L57E HAS MISSING FASTENERS ON REAR SPAR AND IS CRACKED AND LOOSE ON RUDDER COVE. REPAIRED IAW FOKKER SRM 51-31-01, 51-31-05, 51-30-02 AND 55-31-04.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND VERTICAL CONNECTION ANGLE CRACKED AT SPAR 2 BETWEEN HI-LOKS. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 55-31-00 FIGURE 1.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT CABIN FRAME 10966 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: PANEL — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- PANEL 74A HAS FRETTING CORROSION ON INNER SURFACE. REPLACED PANEL.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CLIP CRACKED AT FRAME 10966 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: PANEL — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- PANEL 72A HAS FRETTING CORROSION ON INNER SURFACE. REPAIRED IAW FOKKER SRM 51-10-04 AND 57-01-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- PANEL 85C HAS FRETTING CORROSION ON INNER SURFACE OF PANEL. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 57-01-01.

Part: PANEL — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- PANEL 74B HAS FRETTING CORROSION ON INNER SURFACE. REPAIRED IAW FOKKER SRM 51-10-4 AND 57-01-01.

Part: BEAM — CRACKED (BULKHEAD) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK IN LIGHTENING HOLE, BOTTOM SIDE OF HORIZONTAL BEAM 3, ON FORWARD FACE OF AFT PRESSURE BULKHEAD IN AFT CARGO PIT. REPAIRED IAW HORIZON AIR EA 4-53-1121.

Part: SKIN — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- OPENING ON WING FOR PANEL 72A HAS FRETTING CORROSION ON MOUNTING SURFACES FOR PANEL. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT CABIN FRAME 10346 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 36,579 hrs · 47,425 cycles

PDX- HORIZ STAB JUNCTION FITTING HAS A PIT ON THE LEFT HAND UPPER LUG, ON THE INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 4-55-212.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- THERE ARE 7 RIVETS WITH HEADS POPPED OFF IN THE AREA JUST FORWARD OF APU EXHAUST OUTLET. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX-TWO GOUGES IN FUSELAGE SKIN NEXT TO AFT CARGO DOOR FORWARD APERTURE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6B AND 2B, SRM 53-24-01, PAGE 14-15, FIGURE 3, AND 53-24-08, PAGE 2-3.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT CABIN FRAME 10966 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: PANEL — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- OPENING ON WING FOR PANEL 74A HAS FRETTING CORROSION ON MOUNTING SURFACE FOR PANEL. REPAIRED IAW FOKKER SRM 51-10-4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT CABIN FRAME 10346 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: PANEL — CORRODED (WING) · airframe 36,579 hrs · 47,425 cycles

PDX- OPENING ON WING FOR PANEL 74B HAS FRETTING CORROSION ON MOUNTING SURFACE FOR PANEL. REPAIRED IAW FOKKER SRM 51-10-4 AND 57-01-01 PAGE 5.

Part: PANEL — CORRODED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- OPENING ON WING FOR PANEL 74C HAS FRETTING CORROSION ON MOUNTING SURFACE FOR PANEL. REPAIRED IAW FOKKER SRM 51-10-4 AND 57-01-01 PAGE 5.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 47R. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT FRAME 12405 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: PANEL — CHAFED (ACM BAY) · airframe 36,579 hrs · 47,425 cycles

