N484US

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,250 hrs · 37,712 cycles

PDX- EXIT LIGHT NEAR FRONT OF CABIN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT NEAR FRONT OF CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HARNESS — DAMAGED (ROW 12 - 14) · airframe 31,220 hrs · 37,681 cycles

PDX - EVACUATION PATH LIGHTING NEAR ROW 12, 13 AND 14 WAS FOUND INOPERATIVE. UPON INSPECTION, FOUND DAMAGED WIRING HARNESS ON SEAT 14AB. REMOVED AND REPLACED SEAT 14AB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 30,994 hrs · 37,471 cycles

FAT - CENTER OVERHEAD AISLE EMERGENCY LIGHTS REPORTED INOPERATIVE. FERRIED AIRCRAFT TO PDX. REMOVED AND REPLACED CIRCUIT BOARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — FAILED (LT MLG) · airframe 30,876 hrs · 37,371 cycles

BZN - DURING LANDING ROLL, LEFT BRAKE WAS INEFFECTIVE UNTILL FULL PEDAL DEFLECTION. PERFORMED SERVICE BLEED OF NR 2 BRAKE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,509 hrs · 36,983 cycles

PDX - THE FLOOR PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND FUSELAGE SKIN CHAFED BY OUTBOARD EDGE OF PANEL 92BD BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1306.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- PREVIOUS REPAIR ON RIGHT HAND LOWER FUSELAGE SKIN CHAFED BY PANEL 91BC. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1304.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND LOWER FUSELAGE SKIN CHAFED BY INBOARD EDGE OF PANEL 92BD BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1305.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND LOWER FUSELAGE SKIN IS CHAFED BY PANEL 91BD INBOARD EDGE BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE3, 51-10-4 AND HORIZON AIR EA 4-53-1303.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP, AFT SIDE OF FRAME 24-2 AND STRINGER 33 HAS A CRACK IN RADIUS OF CLIP. RIVET INSTALLED IN CRACKED HOLE, NEEDS WASHER UNDER BUCK TAIL. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-4 AND 53-02-13 PAGE 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- AFT CARGO DOOR AFT TOP CORNER OF APERTURE SUSPECT CRACK GOING BEYOND STOP DRILL IN APERTURE. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-01-01 PAGE 8.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- FUSELAGE BOTTOM PANEL 98G SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 53-53-04, PAGE 12 AND SRM 51-31-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- PREVIOUS REPAIR ON BOTTOM CENTER OF FUSELAGE CHAFED BY PANEL 91BC FORWARD OF FRAME 14285. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-01.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 304,743 hrs

PDX- FUSELAGE BOTTOM PANEL 98F SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 55-53-04, PAGE 9 AND SRM 51-31-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND LOWER FUSELAGE SKIN REPAIR CHAFED BY PANEL 91BC LEFT OF CENTER BOTTOM FUSELAGE BETWEEN FRAME 14285 AND 14775. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-4 AND 53-02-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STRAP PATCH ON BOTTOM OF FUSELAGE ON FRAME 14285 IS CHAFED LEFT AND RIGHT OF CENTER BY PANEL 91BC. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP HAS A CRACK ON AFT SIDE OF FRAME 41-2, STRINGER 45. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- OBLIQUE FRAME TO FUSELAGE CLIP AFT OF FRAME 32-2 AT STRINGER 48 HAS A CRACK. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601 AND SRM 53-02-13, PAGE 5.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SCRATCH IN FUSELAGE SKIN BELOW BOTTOM AFT CORNER OF MAIN CABIN DOOR APERTURE. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01-01, PAGE 3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CONNECTION ANGLE FOR COMPOSITE ATTACHMENT TO FRAME 22293 UPPER RIGHT HAND CORNER IS CRACKED PAST STOP DRILL. REPAIRED IAW HORIZON AIR EA 4-53-1298.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 18 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 7 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SCRATCH IN FUSELAGE SKIN BETWEEN FRAME 3820 AND 3450 BETWEEN STRINGER 18 AND 19. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-1298.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 68 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 64 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 60 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 6 AND 7 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2 BETWEEN STRINGERS 4 AND 5 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 62 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF FRAME 16-2, BETWEEN STRINGERS 8 AND 9 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: BEAM — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACK UNDER 1ST CROSS TIE BEAM AT ENTRY WAY STRINGER 73. REPAIRED IAW FOKKER SRM 53-24-07, PAGE 8 AND SRM 51-31-01, AND SRM 51-31-05.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 11 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEN STRINGERS 70R AND 71 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- FUSELAGE SKIN CRACKED AT RIVET AT FRAME 50-2 BETWEEN STRINGERS 49 AND 50. REPAIRED IAW FOKKER SRM 53-02-02 AND HORIZON AIR EA 4-53-1294.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 66 AND 67 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: STIFFENER — BENT (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 68 AND 69 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.

Part: BRACKET — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND AIR CYCLE MACHINE BAY SKIN BELOW UPPER AIR CYCLE MACHINE MOUNT BRACKET IS DENTED AND GOUGED. REPAIRED IAW FOKKER SRM 53-02-01.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- DISCOVERED HOLE ON DOUBLER PLATE STATION 181496 STRINGER 5. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8.

Part: FASTENER — LOOSE (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE AND SMOKING HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02 AND HORIZON AIR EA 4-55-247.

Part: CLIP — MISDRILLED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP HAS A PREVIOUS STOP DRILL THAT IS DRILLED THRU STRINGER ANGLE AND INTO FUSELAGE SKIN AT FRAME 32-2 STRINGER 9. REPAIRED IAW FOKKER SRM 53-02-12 AND SRM 53-02-13.

Part: FASTENER — LOOSE (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT VERTICAL CONNECTION ANGLE HAS LOOSE HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02, SRM 51-31-01 AND HORIZON AIR EA 4-55-247.

Part: SKIN — NICKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN NICKED ON RIGHT SIDE OF ANTENNA MOUNT ON AFT FUSELAGE BETWEEN FRAME 16060 AND 16660. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, AND SRM 51-30-03, PAGE 703.

