N486US

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 30,783 hrs · 37,289 cycles

SEA - SMOKE DETECTOR IN AFT CARGO COMPARTMENT FOUND TO HAVE RED WARNING LIGHT ILLUMINATED. NO SIGN OF SMOKE OR FIRE. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,584 hrs · 37,108 cycles

GEG - THE OVERHEAD EXIT SIGN, MID CABIN WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,437 hrs · 36,960 cycles

SEA- CENTER OVERHEAD EXIT LIGHT FOUND TO HAVE INOPERATIVE LIGHTS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (GALLEY) · airframe 30,200 hrs · 36,752 cycles

PDX - EMERGENCY EXIT SIGN IN GALLEY INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — LEAKING (AFT) · airframe 30,008 hrs · 36,591 cycles

SEA - THE SMOKE ALARM IN THE LAVATORY SOUNDED, IT RESET ITSELF AND NO FUMES OR SMOKE WERE NOTED. UPON INSPECTION, FOUND APU OIL SEAL LEAKING, ALLOWING OIL CONTAMINATION VIA THE BLEED AIR SYSTEM. PLACED APU ON DEFERRED MAINTENANCE LIST AND REPLACED AIR CONDITIONING WATER SEPARATOR SOCKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,646 hrs · 36,241 cycles

SEA - DURING CLIMB, NOTED OIL SMELL COMING FROM AIR CONDITIONING VENTS. CLEANED AIR CONDITIONING DRAIN LINES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 29,026 hrs · 35,648 cycles

PDX- EMERGENCY EXIT SIGN ABOVE FORWARD GALLEY IS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHTING CIRCUIT BOARD ABOVE GALLEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (ROW 9) · airframe 28,908 hrs · 35,530 cycles

SEA- EMERGENCY EXIT SIGN AT ROW 9 HAS LIGHT OUT. REPLACED EMERGENCY EXIT SIGN CIRCUIT BOARD AT ROW 9. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 28,881 hrs · 35,502 cycles

BOI- EXIT SIGN LIGHTS ABOVE COCKPIT DOOR INOPERATIVE. REPLACED CIRCUIT BOARD ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 28,825 hrs · 35,447 cycles

BOI- RIGHT HAND AFT EXTERIOR EVACUATION LIGHT WILL NOT EXTINGUISH. REPLACED LIGHT POWER SUPPLY. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: HARNESS — CHAFED (NR 2 ENGINE) · airframe 28,675 hrs · 35,303 cycles

SEA - DESCENDING THROUGH 24000 FEET, THE NR 2 FIRE WARNING LIGHTS AND AUDIBLE ALARM ACTIVATED FOR APPROXIMATELY 3 SECONDS, THEN QUIT. THIS OCCURED 3 TIMES. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. TEST OF SYSTEM WAS NORMAL. INSPECTED FIRE LOOP. FOUND CHAFED FLEX HARNESS. REMOVED AND REPLACED FLEX HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

BOI - AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN)

PDX - FOWARD CABIN EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK GOOD.

Part: RADAR INDICATOR — INOPERATIVE (COCKPIT)

SEA - ELECTRICAL BURNING SMELL IN COCKPIT. NO VISABLE SMOKE. FOUND WEATHER RADAR CONTAMINATED WITH WATER. RESEALED WINDSHIELD POST AND REPLACED WEATHER INDICATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRUIT BOARD — FAILED (EMER EXIT)

PDX- CENTER CABIN OVERHEAD EMERGENCY SIGN LIGHTS ARE DIM. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY SIGN CIRCUIT BOARDS, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (PAX DOOR)

PDX - MAIN CABIN DOOR HEADER BEAM IS CRACKED AT FORWARD END AT FRAME 3450. REPAIRED IAW HORIZON AIR EA 4-53-879.

Part: SKIN — MISREPAIRED (LT WING)

PDX - LEFT-HAND WING INBOARD FUEL PANEL MOUNTING FLANGE HAS A SAND THROUGH OPENING IN THE SKIN THAT MATES THE FUEL PANEL. REPAIRED IAW HORIZON AIR EA 4-57-311.

Part: SKIN — CORRODED (FUSELAGE)

PDX - NAV COMM LOWER FUSELAGE SKIN HAS CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-868.

Part: SKIN — CRACKED (FUSELAGE)

PDX - SKIN UNDER LOWER COMM ANTENNA IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-868.

