N479AU

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,063 hrs · 38,748 cycles

PDX - EVACUATION LIGHTS ON EXIT SIGN IN PASSENGER COMPARTMENT COME ON DIM AND THEN GO OFF AFTER ONE TO TWO MINUTES. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 32,861 hrs · 38,593 cycles

PDX - THE NUMBER TWO OVERHEAD EVACUATION LIGHT IS DIM AND UNREADABLE. REMOVED AND REPLACED LAMP ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 32,849 hrs · 38,573 cycles

PDX- NR 6 OVERHEAD EVACUATION LIGHT AND CABIN CEILING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY RIGHT HAND NR 3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,662 hrs · 38,420 cycles

BOI - EMERGENCY EXIT LIGHT IN GALLEY DOOR DOES NOT LIGHT UP. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — SHORTED (NR 2 ENGINE) · airframe 32,449 hrs · 38,243 cycles

BIL - ENROUTE FROM BIL TO SEA THE NR 2 FIRE WARNING SOUNDED AND LIGHT UP. PERFORMED ENGINE FIRE CHECK LIST, SHUTING DOWN NR 2 ENGINE. AFTER PULLING THE FIRE CONTROL GUARD THE FIRE LIGHT WENT OUT. FIRED NR 2 FIRE BOTTLE. DIVERTED TO GEG AND LANDED WITHOUT INCIDENT. CHECKED NR 2 ENGINE FOR FIRE DAMAGE OR LEAKING FLUIDS. NON NOTED. REPLACED FIRE LOOP SECTION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 32,437 hrs · 38,232 cycles

PDX - EMERGENCY EXIT SIGN ABOVE THE FOREWARD GALLEY LINTEL HAS SEVERAL BULBS THAT DID NOT ILLUMINATE. REPLACED LIGHT CARD ON EXIT SIGN ABOVE FORWARD GALLEY LINTEL. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 32,401 hrs · 38,198 cycles

GEG - ROW EIGHT EMERGENCY EXIT SIGNS HAVE INOPERABLE BULBS. REMOVED AND REPLACED CIRCUIT BOARDS. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,943 hrs · 37,792 cycles

GEG - EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,858 hrs · 37,714 cycles

BOI- FORWARD CABIN EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED EXIT SIGN ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — DEFECTIVE (CABIN) · airframe 31,761 hrs · 37,630 cycles

GEG - CENTER AISLE EXIT SIGN LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — LOOSE (CABIN) · airframe 31,707 hrs · 37,575 cycles

SEA - EXIT SIGN ON SEAT 9A WAS FOUND LOOSE. REMOVED AND REPLACED EXIT SIGN. OPERTAIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,252 hrs · 37,184 cycles

BOI-EXIT SIGN ABOVE COCKPIT DOOR 28V LIGHTS INOPERATIVE. REPLACED EXIT SIGN ABOVE COCKPIT DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAULTY (CABIN) · airframe 31,054 hrs · 37,007 cycles

SEA - FORWARD CABIN EXIT SIGN FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,622 hrs · 36,613 cycles

GEG-EMERGENCY EXIT SIGN INOPERATIVE AT ROW 8 AND 9. REPLACED SIGNS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 30,517 hrs · 36,508 cycles

FOUND CABIN OVERHEAD EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 30,317 hrs · 36,318 cycles

PDX - EMERGENCY EXIT SIGN OVER FLIGHT COMPARTMENT DOOR FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RECEIVER — ODOR (E/E BAY) · airframe 29,946 hrs · 35,970 cycles

PDX - A BURNING ELECTRICAL SMELL WAS REPORTED EMANATING FROM THE AVIONICS BAY. FOUND TO BE THE NR 2 DISTANCE MEASURING DEVICE RECEIVER. DEACTIVATED SYSTEM. REPLACED DME INTERIGATOR ON FOLLOWING DAY (9-20-00). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (COCKPIT) · airframe 29,834 hrs · 35,860 cycles

BOI- EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (ROW 8) · airframe 29,834 hrs · 35,860 cycles

BOI- CEILING EMERGENCY EXIT SIGNS ABOVE ROW 8, FORWARD AND ADT FACING, INOPERATIVE. REMOVED AND REPLACED BOTH EXIT SIGN CIRCUIT BOARDS. LIGHTS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FAIRING) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED SUPPORT ANGLE FOR RIGHT HAND FUSELAGE FAIRING PANEL 92G. REPAIRED IAW HORIZON AIR EA 4-57-459.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE IS CORROSION AROUND A SCREW HOLE ON LOWER SIDE OF SPAR WEB AT STATION 6805, JUST INBOARD OF SEAT TRACK FLOORBEAM AT BL 600 RIGHT HAND. REPAIRED IAW FOKKER SRM 51-10-4, AND HORIZON AIR EA 4-53-1326.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- ROW OF RIVETS PULLED THROUGH SKIN AT TOP END OF RIGHT HAND NUMBER 2 INTERMEDIATE SPAR OF VERTICAL STABILIZER. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-253.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- ROW OF RIVETS PULLED THROUGH SKIN AT TOP END OF LEFT HAND NUMBER 2 INTERMEDIATE SPAR OF VERTICAL STABILIZER. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-253.

Part: PANEL — CORRODED (LT WING) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND FUEL PANEL APERTURE HAS FILLET PEELING/FLAKING OFF AT PANEL 71A. REPAIRED IAW HORIZON AIR EA 4-57-188A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- AFT DME ANTENNA MOUNT STRUCTURE INTERNAL REINFORCEMENT SKIN HAS CORROSION WHERE PAINT IS MISSING. REPAIRED IAW FOKKER SRM 53-24-01 AND SRM 53-00-00.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED PAST STOP DRILL, FORWARD SIDE FRAME 67-2 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05 AND HORIZON AIR EA 4-53-1329.

Part: CLIP — MISINSTALLED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP AT STRINGER 1 FRAME 16660 HAS 4 RIVETS THAT ARE NOT PROPERLY DRIVEN. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED FRAME CLIP AT FRAME 16060 AND STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- ON AFT SIDE OF FRAME 15635 AT 11:00 O''CLOCK POSITION LOOKING FORWARD AT STRINGER 39, TOP RIVET HAS SEVERAL CRACKS PROTRUDING FROM RIVET HOLE. REPAIRED IAW HORIZON AIR EA 4-53-1327.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CASTELLATION OF FRAME 16660 AT STRINGER 1 HAS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01.

Part: FASTENER — LOOSE (SPOILER HINGE) · airframe 29,818 hrs · 35,846 cycles

PDX- LOOSE/WORKING FASTENERS INBOARD OF LEFT HAND NR 3 LIFT DUMPER INBOARD HINGE. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-57-457.