Part: BRACKET — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND BAY SKIN BELOW UPPER AIR CYCLE MACHINE BRACKET IS DENTED AND GOUGED. REPAIRED IAW FOKKER SRM 53-02-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- MTX REQUEST INSTALLATION OF REINFORCMENT DOUBLERS ON FORWARD LOWER CORNER OF SERVICE EMERGENCY DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-02-16 PAGE 12, 51-32-01 AND HORIZON AIR EA 4-53-1281.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- AFT CARGO DOOR HINGE ATTACH POINT ON DOOR OPENING APERTURE AFT NUT PLATE BULGED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-31-05.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- CLIP AT FRAME 16060 CRACKED AT STRINGER 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME CLIP CRACKED AT FRAME 13815A BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: RIVET — MISSING (FUSELAGE SKIN) · airframe 30,474 hrs · 36,951 cycles

PDX- 2 RIVETS ON THE EXTERNAL FUSELAGE SKIN JUST FORWARD OF THE APU EXHAUST REQUIRES INSTALLATION. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME CLIP AT FRAME 16660 CRACKED BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: SKIN — CHAFED (TE FLAP) · airframe 30,474 hrs · 36,951 cycles

PDX- CHAFE ON RIGHT HAND INBOARD FLAP UPPER SKIN, 27.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED IAW FOKKER SRM 57-02-05 AND 51-10-4.

Part: FLANGE — CHAFED (ACCESS DOOR) · airframe 30,474 hrs · 36,951 cycles

PDX- ACCESS DOOR 23A IS CHAFED AROUND DOOR FLANGE. REPAIRED IAW FOKKER SRM 52-01-01 AND SRM 51-10-4.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED CLIP AT FRAME 9305, LOWER INBOARD SIDE OF LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-30-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- REPAIR ANGLE CRACKED AT INBOARD RIVET ON BOTTOM LEFT HAND CENTER OF FUSELAGE FORWARD EDGE OF 91BC. REPAIRED IAW FOKKER SRM 53-53-04 PAGE 15 AND 51-31-01.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME CLIP CRACKED AT 13815B BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: FLANGE — DENTED (ACCESS DOOR) · airframe 30,474 hrs · 36,951 cycles

PDX- ACCESS DOOR 21A AFT FLANGE DENTED. REPAIRED IAW FOKKER SRM 52-40-03 AND SRM 51-10-4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CLIP CRACKED ON BOTH ENDS AT FRAME 16660 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: ANGLE — LOOSE (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE HI-LOKS AT FRONT SPAR. REPAIRED IAW FOKKER SRM 51-30-02.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 1. REPAIRED IAW FOKKER SRM 55-31-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- ANGLE CRACKED AT FRAME 4175 ABOVE STRINGER 12. REPAIRED IAW FOKKER SRM 53-14-06, PAGE 2 AND SRM 51-31-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- ANGLE CRACKED FORWARD OF FRAME 4175 ABOVE STRINGER 12. REPAIRED IAW FOKKER SRM 53-14-06, PAGE 2 AND SRM 51-31-01.

Part: RIVET — LOOSE (LT WING TE FLAP) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND WING AT STATION 1700 INBOARD FLAP HAS 5 SMOKING RIVETS. REPAIRED IAW FOKKER SRM 51-00-00 AND HORIZON AIR EA 4-57-441.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- ANGLE CRACKED AFT OF FRAME 4175 ABOVE STRINGER 12. REPAIRED IAW FOKKER SRM 53-14-06, PAGE 2 AND SRM 51-31-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- AFT EDGE OF NOSE LANDING GEAR APERTURE IS CHAFED BY RIGHT NOSE GEAR DOOR. REPAIRED IAW FOKKER SRM 52-01-01 AND 53-01-01.

Part: ANGLE — LOOSE (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE AND SMOKING HI-LOKS AT SPAR 1. REPAIRED IAW FOKKER SRM 51-30-02.

Part: CLIP — CRACKED (FUSELAGE FRAME) · airframe 30,474 hrs · 36,951 cycles

PDX- CLIP CRACKED AT FRAME 4175, LOWER OUTBOARD SIDE OF LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED CLIP AT FRAME 16660 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16060 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: DUCT — CRACKED (ACM BAY) · airframe 30,474 hrs · 36,951 cycles

PDX- AIR CYCLE MACHINE OUTLET HAS POSSIBLE CRACK AT LOWER FORWARD CORNER. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-10-6 AND HORIZON AIR EA 4-53-1283.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16660 AND STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED CLIP AT FRAME 16060 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED ANGLE AT AFT INBOARD LOWER CORNER OF LEFT MAIN WHEEL WELL AT FRAME 13345. REPAIRED IAW HORIZON AIR EA 4-53-1286.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED CLIP AT FRAME 16660 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16660 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CRACKED CLIP AT FRAME 16060 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16660 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2 AND 53-02-13.

Part: MOUNT — CORRODED (ANTENNA) · airframe 30,474 hrs · 36,951 cycles

PDX- ANTENNA MOUNT BETWEEN 15205 FRAME TO 15635, STRINGER 1 AND 74 HAS CORROSION AND NO PAINT. REPAIRED IAW FOKKER SRM 51-10-4.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME 16060 STRINGER 56 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 53-02-13, PAGE 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16060 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SUSPECTED CRACKED CLIP AT FRAME 16060 AND STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01.