Part: BRACKET — CRACKED (SPEED BRAKE)

PDX - CRACK IN LIGHTENING HOLE SPEED BRAKE SUPPORT BRACKET, FORWARD RIGHT-HAND SIDE. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 10, FIGURE 8.

Part: BEAM — CRACKED (FUSELAGE)

PDX - BEAM V HAS A CRACK ALONG UPPER ROW OF RIVETS AT BLL 0 CL. REPAIRED IAW HORIZON AIR EA 4-53-849.

Part: FRAME — DAMAGED (CARGO DOORWAY)

PDX - AFT CARGO DOOR APERTURE FORWARD FRAME HAS DENT WITH DEEP GOUGES AT BL 700R AFT OF STRINGER 67. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.

Part: BEAM — DAMAGED (FUSELAGE)

PDX - UPPER FLANGE ON HORIZONTAL BEAM I DAMAGED DURING RIVET INSTALLATION AT BL 425R, NEXT TO UPPER CONSOLE. REPAIRED IAW 53-02-18, PAGE 36, FIGURE 13, SECTION B-B.

Part: FRAME — CRACKED (FUSELAGE)

PDX - RIGHT-HAND FRAME 67-2 IS CRACKED PAST STOP DRILL AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-10-05.

Part: SKIN — CANNING (CARGO DOOR)

PDX - CENTER CARGO DOOR INNER SKIN IS OIL CANNING AT LOWER END IN CENTER. REPAIRED IAW HORIZON AIR EA 4-52-262.

Part: CLIP — CRACKED (FRAME 5805)

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

Part: STRINGER — CRACKED (FRAME 13815)

PDX - STRINGER 35 CRACKED AT INSULATION RETAINER HOLE, CRACK IS 2 AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1, SRM 51-31-01 AND SRM 51-10-4, PARAGRAPH 4B.

Part: RIB — CRACKED (WING)

PDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.05. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6.

Part: RIB — CRACKED (WING)

PDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.04. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6.

Part: JAMB — GOUGED (RT EMER EXIT)

PDX - RIGHT-HAND AFT EMERGENCY EXIT APERTURE TOP TORSION BOX COVER HAS TWO GOUGE MARKS CAUSED BY SCREWS FROM EMERGENCY EXIT. REPAIRED IAW HORIZON AIR EA 4-53-856.

Part: CLIP — CRACKED (FRAME 10966)

PDX - FRAME CLIP CRACKED AT FRAME 10966 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - FRAME CLIP CRACKED AT 5805 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

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

Part: CLIP — CRACKED (FRAME 13345)

PDX - FRAME CLIP CRACKED AT FRAME 13345 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B-C.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815 AND STRINGER 40. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B-C AND SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-02, PAGE 10 PARAGRAPH C.

Part: CLIP — CRACKED (FRAME 13815)

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

Part: CLIP — CRACKED (FRAME 13815)

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

Part: CLIP — CRACKED (FRAME 13815)

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

Part: CLIP — CRACKED (FRAME 12875)

PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, 1-2-3-4-5.

Part: FRAME — CORRODED (FRAME 9305)

PDX - FORWARD CARGO COMPARTMENT FRAME 9305A HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 357)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT STATION 357. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A AND HORIZON AIR EA 4-53-864.

Part: CLIP — CRACKED (FRAME 12875)

PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3-4-5.

Part: CLIP — CRACKED (FRAME 12875)

PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12875)

PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3-4-5.

Part: FRAME — CORRODED (FRAME 9305)

PDX - FORWARD CARGO COMPARTMENT FRAME 9305 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-852.

Part: FRAME — CORRODED (FRAME 8305)

PDX - FORWARD CARGO COMPARTMENT FRAME 8305 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW HORIZON AIR EA 4-53-858.

Part: SKIN — DENTED (CARGO DOOR)

PDX - FORWARD CARGO DOOR INNER SKIN BULGED AND DENTED FROM LOWER EDGE UP EIGHT INCHES. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 53-02-01.

Part: CLIP — CRACKED (FRAME 12875)

PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3-4-5.

Part: CLIP — CRACKED (FRAME 13815)

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

Part: CLIP — CRACKED (FRAME 10346)

PDX - FRAME CLIP CRACKED AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: FRAME — CORRODED (FRAME 7805)

PDX - FORWARD CARGO COMPARTMENT FRAME 7805 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.