Part: SKIN — GOUGED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE ARE TWO GOUGES AND DENTS IN EXTERIOR SKIN AT FORWARD SIDE OF AFT CARGO DOOR APERTURE AT STRINGER 66 AND 67. REPAIRED IAW HORIZON AIR EA 4-53-1325.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION FOUND AT MOST AFT NUT PLATE ON GILLINER SUPPORT AT STATION 19050 ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CASTELLATION OF FRAME 16060 AT STRINGER 74 HAS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 53-02-13.

Part: BEAM — CRACKED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND REAR PRESSURE BULKHEAD HORIZONTAL BEAM 2 HAS A CRACK ON THE BEAM AT THE MOST OUTBOARD HOLE AT STRINGER 64. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 31.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED FRAME CLIP AT STRINGER 1 AND FRAME 16660. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, PAGE 2.

Part: BEAM — CHAFED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND VERTICAL BEAM BETWEEN REAR PRESSURE BULKHEAD AND FRAME 18075 IS CHAFED JUST AFT OF FORWARD APU ENCLOSURE. VERTICAL LEG OF REPAIR ANGLE WHERE SEVERAL HI-LOKS ARE INSTALLED DO NOT HAVE THICKNESS CALLED OUT FOR IN EA 4-53-131 STEP 2. REPAIRED IAW HORIZON AIR EA 4-53-1324.

Part: DOOR FRAME — DENTED (SERVICE DOOR) · airframe 29,818 hrs · 35,846 cycles

PDX- SERVICE EMERGENCY DOOR OUTER FRAME LOWER FORWARD CORNER RADIUS DENTED. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-52-398.

Part: BEAM — CHAFED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND VERTICAL BEAM BETWEEN REAR PRESSURE BULKHEAD AND FRAME 18075 IS CHAFED JUST AFT OF FORWARD APU ENCLOSURE. VERTICAL LEG OF REPAIR ANGLE DOES NOT HAVE THE THICKNESS CALLED OUT FOR IN EA 4-53-1313 STEP 2. REPAIRED IAW HORIZON AIR EA 4-53-1324.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- REPAIR DOUBLER ON FRAME CASTELLATION AT FRAME 13815B AND STRINGER 73 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: BEAM — CRACKED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND VERTICAL BEAM BETWEEN REAR PRESSURE BULKHEAD AND FRAME 18075 (BL 425R) IS CRACKED JUST AFT OF FORWARD APU ENCLOSURE. REPAIRED IAW HORIZON AIR EA 4-53-1313.

Part: ROD END — WORN (HAND BRAKE) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND SPEED BRAKE PUSHROD AFT ROD END LOOSE/WORN. REPAIRED IAW FOKKER SRM 27-61-5 PAGE 203 AND 20-30-14.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED CLIP LEFT HAND FUSELAGE BELLY AT FRAME 13815B. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME 32-2 CASTELLATION CRACKED ABOVE STRINGER 44 ADJACENT TO BRACE ROD FITTING. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-1323.

Part: CHANNEL — SCRATCHED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE FRAME STIFFENER CHANNEL OUTBOARD OF 24A HATCH APERTURE HAS MULTIPLE SCRATCHES IN SKIN. REPAIRED IAW FOKKER SRM 53-11-07, PAGE 7 AND SRM 51-10-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE HAS A DENT BETWEEN FRAMES 6805 AND 7305 AND STRINGERS 67 AND 68. REPAIRED IAW FOKKER SRM 53-02-01 AND SRM 51-31-01, AND SRM 53-02-02, PAGE 2.

Part: BRACKET — CRACKED (LAVATORY) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND LAVATORY SINK SUPPORT BRACKET MOUNTED TO REAR PRESSURE BULKHEAD IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.

Part: RIVET — CRACKED (BULKHEAD 6) · airframe 29,818 hrs · 35,846 cycles

PDX- RIVETS ABOVE MAIN LANDING GEAR PIN STORAGE BOX, AT TOP BULKHEAD NR 6 AND 7 RIVETS POSSIBLE CRACK. REPAIRED IAW FOKKER SRM 51-31-05 AND HORIZON AIR EA 4-53-1309.

Part: RIVET — CRACKED (BULKHEAD 4) · airframe 29,818 hrs · 35,846 cycles

PDX- RIVET ABOVE MAIN LANDING GEAR STORAGE BOX AT TOP BULKHEAD NR 4 RIVET POSSIBLE CRACK. REPAIRED IAW FOKKER SRM 51-31-05 AND HORIZON AIR EA 4-53-1309.

Part: SKIN — MISDRILLED (VERTICAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- 7 HOLES DRILLED IN LEFT HAND VERTICAL STABILIZER BELOW PANEL 56C. REPAIRED IAW FOKKER SRM 51-10-04.

Part: BRACKET — CRACKED (AFT PRESS BLKHD) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND INBOARD WATER TANK MOUNT BRACKET IN REAR PRESSURE BULKHEAD IS CRACKED ON LOWER INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01.

Part: BRACKET — CRACKED (AFT PRESS BLKHD) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND INBOARD WATER TANK MOUNT BRACKET ON REAR PRESSURE BULKHEAD IS CRACKED ON LOWER INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — SCRATCHED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- ANGLE CLIP AT FRAME, STATION 4610, RBL 58 - 61 WL 22.047 CABIN FLOOR LEVEL HAS DEEP SCRATCH IN RADIUS. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-14-06.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- MULTIPLE SCRATCHES IN APERTURE SKIN OF HATCH 21A AT FUSELAGE LEFT HAND SIDE AROUND HATCH ALIGNMENT PIN SLOT. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-11-11, PAGE 2.

Part: SKIN — CHAFED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE SKIN CHAFED BY WING TO FUSELAGE FAIRING PANEL 91BC AFT EDGE. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1316.

Part: SKIN — CHAFED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE SKIN CHAFED BY WING TO FUSELAGE FAIRING PANEL 91BC AFT EDGE. REPAIRED IAW FOKKER SRM 53-02-01 AND SRM 51-31-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE IS EXFOLIATION CORROSION ON FRAME 5305 AROUND NUT PLATE, JUST ABOVE STRINGER 66. REPAIRED IAW HORIZON AIR EA 4-53-1317.

Part: BEAM — CRACKED (AFT PRESS BLKHD) · airframe 29,818 hrs · 35,846 cycles

PDX- BEAM 1 ON REAR PRESSURE BULKHEAD HAS CRACKS ON UPPER FLANGE JUST INBOARD OF BL 425R. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 30 AND SRM 53-02-18.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- ANGLE IS CHAFED WHERE THE RIGHT HAND INBOARD MAIN LANDING GEAR DOOR OUTER FORWARD EDGE CONTACTS. REPAIRED IAW HORIZON AIR EA 4-57-451, AND FOKKER SRM 51-31-01.