Part: FRAME — CORRODED (CARGO BAY) · airframe 30,474 hrs · 36,951 cycles

PDX- AFT CARGO PIT FRAME 13815A HAS CORROSION ON FRAME NUT PLATE ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1280.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME CAP AND SPLICE AT FRAME 13815A HAS EXFOLIATION CORROSION ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1280.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE IS SCRATCHED AND GOUGED 3 INCHES LONG AT STATION 6305. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE IS SCRATCHED AND GOUGED 3 INCHES FORWARD OF STATION 6805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK ACCESS HATCH PANEL 72A HAS LITE FRETTING CORROSION ON PANEL MOUNTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CORROSION ON FUSELAGE SKIN AT AFT DME MOUNTING POINT. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SERVICE EMERGENCY DOOR UPPER AFT APERTURE CORNER HAS A CRACK. REPAIRED IAW FOKKER SRM 53-02-16 AND HORIZON AIR EA 4-53-1281.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS MULTIPULE AREAS OF FRETTING BETWEEN STATION 9255 AND STATION 9805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SIX INCHES AFT OF STATION 8305 THERE ARE 2 SCRATCHES AT CUTOUT IN LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE HAS SMALL GOUGE AT LUG 11 INCHES AFT STATION 8805. REPAIRED IAW FOKKER SRM 53-10-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK, INBOARD FLANGE HAS FRETTING FROM STATION 11794 TO STATION 13151. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE LEFT HAND OUTBOARD SEAT TRACK IS SCRATCHED/GOUGED 3 INCHES FORWARD OF STATION 8805 AT CUTOUT. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SIX INCHES AFT OF STATION 9305 TOP FLANGE GOUGED ON BOTH SIDES OF TWO CUTOUTS OF LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK CHANNEL HAS A SCRATCH 1 INCH LONG 6.5 INCHES AFT OF FORWARD END. REPAIRED IAW FOKKER SRM 53-40-1 FIGURE 204 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- 1.5 INCHES AFT OF STATION 8805 THE TOP FLANGE CUTOUT OF LEFT HAND OUTBOARD SEAT TRACK HAS SCRATCHES/GOUGES. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE FRETTED FROM STATION 15263 TO STATION 15733. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- THREE INCH FRETTING AT STATION 16595 ON LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE. REPAIRED IAW FOKKER SRM 53-40-01 FIGURE 205 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK, INBOARD FLANGE HAS FRETTING APPROXMATELY 22.5 INCH LONG STARTING AT STATION 7955 TO STATION 8515. REPAIRED IAW 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS FRETTING 18 INCHES LONG STARTING AT STATION 8545. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK CHANNEL IS SCRATCHED 6 INCHES AFT OF STATION 9305. REPAIRED IAW FOKKER 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- INBOARD FLANGE HAS .5 INCH FRET AT STATION 17415 ON INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 FIGURE 205 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE HAS SMALL GOUGE ON INBOARD EDGE/CORNER 1.75 INCHES AFT OF STATION 8305. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK, INBOARD FLANGE HAS FRETTING APPROXMATELY 1.5 INCH LONG AT STATION 7600. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE FRETTED FROM STATION 13151 TO STATION 13853. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK CHANNEL BOTTOM SURFACE HAS LIGHT CORROSION AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-01, PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS 1 INCH FRETTING AT STATION 15923. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK, INBOARD FLANGE HAS FRETTING 3 INCHES LONG AT STATION 11103. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- AT STATION 7805 TOP FLANGE GOUGED 2 INCHES LONG, LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SMALL GOUGE AT CUTOUT OF TOP FLANGE 3 INCHES FORWARD OF STATION 9305. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK TOP RAILS JUST FORWARD OF FRAME 8305 WORN ON TOP OF LUGS. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS FRETTING 7 INCHES LONG FROM STATION 10753 TO STATION 10928. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CORROSION ON FUSELAGE AT UPPER ATC ANTENNA MOUNTING POINT. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 30,474 hrs · 36,951 cycles

PDX- SMALL GOUGE AT CUTOUT OF TOP FLANGE OF LEFT HAND OUTBOARD SEAT TRACK AT STATION 9305. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK ACCESS HATCH PANEL 74A HAS LITE FRETTING CORROSION ON PANEL MATTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8-9 AND 57-01-01 PAGE 5.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- REAR PRESSURE BULKHEAD BL 1250R HAS TWO SHREADED RIVETS AND THREE CRACKS ON VERTICAL ATTACH ANGLE BETWEEN BEAMS 6 AND 7. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-05 AND 51-11-04.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT STATION 15148. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE LEFT HAND SEAT TRACK HAS TWO SCRATCHES AT STATION 16915. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS MULTIPULE AREAS OF FRETTING STARTING AT STATION 9805 TO STATION 10253. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS GOUGE AT STATION 10253. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-01, PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE HAS .25 INCH FRETTING AT STATION 17285. REPAIRED IAW FOKKER SRM 53-40-01 FIGURE 205 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE SCRATCHED 8.5 INCHES LONG BEGINNING 2.5 INCHES AFT OF FORWARD END. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE IS SCRATCHED 13 INCHES AFT OF FORWARD END. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE SCRATCHED AND GOUGED 8 INCHES FORWARD OF STATION 6805, LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE HAS 3 INCH LONG SCRATCH AT STATION 8305 OF LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE IS SCRATCHED AND GOUGED AT CUTOUT AT STATION 8805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE IS SCRATCHED/GOUGED AT CUTOUT 8 INCHES FORWARD OF STATION 8805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- 3.5 INCHES AFT OF STATION 9805 TWO LUGS ARE GOUGED ON TOP FLANGE OF LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 202 AND 51-10-4 PAGE 8.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK ACCESS HATCH PANEL 74D HAS LITE FRETTING CORROSION ON PANEL MATTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5 AND 51-10-4 PAGE 9.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK ACCESS HATCH PANEL 74E HAS LITE FRETTING CORROSION ON PANEL MATTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5 AND 51-10-4 PAGE 9.

Part: PRESSURE PANEL — CRACKED (ACM BAY) · airframe 30,474 hrs · 36,951 cycles

PDX- NOSE LANDING GEAR BAY SIDEWALL APPEARS TO BE CRACKED IN LEFT HAND AIR CYCLE MACHINE BAY AT STATION 2550. REPAIRED IAW FOKKER SRM 53-11-00.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH PANEL 74E HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS AREA OF LIGHT CORROSION ON LEFT HAND SEAT RAIL INSIDE RADIUS 15. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE NICKED/GOUGED AT CUTOUT, CHANNEL ALSO SCRATCHED AT STATION 11794. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT STATION 7550. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS AREA OF LIGHT CORROSION ON LEFT HAND SEAT RAIL INSIDE OF RADIUS 16. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK CHANNEL SCRATCHED 28 INCHES AFT OF STATION 11253. REPAIRED IAW FOKKER SRM 53-40-1 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN BOTTOM OF CHANNEL AND LEFT HAND AND RIGHT HAND RADIUS AT THE FOLLOWING LOCATIONS, 4 INCHES AFT OF FRAME 9305, 0-5 INCHES FORWARD OF FRAME 9305 AND 9-11 INCHES FORWARD OF FRAME 9305. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK PANEL 74B HAS LITE FRETTING CORROSION ON PANEL MATTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE HAS TWO SCRATCHES AT STATION 16810. REPAIRED IAW FOKKER SRM 53-40-01 FIGURE 205.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT LUG AT STATION 11794. REPAIRED IAW FOKKER SRM 53-40-1 PAGE 201.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE CUTOUT SCRATCHED 3.5 INCHES FORWARD OF STATION 12853 AND 6.5 INCHES FORWARD OF STATION 12853 ON LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK BOTTOM CHANNEL HAS SEVERAL SMALL AREAS OF LIGHT SURFACE CORROSION 8 - 9 INCHES AFT OF FRAME 9805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201, 53-01-01 PAGE 8 AND 51-10-4 PAGE 9.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING TO FUSELAGE AREA, UPPER SKIN HAS NUMEROUS AREAS OF BARE METAL AND LITE SURFACE CORROSION ON RIVET BUCK TAILS. REPAIRED IAW FOKKER SRM 51-31-01.