Part: CASTELLATION — CRACKED (FRAME 16060)

PDX - AFT CARGO PIT FRAME 16060 HAS A CRACK IN THE CASTELLATION AT STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 16060)

PDX - CLIP CRACKED AT FRAME 16060 AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815B AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — GOUGED (BS 481)

PDX - RIGHT-HAND INBOARD SEAT TRACK INBOARD FLANGE HAS A GOUGE MARK AT STATION 481. REPAIRED IAW HORIZON AIR EA 4-58-861, STEPS 1 THROUGH 3.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (BS 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: FRAME — FRACKED (FRAME 7805)

PDX - FRAME CRACKED AT 7805 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - FRAME CLIP CRACKED AT FRAME 13815B AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7B.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - FRAME CLIP CRACKED AT 6305 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - FRAME CLIP CRACKED AT 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 14755)

PDX - FRAME CLIP CRACKED AT FRAME 14755 AND STRINGER 39. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 14205)

PDX - FRAME CLIP CRACKED AT FRAME 14205 AND STRINGER 20. REPAIRED IAW FOKKER 51-31-01, PAGE 13, PARAGRAPH 7B.

Part: CLIP — CRACKED (FRAME 14755)

PDX - FRAME CLIP CRACKED AT FRAME 14755 AND STRINGER 27. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7B.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

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

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: UNKNOWN

PDX - FRAME CLIP CRACKED AT R4QME 9305A AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: UNKNOWN

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5803)

PDX - FRAME CLIP CRACKED AT FRAME 5803 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3, SRM 51-11-01.

Part: CLIP — CRACKED (FRAME 5805)

PDX - FRAME CLIP CRACKED AT 5805 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 53-01-00, PARAGRAPH 3.

Part: CLIP — CRACKED (FRAME 5805)

PDX - FRAME CLIP CRACKED AT FRAME 5805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3 AND SRM 51-11-01.

Part: CLIP — CRACKED (FRAME 5305)

PDX - FRAME CLIP CRACKED AT FRAME 5305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3, AND SRM 51-11-01.

Part: CLIP — CRACKED (FRAME 6805)

PDX - FRAME CLIP CRACKED AT 6805 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: SEAT TRACK — GOUGED (BS 567)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 567. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 572)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 572. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 8305)

PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3 AND SRM 51-11-01.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-01.

Part: SEAT TRACK — GOUGED (BS 588)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 588. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

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

Part: SEAT TRACK — CORRODED (BS 588)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 588. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-01.

Part: CLIP — CRACKED (BS 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 25, REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 21. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — GOUGED (BS 530)

PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGED AT STATION 530. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 647)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 647. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 618)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 618. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 639)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 639. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 603)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 603. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — GOUGED (BS 480)

PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 480. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 610)

PDX - RIGHT HAND OUTBOARD SEAT TRACK GOUGED AT STATION 610. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 601)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 601. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 8305)

PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3 AND SRM 51-11-01.

Part: SEAT TRACK — GOUGED (BS 590)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK GOUGED AT STATION 590. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 BELOW STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — GOUGED (BS 659)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 659. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 580)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 580. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 639)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 639. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: SEAT TRACK — GOUGED (BS 498)

PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGED AT STATION 498. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 ABOVE STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 8305)

PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAPH 3 AND SRM 51-11-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 20. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — GOUGED (BS 593)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK GOUGED AT STATION 593. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C.

Part: CLIP — CRACKED (FRAME 12405)

PDX - FRAME CLIP CRACKED AT FRAME 12405 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: FRAME — GOUGED (FRAME 16060)

PDX - FUSELAGE FRAME 16060 HAS GOUGE MARKS ON FRAME CAP BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, 3C, NR 4.

Part: SKIN — GOUGED (FRAME 16660)

PDX - FUSELAGE INTERIOR SKIN HAS GOUGE MARKS STARTING 3 FORWARD OF FRAME 16660 BETWEEN STRINGERS 32 AND 33. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, 3C, NR 4.

Part: CLIP — CRACKED (FRAME 12405)

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

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SEAT TRACK — GOUGED (BS 548)

PDX - LEFT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 548. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B, C.

Part: SKIN — CORRODED (WING)

PDX - FUEL PANEL 73D HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME CLIP CRACKED AT FRAME 9305B AND STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — CORRODED (RT WING)

PDX - FUEL PANEL 74C MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A.

Part: UNKNOWN

PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — CORRODED (RT WING)

PDX - FUEL PANEL 72A MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A.