PDX- LEFT HAND AIR CYCLE MACHINE COMPARTMENT LOWER FORWARD CORNER OF PANEL 23A OPENING HAS CHAFE DAMAGE TO INSIDE SKIN. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3 AND 53-01-01 PAGE 5.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2, AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 33R. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 16A. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT FRAME 12875 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 18. REPAIRED IAW FOKKER SRM 51-1-04, 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 21. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACK AT MAIN CABIN DOOR APERTURE, FORWARD LOWER END OF UPPER TORSION BOX. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND PAGES 8 AND 9.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 33R. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-12 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12875 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12875 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 28. REPAIRED IAW FOKKER SRM 51-10-04, 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CASTELLATION AT AFT CABIN FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 46,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12875 AND STRINGER 21. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815A AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 13815B AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 53-02-15 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX - CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 21A. REPAIRED IAW FOKKER 53-02-13, FIGURE 2 AND FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12875 AND STRINGER 33R. REPAIRED IAW FOKKER SRM 53-02-12 FIGURE 1.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 42R. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND FOKKER SRM 51-31-01 AND FOKKER SRM 53-02-11, FIGURE 1 AND FOKKER SRM 51-10-01, PARAGRAPH 4B, PAGE 9.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 15205 AND STRINGER 58A. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2, AND 53-02-15 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 36,579 hrs · 47,425 cycles

PDX- CRACKED CLIP AT AFT CABIN FRAME 12405 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 36,339 hrs · 47,185 cycles

GEG- EXIT SIGN AT COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN AT COCKPIT DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RT UNIT — FAILED (RADAR SYS)

HLN - ELECTRICAL SMOKE COMING FROM RADIO RACK, TOP LEFT AREA. REMOVED AND REPLACED RADAR RECEIVER TRANSMITTER, OPERATIONAL CHECK GOOD.

Part: SIGN — INOP (CABIN)

PDX- CENTER OVERHEAD FORWARD AND AFT EMERGENCY EXIT SIGNS, 28V BULBS INOPERATIVE. REPLACED BOTH FORWARD AND AFT CENTER AISLE EMERGENCY LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOI - MAINTENANCE REPORTS AFT EXTERIOR LIGHTS DO NOT SHUT OFF WITH SWITCH. REPLACED AFT EMERGENCY POWER SUPPLY. CYCLED LIGHTS: OPERATIONAL CHECK IS NORMAL.

Part: WIRE — BROKEN (ROW 10B)

PDX - EMERGENCY EVACUATION EXIT LIGHTS FROM SEATS 10B AND AFT ILLUMINATED. MAINTENANCE REPAIRED WIRES ON BATTERY PACK CONNECTOR AT SEAT 14A, OPERATIONAL TEST NORMAL.

Part: ACTUATOR — LEAKING (NLG DOOR)

NOSE GEAR DOOR ACTUATOR, MFG MENASCO, LEAKING CAUSING SYSTEM HYDRAULIC FLUID TO DRAIN. CREW HAD TO RELY ON BACKUP SYSTEM TO EXTEND LANDING GEAR DOOR. RE: QXEA.

Part: SIGN — INOP (PAX DOOR)

EXIT SIGN IN MAIN CABIN OVER COCKPIT DOOR HAS SEVERAL BULBS OUT. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN ASSEMBLY, OPERATIONAL TEST WAS NORMAL.

Part: POWER SUPPLY — INOP (ROW 2 & 4)

EVACUATION LIGHTS AT ROWS 2 AND 4 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (ROW 8 &14)

BOI - CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 8 AND 14. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT AT ROW 8A INOP. REMOVED AND REPLACED LAMP AT ROW 8A, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

OVERWING EXIT LIGHTS AT ROWS 8A AND 9A INOP. REMOVED AND REPLACED LAMPS AT ROWS 8A AND 9A, OPERATIONAL CHECK GOOD.

Part: PACK — MALFUNCTIONED (NR 2)

BOI - CREW NOTED SMOKE SMELL AND VIBRATION. TURNED NR 2 PACK OFF, SMOKE AND VIBRATION STOPPED. MAINTENANCE PLACED NR 2 PACK ON MEL.

Part: FAIRING — DENTED (WS 1800)

DENT IN SKIN PLANE FAIRING WEB RIGHT-HAND LOWER WING APPROXIMATELY STATION 1800. REPAIRED IAW HORIZON AIR EA 4-57-138.

Part: COVER — CRACKED (NLG WW)

CRACK AT NOSE GEAR BAY TOP COVER, STATION 2475. REPAIRED IAW HORIZON AIR EA 4-53-532.