Part: BEAM — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- UPPER AND LOWER REPAIR DOUBLERS ON FORWARD PRESSURE BULKHEAD BEAM 6 ARE CRACKED THROUGH HI-LOK ON UPPER SURFACE AND THROUGH RADIUS ON LOWER AT BL 0. REPAIRED IAW FOKKER SRM 53-02-18 AND HORIZON AIR EA 4-53-1237.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK CHANNEL SCRATCHED AT STATION 7550. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH PANEL 74C HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-01-01 PAGE 4.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH PANEL 74F HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.

Part: PRESSURE PANEL — CRACKED (ACM BAY) · airframe 30,474 hrs · 36,951 cycles

PDX- NOSE LANDING GEAR BAY SIDEWALL APPEARS TO BE CRACKED IN LEFT HAND AIR CYCLE MACHINE BAY AT STATION 2775. REPAIRED IAW FOKKER SRM 53-11-00.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK ACCESS HATCH PANEL 74C HAS LITE FRETTING CORROSION ON PAENL MATTING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5 AND 51-10-4 PAGE 9.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN CHAFED AT FORWARD CARGO DOOR APERTURE, LOWER AFT SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3-6 AND SRM 55-10-01, PAGE 4.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK, LEFT HAND AND RIGHT HAND LUGS LOCATED 40 INCHES AFT OF FRAME 9805 HAVE STEP WEAR ON UNDERSIDE. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 - 206.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK TOP FLANGE GOUGED NEAR STATION 11253. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS 2 SMALL SPOTS OF LITE CORROSION IN LEFT HAND SIDE OF SEAT HOLES FORWARD FRAME 9305. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE HAS 2 GOUGES AT STATION 15808. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS LITE SURFACE CORROSION ON BOTTOM OF CHANNEL AFT OF FRAME 12875. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT CUTOUT AT STATION 11103. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION ON SEAT RAIL LUG INBOARD FACES, LOCATED 15 INCHES AFT OF FORWARD END OF SEAT RAILS. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- INBOARD FLANGE CAMLOK HOLE ON INBOARD LEFT HAND SEAT TRACK HAS GOUGES AROUND IT AT STATION 16965. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK CHANNEL BOTTOM SURFACE HAS LITE CORROSION FROM FRAME 13815. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4, PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION ON LEFT HAND SEAT RAIL INSIDE RADIUS BETWEEN 4 - 6 INCHES FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT CUTOUT AT STATION 13753 NEAR SEAT LEG MARKER. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK CHANNEL SCRATCHED AT STATION 5765 TO STATION 6120. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: FRAME — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- FRAME 15635 LEFT HAND BL 700 VERTICAL EXTRUSION HAS A GOUGE. REPAIRED IAW HORIZON AIR EA 4-53-1285.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE SCRACTHED/GOUGED AT STATION 6675. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH PANEL 74D HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL APERTURE FLANGE ABOVE ACCESS HATCH PANEL 74A HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 57-01-01, PAGE 4.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK CHANNEL HAS A SCRATCH 6 INCHES LONG AT STATION 15263. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND SEAT TRACK INBOARD FLANGE HAS FRETTING ON CENTER FLOOR PANEL. REPAIRED IAW FOKKER SRM 53-40-01 AND 51-10-4 PAGE 9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CORROSION ON FUSELAGE SKIN AT LOWER ATC ANTENNA MOUNTING POINT. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-15-01.

Part: SKIN — DENTED (TE FLAP) · airframe 30,474 hrs · 36,951 cycles

PDX- SHARP DENT ON RIGHT HAND INBOARD FLAP LOWER SKIN, 20.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED IAW FOKKER SRM 57-01-01 AND 57-02-05 PAGE 3.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND VERTICAL STABILIZER SKIN HAS A GOUGE BETWEEN SPARS 2 AND AFT ON RIB 304. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 55-01-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN CHAFED AT FORWARD CARGO DOOR APERTURE, LOWER FORWARD SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3-6 AND SRM 51-10-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND SEAT TRACK TOP FLANGE HAS GOUGES 2.5 INCHES AFT OF STATION 17415. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: CLIP — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CLIP CRACKED AT FRAME 4870 BELOW OUTBOARD SIDE OF RIGHT HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 1-11-1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK CHANNEL GOUGED AT TOP FLANGE CUTOUTS FORE AND AFT OF CHANNEL SCRATCH AT STATION 12853. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND SEAT TRACK RIGHT HAND RAIL HAS GOUGE WITH CORROSION IN IT, INSIDE RADIUS AT SEAT PEG HOLE AFT OF FRAME 9305A. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 3,074 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL, LEFT HAND SIDE AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK CHANNEL SCRATCHED AT STATION 8455. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- AFT SIDE OF FORWARD BULKHEAD CRACKED, BEAM 3, BL 400 - 500R. REPAIRED IAW FOKKER SRM 53-02-18 AND SRM 51-10-4, AND HORIZON AIR EA 4-53-1289.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE GOUGED AT CUTOUT 28 INCHES AFT OF STATION 11253. REPAIRED IAW FOKKER SRM 53-40-1 PAGE 201.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGES SCRATCHED AT STATION 6300. REPAIRED IAW FOKKER SRM 53-41-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND INBOARD SEAT TRACK TOP FLANGE HAS 2 GOUGES AT STATION 15733. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND OUTBOARD SEAT TRACK CHANNEL IS SCRATCHED/GOUGED 1.375 INCHES LONG AND 5 INCHES AFT OF STATION 14793. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- TOP FLANGE CUTOUTS 4.5 INCHES AFT OF STATION 15263 NICKED/GOUGED ON LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- LEFT HAND SEAT TRACK CHANNEL HAS 2 INCH SCRATCHES, 6 INCHES FORWARD OF STATION 17845 AND FRAME 15635. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201 AND 51-10-4 PAGE 9.