Part: SKIN — CORRODED (WING)

PDX - FUEL PANEL 71A HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SKIN — CORRODED (WING)

PDX - FUEL TANK 73C SURROUND OPENING HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (WING)

PDX - FUEL TANK 73D SURROUND OPENING HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: CLIP — CRACKED (FRAME 15205)

PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SKIN — CORRODED (RT WING)

PDX - FUEL PANEL 74B MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A.

Part: SKIN — CORRODED (WING)

PDX - FUEL PANEL 73A HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-04.

Part: FLOORBEAM — DIRTY (FRAME 4900)

PDX - RIGHT-HAND FLOORBEAM 1127 REQUIRES CLEANING IN THE AREA OF FRAME 4900. CLEANED AREA AS REQUIRED.

Part: POST — CRACKED (CABIN)

PDX - LEFT-HAND NR 2 WINDOW POST LOWER STRUCTURE HAS A BRACKET THAT IS CRACKED THROUGH TWO RIVETS. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3-4-5.

Part: SKIN — CORRODED (RT WING)

PDX - FUEL PANEL 74A MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A.

Part: SKIN — CORRODED (WING)

PDX - FUEL TANK SURROUND OPENING 71A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (WING)

PDX - FUEL PANEL 73C HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (RT WING)

PDX - FUEL PANEL 74D MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 8-9, PARAGRAPH 4A.

Part: SKIN — CORRODED (WING)

PDX - FUEL PANEL 73B HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (WING)

PDX - FUEL TANK SURROUND OPENING 73B HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (WING)

PDX - FUEL TANK SURROUND OPENING 73A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.

Part: LIGHT — INOPERATIVE (CABIN)

GEG - FORWARD CABIN EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE SIGN. OPERATIONAL TEST PERFORMED, RESULT WAS NORMAL.

Part: APU — INOPERATIVE (APU COMPT)

PDX - LAVATORY SMOKE DETECTOR WENT OFF IN FLIGHT. AIRCRAFT RETURNED TO FIELD. FOUND EVIDENCE OF OIL IN APU DUCT. REMOVED AND REPLACED APU AND COMPLIED WITH THE BLEED AIR SYSTEM BLOWOUT MAINTENANCE TASK CARD. OPERATIONAL CHECK GOOD.

Part: PACK — INOPERATIVE (NR 1)

SEA - AFTER TAKEOFF, SMOKE DETECTOR IN LAVATORY SOUNDED. FLIGHT ATTENDANT OBSERVED A LIGHT HAZE IN CABIN. AFTER 4 MINUTES THE SMOKE DETECTOR STOPPED, HAZE DISAPPEARED. AFTER LANDING, GROUND RUN AIRCRAFT AT POWER, CYCLED NR 1 PACK, NOTICED ACRID SMELL. WITH NR 1 OFF, NO ACRID SMELL. PLACED NR 1 PACK ON MEL. AT BOI, REMOVED AND REPLACED NR 1 PACK. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAV)

SEA - LAV SMOKE DETECTOR SOUNDS INTERMITTENT ALARMS. MAINTENANCE PLACED ON MEL. REMOVED AND REPLACED SMOKE DETECTOR IN LAVATORY, OPERATIONAL CHECK NORMAL. CLEARED MEL.

Part: CONNECTOR — DISCONNECTED (ROW 4B)

GEG- EVACUATION LIGHT AT SEAT 4B IS INOPERATIVE. FOUND ELECTRICAL CONNECTOR WAS DISCONNECTED. RECONNECTED THE CONNECTOR AND THE LIGHT OPERATED NORMAL.

Part: BATTERY PACK — DISCHARGED (ROW 1)

BOI - WHEN POWER IS REMOVED FROM AIRCRAFT THE EMERGENCY AISLE LIGHTS IN ROWS 1 TO 5 REMAIN ON. MAINTENANCE REPLACED THE ROW 1 BATTERY PACK, OPERATIONAL CHECK NORMAL.

Part: LIGHT — BROKEN (ROW 12)

BOI - SEAT MOUNTED EMERGENCY EXIT SIGN AT ROW 12 IS BROKEN. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 12. OPERATIONAL CHECK PERFORMED, NORMAL OPERATION RESTORED.

Part: POWER SUPPLY — INOP (CABIN)

MAINTENANCE REPORTS FORWARD EMERGENCY POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED SAME, OPERATIONAL TEST SHOWS NORMAL FUNCTION.

Part: BULB — FAILED (ROW 9E)

EXIT LIGHT AT ROW 9E IS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST WAS NORMAL.