Part: BEAM — DAMAGED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- BEAM VI ON FORWARD PRESSURE BULKHEAD REQUIRES PERMANENT REPAIR. REPAIRED IAW FOKKER SRM 20-16-0, 51-31-01, 51-30-02, 53-02-18, HORIZON AIR EA 4-53-1071A, 4-53-1318 AND 4-53-1307.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- DENT PUSHED OUT FROM INSIDE FUSELAGE 103 INCHES AFT OF 41A AND BL 340R. REPAIRED IAW FOKKER SRM 53-02-01 AND SRM 53-01-01, PAGE 8.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- DENT PUSHED OUT FROM INSIDE FUSELAGE 109 INCHES AFT OF 41A DOOR. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 53-02-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- REPAIR CLIP CRACK PAST STOP DRILL, AFT SIDE OF FRAME 16-2 JUST ABOVE STRINGER 32. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 53-31-01.

Part: SUPPORT BRACKET — CORRODED (AIRSTAIR DOOR) · airframe 29,818 hrs · 35,846 cycles

PDX- MAIN CABIN DOOR AFT STAIR SUPPORT STRUCTURE IS CORRODED AT BOTTOM. REPAIRED IAW FOKKER SRM 52-10-00 AND SRM 52-01-01 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED ON AFT SIDE OF FRAME 16-2 ABOVE STRINGER 43. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- SHEAR TIE AT FRAME 30-2 AT STRINGER 48 HAS CRACK. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05, PAGE 605.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-10-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE IS A DENT IN EXTERNAL FUSELAGE SKIN, APPROXIMATLEY .060 INCHES DEEP, JUST BELOW FORWARD EDGE OF APU EXHAUST DUCT OPENING. REPAIRED IAW HORIZON AIR EA 4-53-1315.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 JUST ABOVE STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- SKIN IS SWELLED FORWARD SIDE OF APU EXHAUST. RIVET HEADS CAN BE PULLED OUT, STEMS ARE CORRODED AWAY. REPAIRED IAW FOKKER SRM 53-25-01 PAGE 5, 51-10-04 AND HORIZON AIR EA 4-53-1315.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 JUST ABOVE STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.

Part: BELLCRANK — GOUGED (AILERON) · airframe 29,818 hrs · 35,846 cycles

PDX- GOUGES IN LEFT HAND AILERON DUAL INPUT QUADRANT BELLCRANK ABOVE LOCKOUT ACTUATOR CYLINDER. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-27-115.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 AT STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CLIP — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE IS A CRACK IN FUSELAGE SKIN, APPROXIMATELY .5 INCHES LONG AND 2 INCHES BELOW LOWER FORWARD EDGE OF APU EXHAUST DUCT. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1315

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 AT STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: BEAM — CHAFED (BULKHEAD) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND VERTICAL BEAM BETWEEN REAR PRESSURE BULKHEAD AND FRAME 18075 (BL 425L) IS CHAFED JUST AFT OF FORWARD APU ENCLOSURE. REPAIRED IAW HORIZON AIR EA 4-53-1313.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON FORWARD SIDE OF FRAME 16660 AT STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND WING LOWER STRIP JOINT IS DAMAGED. REPAIRED IAW HORIZON AIR EA 4-57-449.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE FRAME STIFFENER CHANNEL OUTBOARD OF 23A HATCH APERTURE HAS MULTIPLE SCRATCHES IN SKIN, APPROXIMATELY 3 X 3 INCH. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FRAME CLIP CRACKED ON AFT SIDE OF FRAME 16060 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- BURR ON EDGE OF HOLE IN RIGHT HAND RAIL OF LEFT HAND OUTBOARD SEAT TRACK, 3 INCHES FORWARD OF FRAME 13345. REPAIRED IAW FOKKER SRM 53-40-01 AND SRM 51-10-4.

Part: FRAME — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- GROUNDING WIRE CONNECTION AT FRAME, STATION 4150, OVER SERVICE DOOR IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-01-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED PAST STOP DRILL, AFT SIDE FRAME 50-2 AT STRINGER 50. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05, PAGE 601.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE SKIN UNDER AFT RADIO ALTIMETER ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-1312.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- BURR ON INBOARD EDGE OF HOLE IN RIGHT HAND RAIL OF LEFT HAND OUTBOARD SEAT TRACK, 10 INCHES AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-40-01.

Part: WIRE — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX-GROUNDING WIRE FOR SERVICE EMERGENCY DOOR APERTURE LIGHT, CONNECTION CORRODED. REPAIRED IAW FOKKER SRM 51-10-01 AND SRM 53-01-01.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT LOWER RIGHT HAND LUGS ON HORIZONTAL STABILIZER DRIVE FITTINGS. REPAIRED IAW FOKKER SRM 55-01-01, PAGE 4 AND HORIZON AIR EA 4-55-254.

Part: MOUNT — CORRODED (NAV ANTENNA) · airframe 29,818 hrs · 35,846 cycles

PDX-AT NAV/COMM UPPER ANTENNA MOUNT SURFACE HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- SERVICE EMERGENCY DOOR APERTURE UPPER BOX INTERCOSTAL, AFT OUTBOARD, INTERNAL CORNER HAS TOOL MARKS AND CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT LOWER LEFT HAND LUGS ON HORIZONTAL STABILIZER DRIVE FITTING. REPAIRED IAW FOKKER SRM 55-01-01, PAGE 4 AND HORIZON AIR EA 4-55-254.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT UPPER RIGHT HAND LUGS ON HORIZONTAL STABILIZER DRIVE FITTING. REPAIRED IAW FOKKER SRM 55-01-01 PAGE 4 AND HORIZON AIR EA 4-55-254.

Part: STRUCTURE — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION ABOVE SERVICE EMERGENCY DOOR BETWEEN STATION 4060 AND STATION 4100. REPAIRED IAW FOKKER SRM 53-01-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- SERVICE EMERGENCY DOOR CUTOUT INTERNAL SKIN IS CHAFED AT FORE AND AFT CONTACT POINTS. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4, PAGE 9.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT UPPER LEFT HAND LUGS ON HORIZONTAL STABILIZER DRIVE FITTING. REPAIRED IAW FOKKER SRM 55-01-01 AND HORIZON AIR EA 4-55-254.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- THERE IS CORROSION UNDER THREE NUT PLATES AT STRINGER 74 AND FRAME 6805. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION ON LEFT HAND INBOARD SEAT TRACK, RIGHT HAND FLANGE Y2 FORWARD OF CAMLOCK RECEPTICAL. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 53-40-01.

Part: RING — CRACKED (RT WINDOW) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND D WINDOW INSIDE APERTURE RING IS CRACKED THIRD MOUNTING SCREW HOLES FROM TOP FORWARD CORNER. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND SIDE OF AIRCRAFT INBOARD TRACK FLANGE HAS LIGHT CORROSION AT FRAME 9035A. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION ON RIGHT HAND FLANGE OF LEFT HAND INBOARD SEAT TRACK FORWARD CAMLOCK RECEPTICAL. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4.