Part: ATTACH FITTING — DAMAGED (RUDDER) · airframe 30,474 hrs · 36,951 cycles

PDX- RUDDER SHANK DRIVE FITTING ATTACH FOR AFT END OF RUDDER ACTUATOR HAS THE COTTER PIN HOLE TORN OUT AND A NICK ON THE EDGE OF UPPER LUG. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 51-30-02 AND SRM 55-02-07, PAGE 10.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH PANEL 72A HAS LITE FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 4 AND SRM 51-10-4.

Part: SKIN — CORRODED (RT WING) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND WING FUEL TANK APERTURE FLANGE ABOVE ACCESS HATCH 74B HAS LITE FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 57-01-01, PAGE 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND SEAT TRACK AFT MOST SECTION RIGHT HAND RAIL HAS A PIT 1 INCH WITH CORROSION ON TOP SURFACE 9.75 INCH AFT OF FORWARD SPLICE. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-40-01.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF RIGHT HAND LOWER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-244.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN CHAFED AT CENTER CARGO DOOR APERTURE, LOWER AFT SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3 -6 AND SRM 51-10-4.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF LEFT HAND UPPER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-245.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK RIGHT HAND RAIL HAS PIT WITH CORROSION IN IT, AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF RIGHT HAND UPPER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-244.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- CORROSION ON FUSELAGE AT FORWARD DME ANTENNA MOUNTING POINT. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS SPOT OF LIGHT SURFACE CORROSION IN BOTTOM CHANNEL BELOW SEAT LUG FORWARD OF FRAME 11905. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 30,474 hrs · 36,951 cycles

PDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF LEFT HAND LOWER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-245.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK HAS 3 SPOTS OF LIGHT SURFACE CORROSION IN BOTTOM OF CHANNEL AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND OUTBOARD SEAT TRACK AFT MOST SEGMENT HAS AREAS WHERE UPPER CORNERS OF SEAT OPENINGS ARE GOUGED. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 201.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN CHAFED AT CENTER CARGO DOOR APERTURE, LOWER FORWARD SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK LEFT HAND RAIL HAS LIGHT CORROSION ON INSIDE RADIUS FROM 28 - 30 AFT OF FRAME 9805. REPAIRED IAW FOKKER 53-40-01 PAGE 201 AND 51-10-4.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- EXTERIOR FUSELAGE SKIN JUST FORWARD AT APU EXHAUST OUTLET HAS 2 RIVET HEADS CORRODED OFF. REPAIRED IAW FOKKER 51-01-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,474 hrs · 36,951 cycles

PDX- SKIN DOUBLER UNDER TCAS ANTENNA HAS LIGHT CORROSION AROUND SCREW HOLES BETWEEN FRAME 4175 AND 4610. BOTTOM CENTER OF FUSELAGE REPAIRED IAW FOKKER SRM 51-10-4.

Part: MOUNT — CORRODED (RADIO ALTIMETER) · airframe 30,474 hrs · 36,951 cycles

PDX- FORWARD RADIO ALTIMETER MOUNTING STRUCTURE HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01-01, PAGE 6.

Part: MOUNT — CORRODED (ANTENNA) · airframe 30,474 hrs · 36,951 cycles

PDX- ANTENNA MOUNT BOTTOM CENTER OF AFT FUSELAGE BETWEEN FRAME 1606 AND 16660 HAS LIGHT CORROSION AND SKIN NICKED ON RIGHT SIDE. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-4 PAGE 9.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 30,262 hrs · 36,738 cycles

PDX- CENTER EXIT SIGN HAS BURNT OUT BULBS ON FORWARD SIDE. REMOVED AND REPLACED LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,232 hrs · 36,738 cycles

PDX- EMERGENCY EXIT LIGHTS AT ROWS 5, 6, AND 8 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT, BATTERY CARTRIDGE AND BATTERY PACK. TEST OF PASSENGER COMPARTMENT EMERGENCY LIGHTS ARE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 29,941 hrs · 36,408 cycles

PDX- LIGHT BULBS BURNT OUT IN EXIT SIGN LIGHT OVER COCKPIT DOOR. REMOVED AND REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (PRESS BULKHEAD) · airframe 35,473 hrs · 44,702 cycles

PDX - CRACK ON BEAM OF AFT PRESSURE BULKHEAD FRONT SIDE. REPAIRED IAW HORIZON AIR EA 4-53-1099.

Part: CIRCUIT BOARD — MALFUNCTIONED (COCKPIT) · airframe 29,545 hrs · 36,023 cycles

SEA- FORWARD EXIT SIGN ABOVE COCKPIT DOOR HAS SEVERAL INOPERATIVE LIGHT BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED (FUSELAGE) · airframe 29,491 hrs · 35,961 cycles

PDX- SMOKE IN CABIN THAN APU SUDDENLY STOPPED. REMOVED AND REPLACED APU, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 29,489 hrs · 35,960 cycles

GEG - PILOT REPORTED A EMERGENCY EXIT SIGN WAS INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 29,481 hrs · 35,952 cycles

GEG - THE EMERGENCY EXIT LIGHT AT ROW 8 WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (EVAC LIGHT)

SEA- THE NR 1 EMERGENCY EVACUATION LIGHT WAS FOUND INOPERATIVE DURING INSPECTION. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN)

SEA - EMERGENCY LIGHTS IN NR 1 EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — MALFUNCTIONED (ANTI SKID SYSTEM)

SEA - DURING LANDING ROLL, BREAKING EFFECTIVNESS DIMINISHED NOTICEABLY. INSPECTED ANTI SKID SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.

Part: SIGN — INOP (ROW 8)

GEG - BOTH EXIT SIGNS AT ROW 8 ARE INOPERATIVE. REMOVED AND REPLACED BOTH EXIT SIGN ASSEMBLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOP (COCKPIT)

PDX- EMERGENCY SIGN OVER COCKPIT DOOR HAD LIGHTS INOP. REPLACED CIRCUIT BOARD OVER COCKPIT DOOR.

Part: SKIN — DAMAGED (FUSELAGE)

SEA - GASH AND DENT IN FUSELAGE SKIN, JUST AFT OF MAIN CABIN DOOR. DAMAGED NOTED 70 MILLIMETERS IN LENGTH FORMING TWO DENTS, .1 INCHES AND .045 INCHES IN DEPTH. DAMAGE OUT OF LIMITS. AIRCRAFT SAFE FOR FERRY FLIGHT. REPAIRED AS REQUIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

GEG - THREE VOLT EVACUATION LIGHTS ON RIGHT EMERGENCY EXITS ARE DIM. MAINTENANCE REPLACED THE POSITION NR 4 EMERGENCY POWER SUPPLY, LIGHTS OPERATIONALLY TESTED NORMAL.