Part: SKIN — DELAMINATED (LT TE FLAP)

LEFT-HAND OUTBOARD LEADING EDGE DELAMINATING AT PREVIOUS REPAIR. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 15.

Part: STRINGER — DAMAGED (FRAME 5805)

STRINGERS 15 AND 16 HAVE NICKS AT SKIN FLANGE RADIUS IN AREA OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 9 FIGURE 4.

Part: SKIN — DENTED (WING)

DENT IN LOWER WING SKIN AFT OF NR 2 LIFT DUMPER BELL CRANK. REPAIRED IAW FOKKER SRM 57-02-04, PAGE 2, FIGURE 1 AND SRM 51-31-04.

Part: ACTUATOR — FAILED (LT MLG DOOR)

BOTH LEFT-HAND INBOARD GEAR DOOR ACTUATOR BEARINGS FELL OUT. REPLACED LEFT-HAND FORWARD AND AFT ACTUATORS IAW FOKKER SRM 32-32-14, PAGE 201, 3A, B, C AND D STEP 1.

Part: SKIN — DAMAGED (LT TE FLAP)

LEFT-HAND WING INBOARD FLAP VANE HAS ROCK DAMAGE TO LOWER SKIN AT FIRST 48 INCHES FROM INBOARD EDGE. REPAIRED IAW FOKKER SRM 51-70-00, PARAGRAPH 5A(2), SRM 51-70-0 METHOD 1 PARAGRAPH 7, HORIZON AIR EA 4-57-152 AND MAINTENANCE MANUAL 27-50-02.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73H OPENING HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73A OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73G OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 71A OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73C OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73D OPENING HAS FRETTING EROSION AROUND SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73J OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73B OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73E OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162.

Part: SKIN — DENTED (FUSELAGE)

DENT .069 INCH DEEP, 6 INCHES AFT OF FRAME 18075 AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 6 AND 7, FIGURE 3, SRM 51-31-01, SRM 51-30-02, PAGE 10.

Part: SKIN — DAMAGED (SERVICE DOORWAY)

SERVICE EMERGENCY DOOR OPENING LOWER LEFT HAND CORNER HAS A TOOLING CUT .25 WIDE BY .1875 DEEP IN THE 3RD AND 4TH SHEETMETAL LAYERS. REPAIRED IAW HORIZON AIR EA 4-53-527.

Part: BEAM — DAMAGED (CARGO DOOR)

AFT CARGO DOOR HAS IMPACT DAMAGE ON UPPER BEAM AFT CORNER. REPAIRED IAW HORIZON AIR EA 4-52-150.

Part: CASTELLATION — FAILED (FRAME 16660)

ONE INCH BREAK IN FRAME CASTELLATION AT FRAME 16660 OUTBOARD OF STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: BEAM — DAMAGED (CARGO DOOR)

AFT CARGO DOOR FORWARD LOWER CORNER HAS IMPACT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01.

Part: BEAM — DAMAGED (CARGO DOOR)

AFT CARGO DOOR INNER BEAM HAVE IMPACT DAMAGE NEXT TO HINGE ASSEMBLY. REPAIRED IAW HORIZON AIR EA 4-52-150.

Part: SKIN — DAMAGED (CARGO DOOR)

AFT CARGO DOOR OUTER SKIN LOWER AFT CORNER AT DOOR HINGE ATTACHMENT HAS TOOLING DAMAGE. REPAIRED IAW HORIZON AIR EA 4-52-150.

Part: DOOR — CORRODED (CARGO COMPT)

AFT CARGO DOOR HAS CORROSION AT WEB AT AFT LOWER CORNER. REPAIRED IAW FOKKER SRM 52-01-01.

Part: SKIN — DAMAGED (FRAME 6305)

DENT .055 INCH PROTRUDING OUT ON LEFT-HAND SIDE OF FUSELAGE SKIN 9 AFT OF FRAME 6305. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, RIG 1 AND SRM 53-01-01, PAGE 9, 6 A-D.