Part: PANEL — CORRODED (LT WING) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND FUEL PANEL 73A MATING SURFACE HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 57-01-01 PAGE 5.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED AFT SIDE FRAME 50.5-2 AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-5, PAGE 601A.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74G HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGES 3, 5 AND SRM 57-14-01, PAGE 4, AND SRM 51-10-4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74C HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74B HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE 74E HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-14-01, PAGE 4 AND SRM 51-10-4, AND SRM 57-01-01, PAGE 5.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74H HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGES 3, 5 AND SRM 57-14-01, PAGE 4, AND SRM 51-10-4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 72A HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: PANEL — CORRODED (LT WING) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND FUEL PANEL 73B MATING SURFACE HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 57-01-01 PAGE 5.

Part: PANEL — CORRODED (LT WING) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND PANEL 73G MATING SURFACE HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 57-01-01 PAGE 5.

Part: PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 74E APERTURE HAS LIGHT FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, 57-01-01 PAGE 5 AND 57-14-01 PAGE 4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74D HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGES 3, 5 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND SIDE OF AIRCRAFT INBOARD TRACK HAS LIGHT CORROSION BETWEEN FRAMES 7305 AND 6805 ON INBOARD FLANGE. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4, AND SRM 53-40-01, PAGE 206.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT UPPER RIGHT HAND LUG AT HORIZONTAL STABILIZER JUNCTION FITTING. REPAIRED IAW HORIZON AIR EA 4-55-252 AND FOKKER SRM 55-01-01 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED CLIP FRAME 17565 AND STRINGER 53A. REPAIRED IAW FOKKER SRM 53-10-05.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 29,818 hrs · 35,846 cycles

PDX- SERVICE EMERGENCY DOOR THRESHOLD HAS WIDE SPREAD LIGHT CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED AFT SIDE OF FRAME 24-2 AT STRINGER 53. REPAIRED IAW FOKKER SRM 53-10-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 74A HAS FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX-PANEL 74E HAS SOME FRETTING CORROSION AT THE SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGES 3, 5.

Part: ACCESS PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 74D HAS FRETTING CORROSION AT THE SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED CLIP AFT OF FRAME 20075 AND STRINGER 37. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- STRINGERS UNDER REMOVED SKIN HAVE LIGHT SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED AFT SIDE OF FRAME 16-2 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-10-05.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED FORWARD SIDE OF FRAME 32-2 AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-10-05.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED, FORWARD SIDE OF FRAME 50-2 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-10-05.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED CLIP AFT SIDE FRAME 32-2 AT STRINGER 45. REPAIRED IAW FOKKER SRM 53-10-05.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CRACKED CLIP AFT SIDE OF FRAME 19976 AND STRINGER 37. REPAIRED IAW FOKKER SRM 53-02-13, SRM 53-10-05.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT LOWER LEFT HAND LUG AT HORIZONTAL STABILIZER JUNCTION FITTING. REPAIRED IAW HORIZON AIR EA 4-55-252 AND FOKKER SRM 55-01-01 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED PAST STOP DRILL, FRAME 50-2 AT STRINGER 31. REPAIRED IAW FOKKER SRM 53-10-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 74B HAS FRETTING CORROSION AT THE SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED PAST STOP DRILL AT FRAME 50-2, FORWARD SIDE AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-10-05.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT LOWER RIGHT HAND LUG AT HORIZONTAL STABILIZER JUNCTION FITTING. REPAIRED IAW HORIZON AIR EA 4-55-252 AND FOKKER SRM 55-01-01 PAGE 4.

Part: ACCESS PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 74C HAS FRETTING CORROSION AT THE SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: MOUNT — GOUGED (ACM BAY) · airframe 29,818 hrs · 35,846 cycles

PDX- LEFT HAND AIR CYCLE MACHINE HAS 2 GOUGES THAT NEED BLENDING OUT AFT OF LOWER MOUNT ON BULKHEAD. REPAIRED IAW FOKKER SRM 53-02-01 AND SRM 51-10-4.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION AT UPPER LEFT HAND LUG AT HORIZONTAL STABILIZER JUNCTION FITTING. REPAIRED IAW HORIZON AIR EA 4-55-252 AND FOKKER SRM 55-01-01, PAGE 4.

Part: SKIN — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- APERTURE FOR 74A HAS SOME FRETTING CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CLIP CRACKED AFT SIDE OF FRAME 32-2 AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-10-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 29,818 hrs · 35,846 cycles

PDX- PANEL 72A HAS SOME FRETTING CORROSION AT THE SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3, 5 AND SRM 51-10-4, PAGE 4.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- CORROSION NEAR LOWER EDGE OF VERTICAL STRUT AT FRAME 5305 JUST ABOVE STRINGER 65. REPAIRED IAW FOKKER SRM 51-10-4.

Part: STRUCTURE — TORN (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- TORN LIGHTNING HOLE FLANGE, HORIZONTAL FRAME 9 INCHES BELOW INNER LATCH HANDLE. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE SKIN UNDER FORWARD RADIO ALTIMETER ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01-01.

Part: BEAM — CORRODED (AFT PRESS BLKHD) · airframe 29,818 hrs · 35,846 cycles

PDX- RIGHT HAND OF REAR PRESSURE BULKHEAD HORIZONTAL BEAM 2 HAS SPOT OF CORROSION AT STRINGER 64. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,818 hrs · 35,846 cycles

PDX- FUSELAGE SKIN CORROSION UNDER AFT END OF MARKER BEACON ANTENNA MOUNTING. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-01-01 PAGE 6.

Part: SIGN — INOPERATIVE (CABIN) · airframe 29,424 hrs · 35,475 cycles

SEA- EMERGENCY EXIT SIGN ON SEAT 9B MISSING LENS COVER. REMOVED AND REPLACED EXIT SIGN ON SEAT 9B. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 28,986 hrs · 35,031 cycles

SEA - EMERGENCY EXIT LIGHT AT ROW 9 INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 28,900 hrs · 34,948 cycles

BOI- EMERGENCY AISLE EXIT LIGHT HAS RIGHT SIDE BURNT OUT. REPLACED WITH NEW CIRCUIT BOARD. OPERATINAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTACLE — FAILED (GALLEY) · airframe 28,890 hrs · 34,942 cycles

SEA- COFFEE WARMER CIRCUIT BREAKER POPPED AGAIN WITH A STRONG ELECTRICAL CORD SMELL. REMOVED AND REPLACED LOWER COFFEE WARMER RECEPTICAL, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — FAILED (COCKPIT) · airframe 28,890 hrs · 34,942 cycles

BOI - EMERGENCY LIGHT ABOVE COCKPIT DOOR HAS LAMPS INOP. INSTALLED NEW CIRCUIT BREAKER IN SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,702 hrs · 34,744 cycles

SEA - EMERGENCY EXIT LIGHT OVER FORWARD GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (SEAT 14)