Part: SIGN — BROKEN (CABIN)

PDX - THE EXIT SIGN OVER THE COCKPIT DOOR FELL AND BROKE A WIRE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN, OPERATIONAL CHECK NORMAL.

Part: FUSE — BLOWN (RT EXTERIOR EEL)

PDX - WHILE AIRCRAFT WAS IN THE HANGAR FOR OTHER MAINTENANCE A NON-ROUTINE WAS GENERATED FOR THE RIGHT FORWARD BELLY FAIRING EMERGENCY LIGHT INOPERATIVE. A FUSE ON THE EMERGENCY BATTERY PACK WAS REPLACED. OPERATIONAL CHECKS SATISFACTORY.

Part: FUSE — FAILED (CABIN)

PDX - RIGHT WING FORWARD EMERGENCY EVACUATION LIGHT INOPERATIVE. MAINTENANCE REPLACED A FAULTY FUSE ON THE POWER SUPPLY. OPERATIONAL CHECKS NORMAL.

Part: POWER SUPPLY — INOP (CABIN)

THREE CABIN CEILING EVACUATION LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE FORWARD RIGHT PASSENGER COMPARTMENT POWER SUPPLY AND OPERATIONALLY TESTED IT, TESTED NORMAL.

Part: SIGN — INOP (ROW 8)

EMERGENCY EXIT SIGN AT ROW 8 INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN ASSEMBLY, OPERATIONAL TEST IS NORMAL.

Part: POWER SUPPLY — INOP (CARGO COMPT)

RIGHT HAND FORWARD EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SELF CONTAINED BATTERY POWER SUPPLY IN FORWARD BELLY CARGO COMPARTMENT, OPERATIONAL TESTS WERE NORMAL.

Part: SPAR — DELAMINATED (WS 4700)

LEFT-HAND WING FRONT SPAR LOWER MOUNTING FLANGE FOR INBOARD END OF PANEL 61C AT STATION 4700 HAS ONE LAYER DELAMINATING. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (2).

Part: LINK — CHAFED (LT SPEED BRAKE)

SPEED BRAKE LEFT-HAND SUPPORT LINK CHAFING ON COMPOSITE TAIL CONE AT UPPER AND LOWER ARMS. REPAIRED IAW HORIZON AIR EA 4-55-103.

Part: SKIN — DAMAGED (LT TE FLAP)

LEFT-HAND INBOARD FLAP LOWER INBOARD TRAILING EDGE HAS LARGE AREAS OF ROCK DAMAGE FROM MAIN TIRES. REPAIRED IAW FOKKER SRM 51-20-0, PARAGRAPH 4.

Part: SKIN — CRACKED (BS 19975-20075)

FUSELAGE SKIN CRACKED AT FOUR RIVETS BETWEEN FRAMES 19976 AND 20075 AND STRINGERS 38 AND 39. REPAIRED IAW HORIZON AIR EA 4-53-585.

Part: DOOR — CRACKED (RT EMER EXIT)

RIGHT-HAND FORWARD OVERWING EMERGENCY EXIT DOOR HAS A CRACK IN LOWER AFT AS SEEN THROUGH LIGHTENING HOLE. REPAIRED IAW HORIZON AIR EO 4-52-21 E.

Part: SKIN — DAMAGED (FUSELAGE)

RIGHT-HAND FUSELAGE AFT OF WING FAIRING AT PANEL 92BD HAS DAMAGE FROM 92BD RUBBING FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — CHAFED (FUSELAGE)

LEFT-HAND FUSELAGE SKIN HAS CHAFE DAMAGE AT PANEL 91BD. REPAIRED IAW FOKKER SRM 51-31-01.

Part: FRAME — CRACKED (FRAME 16-2)

OBLIQUE FRAME 16-2 HAS CRACKED REPAIR ANGLE ON AFT SIDE BETWEEN STRINGER 33 AND V-SKIN CUTOUT. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 4, FIGURE 3.

Part: SIDEWALL — DENTED (RT ACM COMPT)

DENT IN SIDE WALL BY LOWER AFT ACM MOUNT, RIGHT-HAND ACM. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9 PAGE 11 AND HORIZON AIR EA 4-53-579.

Part: SKIN — DENTED (LT TE FLAP)

LEFT-HAND INBOARD FLAP UPPER INBOARD TRAILING EDGE HAS 2 DENTS AT APPROXIMATELY STATION 2000 AND 2600. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 2, PARAGRAPH 7C.

Part: FRAME — CRACKED (BS 17565)

FRAME 17565 HAS CRACKED CLIP AT STRINGER 56. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 A.

Part: SUPPORT — CRACKED (FRAME 4900)

THE FLOOR SUPPORT IS CRACKED AT CLIP LOCATED AT FRAME 4900 BETWEEN AND ABOVE STRINGERS 70 AND 71. REPAIRED IAW FOKKER SRM 51-31-05.

Part: CLIP — CRACKED (FRAME 13815)

AFT CARGO PIT FRAME 13815A STRINGER 72 CRACKED CLIP. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.

Part: CASTELLATION — CRACKED (FRAME 10346)

FRAME CASTELLATION AT FRAME 10346, STRINGER 44 HAS A CRACK. REPAIRED IAW FOKKER SRM 51-31-01 PARAGRAPH 7 PAGE 13-17.

Part: CLIP — CRACKED (FRAME 12405)

THERE IS A CRACKED CLIP AT FRAME 12405 AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-07, PARAGRAPH 7.

Part: CLIP — CRACKED (FRAME 13815)

THERE IS A CRACKED CLIP AT FRAME 13815 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARAGRAPH 7.

Part: CASTELLATION — CRACKED (FRAME 10346)

FRAME CASTELLATION AT FRAME 10346 AT STRINGER 32 HAD A CRACK. REPAIRED IAW FOKKER SRM 51-31-01 PARAGRAPH 7.

Part: CLIP — CRACKED (FRAME 7805)

THERE IS A CRACK IN A CLIP AT FRAME 7805 AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 12875)

THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARAGRAPH 7.

Part: CLIP — CRACKED (FRAME 12875)

THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13-17.

Part: CLIP — CRACKED (FRAME 12875)

THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARAGRAPH 7.

Part: CASTELLATION — CRACKED (FRAME 10966)

FRAME CASTELLATION AT FRAME 10966, STRINGER 43 HAD A CRACK. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7.