Part: BRACKET — CRACKED (BS 1700)

CRACK IN RADIUS/NECK OF T-ATTACH BRACKET FOR Z STRINGER 2.18, STATION 1700R. REPAIRED IAW FOKKER SRM 51-31-01.

Part: FRAME — CRACKED (FRAME 13815)

FRAME 13815B AT STRINGER 74 HAS A CRACK UNDER GILL LINER SUPPORT CONNECTION BRACKET. REPAIRED IAW HORIZON AIR EA 4-53-524.

Part: BULKHEAD WEB — PUNCTURED (FWD PRESS BLKHD)

SMALL PUNCTURE (.025) IN SKIN AT LEFT HAND END OF FRAME NR 7 ON FRONT PRESSURE BULKHEAD. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2.

Part: PANEL — CRACKED (WS 4837.5)

CRACKED Z STRINGER, LEFT WING, FUEL PANEL 73B, STATION 4837.5, STRINGER 2.13. REPAIRED IAW HORIZON AIR EA 4-57-155.

Part: CABLES — RUSTED (TE FLAPS)

FOUR SEGMENTS OF FLAP DRIVE CABLES IN HYDRAULIC TUNNEL HAVE RED RUST CORROSION FROM FRONT BULKHEAD TO SWITCH UNIT. REPAIRED IAW FOKKER SRM 20-30-09 AND SRM 27-51-00, PARAGRAPH B, STEPS 1 THRU 54.

Part: FRAME — CRACKED (FRAME 7805)

FRAME 7805 IS CRACKED. DIRECTLY ABOVE STRINGER 73. REPAIRED IAW HORIZON AIR EA 4-53-522.

Part: SKIN — DENTED (FUSELAGE)

THERE ARE TWO DENTS BELOW AND FORWARD OF SCAB PATCH ABOVE LAV SERVICE PANEL STATION 18870. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1.

Part: CASTELLATION — CRACKED (FRAME 16660)

FRAME 16660 CASTELLATION AT STRINGER 1 HAS A TWO INCH CRACK IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-12 AND 51-31-01.

Part: WEB — CARGO (CARGO DOOR)

AFT CARGO DOOR HAS A CRACK WEB JUST INSIDE BEAR FRAME. REPAIRED IAW FOKKER SRM 52-30-00, 51-31-01 AND 51-30-02.

Part: SKIN — DENTED (BS 18870)

SCAB PATCH ABOVE LAV SERVICE PANEL STATION 18870 HAS DENT IN PATCH. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 2.

Part: FRAME — CRACKED (CARGO DOOR)

AFT CARGO DOOR FORWARD LOWER BEAM FRAME HAS CRACK AT NUT PLATE. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 52-30-00.

Part: STRIP — CRACKED (NLG WW)

TYPE 2 CRACKS (LEFT AND RIGHT) AT INNER FRAME STRIP AFT SIDE OF NOSE LANDING GEAR WHEEL BAY. REPAIRED IAW HORIZON AIR EO 4-53-33B.

Part: STIFFENER — CRACKED (FRAME 11905)

CRACK AT BOTTOM OF STIFFENER 4TH STIFFENER FROM FRAME 11905, RIGHT SIDE, IN BLEED AIR TUNNEL, UNDER PANEL 26A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: EXHAUST — CRACKED (RT ACM)

RIGHT-HAND ACM EXHAUST DUCT CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-05.

Part: FRAME — CRACKED (FRAME 11905)

CRACK IN FRAME 11905 IN BLEED AIR TUNNEL AT 5 O'CLOCK POSITION. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 8, 51-10-4 AND 51-31-01.

Part: CASTELLATION — CRACKED (FRAME4610)

CRACK IN THE CASTELLATION AT FRAME 4610 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: ANGLE — CRACKED (LT MLG WW)

LEFT-HAND WING UPPER LEFT-HAND MLG CONNECTION ANGLE (FROM WING TO MLG) CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 57-02-05.