BOI - EVACUATION LIGHT ASSEMBLY BROKEN ON SEAT 14 A/B. REMOVED AND REPLACED EVACUATION LIGHT ASSEMBLY AT SEAT 14. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (EMER EXIT)

PDX- CENTER OVERHEAD EMERGENCY EXIT SIGN IS DIM. REMOVED AND REPLACED EMERGENCY CIRUIT BOARD, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

BOI - BACK THREE EVACUATION CEILING LIGHTS INOPERABLE. INSTALLED NEW BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — STUCK (HYD SYSTEM)

PILOT REPORTED STABILIZER HYDRAULIC LIGHT ILLUMINATED. TROUBLESHOOTING REVEALED THE STABILIZER ''STICKING SWITCH'' WAS FAULTY. (X)

Part: SKIN — CRACKED (WING)

APERTURE FOR FUEL PANEL 71A INBOARD MOST FASTENER HOLE IN OUTER RING OF FASTENERS HAS A CRACK. REPAIRED IAW HORIZON AIR EA 4-57-188.

Part: SKIN — DAMAGED (FUSELAGE)

LEFT-HAND FUSELAGE BELOW PILOTS WINDOW HAS A 1.33 DIVOT IN PAINT. REMOVED PAINT, INSPECTED SKIN FOR DAMAGE AND REPAIRED IAW FOKKER SRM 51-31-01, 51-10-04 AND MM 53-00-00, PAGE 2.

Part: FLOORBEAM — DAMAGED (BS 3930)

PDX - GALLEY NR 1 FLOORBEAM AT APPROXIMATELY BL900 DAMAGED AT AFT END APPROXIMATELY STATION 3930. NUTPLATE THAT WAS INSTALLED IS NOT LINED UP WITH HOLE. REALIGNED HOLE WITH NUT PLATE.

Part: ANGLE — CORRODED (PAX DOOR)

PDX - TWO ANGLES ON LOWER AFT SIDE NEAR HINGE ON MAIN CABIN DOOR HAVE CORROSION. REPAIRED IAW HORIZON AIR 4-52-113B.

Part: SKIN — CRACKED (WING)

FUEL PANEL 71A APERTURE HAS 3 SMALL CRACKS FROM FASTENER HOLES. REPAIRED IAW HORIZON AIR EA 4-57-188.

Part: SKIN — DAMAGED (FUSELAGE)

LEFT-HAND FUSELAGE BELOW PILOTS WINDOW HAS A 1.5 DIVOT IN PAINT. REMOVED PAINT, INSPECTED SKIN FOR DAMAGE AND REPAIRED IAW FOKKER SRM 53-02-01.

Part: SKIN — CRACKED (WING)

APERTURE FOR FUEL PANEL 71A HAS TWO SMALL CRACKS FROM FASTENER HOLES ON INNER RING AT FASTENERS. REPAIRED IAW HORIZON AIR EA 4-57-188.

Part: TRACK — CORRODED (TE FLAP)

LIGHT CORROSION TO MLG BEAM BOLT HOLES, SPOILER BEAM BOLT HOLES, AND AFT MLG DOOR HINGE FITTING BOLT HOLES. REAMED HOLES TO REMOVE CORROSION. MLG BEAM BOLT HOLES OVERSIZED AND LEFT AS-IS. SPOILER BEAM BOLT HOLES BUSHED. AFT MLG DOOR HINGE FITTING BOLT HOLES OVERSIZED AND OVERSIZED BOLT INSTALLED.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: ANGLE — CRACKED (RT WING)

PDX - RIGHT WING LOWER CONNECTION ANGLE AT MAIN LANDING GEAR BRACKET TO REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-05.

Part: SKIN — BENT (CARGO DOOR)

AFT CARGO DOOR OUTER SKIN BENT AT TOP AFT CORNER. REPAIRED IAW FOKKER SRM 51-11-4, PAGE 2, PARAGRAPH 2 (E-F).

Part: NOSE COWL — CHAFED (FUSELAGE)

DEEP CHAFE AT THE 6 O'CLOCK POSITION ON THE AFT FACE OF THE NOSE COWLING. REPAIRED IAW HORIZON AIR EA 4-72-32.

Part: CLIP — CRACKED (FRAME 58.5-2)

PDX - CLIP CRACKED AT FRAME 58.5-2 AFT SIDE ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 58.5-2)

PDX - CLIP CRACKED AT FRAME 58.5-2 AFT SIDE ABOVE STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-01.

Part: CLIP — CRACKED (BS 16495)

REPAIR CLIP CRACKED AT STATION 16495 AFT END OF RIGHT-HAND MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4(B-C) AND 51-30-02.

Part: CLIP — CRACKED (FRAME 20075)

AFT CLIP CRACKED ON FRAME 20075 AT STRINGER 39 AND 41. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05 PAGE 603.

Part: SKIN — CORRODED (FUSELAGE)

PDX - CORROSION ON FUSELAGE SKIN UNDER UPPER NAV COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 4900)

PDX - LEFT INBOARD SEAT TRACK CORROSION ON TOP INBOARD SIDE AFT OF STATION 4900. REPAIRED IAW FOKKER MM 53-40-01, FIGURE 204.

Part: SEAT TRACK — GOUGED (FRAME 6305)

PDX - NUMEROUS GOUGES IN CENTER OF SEAT TRACK BL600R, JUST FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 53-40-01, FIGURE 204.

Part: SEAT TRACK — CORRODED (FRAME 10346)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 5 AFT OF FRAME 10346, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 16495)

REPAIR CLIP CRACKED AT STATION 16495 AFT END OF LEFT-HAND MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4(B-C) AND 51-30-02.

Part: CLIP — CRACKED (FRAME 24-2)

PDX - CRACK PAST STOP DRILL ON CLIP FRAME 24-2, STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGES 13-17, SRM 51-30-02, PAGE 9, PARAGRAPH 4B THROUGH PAGE 15 AND SRM 53-02-13, PAGE 6, FIGURE 4.

Part: SKIN — CRACKED (BS 3820)

LEFT-HAND FUSELAGE SKIN HAS CRACK ACROSS RIVET HOLE AT STATION 3820, WL 490, BL 1300L. REPAIRED IAW FOKKER SRM 53-02-07, FIGURE 4 AND MM 53-00-00.

Part: COVER — CRACKED (BS 2475)

WHEEL WELL BAG TOP COVER HAS 2.5 INCH CRACK AT STATION 2475, BL 150R AND WL 700. REPAIRED IAW FOKKER SRM 51-33-01.

Part: STRINGER — CRACKED (BS 5805)

PDX - LARGE CRACK IN STRINGER 16 JUST AFT OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-16, FIGURE 1.

Part: CLIP — CRACKED (FRAME 32-2)

PDX - CLIP CRACKED FORWARD SIDE FRAME 32-2, STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 53-02-13, PAGE 5.