Part: CLIP — CRACKED (FRAME 3805)

CLIP REPAIR IS CRACKED AT FRAME 3805, STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 33. REPAIRED IAW FOKKER SRM 51-10-4, STEP 4 AND SRM 51-31-01, PARAGRAPH 7, PAGE 13-17.

Part: CASTELLATION — CRACKED (FRAME 5805)

FRAME CASTELLATION CRACKED AT FRAME 5805, STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 AND 51-31-01.

Part: CLIP — CRACKED (FRAME 5805)

THERE IS A CRACK IN A CLIP AT FRAME 5805 AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 5805)

THERE IS A CRACK IN A CLIP AT FRAME 5805 AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 5305)

THERE IS A CRACK IN A CLIP AT FRAME 5305 AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FRAME 14755)

THERE IS A CRACKED CLIP AT FRAME 14755 AND STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHTS AT 8E INOP. RELAMPED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

GEG - EXIT LIGHT AT ROW 8 INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

GEG - OVERHEAD EXIT LIGHT IN GALLEY AND MID CABIN OUT. MAINTENANCE REPLACED EXIT SIGNS. OPERATIONAL TESTS ARE NORMAL.

Part: BULB — FAILED (CABIN)

COCKPIT ENTRY WAY EMERGENCY LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED AND RESULTS WERE NORMAL.

Part: BULB — FAILED (CABIN)

GEG - EMERGENCY SIGN OVER COCKPIT DOOR IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (CABIN)

SEA - LOWER EVACUATION LIGHT OUT BY ESCAPE SLIDE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

A 28 VOLT LIGHT INOP IN AFT CEILING EXIT SIGN. RELAMPED SIGN, OPERATIONAL CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN)

EMERGEMCY EXIT LIGHT AT ROW 8 HAS BURNT OUT BULBS. MAINTENANCE REPLACED EMERGENCY EXIT SIGN AND OPERATIONALLY TESTED. LIGHT TESTS NORMAL.

Part: SIGN — INOPERATION (COCKPIT)

COCKPIT ENTRANCE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED COCKPIT ENTRANCE SIGN AND OPERATIONALLY TESTED. TESTS NORMAL.

Part: BULB — FAILED (CABIN)

ALL EMERGENCY EXIT SIGNS HAVE BULBS OUT. MAINTENANCE RELAMPED, TESTED NORMAL.

Part: COVER — MISSING (CABIN)

BOI - SEAT 12B EMERGENCY EXIT COVER MISSING. MAINTENANCE REPLACED COVER, OPERATIONAL CHECKS NORMAL.

Part: BULB — FAILED (CABIN)

BOI - 2 EVACUATION LIGHTS IN CABIN INOPERATIVE. MAINTENANCE RELAMPED AND CHECKED OPERATION OF LIGHTS, TEST NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY EVACUATION LIGHT ON ROWS 5, 6, 9 AND 10 ARE INTERMITTENTLY ON. MAINTENANCE REPAIRED A CANNON PLUG ON THE EMERGENCE BATTERY PACK AT 9AB, OPERATIONAL CHECKS ARE NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

SEAT LIGHTING ON ROWS 11, 12, AND 14 GO ON AND OFF INTERMITTENTLY DURING TAXI AND FLIGHT. TIGHTENED CONNECTION AT ROW 9 AB, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.

Part: WIRE — BROKEN (CABIN)

SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS ON THE LAST 4 SEAT ROWS ARE INTERMITTANTLY ON. FOUND 2 BROKEN WIRES UNDER ROW 11. REPAIRED WIRING. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.

Part: CIRCUIT CARD — MALFUNCTION (CABIN)

EXIT SIGN AT ROW 8 OUT. REPLACED CIRCUIT CARD, OPERATIONAL CHECKS GOOD.

Part: LAMP — FAILED (CABIN)

GEG - OVERHEAD EVACUATION LIGHT AT ROW 4 IS INOP. MAINTENANCE RELAMPED.

Part: CIRCUIT BOARD — MALFUNCTION (COCKPIT)

AFT OVERHEAD EMERGENCY LIGHT EXIT SIGN AT CENTER AISLE INOP. REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD.

Part: SLIDE — LOW PRESSURE (CABIN)

EMERGENCY ESCAPE SLIDE PRESSURE BELOW MINIMUM. REPLACED EMERGENCY ESCAPE SLIDE.

Part: CONTROL PANEL — MALFUNCTION (COCKPIT)

ON DEPARTURE, BOTH HORIZIONTAL STABILIZER FLIGHT CONTROL CHANNEL CAUTION LIGHTS ILLUMINATED. ACCOMPLISHED THE EMERGENCY CHECKLIST, REVERTING THE STABILIZER SYSTEM TO MANUAL. ENCOUNTERED NO FURTHER PROBLEMS EN ROUTE, AND ACCOMPLISHED AN UNEVENTFUL LANDING AT FCA. IN FCA MAINTENANCE DRAINED AND SERVICED THE STABILIZER GEAR BOX, INSPECTED THE STICKING SWITCH AND HARNESS, CLEANED AND RECONNECTED ALL ELECTRICAL CONNECTIONS. PERFORMED A TEST OF THE STABILIZER ACTUATOR. REPLACED THE FLIGHT CONTROL PANEL, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (GALLEY)

GEG - SEVERAL 3 VOLT EMERGENCY LIGHT IN FORWARD GALLEY INOP. REPLACED NR 2 POWER SUPPLY, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHTS IN THE FORWARD OVERHEAD ARE OUT. REPLACED LAMPS, OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (CARGO COMPT)

BOI- AFT BELLY CARGO EMERGENCY LIGHTS REMAIN ON WHEN AIRCRAFT POWER IS SHUT DOWN. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

PDX- BOTH AFT EXTERNAL EMERGENCY LIGHTS ARE INOP. REPLACED BATTERY POWER SUPPLY FOR BOTH FORWARD AND AFT EXTERNAL EMERGENCY LIGHTS, OPERATIONAL CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN)

GEG - FORWARD EMERGENCY EXIG SIGN AT GALLEY HAS SEVERAL LAMPS INOP. REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

SEA- EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS BULBS INOP. RELAMPED SIGN, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG- OVERHEAD EXIT SIGN AT ROW 8 IS INOP. REPLACED 28 VOLT LAMPS AS REQUIRED, OPERATIONAL CHECKS GOOD.