Part: BALLAST — FAILED (COCKPIT)

ACRID SMELL OF BALLAST IN CAPTAINS SIDE OF FLIGHT DECK. REPLACED BALLAST TRANSFORMER, OPERATIONAL CHECK GOOD.

Part: COALESCER BAG — CONTAMINATED (COCKPIT)

COCKPIT PACK SMELLS WHEN HEAT IS DEMANDED. REPLACED WATER SOCK IAW MM 21-70-00, OPERATIONAL CHECK GOOD.

Part: CIRCUIT BOARD — FAILED (CABIN)

FORWARD EMERGENCY EXIT SIGN ABOVE CENTER AISLE AT ROW 8 HAS SEVERAL 28V EMERGENCY BULBS OUT. MAINTENANCE REMOVED AND REPLACED THE CIRCUIT BOARD, OPERATIONAL TEST IS NORMAL.

Part: BULB — FAILED (CABIN)

TWO EVENTS OF THE EMERGENCY EXIT LIGHT AT ROW 8CDE REPORTED BURNT OUT. IN BOTH CASES MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. RESULTS WERE NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - BOTH OVERWING EXIT EVACUATION LIGHTS ON RIGHT HAND SIDE ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY AT ROW 8, OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

PDX - SOME LIGHTS OUT ON CENTER AISLE EXIT SIGN. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

SEA - LIGHT INOPERATIVE IN AISLE OVERHEAD EMERGENCY EXIT SIGN. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

PDX - EXIT LIGHTS BURNT OUT IN EXIT SIGN ON CEILING BETWEEN ROWS 8 AND 9. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

BOI - FORWARD CABIN EMERGENCY LIGHT IS DIM. MAINTENANCE RELAMPED SEVERAL LIGHT BULBS AND OPERATIONALLY TESTED. TESTS NORMAL.

Part: BULB — FAILED (CABIN)

OVERHEAD EMERGENCY LIGHT IS INOPERATIVE, OVER ROW 4. MAINTENANCE RELAMPED, OPERATIONAL TEST IS NORMAL.

Part: LIGHT — BROKEN (CABIN)

A 3 VOLT EXIT SIGN ON SEAT 9B IS BROKEN. MAINTENANCE INSTALLED A NEW SIGN ASSEMBLY ON SEAT 9B, OPERATIONAL TESTS ARE NORMAL.

Part: BULB — FAILED (CABIN)

AISLE EVACUATION LIGHT AT SEAT 6 IS INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL.

Part: COVER — LOOSE (CABIN)

EMERGENCY EXIT LIGHT COVER AT ROW 9 NEEDS TO BE SAFETY WIRED. MAINTENANCE APPLIED BRAKE AWAY WIRE TO COVER OVER EXIT HANDLE AT ROW 9.

Part: CIRCUIT PANNEL — FAILED (CABIN)

GEG - FORWARD FACING EXIT SIGN HAS BULBS BURNT OUT. MAINTENANCE REPLACED THE LAMP CIRCUIT PANEL, TESTS GOOD.

Part: CONNECTION — LOOSE (CABIN)

SEAT EVACUATION LIGHTS ON FRONT 6 ROWS ARE ON WITH THE EMERGENCY LIGHT SWITCH IN ARM POSITION. MAINTENANCE INSPECTED AND FOUND LOOSE CONNECTION AT SEAT ROW 1AB. SECURED CONNECTION, OPERATIONAL TEST IS GOOD.

Part: SIGN — INOPERATIVE (CABIN)

EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED EXIT LIGHT ASSEMBLY, OPERATIONAL TEST IS GOOD.

Part: BULB — FAILED (CABIN)

EXIT SIGN AT SEAT 9A INOP. RELAMPED, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT SIGN AT CENTER CABIN IS INOP. REPLACED LAMPS, OPERATIONAL CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN)

OVERHEAD EMERGENCY EXIT SIGN ABOVE AISLE ROW 8 IS ONLY PARTIALLY ILLUMINATED. REPLACED EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

GEG - EMERGENCY EXIT SIGN ROW 8A IS INOP. RELAMPED, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

SEA - FLOOR PROXIMITY LIGHTS IN ROWS 1 THROUGH 6 SEATS A/B ARE ILLUMINATED INFLIGHT AND ON GROUND. REPAIRED BROKEN WIRE AT SEAT 6, OPERATIONAL CHECK GOOD. NO PARTS REPLACED.