Part: RIB — CRACKED (RUDDER)

PDX - RUDDER RIB 5 CRACKED AT LEFT AND RIGHT STRINGER CLIPS. REPAIRED IAW HORIZON AIR EA 4-55-105.

Part: PEDESTAL — CORRODED (COCKPIT)

RIGHT-HAND SIDE OF PEDESTAL BASE IS MISSING PAINT AND HAS CORROSION ALONG EDGE BETWEEN MOUNT POINTS DIRECTLY INBOARD OF FIRST OFFICER CONTROL COLUMN. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-597.

Part: PEDESTAL — CORRODED (COCKPIT)

LEFT-HAND SIDE OF THE PEDESTAL HAS CORROSION AT THE FORWARD MIDDLE END AFT FLOOR MOUNT HOLE BORES. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-597.

Part: SKIN — CRACKED (BS 16495)

SKIN CRACKED AT STATION 16495 ON AFT END ON MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3(C).

Part: SKIN — CRACKED (BS 16495)

SKIN CRACKED AT STATION 16495 ON AFT END OF RIGHT-HAND MAIN LANDING GEAR KEEL. REPAIRED IAW FOKKER SRM 51-31-01, HORIZON AIR EA 4-53-595.

Part: PEDESTAL — CORRODED (COCKPIT)

LEFT-HAND SIDE OF PEDESTAL HAS CORROSION ALONG AFT HALF OF BASE EDGE. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-597.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 8305)

PDX - CRACK IN CLIP AT FRAME 8305 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815B BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 16 AFT OF FRAME 6805, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 14755)

CORROSION ON INBOARD FLANGE OF SEAT TRACK OF BL 1127L AT FRAME 14755, 3 INCHES LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — GOUGED (FRAME 6805)

PDX - GOUGES AND NICKS IN CENTER OF SEAT TRACK BL1127R, 6 1/2 AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-04,PAGE 9, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 28 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 10966)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 5.5 AFT OF FRAME 10966, 7 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 14285)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 1127L, 5 AFT OF FRAME 14285, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4 PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 11703)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, STARTING AT FRAME 11703, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 9805)

CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600L, 13 AFT OF FRAME 9805, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13345)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13345, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 NR 4, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 28 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 7 AFT OF FRAME 13815B, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 10790)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10790, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 15205)

PDX - CRACK IN CLIP AT FRAME 15205 BETWEEN STRINGERS 48 AND 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 10346)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10346, 5.5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 12405)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 11 AFT OF FRAME 12405, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 10966)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10966, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R FORWARD OF FRAME 7805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127L AT FRAME 13815B. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 1 AFT OF FRAME 7305, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 10966)

CORROSION ON INBOARD FLANGE OF SEAT TRACK 1127L, 9 AFT OF FRAME 10966, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - CORROSION IN CENTER OF SEAT TRACK BL 600R STARTING AT FRAME 7805, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815 BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 27 AND 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 15205)

PDX - CRACK IN CLIP AT FRAME 15205 BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: STRAP — GOUGED (WS 1700)

PDX - LEFT WING ROOT/CENTER WING LOWER SKIN JOINT STRAP GOUGED .045 DEEP AT WING STATION 1700 FUSELAGE STATION 11500. REPAIRED IAW HORIZON AIR EA 4-57-137 AND FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH C.

Part: SEAT TRACK — CORRODED (FRAME 14755)

CORROSION IN CENTER OF SEAT TRACK BL 600L, 10 AFT OF FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, PARAGRAPH B AND C.

Part: CLIP — CRACKED (BS 13815)

PDX - CRACK IN CLIP AT FRAME 13815 BETWEEN STRINGERS 32 AND 33. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 2 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 11905)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 11905, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 14 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — GOUGED (FRAME 6305)

PDX - NUMEROUS DEEP GOUGES ON TOP OF SEAT TRACK BL1127R, FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 14285)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, AT FRAME 14285. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORODED (FRAME 6805)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R, 14 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — GOUGED (FRAME 6805)

PDX - NICKS AND GOUGES IN CENTER OF SEAT TRACK BL1127R, 14 AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL600R, 5 AFT OF FRAME 8305, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127R, 1 AFT OF FRAME 7805, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8805)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL1127, FRAME 8805, 10 LONG. REPAIRED IAW FOKKER SRM 51-40-4, PAGE P, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127R STARTING AT FRAME 8305, 8.5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815 AND FORWARD, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 8 AFT OF FRAME 8305, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 12405)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 4 AFT OF FRAME 12405, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 5 AFT OF FRAME 6805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK AROUND NUT PLATE HOLE, 5 AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — GOUGED (FRAME 6805)

PDX - NUMEROUS GOUGES IN CENTER OF SEAT TRACK BL1127R, JUST FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R STARTING AT FRAME 6805, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 9 AFT OF FRAME 13815A, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (BS 4900)

PDX - CORROSION 1 AFT OF STATION 4900 ON INBOARD TOP SIDE OF LEFT INBOARD SEAT TRACK. REPAIRED IAW FOKKER MM 53-40-01, FIGURE 204.

Part: SEAT TRACK — CORRODED (FRAME 7805-8305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, FRAME 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. NR 4, PARAGRAPHS B AND C.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (BS 4900)

PDX - RIGHT OUTBOARD SEAT TRACK CORROSION ON TOP OUTBOARD SIDE AFT OF STATION 4900. REPAIRED IAW FOKKER MM 53-40-01, FIGURE 204.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - CORROSION IN CENTER OF SEAT TRACK BL 600R AT FRAME 7805, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 11 AFT OF FRAME 7305, 8 LONG. REPAIRED IAW SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R, 10 AFT OF FRAME 6805, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13345)

CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600L, 12 AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 16.5 AFT OF FRAME 6805, 12.5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815A, 11 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 7 AFT OF FRAME 8305, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL600R, 5 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - CORROSION ON OUTBOARD FLANGE AROUND NUT PLATE AT SEAT TRACK BL 600A, FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 1127R STARTING AT FRAME 8305, 8.5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 7305)

PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R STARTING 13 AFT OF FRAME 7305 AND CONTINUING PAST FRAME 7805, TOTAL LENGTH 16.5. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 13815)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 3 AFT OF FRAME 13815, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: SEAT TRACK — CORRODED (FRAME 9805)

CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 13 AFT OF FRAME 9805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C.

Part: CLIP — CORRODED (FRAME 8805)

CORROSION ON FRAME CLIP ON FRAME 8805, XBL0 IN FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1.

Part: SKIN — CORRODED (FUSELAGE)

PDX - FUSELAGE SKIN UNDER LOWER COMM VHF ANTENNA HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4C.

Part: STRUCTURE — GOUGED (HORIZ STAB)

PDX - SHARP GOUGE AFT LOWER LIP OF LIGHTNING HOLE THAT STABILIZER ACTUATOR FITS THROUGH IN TOP AFT OF 56G. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 7, VIEW A.