Part: RIB — CHAFED (WING)

LEADING EDGE RIB BETWEEN PANEL 92J AND 62A IS CHAFED IN SEVERAL PLACES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 A-C AND HORIZON AIR EA 4-57-1573.

Part: SEAT TRACK — GOUGED (FRAME 13815)

RIGHT-HAND INBOARD SEAT TRACK INBOARD FLANGE 6 FORWARD OF FRAME 13815B HAS A .014 GOUGE .053 THICK. REPAIRED IAW FOKKER SRM 53-02-15, PAGES 3 AND 4 AND SRM 51-31-01.

Part: HOUSING — BROKEN (RUDDER)

RUDDER ACTUATOR TO RUDDER POST RETAINING BOLT ANTI ROTATION HOUSING IS BROKEN. REPAIRED IAW HORIZON AIR EA 4-27-52.

Part: CLIP — CRACKED (FRAME 41-2)

BACKSIDE OF FRAME 41-2 THERE IS A CRACKED FRAME CLIP AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 51-31-01.

Part: CASTELLATION — CRACKED (FRAME 13815)

FRAME CASTELLATION AT FRAME 13815B BETWEEN STRINGER 2 AND 3 HAS A 1.5 INCH CRACK IN RADIUS AND IS CRACKED AT THE RIVET. REPAIRED IAW FOKKER SRM 53-02-13.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73B HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154.

Part: SEAT TRACK — CHAFED (FRAME 9305)

RIGHT-HAND INBOARD SEAT TRACK BETWEEN FRAME 9305B AND 9305 HAS CHAFE DAMAGE INSIDE OF TRACK. REPAIRED IAW FOKKER SRM 53-02-15.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73C HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73A HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154.

Part: PANEL — FRETTING (WING)

FUEL PANEL 71A HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154.

Part: CASTELLATION — CRACKED (BS 13815)

FRAME CASTELLATION AT FRAME 13815B BETWEEN STRINGER 72 AND 73 HAS A 1.5 INCH CRACK IN RADIUS AND A 1 INCH CRACK AT RIVET. REPAIRED IAW FOKKER SRM 53-02-13.

Part: PANEL — FRETTING (WING)

FUEL PANEL 73D HAS FRETTING EROSION AROUND SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-154.

Part: CLIP — CRACKED (BS 13815)

CRACK ON CLIP TO FUSELAGE ATTACH POINT, STATION 13815B, NEAR LEFT CORNER WHERE PANEL 98H IS INSTALLED. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 7 AND 8.

Part: CLIP — CRACKED (BS 13815)

CRACK ON CLIP TO FUSELAGE ATTACH POINT, STATION 13815B. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 7 AND 8.

Part: BRACKET — CRACKED (NLG WW)

CRACK ON NOSEGEAR ATTACH FITTING INBOARD OF NOSE GEAR ACTUATOR ATTACH BRACKET. REPAIRED IAW HORIZON AIR EA 4-53-503.

Part: SEAT TRACK — CORRODED (FRAME14755-15205)

RIGHT-HAND INBOARD SEAT TRACK INNER FLOOR BOARD FLANGE HAS CORROSION FROM FRAME 14755 TO 15205. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 50-2)

ON BACKSIDE OF OBLIQUE FRAME 50-2 THERE ARE CRACKED FRAME CLIPS AT STRINGERS 25, 27 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND MM 53-10-5, PAGE 601-604.

Part: PINS — DAMAGED (EMER EXIT DOOR)

THREE LATCHING PINS HAVE DAMAGE AT THE ENGAGEMENT ENDS. REPLACED LATCHING PINS IAW HORIZON AIR EO 4-52-79A.