Part: FIRE BOTTLE — EMPTY (NR 2 ENGINE)

GEG - NR 2 ENGINE FIRE BOTTLE AT ZERO PSI. REPLACED NR 2 ENGINE FIRE BOTTLE, TESTED GOOD.

Part: BULB — FAILED (CABIN)

GEG- CENTER AISLE OVERHEAD EXIT SIGN CENTER BULBS ARE INOP. RELAMPED SIGN AS REQUIRED, OPERATIONAL CHECKS GOOD.

Part: PRINTED CIRCUIT — MALFUNCTION (CABIN)

BOI- EXIT SIGN ABOVE COCKPIT DOOR HAS MANY LAMPS INOP. REPLACED CIRCUIT CARD FOR EXIT SIGN, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT ROW 9 BURNED OUT. REPLACED BULBS AS NECESSARY, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

GEG - OVERHEAD EXIT ANNUNCIATOR, AFT ROW 8, 9, 28 VOLT LAMPS INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: LIGHT BALLAST — FAILED (COCKPIT)

SMELLED STRONG ODOR AROUND THE FLIGHT COMPARTMENT GLARESHIELD. THE GLARESHIELD LIGHTS AT THE CAPTAIN'S POSITION ARE INOP. INSPECTED AND FOUND TO BE THE BALLAST (TRANSFORMER). DISCONNECTED THE BALLEST AND PLACED ON MEL, REFERENCE 33-1. MEL CLEARED ON 6/11 BY REPLACING THE BALLAST LG 17 AND RELAMPING THE LIGHTS, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

ONE LIGHT IN THE CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN IS BURNED OUT. RELAMPED, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG- EGRESS LIGHT FORWARD GALLEY, OVERHEAD COCKPIT DOOR 28V EMERGENCY LIGHT ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MECHANISM — OUT OF ADJUST (CABIN DOOR)

SEA - MAIN CABIN DOOR WOULD NOT OPEN ELECTRICALLY FROM INSIDE THE AIRCRAFT. DOOR REQUIRED TWO PEOPLE PUSHING TO START DOOR DOWN IN THE EMERGENCY MODE. NR 2 CABLE RELEASE MECHANISM WAS ADJUSTED I/A/W MAINTENANCE MANUAL. DOOR OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

FORWARD CABIN OVERHEAD EMERGENCY SIGN 28V LAMPS ARE INOP. BULBS 28V AND 3V WERE REPLACED AND SIGN OPS CHECKED GOOD.

Part: BALLAST — SHORTED (LG16 AND LG17)

SEA - SMOKE IN THE COCKPIT. CIRCUIT BREAKER FOR INSTRUMENT PANEL MAIN LIGHTING POPPED. INSTRUMENT FLOOD LIGHTS OUT ON CAPTAIN'S SIDE OUT ALSO. SMOKE TRACED TO INSTRUMENT FLOOD LIGHT BALLAST. BALLAST LG16 AND LG17 REPLACED. INSTRUMENT AND FLOOD LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

CABIN EMERGENCY LIGHTS FROM ROW 11 AFT ARE INOP. POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE FOUR OVER WING EMERGENCY EXIT SIGNS ARE INOP. EMERGENCY EXIT SIGN POWER SUPPLY WAS REPLACED AND THE EXIT SIGNS OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

LEFT HAND EMERGENCY EXIT HAS ONE EMERGENCY LIGHT OUT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.

Part: DNLOCK ACTUATOR — FAILED (LT MLG)

FLT 227 - DAY-CLT - LEFT MAIN GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE ON GEAR EXTENSION. CYCLED GEAR 5 TIMES, THEN DOWN AND LOCKED LIGHT ILLUMINATED. REPLACED LEFT MAIN GEAR DOWNLOCK ACTUATOR. (M)

Part: SWITCH — LOOSE (LT MLG DOOR)

TOA - FL 1250 - AFTER TAKEOFF FROM PIT, THE LEFT GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW CYCLED GEAR AND ALL LIGHTS WENT OUT. MAINTENANCE FOUND THE FORWARD LEFT GEAR DOOR SWITCH LOOSE. SWITCH WAS SECURED AND OPS CHECKED (GEAR SWING). CHECKED GOOD. (M)

Part: SKIN — CRACKED (NR 2 WINDOW POST)

PIT -DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN FUSELAGE SKIN AT LEFT NR 2 WINDOW POST ATTACH FLANGE. EDDY CURRENT INSPECTION REF SIP 53-10-08, PG 2. STOP DRILLED CRACK AND INSTALLED DOUBLER PER USAIR EA NR 32299. (M)

Part: STRINGER — CRACKED (STA 4700)

PIT - DURING SIP VISIT INSPECTION, FOUND 2 INCH CRACK LEFT WING FUEL TANK 'Z' STRINGER NR 13 JUST OUTBOARD OF STATION 4700, SIP REF 57-10-01. INSTALLED DOUBLER REPAIR PER USAIR EA NR 32309. (M)

Part: FRAME — CRACKED (NLG WW)

PIT - DURING SIP VISIT INSPECTION, FOUND .125 INCH CRACK IN FRAME STRIP AFT LEFT CORNER OF NOSE LANDING GEAR WHEEL WELL SIP REF 53-10-24. ROUTED OUT CRACKED AREA AND PRIMED AND PAINTED PER SRM 53-02-18 FIG 10 PARA 7. (M)

Part: FLEX SHAFT — BROKEN (TE FLAPS)

CLT - CREW RECEIVED 'WING FLAP ASYMMETRY' WARNING LIGHT, AFTER TAKEOFF. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE SQUIRREL CAGE DRIVE COUPLING BROKEN AND REPLACED IT. (M)

Part: HINGE — CRACKED (CARGO DOOR)

PIT - DURING SCHEDULED SIP INSPECTION, FOUND .1250 INCH CRACK IN MID CARGO DOOR HINGE FWD END. EDDY CURRENT INSPECTION REF SIP 52-30-09 PG 2. REMOVED AND REPLACED CARGO DOOR PER F28 MM 52-30-01. (W)

Part: VALVE — INOPERATIVE (CENTER WING)

PIT - FLIGHT NR 1141 - ON CLIMB-OUT FROM CVG, THE WING ANTI-ICE MODULATING VALVE WOULD NOT OPEN. NO HEATING OBSERVED ON TEMP GAUGE. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WING-ICE MODULATING VALVE PER MM 30-10-02. OPERATION CHECKS NORMAL. (Z)