Part: LIGHT — MALFUNCTIONED (CABIN)

YEG - FLOOR PROXIMITY LIGHTS IN ROWS 1 THROUGH 6 ILLUMINATED. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK GOOD. NO PARTS REPLACED, SYSTEM FOUND SERVICEABLE.

Part: SWITCH — OUT OF ADJUST (RT MLG)

BOI - RIGHT MAIN LANDING GEAR RED LIGHT ILLUMINATED SHORTLY AFTER GEAR EXTENSION. FOUND SAFE FOR FERRY FLIGHT FROM BOI TO PDX. IN PDX REPLACED RT MLG FWD UPLOCK SWITCH. OPERATIONAL CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (RT MLG DOOR)

PDX - RIGHT MAIN LANDING GEAR HAD 2 GREEN AND 1 RED LIGHT WHEN EXTENDED. CYCLED GEAR SEVERAL TIMES. ADJUSTED MLG DOOR SWITCH AND UPLOCK BRACKET. OPERATIONAL CHECK GOOD.

Part: SEAT TRACK — CORRODED (CABIN)

LEFT INBOARD SEAT TRACK BETWEEN FRAMES 13815A-13815B HAD CORROSION REMOVED AND IS OUT OF LIMITS. REPAIRED IAW FOKKER SRM 53-02-15 FIGURE 1 PAGE 1, 2 AND 3.

Part: SEAT TRACKS — DAMAGED (CABIN)

REMOVE AND REPLACE SEAT TRACK BETWEEN FRAME 12405 AND FRAME 15635 IN REF WITH H/R 300/51, 300/56, 300/57 AND 300/61 LEFT HAND O/B SEAT TRACK. CUT OUT AND REMOVED SEAT TRACK, REPAIRED IAW FOKKER SRM 53-02-15 FIGURE 1 PAGE 1, 2 AND 3.

Part: FRAME — WORN (RUDDER)

PDX - NR 4 FROM TOP RUDDER COVE FRAME HAS ELONGATED RIVET HOLES. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8, FIGURE 4.

Part: FRAME — DAMAGED (RUDDER)

NR 2 FROM TOP RUDDER COVE FRAME HAS ELONGATED RIVET HOLES. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8, FIGURE 4.

Part: FRAME — MISREPAIRED (RUDDER)

BOTTOM RUDDER COVE FRAME AS UNAPPROVED REPAIR INSTALLED. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8, FIGURE 4.

Part: FRAME — DAMAGED (RUDDER)

NR 3 FROM TOP RUDDER COVE FRAME HAS ELONGATED RIVET HOLES. REPAIRED FRAME IAW FOKKER SRM 55-02-05 PAGE 8, FIGURE 4.

Part: CORNER FRAME — DENTED (CARGO DOOR)

PDX - AFT CARGO DOOR LOWER FORWARD CORNER DENTED AFT OF HINGE APPROXIMATELY .095 DEEP. INSTALLED CORNER FRAME SECTION IAW FOKKER SRM 51-31-01 AND 51-30-02 SEALED WITH PR1422B1/2.

Part: DOOR — CORRODED (CARGO COMPT)

PDX - AFT CARGO DOOR HAS WIDE SPREAD SURFACE CORROSION ON INTERNAL FRAMES AND INTERCOSTALS. REMOVED CORROSION FROM INTERNAL FRAMES AND INTERCOSTAL AS MARKED. TREATED WITH ACID AND ALCOLINE IAW FOKKER SRM 51-10-04.

Part: SKIN — CORRODED (CARGO DOOR)

PDX - AFT CARGO DOOR INNER SKIN HAS SURFACE CORROSION ON INTERIOR. FABRICATED NEW SKIN, REPAIRED IAW EO 4-52-31.

Part: SKIN — DENTED (CARGO DOOR)

PDX - AFT CARGO DOOR LOWER AFT CORNER DENTED AFT OF HINGE APPROXIMATELY .120 DEEP. REPAIRED IAW F-28 SRM 51-31-01.

Part: SKIN — DENTED (FUSELAGE)

PDX - REAR FUSELAGE SKIN DENTED WITH SHARP CREASE AT STRINGER 53 FORWARD OF FRAME 41-2. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FOKKER SRM 53-02-01, FIGURE 4.

Part: STRINGER — DAMAGED (CARGO COMPT)

PDX - FORWARD CARGO BAY STRINGER 73 IS HEAVILY DAMAGED JUST FORWARD OF FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06.

Part: SKIN — DENTED (FUSELAGE)

PDX - REAR FUSELAGE SKIN DENTED AT STRINGER 10 BETWEEN FRAMES 22840 AND 22293 .075 DEEP. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1.