Part: CLIP — CRACKED (FRAME 50-2)

ON BACKSIDE OF FRAME 50-2 THERE ARE CRACKED FRAME CLIPS AT STRINGERS 49, 51 AND 52. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-4, 53-02-3 FIGURE 3 AND F-28 MM 53-10-05, PAGE 601.

Part: FRAME — MISREPAIRED (FRAME 41-2)

ON BACKSIDE OF FRAME 41-2 THERE IS A PREVIOUS REPAIR THAT IS NOT IN CONFORMITY WITH FOKKER SRM 53-02-13 AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-30-13, FIGURE 6.

Part: FRAME — CORRODED (FRAME 5305)

CORROSION AT NUT PLATE HOLE IN FRAME 5305 AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9 FIGURE 3 SECTION D-D.

Part: ANGLE — CRACKED (BS 3870)

BOTH FLOOR SUPPORT ANGLES CRACKED ON FUSELAGE KEEL BEAM AT BL600R, FRAME 3870. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-30-02.

Part: FRAME — CRACKED (FRAME 22293)

FRAME 22293 IS CRACKED IN TWO PLACES ON THE FORWARD RIGHT-HAND SIDE BETWEEN STRINGERS 55 AND 56. REPAIRED IAW HORIZON AIR EA 4-53-498, STEPS 1, 3-7, AND FOKKER SRM 51-30-01.

Part: CLIP — CRACKED (FRAME 7305)

FORWARD CARGO BAY CLIP CRACK AT FRAME 7305 STRINGER 66. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, 51-10-09, PAGE 9, PARAGRAPH 4, A-C AND 51-31-01, PAGE 13-17.

Part: SIDE WALL — CRACKED (BS 2570)

NOSE WHEEL BAY RIGHT-HAND STATION 2570 HAS CRACKS FROM A RIVET IN THE SIDE WALL SKIN. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9.

Part: SIDE WALL — CRACKED (BS 2970)

RIGHT-HAND NOSE BAY SIDE WALL STATION 2970 HAS CRACKS FROM A RIVET. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9.

Part: CLIP — CRACKED (FRAME 20075)

THERE ARE TWO CRACKED FRAME CLIPS ON THE BACK SIDE OF FRAME 20075 BETWEEN STRINGERS 33 AND 41. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 10.

Part: SIDE WALL — CRACKED (BS 2570)

NOSE WHEEL BAY LEFT-HAND STATION 2570 HAS CRACKS FROM A RIVET IN THE SIDE WALL SKIN. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9.

Part: CLIP — MISINSTALLED (FRAME 17565)

PREVIOUS CLIP REPAIR ON FRAME 17565 AT STRINGER 21 HAS IMPROPER FASTENERS PER FOKKER SRM 53-02-13. REPLACED FASTENERS IAW FOKKER SRM 51-30-02.

Part: CLIP — CRACKED (FRAME 24-2)

TWO CRACKED FRAME CLIPS ON THE BACK SIDE OF OBLIQUE FRAME 24-2 AT STRINGERS 46 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 5.

Part: CLIP — CRACKED (FRAME 17565)

THERE ARE TWO CRACKED FRAME CLIPS ON THE FORWARD SIDE OF FRAME 17565 AT STRINGERS 49 AND 50. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND SRM 51-10-4.

Part: CLIP — MISREPAIRED (FRAME 175465)

THERE IS A PREVIOUS CLIP REPAIR ON FRAME 17565 AT STRINGER 21 THAT HAS IMPROPER FASTENERS PER FOKKER SRM 53-02-13. REMOVED AND REPLACED FASTENERS IAW FOKKER SRM 51-30-02.

Part: FRAME — CRACKED (FRAME 17565)

PREVIOUS REPAIR ON FORWARD SIDE OF FRAME 17565 BETWEEN STRINGERS 51 AND 52 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3.