Part: SKIN — DENTED (LT ELEVATOR)

PDX - LEFT ELEVATOR HAS A DENT IN THE LOWER SKIN BETWEEN CENTER AND INBOARD HINGE 14 FROM TRAILING EDGE. REPAIRED IAW FOKKER SRM 51-70-0, PAGE 2, PARAGRAPH 3.

Part: CASTELLATION — CRACKED (FRAME 13815)

AFT CARGO PIT FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: PANEL — CORRODED (LT WING)

LEFT-HAND WING ACCESS PANEL 71A HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 4B 1-2.

Part: PANEL — CORRODED (LT WING)

LEFT-HAND WING ACCESS PANEL 73C HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, 4B1-2.

Part: CASTELLATION — CRACKED (FRAME 13815)

AFT CARGO PIT FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 9, PARAGRAPH B THROUGH, AND 51-31-01, PAGE 13, PARAGRAPH 7.

Part: PANEL — CORRODED (LT WING)

LEFT-HAND WING ACCESS PANEL 73A HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: PANEL — CORRODED (LT WING)

LEFT-HAND WING ACCESS PANEL 73B HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: SKIN — CORRODED (LT WING)

PDX - LEFT WING 73B APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: SKIN — CORRODED (LT WING)

PDX - LEFT WING 73D APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: SKIN — CORRODED (LT WING)

PDX - LEFT WING 73A APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: SKIN — CORRODED (LT WING)

PDX - LEFT WING 73C APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: SKIN — CORRODED (LT WING)

PDX - LEFT WING 71A APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 8305)

PDX - CRACK IN CLIP AT FRAME 8305 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 8805)

PDX - CRACK IN CLIP AT FRAME 8805 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CASTELLATION — CRACKED (FRAME 13815)

AFT CARGO PIT FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7.

Part: CLIP — CRACKED (BS 8805)

PDX - CRACK IN CLIP AT FRAME 8805 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: TRACK — CORRODED (TE FLAP)

PITTING CORROSION IN THE UPPER PORTION OF THE FLAP TRACK AT STATION 1700. REPAIRED IAW FOKKER SRM 51-10-04.

Part: CLIP — CRACKED (BS 9305)

PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — DAMAGED (BS 13815)

PDX - FRAME CLIP DAMAGED AT STATION 13815A AND STRINGER 15. REPAIRED IAW FOKKER SRM 51-31-01, 51-11-04.

Part: CLIP — CRACKED (BS 5305)

PDX - CRACK IN CLIP AT FRAME 5305 BETWEEN STRINGERS 48 AND 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SIGN — INOP (COCKPIT DOOR)

GEG - EMERGENCY EXIT SIGN AT COCKPIT DOOR INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT SIGN, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (ROW 8A & 9E)

EMERGENCY EXIT LIGHTS AT ROWS 8A AND 9E ARE INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (ROW 5 &10)

BOI - CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 AND 10. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST IS SATISFACTORY.

Part: BULB — FAILED (CABIN)

AFT FACING EXIT SIGN AT ROW 8 IS DIM. MAINTENANCE RELAMPED, OPERATIONAL TESTS ARE NORMAL.

Part: BULB — FAILED (CABIN)

FORWARD EMERGENCY EXIT SIGN HAS SEVERAL 28 VOLT BULBS OUT. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

GEG - OVERHEAD EXIT LIGHT OUT AT ROW 8. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, ASSEMBLY TESTS NORMAL.

Part: BULB — FAILED (CABIN)

BOI - EMERGENCY EXIT LIGHT AT ROW 9 IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TEST SHOWS NORMAL OPERATION.

Part: BULB — FAILED (CABIN)

EXIT SIGN AT ROW 8 OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT IN SIGN AT ROW 9-CDE IS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. LIGHT TESTS NORMAL.

Part: BULB — FAILED (CABIN)

ROW 1 AISLE EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED AND OPERATIONAL TESTED NORMAL.

Part: BULB — FAILED (CABIN)

GEG - BOTH OVERHEAD EMERGENCY EXIT SIGNS AT ROW 8 OUT. MAINTENANCE RELAMPED, TESTS GOOD.

Part: BULB — FAILED (CABIN)

PDX - EVACUATION LIGHT AT ROW 8 IS INOPERATIVE IN ARM POSITION, WORKED IN ON POSITION. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL.

Part: COVER — MISSING (CABIN)

EVACUATION LIGHT AT ROW 8 MISSING COVER. MAINTENANCE INSTALLED NEW LIGHT ASSEMBLY, TESTED NORMAL.

Part: BULB — FAILED (CABIN)

SEAT 9E EVACUATION LIGHT INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT SEAT 8B REPORTED INOPERATIVE. MAINTENANCE RELAMPED AND SECURED WITH BREAKAWAY SAFETY WIRE, OPERATIONAL CHECK NORMAL.

Part: BULB — FAILED (CABIN)

SEVERAL OVERHEAD EVACUATION LIGHTS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL.

Part: PRINTED CIRCUIT — INOPERATIVE (CABIN)

PDX - OVERHEAD EXIT LIGHT AT ROW 8 INOP. REPLACED EXIT LIGHT CIRCUIT BOARD, OPERATIONAL TEST SATISFACTORY.

Part: PRINTED CIRCUIT — INOPERATIVE (CABIN)

SEA - CEILING EXIT SIGN RIGHT ARROW ON AFT SIDE DOES NOT ILLUMINATE. THE EMERGENCY EXIT SIGN CIRCUIT BOARD ASSY WAS REPLACED. AN OPERATIONAL CHECK OF THE LIGHTS INDICATES NORMAL OPERATION.

Part: BULB — FAILED (CABIN)

BOI - OVERHEAD EMERGENCY EVACUATION LIGHT INOP OVER ROW 8. INSTALLED SERVICEABLE LIGHT BULB, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

YEG - FORWARD EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE IN ARM POSITION WITH AIRCRAFT POWER OFF. RELAMPED, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - FWD SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED FWD CEILING BATTERY POWER SUPPLY. OPERATIONAL CHECK IS GOOD.

Part: PWR SUPPLY — INOPERATIVE (CABIN)

SEA- AFT EXTERIOR EMERGENCY EGRESS LIGHTS ARE INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD.

Part: MEGAPHONE — MALFUNCTION (CABIN)

BOI - AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

SEA- EXIT SIGN AT ROWS 8 AND 9 ARE OUT. REPLACED EXIT SIGN AT AFT SIDE OF ROW 8 AND 9, OPERATIONAL CHECKS GOOD.