Part: ANGLE — CRACKED (VERT STAB)

PDX - CRACKS LOCATED ON THE RIGHT CONNECTION ANGLE IN THE RADIUS AND THROUGH UPPER RIVETS ADJACENT TO 16 PERCENT FRONT SPAR. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.

Part: CLIP — CRACKED (FRAME 50-2)

PDX - TWO CRACKS IN CLIP REPAIR PATCH LOCATED AT FRAME 50-2 AT STRINGER 46 AND 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5.

Part: FRAME — CRACKED (FUSELAGE)

PDX - FRAME 22293 CRACKED LOCATED BETWEEN STRINGERS 53A AND 54. REPAIRED IAW EA 4-53-267.

Part: FRAME — CRACKED (FRAME 50-2)

PDX - CRACK EXTENDING FROM STOP DRILL HOLE OF CRACK IN FRAME 50-2, STRINGER 26. CRACK OUT OF LIMITS IAW HA CARD 4-578, PAGE 3. FABRICATED A NEW DOULBER. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8.

Part: CLIP — CRACKED (FRAME 41-25)

PDX - MULTIPLE CRACKS AND STOP DRILLS AT FRAME 41-25 STRINGER 45 CLIP OUT OF LIMITS. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 6.

Part: CLIP — CRACKED (FRAME 32-2)

PDX - CRACK IN CLIP AT FRAME 32-2 STRINGER 22. CRACK LENGTH AND LOCATION WITHIN LIMITS IAW HA CARD 4-578 PAGE 4 REQUIRES STOP DRILL ON CRACK TO PREVENT FURTHER CRACKING. STOP DRILLED CRACK IAW FOKKER SRM 53-01-01, PARAGRAPH 5 B4.

Part: FRAME — CRACKED (FRAME 32-2)

PDX - CRACK EXTENDING FROM STOP DRILL HOLE LOCATED AT FRAME 32-2 STRINGER 52. FABRICATED AND INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13, PAGE 5.

Part: CLIP — CRACKED (FUSELAGE)

CRACK IN CLIP AT FRAME 32-2 STRINGER 27. CRACK LENTH AND LOCATION OUT OF LIMITS. INSTALLED CLIPS (X2) IAW FOKKER SRM 53-02-13, PAGE 5.

Part: CLIP — CRACKED (FRAME 16-2)

PDX - CRACK IN CLIPS AT FRAME 16-2 STRINGERS 23 AND 26. CRACK LENGTH AND LOCATION WITHIN LIMITS. STOP DRILLED CRACK IAW FOKKER SRM 53-01-01, PARAGRAPH 5B4.

Part: RIB — CRACKED (RUDDER)

PDX - RIB NR 7 AT RUDDER STA 2001 BELOW CENTER HINGE POSITION HAS CRACKS RADIATING ALONG THE ATTACH CLIPS RT AND LT. STOP DRILLED CRACKS IAW EA 4-55-30.

Part: CLIP — CRACKED (FUSELAGE)

CRACKED CLIP AT FRAME 16660 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CRACK IN CLIP AT FRAME 13815E BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.

Part: STRINGER — DENTED (FUSELAGE)

PDX - DENT AT FRAME 14755 OF STRINGER 6. REPAIRED IAW FOKKER SRM 53-02-12 FIGURE 2.

Part: SKIN — DENTED (CARGO DOOR)

PDX - DENTS FROM IMPACT DAMAGE ON AFT CARGO DOOR, AFT LOWER EDGE. REPAIRED IAW FOKKER SRM 53-02-16, FIGURE 2, PAGE 4.

Part: ANGLE — CRACKED (BS 4150)

MIDSPAN TO FLOORBEAM CONNECTION ANGLES (LT) AND (RT) SIDE AT STATION 4150 BL 600L WL 560 ARE CRACKED. FABRICATED ANGLES IAW FOKKER SRM 51-11-07 AND 51-10-05.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGER 72473. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 PAGE 4.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CRACK IN CLIP AT FRAME 13815B BETWEEN STRINGER 72 AND 73. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.

Part: SKIN — CRACKED (FUSELAGE)

OVERWING DOOR HAS CRACK ON THE SKIN OF THE UPP LEFTHAND CORNER ADJACENT TO THE APATURE DOOR JAME JOGGLE, ONE INCH LONG. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5, FIGURE 3.