Part: CLIP — CRACKED (FRAME 16060)

CRACKED CLIP AT FRAME 16060 AND STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 16060)

CRACKED CLIP AT FRAME 16060 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305A AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 16060)

CLIP CRACK AT FRAME 16060 AND STRINGER 55A. REPAIRED IAW FOKKER 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

FRAME CLIP CRACKED AT FRAME 9305A STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305A AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 8305)

FRAME CLIP CRACKED AT FRAME 8305 STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305 AT STRINGER 48A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305 AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305C AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305C AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305 AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 8805)

CLIP CRACKED AT FRAME 8805 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305C AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 9305)

CLIP CRACKED AT FRAME 9305C AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FRAME 7805)

CLIP CRACKED AT FRAME 7805 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

CLIP CRACKED AT FRAME 5805 AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

CLIP CRACKED AT FRAME 7805 AT STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

CLIP CRACKED AT FRAME 7805 AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5808)

CLIP CRACKED AT FRAME 5805 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

CLIP CRACKED AT FRAME 5805 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

CLIP CRACKED AT FRAME 5805 AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

CLIP CRACKED AT FRAME 5805 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

CLIP CRACKED AT FRAME 5805 AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: ALTIMETER — FAILED (COCKPIT)

FAT/LAS - DURING CLIMB, CAPTAIN'S ALTIMETER STUCK AT 5,300 FEET. FIRST OFFICER'S ALTIMETER OK. ALTERNATE SOURCE SELECTED AND NO HELP. CREW REPORTED TO MAINTENANCE CONTROL AND WAS ADVISED TO RETURN TO FAT. CAPTAIN'S ALTIMETER WAS REPLACED, PITOT STATIC TEST WAS ACCOMPLISHED IAW 34-10-02 AND 34-11-02, AND SYSTEM FUNCTIONED NORMALLY. (X)

Part: COALESCENT SOCK — DIRTY (RIGHT)

FAT - ON CLIMB-OUT, NOTICED FUMES AND SMOKE IN COCKPIT AND CABIN. CHECKED COOLING TURBINE, FOUND OIL PRESENT. CHECKED COALESCENT SOCKS AND CLEANED BOTH.

Part: TORQUE LINK — FRACTURED (RT MAIN GEAR)

LAS - LOWER TORQUE LINK FAILED CAUSING INNER CYLINDER TO TURN 90 DEGREES AND SUBSEQUENT TIRE FAILURES. UPON LANDING AT LAS, RT LOWER MLG TORQUE LINK FAILED. REMOVED AND REPLACED RT MLG ASSY.

Part: VALVE — FAULTY (LEFT)

CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. THE CAPTAIN DECIDED TO RETURN TO CLT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE. (M)

Part: RELAY — FAULTY (LEFT)

CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. THE CAPTAIN DECIDED TO RETURN TO CLT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE. REFERENCE NR USAA950896.

Part: EEL — MALFUNCTIONED (CABIN)

CLT - THE OVERHEAD EMERGENCY LIGHTING COMES ON WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE TROUBLESHOT THE EVACUATION LIGHTING SYSTEM. OPERATIONS WERE FOUND TO BE NORMAL. (M)

Part: SKIN — CRACKED (FUSELAGE)

PIT - DURING SCHEDULED SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN THE SED APERATURE AT THE FORWARD UPPER CORNER REF SIP 53-10-20 OUTSIDE LAYER OF SKIN (EDDY CURRENT INSPECTION). CUT OUT CRACKED AREA AND INSTALLED FILLER AND DOUBLER REPAIRS (2 EACH) PER SRM 53-02-16 PG 7, 8 AND 9. (M)

Part: EEL HOLDER — INOPERATIVE (CABIN)

PIT - FLT NR 231 - DURING PREFLIGHT THE FLIGHT ATTENDANT FOUND EMERGENCY EXIT OVERHEAD LIGHTS INOPERATIVE. MAINTENANCE REPLACED LIGHT PLATE ASSEMBLY TO THE EMERGENCY EXIT LIGHTS ON CENTER CABIN PER WING EXIT. OPERATION CHECKS NORMAL. (Z)