Part: LAMP — FAILED (CABIN)

GEG - FORWARD EMERGENCY EXIT SIGN HAS MANY 28V LAMPS INOP. RELAMPED, OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

PDX - BOTH WING BELLY FAIRING EMERGENCY LIGHTS INOP. REPLACED AFT CARGO BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (COCKPIT)

FIRE WARNING LIGHT ON NR 2 FUEL LEVER DOES NOT TEST. FOUND BROKEN WIRE IN PEDESTAL AND PIN ON LIGHT ASSEMBLY. REPLACED LIGHT AND SPLICED BROKEN WIRE, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

SEA - VARIOUS CABIN LIGHTS INOP. RELAMPED AS REQUIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

SEA - FORWARD EXIT SIGN HAS SVERAL BULBS NOT FUNCTIONING IN ARMED OR ACTIVE MODE OF EMERGENCY LIGHTS. REMOVED AND REPLACED EXIT SIGN LIGHT ASSEMBLY AT FORWARD CABIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

SEA - COCKPIT BULKHEAD EXIT SIGN HAS NO LIGHTS ILLUMINATED IN ARMED MODE AND ARE VERY DIM IN ACTIVE MODE. REMOVED AND REPLACED EXIT SIGN ASSMBLY ON FORWARD BULKHEAD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

SEA - CENTER EXIT SIGN HAS SEVERAL OUT IN FORWARD SIGN. RMOVED AND REPLACED EXIT SIGN LIGHT ASSEMLBY IN CENTER CABIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

GEG - EMERGENCY SIGN OVER COCKPIT DOOR IN GALLEY INOP. REMOVED AND REPLACED EXIT SIGN ASSEMBLY ON FORWARD BULKHEAD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

OVERHEAD AND EMERGENCY EXIT DOOR EVACUATION LIGHT INOP. REPLACED POWER SUPPLY AT POSITIONS LV57, LV55, LV53, AND LV52, OPERATIONAL CHECK GOOD.

Part: APU — MALFUNCTION (AFT FUSELAGE)

ON THE GROUND SMOKE SMELL NOTED IN THE CABIN. VISUALLY IDENTIFIED AS BLUE SMOKE. DETERMINED THE OIL SMOKE/SMELL TO BE FROM THE AUXILIARY POWER UNIT. COMPLIED WITH MAINTENANCE TASK CARD 8301001, TO PURGE SMOKE FROM CABIN. NO MORE SMOKE OR SMELL NOTED. PLACED AUXILIARY POWER UNIT ON MEL, REFERENCE 49-1. MEL CLEARED ON 6/4/97 BY REPLACING THE APU, OPERATIONAL CHECKS GOOD.

Part: SMOKE DETECTOR — ACTIVATED (LT LAVATORY)

SMOKE DETECTOR IN LEFT LAVATORY WENT OFF FOR ABOUT 15 SECONDS, ABOUT 1 MINUTE AFTER TAKEOFF. PLACED ON MEL, REFERENCE 26-7. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 5/31/97 BY RECONNECTING SMOKE DETECTOR. PROBLEM WAS WITH THE APU (REF QXEA9700216 ODR), OPERATIONAL CHECKS GOOD.

Part: SMOKE DETECTOR — ACTIVATED (RT LAVATORY)

SMOKE DETECTOR IN RIGHT LAVATORY GOES OFF INTERMITTANTLY. PLACED ON MEL, REFERENCE 26-7. DETECTOR DISCONNECTED, AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 5/31 BY RECONNECTING SMOKE DETECTOR. PROBLEM IS WITH APU WHICH IS ON MEL (REF QXEA9700216 ODR).

Part: SMOKE DETECTOR — MALFUNCTION (RT LAVATORY)

STARBOARD LAVATORY SMOKE DETECTOR BECAME ACTIVE AT 10,000 FEET THROUGH 16,000 FEET DURING CLIMB, THEN QUIT. NO BURNING OR SMOKING MATERIALS NOTED IN FLIGHT OR AFTER THE AIRCRAFT LANDED. INSPECTED SYSTEM AND DETERMINED TO BE SMOKE FROM THE AUXILIARY POWER UNIT. PLACED APU ON MEL, REFERENCE 49-1. MEL CLEARED ON 5/30/97 BY REPLACING THE SMOKE DETECTOR MODULE, WHICH WAS NOTICED TO GO OFF WHEN TOUCHED, OPERATIONAL CHECKS GOOD.

Part: SMOKE DETECTOR — MALFUNCTION (LAVATORY)

LEFT HAND LAVATORY SMOKE DETECTOR SOUNDS IN FLIGHT. DETECTOR IS ABLE TO BE RESET. NO SMOKE OR SMELL NOTED WITHIN CABIN AND LAVATORY. REPLACED LEFT LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS GOOD.

Part: CIRCUIT CARD — FAILED (CABIN)

CEILING EXIT LIGHT AT ROW 8 IS INOP. REPLACED CIRCUIT CARD FOR LIGHT, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS OUT AT ROWS 5, 6, 8 AND 9. REMOVED AND REPLACED POWER SUPPLY AT ROW NR 9, OPERATIONAL CHECKS GOOD.

Part: AIR DISTRIBUTION — ODOR (CABIN)

STRONG OIL SMELL IN CABIN WITH THE CABIN PACK ON. PURGED CABIN AIR CONDITIONING DUCTING, NO SMELL NOTICABLE.

Part: HARNESS — LOOSE (RT MLG)

CLT - FLT 993 - AFTER TAKEOFF FROM TYS, RIGHT MLG RED LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND LIGHT WENT OUT. FLIGHT CONTINUED WITHOUT INCIDENT TO CLT. MAINTENANCE FOUND RIGHT MAIN GEAR HARNESS CONTACTING AFT DOOR HOOK BEFORE DOOR COULD LOCK. RESECURED LOWER HARNESS TO STRUT. (X)

Part: TORQUE LINK — BROKEN (LT UPPER)

HTS - FLT 1028 - ON TOUCHDOWN, AIRCRAFT VEERED TO THE LEFT AND BOTH LEFT MAIN TIRES CAME OFF. AN EMEGENCY EVACUATION WAS NOT NECESSARY. NO INJURIES WERE REPORTED. MAINTENANCE REPLACED THE LEFT UPPER TORQUE LINK. (Z)

Part: HYD LINE — CRACKED (LANDING GEAR)

CLT - FLT 1250 - THE NR 1 HYDRAULIC SYSTEM QUANITY AND PRESSURE WENT TO ZERO IMMEDIATELY AFTER FLAP RETRACTION AFTER TAKEOFF. CREW RETURNED TO CLT. MAINTENANCE REPLACED THE SUPPLY LINE ON THE LANDING GEAR SELECTOR VALVE. LEAK CHECKED GOOD. (W)

Part: ANGLE — CRACKED (FWD PRESS BLKHD)

PIT - DURING SCHEDULED SIP INSPECTION, FOUND CRACK IN THE FORWARD PRESSURE BULKHEAD LOWER CONNECTION ANGLE AT FRAME 1550 BETWEEN STATION 72 AND 3. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-11-00. (W)