Part: BRACKET — CRACKED (CARGO DOOR)

PDX - CRACKS AT CARGO DOOR ROD ATTACH BRACKET. REPAIRED IAW FOKKER SRM 53-02-16.

Part: BEAM — CRACKED (FUSELAGE)

PDX - CRACK ON LOWER SIDE OF BEAM III. REPAIRED IAW FOKKER SRM 53-02-18 FIGURE 13.

Part: CLIP — CRACKED (FRAME 50-2)

PDX - CRACK EXTENDING FROM STOP DRILL HOLE OF CRACK IN FRAME 50-2 CLIP AT STRINGER 25. CRACK OUT OF LIMITS IAW HA CARD 4-578, PAGE 3, REQUIRES REPAIR. FABRICATED A NEW DOUBLER. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8.

Part: APU — FAILED (TAIL)

CLT/TRI - FLT 873 - AFTER TAKEOFF FROM CLT, THE CREW NOTICED A SMOKE SMELL IN BOTH THE COCKPIT AND THE CABIN. THE SMOKE DETECTOR IN THE AFT LAVATORY ACTIVATED. THE FLIGHT RETURNED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED THE SMOKE WAS DUE TO OIL FROM THE APU. THEY REPLACED THE APU. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PIT - MAINTENANCE FOUND AFT EXTERIOR BODY FAIRING EVACUATION LIGHTS STAY ON AT ALL TIMES WITH POWER OFF. THIS CONDITION WAS FOUND ON A ROUTINE OVERNIGHT MAINTENANCE CHECK. REPLACED EXTERIOR EVACUATION LIGHTS BATTERY POWER SUPPLY. (M)

Part: FUEL NOZZLE — BURNED (LT ENGINE)

CLT - FLT 464 - AFTER TAKEOFF, THE NR 1 ENGINE WOULD NOT ADVANCE TO FULL THROTTLE AFTER REACHING 8000 FEET. ENGINE SURGED AFTER 8000 FEET. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED A BORESCOPE ON THE ENGINE. SEVERAL FUEL NOZZLES WERE COKED AND ONE BURNED THROUGH. ENGINE WAS REPLACED. (M)

Part: WEB — CRACKED (BS 2220-3040)

PIT - DURING SCHEDULED STRUCTURAL VISIT (SIP), FOUND A 1.5 INCH CRACK IN WEB BETWEEN STATION 2220 AND 3050 AT BEND LINE ABOVE CONNECTION ANGLES. (VISUAL INSPECTION VERIFIED BY HFEC) SIP REF 53-10-19. INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 29. (M)

Part: GEN SHAFT — LEAKING (NR 1 ENGINE)

EVV - FLT 0689 - ON DESCENT TO EVV, CREW RECEIVED FLUCTUATING OIL PRESSURE ON THE NR 1 ENGINE THEN RECEIVED A CAWS WARNING. AN EMERGENCY WAS DECLARED. THE CREW SHUTDOWN THE NR 1 ENGINE. SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE REMOVED THE OIL FILTER AND SCREWS TO CHECK FOR MATERIAL. ALL CHECKED GOOD. THEY FOUND THE OIL LEAK TO BE COMING FROM THE GENERATOR. THE SHAFT AND SEAL ASSEMBLY WAS REPLACED. OPERATIONAL CHECKED NORMAL. (W)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK. OPERATIONS CHECKED GOOD. REFERENCE USAA950307.

Part: EEL ASSY — INOPERATIVE (CABIN)

CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK. OPERATIONS CHECKED GOOD. REFERENCE 95ZZZW525.

Part: RESERVOIR — LOW PRESSURE (HYD SYSTEM)

CLT - FLT 0366 - AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT. CAPTAIN WENT THROUGH PROPER PROCEDURES AND RECEIVED THREE GREEN DOWNLOCK LIGHTS. CREW DECIDED TO RETURN TO CLT. MAINTENANCE RECHARGED THE HYDRAULIC RESERVOIR PRESSURE. HYDRAULIC SYSTEM AND LANDING GEAR OPERATIONS CHECKED GOOD. (X)

Part: BOLT — MISSING (RT MLG DR ACT)

PIT - FLT 1197 - THE RT MLG GAVE AN USAFE INDICATION UPON LOWERING. CREW RECYCLED THE GEAR AND RECEIVED THREE GREEN LIGHTS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A MISSING BOLT IN THE RT FWD MAIN GEAR DOOR ACTUATOR. OPERATIONS CHECKED GOOD. (W)